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(6) Wing and Centre Section Assembly

Inspect structure for general condition, deterioration, distortion, evidence of failure and insecurity of attachment.

(7) Empennage Assembly

Inspect structure for general condition, deterioration, distortion, evidence of failure, insecure attachment, improper component installation and improper component operation.

  • (8)

    Propeller Group

    • (a)

      Propeller hub assembly - inspect for cracks, nicks, binding and oil leakage; (amended 2000/12/01; previous version)

(b) Bolts and nuts - inspect for improper torque and safety locking; (amended 2000/12/01; previous version)

(c) Anti-icing devices - inspect for improper operation and defects, paying particular attention to: (amended 2000/12/01; previous version)

    • (i)

      deicer boots for cuts, gouges and adherence;

    • (ii)

      slip ring for excessive wear and gouges; and

    • (iii)

      connections and harness for tightness.

  • (d)

    Control mechanisms - inspect for improper operation, insecure mounting and

improper range of travel;

(e) Blades - inspect for (amended 2000/12/01; no previous version)

(i) cracks, nicks, external corrosion, (amended 2000/12/01; no previous version)

(ii) evidence of lightening or object strike, and (amended 2000/12/01; no previous version)

    • (iii)

      correct track, excessive rotational and end play; (amended 2000/12/01; no previous version)

  • (f)

    Spinner assembly - inspect for cracks and wear;

(amended 2000/12/01; no previous version)

COPA Guide to Certified Aircraft 36

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