05-51-54
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (5)  S 212-019Examine the landing gear assemblies, related components and hydraulic lines for damage and/or hydraulic fluid leakage.
 (6)  S 212-020Examine the wheel well doors and wheel well door actuating rods for damage and/or blockage from pieces of the tire.
 (7)  S 212-021Examine the other tires for possible damage (AMM 32-45-00/601).
 NOTE:____ Carefully inspect the other tires for slash and/or wire penetration damage of the tread or the sidewall.
 (8)  S 212-022Examine the engine nacelles and inlets (Ref Chapter 72) for damage when the nose gear tire tread is lost or the nose gear tire burst.

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 05-51-54
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 FLAT SPOTTED TIRES - MAINTENANCE PRACTICES (CONDITIONAL INSPECTION)
___________________________________________________________________
 1.  General_______
 A.  Examine the wheel and brake components and systmes after tires become flat spotted. The tires are damaged when a locked wheel slides (not a tire structural failure) and the cause is not apparent. Examine in the sequence in this section.
 B.  The examinations are divided into two phases. Phase I examinations are for conditions where only one tire is flat spotted. Phase II examinations are for conditions where more than one tire is flat spotted.
 TASK 05-51-55-212-001
 2.  Flat Spotted Tires Conditional Inspection_________________________________________
 A.  References
 (1)  
AMM 29-15-61/201, Hydraulic Return Filter

 (2)  
AMM 32-41-41/601, Main Gear Wheel Brakes

 (3)  
AMM 32-42-00/501, Antiskid/Autobrake System

 (4)  
AMM 32-44-00/501, Parking Brake System

 (5)  
AMM 32-45-00/601, Wheels

 B.  Phase I One Flat Spotted Tire Examinations
 S 712-002
 (1)  
Make sure the brake will operate correctly and is in a serviceable condition (AMM 32-41-41).

 S 212-003

 (2)  
Examine the wheel for cracks or loose wheel bearings (AMM 32-45-00).

 S 712-004

 (3)  
Make sure the brake releases correctly (AMM 32-42-00).

 S 212-005

 (4)  
Make sure the routing of the hydraulic lines and the wiring runs are correct.

 S 712-006

 (5)  
Do the transducer spin test and make sure that the correct brake releases when the transducer motion stops (AMM 32-42-00).

 C.  Phase II More Than One Flat Spotted Tire Examinations
 S 712-007
 (1)  
Make sure the brakes will operate correctly and are in a serviceable condition (AMM 32-41-41).

 (2)  
Make sure the brakes release correctly (AMM 32-42-00).

 S 712-008
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (3)  S 212-009Make sure that the hydraulic return filter is not blocked (Ref 29-15-61).
 (4)  S 212-010Make sure the routing of the hydraulic lines and the wiring runs are correct.
 (5)  S 712-011Do the transducer spin test and make sure that the correct brake releases when the transducer motion stops (AMM 32-42-00).
 (6)  S 712-012Make sure the parking brake valve operates correctly (AMM 32-44-00).
 (7)  S 212-014Also make sure that the valve is fully open when the parking brake releases (AMM 32-44-00).
 (8)  S 742-013Do a BITE test for the Antiskid/Autobrake system and also make sure the system has continuity (AMM 32-42-00).

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