Air Europa A332 Incident Report

ANEXO
Expte. Nº 342/14
ADVERTENCIA
El presente Informe es un documento técnico que refleja la opinión de la

JUNTA DE INVESTIGACIÓN DE ACCIDENTES DE AVIACIÓN CIVIL con relación a
las circunstancias en que se produjo el suceso, objeto de la investigación con sus
causas y con sus consecuencias.
De conformidad con lo señalado en el Anexo 13 al CONVENIO SOBRE

AVIACIÓN CIVIL INTERNACIONAL (Chicago /44) Ratificado por Ley 13.891 y en el
Artículo 185 del CÓDIGO AERONÁUTICO (Ley 17.285), esta investigación tiene un
carácter estrictamente técnico, no generando las conclusiones, presunción de culpas
o responsabilidades administrativas, civiles o penales sobre los hechos investigados.
La conducción de la investigación ha sido efectuada sin recurrir necesa-

riamente a procedimientos de prueba de tipo judicial, sino con el objetivo fundamen-
tal de prevenir futuros accidentes e incidentes.
Los resultados de esta investigación no condicionan ni prejuzgan los de

cualquier otra de índole administrativa o judicial que, en relación con el suceso, pu-
diera ser incoada con arreglo a leyes vigentes.
INFORME FINAL
INCIDENTE OCURRIDO EN: Aeropuerto Internacional Ezeiza -“Ministro Pistarini”,

provincia de Buenos Aires.
FECHA: 9 de septiembre de 2014. HORA (UTC): 11:00 h (aprox)
AERONAVE: Avión. MARCA: Airbus.
MODELO: A-330-202 MATRÍCULA: EC-JPF.
COMANDANTE, PRIMER OFICIAL y PILOTO DE REFUERZO: con licencia españo-

la de piloto transporte de línea aérea [ATPL(A)]
PROPIETARIO: Empresa de transporte aéreo regular internacional.
Nota: Todas las horas están expresadas en Tiempo Universal Coordinado (UTC),
que para el lugar del incidente corresponde al huso horario – 3.
1
1 INFORMACIÓN SOBRE LOS HECHOS
1.1 Reseña del vuelo
1.1.1 El día 8 de septiembre de 2014, a las 21:55 h, la aeronave A-330-202,

matrícula EC-JPF, despegó del Aeropuerto Internacional de Barajas (LEMD), en Ma-
drid, Reino de España, con trece tripulantes y 259 pasajeros, con destino al Aero-
puerto Internacional de Ezeiza (SAEZ), República Argentina.
1.1.2 Luego de volar 12:30 h aproximadamente, el piloto al mando inició el des-

censo para la aproximación final a unas 120 NM del VOR EZE desde el nivel de vue-
lo (FL) 380.
1.1.3 Durante la fase de descenso, mientras se encontraba entre los niveles FL

260 y FL 150, ingresó en una zona de tormentas percibiendo que el avión era impac-
tado por granizo y sometido a una fuerte turbulencia asociada a las condiciones me-
teorológicas.
1.1.4 Producto del impacto de granizo, ambos parabrisas resultaron dañados

no detectándose, en ese momento, otro tipo de daños.
1.1.5 El comandante del vuelo decidió no declararse en emergencia pero solici-

tó la prioridad para el aterrizaje, informando la condición correspondiente a la torre
de Ezeiza la que, no obstante, alertó los servicios concurrentes correspondientes.
1.1.6 El aterrizaje y posterior rodaje a la posición de estacionamiento se efec-

tuaron sin novedad.
1.1.7 Una vez en la posición final de estacionamiento se pudo observar que la

aeronave presentaba otros daños.
1.1.8 El incidente ocurrió de día y en condiciones de vuelo IMC (condiciones

meteorológicas instrumentales).
1.1.9 La notificación del suceso fue realizada por personal de la oficina

ARO/AIS Ezeiza.
1.2 Lesiones a personas
Lesiones Tripulantes Pasajeros Otros

Mortales ---- ---- ----
Graves ---- ---- ----
Leves ---- ---- ----
Ninguna 13 259 ----
1.3 Daños en la aeronave
1.3.1 Célula: Daños en ambos parabrisas frontales, afectando la superficie ex-

terna, inutilizándolos. La cubierta exterior del radome resultó perforada en el cono,
así mismo también se observaron daños en los carenados de cubierta de uniones
2
ANEXO
ala fuselaje, y daños en una compuerta de acceso al pack de aire acondicionado de-
recho. Dos tubos pitot con ligeros daños. En el ala izquierda se encontró la cobertura
del faro de aterrizaje izquierdo rajado y dos paneles de intradós afectados por los
golpes del granizo. En el ala derecha se encontraron daños en paneles de intradós,
en el flight spoiler número 4, como así también en el slat número 1 derecho. En los
estabilizadores horizontales se encontraron pequeños golpes de ambos bordes de
salida.
1.3.2 Motores: los carenados de pilones de sujeción de ambos motores sufrie-

ron daños leves causados por algunos impactos de granizo. El motor izquierdo sufrió
ligeros daños en los álabes de fan, los cuales se encontraban dentro de tolerancia.
También se hallaron dos álabes de guía de salida afectados, los cuales estaban den-
tro de los parámetros permitidos por el manual de mantenimiento. El motor derecho
sufrió daños en dos álabes de la primera etapa del compresor y en nueve álabes
guía de salida.
1.4 Otros daños
No hubo.
1.5 Información sobre el personal.
1.5.1 Piloto
De 55 años de edad, de nacionalidad española, era titular de la licencia

piloto transporte de línea aérea avión, con habilitaciones para: “Airbus A330/IR (A).”
De acuerdo con lo informado por la Comisión de Investigación de Acci-

dentes e Incidentes de Aviación Civil (CIAIAC) del Reino de España, el certificado de
aptitud psicofisiológica estaba vigente hasta el 6 de septiembre de 2015, con la limi-
tación de tener disponible lentes correctores para visión cercana y llevar un par de
repuesto.
La cantidad de horas de vuelo, al momento del incidente, eran las siguien-

tes:
Total de horas de vuelo: 17719:00 h

Últimos 90 días: 203:23 h
Últimas 24 horas: 13:12 h
En el tipo de aeronave: 2559:00 h
1.5.2 Primer oficial

piloto transporte de línea aérea avión, con habilitaciones para: “Airbus A330/IR (A).”
3
De acuerdo con lo informado por la CIAIAC, el certificado de aptitud psico-
fisiológica, estaba vigente hasta el 16 de enero de 2015, con la limitación de tener
disponible lentes correctores para visión cercana y llevar un par de repuesto.

tes:

1.5.3 Piloto de refuerzo

piloto transporte de línea aérea avión, con habilitaciones para: “Airbus A330/A320/IR
(A)”.
De acuerdo con lo informado por la CIAIAC, el certificado de aptitud psico-

fisiológica estaba vigente hasta el 18 de febrero de 2015, con la limitación de tener
que llevar lentes correctoras multifocales.

tes:

1.6 Información sobre la aeronave
1.6.1 Información general
Aeronave fabricada por Airbus Industries, modelo A330-202, con número

de serie 733, de construcción mixta (materiales compuestos y metálicos), semimo-
nocasco, de fuselaje ancho, monoplano de ala baja, bimotor a reacción, con tren de
aterrizaje tipo triciclo retráctil.
1.6.2 Célula
Plan de mantenimiento por aeronavegabilidad continuada conforme al

manual de mantenimiento del fabricante teniendo al iniciar su vuelo LEMD-SAEZ un
total general (TG) de 46132:55 h y total de ciclos (TC) de 6215 ciclos (datos obteni-
dos del sistema electrónico de la empresa).
4
ANEXO
Su certificado de matrícula fue registrado a nombre de una empresa de

transporte aéreo regular internacional, con fecha de inscripción el 20 de octubre de
2011.
Su certificado de aeronavegabilidad fue emitido por la Delegación de Se-

guridad en Vuelo Nº 7 de la Dirección General de Aviación Civil de España el 28 de
marzo de 2006. Categoría: Avión grande. Sin fecha de vencimiento.
Los registros de mantenimiento indicaban que la aeronave estaba equi-

pada y mantenida de conformidad con la reglamentación y procedimientos vigentes
aprobados.
El combustible requerido y utilizado era JET A-1. Al momento del inciden-

te la aeronave disponía de 8281 litros de combustible.
1.6.3 Motores
Marca General Electric, modelo CF6-80E1A4, con número de serie

811486 el motor izquierdo y 811361 el motor derecho, ambos de 66870 lb de empu-
je. El mantenimiento se llevaba a cabo de acuerdo con las instrucciones de aerona-
vegabilidad continuada del fabricante, teniendo al iniciar el vuelo MAD-EZE un TG de
30882:02 h y un TC de 4159 ciclos el motor izquierdo y 44719:18 h y 5922 ciclos el
motor derecho.
1.6.4 Peso y balanceo de la aeronave
El peso máximo de despegue era de 233000 kg, el de aterrizaje era de

182000 kg, y el peso de vacío era de 121826 kg.
Los pesos calculados al momento del incidente eran los siguientes:
Vacío: 121826 kg.

Carga de pago: 26907 kg.
Combustible: 7800 kg.
Total al momento del suceso: 156533 kg.
Máximo de despegue (PMA): 182000 kg.
Diferencia: 25467 kg en menos respecto al PMA.
Los pesos y el centro de gravedad (CG) se encontraban dentro de la en-

volvente operacional de la aeronave.
1.7 Información meteorológica
1.7.1 De acuerdo a los datos aportados por el Servicio Meteorológico Nacional

(SMN), en las imágenes satelitales GOES-13 se apreciaba un sistema frontal frio so-
bre la región con abundante nubosidad convectiva organizada sobre la pendiente de
dicho sistema con movimiento hacia el NE. La temperatura de este sistema de nubes
con gran desarrollo vertical (convectivas) alcanzaba máximos puntuales entre -75ºC
5
y -80ºC. Los radares mostraban ecos compactos con desarrollos verticales que su-
peraban los 58 dBZ. También se encontraba una corriente en chorro al NW del sis-
tema con fuerte cortante vertical de viento.
1.7.2 En función de las apreciaciones anteriormente descriptas se puede inferir

que en la zona comprendida por los aeródromos (AD) SAOM-SAAR-SAAG-SUCA-
SUMU-SULS-SAAI-SADL-SAEZ-SADP-SABE-SADF-SAAJ-SAAR-SAOM, el sistema
nuboso generaba tormentas de moderada a fuerte intensidad, con precipitaciones in-
tensas y granizo entre FL100 y FL300, asociado a condiciones de turbulencia mode-
rada a severa y formación de hielo (engelamiento).
1.7.3 De acuerdo con la información disponible para la tripulación del World

Area Forecast System (WAFS) de Londres, carta de pronóstico de entorno de tiempo
fijo para el área OACI B SIGWX (Significant Weather Chart defined by ICAO) FL250-
630 válida 12 UTC 09 de septiembre 2014 las condiciones pronosticadas eran posi-
ble actividad de tormentas con cúmulos nimbos (CB) dispersos con bases por debajo
de FL 240 y topes pronosticados alcanzando el FL 360.
1.8 Ayuda a la navegación
El piloto efectuó la aproximación a la cabecera 11 de SAEZ. Contaba con

las frecuencias en uso del VOR EZE 116.5 e ILS EZE 110.1. Todas las ayudas a la
navegación se encontraban operables y la aproximación se desarrolló sin novedad.
1.9 Comunicaciones
1.9.1 Las comunicaciones con SAEZ se realizaron sin novedad.
1.9.2 El piloto no se declaró en emergencia, pero solicitó la prioridad para el

aterrizaje por encontrarse con ambos parabrisas rotos. No obstante el aeropuerto
SAEZ alertó los servicios concurrentes correspondientes.
1.10 Información sobre el lugar del incidente
El incidente tuvo lugar en la fase de descenso del vuelo AEA 041, aproxi-
madamente entre las 90 y 60 NM, radial 054º del VOR EZE, entre los niveles de vue-
lo FL260 y FL150.
1.11 Registradores de vuelo
1.11.1 La aeronave estaba equipada con un registrador de datos de vuelo (FDR)

y un registrador de voces de cabina (CVR).
a) FDR marca L3, P/N: 2100-4043-02, S/N: 000347014.
b) CVR marca L3, P/N: 2100-1020-02, S/N: 000346650.
1.11.2 La empresa explotadora puso a disposición los datos contenidos en el

FDR y envió los registros contenidos en el CVR para su análisis en esta JIAAC.
6
ANEXO
1.11.3 De la información contenida en el FDR pudo establecerse que el lugar

donde la aeronave fue afectada por el fenómeno meteorológico fue aproximadamen-
te entre las 90 y 60 NM, radial 054º del VOR EZE, entre los niveles de vuelo FL260 y
FL150.
1.12 Información sobre los restos de la aeronave y el impacto
La aeronave aterrizó en SAEZ con daños en ambos parabrisas frontales,

en el radome de la antena del radar, en el cristal del faro de aterrizaje izquierdo, en
los carenados de raíz de ala, los pilones de motores, en los álabes de fan y de la
guía de salida de ambos motores, producidos por impactos de granizo durante la fa-
se de descenso.
1.13 Información médica y patológica
De lo investigado surge que la condición psicofísica no tuvo injerencia en

el suceso.
1.14 Incendio
No hubo.
1.15 Supervivencia
1.15.1 Los tripulantes del EC-JPF y sus pasajeros desembarcaron la aeronave

en forma normal, por sus propios medios.
1.15.2 No hubo, en la aeronave, rol de evacuación de emergencia.
1.16 Ensayos e investigaciones
1.16.1 Se verificaron en la aeronave los daños sufridos en el incidente documen-

tándose los mismos mediante tomas fotográficas.
1.16.2 Del control de la documentación, se observa las novedades asentadas en

el RTV Nº 1568873 del día del incidente: Item Nº 1 “During descent due to turbulence
02 windshield cracked”; Item Nº 2 “After taxi-in reported several damaged by mainte-
nance in the fuselage.”
1.16.3 Se requirió al Jefe de Escala en SAEZ de la empresa operadora, docu-

mentación complementaria con informe de daños y trabajos realizados para la pues-
ta en servicio de la aeronave. Asimismo, se solicitó información del registro de pará-
metros obtenidos del FDR y del CVR.
1.17 Información orgánica y de dirección
La aeronave pertenece a una empresa de transporte aéreo regular inter-

nacional de pasajeros.
7
1.18 Información adicional
1.18.1 De acuerdo con la declaración de la tripulación, el radar de abordo de la

aeronave funcionaba correctamente.
1.18.2 En el Flight Crew Training Manual - A330/340, Suplementary Information –

Use of radar – Adverse weather (manual de instrucción de tripulaciones de vuelo –
A330/340, información suplementaria – uso del radar – meteorología adversa) se es-
tablecen los procedimientos de operación que permiten una operación con un ade-
cuado nivel de seguridad operacional en condiciones meteorológicas adversas.
1.18.3 El Proyecto de Informe Final (PIF) del incidente fue enviado a la “BEA
Bureau d'Enquêtes et d'Analyses pour la sécurité de l'aviation civile”, la junta
de investigación de accidentes de Francia, a fin que conjuntamente con el asesor del
representante acreditado (Airbus, fabricante de la aeronave), fuese evaluado y se
emitiese una opinión.
1.18.4 Las consideraciones enviadas por la BEA han sido tenidas en cuenta e in-
corporadas al informe. Dicho documento se encuentra como apéndice al informe, al
final del mismo.
1.19 Técnicas de investigaciones útiles o eficaces
Se realizaron las escuchas del registrador de voces de cabina (CVR).
2 ANÁLISIS
2.1 Aspectos operativos
2.1.1 Las licencias y los certificados de aptitud psicofisiológica de los pilotos es-
taban vigentes.
2.1.2 La tripulación del EC-JPF se encontraba realizando un vuelo regular inter-

nacional de transporte aéreo de pasajeros, programado por la empresa (AEA 041),
desde LEMD con destino SAEZ.
2.1.3 De acuerdo con los datos de pronóstico e imágenes satelitales disponi-

bles para la tripulación, las condiciones que afectaron el vuelo deberían haber sido
conocidas por la tripulación de vuelo y tendrían que haber sido objeto de atención de
manera específica, verificando la evolución de las condiciones meteorológicas.
2.1.4 Es probable que la penetración en el área de tormenta no haya sido pre-

cedida por el análisis de las condiciones meteorológicas reinantes, lo que no permitió
la utilización de los procedimientos establecidos para este tipo de operación destina-
da a minimizar la posibilidad de la ocurrencia de un suceso.
8
ANEXO
2.2 Aspectos Técnicos
De lo investigado no se identifican fallas técnicas o valores fuera de los

normales en los parámetros de funcionamiento de la aeronave al momento del inci-
dente, o previo a la ocurrencia del mismo.
3 CONCLUSIONES
3.1 Hechos definidos
3.1.1 La tripulación se encontraba realizando un vuelo programado de transpor-

te aéreo internacional regular de pasajeros.
3.1.2 La tripulación contaba con sus respectivas licencias y certificados de apti-
tud psicofisiológica vigentes.
3.1.3 Las defensas tecnológicas para estas situaciones, a saber, radar de abor-
do de la aeronave y radares de superficie del SMN, funcionaron correctamente y de
acuerdo con lo previsto.
3.1.4 La aeronave poseía certificados de matrícula y de aeronavegabilidad en

vigencia.
3.1.5 Los registros de mantenimiento indicaban que el mantenimiento se reali-

zaba de acuerdo a lo establecido por el fabricante de la aeronave y aprobados por la
firma explotadora.
3.1.6 El peso y el CG de la aeronave estaban dentro de los límites de la envol-

vente.
3.2 Conclusiones del análisis
Durante la fase de descenso de un vuelo comercial internacional regular,

ingreso de la aeronave en un área de tormentas, con importante actividad convecti-
va, granizo y turbulencia severa, resultando la aeronave con daños leves, debido a:
a) Programación del descenso en una zona con CB dispersos pronostica-

dos, sin el análisis adecuado.
b) No utilizar los recursos tecnológicos disponibles para la detección de la

actividad de desarrollo vertical, de acuerdo con la normativa vigente en la
empresa explotadora.
c) Inadecuada percepción del peligro meteorológico.
Condición latente causal probable:
9
Deficiencia en la empresa aérea para inducir las conductas operativas
comprometidas con la gestión de la seguridad operacional en las tripulaciones.
4 RECOMENDACIONES SOBRE SEGURIDAD
4.1 A la Comisión de Investigación de Accidentes de Incidentes de Aviación

Civil (CIAIAC) del Reino de España
Considere la necesidad de recomendar a la empresa explotadora adoptar

las medidas de instrucción y adiestramiento que fueran adecuadas para que los
pilotos que operen sus aeronaves adopten oportunamente las acciones adecuadas
para la operación en zonas donde las condiciones meteorológicas hagan prever
turbulencia severa y actividad de nubes de gran desarrollo vertical.
5 REQUERIMIENTOS ADICIONALES
Las personas físicas o jurídicas a quienes vayan dirigidas las recomenda-

ciones emitidas por la Junta de Investigación de Accidentes de Aviación Civil, debe-
rán informar a la AUTORIDAD AERONÁUTICA en un plazo no mayor a sesenta (60)
días hábiles, contados a partir que recibieran el Informe Final y la Resolución que lo
aprueba, el cumplimiento de las acciones que hayan sido puestas a su cargo (Dispo-
sición Nº 51/02 Comandante de Regiones Aéreas -19 JUL 02- publicada en el Bole-
tín Oficial del 23 de Julio 2002).
La mencionada información deberá ser dirigida a:
Administración Nacional de Aviación Civil (ANAC)

Av. Azopardo 1405, esquina Av. Juan de Garay
(C 1107 ADY) Ciudad Autónoma de Buenos Aires
ó a la dirección e-mail: “info@anac.gov.ar”
BUENOS AIRES,
10
AEA A330-202 EC-JPF (MSN0733)
Hailstorm in descent
09-Sep-2014
Airbus Report
Prepared by: Thomas LEPAGNOT
GSI 420.1022/15 (TL) 13-Feb-15 1/21

Introduction
The sole objective of this report is to prevent reoccurrence. It is not aimed to apportion blame
or liability.
This report has been compiled thanks to the information available at Airbus at the date of its
publication and could be updated should new information becomes available.
GSI 420.1022/15 (TL) 13-Feb-15 2/21

Synopsis
On September 9th, 2014 the Air Europa (AEA) A330 MSN0733 (EC-JPF) experienced a
severe hailstorm during descent to Buenos Aires (EZE). The aircraft suffered extensive
damage on windshield and radome and minor structural damage on pylon, wings and
horizontal stabilizer.
GSI 420.1022/15 (TL) 13-Feb-15 3/21

Table of contents:
1. FACTUAL INFORMATION 5
1.1 HISTORY OF THE FLIGHT 5
1.2 INJURIES TO PERSONS 6
1.3 DAMAGE TO AIRCRAFT 6
1.4 AIRCRAFT INFORMATION 7
1.5 METEOROLOGICAL INFORMATION 7
1.6 CAS MONITORING BY FMGEC AND FCPC 8
1.6.1 Monitoring 8
1.6.2 Consequence on system 9
1.7 RECORDING LOGIC IN DFDR 9
1.7.1 Calibrated Air Speed (CAS) parameters 9
1.7.2 Corrected Angle of Attack (CAOA) parameters 10
2. SEQUENCE OF EVENTS 11
2.1 INITIAL CONDITIONS 11
2.2 TURBULENCE AREA 11
3. CONCLUSION 15
GSI 420.1022/15 (TL) 13-Feb-15 4/21

1. FACTUAL INFORMATION
1.1 HISTORY OF THE FLIGHT
On September 9th, 2014 the A330-202 MSN0733 (EC-JPF) operated by Air Europa
(AEA) was performing flight AEA041 from Madrid (MAD) to Buenos Aires (EZE).
During the descent to EZE, the aircraft entered a turbulent area and experienced a
hailstorm. During this period, Recorded CAS dropped by more than 90kt in 1sec. In the
same second, AP1, both FDs and ATHR disengaged, followed by a reversion in
Alternate Law.
During the turbulence zone, the Vertical Acceleration (VRTG) varied between 0.05g
and 2.2g and the Lateral Acceleration (LATG) between 0.06g (left) and 0.25g (right)
and CAS increased up to 314kt.
FDs engaged automatically between 3 to 4 seconds after disengagement. On the same

time, recorded CAS recovered. Normal Law was recovered 10s after reversion in
Alternate Law.
Several pitch up orders on captain side resulted on slight pitch increase. Thrust levers
were pulled to IDLE detent and then CAS decreased. AP1 was reengaged. The thrust
levers were selected back to CLIMB and ATHR was reengaged.
Aircraft performed an uneventfully approach and landing to Buenos Aires (EZE).
GSI 420.1022/15 (TL) 13-Feb-15 5/21

1.2 INJURIES TO PERSONS
No injury has been reported.
1.3 DAMAGE TO AIRCRAFT
The following damages have been reported:
• LH and RH Windshields severely cracked (local maintenance technician

reported that the outer ply was practically destroyed but the inner ply was found
intact. The analysis of the intermediate ply could not be performed because the
condition of the outer ply prevented from differentiating between layers)
• Radome severely damaged (but without passing holes),
• Panels 452CR LH Pylon – and 462CL RH Pylon damaged,

• LH Landing light lens cracked,
• All Pitot probes damaged,
• Panel over RH landing light damaged,
• Wing panels fin numbers 522RB , 523EB, 623CB and 622LB minor damage,
• Wing to body fairing Access door, minor damage,
• Spoiler #4 dented,
• Horizontal stabilizer leading edge tip, dent.
GSI 420.1022/15 (TL) 13-Feb-15 6/21

1.4 AIRCRAFT INFORMATION
A/C Flight Hours and Cycles, here above, are the latest values known by Airbus at the
time of the event.
1.5 METEOROLOGICAL INFORMATION
The METAR information at Buenos Aires airport (SAEZ / EZE) around the time of the
turbulence event (that occurred between 10:30:30 and 13:35:21 UTC) is the following:
• SAEZ 091000Z 29007KT 230V320 9000 -TSRA BKN020 FEW050CB OVC080 20/19 Q1000
• SPECI SAEZ 091028Z 17014KT 140V210 5000 TSRA BKN007 FEW045CB OVC050 20/19 Q1001
• SPECI SAEZ 091040Z 18015G27KT 150V220 5000 TSRA BKN007 FEW045CB OVC050
20/19 Q1002
• SAEZ 091100Z 18020KT 5000 TSRA BKN010 FEW045CB OVC080 16/15 Q1002
Satellite view at 10:00 UTC Satellite view at 11:00 UTC
GSI 420.1022/15 (TL) 13-Feb-15 7/21

Aircraft trajectory from approach to landing with satellite view taken at 10:00 UTC:
1.6 CAS MONITORING BY FMGEC AND FCPC
1.6.1 Monitoring
FMGEC CAS monitoring:

FMGEC monitors the air data and in particular the CAS through a 2 by 2
comparison. The Threshold for an ADR rejection due to CAS monitoring is 20kt
confirmed during 450ms.
Once a first ADR is rejected, there are two possibilities in case of additional
failures:
• One ADR self-detected as Fault 2 ADRs are rejected, 1 remains available
for FMGEC,
• One ADR rejected by comparison (not self-detected) the 3 ADRs are
rejected (FMGEC being unable to determine the erroneous ADR).
Any ADR rejected by comparison by the FMGEC is latched in Fault condition as

long as AP is engaged. As soon as AP is OFF, the Fault is unlatched and if the
rejection condition is no longer valid, the ADR is used again by the FMGEC.
FCPC Icing monitoring:

High density of ice crystals encountered at high altitude may lead to temporary
obstruction of the Pitot inlet. This will result in a rapid drop of the Total Pressure
(Pt) measured by the Pitot and therefore in an abrupt decrease of the associated
CAS.
GSI 420.1022/15 (TL) 13-Feb-15 8/21

To detect any multiple CAS drops due to multiple Pitot obstructions (by ice
crystals), an icing monitoring is performed by FCPC on CAS parameter using a
“voted CAS” defined as followed:
• In case of 3 ADR valid, “voted CAS” is the median value,

• In case of 2 ADR valid, “voted CAS” is the mean of the two remaining CAS.
• In case of 1 ADR valid, “voted CAS” is the last CAS.
In case of Pitot obstruction, if voted CAS drops by more than 30kt within 1s (which
could only happen if at least 2 Pitots are obstructed by ice crystals), the 3 ADRs
are not used anymore by FCPC during 10s and F/CTL downgrades in Alternate 2B
Law (normal longitudinal law + direct lateral law + loss of protections).
The triggering of this monitoring is associated with the following messages on

PFR:
- “PROBE PITOT 1+2/2+3/1+3 (9DA)”, and
- On aircraft fitted with FCDC L21 standard and onwards with the ECAM
CAUTION “NAV IAS DISCREPANCY”. For information the A330 MSN0733
was fitted at the time of the event with the FCDC L23 standard.
After 10s, current voted CAS is compared to the voted one recorded just before
Pitot obstruction. If the difference is lower than 50kt, the 3 ADR are used again and
the Normal law is available again. If not, the 3 ADRs are considered as lost by the
FCPC and the Alternate 2B law is latched.
1.6.2 Consequence on system
1.7 RECORDING LOGIC IN DFDR
1.7.1 Calibrated Air Speed (CAS) parameters
If AIR DATA selector is set to “NORM”, DFDR CAS parameter is recorded from:
ADR1 (CAS1, i.e. from CPT side), as long as CAS1 is valid, i.e. Normal
Operation (NO) and
ADR2 (CAS2, i.e. from F/O side), if CAS1 becomes invalid, i.e. Non Computed
Data (NCD) of fault. CAS is NCD when below 30kt.
GSI 420.1022/15 (TL) 13-Feb-15 9/21

DFDR ISISCAS parameter is recorded from the same probe than CAS from ADR3 (i.e.
is equivalent to CAS3).
1.7.2 Corrected Angle of Attack (CAOA) parameters
When AIR DATA selector is set to “NORM”:

