(2)  
Hail strike on the ground conditional inspection.

 C.  For allowable hail damage, refer to the aerodynamic smoothness and investigation and cleanup of damage (SRM 51-10-00).
 TASK 05-51-37-212-001
 2.  Bird/Hail Strike Conditional Inspection_______________________________________
 A.  References
 (1)  
27-51-00/201, Trailing Edge Flap System

 (2)  
27-81-00/201, Leading Edge Flap System

 (3)  
71-00-47/101, Power Plant - Trouble Shooting

 B.  Bird/Hail Strike Conditional Inspection
 S 862-002
 WARNING: DO THE DEACTIVATION PROCEDURE FOR THE FLAP/SLAT ACTUATION
_______ SYSTEMS. INJURY TO A PERSON OR DAMAGE TO EQUIPMENT CAN OCCUR IF THE FLAPS/SLATS MOVE. FLAP/SLAT ACTUATION SYSTEMS MUST NOT BE OPERATED DURING THIS INSPECTION. FAILURE TO OBEY CAN CAUSE INJURY TO PERSONS.
 (1)  Extend the leading edge flap and slat system and the trailing edge flap system in the full extend position.
 (a)  
Do the deactivation procedure for the leading edge flap and slat system (AMM 27-81-00/201).

 (b)  
Do the deactivation procedure for the trailing edge flap system (AMM 27-51-00/201).

 S 212-004
 (2)  Do the examinations that follow:
 (a)  Examine the wing, nacelle strut, and the horizontal and vertical stabilizer leading edge fairing. Look for displacement, distortion, fastener hole elongation or tearout, and paint that has flaked. Also look for skin cracks, and fasteners that have pulled out or are not there.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 05-51-37
 ALL  ú ú 02 Page 201 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (b)  
Examine the strut panels, doors, and structure for buckling, cracks, and fasteners that have pulled out or are not there.

 (c)  
Examine the wing leading and trailing edge structure, panels, and doors. Look for displacement, distortion, paint that has flaked, cracks, and fasteners that have pulled out or are not there. Also examine the two sides of the honeycomb panels for cracks, delamination, soft spots and core damage.

 (d)  
Examine the leading edge slat mechanism and track fairing links. Look for distortion, cracks, misalignment, or other signs of distress.

 (e)  
Examine the trailing edge flap mechanism and track fairing links. Look for distortion, cracks, misalignment, or other signs of distress.

 (f)  
Examine the control surfaces. Look for binding, too much play, misalignment, distortion, or displacement of skins. Also look for fasteners that have pulled out or are missing.

 (g)  
Examine the nose landing gear doors and linkage. Look for distortion, cracks, and other signs of distress.

 (h)  
Examine the main landing gear doors and linkage. Look for distortion, cracks, and other signs of distress.

 (i)  
Examine the pilots' windows for delamination, spalling, or cracks. Also examine the adjacent structure for distortion, cracks, and fasteners that have pulled out or are not there.

 (j)  
Examine the forward-body nose section "eyebrow" area above the windows and radome. Look for cracks, distortion, delamination, misalignment, and displacement of the skins. Also look for fasteners that have pulled out or are not there.

 (k)  
Examine the internal and external areas of the radome. Look for honeycomb damage and for soft spots.

 S 212-005
 (3)  Examine the nose cowl and the engine for foreign object damage (Ref 71-00-47/101).
 TASK 05-51-37-212-007
 3.  Hail Strike on the Ground Conditional Inspection________________________________________________
 A. References
 (1)  27-51-00/201, Trailing Edge Flap System
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 05-51-37
 ALL  ú ú 02 Page 202 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊 TIME LIMITS/MAINTENANCE CHE(42)