AD Amdt-39-10845

final rule
Data completeness: 70%

Airworthiness Directives; Robinson Helicopter Company Model R44 Helicopters

AD Number
Amdt-39-10845
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-SW-01-AD
FR Citation
63 FR 55783

Applicability

TypeManufacturerModelDetails
aircraft Robinson Helicopter Company Model R44 Airworthiness Directives; Robinson Helicopter Company Model R44 Helicopters

Unsafe Condition

A crack in the welded corner of the cyclic control pilot's grip assembly may lead to failure of the grip assembly 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

Remove and replace the cyclic control pilot's grip assembly with an airworthy grip assembly.

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

Robinson Helicopter Company Model R44 helicopters.

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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