CAOA1 is invalid (NCD) when CAS1 < 60kt,
CAOA2 is invalid (NCD) when CAS2 < 60kt.
Note: AOA from IRS are also recorded in this DFDR data frame (AOAIRS parameters).
For these parameters, a value is recorded from each ADIRU (3 different parameters
recorded) independently of the AIR DATA selector position. AOAIRS corresponds to a
pure copy of each CAOA but transmitted via the IRS part of the ADIRU
GSI 420.1022/15 (TL) 13-Feb-15 10/21

2. SEQUENCE OF EVENTS
The following description and analysis have been carried out using data extracted from
DFDR, Pilot Report (ref. Annex N°1 ) and Post Flight Report (ref. Annex N°2 ). The DFDR
parameters’ list is available in Annex N°3 . The associated plots are available in Annexes
N°4 and 5 .
2.1 INITIAL CONDITIONS
According to the Pilot Report, before starting the descent, at FL360 the flight crew
experienced some light turbulence in clear air, and decided to put the Seat Belt Sign
to “ON”.
They started the descent, and still according to Pilot Report, the weather radar
showed areas of turbulences (magenta) on the right of their route, and areas of
precipitations ahead which occupied an area of approximately 100NM to each side of
their track and was 10 to 15NM deep. They saw areas of red colour clearly sided by
areas of yellow and green towards they were heading.
• At 10:30:30 UTC, the aircraft was in the following initial conditions:

In descent passing 27700ft
AP1 was engaged in NAV/DES modes
FD1 and 2 were engaged
ATHR was engaged and active in THR IDLE mode
Speed was managed
Weather Radar was in WX+TURB mode
ND ranges were 80NM on both Captain and F/O sides
AIR DATA Selector was on the “NORM” position
It can be also mentioned that the TAT was increasing to 0°C, reaching -1.7°C at
10:29:01 UTC then decreasing to -12°C but starting again to inc rease slowly towards
0°C (at 10:30:30 UTC TAT is -8.6°C).This behaviour is typical of a TAT probe icing,
revealing that aircraft was flying in ice crystal environment.
2.2 TURBULENCE AREA
• From 10:30:30 UTC to 10:33:28 UTC, between 27700ft and 23200ft, the Vertical
Acceleration (VRTG) and the Lateral Acceleration (LATG) variations started to
increase:
VRTG between 0.54g to 1.64g and
LATG between 0.06g (left) to 0.13g (right)
• At 10:31:14 UTC, speed control was changed to Selected and selected CAS was set
at 280kt, then at 283kt at 10:32:06 UTC and finally at 260kt (recommended
turbulence speed) at 10:33:32 UTC.
• From 10:31:47 UTC to 10:36:23 UTC, AOA3 reacted with a low sensitivity during
several short periods.
Note: Such behaviour has been already encountered and is likely due to transient ice
crystal accumulation at the AOA3 vane base.
• At 10:33:26 UTC, recorded TAT reached 0.17°C

Note: A recorded TAT increasing and stabilizing at 0°C in flight is typical of a TAT
probe icing.
GSI 420.1022/15 (TL) 13-Feb-15 11/21

• From 10:33:28 UTC to 10:34:33 UTC, between 23200ft and 22200ft, the aircraft flew
through a severe turbulence area and experienced large vertical (VTRG) and lateral
(LATG) accelerations:
VRTG varied between 0.05g and 2.2g and
LATG varied between 0.13g (left) and 0.25g (right).
• At 10:33:38 UTC, the flight crew selected HDG-V/S (FCU V/S was at -1024ft/min).
• From 10:34:31 UTC to 10:34:35 UTC, between 22400ft and 22200ft recorded CAS
dropped from 275kt to 156kt with a loss of more than 90kt in 1sec. During the event,
the recorded CAS is CAS1.
Note: As per DFDR logic, if AIR DATA selector is set on “NORM”, the CAS recorded
by the DFDR is the CAS from CPT side (i.e. CAS1) as long as the CAS1 is
valid (NO). During the whole event period, the AIR DATA selector was in the
“NORM” position and CAS1 remained valid (no fault or NCD).
• At 10:34:33 UTC, the Rudder Travel Limit function was lost (TLU1V and TLU2V
parameters switched to 1 = Not avail).
Note: These two recorded parameters (TLU1V and TLU2V) correspond to the
availability of the rudder Travel Limiter Unit which computes the available
range of the rudder function of the speed. The loss of this function is the
consequence of the loss of speed information by the FCPC.
• From 10:34:33 UTC to 10:35:21 UCT, the aircraft continued to experience strong
turbulences:
VRTG varied between 0.17g and 1.60g and
LATG varied between 0.10g (left) and 0.15g (right).
• At 10:34:34 UTC, loss of AP1, FD1&2 and A/THR and Normal Law reverted in
Alternate Law. Master Warning (MW) triggered during 10sec and the message “THR
LK” was displayed on the FMA until 10:34:57 UTC. ISISCAS dropped from 280kt to
241kt in 1sec and then re-increased to reach 300kt at 10:34:38 UTC.
According to the PFR, at 10:34 UTC the following ECAM alerts were triggered:
A. ICE L WSHLD HEAT
NAV IAS DISCREPANCY associated with the failure message
PROBE PITOT 1+2/2+3/1+3 (9DA)
A. ICE L+R WSHLD HEAT
AUTO FLT A/THR OFF
F/CTL ALTN LAW
FLAG ON CAPT PFD SPD LIMIT
FLAG ON F/O PFD SPD LIMIT
Note: The triggering of the “A. ICE L WSHLD HEAT” followed by “A. ICE L+R
WSHLD HEAT” could be explained by the hail impacts on the windshield.
• At 10:34:35 UTC, Recorded CAS (i.e. CAS1) increased from 156kt and reached a
maximum of 314kt at 10:34:40 UTC.
• At 10:34:37 UTC, the FD2 was recovered followed 1sec later by the FD1.
Analysis: Since ADR failures are not latched by the FMGEC as long as AP is off, FD
reengaged automatically as soon as at least 2 CAS are recovered by the
FMGEC (difference less than 20kt during 450ms).
• At 10:34:43 UTC, the Normal law and TLU function were recovered.
GSI 420.1022/15 (TL) 13-Feb-15 12/21

Analysis: The three ADRs were most likely rejected by the FMGEC leading to the
loss of AP, FD, A/THR and SPD LIM (computed by the FE) on both PFDs.
“FLAG ON CAPT PFD SPD LIMIT” and “FLAG ON F/O PFD SPD LIMIT”
messages on the PFR are explained by the loss of the FE function of the
FMGEC following the 3 ADR rejections. In this case, the following PFD
information is lost: VLS, S, F, Green Dot, Vtrend, VMAX, VFE next, VSW.
The reversion in ALTN law is explained by the triggering of the icing
monitoring of the FCPC. Indeed, the ECAM message NAV IAS
DISCREPANCY associated with the failure message PROBE PITOT
1+2/2+3/1+3 (9DA) are the signature of this triggering.
The icing monitoring is triggered when the Voted CAS (i.e. in that case the
median of the three CAS) dropped by more than 30kt in 1sec. When
looking at the CAS1 (=Recorded CAS) and CAS3 (≈ISISCAS) behaviours
during the second before the rejection in ALTN law (see here below
graph), CAS2 was most probably the median. In any case, as the CAS3
decreased by only 7kt in this second, CAS2 has necessarily dropped
meaning that the F/O Pitot Probe has been also obstructed by ice crystal.
10 sec after the reversion in ALTN law, the NORM law is recovered. This
also corroborates that the ALTN law was triggered by the icing monitoring
of the FCPC. Difference between current Voted CAS and Voted CAS
before the Pitot obstruction was most probably lower than 50kt at that
time, leading the FCPC to use again the three ADRs and to the recovery
of the NORM law.
GSI 420.1022/15 (TL) 13-Feb-15 13/21

• At 10:34:48 UTC, ALT reached a minimum of 22180ft and then increased after
several pitch up orders recorded on Capt. side. Pitch increased to reach 2.11° at
10:34:53 UTC.
• At 10:34:56 UTC, a pitch up order (4.13° back stick) was recorded f ollowed by a
second one at 10:35:20 UTC (6.33° back stick). The pitch increased to 3.52°. C AS
reached 305kt and then decreased. ALT was increasing and reached 23150ft at
10:35:59 UTC before decreasing again.
• At 10:34:57 UTC, the Thrust Levers were retarded from CLIMB to IDLE detent.
• At 10:35:21 UTC, AP1 engaged (still HDG-V/S mode).
• At 10:35:33 UTC, the Thrust Levers were set back to CLIMB detent and A/THR was
reengaged (in SPD mode).
• At 10:35:55 UTC, OP DES mode was engaged (lateral mode remained in HDG).
Then the aircraft proceeded to the approach and performed an uneventful landing in
Buenos Aires airport (EZE).
Probable collision with tree
GSI 420.1022/15 (TL) 13-Feb-15 14/21

3. CONCLUSION
On September 9th 2014, A330 MSN0733 (Reg. EC-JPF) operated by Air Europa (AEA)
was performing a flight from Madrid (MAD, Spain) to Buenos Aires (EZE, Argentina).
During the descent to EZE, passing FL230 the aircraft crossed a turbulence area and
hailstorm conditions.
According to Pilot Report, the flight crew was aware of the vicinity of strong weather cells
(weather radar was in WX+TURB mode) but did not expect such heavy precipitations.
The hailstorm severely damaged both windshields and radome. The turbulence zone last
almost 5mn during which the Vertical Acceleration (VRTG) varied between 0.05g and
2.2g and the Lateral Acceleration (LATG) between 0.06g (left) and 0.25g (right).
There are some indications (TAT probe freezing and low AOA sensibility) that the aircraft
was flying in ice crystal environment for at least few minutes before entering the
turbulence area. When crossing 22350ft, the CAS1 dropped by more than 90kt in 1sec.
3sec after, ISISCAS (equivalent to CAS3) dropped by 30kt in 1sec. In the meantime,
AP1, both FDs and A/THR were lost and F/CTL law reverted in Alternate law.
Loss of AP, FDs and A/THR is most likely due to the rejection of the three ADRs by the
FMGEC (due to CAS monitoring). The transient reversion in Alternate law is due to the
temporary rejection of the 3 ADR by FCPC (icing monitoring).
FD2 and FD1 were recovered respectively 3 and 4sec after their disengagement,
meaning that at least two ADRs were revalidated by the FMGEC. 10sec after the
reversion in Alternate law, the Normal law was recovered (as per FCPC icing monitoring
logic in case of CAS recovery).
The Thrust Levers were selected on IDLE detent for 36sec, to reduce the speed
according to the Pilot Report (at that time the CAS was 305kt). When the thrust levers
were set back to CLIMB detent, A/THR was reengaged. In the meantime AP1 was
reengage in HDG-V/S mode and then in OP DES mode. Then the aircraft proceeded to
the approach and performed an uneventful landing in Buenos Aires airport (EZE).
GSI 420.1022/15 (TL) 13-Feb-15 15/21

ANNEXES
1. Pilot Report (PIREP)
2. Post Flight Report (PFR)
3. List of recorded parameters
4. FDR data plots – overall
5. FDR data plots – Zoom
GSI 420.1022/15 (TL) 13-Feb-15 16/21

Annex N° 1
Pilot Report (PIREP)
GSI 420.1022/15 (TL) 13-Feb-15 17/21

EZE A330 WEATHER ENCOUNTER – CATAIN’S REPORT
On last September 8th, I signed-in at 20:25 UTC in MAD for the AEA 041 flight. I had previously
downloaded the flight plan at home and also inserted the route in the Jeppesen iPad app, and also
updated weather information provided by this and thus have extra help.
We took off from Madrid, made the expected flight level changes during the flight, run the entire
route without any impact initially, and carried out the planned rests for all members of the crew.
According the weather information obtained during the flight, we selected a VOR approach to
runway 29, and loaded an ILS 25 in the secondary flight plan, giving the briefing in this way.
Once in contact with Montevideo Control, as we could not receive yet the ATIS-EZE by VHF (only
means possible, having no D-ATIS), they told us the runway in use was the 35. We activated the
secondary flight plan and re-programmed as a secondary RWY 29, again reviewing the briefing for
this new plan.
Before the descent, at level 360 we experienced some light turbulence in clear air, and we decided
to put the belts sign ON.
We started the descent, and the weather radar showed areas of turbulence (magenta) to the right
of our route, and areas of precipitation in front of us which occupied an area of approximately 100
NM to each side of the track and 10-15 NM deep initially at that time. We saw areas of red color
clearly sided by areas of yellow and green, that was where our path was directed. We began our
descent aiming to that green/yellow narrow aisle, that couldn’t predict high-intensity precipitation.
Passing through FL260, we receive hail impacts, cracking both windshield from the very beginning,
and experiencing at the same time severe to extreme turbulence; as I mentioned, it did not show
on the radar for this area we were flying, nor had been reported by radio, VOLMET ATIS, or the
presence of storm or hail at these levels.
Just at the beginning of the descent we received the ATIS, which gave RWY 35 in use, but in the
subsequent communication with EZE they said then that RWY in use was 11. Therefore, I asked the
Copilot to load the ILS approach to runway 11, while I had controls and communications, and the
relief Copilot assisted us with the QRH procedure “cockpit windshield/window cracked”.
Due to that turbulence turbulence, the autopilot disengaged without crew action, so I set IDLE to
reduce our airspeed, then selected 260Kts and connected back A/P and ATHR. They told us to
proceed direct to point ARSOT and we told them back that we were to fly to a heading to the left of
the route due to the weather conditions.
An ECAM Caution consistent to the cracked windshields arose: “L & R Windshield Heat Fail”, getting
help from the relief Copilot.
Once free of adverse weather (around FL150), we required priority for landing, telling them about
what we just experienced in the aircraft and weather. At this time the Copilot had the
communications back and I had the controls.
I gave another briefing for the new runway in use, preparing for CATIIIA at the prospect of poor
visibility due to the damaged windshield. We made an uneventful approach from the South of the
field towards ARSOT, and in final I decided to land manually, since although it was within limits for
autoland, the wind was strong enough to consider it the best option, and my window was less
damaged that the one on the other side.
We taxied to the ramp and had to wait for the marshaller, since the ground personnel was not
allowed to approach any aircraft under those storms at the airport. Once the technician climbs on
board, he told us that we also had a damaged nose radome, as well as some damage on each
engine pylon and the landing light, so I checked and took pictures of all damage before filling-in the
logbook.
I called the Flight Manager and the Flight Following Captain on duty, telling them what had just
happened, and reporting that pictures would be sent from the hotel.
We had to wait a while for the baggage at the claim area (until handling personnel were allowed to
work on the ramp), what gave the opportunity to many passengers to congratulate us personally,
which we thank them.
Once in the hotel, we called back the Flight Following Duty Captain, in order to arrange an interview
with the National Authority (JIAAC) personnel, what we had at noon in the hotel lobby.
We were then told that another aircraft was on its way to EZE, with some spare parts, and that we
would fly back to MAD as scheduled.
During the afternoon, the whole crew (pilots and cabin crew) had the opportunity to join for a long
debriefing were to explain and discuss all that happened.
Signed,
Captain
Annex N° 2
Post Flight Report (PFR)
GSI 420.1022/15 (TL) 13-Feb-15 18/21

