(c)  
Look for fuel leaks, and other fluid leaks, in the areas that follow. 1) The lower external surface of the fuselage in the area of

 the wing-to-body fairing. 2) The forward wall of the wheel wells of the main landing gear.
 S 212-048
 (4)  Reduced Vertical Separation Minimum (RVSM) Inspection
 (a)  Examine the reduced vertical separation minimum (RVSM) (AMM 51-10-00/601).
 S 212-031
 (5)  Wing Inspection
 (a)  
Examine the leading edge fairing at the wing-to-body joint.

 (b)  
Examine the trailing edge flaps on the inboard side.

 (c)  
Look for fuel leaks, and other fluid leaks, in the areas that follow: 1) The wing 2) The nacelles 3) The nacelle-struts.

 S 212-032
 (6)  Engine Nacelle Inspection
 (a)  
Examine the doors, panels, and the structure on the nacelle strut.

 (b)  
Do the four steps that follow before the next 10 flights:

 1)  Identify these fuse pins on the engine nacelle strut and wing: a) Upper link (forward pin) b) Diagonal brace (aft pin)
 2) Remove the through bolt and end caps of each fuse pin. 3) Clean the grease from the inner diameter of the fuse pin. 4) Look for distortion of the inner diameter of the fuse pin.
 a) Use a straight edge or an equivalent device.
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 C. Cabin Inspections
 S 212-043
 (1)  
Do a visual inspection of all ceiling panels for dislodging and evi dence do to impact damage.

 S 212-044

 (2)  
Do a visual inspection of all ceiling overhead bins for evidence of looseness and impact damage.

 S 212-045

 (3)  
Do a detailed visual inspection of all ceiling panels equipped with video monitors.

 (a)  Inspect latches, stops, potting inserts and all fasteners.
 S 212-046
 (4)  Continue the Cabin Inspection in the Phase II inspection if any cabin damage was found in the above Cabin Inspection including the ceiling panels, central overhead bins, or the video monitors. If no damage was found, no further cabin inspection is required and it is not necessary to continue the Cabin Inspection in Phase II.
 TASK 05-51-01-212-033
 3.  Phase 2 Inspection__________________
 A. References
 (1)  
AMM 05-51-10/201, Dragged Engine Nacelle/Engine Seizure/Engine and Strut Damage Condition

 (2)  
AMM 07-11-01/201, Jacking Airplane

 (3)  
AMM 12-15-01/301, Main Gear Shock Strut - Servicing

 (4)  
AMM 12-15-02/301, Nose Gear Shock Strut - Servicing

 (5)  
AMM 27-00-01/201, Flight Controls

 (6)  
AMM 32-11-01/401, Main Landing Gear

 (7)  
AMM 32-21-01/401, Nose Landing Gear

 (8)  
AMM 32-32-00/501, Main Landing Gear Extension and Retraction

 (9)  
AMM 32-34-00/501, Nose Landing Gear Extension and Retraction

 (10)
 AMM 32-51-00/501, Nose Wheel Steering System

 B. Airplane Inspection
 S 022-034
 (1)  Main Landing Gear and Support Structure Inspection
 (a)  
Make sure the shock strut pressures are normal and the hydraulic fluids are at the correct levels (AMM 12-15-01/301).

 (b)  
Lift the airplane with jacks (AMM 07-11-01/201).

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MAINTENANCE MANUAL

 WARNING:_______ MAKE SURE YOU SUFFICIENTLY HOLD THE LANDING GEAR AND THE
 SUPPORT STRUCTURE WHEN YOU REMOVE THE FUSE PINS.  IF YOU
 DO NOT SUFFICIENTLY HOLD THESE COMPONENTS, YOU CAN CAUSE
　
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