Airworthiness Directive

AD 2004-09-07 69 FR 24941 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to repetitively inspect the canted bulkhead located at Fuselage Station (FS) 588.

FR document
04-9898
Amendment
39-13596
Published
2004-05-05
Effective
2004-06-14
Models covered
1

Last live check: 2026-10-04

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AD

2004-09-07

FR doc 04-9898 · 69 FR 24941

AD 2004-09-07Published 2004-05-05Effective 2004-06-14

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 repetitively inspect the canted bulkhead located at Fuselage Station (FS) 588.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company (Raytheon) Model 1900, 1900C, 1900C (C-12J), and 1900D airplanes that do not have canted bulkhead Kit No. 129-4005-1 S incorporated. This AD requires you to repetitively inspect the canted bulkhead located at Fuselage Station (FS) 588.10 for cracks and incorporate canted bulkhead Repair Kit No. 129-4005-1 S anytime cracks are found. When Kit No. 129-4005-1 S is incorporated, the repetitive inspection requirement in this AD is terminated and no further action is required. This AD is the result of numerous reports of multi-site cracks occurring in the canted bulkhead at FS 588.10. We are issuing this AD to detect and correct cracks in the canted bulkhead. These cracks could result in failure of the bulkhead. Failure of the canted bulkhead could lead to loss of rudder and elevator control, which could result in loss of control of the airplane.

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Applies to 1 model in our index