Annex N° 3
List of recorded parameters
GSI 420.1022/15 (TL) 13-Feb-15 19/21

RESOL SIGN
MNEMO LIBELLE UNIT SOURCE PPS
Info CONV
43011 E.G.P.W.S OPERATING MODE (NOT USED) NA DMC Label = 016/24-26 1/4 NA 1= TBD
73011 F/O PFD/DU (6) VALID NA DMC (F/O BUS) Label = 332/15 1/4 NA 1= VALID
73021 F/O ND/DU (5) VALID NA DMC (F/O BUS) Label = 332/17 1/4 NA 1= VALID
10NMC 10 NM RANGE ND ON CAPT (MATRIX 15) NA DMC Label = 215/23 1/4 NA NA
10NMF 10 NM RANGE ND ON F/O NA DMC (MATRIX 15) Label = 215/23 1/4 NA NA
121120 N1 ACTUAL ENG.1 FINE bits16-27 (%) FADEC/EEC DMC Label = 346 1/1 NA NA
125121 N1 ACTUAL ENG.2 FINE bits16-27 (%) ADEC(EEC or ECU) DMC Label = 34 1/1 NA NA
131010 N1 ACTUAL ENG.1 COARSE bits 28 (%) FADEC/EEC DMC Label = 346 1/1 NA NA
135011 N1 ACTUAL ENG.2 COARSE bits 28 (%) ADEC(EEC or ECU) DMC Label = 34 1/1 NA NA
160NMF 160 NM RANGE ND ON F/O (MATRIX 15) NA DMC Label = 215/27 1/4 NA NA
191110 FUEL FLOW ENG.1 MSB PART bits 27-28 (LBS/H) ADEC(ECU or EEC) DMC Label = 24 1/1 NA NA
191111 FUEL FLOW ENG.2 MSB PART bits 27-28 (LBS/H) ADEC(ECU or EEC) DMC Label = 24 1/1 NA NA
1DATBROAD MMR1 MODE DATA BROADCAST MODE NA MMR Label = 033/11-14 1/4 NA NA
1FLS MMR1 MODE FLS NA MMR Label = 033/11-14 1/4 NA NA
1GLS MMR1 MODE GLS MODE NA MMR Label = 033/11-14 1/4 NA NA
1GLSC GLS OR MMR1 FREQUENCY 100 and 10 mhz (MHZ) ILS or MMR DMC Label = 033 1/4 4096.000 NA
1GLSC2 GLS OR MMR1 FREQUENCY (MHZ) ILS or MMR Label = 033 NA 1200.000 NA
1GLSCH GLS OR MMR1 FREQUENCY (MHZ) ILS or MMR Label = 033 NA 1.000 NA
1GLSF GLS OR MMR1 FREQUENCY 0.1 0.01 mhz (MHZ) ILS or MMR DMC Label = 033 1/4 1.000 NA
1GLSSC GLS OR MMR1 FREQUENCY 100 and 10 mhz (MHZ) ILS or MMR DMC Label = 033 1/4 32768.000 NA
1ILS MMR1 MODE ILS NA MMR Label = 033/11-14 1/4 NA NA
1ILSFLS MMR1 MODE COMBINED ILS/FLS NA MMR Label = 033/11-14 1/4 NA NA
1ILSVC MMR1 ILS/VOR FREQUENCY/CHANNEL 100 and 10 mhz COARSE bits 27-29 (MHZ) ILS DMC Label = 033 1/4 10.000 NA
1ILSVF MMR1 ILS/VOR FREQUENCY/CHANNEL 1 0.1 0.01 mhz FINE bits 15-26 NA ILS DMC Label = 033 1/4 0.010 NA
1ILSVORF MMR1 ILS/VOR FREQUENCY/CHANNEL ELAB bits 15-29 (MHZ) ILS DMC Label = 033 NA 0.010 NA
1MLSAUTO MMR1 MODE MLS AUTO MODE NA MMR Label = 033/11-14 1/4 NA NA
1MLSBAZ MMR1 MODE MLS BAZ MODE (MILITARY OPTION) NA MMR Label = 033/11-14 1/4 NA NA
1MLSC MMR1 MLS CHANNEL COARSE bits 26-29 NA MMR DMC Label = 033 1/4 100.000 NA
1MLSCH MMR1 MLS CHANNEL ELAB bits 18-29 NA MMR DMC Label = 033 NA 1.000 NA
1MLSCOMP MMR1 MODE MLS COMPUTED MODE (MILITARY OPTION) NA MMR Label = 033/11-14 1/4 NA NA
1MLSF MMR1 MLS CHANNEL FINE bits 18-25 (MHZ) NA 1/4 1.000 NA
1PC1 DC1/DC BAT CONTACTOR CLOSED NA ECMU SDAC Label = 003/20 1/4 NA 1= CLOSED
1PC2 DC2/DC BAT CONTACTOR CLOSED NA ECMU SDAC Label = 003/20 1/4 NA 1= CLOSED
1PH DC ESS/DC ESS SHED CONTACTOR OPEN NA ECMU SDAC Label = 005/20 1/4 NA 1= OPEN
1PP DC1 BUS NO VOLTAGE NA ECMU SDAC Label = 003/14 1/4 NA 1= NO VOLTAGE
1RSVD MMR1 MODE RSVD. FUTURE EXPANSION NA MMR Label = 033/11-14 1/4 NA NA
1SPARE MMR1 MODE SPARE NA MMR Label = 033/11-14 1/4 NA NA
1VHFHYB MMR1 MODE RSVD.VHF HYBRID MODE NA MMR Label = 033/11-14 1/4 NA NA
1VORMODE MMR1 MODE RSVD.VOR MODE NA MMR Label = 033/11-14 1/4 NA NA
1XP1 1XP NO VOLTAGE NA ECMU SDAC Label = 055/19 1/4 NA 1= NO VOLTAGE
201120 FUEL FLOW ENG.1 LSB PART bits 15-26 (LBS/H) ADEC(ECU or EEC) DMC Label = 24 1/1 NA NA
201121 FUEL FLOW ENG.2 LSB PART bits 15-26 (LBS/H) ADEC(ECU or EEC) DMC Label = 24 1/1 NA NA
20NMF 20 NM RANGE ND ON F/O NA DMC (MATRIX 15) Label = 215/24 1/4 NA NA
2DATBROAD MMR2 MODE DATA BROADCAST MODE NA MMR Label = 033/11-14 1/4 NA NA
2FLS MMR2 MODE FLS NA MMR Label = 033/11-14 1/4 NA NA
2GLS MMR2 MODE GLS MODE NA MMR Label = 033/11-14 1/4 NA NA
2GLSC GLS OR MMR1 FREQUENCY 100 and 10 mhz (MHZ) ILS or MMR DMC Label = 033 1/4 4096.000 NA
2GLSC2 GLS OR MMR1 FREQUENCY (MHZ) ILS or MMR Label = 033 NA 1200.000 NA
2GLSCH GLS OR MMR1 FREQUENCY (MHZ) ILS or MMR Label = 033 NA 1.000 NA
2GLSF GLS OR MMR1 FREQUENCY 0.1 0.01 mhz (MHZ) ILS or MMR DMC Label = 033 1/4 1.000 NA
2GLSSC GLS OR MMR1 FREQUENCY 100 and 10 mhz (MHZ) ILS or MMR DMC Label = 033 1/4 32768.000 NA
2ILS MMR2 MODE ILS NA MMR Label = 033/11-14 1/4 NA NA
2ILSFLS MMR2 MODE COMBINED ILS/FLS NA MMR Label = 033/11-14 1/4 NA NA
2ILSVC MMR2 ILS/VOR FREQUENCY/CHANNEL 100 and 10 mhz COARSE (MHZ) ILS or MMR DMC Label = 033 1/4 10.000 NA
2ILSVF MMR2 ILS/VOR FREQUENCY/CHANNEL 1 0.1 0.01 mhz FINE NA ILS or MMR DMC Label = 033 1/4 0.010 NA
2ILSVORF MMR2 ILS/VOR FREQUENCY/CHANNEL (MHZ) ILS or MMR DMC Label = 033 NA 0.010 NA
2MLSAUTO MMR2 MODE MLS AUTO MODE NA MMR Label = 033/11-14 1/4 NA NA
2MLSBAZ MMR2 MODE MLS BAZ MODE (MILITARY OPTION) NA MMR Label = 033/11-14 1/4 NA NA
2MLSC MMR2 MLS CHANNEL COARSE NA MMR DMC Label = 033 1/4 100.000 NA
2MLSCH MMR2 MLS CHANNEL NA MMR DMC Label = 033 NA 0.010 NA
2MLSCOMP MMR2 MODE MLS COMPUTED MODE (MILITARY OPTION) NA MMR Label = 033/11-14 1/4 NA NA
2MLSF MMR2 MLS CHANNEL FINE (MHZ) NA 1/4 1.000 NA
2PP DC2 BUS NO VOLTAGE NA ECMU SDAC Label = 003/14 1/4 NA 1= NO VOLTAGE
2RSVD MMR2 MODE RSVD. FUTURE EXPANSION NA MMR Label = 033/11-14 1/4 NA NA
2SPARE MMR2 MODE SPARE NA MMR Label = 033/11-14 1/4 NA NA
2VHFHYB MMR2 MODE RSVD.VHF HYBRID MODE NA MMR Label = 033/11-14 1/4 NA NA
2VORMODE MMR2 MODE RSVD.VOR MODE NA MMR Label = 033/11-14 1/4 NA NA
385360 TCAS UP ADVISORY NOT USED (MATRIX 8) ******* NA TCAS DMC Label = 270/24-26 1/1 NA NA
385370 TCAS UP ADVISORY NOT USED ******* NA TCAS DMC Label = 270/24-26 1/1 NA NA
385460 TCAS DOWN ADVISORY NOT USED (MATRIX 9) ******** NA TCAS DMC Label = 270/27-29 1/1 NA NA
385470 TCAS DOWN ADVISORY NOT USED (MATRIX 9) ******** NA TCAS DMC Label = 270/27-29 1/1 NA NA
3ADRNOVALID 3 ADR NOT VALID IN FLIGHT CONDITION NA DMC Label = 331/20 1/4 NA 1= 3 ADR NOT VALID
3PE ESS TR CONTACTOR CLOSED NA ECMU SDAC Label = 003/18 1/4 NA 1= CLOSED
3PP 3PP DC BAT BUS NO VOLTAGE NA ECMU SDAC Label = 055/23 1/4 NA 1= NO VOLTAGE
3XC1 AC1/AC ESS CONTACTOR CLOSED NA ECMU SDAC Label = 003/24 1/4 NA 1= CLOSED
3XC2 AC2/AC ESS CONTACTOR CLOSED NA ECMU SDAC Label = 003/24 1/4 NA 1= CLOSED
415332 TCAS COMBINATED CONTROL NOT USED (MATRIX 7) ******* NA TCAS DMC Label = 270/18-20 1/1 NA NA
451121 ADF2 FREQUENCY PART ONE bits 15-26 (KHZ) ADF DMC Label = 032 1/4 1.000 NA
458120 ADF1 FREQUENCY PART ONE bits 15-26 (KHZ) ADF DMC Label = 032 1/4 1.000 NA
461021 ADF2 FREQUENCY PART TWO bits 14&27 (KHZ) ADF DMC Label = 032 1/4 0.500 NA
464100 VOR1 FREQUENCY FINE bits 15 NA VOR1 DMC Label = 034 1/4 0.050 NA
467010 DME1 FREQUENCY FINE bits 18 (MHZ) DME DMC Label = 035 1/4 0.050 NA
467011 DME2 FREQUENCY FINE bits 18 (MHZ) DME DMC Label = 035 1/4 0.050 NA
467110 DME1 FREQUENCY COARSE bits 19-29 (MHZ) DME DMC Label = 035 1/4 0.100 NA
467111 DME2 FREQUENCY COARSE bits 19-29 (MHZ) DME DMC Label = 035 1/4 0.100 NA
468020 ADF1 FREQUENCY PART TWO bits 14&27 (KHZ) ADF DMC Label = 032 1/4 0.500 NA
468031 VOR2 FREQUENCY FINE bits 15 NA VOR DMC Label = 034 1/4 0.050 NA
468090 VOR1 FREQUENCY COARSE bits 19-27 (MHZ) VOR1 DMC Label = 034 1/4 0.100 NA
468091 VOR2 FREQUENCY COARSE bits 19-27 (MHZ) VOR DMC Label = 034 1/4 0.100 NA
4PC DC BAT/DC ESS CONTACTOR CLOSED NA ECMU SDAC Label = 005/22 1/4 NA 1= CLOSED
4PP DC ESS BUS NO VOLTAGE NA ECMU SDAC Label = 003/15 1/4 NA 1= NO VOLTAGE
575011 RED WARNING SPARE 3 NA FWC Label = 124/28 1/1 NA 1=
5PB APU BAT CONTACTOR CLOSED NA ECMU SDAC Label = 005/18 1/4 NA 1= CLOSED
5PU1 TR1 CONTACTOR CLOSED NA ECMU SDAC Label = 003/14 1/4 NA 1= CLOSED
5PU2 TR2 CONTACTOR CLOSED NA ECMU SDAC Label = 003/14 1/4 NA 1= CLOSED
601063 TCAS CREW SELECTION NOT USED (MATRIX 10) ****** NA TCAS DMC Label = 016/15-17 1/1 NA NA
6PB1 BAT.1 CONTACTOR CLOSED NA ECMU SDAC Label = 005/14 1/4 NA 1= CLOSED
6PB2 BAT.2 CONTACTOR CLOSED NA ECMU SDAC Label = 005/16 1/4 NA 1= CLOSED
7PU APU TR CONTACTOR CLOSED NA ECMU SDAC Label = 003/16 1/4 NA 1= CLOSED
9528045 HEIGHT VALUE MDA/MDH FINE ELAB (FT) FMGEC(FM) DMC 1/62 1.000 NA
9528046 HEIGHT VALUE MDA/MDH COARSE ELAB (FT) FMGEC(FM) DMC 1/62 4096.000 NA
9XP 9XP NO VOLTAGE NA ECMU SDAC Label = 003/25 1/4 NA 1= NO VOLTAGE
ACRGSMOW AFT CARGO SMOKE NA FWC Label = 124/14 1/1 NA 1= SMOKE
ACT1QKG ACT.1 FUEL QUANTITY (KG) FCMC DMC Label = 312 1/62 29.030 NA
ACT1QLB ACT.1 FUEL QUANTITY (LBS) FCMC DMC Label = 312 1/62 64.000 NA
ACT1V ACT.1 INSTALLED NA FCMC DMC Label = 313/11 1/62 NA 1= INSTALLED
ACT2QKG ACT.2 FUEL QUANTITY (KG) FCMC DMC Label = 316 1/62 29.030 NA
ACT2QLB ACT.2 FUEL QUANTITY bits 18-28 (LBS) FCMC DMC Label = 316 1/62 64.000 NA
ACT2V ACT.2 INSTALLED NA FCMC DMC Label = 313/12 1/62 NA 1= INSTALLED
ACTAIL A/C TAIL NUMBER NA DCP FDIU NA NA NA
ACTAIL1 A/C TAIL NUMBER C1 NA DCP FDIU Label = 1/62 NA NA
ACTYPE A/C TYPE NA FDIU Label = 1/62 NA 53= A330-GE
ADFF1 ADF1 FREQUENCY ELAB. (KHZ) ADF DMC Label = 032 NA 0.500 NA
ADFF2 ADF2 FREQUENCY ELAB. (KHZ) ADF DMC Label = 032 NA 0.500 NA
ADR123F ADR 1+2+3 FAULT NA FWC Label = 124/27 1/1 NA 1= FAULT
ADR1F ADR.1 FAIL NA DMC Label = 360/14 1/4 NA 1= FAULT
ADR1PFDC ADR1 SELECTED ON PFD (CAPT) NA DMC Label = 341/21 1/4 NA 1= SELECTED
ADR2PFDF ADR2 SELECTED ON PFD (F/O) NA DMC Label = 341/22 1/4 NA 1= SELECTED
ADVN1V1 ADV ENG.1 N1 VIBRATION NA EIVMU DMC Label = 300/13 1/1 NA 1= ACTIVE
AFLOORD FMA A/THR ALPHA FLOOR DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
AGC AGC CLOSED NA ECMU SDAC Label = 055/13 1/4 NA 1= CLOSED
AIDLEAC Auto idle activated NA FWC Label = 172 2/1 NA NA
AIDRIVENWING WING ANTI-ICE DRIVEN ON NA WHC1 SDAC Label = 003/18 1/2 NA 1= SELECTED ON
AILLI LH INNER AILERON bits18-26+29 (DA) FCPC-FCSC FCDC Label = 310 2/1 0.088 >0= AIL.DOWN
AILLIBV INNER LH AILERON BLUE AVAILABILITY NA FCDC Label = 42/16 2/1 NA 1= AVAILABLE
AILLIGV INNER LH AILERON GREEN AVAILABILITY NA FCDC Label = 42/17 2/1 NA 1= AVAILABLE
AILLO LH OUTER AILERON bits18-26+29 (DA) FCPC-FCSC FCDC Label = 320 1/1 0.088 >0= AIL DOWN
AILLOGV OUTER LH AILERON GREEN AVAILABILITY NA FCDC Label = 42/21 1/1 NA 1= AVAILABLE
AILLOYV OUTER LH AILERON YELLOW AVAILABILITY NA FCDC Label = 42/20 1/1 NA 1= AVAILABLE
AILRI RH INNER AILERON bits18-26+29 (DA) FCPC-FCSC FCDC Label = 330 2/1 0.088 >0= AIL.DOWN
AILRIBV INNER RH AILERON BLUE AVAILABILITY NA FCDC Label = 42/18 2/1 NA 1= AVAILABLE
AILRIGV INNER RH AILERON GREEN AVAILABILITY NA FCDC Label = 42/19 2/1 NA 1= AVAILABLE
AILRO RH OUTER AILERON bits18-26+29 (DA) FCPC-FCSC FCDC Label = 340 1/1 0.088 >0= AIL.DOWN
AILROGV OUTER RH AILERON GREEN AVAILABILITY NA FCDC Label = 42/22 1/1 NA 1= AVAILABLE
AILROYV OUTER RH AILERON YELLOW AVAILABILITY NA FCDC Label = 42/23 1/1 NA 1= AVAILABLE
AIRL1 AIRLINE IDENT CODE C1 NA DCP FDIU Label = 1/62 NA NA
AIRL2 AIRLINE IDENT CODE C2 NA DCP FDIU Label = 1/62 NA NA
AISEL AUTO ANTI-ICE SELECTION NA P/B-COCKPIT SDAC Label = 001/20 1/2 NA 1= SELECTED ON
ALAW ALTERNATE FLIGHT LAW NA FCPC-FCSC FCDC Label = 040/12 1/1 NA 1= ENGAGED
ALIGN ALIGN MODE NA FMGEC(FG) DMC Label = 176/25 1/1 NA 1= ENGAGED
ALT ALTITUDE ELAB Bits 14-27+29 (FT) ADIRS(ADC) DMC Label = 203 NA NA NA
ALTACQCRZD FMA LONGI. MODE ALT CRZ* DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
ALTACQCSTD FMA LONGI. MODE ALT CST* DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
ALTACQD FMA LONGI. MODE ALT* DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
ALTARM ALT ARMED NA FMGEC(FG) DMC Label = 274/25 1/1 NA 1= ARMED
ALTBRKPLHB ALTERNATE PRESSURE ON LEFT SIDE (Bar) BSCU Label = 365 1/1 4.413 NA
ALTBRKPLHP ALTERNATE PRESSURE ON LEFT SIDE (PSI) BSCU Label = 365 1/1 64.000 NA
ALTBRKPRHB ALTERNATE PRESSURE ON RIGHT SIDE (Bar) BSCU Label = 364 1/1 4.413 NA
ALTBRKPRHP ALTERNATE PRESSURE ON RIGHT SIDE (PSI) BSCU Label = 364 1/1 64.000 NA
ALTBW PRESSURE ALTITUDE WARNING (ALTIBARO DISCREPANCY) NA FWC Label = 124/25 1/1 NA 1= WARNING
ALTC STD ALTITUDE COARSE(ADC) Bits 23-27 (FT) ADIRS(ADC) DMC Label = 203 1/1 NA NA
ALTCRZD FMA LONGI. MODE ALT CRZ DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
ALTCSTD FMA LONGI. MODE ALT CST DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
ALTF ALTITUDE FINE Bits 14-22 (FT) ADIRS(ADC) DMC Label = 203 1/1 4.000 NA
ALTFCUCSTS FCU SELECTED/CONSTRAINED ALTITUDE FG SELECTION NA FMGEC(FG) DMC Label = 274/20 1/1 NA 1= SEL.ALT 0= CST.ALT
ALTLOST TCAS COMBINATED CONTROL.ALTITUDE LOST. (MATRIX 7) NA TCAS DMC Label = 270/18-20 1/1 NA NA
ALTMODD FMA LONGI. MODE ALT DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
ALTS ALTITUDE FINE Bits 29 (FT) ADIRS(ADC) DMC Label = 203 1/1 4.000 NA
ALTSTDW PRESSURE ALTITUDE WARNING (ALTIBARO STD DISCREPANCY) NA FWC Label = 124/24 1/1 NA 1= WARNING
AOAIRS1 AOA VALUE EMITTED BY IRS1 (DA) ADIRS(IRS) DMC Label = 337 1/1 0.352 >0= UP
AP1E A/P1 ENGAGED NA FMGEC(FG) DMC Label = 274/14 1/1 NA 1= ENGAGED
AP2E A/P2 ENGAGED NA FMGEC(FG) DMC Label = 274/15 1/1 NA 1= ENGAGED
APOFFV A/P OFF VOLONTARY NA FWC Label = 100/27 1/1 NA 1= ENGAGED
APOFFW AUTO-PILOT OFF UNVOLUNTARY NA FWC Label = 124/23 1/1 NA 1= WARNING
APPNAVD FMA LATERAL MODE APP NAV DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
APU A.P.U PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
APUBV APU BLEED V. NOT FULLY OPEN NA BMC SDAC Label = 040/13 1/4 NA 1= NOT FULLY OPEN
APULEAK APU LEAK MEMORIZED NA BMC FWC Label = 100/24 1/4 NA 1= LEAK
APUPB APU BLEED PUSH BUTTON OFF NA BMC SDAC Label = 040/12 1/1 NA 1= OFF
ARCC ARC MODE MODE DISPLAYED ON ND CAPT (MATRIX 16) NA DMC Label = 214/26-28 1/4 NA NA
ARCF ARC MODE MODE DISPLAYED ON ND F/O (MATRIX 16) NA DMC Label = 214 1/4 NA NA
ASKIDF ANTISKID FAULT NA BSCU Label = 026/24 1/1 NA 1= FAULT
ASKIDOFF ANTISKID OFF NA BSCU Label = 026/29 1/1 NA 0= FALSE 1= TRUE
ATCLIGHT ATC MESSAGE LIGHTS NA FWC Label = 262/14 1/4 NA 1= LIGHTS ON
ATHRA A/THR ACTIVE NA FMGEC(FG) DMC Label = 274/16 1/1 NA 1= ACTIVE
ATHRE A/THR ENGAGED NA FMGEC(FG) DMC Label = 274/17 1/1 NA 1= ENGAGED
ATHRRTD A/THR RETARD NA FMGEC(FG) DMC Label = 274/18 1/1 NA 1= ACTIVE
ATHRSUBM A/P-A/THR SUB MODE MATRIX 5 NA FMGEC(FG) DMC Label = 145 1/1 NA NA
AUDIOTRF AUDIO TRANSMITTER FAIL NA FDIU Label = 1/62 NA NA
AUTBRKF AUTOBRAKE FAULT NA BSCU Label = 026/20 1/1 NA 1= FAULT
AUTOLAND AUTOLAND NA FWC Label = 126/16 1/1 NA 1= AUTOLAND ON
AVCCSMO SMOKE AUTONOMOUS VCC NA FWC Label = 101/13 1/1 NA 1= WARNING
AVISMOW AVIONICS SMOKE NA FWC Label = 124/11 1/1 NA 1= SMOKE
BAROD BARO DISPLAYED MATRIX.12 (EIS2 ONLY) NA FMGEC(FM) DMC Label = 155 1/62 NA NA
BCKPALTGPSACT BACKUP ALTI GPS ACTIVE NA DMC Label = 331/16 1/4 NA 1= ACTIVATED
BCKPSPD BACK UP SPEED VALUE DISPLAYED bits16-27 (KT) DMC Label = 336 1/1 0.352 NA
BCKPSPDACT BACKUP SPEED SCALE ACTIVE NA DMC Label = 331/17 1/4 NA 1= ACTIVATED
BCKPSPDV BACKUP SPEED SCALE VALID NA DMC Label = 331/15 1/4 NA 1= VALID
BCRCSMO BCRC SMOKE NA FWC Label = 101/12 1/1 NA 1= WARNING
BITE10 B.I.T.E CYCLE.10 NA FDIU Label = 1/62 1.000 NA
BITE7 B.I.T.E CYCLE.7 NA FDIU 1/62 1.000 NA
BLATG BODY LATERAL ACCELERATION bits19-27+29 (G) ADIRS(IRS) DMC Label = 335 1/1 0.004 >0= RH SIDESLIP
BLDLOWT BLEED LOW TEMP. NA BMC SDAC Label = 100/23 1/1 NA 1= LOW TEMP
BLEED BLEED PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
BRKLOW AUTOBRAKE LOW ARMED NA BSCU Label = 027/20 1/1 NA 1= ARMED
BRKMAX AUTOBRAKE MAX ARMED NA BSCU Label = 027/22 1/1 NA 1= ARMED
BRKMED AUTOBRAKE MED ARMED NA BSCU Label = 027/21 1/1 NA 1= ARMED
BRKPDL LEFT BRAKE PEDAL POSITION bits 23-28 (DA) BSCU Label = 331 1/1 2.000 NA
BRKPDR RIGHT BRAKE PEDAL POSITION bits 23-28 (DA) BSCU Label = 330 1/1 2.000 NA
BSCUCHAN1A BSCU CHANNEL 1 IN CONTROL NA SCU SYSTEM 1 ONLY Label = 030/ 1/4 NA 1= ACTIVE
BSCUCHAN1F BSCU CHANNEL 1 FAULT NA FWC Label = 100/25 1/4 NA 1= FAULT
BSCUCHAN2A BSCU CHANNEL 2 IN CONTROL NA SCU SYSTEM 2 ONLY Label = 030/ 1/4 NA 1= ACTIVE
BSCUCHAN2F BSCU CHANNEL 2 FAULT NA FWC Label = 100/26 1/4 NA 1= FAULT
BTC1 BTC.1 CLOSED NA ECMU SDAC Label = 055/15 1/4 NA 1= CLOSED
BTC2 BTC.2 CLOSED NA ECMU SDAC Label = 055/16 1/4 NA 1= CLOSED
BULKSMOW BULK AVIONIC SMOKE NA FWC Label = 126/29 1/1 NA 1= WARNING
CABALTW EXCESS CABIN ALTITUDE NA FWC Label = 126/22 1/1 NA 1= EXCESS CABIN ALT.
CABRSMOW CABIN REST SMOKE NA FWC Label = 124/12 1/1 NA 1= SMOKE
CAOA1 CORRECTED LH ANGLE OF ATTACK bits 20-27+29 (DA) ADIRS(ADC) DMC Label = 241 1/1 0.352 >0= UP
CAOA2 CORRECTED RH ANGLE OF ATTACK bits 20-27+29 (DA) ADIRS(ADC) DMC Label = 241 1/1 0.352 >0= UP
CAS COMPUTED AIRSPEED bits16-27 (KT) ADIRS(ADC) DMC Label = 206 1/1 0.125 NA
CB CIRCUIT BREAKER PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
CDSSONSD VIDEO SYSTEM CDSS SELECTION ON SD NA DMC Label = 333/16 1/4 NA 1= CDSS SELECTED
CEGNUL CENTER GEAR NOT UP LOCKED (if Center not installed M36a07 = 0) NA LGCIU FWC Label = 021/17 2/1 NA 1= NOT UP LOCKED
CEGOPINST CENTER GEAR OPTION INSTALLED NA LGCIU FWC Label = 022/27 2/1 NA 1= OPTION INSTALLED
CEGPWSI CAPTAIN E.G.P.W.S INSTALLED NA DMC Label = 055/15 1/1 NA 1= INSTALLED
CEGPWSV CAPTAIN E.G.P.W.S VALID NA DMC Label = 055/12 1/1 NA 1= VALID
CESQUAT L/G CENTER SQUAT SWITCH NA LGCIU FWC Label = 020/17 4/1 NA 1= COMPRESSED
CG CENTER OF GRAVITY (%) FCMC DMC Label = 076 1/62 0.080 NA
CGW EXCESS AFT CG NA FWC Label = 124/16 1/1 NA 1= EXCESS AFT CG
CLATDEV CAPTAIN LATERAL DEVIATION bits 17-25+29 (NM) FMGEC(FM) DMC Label = 116 1/2 0.031 >0= RIGHT OF BEAM
CLATDEVD CAPT LATERAL DEVIATION DISPLAYED ON PFD NA FMGEC(FM) DMC Label = 116/12 1/2 NA 1= DISPLAYED
CLATDEVR CAPT LATERAL DEVIATION REQUIRED ON PFD NA FMGEC(FM) DMC Label = 116/11 1/2 NA 1= REQUIRED
CLATP CAPTAIN LATITUDE POSITION (DA) FMGEC(FM) DMC Label = 310 NA NA >0= NORTH
CLATP_S CAPTAIN LATITUDE POSITION Bits 9-19+29 (DA) FMGEC(FM) DMC 1/2 NA NA
CLATP_coarse CAPTAIN LATITUDE POSITION Bits 20-27 (DA) FMGEC(FM) DMC 1/2 0.352 NA
CLATP_fine CAPTAIN LATITUDE POSITION Bits 9-19+29 (DA) FMGEC(FM) DMC 1/2 NA NA
CLBD FMA LONGI. MODE CLIMB DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
CLIMB TCAS UP ADVISORY.CLIMB. (MATRIX 8) NA TCAS DMC Label = 270/24-26 1/1 NA NA
0= AVAILABLE 1= NOT
CLOCKF ARINC CLOCK NOT AVAILABLE NA FDIU Label = 125/150 1/4 NA
AVAILABLE
CLOCKGPS CLOCK SYNCHRONISED BY GPS NA GPS CLOCK Label = 150/11 1/4 NA 1= SYNCHRO. BY GPS
CLONP LONGITUDE POSITION ELAB Bits 9-29 (DA) FMGEC(FM) DMC Label = 311 NA NA >0= EAST
CLONP_S LONGITUDE POSITION Bits 9-19+29 (DA) FMGEC(FM)DMC 1/2 NA NA
CLONP_coarse LONGITUDE POSITION Bits 20-28 (DA) FMGEC(FM) DMC 1/2 0.352 NA
CLONP_fine LONGITUDE POSITION Bits 9-19+29 (DA) FMGEC(FM)DMC 1/2 NA NA
CLRCFL TCAS COMBINATED CONTROL.CLEAR OF CONFLICT. (MATRIX 7) NA TCAS DMC Label = 270/18-20 1/1 NA NA
CLSBUTTON CAPT LS PUSH-BUTTON NA FMGEC(FM) DMC Label = 275/21 1/2 NA 1= ACTIVE
CMACH CALCULATED MACH NUMBER ************** NA CALCULATED WITH ALT & Label = NA NA NA
CMC1F CMC1 FAIL NA DMC Label = 360/18 1/4 NA 1= FAULT
CMCTRF CMC TRANSMITTER FAIL NA FDIU Label = 1/62 NA NA
CNWS CAPTAIN N/WS HANDWHEEL ORDER bits 22-28+29 (DA) BSCU Label = 340 1/1 1.000 NA
COND AIR COND PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
CPTMC1 CAPTAIN MASTER CAUTION ON NA FWC1 Label = 126/15 1/1 NA 1= ON
CPTMC2 CAPTAIN MASTER CAUTION ON NA FWC2 Label = 126/15 1/1 NA 1= ON
CPTMW1 CAPTAIN MASTER WARNING ON NA FWC1 Label = 126/14 1/1 NA 1= ON
CPTMW2 CAPTAIN MASTER WARNING ON NA FWC2 Label = 126/14 1/1 NA 1= ON
CREWAUTO TCAS CREW SELECTION.AUTOMATIC. (MATRIX 10) NA TCAS DMC Label = 016/15-17 1/1 NA NA
CREWSTBY TCAS CREW SELECTION.STANDBY. (MATRIX 10) NA TCAS DMC Label = 016/15-17 1/1 NA NA
CREWTA TCAS CREW SELECTION.TA ONLY.(MATRIX 10) NA TCAS DMC Label = 016/15-17 1/1 NA NA
CRGRSMOW CARGO REST SMOKE NA FWC Label = 124/13 1/1 NA 1= SMOKE
CRUISE CRUISE PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
CSASIV1 CSAS iso valve V1 NA FWC Label = 25 1/1 NA NA
CSASTEMP CSAS temperature NA FWC Label = 25 1/1 1.280 NA
CSDBC CAPTAIN SELECTED DATA BASE CYCLE NA FMGEC(FM) DMC Label = 230 1/62 NA 0= 1ST / 1= 2ND
CSDBD CAPTAIN DATA BASE VALIDITY DAY NA FMGEC(FM) DMC Label = 230 1/62 NA NA
CSDBM CAPTAIN DATA BASE VALIDITY MONTH NA FMGEC(FM) DMC Label = 230 1/62 NA NA
CSTALT CONSTRAINT ALTITUDE bits 19-28 (FT) FMGEC(FG) DMC Label = 102 1/1 64.000 NA
CSWADR3C CAPT SWITCHED ON ADR3 (CAPT) NA DMC Label = 340/21 1/4 NA 1= ADR3 0=ADR1
CSWADR3F CAPT SWITCHED ON ADR3 (F/O) NA DMC Label = 340/21 1/4 NA 1= ADR3 0=ADR1
CSWFM2C CAPT SWITCHED ON FM2 (CAPT) NA DMC Label = 340/25 1/4 NA 1= FM2 0=FM1
CSWFM2F CAPT SWITCHED ON FM2 (F/O) NA DMC Label = 340/25 1/4 NA 1= FM2 0=FM1
CSWIRS3C CAPT SWITCHED ON IRS3 (CAPT) NA DMC Label = 340/23 1/4 NA 1= IRS3 0=IRS1
CSWIRS3F CAPT SWITCHED ON IRS3 (F/O) NA DMC Label = 340/23 1/4 NA 1= IRS3 0=IRS1
CTASSAT CALCULATED TRUE AIRSPEED ************** NA CULATED WITH SAT & CMACH Lab NA NA NA
CTERC CAPTAIN TERRAIN CAUTION NA DMC Label = 055/13 1/1 NA 1= CAUTION
CTERW CAPTAIN TERRAIN WARNING NA DMC Label = 055/14 1/1 NA 1= WARNING
CTLU COMPUTED TLU bits 21-26+29 (Enhanced) (DA) FCSC FCDC Label = 167 1/1 0.703 NA
CTLU1V COMPUTED RUDDER LIMITATION AVAILABILITY USED BY FWC (Enhanced NA FCDC Label = 041/11 1/1 NA 1= NOT AVAILABILITY
CTLU2V COMPUTED RUDDER LIMITATION AVAILABILITY USED BY DMC (Enhanced NA FCDC Label = 041/12 1/1 NA 1= NOT AVAILABILITY
CTQKG CENTRAL TANK FUEL QUANTITY (KG) FCMC DMC Label = 262 1/62 29.030 NA
CTQLB CENTRAL TANK FUEL QUANTITY (LBS) FCMC DMC Label = 262 1/62 64.000 NA
CVERTDEV CAPTAIN VERTICAL DEVIATION bits 21-28+29 (DA) FMGEC(FM) DMC Label = 124 1/2 0.004 >0= LEFT OF BEAM
CVERTDEVD CAPT VERTICAL DEVIATION DISPLAYED ON PFD NA FMGEC(FM) DMC Label = 124/12 1/2 NA 1= DISPLAYED
CVERTDEVR CAPT VERTICAL DEVIATION REQUIRED ON PFD NA FMGEC(FM) DMC Label = 124/11 1/2 NA 1= REQUIRED
CVMSONSD VIDEO SYSTEM CVMS SELECTION ON SD NA DMC Label = 333/15 1/4 NA 1= SELECTED
CWXRABLE CAPTAIN XFR TERR/RADAR DISPLAY ABLE NA DMC Label = 055/25 1/1 NA 1= ABLE
CWXRV CAPTAIN W.X.R VALID NA DMC Label = 055/11 1/1 NA 1= VALID
D1SICEDET1 DETECTOR.1 SEVERITY ICE DETECTED NA 1DD FWC Label = 015/15 1/4 NA 1= SEV ICE DETECTED
D2SICEDET1 DETECTOR.2 SEVERITY ICE DETECTED NA 1DD FWC Label = 015/15 1/4 NA 1= SEV ICE DETECTED
POSITIVE SENSE:
DA DRIFT ANGLE bits 18-27+29 (DA) ADIRS(IRS) DMC Label = 321 1/1 0.088
CLOCKWISE
DALT DISPLAYED ALTITUDE ELAB Bits 14-27+29 (FT) ADIRS(ADC) DMC Label = 200 NA NA NA
DALTC DISPLAYED ALTITUDE COARSE Bits 23-27 (FT) ADIRS(ADC) DMC Label = 200 1/1 NA NA
