曝光臺 注意防騙
網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者
54-51-17-000-002 Removal of the Pylon-to-Wing Aft Attach Fitting at
RIB10
54-51-17-200-001 Inspection of the Pylon-to-Wing Forward
Attach-Fitting
54-51-17-200-002 Inspection of the Pylon-to-Wing Aft Attach-Fitting
54-51-17-400-001 Installation of Pylon-to-Wing Forward Attach Fitting
at RIB4
54-51-17-400-002 Installation of the Pylon-to-Wing Aft Attach Fitting
at RIB10
55-10-00-210-001 Detailed Inspection of Horizontal Stabilizer Internal
Structure of Torque Box Inboard of Fuselage Fairings
55-16-00-200-001 Detailed Inspection of Horizontal Stabilizer Rear
Support Fittings, Upper and Lower Attach Fittings and
Surrounding External Structure, LH/RH
55-30-00-200-001 Detailed Visual Inspection of Vertical Stabilizer
Center Box Internal Structure as far as Visible,
Front Spar FWD Face Upper Closing Rib Upper Surface
55-36-00-210-001 Detailed Visual Inspection of the Vertical Stabilizer
Attach Fittings Including the Load Introduction Area
at the Skin Panels
57-51-33-000-001 Removal of the No.1 Flap Track Beam
57-51-33-000-002 Removal of the No.2 Flap Track Beam
57-51-33-000-003 Removal of the No.3 Flap Track Beam
57-51-33-000-004 Removal of the No.4 Flap Track Beam
57-51-33-400-001 Installation of the No.1 Flap Track Beam
57-51-33-400-002 Installation of the No.2 Flap Track Beam
57-51-33-400-003 Installation of the No.3 Flap Track Beam
57-51-33-400-004 Installation of the No.4 Flap Track Beam
57-55-11-000-001 Removal of the Flap Track Fairings Nos. 2, 3 and 4
57-55-11-400-001 Installation of the Flap Track Fairings Nos. 2, 3 and
4
71-00-00-000-042 Removal of the Power Plant
71-00-00-400-042 Installation of the Power Plant
71-00-00-710-008 Power Assurance Check
71-13-00-010-040 Opening of the Fan Cowl Doors
71-13-00-410-040 Closing of the Fan Cowl Doors
72-00-00-200-008 Inspection/Check After the Engine has Exceeded the
Operational Limits
78-31-00-710-042 Operational Test of the Thrust Reverser System
78-36-00-010-040 Opening of the Thrust Reverser Doors
78-36-00-410-040 Closing of the Thrust Reverser Doors
R 1EFF : 001-003, 051-054, 1 05-51-11Page 603 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
79-00-00-281-002 Check of the Electrical Master Chip Detector for
Particles 05-51-11-991-004 Fig. 601 05-51-11-991-005 Fig. 602 05-51-11-991-007 Fig. 603 05-51-11-991-008 Fig. 604 05-51-11-991-009 Fig. 605 05-51-11-991-010 Fig. 606 05-51-11-991-011 Fig. 607 05-51-11-991-012 Fig. 608 05-51-11-991-013 Fig. 609 05-51-11-991-014 Fig. 610
3. Job Set-up
__________
Subtask 05-51-11-941-050
A. Inspection Preparation
(1)
We can not give you accurate details of the inspection procedure to be applied after each incident. This is because there can be important variations in the weight, the speed and the direction of the loads. Thus, before you start, we recommend that you get information:
(a)
From the crew about the landing conditions. For example, find out:
-
if the landing was straight, drifting, wing-low, tail or nose heavy.
-
if the crew heard a noise possibly related to a structural failure.
(b)
From the flight recorder (DFDR):
-vertical acceleration, vertical speed (V/S), weight of the aircraft.
(2)
With these pieces of information refer to the inspection definition diagram. (Ref. Fig. 601/TASK 05-51-11-991-004)
R 1EFF : 001-003, 051-054, 1 05-51-11Page 604 1 1 May 01/05 1 1 1CES 1
Inspection - Definition Diagram
Figure 601/TASK 05-51-11-991-004
1EFF : ALL 1 05-51-11 Page 605
1 1 Feb 01/98
1 1
1CES 1
Subtask 05-51-11-481-050
B. Safety precautions
(1)
Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-001).
(2)
Put a warning notice in the cockpit to tell persons not to operate the aircraft systems.
Subtask 05-51-11-866-050
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM 時間限制/維護檢查 3(101)
