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ASSEMBLY AND HANDLING

Aircraft Assembly and Major-Component Handling

General planning and control principles for aircraft assembly and major-component handling.

Concept illustration of a large aircraft component supported by a sling and cradle
Generic handling arrangement. Use only the aircraft-defined lifting points, support geometry, capacity and safety devices.

Key reference points

  • Use current task data and approved handling equipment.
  • Align components without forcing attachment interfaces.
  • Complete rigging, security and operational checks.

Organised training notes

1Prepare the assembly task

Use the current maintenance instructions and illustrated parts data to establish configuration, access, hardware and tooling.

  1. 1.1 Task dataConfirm removal or installation sequence, component weight, centre of gravity, clearances and required inspections.
  2. 1.2 EquipmentUse approved jigs, cradles, slings, spreader bars, hoists, jacks and adapters with adequate capacity.

2Control the interfaces

Support and align the assembly so attachment points meet naturally without forcing or transferring unintended loads.

  1. 2.1 StructureInspect mounting areas, fittings and hardware; protect finished surfaces and approved load paths.
  2. 2.2 SystemsIdentify, protect and verify the routing of controls, wiring, hoses and tubing before closing the interface.

3Complete and verify

Finish the aircraft-specific rigging, torque, locking, safetying and operational checks before release.

  1. 3.1 Hardware securityUse the specified fastener, installation direction, torque method and safetying device.
  2. 3.2 Post-installation checksComplete alignment, clearance, freedom-of-movement, leak, function and independent inspections as required.
Training-reference boundary

This summary is not approved repair or maintenance data. Do not inspect, classify, select material, alter structure or perform a repair from this page alone. Use the current applicable SRM, AMM, engineering order, drawing and company procedures.