(10) Put blanking plugs on the elbow connectors (19).
NOTE : Make sure that the blanking plugs are correctly installed
____ before each flight if subsequent flights in this configuration are necessary.
R **ON A/C 001-003, 051-052,
Subtask 32-12-00-860-058
C. ECAM Display During Flight with One MLG Door Assembly Missing
NOTE : The main landing gear and the nose landing gear must be extended
____ at all times during flight with one MLG door missing (control lever 6GA in the DOWN position).
(1) The ECAM displays (for the applicable missing MLG door) are as follows:
(a)
ECAM indications:
-door position hinge bar - DOOR IN TRANSIT (amber)
-L/G DOOR NOT CLOSED (amber) - in flight phases 1, 2, 3, 6, 7, 9 & 10
-landing gear locked down triangles (green).
(b)
ECAM warnings:
-L/G DOOR.
NOTE : The warning(s) that follow will only show if LGCIU 1
____ and/or 2 are reset above 70 knots (or a power interrupt occurs above 70 knots).
-
L/G LGCIU 1 FAULT (Reverser 1 does operate although listed as "INOP") or
-
L/G LGCIU 2 FAULT (Reverser 1 does operate although listed as "INOP") or
-
L/G LGCIU 1 + 2 FAULT
-
L/G RECYCLE, MAX SPEED 260 KNOTS, INCREASED FUEL CONSUMPTION, GRAVITY EXTENSION, GPWS OFF, L/G CONTROL NOT AVAIL, ENGINE APPROACH IDLE ONLY, REVERSER 1 + 2, NW STEER, LGCIU 1 + 2.
1EFF : ALL 1 32-12-00Page 408 1 1 May 01/05 1 1 1CES 1
**ON A/C ALL R Post SB 32-1182 For A/C 001-003,051-052, Subtask 32-12-00-860-058-A
C. ECAM Display During Flight with One MLG Door Assembly Missing NOTE : The main landing gear and the nose landing gear must be extended
____ at all times during flight with one MLG door missing (control lever 6GA in the DOWN position).
(1) The ECAM displays (for the applicable missing MLG door) are as follows:
(a)
ECAM indications:
-door position hinge bar - DOOR IN TRANSIT (amber)
-L/G DOOR NOT CLOSED (amber) - in flight phases 1, 2, 3, 6, 7, 9 & 10
-landing gear locked down triangles (green).
(b)
ECAM warnings:
-L/G DOOR.
NOTE : The warning(s) that follow will only show if LGCIU 1
____ and/or 2 are reset above 70 knots (or a power interrupt occurs above 70 knots).
-L/G RECYCLE, MAX SPEED 250 KNOTS, INCREASED FUEL CONSUMPTION. **ON A/C ALL
Subtask 32-12-00-020-063
D. Removal of the MLG Fixed Fairing Assembly and Attaching Parts
(Ref. Fig. 403/TASK 32-12-00-991-009)
CAUTION : DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF
_______
CARBONFIBER REINFORCED PLASTIC.
(1)
Remove the applicable fixed fairing assembly (Ref. TASK 32-12-14-000-001).
(2)
Remove and retain all the nuts and bolts that attach the fixed fairing assembly from the MLG.
1EFF : ALL 1 32-12-00Page 409 1 1 May 01/05 1 1 1CES 1
Bonding Straps to MLG Leg - Removal/Installation Figure 403/TASK 32-12-00-991-009
1EFF : 1 1R 1CES ALL 1 11 1 32-12-00 Page 410 Nov 01/00
(3)
Remove and discard the cotter pin (51) from the nut (50).
(4)
Remove the nut (50), the washer (49) and the bolt (48). Remove and retain the bonding strap (47) from the bracket (46).
(5)
Install the bolt (48), the washer (49) and the nut (50).
(6)
Safety the nut (50) with a new cotter pin (51).
(7)
Apply SEALANTS (Material No. 09-016) to the head of the bolt (48) and the nut (50).
R WARNING : CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE TASK.
_______ R LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
(8)
Remove and discard the lockwire from the bolts (53) and (56).
(9)
Remove the bolt (56), the washer (55) and the bonding strap (54) from the bracket (52). Retain the bonding strap (54).
(10)
Install the washer (55) and the bolt (56).
(11)
TORQUE the bolt (56) to between 0.904 and 1.808 m.daN (79.99 and
159.99 lbf.in).
(12)
Safety the bolts (53) and (56) with MISCELLANEOUS (Material No. 19-010).
(13) Apply SEALANTS (Material No. 09-016) to the heads of the bolts (53) and (56). Subtask 32-12-00-020-064 R E. Removal of the Secondary Hinged Fairing and Attaching Parts
(Ref. Fig. 404/TASK 32-12-00-991-010)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架3(7)
