Flap System Shaft Overspeed.
1. Possible Causes
_______________
- ACTUATOR ASSY (6205CM)
- ACTUATOR ASSY (6211CM)
- ACTUATOR ASSY (6221CM)
- ACTUATOR ASSY (6233CM)
- ACTUATOR ASSY (6255CM)
- ACTUATOR ASSY (6261CM)
- ACTUATOR ASSY (6271CM)
- ACTUATOR ASSY (6283CM)
- BRAKE-L WING TIP (33CV)
- BRAKE-R WING TIP (34CV)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific Titanine JC5A
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-50-00-866-008 Extension of the Flaps on the Ground AMM 27-50-00-866-009 Retraction of the Flaps on the Ground AMM 27-50-00-869-006 Reset of the Wing Tip Brake (WTB) of the Flap System
on the Ground
AMM 27-51-51-000-001 Removal of the Flap Wing-Tip Brake
AMM 27-51-51-400-001 Installation of the Flap Wing-Tip Brake
AMM 27-54-00-200-001 Detailed Visual Inspection of the Transmission
Assembly (Including Part of the Transmission in Zone 140) AMM 27-54-49-000-001 Removal of the Flap Track 1 Actuator 6205CM(6255CM)
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 287
May 01/05 CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-54-49-000-002 Removal of the Flap Track 2 Actuator 6211CM(6261CM) AMM 27-54-49-000-003 Removal of the Flap Track 3 Actuator 6221CM(6271CM) AMM 27-54-49-000-004 Removal of the Flap Track 4 Actuator 6233CM(6283CM) AMM 27-54-49-400-001 Installation of the Flap Track 1 Actuator
6205CM(6255CM) AMM 27-54-49-400-002 Installation of the Flap Track 2 Actuator 6211CM(6261CM) AMM 27-54-49-400-003 Installation of the Flap Track 3 Actuator 6221CM(6271CM) AMM 27-54-49-400-004 Installation of the Flap Track 4 Actuator
6233CM(6283CM) 27-51-00-991-001 Fig. 201
3. Fault Confirmation
__________________
A. For the fault confirmation do the fault isolation.
4. Fault Isolation
_______________
A. Procedure
(1) Do the wing tip brake (WTB) reset procedure (Ref. AMM TASK 27-50-00-869-006).
(2) Do the inspection/check of the flap system (Ref. AMM TASK 27-54-00-200-001). Repair or correct any defect found.
(3) While the flaps are extended examine the flap actuator assemblies on the identified wing:
- For the LH wing ACTUATOR ASSY (6205CM) ACTUATOR ASSY (6211CM) ACTUATOR ASSY (6221CM) and ACTUATOR ASSY (6233CM)
- For the RH wing ACTUATOR ASSY (6255CM) ACTUATOR ASSY (6261CM) ACTUATOR ASSY (6271CM) and ACTUATOR ASSY (6283CM). (Ref. Fig. 201/TASK 27-51-00-991-001)
(a) Remove the inspection plugs (1) and (2) on each actuator, clear the grease in the inspection holes and examine for water.
(b) Install the inspection plugs (1) and (2) into the actuators:
- seal the inspection plugs with Titanine JC5A
- torque the inspection plugs (1) to between 0.36 and 0.44 m.daN
(31.85 and 38.93 lbf.in)
- torque the inspection plugs (2) to between 0.54 and 0.66 m.daN
(47.78 and 58.40 lbf.in).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 288
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 2(10)
