(b)
Examine the wheels of the main landing gear for cracks.
(c)
Examine the upper and lower ends of the shock strut for the main landing gear for signs of hydraulic fluid leakage.
NOTE: A small quantity of hydraulic fluid on the inner
____
cylinder is satisfactory.
(d)
Examine the doors and linkage of the strut doors of the main landing gear for distortion, cracks, or other signs of damage.
(e)
Examine the trunnion link for the main gear and the upper end of the shock strut for cracks.
(f)
Examine the landing gear beam and attachment fittings for cracks and loose or missing fasteners.
(g)
Examine the attach nut for the orifice support tube on the main gear for fluid leakage.
S 212-004
(2) Examine the areas of the nose landing gear as follows:
(a)
Examine the nose wheel well for buckling, and paint that is flaked.
(b)
Look for fasteners that have pulled out, or that are not in the web of the nose wheel well.
NOTE: Look carefully in the area near the trunnion and the
____ support fittings of the drag strut.
(c)
Examine the tires of the nose landing gear for damage.
(d)
Examine the wheels of the nose landing gear for cracks.
(e)
Examine the upper and lower ends of the shock strut for the nose landing gear for signs of hydraulic fluid leakage.
NOTE: A small quantity of hydraulic fluid on the inner
____
cylinder is satisfactory.
(f)
Examine the outer cylinder of the nose landing gear for distortion, cracks, or paint that has flaked.
(g)
Examine the attach nut for the orifice support tube on the nose gear for fluid leakage.
(h)
Examine the doors, the hinges, and the retraction mechanism for damage, distortion, buckles, and pulled or missing fasteners.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
05-51-74
ALL ú ú 01 Page 202 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 212-005
(3) Examine the Fuselage and Wing areas as follows:
(a)
Examine the engine strut panels, doors, and structure. Look for buckling, cracks, and for fasteners that are pulled out, or are not there.
(b)
Examine the leading edge wing-to-body fairing for movement from its usual position. Look for fastener hole elongation or tear out, and cracks in the skin. Also look for fasteners that are pulled out, or are not there.
(c)
Look at the inboard trailing edge flaps for damage.
(d)
Examine the top and lower fuselage skin panels forward and aft of the wing for buckles, wrinkles or tears.
NOTE: Permanent wrinkles often occur on the lower side
____ fuselage skins aft of STA 727. An interior inspection is necessary if you find these wrinkles and they did not exist before the landing. If they did exist, examine the wrinkles carefully for cracks.
(e)
Examine the keel beam chords, stiffeners, webs, and splices at STA 663 through 727A for distortion, buckled or damaged panels, and pulled or missing fasteners.
(f)
Examine the strut-to-wing fairing panels for the top and lower nacelle for buckling, cracks, and pulled or missing fasteners.
(g)
Examine the wing leading edge-fairing for displacement, fastener hole elongation or tear-out, skin cracks, and pulled or missing fasteners.
TASK 05-51-74-212-006
3. Phase II Examination____________________
A. References
(1)
AMM 05-51-61/201, Dragged Engine Nacelle/Engine Seizure
(2)
AMM 07-11-11/201, Jacking Airplane
(3)
AMM 27-00-00, Flight Controls
(4)
AMM 32-00-00, Landing Gear
(5)
AMM 32-11-00, Main Landing Gear
(6)
AMM 32-21-00, Nose Landing Gear
(7)
AMM 32-32-00/501, Main Landing Gear Extension and Retraction
(8)
AMM 32-33-00/501, Nose Landing Gear Extension and Retraction
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