DALTF DISPLAYED ALTITUDE FINE Bits 14to23+29 (FT) ADIRS(ADC) DMC Label = 200 1/1 4.000 NA
DALTS DISPLAYED ALTITUDE FINE Bits 29 (FT) ADIRS(ADC) DMC Label = 200 1/1 4.000 NA
DAY DAY OF DATE bits 24-29 NA CLOCK/CMC Label = 260 1/62 NA NA
DD1F ICE DETECTOR.1 FAULT NA 1DD FWC Label = 015/17 1/4 NA 1= FAULT
DD1ICEDET DETECTOR.1 ICE DETECTED NA 1DD FWC Label = 015/14 1/4 NA 1= ICE DETECTED
DD2F ICE DETECTOR.2 FAULT NA 1DD FWC Label = 015/17 1/4 NA 1= FAULT
DD2ICEDET DETECTOR.2 ICE DETECTED NA 1DD FWC Label = 015/14 1/4 NA 1= ICE DETECTED
DECKSMOW LOWER DECK STOWAGE SMOKE NA FWC Label = 126/28 1/1 NA 1= WARNING
DESCEND TCAS DOWN ADVISORY.DESCEND. (MATRIX 9) NA TCAS DMC Label = 270/27-29 1/1 NA NA
DESD FMA LONGI. MODE DESCENT DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
1=AT LEAST ONE TA
DETTAD TCAS TA DETECTED NA TCAS DMC Label = 016/21 1/1 NA
DISPLAYED
DFDRF DFDR FAIL NA FDIU Label = 1/62 NA NA
DFDRPLAYF DFDR PLAYBACK RECEIVER FAIL NA FDIU Label = 1/62 NA NA
DFDRTRF DFDR TRANSMITTER FAIL NA FDIU Label = 1/62 NA NA
DH DECISION HEIGHT VALUE bits 16-25 (FT) FMGEC(FM) DMC Label = 370 1/62 1.000 NA
DHD DH DISPLAYED MATRIX.12 NA FMGEC(FM) DMC Label = 155 1/62 NA NA
DLAW DIRECT FLIGHT LAW NA FCPC-FCSC FCDC Label = 040/13 1/1 NA 1= ENGAGED
DMED1 VOR/DME1 DISTANCE bits 20-27 (NM) DME DMC Label = 202 1/4 1.000 NA
DMED2 VOR/DME2 DISTANCE bits 20-27 (NM) DME DMC Label = 202 1/4 1.000 NA
DMEF1 DME.1 FREQUENCY bits 18-29 (MHZ) DME DMC Label = 035 NA 0.050 NA
DMEF2 DME.2 FREQUENCY bits 18-29 (MHZ) DME DMC Label = 035 NA 0.050 NA
DOOR DOOR PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
DROPTRK TCAS COMBINATED CONTROL.DROP TRACK. (MATRIX 7) NA TCAS DMC Label = 270/18-20 1/1 NA NA
DTCLB TCAS DOWN ADVISORY.DON'T CLIMB. (MATRIX 9) NA TCAS DMC Label = 270/27-29 1/1 NA NA
DTCLB1000 TCAS DOWN ADVISORY.DON'T CLIMB >1000. (MATRIX 9) NA TCAS DMC Label = 270/27-29 1/1 NA NA
DTDES TCAS UP ADVISORY.DON'T DESCENT. (MATRIX 8) NA TCAS DMC Label = 270/24-26 1/1 NA NA
DTDES1000 TCAS UP ADVISORY.DON'T DESCENT >1000. (MATRIX 8) NA TCAS DMC Label = 270/24-26 1/1 NA NA
DTO1 DERATED T/O 1 LIMIT MODE SELECTED NA DEC(EEC or ECU) DMC Label = 154 1/1 NA 1=SELECTED
DTO7 DERATED T/O 7 LIMIT MODE SELECTED (EIS2 SPECIFICITY) NA DEC(EEC or ECU) DMC Label = 154 1/1 NA 1=SELECTED
DTO8 DERATED T/O 8 LIMIT MODE SELECTED (EIS2 SPECIFICITY) NA DEC(EEC or ECU) DMC Label = 154 1/1 NA 1=SELECTED
DU3OPER DU3 OPER NA DMC Label = 352/23 1/4 NA 1= ACTIVE
DU4OPER DU4 OPER NA DMC Label = 352/24 1/4 NA 1= ACTIVE
DUALINPUT DUAL INPUT PILOT NA FCPC-FCSC FCDC Label = 046/29 1/1 NA 1= DUAL
DWNADVCOR TCAS COMBINATED CONTROL.DOWN ADVISORY CORRECTIVE. (MATRIX 7 NA TCAS DMC Label = 270/18-20 1/1 NA NA
ECAMADVY SYSTEM PAGE CALLED FOR ADVISORY REASON (EIS1/EIS2) NA DMC Label = 276/23 1/4 NA 1= SYSTEM PAGE CALLED
ECAMCLEAR DMC REQUEST ECAM CLEAR STATUS (EIS2) NA DMC Label = 276/26 1/4 NA 1= ECAM CLEAR STATUS
ECAMECP ECP LIGHT BLINKING (EIS1/EIS2) NA DMC Label = 276/25 1/4 NA 1= ECP LIGHT BLINKING
ECAMFLTPH1 SYSTEM PAGE CALLED FOR FLIGHT PHASE REASON (EIS1) NA DMC Label = 276/24 1/4 NA 1= SYSTEM PAGE CALLED
ECAMFLTPH2 SYSTEM PAGE CALLED FOR FLIGHT PHASE REASON (EIS2) NA DMC Label = 276/24 1/4 NA 1= SYSTEM PAGE CALLED
ECAMMAN1 SYSTEM PAGE CALLED MANUALLY (EIS1) NA DMC Label = 276/26 1/4 NA 1= SYSTEM PAGE CALLED
ECAMMAN2 SYSTEM PAGE CALLED MANUALLY (EIS2) NA DMC Label = 276/24 1/4 NA 1= SYSTEM PAGE CALLED
ECAMWNG SYSTEM PAGE CALLED DUE TO WARNING (EIS1/EIS2) NA DMC Label = 276/27 1/4 NA 1= SYSTEM PAGE CALLED
ECND1 ECAM REQUESTED ON ND1 NA DMC Label = 330/25 1/4 NA 1= REQUESTED ON ND1
ECND2 ECAM REQUESTED ON ND2 NA DMC Label = 330/26 1/4 NA 1= REQUESTED ON ND2
ECPF ECP FAIL NA DMC Label = 360/23 1/4 NA 1= FAULT
EFACTC EFIS ACTIVE ON CAPTAIN SIDE NA DMC (CPT BUS) Label = 330/27 1/4 NA 1= ACTIV. ON CPT SIDE
EFACTFO EFIS ACTIVE ON FIRST-OFFICER SIDE NA DMC (F/O BUS) Label = 330/28 1/4 NA 1= ACTIV. ON F/O SIDE
EFCAEF2S EFIS CAPTAIN SELECTOR ON EFIS.2 NA DMC (CPT BUS) Label = 330/16 1/4 NA 1= CPT ON EFIS 2
1= SELECTED ON OPPOSITE
EFCAOPPS CAPTAIN EFIS SELECTED ON OPPOSITE SIDE NA DMC (CPT BUS) Label = 330/24 1/4 NA
SIDE
1= SELECTED ON OPPOSITE
EFFOOPPS F/O EFIS SELECTED ON OPPOSITE SIDE NA DMC (F/O BUS) Label = 330/24 1/4 NA
SIDE
EGPWSNO E.G.P.W.S OPERATING MODE (NORMAL OPERATION) MATRIX 14 NA DMC Label = 016/24-26 1/4 NA 1= NORMAL OPERATION
EGPWSPEAK EGPWS PEAKS NA DMC Label = 055/16 1/1 NA 1= ACTIVE
EGPWSTER E.G.P.W.S OPERATING MODE (TERRAIN) NA DMC Label = 016/24-26 1/4 NA 1= TERRAIN
EGPWSTEST E.G.P.W.S OPERATING MODE (TEST) NA DMC Label = 016/24-26 1/4 NA 1= TEST
EGT1 EXHAUST GAZ TEMPERATURE ENG.1 bits 18-28 (DC) ADEC(ECU or EEC) DMC Label = 34 1/1 1.000 NA
EGT1W EGT.1 OVER LIMIT NA FWC Label = 100/23 1/1 NA 1= OVER LIMIT
EGT2 EXHAUST GAZ TEMPERATURE ENG.2 bits 18-28 (DC) ADEC(ECU or EEC) DMC Label = 34 1/1 1.000 NA
EGT2W EGT.2 OVER LIMIT NA FWC Label = 100/24 1/1 NA 1= OVER LIMIT
EIS2 EIS2 INSTALLED NA DMC Label = 330/29 1/4 NA 1= INSTALLED
ELECAC ELEC AC PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
ELECDC ELEC DC PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
ELVL LEFT ELEVATOR POSITION bits18-26+29 (DA) FCPC-FCSC FCDC Label = 314 2/1 0.088 >0= NOSE DOWN
ELVLBV ELEVATOR LH BLUE AVAILABILITY NA FCDC Label = 42/24 2/1 NA 1= AVAILABLE
ELVLGV ELEVATOR LH GREEN AVAILABILITY NA FCDC Label = 42/25 2/1 NA 1= AVAILABLE
ELVR RIGHT ELEVATOR POSITION bits18-26+29 (DA) FCPC-FCSC FCDC Label = 334 2/1 0.088 >0= NOSE DOWN
ELVRGV ELEVATOR RH GREEN AVAILABILITY NA FCDC Label = 42/27 2/1 NA 1= AVAILABLE
ELVRYV ELEVATOR RH YELLOW AVAILABILITY NA FCDC Label = 42/26 2/1 NA 1= AVAILABLE
EMERGW EMERGENCY CONFIGURATION NA FWC Label = 124/22 1/1 NA 1= WARNING
EMPTY FMA A/THR EMPTY NA FMGEC(FG) DMC Label = 150 1/1 NA NA
ENERGYW LOW ENERGY NA DMC Label = 040/18 1/1 NA 1= WARNING
ENG SECONDARY ENGINE PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
ENG1BF ENGINE.1 BLEED FAULT NA BMC SDAC Label = 100/15 1/1 NA 1= FAULT
ENG1PB ENG.1 AIR BLEED PUSH BUTTON ON NA BMC SDAC Label = 066/18 1/1 NA 1= ON
ENG2BF ENGINE.2 BLEED FAULT NA BMC SDAC Label = 100/16 1/1 NA 1= FAULT
ENG2PB ENG.2 AIR BLEED PUSH BUTTON ON NA BMC SDAC Label = 067/18 1/1 NA 1= ON
ENGW ENGINES OUT (1+2) NA FWC Label = 100/28 1/1 NA 1= WARNING
ENHANCED ENHANCED FUNCTION INSTALLED NA FCPC-FCSC FCDC Label = 100/22 1/4 NA 1= INSTALLED
ESN1L ENG.1 IDENT LSP NA ADEC(ECU or EEC) EIVMU Label = 0 1/62 NA NA
ESN1M ENG.1 IDENT MSP NA ADEC(ECU or EEC) EIVMU Label = 0 1/62 NA NA
ESN2L ENG.2 IDENT LSP NA ADEC(ECU or EEC) EIVMU Label = 0 1/62 NA NA
ESN2M ENG.2 IDENT MSP NA ADEC(ECU or EEC) EIVMU Label = 0 1/62 NA NA
EVTMKR EVENT MARKER NA EVENT P/B FDIU Label = 1/1 NA 1= EVENT
EWDIM EWD IMAGE ON EWD/DU NA DMC Label = 313/17 1/4 NA 1= ON EWD-DU
EWDIMEWD NONE EWD IMAGE ON THE DISPLAY (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
EWDIMND1D EWD IMAGE ON CAPT ND DU NA DMC Label = 313/19 1/4 NA 1= ON CAPT-DU
EWDIMND2D EWD IMAGE ON F/O ND DU NA DMC Label = 313/20 1/4 NA 1= ON F/O-DU
EWDIMSDD EWD IMAGE ON SD/DU NA DMC Label = 313/18 1/4 NA 1= ON SD-DU
EWDINV EWD FEEDBACK BUS INVALID (DU3) NA DMC Label = 314/13 1/4 NA 1= INVALID
EWDMSG CHECK EWD MSG ACTIVATED NA DMC Label = 334/19 1/4 NA 1= ACTIVE
EWDNOTMONIT EDW NOT MONITORED NA DMC Label = 051/25 1/4 NA 1= NOT MONITORED
EWDOFF EWD/DU OFF NA DMC Label = 314/21 1/4 NA 1= OFF
FADEC1F FADEC 1 FAULT NA FWC Label = 124/11 1/4 NA 1= FAULT
FADEC2F FADEC 2 FAULT NA FWC Label = 124/12 1/4 NA 1= FAULT
FAPU APU FIRE NA FWC Label = 124/15 1/1 NA 1= FIRE
FCMC1F FCMC1 FAULT NA FWC Label = 376/19 1/4 NA 1= FAULT
FCMC2F FCMC2 FAULT NA FWC Label = 376/20 1/4 NA 1= FAULT
FCPC1CL FCPC 1 ON CONTROL LAW (MATRIX 20) NA FCDC Label = 040/19-23 1/4 NA NA
FCPC1F FCPC 1 FAULT NA FWC Label = 040/25 1/4 NA 1= FAULT
FCRGSMOW FWD CARGO SMOKE NA FWC Label = 124/15 1/1 NA 1= SMOKE
FCSC1CL FCSC 1 ON CONTROL LAW (MATRIX 20) NA FCDC Label = 040/19-23 1/4 NA NA
FCSC1F FCSC 1 FAULT NA FWC Label = 040/28 1/4 NA 1= FAULT
FCSC2CL FCSC 2 ON CONTROL LAW (MATRIX 20) NA FCDC Label = 040//19-23 1/4 NA NA
FCSC2F FCSC 2 FAULT NA FWC Label = 040/29 1/4 NA 1= FAULT
FCTL FLIGHT CONTROL PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
FCTR FRAME COUNTER NA FDIU Label = 1/4 1.000 NA
FCUFG1S FG 1/2 PRIORITY NA FCU Label = 272/11 1/1 NA 1= FG1 SELECTED
FD1E FD1 ENGAGED CONFIRMED NA FMGEC(FG) DMC Label = 274/12 1/1 NA 1= ENGAGED
FD2E FD2 ENGAGED CONFIRMED NA FMGEC(FG) DMC Label = 274/13 1/1 NA 1= ENGAGED
FDESARM FINAL DESCENT ARMED NA FMGEC(FG) DMC Label = 274/24 1/1 NA 1= ARMED
FDIUBSCU1F FDIU BSCU SYSTEM 1 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUBSCU2F FDIU BSCU SYSTEM 2 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUCLOCKF FDIU CLOCK INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUCMCF FDIU CMC INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUECHS1F FDIU ECHS1 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUECHS2F FDIU ECHS2 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUEFHS1F FDIU EFHS1 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUEFHS2F FDIU EFHS2 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUEIVMU1F FDIU EIVMU1 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUEIVMU2F FDIU EIVMU2 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUFCDC1F FDIU FCDC1 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUFCDC2F FDIU FCDC2 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUFCUF FDIU FCU INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUFWC1F FDIU FWC1 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUFWC2F FDIU FWC2 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUMDDUF FDIU MDDU INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUSDAC1F FDIU SDAC1 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDIUSDAC2F FDIU SDAC2 INPUT PORT FAILED NA FDIU Label = 1/62 NA NA
FDRSTS DFDR STATUS SIGNAL NA DFDR SDAC Label = 006/14 1/1 NA 1=SET / 0=NOT SET
FDTCMARM AP/FD TCAS mode armed NA EFHS Label = 52 1/1 NA NA
FDTCMENG AP/FD TCAS mode engaged NA EFHS Label = 52 1/1 NA NA
FE1V FE1 VALIDITY NA DMC Label = 340/17 1/4 NA 1= VALID
FE2V FE2 VALIDITY NA DMC Label = 340/18 1/4 NA 1= VALID
FEGPWSI FIRST-OFFICER E.G.P.W.S INSTALLED NA DMC Label = 055/15 1/1 NA 1= INSTALLED
FEGPWSV FIRST-OFFICER E.G.P.W.S VALID NA DMC Label = 055/12 1/1 NA 1= VALID
FENG1 ENGINE.1 FIRE NA FWC Label = 124/11 1/1 NA 1= FIRE
FENG2 ENGINE.2 FIRE NA FWC Label = 124/12 1/1 NA 1= FIRE
FFKG1 FUEL FLOW ENG.1 bits15-28 (KG/H) ADEC(ECU or EEC) DMC Label = 24 NA 1.814 NA
FFKG2 FUEL FLOW ENG.2 bits15-28 (KG/H) ADEC(ECU or EEC) DMC Label = 24 NA 1.814 NA
FFLB1 FUEL FLOW ENG.1 bits15-28 (LBS/H) ADEC(ECU or EEC) DMC Label = 24 NA 4.000 NA
FFLB2 FUEL FLOW ENG.2 bits15-28 (LBS/H) ADEC(ECU or EEC) DMC Label = 24 NA 4.000 NA
FG1DVPFDC FG1 DV DATA SELECTION ON PFD (CAPT) NA DMC Label = 341/16 1/4 NA 1= FG1 0=FG2
FG1DVPFDF FG1 DV DATA SELECTION ON PFD (F/O) NA DMC Label = 341/16 1/4 NA 1= FG1 0=FG2
FG1F FG.1 FAIL NA DMC Label = 361/27 1/4 NA 1= FAULT
FG1PFDC FG1 SELECTED ON PFD (CAPT) NA DMC Label = 341/24 1/4 NA 1= SELECTED
FG1PFDF FG1 SELECTED ON PFD (F/O) NA DMC Label = 341/24 1/4 NA 1= SELECTED
FG2F FG.2 FAIL NA DMC Label = 361/28 1/4 NA 1= FAULT
FINAPPA FINAL APPROACH ACTIVE NA FMGEC(FG) DMC Label = 274/27 1/1 NA 1= ACTIVE
FLAGLSPFDC CAPTAIN FLAG LS ON PFD NA MMR DMC Label = 50/24 1/4 NA 1= ACTIVE
FLAGLSPFDF FIRST-OFFICER FLAG LS ON PFD NA MMR DMC Label = 50/24 1/4 NA 1= ACTIVE
FLALMO Flare low manual order NA FCDC Label = 31 1/1 0.063 NA
FLAP FLAP SURFACE ANGLE bits21-28 (DA) SFCC/FWC DMC Label = 134 1/2 0.250 NA
FLARE FLARE GREEN NA FMGEC(FG) DMC Label = 302/25 1/1 NA 1= HUD FLARE MODE ACTIVE
FLATDEV FIRST-OFFICER LATERAL DEVIATION (NM) FMGEC(FM) DMC Label = 116 1/2 0.031 >0= RIGHT OF BEAM
FLATDEVD F/O LATERAL DEVIATION DISPLAYED ON PFD NA FMGEC(FM) DMC Label = 116/12 1/2 NA 1= DISPLAYED
FLATDEVR F/O LATERAL DEVIATION REQUIRED ON PFD NA FMGEC(FM) DMC Label = 116/11 1/2 NA 1= REQUIRED
FLATP FIRST-OFFICER LATITUDE POSITION (DA) FMGEC(FM) DMC Label = 310 NA NA >0= NORTH
FLATP_S FIRST-OFFICER LATITUDE POSITION Bits 9-19+29 (DA) FMGEC(FM) DMC 1/2 NA NA
FLATP_coarse FIRST-OFFICER LATITUDE POSITION Bits 20-27 (DA) FMGEC(FM) DMC 1/2 0.352 NA
FLATP_fine FIRST-OFFICER LATITUDE POSITION Bits 9-19+29 (DA) FMGEC(FM) DMC 1/2 NA NA
FLEET FLEET IDENT NA FDIU Label = 1/62 NA NA
FLEXGA FMA A/THR FLEX GO AROUND (EIS2 SPECIFICITY) NA FMGEC(FG) DMC Label = 150 1/1 NA NA
FLEXT FLEX TEMPERATURE bits22-28+29 (DC) FADEC(ECU) DMC Label = 151 1/1 1.000 NA
FLONP LONGITUDE POSITION ELAB Bits 9-29 (DA) ADIRS FM DMC Label = 311 NA NA >0= EAST
FLONP_S LONGITUDE POSITION Bits 9-19+29 (DA) ADIRS FM DMC 1/2 NA NA
FLONP_coarse LONGITUDE POSITION Bits 20-28 (DA) ADIRS FM DMC 1/2 0.352 NA
FLONP_fine LONGITUDE POSITION Bits 9-19+29 (DA) ADIRS FM DMC 1/2 NA NA
FLOW1F FLOW CTL VALVE 1 DISAGREE NA BMC SDAC Label = 006/19 1/2 NA 1= DISAGREE
FLOW2F FLOW CTL VALVE 2 DISAGREE NA BMC SDAC Label = 006/19 1/2 NA 1= DISAGREE
FLP1F FLAP 1 FAULT NA SDAC Label = 006/29 1/4 NA 1= FAULT
FLP2F FLAP 2 FAULT NA SDAC Label = 006/29 1/4 NA 1= FAULT
FLPAUTOSET FLAP AUTO SETTING NA SFCC Label = 50/15 1/1 NA 1= ENGAGED
FLPLOCK FLAP LOCKED NA SFCC/FWC DMC Label = 46/14 1/2 NA 1= LOCKED
FLPLVRW FLAP LEVER NOT ZERO NA FWC Label = 126/27 1/1 NA 1= WARNING
FLSBUTTON F/O LS PUSH-BUTTON NA FMGEC(FM) DMC Label = 275/21 1/2 NA 1= ACTIVE
FLT FLIGHT NUMBER NA FMGEC(FM) CMC Label = 237 NA NA NA
FLT1 FLIGHT NUMBER 1 NA FMGEC(FM) CMC Label = 233 1/62 NA NA
FLT_cpt1 FLIGHT NUMBER Character 1 NA FMGEC(FM) CMC 1/62 NA NA
FM1F FM.1 FAIL NA DMC Label = 362/11 1/4 NA 1= FAULT
FM2F FM.2 FAIL NA DMC Label = 362/12 1/4 NA 1= FAULT
FM2PFDC FM2 SELECTED ON PFD (CAPT) NA DMC Label = 341/25 1/4 NA 1= SELECTED
FM2PFDF FM2 SELECTED ON PFD (F/O) NA DMC Label = 341/25 1/4 NA 1= SELECTED
FMAD FMA DISPLAYED NA FMGEC(FG) DMC Label = 274/11 1/1 NA 1= FMA DISPLAYED
FNTO FLAPS NOT IN T/O CONFIGURATION NA FWC Label = 124/16 1/1 NA 1= NOT IN T/O CONF
FNWS FIRST-OFFICER N/WS HANDWHEEL ORDER bits 22-28+29 (DA) BSCU Label = 341 1/1 1.000 NA
FOEF1 EFIS F/O SELECTOR ON EFIS1 NA DMC (F/O BUS) Label = 330/17 1/4 NA 1= ON EFIS 1
FOMC1 FIRST-OFFICER MASTER CAUTION ON NA FWC1 Label = 126/23 1/1 NA 1= ON
FOMC2 FIRST-OFFICER MASTER CAUTION ON NA FWC2 Label = 126/23 1/1 NA 1= ON
FOMW1 FIRST-OFFICER MASTER WARNING ON NA FWC1 Label = 126/22 1/1 NA 1= ON
FOMW2 FIRST-OFFICER MASTER WARNING ON NA FWC2 Label = 126/22 1/1 NA 1= ON
FPAD FMA LONGI. MODE FLIGHT PATH ANGLE DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
FPAIRS FLIGHT PATH ANGLE bits 20-27+29 (DA) ADIRS(IRS) DMC Label = 322 1/1 0.352 >0=UP
FPASPD A/P-A/THR SUB MODE FPA/SPEED NA FMGEC(FG) DMC Label = 145/17 1/1 NA NA
FPLANCV FM FLIGHT PLAN VALID CAPTAIN NA DMC (CPT BUS) Label = 016/13 1/4 NA 0= FLT PLAN DISPLAYED
FPLANFV FM FLIGHT PLAN VALID F/O NA DMC (F/O BUS) Label = 016/13 1/4 NA 0= FLT PLAN DISPLAYED
FROM CITY PAIR FROM C1-4 NA FMGEC CMC NA NA NA
FROMC1 CITY FROM Character 1 NA FMGEC(FM) CMC Label = 040 1/62 NA NA
FROM_cpt1 CITY FROM Character 1 NA FMGEC CMC Label = 040 1/62 NA NA
FSDBC FIRST-OFFICER SELECTED DATA BASE CYCLE NA FMGEC(FM) DMC Label = 230 1/62 NA 0= 1ST / 1= 2ND
FSDBD FIRST-OFFICER DATA BASE VALIDITY DAY NA FMGEC(FM) DMC Label = 230 1/62 NA NA
FSDBM FIRST-OFFICER DATA BASE VALIDITY MONTH NA FMGEC(FM) DMC Label = 230 1/62 NA NA
FSWADR3C F/O SWITCHED ON ADR3 (CAPT) NA DMC Label = 340/22 1/4 NA 1= ADR3 0=ADR2
FSWADR3F F/O SWITCHED ON ADR3 (F/O) NA DMC Label = 340/22 1/4 NA 1= ADR3 0=ADR2
FSWFM1C F/O SWITCHED ON FM1 (CAPT) NA DMC Label = 340/26 1/4 NA 1= FM1 0=FM2
FSWFM1F F/O SWITCHED ON FM1 (F/O) NA DMC Label = 340/26 1/4 NA 1= FM1 0=FM2
FSWIRS3C F/O SWITCHED ON IRS3 (CAPT) NA DMC Label = 340/24 1/4 NA 1= IRS3 0=IRS2
FSWIRS3F F/O SWITCHED ON IRS3 (F/O) NA DMC Label = 340/24 1/4 NA 1= IRS3 0=IRS2
FTERC FIRST-OFFICER TERRAIN CAUTION NA DMC Label = 055/13 1/1 NA 1= CAUTION
FTERW FIRST-OFFICER TERRAIN WARNING NA DMC Label = 055/14 1/1 NA 1= WARNING
FTISFAIL FTIS failure NA FWC Label = 25 1/1 NA NA
FUEL FUEL PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
FULDEP1 THR REVERSER FULLY DEPLOYED ENG.1 NA FADEC(ECU) DMC Label = 274/11 1/1 NA 1= FULLY DEPLOYED
FULDEP2 THR REVERSER FULLY DEPLOYED ENG.2 NA FADEC(ECU) DMC Label = 274/11 1/1 NA 1= FULLY DEPLOYED
FULSTW1 THR REVERSER FULLY STOWED ENG.1 NA FADEC(ECU) DMC Label = 274/17 1/1 NA 1= FULLY STOWED
FULSTW2 THR REVERSER FULLY STOWED ENG.2 NA FADEC(ECU) DMC Label = 274/17 1/1 NA 1= FULLY STOWED
FVERTDEV FIRST-OFFICER VERTICAL DEVIATION bits 21-28+29 (DA) FMGEC(FM) DMC Label = 124 1/2 0.004 >0= LEFT OF BEAM
FVERTDEVD F/O VERTICAL DEVIATION DISPLAYED ON PFD NA FMGEC(FM) DMC Label = 124/12 1/2 NA 1= DISPLAYED
FVERTDEVR F/O VERTICAL DEVIATION REQUIRED ON PFD NA FMGEC(FM) DMC Label = 124/11 1/2 NA 1= REQUIRED
FWC1F FWC.1 FAIL NA DMC Label = 362/13 1/4 NA 1= FAULT
FWC1MESF FWC.1 MESSAGE FAIL NA DMC Label = 362/14 1/4 NA 1= FAULT
FWC2F FWC.2 FAIL NA DMC Label = 362/15 1/4 NA 1= FAULT
FWC2MESF FWC.2 MESSAGE FAIL NA DMC Label = 362/16 1/4 NA 1= FAULT
FWC2S FWC2 MESSAGE BUS SELECTION NA DMC Label = 315/11 1/1 NA 1= FWC2 MESS BUS SEL.
FWCF1 FWC1 FAULT FROM FWC1 NA FWC Label = 124/17 1/4 NA 1= FWC1 FAULT
FWCF2 FWC2 FAULT FROM FWC2 NA FWC Label = 124/17 1/4 NA 1= FWC2 FAULT
FWXRABLE FIRST-OFFICER XFR TERR/RADAR DISPLAY ABLE NA DMC Label = 055/25 1/1 NA 1= ABLE
FWXRV FIRST-OFFICER W.X.R VALID NA DMC Label = 055/11 1/1 NA 1= VALID
GDL GEAR DOWN LOCKED NA LGCIU FWC Label = 024/17 2/1 NA 1= DOWN LOCKED
GLC1 GEN LINE CONTACTOR.1 CLOSED NA ECMU SDAC Label = 003/21 1/4 NA 1= CLOSED
GLC2 GEN LINE CONTACTOR.2 CLOSED NA ECMU SDAC Label = 003/22 1/4 NA 1= CLOSED
GLS1 GLIDESLOPE DEV. ILS1 bits 20-28+29 (óA) ILS DMC Label = 174 1/2 1.339 >0= ABOVE BEAM
GLS1+2 GLIDESLOPE DEV. ILS 1+2 bits 20-28+29 (óA) ILS DMC Label = 174 1/1 1.339 >0= ABOVE BEAM
GLS1DDM GLIDESLOPE DEV. ILS1 bits 20-28+29 (DDM) ILS DMC Label = 174 1/2 0.002 >0= ABOVE BEAM
GLS2 GLIDESLOPE DEV. ILS2 bits 20-28+29 (óA) ILS DMC Label = 174 1/2 1.339 >0= ABOVE BEAM
GLS2DDM GLIDESLOPE DEV. ILS2 bits 20-28+29 (DDM) ILS DMC Label = 174 1/2 0.002 >0= ABOVE BEAM
GLSMESPFDC CAPTAIN GLS MESSAGE DISPLAYED ON PFD NA MMR DMC Label = 50/27 1/4 NA 1= ACTIVE
GLSMESPFDF FIRST-OFFICER GLS MESSAGE DISPLAYED ON PFD NA MMR DMC Label = 50/27 1/4 NA 1= ACTIVE
GND GEAR NOT DOWN NA FWC Label = 126/21 1/1 NA 1= RED ARROW ON L/G ON
GNDL GEAR NOT DOWN LOCKED NA FWC Label = 126/25 1/1 NA 1= NOT DOWN LOCKED
GPSALT GPS ALTITUDE EMITTED BY IRS SELECTED BY THE DMC (Bits 14to27+29) (FT) DMC Label = 076 NA NA NA
GPSALTC PS ALTITUDE EMITTED BY IRS SELECTED BY THE DMC (COARSE) Bits 24to (FT) DMC Label = 076 1/1 NA NA
GPSALTF PS ALTITUDE EMITTED BY IRS SELECTED BY THE DMC (FINE) Bits 14to23+ (FT) DMC Label = 076 1/1 4.000 NA
GPSALTS GPS ALTITUDE EMITTED BY IRS SELECTED BY THE DMC (SIGN) (FT) DMC Label = 076 1/1 4.000 NA
GPWS14 G.P.W.S TERRAIN ALERTS NA GPWS FWC Label = 014/19 1/1 NA 1= WARNING
GPWS5 BASIC G.P.W.S MODE 5 NA GPWS FWC Label = 014/18 1/1 NA 1= WARNING
GPWSF G.P.W.S SYSTEM FAULT NA GPWS FWC Label = 004/14 1/4 NA 1= FAULT
GPWSOFF G.P.W.S TERRAIN OFF NA GPWS SDAC Label = 004/27 1/1 NA 1= OFF
GPWSTF G.P.W.S TERRAIN DETECTION FAULT NA GPWS FWC Label = 004/17 1/4 NA 1= FAULT
GS GROUND SPEED bits 17-26 (KT) ADIRS(IRS) DMC Label = 312 1/1 1.000 NA
GSCPTD FMA LONGI. MODE G/S* DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
GSD GEAR SELECTOR DOWN NA LGCIU FWC Label = 021/23 2/1 NA 1= DOWN
GSPA GROUND SPOILER ARMED NA FCPC FCDC Label = 043/27 2/1 NA 1= ARMED
GSPO GROUND SPOILER OUT NA FCPC FCDC Label = 043/28 2/1 NA 1= OUT
GSTRKD FMA LONGI. MODE G/S DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
GSU GEAR SELECTOR UP NA LGCIU FWC Label = 021/24 2/1 NA 1= UP
GWK A/C GROSS WEIGHT bits 14-28 (KG) FCMC DMC Label = 075 NA 18.144 NA
GWKC A/C GROSS WEIGHT COARSE (KG) FCMC DMC Label = 075 1/62 NA NA
GWKF A/C GROSS WEIGHT FINE (KG) FCMC DMC Label = 075 1/62 NA NA
GWL A/C GROSS WEIGHT bits 14-28 (LBS) FCMC DMC Label = 075 NA 40.000 NA
GWLC A/C GROSS WEIGHT COARSE (LBS) FCMC DMC Label = 075 1/62 NA NA
GWLF A/C GROSS WEIGHT FINE (LBS) FCMC DMC Label = 075 1/62 NA NA
HDG HEADING (DA) ADIRS(IRS) DMC Label = 314 1/1 NA NA
HDGD FMA LATERAL MODE HDG DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
HDGS TRUE OR MAGNETIC HEADING SELECTION NA DMC Label = 340/16 1/1 NA 1= TRUE HDG 0= MAGN HDG
1= TRK-FPA SEL. 0= HDG-V/S
HDGTRKS HEADING/TRACK SELECTED NA FCU DMC Label = 274 1/1 NA SEL. (for EIS2) / 1= HDG-
V/SVL=
HDGW WARNING HEADING DISCREPANCY NA FWC Label = 126/18 1/1 NA 1= WARNING
HF1 H.F.1 MANUAL RADIO TRANSMITTER NA HF1 SDAC Label = 005/14 1/1 NA 1= EMITTING
HF2 H.F.2 MANUAL RADIO TRANSMITTER NA HF2 SDAC Label = 005/14 1/1 NA 1= EMITTING
HPFSOV1 HP FUEL VALVE ENG.1 NA EIVMU Label = 275/21 1/1 NA 1= OPEN
HPFSOV2 HP FUEL VALVE ENG.2 NA EIVMU Label = 275/21 1/1 NA 1= OPEN
HPUOFFC HPU-CAPT OFF NA HUD FWC Label = 065/16 1/4 NA 1= POWER OFF
HPUOFFF HPU-F/O OFF NA HUD FWC Label = 065/16 1/4 NA 1= POWER OFF
HPV1 HIGH PRES.VLV ENG.1 NOT FULLY CLOSED NA BMC DMC Label = 273/15 1/4 NA 1= NOT FULLY CLOSED
HPV2 HIGH PRES.VLV ENG.2 NOT FULLY CLOSED NA BMC DMC Label = 273/15 1/4 NA 1= NOT FULLY CLOSED
HUD1DECL1 HUD1 DECLUTTER 1 NA HUD FWC Label = 065/14 1/4 NA 1= DECLUTTER 1
HUD1DON HUD1 DISPLAY ON NA HUD FWC Label = 065/11 1/4 NA 1= ON
0= SINGLE INSTALLATION 1=
HUD1DUAL SINGLE OR DUAL INSTALLATION PIN-PROGRAM HUD1 NA HUD FWC Label = 065/24 1/4 NA
DUAL INSTALLATION
HUD1FLT HUD 1 - FLIGHT PHASE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD1HEALTH HUD1 HEALTHY NA HUD FWC Label = 014/21 1/4 NA 1= HEALTHY
HUD1ND HUD1 NORMAL DISPLAY NA HUD FWC Label = 065/13 1/4 NA 1= NORMAL DISPLAY
HUD1NONE HUD 1 - NONE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD1ROLOUT HUD 1 - ROLL-OUT PHASE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD1SPARE HUD 1 SPARE NA HUD FWC Label = 065/23 1/4 NA NA
HUD1TAXI HUD 1 - TAXI PHASE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD1TO HUD 1 - TAKE-OFF PHASE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD2DON HUD2 DISPLAY ON NA HUD FWC Label = 065/11 1/4 NA 1= ON
0= SINGLE INSTALLATION 1=
HUD2DUAL SINGLE OR DUAL INSTALLATION PIN-PROGRAM HUD2 NA HUD FWC Label = 065/24 1/4 NA
