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Airworthiness Directive

AD 2005-26-53 71 FR 2453 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires you to insert text into the Limitations Section of the Airplane Flight Manual (AFM) that reduces the maximum takeoff weight from 7,500 pounds to 7,125 pounds.

Superseded by AD 2006-13-05Federal Register (opens in a new tab)

FR document
06-260
Amendment
39-14451
Published
2006-01-17
Effective
2006-01-16
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2005-26-53 · 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

2005-26-53

FR doc 06-260 · 71 FR 2453

AD 2005-26-53Published 2006-01-17Effective 2006-01-16

Superseded by 2006-13-05

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 insert text into the Limitations Section of the Airplane Flight Manual (AFM) that reduces the maximum takeoff weight from 7,500 pounds to 7,125 pounds.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all Pacific Aerospace Corporation (PAC) Ltd. Model 750XL airplanes. This AD contains the same information as emergency AD 2005-26-53 and publishes the action in the Federal Register. This AD requires you to insert text into the Limitations Section of the Airplane Flight Manual (AFM) that reduces the maximum takeoff weight from 7,500 pounds to 7,125 pounds. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for New Zealand. We are issuing this AD to reduce the maximum takeoff weight that will allow wing ultimate load requirements to be met. If wing ultimate load requirements are not met, wing failure could result and subsequent 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) Search DRS manually for AD 2005-26-53 (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