W DOC AIRBUS | AMM A320F

57-41 LEADING EDGE


    57-41-00 LEADING EDGE

  • PB.001 LEADING EDGE - DESCRIPTION AND OPERATION
  • PB.601 LEADING EDGE - INSPECTION/CHECK
    • 57-41-00-200-001-A [10]
      Inspection of the Wing Leading Edge
    • 57-41-00-200-002-A [10]
      Detailed Inspection of Slat 1, Tracks 1 to 4: Visible Part of Roller Contact Area when Slat is Fully Extended, LH/RH
    • 57-41-00-200-003-A [10]
      Detailed Inspection of Outer Wing, Bottom Skin, Lower Surface at Drain Holes for Track Cans, 1, 2, 3 and 4 (Rib-Bays 1-2, 2-3, 4-5, 5-6)....
    • 57-41-00-200-005-A [10]
      Detailed Visual Inspection of the Outer Wing Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIBS 15-16 and 22-23
    • 57-41-00-200-005-A-01 [10]
      Detailed Visual Inspection of the Outer Wing Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIB 22-23 and Magnetic Level Indicator Position
    • 57-41-00-200-008-A [10]
      Detailed Inspection of Slat 2, Tracks 5 and 6: Visible Part of Roller Contact Area When Slat is Fully Extended, LH/RH
    • 57-41-00-200-009-A [10]
      Detailed Inspection of Slat 3, Tracks 7 and 8: Visible Part of Roller Contact Area When Slat is Fully Extended, LH/RH
    • 57-41-00-200-010-A [10]
      Detailed Inspection of Slat 4, Tracks 9 and 10: Visible Part of Roller Contact Area When Slat is Fully Extended, LH/RH
    • 57-41-00-200-011-A [10]
      Detailed Visual Inspection of Slat 5, Tracks 11 and 12: Visible Part of Roller Contact Area
    • 57-41-00-200-012-A [10]
      Detailed Inspection of Outer Wing, Fixed Leading Edge, Roller Pin Holes and other Cutouts in Track Rib 1 to 12
    • 57-41-00-200-014-A [10]
      Detailed Inspection of Outer Wing, Fixed Leading Edge, Bottom Attachment Joint on Track Rib 1 to 12
    • 57-41-00-200-015-A [10]
      Detailed Visual Inspection of the Outer Wing Fixed Leading Edge Bottom Wing Skin Upper and Lower Surfaces Forward of Front Spar from RIB1 to RIB27 ....
    • 57-41-00-200-016-A [10]
      Detailed Inspection of Outer Wing, Fixed Leading-Edge Top-Wing-Skin, Upper and Lower Surfaces, Forward of Front Spar, from RIB 1 to 27
    • 57-41-00-200-017-A [10]
      Special Detailed Inspection of Outer Wing, Fixed Leading Edge Pinion Fitting Bolting and Actuator Bolting Lower Bolt Holes on Ribs 2, 3, 5, 6, 7, 8....
    • 57-41-00-210-801-A [10]
      General Visual Inspection of Outer Wing, Fixed Leading Edge, Bottom Wing Skin, Upper and Lower Surfaces, Forward of Front Spar, from RIB 1 to RIB 27...
    • 57-41-00-220-801-A [10]
      Detailed Inspection of Outer Wing, Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIB 22-23, and Magnetic Level Indicator Position...
    • 57-41-00-220-802-A [10]
      Detailed Inspection of Outer Wing, Bottom Skin Lower Surface at Fuel Tank Water Drain Holes between RIB 22-23
    • 57-41-00-200-802-A [10]
      Detailed Inspection of Outer Wing, Bottom Skin, Lower Surface at Drain Holes for Track Cans 1, 2, 3 and 4 (Rib-bays 1-2, 2-3, 4-5, 5-6), Dry Bay...
    • 57-41-00-280-801-A [10]
      Special Detailed Inspection (US) of Outer Wing, Bottom Skin, Lower Surface at Drain Holes For Track Cans 1-4 (Rib Bays 1-2, 2-3, 4-5, 5-6), Magnetic Level...
    • 57-41-00-280-802-A [10]
      Special Detailed Inspection (US) of Outer Wing, Bottom Skin, Lower Surface at Drain Holes For Track Cans 1-4 (Rib Bays 1-2, 2-3, 4-5, 5-6), Dry Bay Drain ...
    • 57-41-00-200-013-A [8]
      Special Detailed Inspection of the Outer Wing Fixed Leading Edge Forward Upper Roller Pin Holes in Track Ribs 5, 6, 7, 8, 9, 10, 11 and 12
  • 57-41-33 MOUNTINGS - SUPPORTS

  • PB.401 MOUNTINGS - SUPPORTS - REMOVAL/INSTALLATION
  • 57-41-37 ACCESS PANELS AND COVERS

  • PB.401 ACCESS PANELS AND COVERS - REMOVAL/INSTALLATION
  • PB.801 ACCESS PANELS AND COVERS - REPAIRS
    • 57-41-37-350-001-A [10]
      Repair to the Leading Edge Pressure-Relief Panel After it has Operated
    • 57-41-37-350-002-A [10]
      Repair to the Leading Edge Pressure-Relief Panel After it has Operated
    • 57-41-37-350-003-A [10]
      Repair to the Leading Edge Pressure-Relief Panel After it has Operated
    • 57-41-37-350-004-A [10]
      Repair to the Leading Edge Pressure-Relief Panel After it has Operated
    • 57-41-37-350-005-A [10]
      Repair to the Leading Edge Pressure-Relief Panel After it has Operated