DUAL INSTALLATION
HUD2FLT HUD 2 - FLIGHT PHASE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD2HEALTH HUD2 HEALTHY NA HUD FWC Label = 013/27 1/4 NA 1= HEALTHY
HUD2ND HUD2 NORMAL DISPLAY NA HUD FWC Label = 065/13 1/4 NA 1= NORMAL DISPLAY
HUD2NONE HUD 2 - NONE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD2ROLOUT HUD 2 - ROLL-OUT PHASE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD2SPARE HUD 2 SPARE NA HUD FWC Label = 065/23 1/4 NA NA
HUD2TAXI HUD 2 - TAXI PHASE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
HUD2TO HUD 2 - TAKE-OFF PHASE (MATRIX 22) NA HUD FWC Label = 065/19-22 1/4 NA 1= SELECTED
0= HUD NOT INSTALLED 1=
HUDINST HUD INSTALLED PIN-PROGRAM NA HUD SDAC Label = 016/28 1/4 NA
HUD INSTALLED
HYD HYD. PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
HYDBP BLUE HYDRAULIC PRESSURE bits 22-27 (PSI) 6JS2 SDAC Label = 174 1/2 64.000 NA
HYDBW HYDRAULIC LOW PRESS BLUE NA FWC Label = 126/23 1/1 NA 1= LOW PRESSURE
HYDGP GREEN HYDRAULIC PRESSURE bits 22-27 (PSI) 6JS1 SDAC Label = 174 1/2 64.000 NA
HYDGW HYDRAULIC LOW PRESS GREEN NA FWC Label = 126/25 1/1 NA 1= LOW PRESSURE
HYDYP YELLOW HYDRAULIC PRESSURE bits 22-27 (PSI) 6JS3 SDAC Label = 174 1/2 64.000 NA
HYDYW HYDRAULIC LOW PRESS YELLOW NA FWC Label = 126/24 1/1 NA 1= LOW PRESSURE
IFECSMO IFEC SMOKE NA FWC Label = 101/11 1/1 NA 1= WARNING
ILSMESPFDC CAPTAIN ILS MESSAGE DISPLAYED ON PFD NA MMR DMC Label = 50/25 1/4 NA 1= ACTIVE
ILSMESPFDF FIRST-OFFICER ILS MESSAGE DISPLAYED ON PFD NA MMR DMC Label = 50/25 1/4 NA 1= ACTIVE
0= VOR MODE SEL ON CPT(IF
ILSVORCS ILS/VOR SELECTION CAPTAIN NA DMC (CPT BUS) Label = 342/22 1/4 NA ROSE VOR/ILS=1) / 1= ILS
MODEVL=
0= VOR MODE SEL ON CPT(IF
ILSVORFS ILS/VOR SELECTION F/O NA DMC (F/O BUS) Label = 342/22 1/4 NA ROSE VOR/ILS=1) / 1= ILS
MODEVL=
IMKR INNER MARKER BEACON PASSAGE NA VOR1 DMC Label = 222/13 1/1 NA 1= PASSAGE
IMPFDND1 PFD IMAGE ON ND1/DU (2) NA DMC Label = 332/19 1/4 NA 1= PFD IMAGE ON ND1 (2)
IMPFDND2 PFD IMAGE ON ND2/DU (5) NA DMC Label = 332/21 1/4 NA 1= PFD IMAGE ON ND2/DU (5)
INPUTPITCH COKPIT TRIM CTL INPUT POS. PITCH INPUT SHAFT SENSOR bits 16-25+29 (DA) FCPC FCDC Label = 016 1/1 0.022 >0= NOSE DOWN
IRS1F IRS.1 FAIL NA DMC Label = 362/19 1/4 NA 1= FAULT
IRS1PFDC IRS1 SELECTED ON PFD (CAPT) NA DMC Label = 341/19 1/4 NA 1= SELECTED
IRS2PFDF IRS2 SELECTED ON PFD (F/O) NA DMC Label = 341/20 1/4 NA 1= SELECTED
ISIFWC1OFF ISIS FWC 1 STATUS (MATRIX 24) - ISIS OFF NA ISIS Label = 270/27-28 1/1 NA NA
ISIFWC1OUT ISIS FWC 1 STATUS (MATRIX 24) - ISIS OUT OF ORDER NA ISIS Label = 270/27-28 1/1 NA NA
ISIFWC1SFD ISIS FWC 1 STATUS (MATRIX 24) - FLIGHT DISPLAY SELECTED (SFD) NA ISIS Label = 270/27-28 1/1 NA NA
ISIFWC1SND ISIS FWC 1 STATUS (MATRIX 24) - NAVIGATION DISPLAY SELECTED (SND) NA ISIS Label = 270/27-28 1/1 NA NA
ISIFWC2OFF ISIS FWC 2 STATUS (MATRIX 25) - ISIS OFF NA ISIS Label = 270/27-28 1/1 NA NA
ISIFWC2OUT ISIS FWC 2 STATUS (MATRIX 25) - ISIS OUT OF ORDER NA ISIS Label = 270/27-28 1/1 NA NA
ISIFWC2SFD ISIS FWC 2 STATUS (MATRIX 25) - FLIGHT DISPLAY SELECTED (SFD) NA ISIS Label = 270/27-28 1/1 NA NA
ISIFWC2SND ISIS FWC 2 STATUS (MATRIX 25) - NAVIGATION DISPLAY SELECTED (SND) NA ISIS Label = 270/27-28 1/1 NA NA
ISIS1F FDIU ISIS INPUT PORT FAILED ** For dual ISIS configuration ** NA FDIU Label = 1/62 NA NA
ISIS2F FDIU ISIS 2 INPUT PORT FAILED ** For dual ISIS configuration ** NA FDIU Label = 1/62 NA NA
ISISALT I.S.I.S ALTITUDE (Bits 14to27+29) (FT) ISIS Label = 203 NA NA NA
ISISALTC I.S.I.S ALTITUDE COARSE Bits 23to27 (FT) ISIS Label = 203 1/1 NA NA
ISISALTF I.S.I.S ALTITUDE FINE SCALE Bits 14to22 (FT) ISIS Label = 203 1/1 NA NA
ISISALTS I.S.I.S ALTITUDE SIGNE Bits 29 (FT) ISIS Label = 203 1/1 NA NA
ISISANEMOF DIU ISIS ANEMOMETRIC INPUT PORT FAILED ** For single ISIS configuration NA FDIU Label = 1/62 NA NA
ISISCAS I.S.I.S CALIBRATED AIRSPEED bits16-27 (KT) ISIS Label = 206 1/1 0.125 NA
1= DUAL CONF 0= SINGLE
ISISDUAL ISIS SINGLE/DUAL CONF NA ISIS CMC Label = 162/18 1/4 NA
CONF
ISISINERTF FDIU ISIS INERTIAL INPUT PORT FAILED ** For single ISIS configuration ** NA FDIU Label = 1/62 NA NA
ISISINST ISIS INSTALLED NA ISIS CMC Label = 157/16 1/4 NA 1= INSTALLED
ISISLATG I.S.I.S BODY LATERAL ACCELERATION bits19-27+29 (G) ISIS Label = 332 1/1 0.004 >0= RH SIDESLIP
ISISPTCH I.S.I.S PITCH ATTITUDE bits20-27+29 (DA) ISIS Label = 324 4/1 0.352 >0= NOSE UP
ISISROLL I.S.I.S ROLL ATTITUDE bits20-28+29 (DA) ISIS Label = 325 2/1 0.352 >0= RH WING DOWN
ISISSBARO I.S.I.S BARO REFERENCE Bits 15-26 (MB) ISIS Label = 234 1/4 NA NA
K1K2S1 K1 K2 SELECTED ENG1 NA FWC Label = 104/11 1/1 NA 1= SELECTED
K1K2S2 K1 K2 SELECTED ENG2 NA FWC Label = 104/12 1/1 NA 1= SELECTED
K3S1 K3 SELECTED ENG1 NA FWC Label = 104/14 1/1 NA 1= SELECTED
K3S2 K3 SELECTED ENG2 NA FWC Label = 104/15 1/1 NA 1= SELECTED
K4K5K6S1 K4 K5 K6 SELECTED ENG1 NA FWC Label = 104/17 1/1 NA 1= SELECTED
K4K5K6S2 K4 K5 K6 SELECTED ENG2 NA FWC Label = 104/18 1/1 NA 1= SELECTED
LANDARM LAND ARMED NA FMGEC(FG) DMC Label = 274/26 1/1 NA 1= ARMED
LANDTRK LAND GREEN NA FMGEC(FG) DMC Label = 300/14 1/1 NA 1= ACTIVE
LATG LATERAL ACCELERATION bits19-27+29 (G) LA SDAC Label = 332 4/1 0.004 >0= RH SIDESLIP
LATGCHK LAT ACCEL. CHECK NOT RUN NA FDIU 1/62 NA NA
LATGCHKF LAT ACCEL. CHECK FAIL NA FDIU 1/62 NA NA
1= AMBER WARNING / 0= RED
LAVSMORED LAVATORY SMOKE ALERT NA FWC Label = 016/11 1/1 NA
WARNING
LAVSMOW LAVATORY SMOKE NA FWC Label = 124/16 1/1 NA 1= SMOKE
LEVPOS0 SLAT-FLAP LEVER POSITION 0 NA SFCC FWC Label = 137/11 1/1 NA NA
LEVPOSF SLAT-FLAP LEVER POSITION F NA SFCC FWC Label = 137/15 1/1 NA NA
LGCIU1F LGCIU.1 FAIL NA DMC Label = 362/22 1/4 NA 1= FAULT
LGCIU2F LGCIU.2 FAIL NA DMC Label = 362/23 1/4 NA 1= FAULT
LHGNUL LH GEAR NOT UP LOCKED NA LGCIU FWC Label = 021/13 2/1 NA 1= NOT UP LOCKED
LHSQUAT L/G LEFT SQUAT SWITCH NA LGCIU FWC Label = 020/28 4/1 NA 1= ON GROUND
LHWGLEAK LEFT WING LEAK MEMORIZED NA BMC FWC Label = 100/19 1/2 NA 1= LEAK
LI1TQKG LEFT INNER 1 TANK FUEL QUANTITY (KG) FCMC DMC Label = 257 1/62 29.030 NA
LI1TQLB LEFT INNER 1 TANK FUEL QUANTITY (LBS) FCMC DMC Label = 257 1/62 64.000 NA
LOC1 LOCALIZER DEV.ILS1 bits 18-28+29 (óA) ILS DMC Label = 173 1/2 0.189 >0= LEFT OF BEAM
LOC1+2 LOCALIZER DEV.ILS 1+2 bits 18-28+29 (óA) ILS DMC Label = 173 1/1 0.189 >0= LEFT OF BEAM
LOC1DDM LOCALIZER DEV.ILS1 bits 18-28+29 (DDM) ILS DMC Label = 173 1/2 NA >0= LEFT OF BEAM
LOC2 LOCALIZER DEV.ILS2 bits 18-28+29 (óA) ILS DMC Label = 173 1/2 0.189 >0= LEFT OF BEAM
LOC2DDM LOCALIZER DEV.ILS2 bits 18-28+29 (DDM) ILS DMC Label = 173 1/2 NA >0= LEFT OF BEAM
LOCBCCPTD FMA LATERAL MODE LOC B/C* DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
LOCBCTRKD FMA LATERAL MODE LOC B/C DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
LOCCPTD FMA LATERAL MODE LOC* DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
LOCTRKD FMA LATERAL MODE LOC DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
LONG LONGITUDINAL ACCELERATION bits19-27+29 (G) LA SDAC Label = 331 4/1 0.004 <0= ACCELERATION
LONGCHK LONG ACCEL. CHECK NOT RUN NA FDIU 1/62 NA NA
LONGCHKF LONG ACCEL. CHECK FAIL NA FDIU 1/62 NA NA
LOTQKG LEFT OUTER TANK FUEL QUANTITY (KG) FCMC DMC Label = 256 1/62 29.030 NA
LOTQLB LEFT OUTER TANK FUEL QUANTITY (LBS) FCMC DMC Label = 256 1/62 64.000 NA
LPFSOV1 LP FUEL VALVE FULLY CLOSED ENG.1 NA 400QG1 SDAC Label = 001/15 1/1 NA 1= Fully Closed
LPFSOV2 LP FUEL VALVE FULLY CLOSED ENG.2 NA 400QG2 SDAC Label = 001/17 1/1 NA 1= Fully Closed
LRELVF LEFT + RIGHT ELEVATORS FAULT NA FWC Label = 124/21 1/1 NA 1= FAULT
LSDD DISTANCE LS DISPLAYED bits 16-27 (NM) DME DMC Label = 036 1/4 0.063 NA
MACHD MACH (A/THR) NA FMGEC(FG) DMC Label = 274/25 1/1 NA 1= DISPLAYED
MACHFCUS MACH SELECTION NA FCU Label = 270/19 1/1 NA 1= MACH SEL 0= SPEED SEL
MANDTOD FMA A/THR MAN DTO DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
MANFLXD FMA A/THR MAN FLEX DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
MANMCTD FMA A/THR MAN MCT DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
MANTHRD FMA A/THR MAN THR DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
MANTOGAD FMA A/THR MAN TOGA DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
MATRIX1 FMA A/THR MODE MATRIX 1 BITS 24 to 28 NA FMGEC(FG) DMC Label = 150 1/1 NA NA
MATRIX10 TCAS CREW SELECTION MATRIX 10 NA TCAS DMC Label = 016/15-17 1/1 NA NA
MATRIX11 SELECTED SPEED ORIGINE MATRIX 11 NA FCU/FG DMC Label = 274/21-22 1/1 NA NA
MATRIX12 BARO DISPLAYED MATRIX.12 (EIS2 ONLY) NA FMGEC(FM) DMC Label = 155 1/62 NA NA
MATRIX13 RADAR OPERATING MODE MATRIX 13 NA DMC Label = 016/27-29 1/4 NA NA
MATRIX14 E.G.P.W.S OPERATING MODE MATRIX 14 NA DMC Label = 016/24-26 1/4 NA NA
MATRIX15C EFIS RANGE ND ON CAPT MATRIX 15 NA DMC Label = 215/28 1/4 NA NA
MATRIX15F EFIS RANGE ND ON F/O MATRIX 15 NA DMC Label = 215/28 1/4 NA NA
MATRIX16C MODE DISPLAYED ON ND CAPT MATRIX 16 NA DMC Label = 214/26-28 1/4 NA NA
MATRIX16F MODE DISPLAYED ON ND F/O MATRIX 16 NA DMC Label = 214 1/4 NA NA
MATRIX17 ECAM DISPLAYED IMAGE MATRIX 17 NA DMC Label = 251/24-28 1/4 NA NA
MATRIX18 ECAM DISPLAYED IMAGE MODE MATRIX 18 NA DMC Label = 276/23-27 1/4 NA NA
MATRIX19C CAPTAIN NAVIGATION MODE MATRIX 19 NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA NA
MATRIX19F FIRST-OFFICER NAVIGATION MODE MATRIX 19 NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA NA
MATRIX2 FMA LATERAL MODE MATRIX 2 BITS 25 to 28 NA FMGEC DMC Label = 152 1/1 NA NA
MATRIX20 COMPUTER ON CONTROL LAW MATRIX 20 NA FCDC Label = 040/19-23 1/4 NA NA
MATRIX21 SLAT-FLAP LEVER POSITION MATRIX 21 NA SFCC FWC Label = 137/11-15 1/1 NA NA
MATRIX221 HUD 1 - MATRIX 22 NA HUD FWC Label = 065/19-22 1/4 NA NA
MATRIX222 HUD 2 - MATRIX 22 NA HUD FWC Label = 065/19-22 1/4 NA NA
MATRIX24 ISIS FWC 1 STATUS MATRIX 24 NA ISIS Label = 270/27-28 1/1 NA NA
MATRIX25 ISIS FWC 2 STATUS MATRIX 25 NA ISIS Label = 270/27-28 1/1 NA NA
MATRIX3 FMA LONGITUDINAL MODES MATRIX 3 BITS 25 to 28 NA FMGEC DMC Label = 153 1/1 NA NA
MATRIX50 MMR1 MODE NA MMR DMC Label = 033 1/4 NA NA
MATRIX51 MMR2 MODE NA MMR DMC Label = 033 1/4 NA NA
MATRIX6 DERATED T/O LIMIT MODE SELECTED MATRIX 6 NA EC(EEC or ECU) DMC Label = 154/1 1/1 NA NA
MATRIX7 TCAS COMBINATED CONTROL MATRIX 7 NA TCAS DMC Label = 270/18-20 1/1 NA NA
MATRIX8 TCAS UP ADVISORY MATRIX 8 NA TCAS DMC Label = 270/24-26 1/1 NA NA
MATRIX9 TCAS DOWN ADVISORY MATRIX 9 NA TCAS DMC Label = 270/27-29 1/1 NA NA
MDADHD MDA/MDH DISPLAYED MATRIX.12 NA FMGEC(FM) DMC Label = 155 1/62 NA NA
MDAMDH HEIGHT VALUE MDA/MDH (BITS 12to26) (FT) FMGEC DMC Label = 367 NA NA NA
MDAMDHC HEIGHT VALUE MDA/MDH COARSE (FT) FMGEC(FM) DMC Label = 367 1/62 2048.000 NA
MDAMDHF HEIGHT VALUE MDA/MDH FINE bits 12-23 (FT) FMGEC(FM) DMC Label = 367 1/62 1.000 NA
MDDUTRF MDDU TRANSMITTER FAIL NA FDIU Label = 1/62 NA NA
MICROSW1 MICROSWITCH DIGITAL ELECTRONIC MODULE.1 NA FCPC FCDC Label = 100/26 1/1 NA 1= HOLD PRIORITY
MLSMESPFDC CAPTAIN MLS MESSAGE DISPLAYED ON PFD NA MMR DMC Label = 50/26 1/4 NA 1= ACTIVE
MLSMESPFDF FIRST-OFFICER MLS MESSAGE DISPLAYED ON PFD NA MMR DMC Label = 50/26 1/4 NA 1= ACTIVE
MMKR MIDDLE MARKER BEACON PASSAGE NA VOR1 DMC Label = 222/12 1/1 NA 1= PASSAGE
MMOPT MMO protection threshold NA FCDC Label = 33 1/1 0.008 NA
MNADC MACH NUMBER bits 19-26 NA ADIRS(ADC) DMC Label = 205 1/1 0.004 NA
MONTH MONTH OF DATE bits 19-23 NA CLOCK/CMC Label = 260 1/62 NA NA
MSTLA1 ENG 1 MASTER LEVER OFF NA FWC Label = 015/22 1/1 NA 1= OFF
MSTLA2 ENG 2 MASTER LEVER OFF NA FWC Label = 017/22 1/1 NA 1= OFF
N1A1 N1 ACTUAL ENG.1 ELAB bits16-28 (%) ADEC(EEC or ECU) DMC Label = 34 NA NA NA
N1A2 N1 ACTUAL ENG.2 ELAB bits16-28 (%) ADEC(EEC or ECU) DMC Label = 34 NA NA NA
N1C1 N1 COMMAND ENG.1 bits 22-28 (%) U or EEC) DMC Label = 341 or 254 1/2 2.000 NA
N1C2 N1 COMMAND ENG.2 bits 22-28 (%) U or EEC) DMC Label = 341 or 254 1/2 2.000 NA
N1L1 N1 LIMIT ENG.1 bits17-28 (%) ADEC(EEC or ECU) DMC Label = 33 1/1 0.063 NA
N1L2 N1 LIMIT ENG.2 bits17-28 (%) ADEC(EEC or ECU) DMC Label = 33 1/1 0.063 NA
N1T ENGINE THRUST TARGET N1 bits 21-28 (%) FMGEC(FG) FCU Label = 343 1/4 1.000 NA
N1V1 N1 VIBRATION ENG.1 bits 20-26 (CU) EIVMU Label = 135 1/1 0.100 NA
N2A1 N2 Actual Eng 1 bits 17-28 (%) ADEC(ECU or EEC) DMC Label = 34 1/1 0.063 NA
N2A2 N2 Actual Eng 2 bits 17-28 (%) ADEC(ECU or EEC) DMC Label = 34 1/1 0.063 NA
NAI1F ANTI-ICE VALVE FAULT ENG.1 NA 1DN SDAC Label = 001/26 1/2 NA 1= FAULT
NAI1ON ANTI-ICE PUSH-BUTTON ON ENG.1 NA 1DN SDAC Label = 001/17 1/2 NA 1= ON
NAI1S NACELLE ANTI-ICE ENG 1 SELECTED NA WHC1 SDAC Label = 013/16 1/2 NA 1= SELECTED ON
NAI2F ANTI-ICE VALVE FAULT ENG.2 NA 1DN SDAC Label = 001/27 1/2 NA 1= FAULT
NAI2ON ANTI-ICE PUSH-BUTTON ON ENG.2 NA 1DN SDAC Label = 001/18 1/2 NA 1= ON
NAI2S NACELLE ANTI-ICE ENG 2 SELECTED NA WHC2 SDAC Label = 005/17 1/2 NA 1= SELECTED ON
NAVACCC NAVIGATION ACCURACY CAPTAIN NA FMGEC DMC Label = 255/16 1/4 NA 1= HIGH
NAVACCF NAVIGATION ACCURACY FIRST-OFFICER NA FMGEC(FM) DMC Label = 255/16 1/4 NA 1= HIGH
NAVD FMA LATERAL MODE NAV DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
NAVHDG NAV SUB MODE HEADING NA FMGEC(FG) DMC Label = 176/21 1/1 NA NA
NAVHNONE NAV SUB MODE NONE NA FMGEC(FG) DMC Label = 176 1/1 NA NA
NAVHPATH NAV SUB MODE HORIZONTAL PATH NA FMGEC(FG) DMC Label = 176/20 1/1 NA NA
NAVLCSTATF NAV L CAPT STATIC FAULT (AMBER ALERT) NA FWC Label = 101/19 1/1 NA 1= FAULT
NAVLFSTATF NAV L F/O STATIC FAULT (AMBER ALERT) NA FWC Label = 101/20 1/1 NA 1= FAULT
NAVRCSTATF NAV R CAPT STATIC FAULT (AMBER ALERT) NA FWC Label = 101/21 1/1 NA 1= FAULT
NAVRFSTATF NAV R F/O STATIC FAULT (AMBER ALERT) NA FWC Label = 101/22 1/1 NA 1= FAULT
NAVSUBM NAV SUB MODE (MATRIX-4) NA FMGEC(FG) DMC Label = 176 1/1 NA NA
NAVTRK NAV SUB MODE TRACK NA FMGEC(FG) DMC Label = 176/22 1/1 NA NA
NBRKP1B NORMAL BRAKE PRESSURE 1 bits 23-28 (Bar) BSCU Label = 300 1/4 4.413 NA
NBRKP1P NORMAL BRAKE PRESSURE 1 bits 23-28 (PSI) BSCU Label = 300 1/4 64.000 NA
NBRKP8B NORMAL BRAKE PRESSURE 8 bits 23-28 (BAR) BSCU Label = 307 1/4 64.000 NA
NBRRADET TCAS NUMBER OF RA DETECTED NA TCAS DMC Label = 040/24-26 1/1 NA NA
NCCL NO COMPUTER ON CONTROL LAW (MATRIX 20) NA FCDC Label = 040/19-23 1/4 NA NA
ND1C CPT ND/DU (2) VALID NA DMC (CPT BUS) Label = 332/16 1/4 NA 1= VALID
ND1FEED ND1/DU (2) FEEDBACK BUS INVALID NA DMC Label = 334/11 1/4 NA 1= INVALID
ND1MSG CHECK ND1 MSG ACTIVATED NA DMC Label = 334/26 1/4 NA 1= ACTIVE
ND1OFF CPT ND/DU (2) OFF NA DMC Label = 330/22 1/4 NA 1= OFF
ND2FEED ND2/DU (5) FEEDBACK BUS INVALID NA DMC Label = 334/12 1/4 NA 1= INVALID
ND2FO CPT ND/DU (2) VALID NA DMC (F/O) Label = 332/16 1/4 NA 1= VALID
ND2MSG CHECK ND2 MSG ACTIVATED NA DMC Label = 334/27 1/4 NA 1= ACTIVE
ND2OFF F/O ND/DU (5) OFF NA DMC Label = 330/23 1/4 NA 1= OFF
ND2V F/O ND/DU (5) VALID NA DMC (CAPT BUS) Label = 332/17 1/4 NA 1= VALID
NIC CAPTAIN NAVIGATION MODE.N IRS ONLY. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIDDC CAPTAIN NAVIGATION MODE.N IRS/DME/DME. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIDDF FIRST-OFFICER NAVIGATION MODE.N IRS/DME/DME. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIDLC CAPTAIN NAVIGATION MODE.N IRS/DME/LOC. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIDLF FIRST-OFFICER NAVIGATION MODE.N IRS/DME/LOC. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIDMC CAPTAIN NAVIGATION MODE.N IRS/DME/MLS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIDMF FIRST-OFFICER NAVIGATION MODE.N IRS/DME/MLS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIF FIRST-OFFICER NAVIGATION MODE.N IRS ONLY. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIGC CAPTAIN NAVIGATION MODE.N IRS/GPS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIGF FIRST-OFFICER NAVIGATION MODE.N IRS/GPS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIGLC CAPTAIN NAVIGATION MODE.N IRS/GPS/LOC. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIGLF FIRST-OFFICER NAVIGATION MODE.N IRS/GPS/LOC. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIGMC CAPTAIN NAVIGATION MODE.N IRS/GPS/MLS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIGMF FIRST-OFFICER NAVIGATION MODE.N IRS/GPS/MLS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIIVDC CAPTAIN NAVIGATION MODE.N IRS/VOR/DME. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIIVDF FIRST-OFFICER NAVIGATION MODE.N IRS/VOR/DME. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NILC CAPTAIN NAVIGATION MODE.N IRS/LOC. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NILF FIRST-OFFICER NAVIGATION MODE.N IRS/LOC. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIMC CAPTAIN NAVIGATION MODE.N IRS/MLS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIMF FIRST-OFFICER NAVIGATION MODE.N IRS/MLS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIVLC CAPTAIN NAVIGATION MODE.N IRS/VOR/LOC. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIVLF FIRST-OFFICER NAVIGATION MODE.N IRS/VOR/LOC. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIVMC CAPTAIN NAVIGATION MODE.N IRS/VOR/MLS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NIVMF FIRST-OFFICER NAVIGATION MODE.N IRS/VOR/MLS. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NLAW NORMAL FLIGHT LAW NA FCPC-FCSC FCDC Label = 040/11 1/1 NA 1= ENGAGED
NNC CAPTAIN NAVIGATION MODE.NO NAV. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NNF FIRST-OFFICER NAVIGATION MODE.NO NAV. (MATRIX 19) NA FMGEC(FM) DMC Label = 255/11-14 1/4 NA 1= ACTIVE
NOADV TCAS COMBINATED CONTROL.NO ADVISORY. (MATRIX 7) NA TCAS DMC Label = 270/18-20 1/1 NA NA
NODHD NO DH DISPLAYED MATRIX.12 NA FMGEC(FM) DMC Label = 155 1/62 NA NA
NODOWN TCAS DOWN ADVISORY.NO DOWN ADVISORY. (MATRIX 9) NA TCAS DMC Label = 270/27-29 1/1 NA NA
NODTO NO LIMIT MODE SELECTED NA ADEC(EEC or ECU) DMC Label = 15 1/1 NA 1=SELECTED
NOGNUL NOSE GEAR NOT UP LOCKED NA LGCIU FWC Label = 021/15 2/1 NA 1= NOT UP LOCKED
NOISETHR1 FMA A/THR NOISE THR1 (EIS2 SPECIFICITY) NA FMGEC(FG) DMC Label = 150 1/1 NA NA
NOISETHR2 FMA A/THR NOISE THR2 (EIS2 SPECIFICITY) NA FMGEC(FG) DMC Label = 150 1/1 NA NA
NONED NONE MATRIX.12 (EIS2 ONLY) NA FMGEC(FM) DMC Label = 155 1/62 NA NA
NORBRKF NORMAL BRAKE FAULT NA BSCU Label = 026/21 1/1 NA 1= FAULT
NOSQUAT L/G NOSE SQUAT SWITCH NA LGCIU FWC Label = 020/15 4/1 NA 1= COMPRESSED
NOUP TCAS UP ADVISORY.NO UP ADVISORY. (MATRIX 8) NA TCAS DMC Label = 270/24-26 1/1 NA NA
NSRA1 RADIO HEIGHT NO.1 (NOT SIGNED) bits 16-26 (FT) RA DMC Label = 164 1/2 1.000 NA
NSRA2 RADIO HEIGHT NO.2 (NOT SIGNED) bits 16-26 (FT) RA DMC Label = 164 1/2 1.000 NA
NWSAP N/WS AUTOPILOT ORDER bits 22-28+29 (DA) BSCU Label = 342 1/1 0.250 NA
NWSDMD N/WS DEMAND ANGLE bits 22-28+29 (DA) BSCU Label = 153 1/1 1.000 NA
NWSMSTR NOSE WHEEL ANGLE (CFM) bits 20-28+29 (DA) BSCU Label = 334 1/1 0.250 NA
NWSRUDP N/WS RUDDER PEDAL ORDER bits 22-28+29 (DA) BSCU Label = 343 1/1 0.250 NA
NWSSLV NOSE WHEEL ANGLE (CFM) bits 20-28+29 (DA) BSCU Label = 336 1/1 0.250 NA
OIP1 OIL PRESSURE ENG.1 bits 17-27 (PSI) FADEC(ECU) DMC Label = 317 1/1 0.125 NA
OIP2 OIL PRESSURE ENG.2 bits 17-27 (PSI) FADEC(ECU) DMC Label = 317 1/1 0.125 NA
OIQ1 OIL QUANTITY ENG.1 bits 17-27 (USQG) ADEC(ECU or EEC) DMC Label = 07 1/1 0.016 NA
OIQ2 OIL QUANTITY ENG.2 bits 17-27 (USQG) ADEC(ECU or EEC) DMC Label = 07 1/1 0.016 NA
OIT1 OIL TEMPERATURE ENG.1 bits 18-27+29 (DC) ADEC(EEC or ECU) EIVMU Label = 3 1/1 0.250 NA
OIT2 OIL TEMPERATURE ENG.2 bits 18-27+29 (DC) ADEC(EEC or ECU) EIVMU Label = 3 1/1 0.250 NA
OLP1 ENG1 OIL LOW PRESS NA FWC Label = 124/17 1/1 NA 1= LOW PRESS
OLP2 ENG2 OIL LOW PRESS NA FWC Label = 124/18 1/1 NA 1= LOW PRESS
OMKR OUTER MARKER BEACON PASSAGE NA VOR1 DMC Label = 222/11 1/1 NA 1= PASSAGE
OPCLBD FMA LONGI. MODE OPEN CLIMB DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
OPDESD FMA LONGI. MODE OPEN DESCENT DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
OVERN11 ENG.1 N1 OVER LIMIT NA FWC Label = 100/11 1/1 NA 1= OVER LIMIT
PAIDET PRIMARY AUTO-ICE DETECTION SYSTEM INSTALLED NA DAC (PIN-PROG SDAC) Label = 007 1/2 NA 1= INSTALLED
PAXBRDBSMO SMOKE PAX BROADBAND NA FWC Label = 101/16 1/1 NA 1= SMOKE
PBRKON PARK BRAKE ON NA BSCU SDAC Label = 005/24 1/1 NA 1= ON
PBRKW PARKING BRAKE ON NA FWC Label = 124/27 1/1 NA 1= WARNING
PCK1OFF PACK CONTROLER.1 PUSH-BUTTON OFF NA BMC SDAC Label = 006/17 1/2 NA 1= P/B OFF
PCK2OFF PACK CONTROLER.2 PUSH-BUTTON OFF NA BMC SDAC Label = 006/14 1/2 NA 1= P/B OFF
PCP1 ENG.1 PRE COOLER INLET PRESSURE bits 19-28 (PSI) BMC SDAC Label = 142 1/1 0.500 NA
PCP2 ENG.2 PRE COOLER INLET PRESSURE bits 19-28 (PSI) BMC SDAC Label = 143 1/1 0.500 NA
PCT1 ENG.1 PRE COOLER OUTLET TEMPERATURE bits 19-28 (DC) BMC SDAC Label = 140 1/4 0.500 NA
PCT2 ENG.2 PRE COOLER OUTLET TEMPERATURE bits 19-28 (DC) BMC SDAC Label = 141 1/4 0.500 NA
PFD1C CPT PFD/DU (1) VALID NA DMC (CPT BUS) Label = 332/14 1/4 NA 1= VALID
PFD1FEED PFD1/DU (1) FEEDBACK BUS INVALID NA DMC Label = 334/13 1/4 NA 1= INVALID
PFD1MSG CHECK PFD1 MSG ACTIVATED NA DMC Label = 334/23 1/4 NA 1= ACTIVE
PFD1OFF CPT PFD/DU (1) OFF NA DMC Label = 330/20 1/4 NA 1= OFF
PFD2FEED PFD2/DU (6) FEEDBACK BUS INVALID NA DMC Label = 334/14 1/4 NA 1= INVALID
PFD2FO CPT PFD/DU (1) VALID NA DMC (F/O) Label = 332/14 1/4 NA 1= VALID
PFD2MSG CHECK PFD2 MSG ACTIVATED NA DMC Label = 334/24 1/4 NA 1= ACTIVE
PFD2OFF F/O PFD/DU (6) OFF NA DMC Label = 330/21 1/4 1.000 1= OFF
PFD2V F/O PFD/DU (6) VALID NA DMC (CAPT BUS) Label = 332/15 1/4 NA 1= VALID
PFDCPTMONIT PFD CAPTAIN NOT MONITORED NA DMC Label = 051/24 1/4 NA 1= NOT MONITORED
PGPSC GPS PRIMARY CAPT SIDE NA FMGEC(FM) DMC Label = 055/28 1/1 NA 1= PRIMARY
PGPSF GPS PRIMARY F/O SIDE NA FMGEC(FM) DMC Label = 055/28 1/1 NA 1= PRIMARY
PH FLIGHT PHASE bits 25-29 NA FWC Label = 126 1/1 NA NA
PINBCKPSPDACT PIN PROG BACKUP SPEED SCALE ACTIVATED NA DMC Label = 331/14 1/4 NA 1= ACTIVATED
PINPROG PIN PROG TCAS STATUS NA TCAS DMC Label = 154/26 1/1 NA 1= TCAS ACTIVE
PLANC PLAN MODE DISPLAYED ON ND CAPT (MATRIX 16) NA DMC Label = 214/26-28 1/4 NA NA
PLANF PLAN MODE DISPLAYED ON ND F/O (MATRIX 16) NA DMC Label = 214 1/4 NA NA
PLAYBACKF PLAYBACK FAIL NA FDIU 1/62 NA NA
PRESS CAB. PRESS PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
PREVENT TCAS COMBINATED CONTROL.PREVENTIVE. (MATRIX 7) NA TCAS DMC Label = 270/18-20 1/1 NA NA
