Airworthiness Directive

AD 2005-26-53 71 FR 2453

Federal Aviation Administration · 14 CFR part 39

FR document
06-260
Amendment
39-14451
Published
2006-01-17
Models covered
1
Last live check
2026-08-17
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Superseded by 2006-13-05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.

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.

Applies to 1 model in our index