S 722-014
(4) Make sure the flight controls move freely.
(a) If you find unusual conditions, do a check of the flight control force specifications. Also check the cable tensions. If necessary, refer to the applicable Chapter 27 sections that follow: 1) AMM 27-11-00/001, Aileron and Aileron Trim Control System 2) AMM 27-21-00/001, Rudder and Rudder Trim Control System 3) AMM 27-31-00/001, Elevator and Tab Control System 4) AMM 27-51-00/201, Trailing Edge Flap System 5) AMM 27-61-00/001, Spoiler Control System 6) AMM 27-81-00/201, Leading Edge Flap and Slat Control System
TASK 05-51-31-212-021
4. Cabin Payload Inspections__________________________
A. Procedure
S 212-022
(1) Phase I Inspection
(a)
Do a visual inspection of all ceiling panels for dislodging and evidence of impact damage.
(b)
Do a visual inspection of all ceiling overhead bins for evidence of looseness and impact damage.
(c)
Do a detailed visual inspection of all ceiling panels equipped with video monitors. 1) Inspect latches, stops, potting inserts and all fasteners.
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737-300/400/500MAINTENANCE MANUAL
(d)
If the Cabin Payloads Phase I inspections did not find any damage, no further cabin payload action/inspection is required.
(e)
If any of the above Cabin Payloads Phase I inspections conditions were found, refer to the Cabin Payloads Phase II inspections for affected and adjacent zones.
S 212-023
(2) Phase II Inspection:
(a)
Check for proper latching and installation of ceiling panels and stowage bins.
(b)
Examine lavatory, galley and closet tie rod attachments for damage consisting of breakage, cracks, and deformation. 1) Inspect the tie rods for evidence of buckling or rupture.
(c)
Examine lavatory, galley and closet floor fittings for damage consisting of breakage, cracks, and deformation.
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HOT AIR DUCT RUPTURE CONDITION - MAINTENANCE PRACTICES
______________________________________________________ (CONDITIONAL INSPECTION)
________________________
1. General_______
A. One task is supplied in this procedure. The task is hot air duct rupture conditional inspection.
B. This task examines the airplane structure for possible heat damage caused by a ruptured duct.
TASK 05-51-34-202-001
2. Hot Air Duct Rupture Conditional Inspection___________________________________________
A. References
(1) 51-00-00, Part 6, Nondestructive Test Manual
B. Procedure
S 282-002
(1) Examine any airplane structure which has gone through a high heat condition caused by a ruptured pneumatic duct. Make sure the structure has not been damaged (Ref 51-00-00, Part 6, Nondestructive Test Manual).
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BIRD/HAIL STRIKE CONDITION - MAINTENANCE PRACTICES
__________________________________________________ (CONDITIONAL INSPECTION)
________________________
1. General_______
A. The examinations that follow are for a bird strike and a hail strike condition. Examine the external surfaces of the airplane structure in the general area of the bird/hail strike. If the initial examination shows structural damage, then the internal structure must be inspected. Also inspect the hydraulic, pneumatic, and other systems in the area of the bird/hail strike for damage. The procedures that follow are made for the airplane structure in general. But, the examinations can be confined to the general area of the bird/hail strike.
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