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Airworthiness Directive

AD 2005-24-07 70 FR 71381 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the condition of the left and right outer panel attachment lugs for damage (scoring and gouging) and/or cracks (using a fluorescent penetrant inspection procedure for the crack inspection); to inspect the…

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FR document
05-23260
Amendment
39-14387
Published
2005-11-29
Effective
2005-12-29
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2005-24-07 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

2005-24-07

FR doc 05-23260 · 70 FR 71381

AD 2005-24-07Published 2005-11-29Effective 2005-12-29

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires you to inspect the condition of the left and right outer panel attachment lugs for damage (scoring and gouging) and/or cracks (using a fluorescent penetrant inspection procedure for the crack inspection); to inspect the spacing of left and right outer panel attachment lugs; to replace the lugs if damage is found; and to make necessary corrections to the spacing.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Pacific Aerospace Corporation Ltd Model 750XL airplanes. This AD requires you to inspect the condition of the left and right outer panel attachment lugs for damage (scoring and gouging) and/or cracks (using a fluorescent penetrant inspection procedure for the crack inspection); to inspect the spacing of left and right outer panel attachment lugs; to replace the lugs if damage is found; and to make necessary corrections to the spacing. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for New Zealand. We are issuing this AD to prevent structural failure of the outer panel and spar due to a cracked, bent, or distorted condition of the left and right outer panel attachment lugs; and incorrect spacing of the left and right outer panel attachment lugs. This failure could lead to loss of control of the airplane.

More directives for Pacific Aerospace 750XL/FU24

  1. AD 2021-23-16 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2022-01-11
  2. AD 2021-23-19 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2022-01-11
  3. AD 2021-21-11 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2021-12-10
  4. AD 2021-21-10 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2021-12-10
  5. AD 2021-20-20 Airworthiness Directives; Pacific Aerospace Limited Airplanes Effective 2021-11-22

All Pacific Aerospace 750XL/FU24 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index