PRI1 POSITIVE ENG.1 RELIGHT INDICATION NA DMC Label = 046/25 1/1 NA 1= DISPLAYED
PRI2 POSITIVE ENG.2 RELIGHT INDICATION NA DMC Label = 046/26 1/1 NA 1= DISPLAYED
PROBEPB PROBE WINDOW HEAT P/B NA 6DGA SDAC Label = 001/25 1/2 NA 1= P/B ON
PROGID RECORD VERSION (PROG IDENT) MATRIX NA FDIU Label = 1/62 NA 4= A330-GE 256W/S
PRV1 PRES.REG.VLV ENG.1 NOT FULLY CLOSED NA BMC DMC Label = 273/17 1/4 NA 1= NOT FULLY CLOSED
PRV2 PRES.REG.VLV ENG.2 NOT FULLY CLOSED NA BMC DMC Label = 273/17 1/4 NA 1= NOT FULLY CLOSED
PS31 PS3 Eng 1 bits 19-28 (PSI) ADEC(EEC or ECU) DMC Label = 26 1/1 1.000 NA
PS32 PS3 Eng 2 bits 19-28 (PSI) ADEC(EEC or ECU) DMC Label = 26 1/1 1.000 NA
PTCH PITCH ATTITUDE bits20-27+29 (DA) ADIRS(IRS) DMC Label = 324 4/1 0.352 >0= NOSE UP
PTCHW WARNING PITCH DISCREPANCY NA FWC Label = 126/20 4/1 NA 1= WARNING
PVIC PVI P/B ON (CPT SIDE) NA PVI SDAC Label = 006/16 1/1 NA 1= ON
PWSAC PREDICTIVE WINDSHEAR AMBER CAUTION NA EATHER_RADAR DMC Label = 055 1/1 NA 1= WARNING
PWSEF PREDICTIVE WINDSHEAR EXTERNAL FAILURE NA EATHER_RADAR DMC Label = 055 1/1 NA 1= FAILURE
PWSIF PREDICTIVE WINDSHEAR INTERNAL FAILURE NA EATHER_RADAR DMC Label = 055 1/1 NA 1= FAILURE
PWSOFF PREDICTIVE WINDSHEAR OFF NA EATHER_RADAR DMC Label = 055 1/1 1.000 1= OFF
PWSPP PREDICTIVE WINDSHEAR PIN-PROG NA EATHER-RADAR DMC Label = 055/ 1/1 1.000 1= INSTALLED
PWSRW PREDICTIVE WINDSHEAR RED WARNING NA EATHER_RADAR DMC Label = 055 1/1 NA 1= WARNING
PYLLEAK1 ENG.1 PYLON LEAK MEMORIZED NA BMC FWC Label = 100/11 1/2 NA 1= LEAK
PYLLEAK2 ENG.2 PYLON LEAK MEMORIZED NA BMC FWC Label = 100/12 1/2 NA 1= LEAK
QARF QAR FAIL NA FDIU Label = 1/62 NA NA
QARTAPELOW QAR MEDIA LOW NA FDIU Label = 1/62 NA NA
QARTRF QAR TRANSMITTER FAIL NA FDIU Label = 1/62 NA NA
QFEC ALT. BARO QFE SEL.CAPTAIN NA DMC Label = 275/15 1/4 NA 1= IN QFE
QFEF ALT. BARO QFE SEL.F/O NA DMC Label = 275/15 1/4 NA 1= IN QFE
QNHC ALT. BARO QNH SEL.CAPTAIN NA DMC Label = 275/14 1/4 NA 1= IN QNH
QNHF ALT. BARO QNH SEL.F/O NA DMC Label = 275/14 1/4 NA 1= IN QNH
RA2PFDC RA2 SELECTED ON PFD (CAPT) NA DMC Label = 341/23 1/4 NA 1= SELECTED
RA2PFDF RA2 SELECTED ON PFD (F/O) NA DMC Label = 341/23 1/4 NA 1= SELECTED
RADCONT RADAR OPERATING MODE ( CONTOUR ) MATRIX 13 NA DMC Label = 016/27-29 1/4 NA 1= CONTOUR
RADMAP RADAR OPERATING MODE ( MAP ) MATRIX 13 NA DMC Label = 016/27-29 1/4 NA 1= MAP
RADSTBY RADAR OPERATING MODE ( STANDBY ) MATRIX 13 NA DMC Label = 016/27-29 1/4 NA 1= STANDBY
RADTEST RADAR OPERATING MODE ( TEST ) MATRIX 13 NA DMC Label = 016/27-29 1/4 NA 1= TEST
RADTURB RADAR OPERATING MODE ( TURBULENCE ONLY ) MATRIX 13 NA DMC Label = 016/27-29 1/4 NA 1= TURB. ONLY
RADWEAT RADAR OPERATING MODE ( WEATHER ONLY ) MATRIX 13 NA DMC Label = 016/27-29 1/4 NA 1= WEATHER ONLY
1= PREDICTIVE WINDSHEAR
RADWSHR RADAR OPERATING MODE (PREDICTIVE WINDSHEAR ONLY) MATRIX 13 NA DMC Label = 016/27-29 1/4 NA
ONLY
RADWXRTURB RADAR OPERATING MODE ( WXR + TURB. ) MATRIX 13 NA DMC Label = 016/27-29 1/4 NA 1= WXR + TURB.
RALT1 RADIO HEIGHT NO.1 SIGNED AND CORRECTED (-96 TO 4000 FT) (FT) RA DMC Label = 164 1/2 1.000 NA
RALT1+2 RADIO HEIGHT NO.1+2 SIGNED AND CORRECTED (-96 TO 4000 FT) (FT) RA DMC Label = 164 1/1 1.000 NA
RALT2 RADIO HEIGHT NO.2 SIGNED AND CORRECTED (-96 TO 4000 FT) (FT) RA DMC Label = 164 1/2 1.000 NA
RCTQLB RCT FUEL QUANTITY bits 18-28 (LBS) FCMC DMC Label = 317 1/62 64.000 NA
RCTV RCT INSTALLED NA FCMC DMC Label = 313/13 1/62 NA 1= INSTALLED
REFSPD REF SPEED GLOBAL Bits 21-28 (KT) BSCU Label = 332 1/1 1.000 NA
RENGC ENGINE DISPLAYED ON ND CAPT (MATRIX 16) NA DMC Label = 214/26-28 1/4 1.000 NA
RENGF ENGINE DISPLAYED ON ND CAPT (MATRIX 16) NA DMC Label = 214/26-28 1/4 1.000 NA
1= RESIDUAL CABIN
RESIDUALP EXCESS RESIDUAL CABIN PRESSURE NA FWC Label = 124/26 1/1 NA
PRESSURE
REVSEL1 REVERSE MODE SELECTED ENG.1 NA FADEC(ECU) DMC Label = 274/22 1/1 NA 1= SELECTED
REVSEL2 REVERSE MODE SELECTED ENG.2 NA FADEC(ECU) DMC Label = 274/22 1/1 NA 1= SELECTED
RHGNUL RH GEAR NOT UP LOCKED NA LGCIU FWC Label = 021/11 2/1 NA 1= NOT UP LOCKED
RHSQUAT L/G RIGHT SQUAT SWITCH NA LGCIU FWC Label = 020/29 4/1 NA 1= ON GROUND
RHWGLEAK RIGHT WING LEAK MEMORIZED NA BMC FWC Label = 100/20 1/2 NA 1= LEAK
RI3TQKG RIGHT INNER 3 TANK FUEL QUANTITY (KG) FCMC DMC Label = 265 1/62 29.030 NA
RI3TQLB RIGHT INNER 3 TANK FUEL QUANTITY (LBS) FCMC DMC Label = 265 1/62 64.000 NA
RMAINT100 TCAS ALTITUDE RATE TO MAINTAIN 100 FT/MN NA TCAS DMC Label = 270/11 1/1 NA 1= 100 FT/MN
RMAINTSIGN TCAS ALTITUDE RATE TO MAINTAIN SIGN NA TCAS DMC Label = 270/17 1/1 NA 1=- 0=+
RNAVC ROSE NAV DISPLAYED ON ND CAPT (MATRIX 16) NA DMC Label = 214/26-28 1/4 NA NA
RNAVF ROSE NAV DISPLAYED ON ND F/O (MATRIX 16) NA DMC Label = 214 1/4 NA NA
RNPMEN RNP manually enabled NA EFHS Label = 55 1/1 NA NA
ROLL ROLL ATTITUDE bits20-28+29 (DA) ADIRS(IRS) DMC Label = 325 2/1 0.352 >0= RH WING DOWN
ROLLOUT ROLL OUT GREEN NA FMGEC(FG) DMC Label = 176/26 1/1 NA 1= ACTIVE
ROLLW WARNING ROLL DISCREPANCY NA FWC Label = 126/19 2/1 NA 1= WARNING
ROTQKG RIGHT OUTER TANK FUEL QUANTITY (KG) FCMC DMC Label = 306 1/62 29.030 NA
ROTQLB RIGHT OUTER TANK FUEL QUANTITY (LBS) FCMC DMC Label = 306 1/62 64.000 NA
RUDCTLF RUDDER NORN CONTROL FAULT NA FWC Label = 100/28 1/4 NA 1= FAULT
RUDD RUDDER POSITION bits 18-26+29 (DA) FCPC-FCSC FCDC Label = 312 2/1 0.088 >0= TURN LEFT
RUDDBSERVE RUDDER BLUE SERVO ELECTRICAL FAILURE (fly by wire) NA FCPC-FCSC FCDC Label = 041/13 1/1 NA 1= AVAILABLE
RUDDBSERVJ RUDDER BLUE SERVO JAMMED (if not enhanced parm. M17a02=0) NA FCDC Label = 045/24 1/4 NA 1= JAMMED
RUDDBSNA RUDDER BLUE SERVO NOT AVAILABLE (if enhanced parm. M17a02=1) NA FCDC Label = 045/24 1/4 NA 1= NOT AVAILABLE
RUDDBV RUDDER BLUE AVAILABILITY (if M17a02=1) NA FCPC-FCSC FCDC Label = 100/14 2/1 NA 1= AVAILABLE
RUDDGSERVE RUDDER GREEN SERVO ELECTRICAL FAILURE (fly by wire) NA FCPC-FCSC FCDC Label = 041/14 1/1 NA 1= AVAILABLE
RUDDGSERVJ RUDDER GREEN SERVO JAMMED (if not enhanced parm. M17a02=0) NA FCDC Label = 045/25 1/4 NA 1= JAMMED
RUDDGSNA RUDDER GREEN SERVO NOT AVAILABLE (if enhanced parm. M17a02=1) NA FCDC Label = 045/26 1/4 NA 1= NOT AVAILABLE )
RUDDGV RUDDER GREEN AVAILABILITY (if M17a02=1) NA FCPC-FCSC FCDC Label = 100/15 2/1 NA 1= AVAILABLE
RUDDYSERVJ RUDDER YELLOW SERVO JAMMED (if not enhanced parm. M17a02=0) NA FCDC Label = 045/26 1/4 NA 1= JAMMED
RUDDYSNA RUDDER YELLOW SERVO NOT AVAILABLE (if enhanced parm. M17a02=1) NA FCDC Label = 045/25 1/4 NA 1= NOT AVAILABLE
RUDDYV RUDDER YELLOW AVAILABILITY (if M17a02=1) NA FCPC-FCSC FCDC Label = 100/16 2/1 NA 1= AVAILABLE
RUDP DDER PEDAL POSITION bits 18-26+29 (M14a01:non fly by wire/M14b01:fly by (DA) FCPC-FCSC FCDC Label = 304 2/1 0.088 >0= LEFTL=
RUDPF RUDDER PEDAL INPUT FORCES bits 20-28+29 (DA) FCDC Label = 030 1/1 4.000
RUDT YAW TRIM POSITION (INDICATOR) bits 18-28+29 (DA) FCSC FCDC Label = 313 1/1 0.088 >0= TURN LEFT
0= AVAILABLE 1= NOT
RUDT1V RUDDER TRIM ACTUATOR 1 AVAILABILITY NA FCSC FCDC Label = 044/24 1/1 NA
AVAILABLE
0= AVAILABLE 1= NOT
RUDT2V RUDDER TRIM ACTUATOR 2 AVAILABILITY NA FCSC FCDC Label = 044/25 1/1 NA
AVAILABLE
RUDTW RUDDER TRIM NA FWC Label = 124/19 1/1 NA 1= WARNING
RUDYSEF Rudder Yellow servo electrical failure NA FCDC Label = 41/ 1/1 NA 1=
RVORC ROSE VOR/ILS DISPLAYED ON ND CAPT (MATRIX 16) NA DMC Label = 214/26-28 1/4 NA NA
RVORF ROSE VOR/ILS DISPLAYED ON ND F/O (MATRIX 16) NA DMC Label = 214 1/4 NA NA
RWSPARE10 RED WARNING : SPARE 10 NA FWC Label = 124/ 1/1 NA 1=
RWSPARE7 RED WARNING : SPARE 7 NA FWC Label = 101/17 1/1 NA 1= WARNING
RWYLOCD FMA LATERAL MODE RWY DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
RWYTRKD FMA LATERAL MODE RWY TRACK DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
SALTFCU SELECTED ALTITUDE bits 19-28 (FT) FCU/FG Label = 102 1/1 64.000 NA
SAT STATIC AIR TEMPERATURE bits18-26+29 (DC) DIRS(ADC) DMC or FWC Label = 21 1/1 0.250 NA
SAV1F ENG.1 STARTER AIR/V FAIL OPEN NA BMC FWC Label = 276/28 1/2 NA 1= FAILED
SAV2F ENG.2 STARTER AIR/V FAIL OPEN NA BMC FWC Label = 276/28 1/2 NA 1= FAILED
SBAROC SELECTED BARO SETTING CAPTAIN Bits 15-26 (MB) ADIRS DMC Label = 234 1/4 NA NA
SBAROF SELECTED BARO SETTING FIRST-OFFICER Bits 15-26 (MB) ADIRS DMC Label = 234 1/4 NA NA
SBC SPEED BRAKE COMMANDED NA FCPC FCDC Label = 043/29 2/1 NA 1= COMMANDED
SBNR SPEED BRAKES NOT RETRACTED NA FWC Label = 124/18 1/1 NA 1= NOT RETRACTED
SCASAPPS APPROACH SPEED TARGET (MATRIX 11) NA FCU/FG DMC Label = 274/21-22 1/1 NA NA
SCASFCUS SELECTED SPEED ORIGINE.FROM FCU. (MATRIX 11) NA FCU/FG DMC Label = 274/21-22 1/1 NA NA
SCASFGS SELECTED SPEED ORIGINE.FROM FG. (MATRIX 11) NA FCU/FG DMC Label = 274/21-22 1/1 NA NA
SCASPFD SELECTED SPEED DISPLAYED bits 20-28 (KT) FCU/FG DMC Label = 103 1/1 1.000 NA
SCRSV1 SELECTED COURSE VOR.1 bits 20-28+29 (DA) VOR DMC Label = 100 1/1 0.352 NA
SCRSV2 SELECTED COURSE VOR.2 bits 20-28+29 (DA) VOR DMC Label = 100 1/1 0.352 NA
SDAC11F SDAC.1-1 FAIL NA DMC Label = 362/26 1/4 NA 1= FAULT
SDAC1V SDAC1 VALID NA FWC Label = 126/11 1/4 NA 1= VALID
SDAC2V SDAC2 VALID NA FWC Label = 126/12 1/4 NA 1= VALID
SDIMEWDD SD IMAGE ON EWD/DU NA DMC Label = 313/25 1/4 NA 1= ON EWD-DU
SDIMND1D SD IMAGE ON CAPT/ND DU NA DMC Label = 313/27 1/4 NA 1= ON CAPT-DU
SDIMND2D SD IMAGE ON F/O/ND NA DMC Label = 313/28 1/4 NA 1= ON F/O DU
SDIMSDD SD IMAGE ON SD/DU NA DMC Label = 313/26 1/4 NA 1= ON SD-DU
SDINV SD FEEDBACK BUS INVALID (DU4) NA DMC Label = 314/14 1/4 NA 1= INVALID
SDMSG CHECK SD MSG ACTIVATED NA DMC Label = 334/18 1/4 NA 1= ACTIVE
SDOFF SD/DU OFF NA DMC Label = 314/20 1/4 NA 1= OFF
SDUCHN1 SATCOM SDU CHANNEL.1 NA SDU FWC Label = 372/26 1/1 NA 1= COMM.THROUGH CHAN.1
SDUCHN2 SATCOM SDU CHANNEL.2 NA SDU FWC Label = 372/27 1/1 NA 1= COMM.THROUGH CHAN.2
SFCTR_116_1 NA NA NA 1/4 NA NA
SFLP SLAT-FLAP LEVER POSITION (MATRIX 21) (NOTCH) SFCC FWC Label = 137/11-15 1/1 NA NA
SFPA SELECTED FLIGHT PATH ANGLE bits 18-24+29 (DA) FCU Label = 115 1/1 0.088 >0=UP
SHDG SELECTED HEADING bits 21-28+29 (DA) FCU DMC Label = 101 1/1 0.703 NA
SIC SIC CLOSED NA ECMU SDAC Label = 055/14 1/4 NA 1= CLOSED
SLAT SLAT SURFACE ANGLE bits21-27 (DA) SFCC/FWC DMC Label = 124 1/1 0.250 NA
SLDGANT1 SELECT LANDING ANTENNA.1 NA MMR DMC Label = 271/20 1/2 NA 1= ACTIVE
SLDGANT2 SELECT LANDING ANTENNA.2 NA MMR DMC Label = 271/20 1/2 NA 1= ACTIVE
SLT1F SLAT 1 FAULT NA SDAC Label = 006/28 1/4 NA 1= FAULT
SLT2F SLAT 2 FAULT NA SDAC Label = 006/28 1/4 NA 1= FAULT
SLTLOCK SLAT LOCKED NA SFCC/FWC DMC Label = 46/12 1/1 NA 1= LOCKED
SMACH SELECTED MACH Bits 20-26 NA FCU Label = 106 1/1 0.008 NA
SMALT METRIC ALTITUDE SELECTED NA FCU DMC Label = 154/27 1/1 NA 1= SELECTED
SMOAREA1 SMOKE AUX AREA 1 (additional information to M30a77) NA FWC Label = 101/23 1/1 NA 1= SMOKE
SNTO SLATS NOT IN T/O CONFIGURATION NA FWC Label = 124/15 1/1 NA .1= NOT IN T/O CONF
SOFTNB1 SOFTWARE PART NUMBER (1ST NUMBER) NA FDIU 1/62 NA NA
SOFTNB2 SOFTWARE PART NUMBER (2ND NUMBER) NA FDIU 1/62 NA NA
SOFTNB3 SOFTWARE PART NUMBER (3RD NUMBER) NA FDIU 1/62 NA NA
SOFTNB4 SOFTWARE PART NUMBER (4TH NUMBER) NA FDIU 1/62 NA NA
SP1V SPOILER 1 AVAILABILITY NA FCPC FCDC Label = 043/14 2/1 NA 1= AVAILABLE
SP2V SPOILER 2 AVAILABILITY NA FCPC-FCSC FCDC Label = 043/15 1/1 NA 1= AVAILABLE
SPDAUTO AUTO SPEED CONTROL ACTIVE NA FCU/FG DMC Label = 145/23 1/1 NA 1= ACTIVE
SPDBRK SPEED BRAKE SELECTION BITS18-27+29 (DA) FCPC FCDC Label = 134 2/1 0.088 NA
SPDMANU MANUAL SPEED CONTROL ACTIVE NA FCU/FG DMC Label = 145/24 1/1 NA 1= ACTIVE
SPDTHR A/P-A/THR SUB MODE SPEED/THRUST NA FMGEC(FG) DMC Label = 145/21 1/1 NA NA
SPEEDD FMA A/THR SPEED DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
SPLH2 SPOILER LH.2 POSITION bits18-27 (DA) FCPC-FCSC FCDC Label = 362 1/1 0.088 <0= EXTENDED
SPLH3 SPOILER LH.3 POSITION (DA) FCPC-FCSC FCDC Label = 363 1/1 0.088 <0= EXTENDED
SPRH2 SPOILER RH.2 POSITION (DA) FCPC-FCSC FCDC Label = 372 1/1 0.088 <0= EXTENDED
SRALT1 RADIO HEIGHT NO.1 (SIGNED RANGE/2) ******** bits 16-26 (FT) RA DMC Label = 164 1/2 1.000 NA
SRALT1+2 RADIO HEIGHT NO.1+2 (SIGNE RANGE/2) ******** (FT) NA 1/1 NA NA
SRALT2 RADIO HEIGHT NO.2 (SIGNED RANGE/2) ******** bits 16-26 (FT) RA DMC Label = 164 1/2 1.000 NA
SRSD FMA LONGI. MODE SRS DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
SSLIP ESTIMATED SIDE SLIP bits23-28+29 (DA) FCDC Label = 227 1/1 0.500 >0= RH SIDESLIP
SSLIPFLAG SIDE SLIP FLAG DISPLAYED NA ADIRS(IRS) DMC Label = 350/22 1/1 NA 1= ACTIVE
SSLIPIRS SIDE SLIP FROM IRS NA ADIRS(IRS) DMC Label = 350/19 1/1 NA 1= ACTIVE
SSLIPYEL SIDE SLIP IN YELLOW DISPLAYED NA ADIRS(IRS) DMC Label = 350/21 1/1 NA 1= ACTIVE
STAB STABILIZER POSITION bits 17-25+29 (DA) FCPC FCDC Label = 315 1/1 0.044 >0= NOSE DOWN
STABCTL THS ELECTRICAL CONTROL AVAILABILITY NA FCPC-FCSC FCDC Label = 041/29 1/1 NA 1= NOT AVAILABLE
STABNTO PITCH TRIM NOT IN T/O CONFIG NA FWC Label = 124/17 1/1 NA 1= NOT IN T/O CONFIG
STALLW STALL WARNING VOICE NA FWC Label = 126/17 1/1 NA 1= STALL ON
STATUS STATUS PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
STDC ALT. STD/BARO SEL.CAPTAIN NA DMC Label = 275/13 1/4 NA 1= IN STD
STDF ALT. STD/BARO SEL.F/O NA DMC Label = 275/13 1/4 NA 1= IN STD
STKCF LEFT SIDE STICK FAULT NA FWC Label = 124/20 1/1 NA 1= FAULT
STKCINOP CAPTAIN SIDE STICK INOPERATIVE NA FCPC-FCSC FCDC Label = 042/14 1/1 NA 1= INOPERATIVE
STKFF RIGHT SIDE STICK FAULT NA FWC Label = 124/21 1/1 NA 1= FAULT
STKFINOP FIRST-OFFICER SIDE STICK INOPERATIVE NA FCPC-FCSC FCDC Label = 042/15 1/1 NA 1= INOPERATIVE
STKPC CAPTAIN PITCH COMMAND POSITION bits17-25+29 (DA) FCPC-FCSC FCDC Label = 305 4/1 0.044 >0= NOSE DOWN
STKPF FIRST-OFFICER PITCH COMMAND POSITION bits17-25+29 (DA) FCPC-FCSC FCDC Label = 306 4/1 0.044 >0= NOSE DOWN
STKRC CAPTAIN ROLL COMMAND POSITION bits17-25+29 (DA) FCPC-FCSC FCDC Label = 301 4/1 0.044 >0= LEFT
STKRF FIRST-OFFICER ROLL COMMAND POSITION bits17-25+29 (DA) FCPC-FCSC FCDC Label = 302 4/1 0.044 >0= LEFT
SVS SELECTED VERTICAL SPEED bits 21-27+29 (FT/MN) FCU Label = 104 1/1 64.000 >0= UP
SWPOSACK1 SWITCH POS. ACK SELECTION CONFIRMED 1 NA MMR DMC Label = 271/21 1/2 NA 1= CONFIRMED
SWPOSACK2 SWITCH POS. ACK SELECTION CONFIRMRD 2 NA MMR DMC Label = 271/21 1/2 NA 1= CONFIRMRD
e Raw Param w116_ NA NA NA 1/4 NA NA
T31 T3 ENG.1 HPC EXIT TEMPERATURE bits 18-28+29 (DC) EIVMU Label = 265 1/1 0.500 NA
T32 T3 ENG.2 HPC EXIT TEMPERATURE bits 18-28+29 (DC) EIVMU Label = 265 1/1 0.500 NA
TACAC TAC activated NA FCDC Label = 102 2/1 NA NA
TACAV TAC available NA FCDC Label = 102 2/1 NA NA
TACSINST TACS INSTALLED NA DMC Label = 333/14 1/4 NA 1= INSTALLED
TAONLY TCAS TA ONLY (DEGRADED) NA TCAS DMC Label = 016/12 1/1 NA 1= TA ONLY
TARGEXC VZ/FPA TARGET EXCESSIVE NA FMGEC(FG) DMC Label = 274/29 1/1 NA 1= TARGET EXCESSIVE
TCASF TCAS FAIL NA DMC Label = 363/13 1/4 NA 1= FAULT
TCASVAL TCAS Valid NA EFHS Label = 16/ 1/1 NA 1=
TCRAIMDIS TCAS RA inhibited message displayed NA EFHS Label = 52 1/1 NA NA
TEMPIV3 Temperature iso valve V3 NA FWC Label = 25 1/1 NA NA
TGTSSLIP TARGET SIDE SLIP bits23-26+29 (DA) FCDC Label = 077 1/1 0.500 >0= RH SIDESLIP
TGTSSLIPCYAN TARGET SIDE SLIP IN CYAN DISPLAYED NA ADIRS(IRS) DMC Label = 350/29 1/1 NA 1= ACTIVE
THRCLBD FMA A/THR THR CLB DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
THRDCLB1D FMA A/THR THR DCLB1 DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
THRDCLB2D FMA A/THR THR DCLB2 DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
THRDESD FMA A/THR THR DES DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
THRIDLED FMA A/THR THR IDLE DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
THRLKD THR LK NA FMGEC(FG) DMC Label = 274/23 1/1 NA 1= DISPLAYED SUBMODE
THRLV1 Eng 1 THR LVR above idle NA FWC Label = 101/ 1/1 NA 1=
THRLV2 Eng 2 THR LVR above idle NA FWC Label = 101/ 1/1 NA 1=
THRLVANY Any Eng. THR LVR above idle NA FWC Label = 124/29 1/1 NA 1=
THRLVRD FMA A/THR THROTTLE LEVER DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
THRMCTD FMA A/THR THR MCT DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
TLU1V TLU1 AVAILABILITY (non Enhanced) NA FCDC Label = 041/11 1/1 NA 1= NOT AVAILABILITY
TLU2V TLU2 AVAILABILITY (non Enhanced) NA FCDC Label = 041/12 1/1 NA 1= NOT AVAILABILITY
TLUP TLU POSITION bits 21-26+29 (non Enhanced) (DA) FCSC FCDC Label = 167 1/1 0.703 NA
TO CITY PAIR TO C1-4 NA FMGEC CMC NA NA NA
TOC1 CITY TO Character 1 NA FMGEC(FM) CMC Label = 041 1/62 NA NA
TOGALKD FMA A/THR TOGA LK DISPLAYED NA FMGEC(FG) DMC Label = 150 1/1 NA NA
TOGOC BEARING TO GO FROM FMGEC 1 bits 20-28+29 (DA) FMGEC1 DMC Label = 117 1/1 0.352 NA
TOGOF BEARING TO GO FROM FMGEC 2 bits 20-28+29 (DA) FMGEC2 DMC Label = 117 1/1 0.352 NA
TOTHRW WARNING "TO THRUST DISAGREE" NA FWC Label = 124/24 1/1 NA 1= WARNING
TO_cpt1 CITY TO Character 1 NA FMGEC CMC Label = 041 1/62 NA NA
TRA1 THRUST RESOLVER ANGLE ENG.1 bits17-27+29 (DA) ADEC(ECU or EEC) DMC Label = 13 1/1 0.044 0<= REVERSER
TRA2 THRUST RESOLVER ANGLE ENG.2 bits17-27+29 (DA) ADEC(ECU or EEC) DMC Label = 13 1/1 0.044 0<= REVERSER
TRKD FMA LATERAL MODE TRACK DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
TRKGAD FMA LATERAL MODE GA TRACK DISPLAYED NA FMGEC DMC Label = 152 1/1 NA NA
TTQKG TRIM TANK FUEL QUANTITY bits 18-25 (KG) FCMC DMC Label = 311 1/62 29.030 NA
TTQLB TRIM TANK FUEL QUANTITY bits 18-25 (LBS) FCMC DMC Label = 311 1/62 64.000 NA
UNSTW1 THR REVERSER UNSTOWED ENG.1 NA FADEC(ECU) DMC Label = 274/12 1/1 NA 1= UNSTOWED
UNSTW2 THR REVERSER UNSTOWED ENG.2 NA FADEC(ECU) DMC Label = 274/12 1/1 NA 1= UNSTOWED
UPADVCOR TCAS COMBINATED CONTROL.UP ADVISORY CORRECTIVE. (MATRIX 7) NA TCAS DMC Label = 270/18-20 1/1 NA NA
UTC GMT ED55F2 NA NA NA NA NA
UTCH HEURE BCD UTC bits 24-28 NA CLOCK Label = 125 1/62 NA NA
UTCM MINUTE UTC bits 18-23 NA CLOCK Label = 150 1/4 NA NA
UTCS SECONDE UTC bits 12-17 NA CLOCK Label = 150 1/4 NA NA
VCC1SMO SMOKE VCC 1 NA FWC Label = 101/14 1/1 NA 1= WARNING
VCC2SMO SMOKE VCC 2 NA FWC Label = 101/15 1/1 NA 1= WARNING
VERTSPAC Vertical speed protection active NA FCDC Label = 102 4/1 NA NA
VERTSPAV Vertical speed protection available NA FCDC Label = 102 2/1 NA NA
VERTSPO Vertical speed protection order NA FCDC Label = 32 2/1 0.063 NA
VFEW VFE OVERSPEED (240-215-196-186-180) NA FWC Label = 126/19 1/1 NA 1= WARNING
VHF1 V.H.F.1 MANUAL RADIO TRANSMITTER NA VHF1 SDAC Label = 005/15 1/1 NA 1= TRANSMITTING
VIDCLEARC CAPT VIDEO CLEAR NA HUD FWC Label = 065/18 1/4 NA 1= CLEARED
VIDCLEARF F/O VIDEO CLEAR NA HUD FWC Label = 065/18 1/4 NA 1= CLEARED
VIDEO VIDEO PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
VIDEOOFFC CAPT VIDEO OFF NA HUD FWC Label = 065/17 1/4 NA 1= OFF
VIDEOOFFF F/O VIDEO OFF NA HUD FWC Label = 065/17 1/4 NA 1= OFF
VIDFORPFD1 VIDEO DISCRETE FOR PFD1 NA TACS Label = 333/11 1/4 NA 1= ACTIVE
VIDFORPFD2 VIDEO DISCRETE FOR PFD2 NA TACS Label = 333/12 1/4 NA 1= ACTIVE
VIDFORSD TACS SELECTION ON SD NA TACS Label = 333/13 1/4 NA 1= TACS SELECTED
1= MESSAGE DISPLAYED ON
VIDNOTAVAIL "VIDEO NOT AVAIL" MESSAGE DISPLAYED ON SD NA DMC Label = 333/25 1/4 NA
SD
VIDONPFD1 VIDEO ON PFD1 NA TACS Label = 333/28 1/4 NA 1= ACTIVE
VIDONPFD2 VIDEO ON PFD2 NA TACS Label = 333/27 1/4 NA 1= ACTIVE
VIDONSD VIDEO AUTHORIZED ON SD NA TACS Label = 333/26 1/4 NA 1= AUTHORIZED ON SD
VIDSPARE1ONSD VIDEO SPARE N³1 SELECTION ON SD NA DMC Label = 333/17 1/4 NA 1= SELECTED
VLEW VLE OVERSPEED NA FWC Label = 126/18 1/1 NA 1= WARNING
VMOW VMO/MMO OVERSPEED NA FWC Label = 126/26 1/1 NA 1= OVERSPEED
VOR1BG VOR.1 BEARING bits 20-28+29 (DA) VOR1 DMC Label = 222 1/1 0.352 NA
VOR2BG VOR.2 BEARING bits 20-28+29 (DA) VOR2 DMC Label = 222 1/1 0.352 NA
VORF1 VOR1 FREQUENCY bits 15+19-27 (MHZ) VOR1 DMC Label = 034 NA 0.050 NA
VORF2 VOR2 FREQUENCY ELAB. bits 15+19-27 (MHZ) VOR DMC Label = 034 NA 0.050 NA
VPATHNONE A/P-A/THR SUB MODE NONE NA FMGEC(FG) DMC Label = 145/12 1/1 NA NA
VPATHSPD A/P-A/THR SUB MODE VERT.PATH/SPEED NA FMGEC(FG) DMC Label = 145/12 1/1 NA NA
VPATHTHR A/P-A/THR SUB MODE VERT.PATH/THRUST NA FMGEC(FG) DMC Label = 145/13 1/1 NA NA
VRTG NORMAL ACCELERATION bits18-28+29 (G) LA SDAC Label = 333 8/1 0.004 >0= UP
VRTGCHK NORM ACCEL. CHECK NOT RUN NA FDIU 1/62 NA NA
VRTGCHKF NORM ACCEL. CHECK FAIL NA FDIU 1/62 NA NA
VSD FMA LONGI. MODE V/S DISPLAYED NA FMGEC DMC Label = 153 1/1 NA NA
VSPD VERTICAL SPEED bits 18-27+29 NA IR or ADR DMC Label = 365 1/1 16.000 NA
VSS VERTICAL SPEED SELECTED FROM ADR NA IR/ADR DMC Label = 341 1/1 NA 1= ADR 0=IR
VSSPD A/P-A/THR SUB MODE V/S/SPEED NA FMGEC(FG) DMC Label = 145/14 1/1 NA NA
WAION WING ANTI-ICE SYSTEM ON NA 5DL SDAC Label = 001/24 1/2 NA 1= SYSTEM ON
WAISEL WING ANTI-ICE SYSTEM SELECT ON NA 3DLA SDAC Label = 001/23 1/2 NA 1= SELECT ON
WAIVLI WING A-I LH INNER VALVE CLOSED NA SDAC Label = 001/26 1/2 NA 1= CLOSED
WAIVLO WING A-I LH OUTER VALVE CLOSED NA SDAC Label = 001/28 1/2 NA 1= CLOSED
WAIVRI WING A-I RH INNER VALVE CLOSED NA SDAC Label = 001/27 1/2 NA 1= CLOSED
WAIVRO WING A-I RH OUTER VALVE CLOSED NA SDAC Label = 001/29 1/2 NA 1= CLOSED
WD WIND DIRECTION TRUE bits 21-28+29 (DA) ADIRS(IRS) DMC Label = 316 1/1 0.703 NA
WHC1F FAULT DETECTED ON WHC1 *** VALID IF M72a16=1 *** NA WHC1 SDAC Label = 013/15 1/2 NA 1= FAULT
WHC2F FAULT DETECTED ON WHC2 *** VALID IF M72a16=1 *** NA WHC2 SDAC Label = 005/16 1/2 NA 1= FAULT
WHEEL WHEEL PAGE SELECTED (MATRIX 17) NA DMC Label = 251/24-28 1/4 NA 1= SELECTED
WHLSPD1 WHEEL SPEED.1 Bits 21-28 (KT) BSCU Label = 320 1/4 1.000 NA
WS WIND SPEED bits 21-28 (KT) ADIRS(IRS) DMC Label = 315 1/1 1.000 NA
WSHRW WARNING WINDSHEAR NA FWC Label = 126/18 1/1 NA 1= WARNING
WXRNDCF WXR DU ND CAPTAIN FAIL NA DMC Label = 363/26 1/4 NA 1= FAULT
WXRNDFF WXR DU ND FIRST-OFFICER FAIL NA DMC Label = 363/27 1/4 NA 1= FAULT
WXRPFDCF WXR DU PFD CAPTAIN FAIL NA DMC Label = 363/25 1/4 NA 1= FAULT
WXRPFDFF WXR DU PFD FIRST-OFFICER FAIL NA DMC Label = 363/28 1/4 NA 1= FAULT
XBV X BLEED VALVE NOT FULLY CLOSED NA BMC SDAC Label = 040/16 1/2 NA 1= NOT FULLY CLOSED
YAWFD YAW FD bits 18-26+29 (DA) FMGEC(FG) DMC Label = 143 1/1 0.088 NA
YDGV YAW DAMPER GREEN AVAILABLE (non fly by wire) NA FCPC-FCSC FCDC Label = 041/13 1/1 NA 1= AVAILABLE
YDO YAW DAMPER ORDER bits 18-26+29 (non fly by wire) (DA) FCPC-FCSC FCDC Label = 021 2/1 0.088 >0= LEFT=
YDYV YAW DAMPER YELLOW AVAILABLE (non fly by wire) NA FCPC-FCSC FCDC Label = 041/14 1/1 NA 1= AVAILABLE
Annex N° 4
FDR data plots – Overall
GSI 420.1022/15 (TL) 13-Feb-15 20/21

