5-CONTENTS

 ú ú BEJ.101 Page 3 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 
737-300/400/500MAINTENANCE MANUAL
 CONDITIONAL INSPECTIONS - MAINTENANCE PRACTICES_______________________________________________
 TASK 05-51-00-282-001
 1.  Conditional Inspections_______________________
 A. General
 (1) This table contains recommended checks and inspections. The
 conditional inspections covered are listed below:
 ú  ~.................................................................
 ú  | TABLE 1 |
 ú  ...................................................................
 ú  | TITLE | CHAPTER/SEC/SUB/PAGE |
 ú  ...................................................................
 |Brake Seizure | AMM 05-51-04/201 |
 ú  ...................................................................
 |High Energy Stop/Heat Damage | AMM 05-51-07/201 |
 ú  ...................................................................
 |Ice or Snow | AMM 05-51-11/201 |
 ú  ...................................................................
 |Mercury Spillage | AMM 05-51-14/201 |
 ú  ...................................................................
 |Hydraulic Fluid Reaction With | AMM 05-51-17/201 |
 ú  |Titanium | |
 ú  ...................................................................
 |Extreme Dust | AMM 05-51-21/201 |
 ú  ...................................................................
 |Cabin Overpressurization | AMM 05-51-24/201 |
 ú  ...................................................................
 |Lightning Strike | AMM 05-51-27/201 |
 ú  ...................................................................
 |Exceeding Design Speed, Severe | AMM 05-51-31/201 |
 |Turbulance or Buffeting | |
 ú  ...................................................................
 |Hot Air Duct Rupture | AMM 05-51-34/201 |
 ú  ...................................................................
 |Bird Strike | AMM 05-51-37/201 |
 ú  ...................................................................
 |Exceeding Flap Down Speeds | AMM 05-51-41/201 |
 ú  ...................................................................
 |Nacelle/Strut Pressure Relief | AMM 05-51-44/201 |
 |Doors Open | |
 ú  ...................................................................
 |Landing Gear Down Overspeed | AMM 05-51-47/201 |
 ú  ...................................................................
 |Hard Landing or High Drag/Side | AMM 05-51-51/201 |
 |Load | |
 ú  ...................................................................
 |Tire Tread Loss or Tire Burst | AMM 05-51-54/201 |
 ú  ...................................................................
 |Flat Spotted Tires | AMM 05-51-55/201 |

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 05-51-00
 ALL  ú ú 01.1 Page 201 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 ú ~................................................................. ú | TABLE 1 | ú ................................................................... ú | TITLE | CHAPTER/SEC/SUB/PAGE | ú ................................................................... |Volcanic Ash | AMM 05-51-57/201 | ú ................................................................... |Dragged Engine Nacelle/Engine | AMM 05-51-61/201 | |Seizure/Thrust Reverser and | | |Attach Point | | ú ................................................................... |Tail Drag | AMM 05-51-64/201 | ú ................................................................... |Airframe Vibration Condition | AMM 05-51-67/201 | ú ................................................................... |Overweight Landing | AMM 05-51-74/201 | ú ................................................................... ú |Excessive Aileron or Rudder Trim | AMM 05-51-75/201 | ú |Correction with Flaps Extended | | ú ................................................................... |Cabin Depressurization Condition | AMM 05-51-81/201 | ú ................................................................... |Excess Cabin Pressure Leakage | AMM 05-51-91/201 | 2..........................................…......................1
　
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