R Position)
R Figure 401/TASK 78-30-00-991-300- 22 (SHEET 2)
F EEFF : ALL 『E 78-30-00 Page 405
E E May 01/03
E E
ECES E
F 『 E C F M E E E E 56-5B E F 『 E C F M E E E E 56-5B E
Lockout Fairing and Storage Bracket Figure 402/TASK 78-30-00-991-302
F EEFF : E ER ECES ALL 『E 78-30-00EE E Page 406 May 01/03
Lockout Bolt and Lockplate
Figure 403/TASK 78-30-00-991-303
F 『 EEFF : ALL E Page 40778-30-00
E E May 01/03 ERE
ECES E F 『 E C F M E E E E 56-5B E E E
1 If the following message is present, replace the four deploy
_ switches (Ref. TASK 78-31-17-000-001) and (Ref. TASK 78-31-17-400-001) and do the test again:
- "DEPL SW, J5/J6,ECU"
2 If the following message is present, replace the four stow
_ switches (Ref. TASK 78-31-18-000-001) and (Ref. TASK 78-31-18-400-001) and do the test again:
- "STOW SW, J5/J6,ECU"
3 If the following message is present, replace the four deploy
_ switches (Ref. TASK 78-31-17-000-001), (Ref. TASK 78-31-17-400-001) and the four stow switches (Ref. TASK 78-31-18-000-001), (Ref. TASK 78-31-18-000-001) and do the test again:
- "DPLSTW SW,J5/6,ECU"
4 If the ECAM warning ENG 1(2) REV PRESSURIZED appears together
_ with one of the following messages, troubleshoot per (Ref. TSM 78 PB101)
- "HCU(TRPV OPEN)" or "HCU(TRPV), HYD"
5 If the message "HCU (TRPV), HYD" or "HCU, TRSOV, HYD" is
_ present and if there is no other message above mentioned, continue the deactivation procedure.
NOTE : The maintenance messages linked to the fault(s)
____ occurred before the deactivation, can be recorded in this T/R test report.
(4) Deactivation of the thrust reverser. (Ref. Fig. 402/TASK 78-30-00-991-302, 403/TASK 78-30-00-991-303)
(a) Remove the bolts (3) that attach the lockplates (2) to the storage bracket (4).
(b) Remove the lockplates (2) from the storage bracket (4).
(c) Remove the lockout bolts (1) from the storage bracket (4).
(d) Remove the screws (5) that attach the lockout fairings (6) to the blocker doors.
(e) Attach the lockout fairings (6) to the storage bracket (4) with the screws (5).
(f) TORQUE screws (5) to between 0.16 and 0.19 m.daN (14.15 and 16.81 lbf.in)
F 『R EEFF : 001-049, 056-056, 058-058, 061-099, E Page 40878-30-00
E E101-105, 151-199, 201-211, May 01/05 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
(g) Install the lockout bolts (1) on the blocker doors. (Ref. Fig. 403/TASK 78-30-00-991-303)
(h) TORQUE the lockout bolts (1) to between 0.65 and 0.70 m.daN
(57.52 and 61.94 lbf.in).
(5) Put the lockplates (2) over the lockout bolts (1) and install the bolts (3).
(6) TORQUE the bolts (3) to between 0.33 and 0.45 m.daN (29.20 and 39.82 lbf.in).
R **ON A/C 051-055, 057-057, 059-060, 106-149, 212-299, 301-399, 401-499,
Subtask 78-30-00-040-050-A
A. Thrust Reverser Deactivation.
WARNING : MAKE SURE THAT THE THRUST REVERSER IS LOCKED. IF NOT, THE
_______ THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE INJURY TO PERSONNEL AND/OR DAMAGE TO THE REVERSER.
(1) Do a check of the primary lock, as follows:
(a) Make sure the blocker doors are closed and flush with the thrust reverser structure.
(b) Pull the blocker door with your hand to make sure the door cannot open.
(2) Make the Thrust Reverser Unserviceable.
(Ref. Fig. 401/TASK 78-30-00-991-300)
(a) Remove the quick-release pin from the operational position on the HCU (see sheet.1).
(b) Move the inhibit lever from the operational position to the OFF position.
(c) Install the quick-release pin to hold the inhibit lever in the OFF position (see sheet.2).
F 『 EEFF : ALL E Page 40978-30-00
E E Aug 01/05 E E ECES E
F 『
E C F M E
E E
E 56-5B E
E E
(3) Do a test of the deploy switches and make sure that they are operative.
(a) Do an operational test of the thrust reverser system through the CFDS (Ref. TASK 78-31-00-710-042) and when the throttle control lever is in the reverse position:
- check that the green or amber REV indication in the N1 indicator of the engine 1(2) does not appears
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EXHAUST 1(29)
