W DOC AIRBUS | AMM A320F

53-51 MAIN STRUCTURE


    53-51-00 MAIN STRUCTURE

  • PB.001 MAIN STRUCTURE - DESCRIPTION AND OPERATION
  • PB.601 MAIN STRUCTURE - INSPECTION/CHECK
    • 53-51-00-210-001-A [10]
      Detailed Inspection of Rear Pressure Bulkhead Complete Aft Face, and Fuselage Internal Structure, between FR 70 and FR 71, from Stringer 26, LH/RH to Bottom Center Line
    • 53-51-00-210-002-A [10]
      Detailed Visual Inspection of Rear Pressure Bulkhead Forward Face below Cabin Floor Level
    • 53-51-00-210-004-A [10]
      Detailed Inspection of Fuselage Skin at Horizontal Stabilizer Cutout at Forward, Upper and Lower Corners, LH/RH
    • 53-51-00-210-005-A [10]
      Detailed Visual Inspection of FR74, Splices at STGR12 and STGR19 LH/RH, Internal Structure
    • 53-51-00-210-007-A [10]
      Detailed Inspection of Horizontal Stabilizer Attachment and Back-up Structure at FR77, from Stringer 8 to Stringer 21, LH/RH
    • 53-51-00-210-008-A [10]
      Detailed Inspection of Forward Face of the Rear Pressure Bulkhead above the Cabin Floor Level
    • 53-51-00-210-009-A [10]
      Detailed Visual Inspection of Tail Cone Attachment Fittings at FR77 and FR78
    • 53-51-00-210-012-A [10]
      Detailed Inspection of Fin to Fuselage, Forward, MID and AFT Attach Fittings, Outside Fuselage, LH/RH
    • 53-51-00-210-017-A [10]
      Detailed Visual Inspection of Shear Ties and Frame Clips at FR72 and FR74, between Stringer 3 and Stringer 9, LH/RH, Internal Structure
    • 53-51-00-210-019-A [10]
      General Visual Inspection of Fuselage Skin around Cutout for Tail Compartment Access Door, between FR 70 and FR 73 and between STGR 25 RH and Bottom ...
    • 53-51-00-220-802-A [10]
      Special Detailed Inspection (HFEC) of the Lower Flanges of FR 72 and FR 74, between STGR 10 LH and STGR 10 RH
    • 53-51-00-210-018-A [10]
      General Visual Inspection of Fuselage External Surface and Vertical Stabilizer Attachment Fitting, underneath Vertical Stabilizer/Fuselage Fairings
    • 53-51-00-210-020-A [10]
      General Visual Inspection of the Rear Fuselage Internal Structure, between FR70 and FR77
    • 53-51-00-210-021-A [10]
      General Visual Inspection of the Rear Fuselage External Surface, between FR70 and FR87
    • 53-51-00-250-801-A [10]
      Special Detailed Inspection (ROTO) of Ring Frame at Circumferential Joint of Rear Pressure Bulkhead Skin at FR 70, AFT Face
    • 53-51-00-210-003-A [8]
      Detailed Inspection of the Ring Frame at the Circumferential Joint of the Rear Pressure Bulkhead Skin at FR70, AFT Face
    • 53-51-00-210-014-A [8]
      Detailed Inspection of Rear Pressure Bulkhead AFT Face, Reinforcement Splice at Forward Fin Attachment Area
  • 53-51-17 MAINTENANCE PLATFORM

  • PB.401 MAINTENANCE PLATFORM - REMOVAL/INSTALLATION
    • 53-51-17-000-001-A [10]
      Removal of the Maintenance Platform Panels (AFT Equipment Compartment)
    • 53-51-17-400-001-A [10]
      Installation of the Maintenance Platform Panels (AFT Equipment Compartment)