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On A/c 001-002, 101-150

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Customer : IYE Manual : AMM

Type : A318/A319/A320/A321 Selected applicability : ALL


Rev. Date : Nov 01, 2022

** ON A/C 001-002, 101-150


7. Operation/Control and Indicating
(Ref. Fig. Starting System - Block Diagram SHEET 1)

Print Date: February 27, 2024 Page 1 of 3


© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Customer : IYE Manual : AMM
Type : A318/A319/A320/A321 Selected applicability : ALL
Rev. Date : Nov 01, 2022

AVAIL
ON
2KD
START COMMAND IN

301PP 2KA
28VDC COCKPIT
START SWITCH

START CONTACTOR IN
BATTERY
6KA

START CONTACTOR OUT


3PP
28VDC 10KA 5KA
BACK-UP START
START CONTACTOR
CONTACTOR

BCL1 1PB1

BCL2 1PB2

BACK-UP START
CONTACTOR OUT

MOTOR CTL

59KD ECB

IGN
UNIT
P10
M
8KA
STARTER MOTOR

APU

N_MM_494200_0_LEM0_01_00

Figure 49-42-00-18500-12-A / SHEET 1/1 - Starting System - Block Diagram


** ON A/C 001-002, 101-150

Print Date: February 27, 2024 Page 2 of 3


© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Customer : IYE Manual : AMM
Type : A318/A319/A320/A321 Selected applicability : ALL
Rev. Date : Nov 01, 2022

When you put the MASTER SW pushbutton switch in the ON position:


· the main relay 4KD is energized,
· the ECB starts the prestart test,
· the APU fuel pump system is energized,
· the APU air inlet door opens.
When you put the START pushbutton switch in the ON position:
· the ON legend in the START pushbutton switch comes on,
· The ECB energizes the back-up start contactor 10KA and (1.5 seconds later) the start contactor 5KA, The
contactors energize the starter motor 8KA with 28 V DC when these conditions are met:
.the air intake is open,
.the Power-Up Test (PUT) is complete,
.the oil level test is complete.
· the contactors energize the starter motor 8KA with 28 V DC and the APU starter motor starts to turn. The
starter clutch engages and turns the APU main shaft,
· the ECB energizes the igniters,
· the ECB energizes the de-oil solenoid valve to the open position,
· the APU operation data is shown on the lower ECAM display unit.

NOTE: During Ram Air Turbine (RAT) extension, APU starting is inhibited by the Battery Charge Limiters (BCL
1 and BCL 2), which prevent operation of the main start contactor 5 KA.

At 3% speed, the ECB energizes the fuel solenoid valve to the open position.

At 5% speed, the ECB controls the fuel flow to the APU.

At 55% speed, the ECB:


· de-energizes the start contactor 5KA which switches off the starter motor 8KA and the ECB accelerates the
APU automatically,
· de-energizes the back-up start contactor 10KA, after 5 seconds,
· de-energizes the de-oil solenoid valve to the closed position.
At 95% speed:
· the ECB controls and monitors the APU automatically,
· the green AVAIL legend in the START pushbutton switch comes on,
· the blue ON legend in the START pushbutton switch goes off.
· the APU bleed valve is ready for operation,
· the APU generator is ready for operation.

End of document

Print Date: February 27, 2024 Page 3 of 3


© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

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