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时间:2011-03-29 20:46来源:蓝天飞行翻译 作者:航空
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505 May 01/99 Contents 5 Page 1 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.

Subject Subject No.
High Energy Stop/Heat Damage Condition ............................................................. 5-51-111 Conditional Inspection
Mercury Spillage Condition...................................................................................... 5-51-121 Conditional Inspection
Hydraulic Fluid Reaction with Titanium.................................................................... 5-51-131 Conditional Inspection
Overpressurization................................................................................................... 5-51-141 Conditional Inspection
Lightning Strike ........................................................................................................ 5-51-151 Conditional Inspection
Hot Air Duct Rupture Condition................................................................................ 5-51-171 Conditional Inspection
Excessive Aileron or Rudder Trim with Flaps Extended.......................................... 5-51-191 Conditional Inspection
Bird/Hail Strike Condition ......................................................................................... 5-51-201 Conditional Inspection
Nacelle Pressure Relief Doors Open Condition....................................................... 5-51-211 Conditional Inspection
Landing Gear Down Overspeed Condition.............................................................. 5-51-231 Conditional Inspection
Tire Tread Loss or Tire Burst................................................................................... 5-51-251 Conditional Inspection
Volcanic Ash Condition ............................................................................................ 5-51-261 Conditional Inspection
Dragged Tail Condition ............................................................................................ 5-51-271 Conditional Inspection
Airframe Vibration Condition.................................................................................... 5-51-281 Conditional Inspection
Overweight Landing Condition................................................................................. 5-51-291 Conditional Inspection
506 
Contents 5 Page 2  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Sep 01/02 


CONDITIONAL INSPECTIONS - GENERAL
1.  General
A.  This section contains the recommended checks and inspections which are dictated by special or unusual conditions. The following subjects identify the conditions and list the recommended checks and inspections. Procedures required for accomplishing specific checks or inspections are covered in the individual system or component subjects in the appropriate chapters of the manual.
500 
May 15/67  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  5-51-0 Page 201 


OVERWEIGHT TAXI CONDITION - MAINTENANCE PRACTICES (CONDITIONAL INSPECTION)
1.  General Overweight Taxi: Taxiing at a weight that is more than the maximum-design-taxi-weight (MTW). Before flight, you must decrease airplane weight to that specified by the Airplane Flight Manual for takeoff.
A.  Inspection Criteria; An immediate structural inspection is necessary if you:
(1)  
taxi the airplane overweight by more than 1/2% of the maximum-taxi-weight (MTW).

(2)  
taxi the airplane overweight any weight over the Maximum Design Taxi Weight (MTW) and have any of these conditions:

(a)  
High speed ground turn

(b)  
Sharp radius turn

(c) 
 Heavy braking

(d)  
Taxi over rough pavement

(e)  
Pivoting (sharp radius turning with brakes on)

 


B.  The Inspections
(1)  
The inspection is divided into Phase 1 and 2.

(2)  
If the inspection for Phase 1 shows no signs of damage, the inspection is complete. If the Phase 1 inspection shows any sign of damage, the Phase 2 inspection must be done.

(3)  
If the criteria for the above paragraphs 1.B.(1) or 1.B.(2) have not been met, no inspection is required, but you must decrease airplane weight to that specified by the Airplane Flight Manual before takeoff.


C.  Inspections, Repairs, and Replacements
(1)  
When this procedure tells you to "examine" a part, look for these conditions:

–  
cracks

–  
structure that pulled apart

–  
loose paint (paint flakes)

–  
twisted parts (distortion)

–  
bent parts

–  
wrinkles or buckles in structure
 
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