AD 2002-03-16

Recurring final rule
Data completeness: 60%

Airworthiness Directives; Bell Helicopter Textron, Inc.-Manufactured Model OH-13E, OH-13H, and OH-13S Helicopters

AD Number
2002-03-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-SW-17-AD
FR Citation
67 FR 7594

Applicability

TypeManufacturerModelDetails
aircraft Textron Various Airworthiness Directives; Bell Helicopter Textron, Inc.-Manufactured Model OH-13E, OH-13H, and OH-13S Helicopters
aircraft Bell Helicopter Textron Airworthiness Directives; Bell Helicopter Textron, Inc.-Manufactured Model OH-13E, OH-13H, and OH-13S Helicopters

Unsafe Condition

Cracks in the main rotor blade grip threads could lead to failure of the grip, loss of a main rotor blade, and subsequent loss of control of the helicopter.

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

Required Actions

Conduct recurring eddy current inspections of the main rotor blade grip threads. Replace any cracked grip with an airworthy grip before further flight. Report inspection results to the FAA Rotorcraft Certification Office.

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

Compliance Time

Before further flight if a crack is detected.

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

Affected Aircraft

Bell Helicopter Textron, Inc. Model OH-13E, OH-13H, and OH-13S helicopters with two added part numbers (P/N).

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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