Airworthiness Directive

AD 2007-21-02 72 FR 57850 Active

Federal Aviation Administration · 14 CFR part 39

Requires a reduction in the structural life limit to 4,500 hours time-in-service (TIS) for the airframe (wing, fuselage, empennage, and associated structure).

FR document
E7-19888
Amendment
39-15220
Published
2007-10-11
Effective
2007-11-15
Models covered
1

Last live check: 2026-08-19

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AD

2007-21-02

FR doc E7-19888 · 72 FR 57850

AD 2007-21-02Published 2007-10-11Effective 2007-11-15

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 a reduction in the structural life limit to 4,500 hours time-in-service (TIS) for the airframe (wing, fuselage, empennage, and associated structure).

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company (RAC) Models 58P and 58TC airplanes that were used as lead airplanes by the United States Forest Service (USFS). This AD establishes new limits for the structural life of the airframe (wing, fuselage, empennage, and associated structure) through the incorporation of a supplement to the Limitations Section of the pilot's operating handbook and airplane flight manual (POH/AFM). This AD results from the FAA's analysis and determination that the operational history and usage of the affected airplanes requires a reduction in the structural life limit to 4,500 hours time-in-service (TIS) for the airframe (wing, fuselage, empennage, and associated structure). We are issuing this AD to prevent structural failure of the airframe (wing, fuselage, empennage, or associated structure) based on the operational history and usage of the affected airplanes. Such failure could lead to loss of control.

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Applies to 1 model in our index