AD Amdt-39-10377

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Raytheon Model DH 125-1A and -3A Series Airplanes

AD Number
Amdt-39-10377
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 96-NM-196-AD
FR Citation
63 FR 11114

Applicability

TypeManufacturerModelDetails
aircraft Raytheon DH 125-1A and -3A Airworthiness Directives; Raytheon Model DH 125-1A and -3A Series Airplanes

Unsafe Condition

Fatigue cracking of the main entry door/frame pressing due to cyclic loading of the door frame.

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

Required Actions

Perform repetitive eddy current inspections to detect fatigue cracking of the main entry door/frame pressing. Repair, if necessary.

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 Model DH 125-1A and -3A series airplanes

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

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