AP1E
AP2E 1.00
ATHRE 0.00
ATHRA 1.00
VMOW
1.00
CPTMW1 0.00
CPTMW2 0.00
FOMW1 0.00
FOMW2 0.00
0.00
STKP
10
STKPC
STKPF
DA ELV SIDE STICK PITCH POSITION FIRST-OFFICER (STKPF - -)

0 10
ELVL -0.09
0.00 DA
DA
CAPTAIN (STKPC__ )
ELVR
STAB ELEVATORS RIGHT (ELVR - -)

0 STAB
DA
LEFT (ELVL __ )
-1.05 DA
-1.41 DA
DA
-1.85
VRTG VSPD
1.5 -1000
G VRTG FT/MI
1.0 1.05 G -2000
MNADC -2208.00 FT/MI

0.75
LONG
0.70 0.5
MNADC
SALT
G LONG FCU
0.65 0.0 10:34:31-666.667 36
0.04 G
ALT
CAOA ALT 0.62

2
VSPD
10 22392.00 FT 20
SALTFCU
PTCH
14976.00 FT
10^3
FT
5 4
CAOA CAOA2 - - CAOA1 ___
GS
1
420
2.11 DA
DA CTASSAT 1.41 DA
417.00 KT
0
PTCH CTASSAT SCAS
PFD
410 290
-2.81 DA
CAS_ADC
SCASPF
N1A2
120 400 280
N1A1
275.00 KT
KT
80 390 270
389.25
N1A
CAS_ADC
TRA KT
40 100 46.91 %
47.03 % 260
TRA2 260.00
TRA1
0 50 TRA GS
46.85 DA
47.11 DA
% DA
-40 0
10:28:00 10:29:00 10:30:00 10:31:00 10:32:00 10:33:00 10:34:00 10:35:00 10:36:00 10:37:00 10:38:00
TEMPS(H)
MR1 : P0733V0041DFDR
A/C : A330- MSN 0733 FLIGHT No 0041
CG (%) 31.36
GWL (LBS) 347320
GWK (KG) 157542
CRUISE(LONGITUDINAL AXIS) Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/bertille/2014/P0733V0041-Hailstorm/T1-cruise-longi.ilv 1.1.1
Electronically validated - Released on 20 Oct 2014
AP1E STKR
AP2E
1.00 10
STKRF
0.00
STKRC
AIL
O SIDE STICK ROLL POSITION FIRST-OFFICER (STKRF - - ) DA
10 0
AILRO -0.09 DA
-0.04 CAPTAIN (STKRC ___ )
AILLO
AIL
DA I OUTER AILERONS RIGHT (AILRO - -)
0 10 1.49 DA
AILRI LEFT (AILLO__ )
-1.85 DA
AILLI
DA INNER AILERONS RIGHT (AILRI - -) SSLIP

0 1.67 DA 5
LEFT (AILLI__ )
-2.02 DA
DA DA
SSLIP
5 0
0.00 DA
DA
0
ROLL
13.36 DA 10
RUDP RUDD ROLL

10 10 0
RUDT DA
-10
DRIFT ANGLE
DA RUDP RUDD RUDT
0 0
0.79 DA
0.00 DA
LATG -10.72 DA
0.1
LATG
SAT
G
0.02 G
0.0 -20
SAT
-20.75
SAT
10:33:25-833.333 -30
CTAS
SAT
500 -40
GS
HDG
400 360
400.55 KT CTASSAT
WD
GS
362.00 KT
305.86 DA
KT
300 WD 270
258.05 DA HDG
80.00 KT
WS DA
180
WS
60
KT
40
SLAT FLAP SFLP

20 20 5
SFLP
0
0.00
DA DA SLAT FLAP
0 0
0.00 DA
10:28:00 10:29:00 10:30:00 10:31:00 10:32:00 10:33:00 10:34:00 10:35:00 10:36:00 10:37:00 10:38:00
TEMPS(H)
CG (%) 31.36
GWL (LBS) 347320 CRUISE (LATERAL AXIS)
GWK (KG) 157542 Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/source/dfdr/dfdr/LR/cruise_lat.ilv 1.1.2
FMA :ZONE E1,E2 ET E3
AP1E AP1 (WHITE)
AP2E
AP2 (WHITE)
0.00
FD1E
FD2E
0.00 FD1 (WHITE)
1.00 FD2 (WHITE)
ATHRE 1.00
ATHRA ATHR (WHITE)
0.00 ATHR (CYAN)
APOFFW
APOFFV
0.00
1.00
SRSD FMA LONGI. MODE: ZONE B1 0.00 SRS (GREEN)
ALTCSTD 0.00 ALT CST (GREEN)
ALTCRZD ALT CRZ (GREEN)
0.00
ALTMODD 0.00 ALT (GREEN)
ALTACQCS 0.00 ALT CST* (GREEN)
ALTACQCR ALT CRZ* (GREEN)
0.00
ALTACQD 0.00 ALT* (GREEN)
VSD V/S (GREEN)
0.00
CLBD 1.00 CLB (GREEN)
DESD 0.00 DES (GREEN)
OPCLBD OP CLB (GREEN)
0.00
OPDESD 0.00 OP DES (GREEN)
GSTRKD G/S (GREEN)
0.00
GSCPTD 0.00 G/S* (GREEN)
FPAD 0.00 FPA (GREEN)
FMA LONGI. MODE ARM.: ZONE B2 0.00 ALT (CYAN ALTACQARM)

ALTARM
FDESARM 1.00 FINAL (CYAN)
FG LONGI. SUBMODES 0.00

SPDTHR SPEED/THRUST
VSSPD VS SPEED
0.00
FPASPD 0.00 FPA SPEED
VPATHSPD VPATH SPEED
0.00
VPATHTHR 0.00 VPATH THRUST
FMA MODE: ZONE BC1 0.00

ROLLOUT ROLL OUT (GREEN)
FLARE 0.00 FLARE (GREEN)
LANDTRK LAND (GREEN)
0.00
LANDARM 0.00 LAND ARM
ALIGN 0.00 ALIGN
FMA LAT. MODE: ZONE C1 0.00

TRKGAD GA TRK (GREEN)
LOCBCCPT LOC B/C* (GREEN)
0.00
LOCCPTD 0.00 LOC* (GREEN)
HDGD 0.00 HDG (GREEN)
RWYLOCD 1.00 RWY LOC (GREEN)
RWYTRKD 0.00 RWY TRK (GREEN)
TRKD TRACK (GREEN)
0.00
LOCBCTRK 0.00 LOC B/C (GREEN)
LOCTRKD 0.00 LOC (GREEN)
APPNAVD APP NAV (GREEN)
0.00
NAVD 0.00 NAV (GREEN)
FG LAT. SUBMODES 0.00

NAVTRK NAV TRACK
NAVHDG 0.00 NAV HDG
NAVHPATH NAV HPATH
0.00
SPEED/MACH TARGET SELECTION 0.00
SCASFCUS SPDTGT FROM FCU SEL
SCASFGS 0.00 SPDTGT FROM FG PFD
SCASAPPS
1.00
SPDTGT FROM FG/FM VAP
SPDAUTO 0.00 AUTO SPEED CONTROL
SPDMANU 0.00 MANUAL SPEED CONTROL
MACHFCUS 1.00 MACH SEL
0.00
FMA MODE: ZONE A1+A2
MANTOGAD 10:34:57-500 MAN TOGA (WHITE)
THRMCTD THR MCT (GREEN)
0.00
MANFLXD 0.00 MAN FLX (WHITE)
MANDTOD MAN DTO (WHITE)
0.00
THRDCLB1 0.00 THR DCLB1 (GREEN)
THRCLBD THR CLB (GREEN)
0.00
MANMCTD 0.00 MAN MCT (WHITE)
MANTHRD MAN THR (WHITE)
0.00
THRLVRD 0.00 THR LVR (GREEN)
THRIDLED 0.00 THR IDLE (GREEN)
THRDESD THR DES (GREEN)
0.00
AFLOORD 0.00 A FLOOR (GREEN)
TOGALKD TOGA LK (GREEN)
0.00
SPEEDD 0.00 SPEED (GREEN)
MACHD 0.00 MACH (GREEN)
FMA MODE: ZONE A3 0.00

