200-32-15 SB Index

se
LANDING GEAR - MAIN UNDERCARRIAGE - INTRODUCTION OF ‘P’ CLIPS TO BRAKE SERVO VALVE

ns e u
HARNESS
1. PLANNING INFORMATION

itio siv
A. Effectivity

nd clu
Aircraft affected : AIRBUS A320-100

Co ex
A320-200 TWIN

s & the
Unit affected : Main Landing Gear
Type Nos. A320-100 MLG AND DRESSINGS

rm or
Te 3 f
201088011 Iss 1
201088012 Iss 1 } Production Aircraft

S 02
SL -2
201220023 Iss 1
201220024 Iss 1
er eb } 4th Aircraft

201220021 Iss 1
}
nd 8-F
201220022 Iss 1 3rd Aircraft
)u 0

201220019 Iss 1
201220020 Iss 1 } 1st and 2nd Aircraft
up on

A320-200 TWIN MLG & DRESSINGS

ro m
(G Ki

201162007 Iss 1
201162008 Iss 1
es ang

B. Reason
rlin Y

(1) To ensure correct assembly of connections, to avoid the chafing of harnesses of the brake
Ai y:

servo valve harness as requested by Air France. It is recommended by DRL that the
rn d b

modification is carried out fully retrospectively at the first opportunity.

he e

C. Description
ut ad

(1) This bulletin introduces two ‘P’ clips fitted to the harnesses on the brake servo valve.
So wnlo

D. Approval
(1) The technical content of this bulletin is approved under CAA Approval No. DAI/1018/39.
ina Do

E. Man Power -
Ch l -

(1) The work will take an estimated 1 1/2 manhours to embody the modification.
of ntia
ide
nf
Co

AC11042 200-32-15
Oct 19/89 Page 1 of 7
 se
F. Material

ns e u
Qty.
Part No. Per Unit Description Availability/Cost

itio siv
(1) P338321 2 ‘P’ Clip On Request

nd clu
(2) AN3-4A 1 Bolt On Request

Co ex
(3) AN960-10L 1 Washer On Request

s & the
(4) NAS1021-N3 1 Nut On Request

rm or
Date of delivery of Mod. Sets : 5 months from receipt of order

Te 3 f
Rate of delivery : As required

S 02
G. Tooling

SL -2
(1) None.
er eb
H. Weight and Balance
nd 8-F

(1) Not affected.

)u 0

I. References
up on

(1) Dowty Rotol Component Maintenance Manual 32-11-12 for A320-100.

ro m

(2) Dowty Rotol Component Maintenance Manual 32-11-24 for A320-200 TWIN.
(G Ki

(3) Dowty Rotol Standard Practices manual 20-00-05.

es ang

(4) Figures 1, 2, 3 and 4 of this bulletin.

rlin Y

J. Other Publications Affected

Ai y:

(1) Component Maintenance Manual 32-11-12 and its illustrated parts list will be revised
rn d b

accordingly.
he e

(2) Component Maintenance Manual 32-11-24 and its illustrated parts list will be revised
ut ad

accordingly.
So wnlo

2. ACCOMPLISHMENT INSTRUCTIONS
A. Embodiment Instructions
ina Do

(1) -
Fit the ‘P’ clips to the electrical harnesses as shown in Figures 1, 2, 3 and 4. Secure the ‘P’ clips
Ch l -

using the bolts, washers and nuts and tighten securely.

of ntia

(2) Ensure that the routing of the harnesses follows the routing shown in Figures 1, 2, 3 and 4.
B. Method of Identification
ide

NOTE : Retain the part number scribed in the ‘REF(P/N)’ position on the nameplate.
nf

(1) Identify the embodiment of the modification by scribing the modification number, in accordance
Co

with PS405-3, in the ‘MODIF’ position as follows:

Modification No.
(c)AC11042

200-32-15 Nov 9/89

Page 2
 se
C. Part Number Changes

ns e u
Old Part Number New Part Number

itio siv
nd clu
A320-100 201089001-40 201089001-41
MLG COMPLETE 201089002-40 201089002-41 } Production Aircraft

Co ex
201219005-10 201219005-11
201219006-10 201219006-11 } 4th Aircraft

s & the
201219003-10 201219003-11
} 3rd Aircraft

rm or
201219004-10 201219004-11

Te 3 f
201219001-7 201219001-8
201219002-7 201219002-8 } 1st and 2nd Aircraft

S 02
SL -2
A320-100 201088011 201088013
MLG & DRESSINGS 201088012
er eb 201088014 } Production Aircraft
nd 8-F
201220023 201220029
201220024 201220030 } 4th Aircraft
)u 0

201220021 201220027
} 3rd Aircraft
up on

201220022 201220028
201220019 201220025
} 1st and 2nd Aircraft
ro m

201220020 201220026
(G Ki

A320-100 201127003 201127005

} Production Aircraft
es ang

DRESSINGS 201127004 201127006

201223005 201223009
} 4th Aircraft
rlin Y

201223006 201223010
Ai y:
rn d b

201223003 201223007
201223004 201223008 } 3rd Aircraft
he e

201127095 201223001
ut ad

201127094 201223002 } 1st and 2nd Aircraft

So wnlo

A320-200 TWIN 201167001-6 201167001-7

MLG COMPLETE 201167002-6 201167002-7
ina Do

A320-200 TWIN
MLG & DRESSINGS
201162007
201162008 -
201162009
201162010
Ch l -
of ntia

A320-200 TWIN 201161001 201161003

DRESSINGS 201161002 201161004
ide
nf
Co

3. MATERIAL INFORMATION
A. None.

Oct 19/89 200-32-15

Page 3
Page 4
Co

200-32-15
nf
ide
of ntia
Ch l -
ina Do
So wnlo
ut ad
he e
rn d b
Ai y:
rlin Y
es ang
(G Ki
ro m
up on
)u 0

-
nd 8-F
er eb
SL -2
S 02
Te 3 f

FIGURE 1 FITTING OF ‘P’ CLIP A320-100 LH

rm or
s & the
Co ex
nd clu
itio siv
ns e u
se

1347/7/88K

Oct 19/89
 Co
nf
ide

Oct 19/89
of ntia
Ch l -
ina Do
So wnlo
ut ad
he e
rn d b
Ai y:
rlin Y
es ang
(G Ki
ro m
up on
)u 0

-
nd 8-F
er eb
SL -2
S 02
Te 3 f
rm or
s & the

FIGURE 2 FITTING OF ‘P’ CLIP A320-100 RH

Co ex
nd clu
itio siv
ns e u
se

1347/81/88K

200-32-15
Page 5
Page 6
Co

200-32-15
nf
ide
of ntia
Ch l -
ina Do
So wnlo
ut ad
he e
rn d b
Ai y:
rlin Y
es ang
(G Ki
ro m
up on
)u 0

-
nd 8-F
er eb
SL -2
S 02
Te 3 f
rm or

FIGURE 3 FITTING OF ‘P’ CLIP A320-200 TWIN LH

s & the
Co ex
nd clu
itio siv
ns e u
se

1347/82/88K

Oct 19/89
 Co
nf
ide

Oct 19/89
of ntia
Ch l -
ina Do
So wnlo
ut ad
he e
rn d b
Ai y:
rlin Y
es ang
(G Ki
ro m
up on
)u 0

-
nd 8-F
er eb
SL -2
S 02
Te 3 f
rm or
s & the
Co ex

FIGURE 4 FITTING OF ‘P’ CLIP A320-200 TWIN RH

nd clu
itio siv
ns e u
se

1347/83/88K

200-32-15
Page 7