AD 2004-09-07

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Aircraft Company Model 1900, 1900C, 1900C (C-12J), and 1900D Airplanes

AD Number
2004-09-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 95-CE-46-AD
FR Citation
69 FR 24941

Applicability

TypeManufacturerModelDetails
aircraft Raytheon Aircraft Company Model 1900 Airworthiness Directives; Raytheon Aircraft Company Model 1900, 1900C, 1900C (C-12J), and 1900D Airplanes

Unsafe Condition

Cracks in the canted bulkhead located at Fuselage Station (FS) 588.10 could result in failure of the bulkhead, leading to loss of rudder and elevator control, which could result in loss of control of the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Repetitively inspect the canted bulkhead at FS 588.10 for cracks. Incorporate canted bulkhead Repair Kit No. 129-4005-1 S anytime cracks are found. Terminate repetitive inspection requirements after Kit No. 129-4005-1 S is installed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Raytheon Aircraft Company Model 1900, 1900C, 1900C (C-12J), and 1900D airplanes that do not have canted bulkhead Kit No. 129-4005-1 S incorporated.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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