PHASE NO. _____
Area Name and No.
Aircraft Serial No.
LEFT FUSELAGE, AREA #2
Faults and/or Remarks
2.33 Fluid drain lines for damage and
2.34 Access doors, work platforms,
and panels for damage. Latching
mechanism for security and proper
operation. Seals for cuts, tears, cracks,
and security. Engine work platform
support struts for security, twisting, and
proper operation of pins. Access 57,
60, 61, 62, 63, 66, 68, 69, 70
2.35 Entire area for structural damage,
skin cracks, dents or buckling, loose or
missing rivets, evidence of corrosion.
Paint for chipping or peeling. Stencils
and decals for condition.
2.36 Static port for obstruction and
Check work area for tools and parts after completion of maintenance and inspection.