(2)
Close the access doors and panels opened during the inspection.
(3)
Close the nose gear doors (Ref. TASK 32-22-00-410-001).
(4)
Close the main gear doors (Ref. TASK 32-12-00-410-001).
(5)
Remove the access platform(s).
(6)
Remove the warning notice(s).
R 1EFF : ALL 1 05-51-11Page 673 1 1 Nov 01/01 1 1 1CES 1 INSPECTION AFTER LANDING GEAR DOWN LIMITING SPEED EXCEEDED - INSPECTION/CHECK
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TASK 05-51-12-200-001
Inspection after Landing Gear Extension at more than the Geardown Limiting Speed
1. Reason for the Job
__________________
You must do this inspection if:
-
the landing gear extends/retracts, while the aircraft speed is more than the limit speed (VLO),
-
the aircraft speed increases to more than the limit speed (VLE), while the landing gear is downlocked.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION
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No specific warning notice
No specific access platform 3 m (9 ft. 10 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
05-56-00-200-001 Inspection/Check of the Leveling and Measurement
after Abnormal Operation of the Aircraft 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power 27-50-00-866-008 Extension of the Flaps on the Ground 27-50-00-866-009 Retraction of the Flaps on the Ground 27-54-00-710-001 Operational Test of the Flap System 27-64-00-710-001 Operational Test of the Spoiler Hydraulic Actuation 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized
Configuration before Maintenance Action 32-00-00-481-001 Installation of the Safety Devices on the Landing
Gears 32-11-00-200-001 Inspection/Check of the Main Gear 32-12-00-010-001 Open the Main Gear Doors for Access
1EFF : ALL 1 05-51-12Page 601 1 1 Nov 01/00R 1 1 1CES 1
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REFERENCE DESIGNATION -------------------------------------------------------------------------------
32-12-00-410-001 Close the Main Gear Doors after Access 32-12-00-710-002 Operational Test of the Main Landing Gear (MLG) Doors Ground-Opening-Mechanism
R 32-21-00-200-002 General Visual Inspection of the Nose Landing Gear 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 32-22-11-000-001 Removal of the Main Door Assy 32-22-11-400-001 Installation of the Main Door Assy 32-22-13-000-001 Removal of the Aft Door Assy 32-22-13-400-001 Installation of the Aft Door Assy 32-22-15-000-001 Removal of the Leg Door Assy 32-22-15-400-001 Installation of the Leg Door Assy 32-31-00-720-002 Functional Test of the Normal Extension and
Retraction of the Landing Gear 32-31-16-000-001 Removal of the NLG Door Actuating Cylinder (2531GM) 32-31-16-400-001 Installation of the NLG Door Actuating Cylinder
(2531GM)
32-69-00-740-001 BITE Test of the Landing Gear
57-27-11-400-001 Installation of the Access Panel (540AB, 540BB,
540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)
57-27-11-400-002 Installation of the Access Panel (540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, ....)
05-51-12-991-001 Fig. 601
05-51-12-991-002 Fig. 602
05-51-12-991-003 Fig. 603
05-51-12-991-004 Fig. 604
05-51-12-991-005 Fig. 605
05-51-12-991-006 Fig. 606
3. Job Set-up
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Subtask 05-51-12-860-050
A. Aircraft Maintenance Configuration
(1)
Make sure that the hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001)
(2)
Make sure that the electrical circuits are de-energized (Ref. TASK 24-41-00-862-002).
Subtask 05-51-12-481-050
