(b)
Examine the trailing edge flaps on the inboard side.
(c)
Look for fuel leaks, and other fluid leaks, in the areas that follow: 1) The wing 2) The nacelles 3) The nacelle-struts.
S 212-036
(6) Engine Nacelle Inspection
(a) Examine the doors, panels, and the structure on the nacelle strut.
TASK 05-51-35-212-037
3. Phase 2 Inspection
__________________
A. References
(1)
AMM 05-51-10/201, Dragged Engine Nacelle/Engine Seizure/Engine and Strut Damage Condition
(2)
AMM 07-11-01/201, Jacking Airplane
(3)
AMM 12-15-01/301, Main Gear Shock Strut - Servicing
(4)
AMM 12-15-02/301, Nose Gear Shock Strut - Servicing
(5)
AMM 27-00-01/201, Flight Controls
(6)
AMM 32-11-01/401, Main Gear
(7)
AMM 32-21-01/401, Nose Gear
(8)
AMM 32-32-00/501, Main Landing Gear Extension and Retraction
(9)
AMM 32-34-00/501, Nose Landing Gear Extension and Retraction
(10)
AMM 32-51-00/501, Nose Wheel Steering System
B. Airplane Inspection
S 022-038
(1) Main Landing Gear and Support Structure Inspection
(a)
Make sure the shock strut pressures are normal and the hydraulic fluids are at the correct levels (AMM 12-15-01/301).
(b)
Lift the airplane with jacks (AMM 07-11-01/201).
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05-51-35
ALL ú ú 01.1 Page 204 ú Sep 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
WARNING:_______ MAKE SURE YOU SUFFICIENTLY HOLD THE LANDING GEAR AND THE
SUPPORT STRUCTURE WHEN YOU REMOVE THE FUSE PINS. IF YOU
DO NOT SUFFICIENTLY HOLD THESE COMPONENTS, YOU CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
WARNING:_______ DO NOT REMOVE MORE THAN ONE FUSE PIN AT A TIME. INSTALL
THE FUSE PIN IMMEDIATELY AFTER YOU EXAMINE IT. IF THE
FUSE PIN HAS DAMAGE, REPLACE IT WITH A NEW FUSE PIN. IF
YOU REMOVE MORE THAN ONE FUSE PIN AT A TIME THE LANDING
GEAR MAY FALL AWAY FROM THE AIRPLANE. THIS CAN CAUSE
INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(c) Remove and examine the fuse pins from the main landing gear as follows (AMM 32-11-01/401): 1) The fuse pin (Fig. 201, sheet 2, item 1) that connects the
drag strut to the trunnion link.
2) The fuse pin (Fig. 201, sheet 2, item 2) that connects the trunnion link to the forward trunnion bearing.
3) The upper two fuse pins (Fig. 201, sheet 2, item 3) on the forward trunnion fitting. If damage is found, remove and examine the lower two fuse pins.
CAUTION: INSTALL THE GROUND LOCK PIN BEFORE YOU REMOVE THE
_______ FUSE PIN.
4) The fuse pin (Fig. 201, sheet 3, item 4) that connects the upper downlock link to the downlock spindle.
5) The fuse pin (Fig. 201, sheet 4, item 5) that connects the reaction link to the forward trunnion fitting.
6) The forward two fuse pins (Fig. 201, sheet 5, item 6) on the aft trunnion fitting. IF damage is found, remove and examine the aft two fuse pins.
7) The forward and aft fuse pins (Fig. 202, sheet 2, item 7) of the inboard stabilizing link.
8) The forward and aft fuse pins (Fig. 202, sheet 3, item 8) of the outboard stabilizing link.
9) The fuse pin (Fig. 202, sheet 4, item 9) that connects the landing gear beam to the support fitting on the wing rear spar.
NOTE: You must sufficiently lift the outboard wing to
____ easily remove the fuse pin. Make sure you safely hold the landing gear.
10) The pin (not a fuse pin)(Fig. 202, sheet 4, item 10) that connects the inboard end of the landing gear beam to the support fitting.
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