THRLKD THR LK (AMBER)
ATHRRTD 1.00 RETARD
0.00
FCU: BARO. REF. SELECTION
STDC
STDF 1.00
QNHF
QNHC 1.00
QFEC 0.00
QFEF 0.00
FE1V 0.00
FE2V
FG1F
0.00
1.00
FG2F 1.00
FM1F 0.00
FM2F 0.00
0.00
FMAD 0.00 FMA DISPLAYED
EVTMKR 1.00 EVENT MARKER
0.00
10:28:00 10:29:00 10:30:00 10:31:00 10:32:00 10:33:00 10:34:00 10:35:00 10:36:00 10:37:00 10:38:00
TEMPS(H)
FMA DISPLAYS-AP MODES Edited : 8/10/2014 Figure

/workgroup/operation/dfdr/visage/source/dfdr/dfdr/LR/AP_modes.ilv 1.1.3
AP1E
AP2E
FCTL
HYDGW
HYDYW
HYDBW
LAW
NLAW
ALAW
DLAW
FCPC1CL
FCPC2CL
FCPC3CL
FCSC1CL
FCSC2CL
NCCL
FAULT (COMPUTERS AND ELEVATORS)

FCPC1F
FCPC2F
FCPC3F
FCSC1F
FCSC2F
SLT1F
SLT2F
FLP1F
FLP2F
STKP
LRELVF
10
STKPC
STKPF STICKS (POSITION AND VALIDITY)
DA CAPTAIN (STKPC __) FIRST-OFFICER (STKPF - - )

0
STKR
10
STKRC
PH
7.0 STKRF
DA CAPTAIN (STKRC __ ) FIRST-OFFICER (STKRF - - )

0
6.5
FLIGHT PHASE
6.0
STKCF
STKFF
STKFINOP
STKCINOP
AILLIBV
CAS_ADC
AILLIGV
CAS_ADC ALT
300 36000
CAS_ADC ALT
AILLOGV
AILERON VALIDITY
AILLOYV 1=AVAILABLE
AILRIBV
AILRIGV
200 28000
ALT
AILROGV
AILROYV
100 20000
ELVRGV
ELVRYV
ELVLBV ELEVATOR VALIDITY

ELVLGV 1=AVAILABLE
YAW DAMPER
YDGV
YDYV
SBNR
RUDTW
MASTER WARNING
CPTMW1
CPTMW2
FOMW1
FOMW2
10:28:00 10:29:00 10:30:00 10:31:00 10:32:00 10:33:00 10:34:00 10:35:00 10:36:00 10:37:00 10:38:00
TEMPS(H)
OVERViEW
WGT(KG) 157542
CDVE-LAW-FAULT-STICKS-YAW DAMPER
WGT(LBS) 347320 Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/source/dfdr/dfdr/LR/CDVE.ilv 1.1.4
CAPT / FO MAST WNG & CAUTION
CPTMW1
FOMW2
CPTMC1
FOMC2
ICE DETECTOR
DD1F
DD2F
DD1ICEDET
DD2ICEDET
D1SICEDET1
D2SICEDET1
NAI P/B ON ENG1

NAI1ON
NAI ENG1 SEL
NAI1S
NAI1F NAI VALVE FAULT ENG1

NAI P/B ON ENG2
NAI2ON
NAI ENG2 SEL
NAI2S
WAISEL WAI SYS SELECT ON
WAION WAI SYS ON

WAI LH IN VLV OPEN
WAIVLI
WAI RH IN VLV OPEN
WAIVRI
WAI RH OUT VLV OPEN
WAIVRO
WAI LH OUT VLV OPEN
WAIVLO
PROBEPB PROBE WINDOW HEAT P/B
WSHRW
N1L1 N1L2
N1A1
100
N1A2
N1A1
50
N1A2
AIR TEMP
CTAT
0
SAT--
(%)
0 CTAT
SAT
-50
DEGC
-100
ALT
40
30
ALT
CAS
400
CAS
20
200
10
KT
0
10^3
0
10:28:00 10:29:00 10:30:00 10:31:00 10:32:00 10:33:00 10:34:00 10:35:00 10:36:00 10:37:00 10:38:00
TEMPS(H)
A/C : A330- MSN 0733 FLIGHT No 0041 Immat: . E C- J P F
Airline: X F Type: Flight: A EA 0 4 1 From: LEMD To: SAEZ
CG (%) 31.12
WGT (LBS) 347320.00
OVERViEW
WGT (KG) 157378.41 ICE Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/source/dfdr/dfdr/LR/Ice.ilv 1.1.5
AP12E
FD12E
ATHRE
ATHRA
MW
STALLW
TLU2V
TLU1V
NLAW
ALAW
WAION (1=ON)
CPT ADC1
F/O ADC2
CPT IRS1
F/O IRS2
ADR2F
ADR1F
ADR3F
ADR123F
AOAIRS1
5
AOAIRS2
AOAIRS3
AOAIRS3
AOAIRS2
AOAIRS1
(DA)
-0
VRTG
1.0 VRTG
VRTG
G
0.5
AOA ALT
5 37500
CAOA1 ALT
ISISALT
CAOA2 CAOA1 (__) CAOA2 (--)
DEG
MNADC
-0 35000
CMACH
1.0
CMACH
MNADC
32500
CAS
0.5 350
CAS
CAS
ISISCAS 30000
()
0.0 300
AIR TEMP
ISISCAS
27500 50
SAT
(KT)
250 CTAT
ALT
CTAT
25000 0
ISISALT
DEGC
22500 SAT -50
(FT)
20000
10:28:00 10:29:00 10:30:00 10:31:00 10:32:00 10:33:00 10:34:00 10:35:00 10:36:00 10:37:00 10:38:00
MR1 : P0733V0041DFDR Time
CG (%) 31.4
WGT(KG)
OVERViEW 157542 AIR DATA DISCREPANCY
/workgroup/operation/dfdr/visage/bertille/2014/P0733V0041-Hailstorm/ADR-DISAGREE.ilv 1.1.6
OIL LP 1
OIL LP 2
Oil Q
20 Oil Q2
Oil Q2 Oil Q1
Oil Q1
10
Qts
0
N2VIB
3
1 N2V1 N2V2
N1VIB CU
3 0
1
N1V1 N1V2
CU
0
N2ACT
100 N2A2
N2A1
80
60
40
20
%
0
N1ACT
100
N1A2
80
60 N1A1
40
20
%
0
EGT
800
EGT2
deg C EGT1
400
TRA
80
TRA1 TRA2
deg A
0
ZP
40
SAT CAS CAS

30 300
ZP
MACH
20 0 200 0.8 MACH
SAT
-30 100 0.4
10^3
FT deg C KT
0 -60 0 0.0
10:28:00 10:29:00 10:30:00 10:31:00 10:32:00 10:33:00 10:34:00 10:35:00 10:36:00 10:37:00 10:38:00 10:39:00
TIME(H)
A/C : A330- MSN 0733 FLIGHT No 0041 MR1 : P0733V0041DFDR
DFDR Data - A330 MSN 0486 - GE - Oil and Vibrations parameters AT GMT START
ZP = 35980 FT
OVERViEW ENG 1 CAS = 266 KT

MACH = 0.80
ENG 2 SAT = -50 DC
Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/source/engs/Long_Range/GE/DFDR_plots/DFDR-LR-GE-VibrationMain-Eng12.ilv 1.1.7
ND FIRST OFFICER RANGE
10NMF
20NMF
40NMF
80NMF
160NMF
320NMF
ND CAPTAIN RANGE
10NMC
20NMC
40NMC
80NMC
160NMC
320NMC
ND FIRST OFFICER MODE
ARCF
PLANF
RVORF
RNAVF
RENGF
ND CAPTAIN MODE
ARCC
PLANC
RVORC
RNAVC
RENGC
RADAR OPERATING MODE

0=STBY,1=WXR ONLY,2=MAP,3=CONTOUR,4=TEST
5=TURB ONLY,6=WXR+TURB
RADSTBY
RADWEAT
RADMAP
RADCONT
RADTEST
RADTURB
RADWXRTURB
RADWSHR
10:28:00 10:29:00 10:30:00 10:31:00 10:32:00 10:33:00 10:34:00 10:35:00 10:36:00 10:37:00 10:38:00
TEMPS(H)
OVERViEW DMC_MODE_RANGE Edited : 8/10/2014 Figure

/workgroup/operation/dfdr/visage/source/dfdr/dfdr/LR/DMC_mode_range.ilv 1.1.8
Annex N° 5
FDR data plots – Zoom
GSI 420.1022/15 (TL) 13-Feb-15 21/21

AP1E
AP2E 0.00
ATHRE 0.00
ATHRA 0.00
VMOW 0.00
CPTMW1 0.00
CPTMW2 0.00
FOMW1 0.00
FOMW2 0.00
0.00
STKP
10
STKPC
-0.09 DA
STKPF
-0.22 DA
DA ELV SIDE STICK PITCH POSITION FIRST-OFFICER (STKPF - -)

0 10
ELVL
CAPTAIN (STKPC__ )
ELVR
STAB ELEVATORS RIGHT (ELVR - -)

0 STAB 1616.00 FT/MI
DA 0.26 DA
0.09
LEFT (ELVL __ )
-1.89 DA
VRTG VSPD
1.5 0
G VSPD
VRTG FT/MI
1.0 -1000
MNADC
0.70 MNADC 0.85 G
LONG CTASSAT
0.65 0.5
0.65
10:35:09-166.667
ALT SALT
G FCU
LONG
0.60 0.0 20
0.02 G
SALTFCU ALT
22492.00 FT
CAOA 14976.00 FT
2
10 10
3.52 DA
PTCH
10^3
FT
5 0
405.31 CAOA1 ___
CAOA
GS CAOA2 - -
1
400
DA CTASSAT 1.76 DA
287.12 KT
1.05 DA
0
SCAS
PTCH PFD
390 280
GS
CAS_ADC
385.00 KT
N1A2
160 380 270
N1A1
SCASPF
KT 263.00
120 370 CAS_ADC 260
TRA KT
80 100 250
TRA2
TRA1
N1A
56.53 %
52.91 %
40 50 TRA
% DA 16.08
14.06DA
DA
-0 0
10:33:00 10:33:20 10:33:40 10:34:00 10:34:20 10:34:40 10:35:00 10:35:20 10:35:40 10:36:00 10:36:20
TEMPS(H)
CG (%) 31.20
GWL (LBS) 346960
GWK (KG) 157378
CRUISE(LONGITUDINAL AXIS) Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/bertille/2014/P0733V0041-Hailstorm/cruise-longi.ilv 1.2.1
AP1E STKR
AP2E 10
STKRF
STKRC
AIL
O SIDE STICK ROLL POSITION FIRST-OFFICER (STKRF - - ) DA
10 0
AILRO
CAPTAIN (STKRC ___ )
AILLO OUTER AILERONS RIGHT (AILRO - -)
AIL
DA I
0 10
AILRI LEFT (AILLO__ )
AILLI INNER AILERONS RIGHT (AILRI - -)
DA SSLIP
0 5
LEFT (AILLI__ )
DA DA
5 0
SSLIP
DA
0
ROLL
10
RUDP RUDD
ROLL
10 10 0
RUDT DA
-10
DA RUDP RUDD RUDT

0 0 DRIFT ANGLE
LATG
0.1
LATG
SAT
G
0.0 -10
SAT
-20
SAT
CTAS
SAT
500 -30
GS
HDG
400 360
CTASSAT GS WD
WD
KT
300 270
HDG
DA
180
WS
WS
60
KT
40
SLAT FLAP SFLP

20 20 5
SFLP
0
DA DA SLAT FLAP
0 0
10:33:00 10:33:20 10:33:40 10:34:00 10:34:20 10:34:40 10:35:00 10:35:20 10:35:40 10:36:00 10:36:20
TEMPS(H)
CG (%) 31.20
GWL (LBS) 346960 CRUISE (LATERAL AXIS)
GWK (KG) 157378 Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/bertille/2014/P0733V0041-Hailstorm/cruise-lat.ilv 1.2.2
FMA :ZONE E1,E2 ET E3
AP1E AP1 (WHITE)
AP2E 1.00 AP2 (WHITE)
FD1E
FD2E
0.00 FD1 (WHITE)
1.00 FD2 (WHITE)
ATHRE 1.00
ATHRA ATHR (WHITE)
0.00 ATHR (CYAN)
APOFFW
APOFFV
0.00
FMA LONGI. MODE: ZONE B1 0.00 SRS (GREEN)
SRSD 0.00
ALTCSTD 0.00 ALT CST (GREEN)
ALT CRZ (GREEN)
ALTCRZD 0.00 0.00
ALTMODD 0.00 0.00 ALT (GREEN)
ALTACQCS 0.00 ALT CST* (GREEN)
ALTACQCR ALT CRZ* (GREEN)
0.00
ALTACQD ALT* (GREEN)
VSD V/S (GREEN)
CLBD CLB (GREEN)
DESD 0.00 DES (GREEN)
OPCLBD OP CLB (GREEN)
0.00
OPDESD 0.00 1.00 OP DES (GREEN)
GSTRKD G/S (GREEN)
0.00
GSCPTD 0.00 G/S* (GREEN)
FPAD 0.00 FPA (GREEN)
FMA LONGI. MODE ARM.: ZONE B2 0.00 ALT (CYAN ALTACQARM)

ALTARM
FDESARM 1.00 FINAL (CYAN)
FG LONGI. SUBMODES 0.00

SPDTHR SPEED/THRUST
VSSPD VS SPEED
0.00
FPASPD 0.00 FPA SPEED
VPATHSPD VPATH SPEED
0.00
VPATHTHR 0.00 VPATH THRUST
FMA MODE: ZONE BC1 0.00

ROLLOUT ROLL OUT (GREEN)
FLARE 0.00 FLARE (GREEN)
LANDTRK LAND (GREEN)
0.00
LANDARM 0.00 LAND ARM
ALIGN 0.00 ALIGN
FMA LAT. MODE: ZONE C1 0.00

TRKGAD GA TRK (GREEN)
LOCBCCPT LOC B/C* (GREEN)
0.00
LOCCPTD 0.00 LOC* (GREEN)
HDGD 0.00 HDG (GREEN)
RWYLOCD 1.00 RWY LOC (GREEN)
RWYTRKD 0.00 RWY TRK (GREEN)
TRKD TRACK (GREEN)
0.00
LOCBCTRK 0.00 LOC B/C (GREEN)
LOCTRKD 0.00 LOC (GREEN)
10:35:21-944.444 APP NAV (GREEN)
APPNAVD 0.00
NAVD 0.00 NAV (GREEN)
FG LAT. SUBMODES 0.00

NAVTRK NAV TRACK
NAVHDG 0.00 NAV HDG
NAVHPATH NAV HPATH
0.00
SPEED/MACH TARGET SELECTION 0.00
SCASFCUS SPDTGT FROM FCU SEL
SCASFGS 0.00 SPDTGT FROM FG PFD
SCASAPPS
1.00
SPDTGT FROM FG/FM VAP
SPDAUTO 0.00 AUTO SPEED CONTROL
SPDMANU 0.00 MANUAL SPEED CONTROL
MACHFCUS 1.00 MACH SEL
FMA MODE: ZONE A1+A2 0.00

MANTOGAD MAN TOGA (WHITE)
THRMCTD THR MCT (GREEN)
0.00
MANFLXD 0.00 MAN FLX (WHITE)
MANDTOD MAN DTO (WHITE)
0.00
THRCLBD THR CLB (GREEN)
0.00
MANMCTD 0.00 MAN MCT (WHITE)
MANTHRD MAN THR (WHITE)
0.00
THRLVRD 0.00 THR LVR (GREEN)
THRIDLED 0.00 THR IDLE (GREEN)
THRDESD THR DES (GREEN)
0.00
AFLOORD 0.00 A FLOOR (GREEN)
TOGALKD TOGA LK (GREEN)
0.00
SPEEDD 0.00 SPEED (GREEN)
MACHD 0.00 MACH (GREEN)
FMA MODE: ZONE A3 0.00

THRLKD THR LK (AMBER)
ATHRRTD RETARD
0.00
0.00
FCU: BARO. REF. SELECTION
STDC
STDF 1.00
QNHF
QNHC 1.00
QFEC 0.00
QFEF 0.00
FE1V 0.00
FE2V
FG1F
0.00
1.00
FG2F 1.00
FM1F 0.00
FM2F 0.00
0.00
FMAD 0.00 FMA DISPLAYED
EVTMKR 1.00 EVENT MARKER
0.00
10:33:00 10:33:20 10:33:40 10:34:00 10:34:20 10:34:40 10:35:00 10:35:20 10:35:40 10:36:00 10:36:20
TEMPS(H)
FMA DISPLAYS-AP MODES Edited : 8/10/2014 Figure

/workgroup/operation/dfdr/visage/bertille/2014/P0733V0041-Hailstorm/AP-modes.ilv 1.2.3
AP1E
AP2E
FCTL
HYDGW
HYDYW
HYDBW
LAW
NLAW
ALAW
DLAW
FCPC1CL
FCPC2CL
FCPC3CL
FCSC1CL
FCSC2CL
NCCL
FAULT (COMPUTERS AND ELEVATORS)

FCPC1F
FCPC2F
FCPC3F
FCSC1F
FCSC2F
SLT1F
SLT2F
FLP1F
FLP2F
STKP
LRELVF
10
STKPC
STKPF STICKS (POSITION AND VALIDITY)
DA CAPTAIN (STKPC __) FIRST-OFFICER (STKPF - - )

0
STKR
10
STKRC
PH
7.0 STKRF
DA CAPTAIN (STKRC __ ) FIRST-OFFICER (STKRF - - )

0
6.5
FLIGHT PHASE
6.0
STKCF
STKFF
STKFINOP
STKCINOP
CAS_ADC
AILLIBV
CAS_ADC ALT
AILLIGV
300 23600
CAS_ADC ALT
AILLOGV
AILLOYV AILERON VALIDITY
1=AVAILABLE
AILRIBV
AILRIGV
200 22800
AILROGV ALT
AILROYV
100 22000
ELVRGV
ELVRYV
ELVLBV
ELVLGV ELEVATOR VALIDITY
1=AVAILABLE
YAW DAMPER
YDGV
YDYV
SBNR
RUDTW
MASTER WARNING
CPTMW1
CPTMW2
FOMW1
FOMW2
10:33:00 10:33:20 10:33:40 10:34:00 10:34:20 10:34:40 10:35:00 10:35:20 10:35:40 10:36:00 10:36:20
TEMPS(H)
ZOOM
WGT(KG) 157378
CDVE-LAW-FAULT-STICKS-YAW DAMPER
/workgroup/operation/dfdr/visage/bertille/2014/P0733V0041-Hailstorm/CDVE.ilv 1.2.4
CAPT / FO MAST WNG & CAUTION
CPTMW1
FOMW2
CPTMC1
FOMC2
ICE DETECTOR
DD1F
DD2F
DD1ICEDET
DD2ICEDET
D1SICEDET1
D2SICEDET1
NAI P/B ON ENG1

NAI1ON
NAI ENG1 SEL
NAI1S

NAI P/B ON ENG2
NAI2ON
NAI ENG2 SEL
NAI2S
WAISEL WAI SYS SELECT ON
WAION WAI SYS ON

WAI LH IN VLV OPEN
WAIVLI
WAI RH IN VLV OPEN
WAIVRI
WAI RH OUT VLV OPEN
WAIVRO
WAI LH OUT VLV OPEN
WAIVLO
PROBEPB PROBE WINDOW HEAT P/B
WSHRW
N1L1 N1L2
N1A1
100
N1A2
N1A2
N1A1
50
AIR TEMP
CTAT
0
SAT--
SAT
(%)
0 CTAT
-50
DEGC
-100
ALT
40
30
CAS
400 ALT
CAS
20
200
10
KT
0
10^3
0
10:33:00 10:33:20 10:33:40 10:34:00 10:34:20 10:34:40 10:35:00 10:35:20 10:35:40 10:36:00 10:36:20
TEMPS(H)
A/C : A330- MSN 0733 FLIGHT No 0041 Immat: . E C- J P F
Airline: X F Type: Flight: A EA 0 4 1 From: LEMD To: SAEZ
CG (%) 31.36
WGT (LBS) 346960.00
ZOOM
WGT (KG) 157160.68 ICE Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/bertille/2014/P0733V0041-Hailstorm/Ice.ilv 1.2.5
AP12E
1.00
FD12E 0.00
1.00
ATHRE
1.00
ATHRA
1.00
MW
STALLW 0.00
0.00
TLU2V
TLU1V 0.00
NLAW 0.00
1.00
ALAW
WAION (1=ON) 0.00
CPT ADC1 0.00
1.00
F/O ADC2
1.00
CPT IRS1
1.00
F/O IRS2
1.00
ADR2F
ADR1F 0.00
ADR3F 0.00
ADR123F 0.00
AOAIRS1 0.00
5
AOAIRS2
AOAIRS3
AOAIRS3
AOAIRS2
AOAIRS1 2.11
2.11 (DA)
(DA)
(DA)
-0
10:36:15-833.333
VRTG
1.13 G
1.0
VRTG
VRTG
G
0.5
AOA ALT
5 23850
CAOA1 ALT
ISISALT
CAOA2 CAOA1 (__) CAOA2 (--)
2.46
2.11 DEG
DEG
DEG
-0 23600 MNADC
CMACH
1.0
MNADC
23350
CMACH
CAS
0.64
0.64
0.5 350
CAS
ISISCAS 23100
CAS
()
0.0 300
AIR TEMP
22850 279.38 KTS
kt 50
ISISCAS 278.75 SAT
22816.00 ft
22804.00
(KT) (FT)
250 CTAT
ALT CTAT
22600 0
1.01
SAT -19.75 DEGC
DEGC
22350 -50
ISISALT
(FT)
22100
10:33:00 10:33:20 10:33:40 10:34:00 10:34:20 10:34:40 10:35:00 10:35:20 10:35:40 10:36:00 10:36:20
MR1 : P0733V0041DFDR Time
CG (%) 31.2
WGT(KG)
ZOOM 157378 AIR DATA DISCREPANCY
/workgroup/operation/dfdr/visage/bertille/2014/P0733V0041-Hailstorm/ADR-DISAGREE.ilv 1.2.6
OIL LP 1
OIL LP 2
Oil Q
20 Oil Q2
Oil Q2 Oil Q1
Oil Q1
10
Qts
0
N2VIB
3
1 N2V1
N1VIB N2V2
CU
3 0
1
N1V1 N1V2
CU
0
N2ACT
100
N2A1 N2A2
80
60
40
20
%
0
N1ACT
100
80
60 N1A2
N1A1
40
20
%
0
EGT
800
deg C
400 EGT1 EGT2
TRA
80
TRA1 TRA2
deg A
0
ZP
40
SAT CAS
CAS
30 300
MACH ZP
20 0 200 0.8 MACH
SAT
-30 100 0.4

10^3
FT deg C KT
0 -60 0 0.0
10:33:00 10:33:20 10:33:40 10:34:00 10:34:20 10:34:40 10:35:00 10:35:20 10:35:40 10:36:00 10:36:20 10:36:40
TIME(H)
A/C : A330- MSN 0733 FLIGHT No 0041 MR1 : P0733V0041DFDR
DFDR Data - A330 MSN 0486 - GE - Oil and Vibrations parameters AT GMT START
ZP = 23728 FT
ZOOM ENG 1 CAS = 288 KT

MACH = 0.67
ENG 2 SAT = -26 DC
Edited : 8/10/2014 Figure
/workgroup/operation/dfdr/visage/source/engs/Long_Range/GE/DFDR_plots/DFDR-LR-GE-VibrationMain-Eng12.ilv 1.2.7
ND FIRST OFFICER RANGE
10NMF
20NMF
40NMF
80NMF
160NMF
320NMF
ND CAPTAIN RANGE
10NMC
20NMC
40NMC
80NMC
160NMC
320NMC
ND FIRST OFFICER MODE
ARCF
PLANF
RVORF
RNAVF
RENGF
ND CAPTAIN MODE
ARCC
PLANC
RVORC
RNAVC
RENGC
RADAR OPERATING MODE

0=STBY,1=WXR ONLY,2=MAP,3=CONTOUR,4=TEST
5=TURB ONLY,6=WXR+TURB
RADSTBY
RADWEAT
RADMAP
RADCONT
RADTEST
RADTURB
RADWXRTURB
RADWSHR
10:33:00 10:33:20 10:33:40 10:34:00 10:34:20 10:34:40 10:35:00 10:35:20 10:35:40 10:36:00 10:36:20
TEMPS(H)
ZOOM DMC_MODE_RANGE Edited : 8/10/2014 Figure

/workgroup/operation/dfdr/visage/source/dfdr/dfdr/LR/DMC_mode_range.ilv 1.2.8

Air Europa A332 Incident Report

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ANEXO

El presente Informe es un documento técnico que refleja la opinión de la

De conformidad con lo señalado en el Anexo 13 al CONVENIO SOBRE

La conducción de la investigación ha sido efectuada sin recurrir necesa-

Los resultados de esta investigación no condicionan ni prejuzgan los de

INCIDENTE OCURRIDO EN: Aeropuerto Internacional Ezeiza -“Ministro Pistarini”,

FECHA: 9 de septiembre de 2014. HORA (UTC): 11:00 h (aprox)

AERONAVE: Avión. MARCA: Airbus.

MODELO: A-330-202 MATRÍCULA: EC-JPF.

COMANDANTE, PRIMER OFICIAL y PILOTO DE REFUERZO: con licencia españo-

PROPIETARIO: Empresa de transporte aéreo regular internacional.

1.1 Reseña del vuelo

1.1.1 El día 8 de septiembre de 2014, a las 21:55 h, la aeronave A-330-202,

1.1.2 Luego de volar 12:30 h aproximadamente, el piloto al mando inició el des-

1.1.3 Durante la fase de descenso, mientras se encontraba entre los niveles FL

1.1.4 Producto del impacto de granizo, ambos parabrisas resultaron dañados

1.1.5 El comandante del vuelo decidió no declararse en emergencia pero solici-

1.1.6 El aterrizaje y posterior rodaje a la posición de estacionamiento se efec-

1.1.7 Una vez en la posición final de estacionamiento se pudo observar que la

1.1.8 El incidente ocurrió de día y en condiciones de vuelo IMC (condiciones

1.1.9 La notificación del suceso fue realizada por personal de la oficina

1.2 Lesiones a personas

Lesiones Tripulantes Pasajeros Otros

1.3 Daños en la aeronave

1.3.1 Célula: Daños en ambos parabrisas frontales, afectando la superficie ex-

1.3.2 Motores: los carenados de pilones de sujeción de ambos motores sufrie-

1.4 Otros daños

1.5 Información sobre el personal.

De 55 años de edad, de nacionalidad española, era titular de la licencia

De acuerdo con lo informado por la Comisión de Investigación de Acci-

La cantidad de horas de vuelo, al momento del incidente, eran las siguien-

Total de horas de vuelo: 17719:00 h

1.5.2 Primer oficial

De 47 años de edad, de nacionalidad española, era titular de la licencia

La cantidad de horas de vuelo, al momento del incidente, eran las siguien-

Total de horas de vuelo: 11585:00 h

1.5.3 Piloto de refuerzo

De 53 años de edad, de nacionalidad española, era titular de la licencia

De acuerdo con lo informado por la CIAIAC, el certificado de aptitud psico-

La cantidad de horas de vuelo, al momento del incidente, eran las siguien-

Total de horas de vuelo: 19047:00 h

1.6 Información sobre la aeronave

1.6.1 Información general

Aeronave fabricada por Airbus Industries, modelo A330-202, con número

Plan de mantenimiento por aeronavegabilidad continuada conforme al

Su certificado de matrícula fue registrado a nombre de una empresa de

Su certificado de aeronavegabilidad fue emitido por la Delegación de Se-

Los registros de mantenimiento indicaban que la aeronave estaba equi-

El combustible requerido y utilizado era JET A-1. Al momento del inciden-

Marca General Electric, modelo CF6-80E1A4, con número de serie

1.6.4 Peso y balanceo de la aeronave

El peso máximo de despegue era de 233000 kg, el de aterrizaje era de

Los pesos calculados al momento del incidente eran los siguientes:

Vacío: 121826 kg.

Los pesos y el centro de gravedad (CG) se encontraban dentro de la en-

1.7 Información meteorológica

1.7.1 De acuerdo a los datos aportados por el Servicio Meteorológico Nacional

1.7.2 En función de las apreciaciones anteriormente descriptas se puede inferir

1.7.3 De acuerdo con la información disponible para la tripulación del World

1.8 Ayuda a la navegación