AD 72-07-01

final rule
Data completeness: 70%

Airworthiness Directives; McCulloch Aircraft Corp. Model J-2 Aircraft

AD Number
72-07-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Aero Resources Inc. J-2 Gyroplane Airworthiness Directives; McCulloch Aircraft Corp. Model J-2 Aircraft

Unsafe Condition

The angle between the rotor mast and pitch bearing case may be outside the 3.9 to 5.0 degree tolerance, and loose rivets on the collective stick assembly (part number 27133) at the juncture with collective stick shaft (part number 27104) may cause failure.

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

Required Actions

Inspect the rotor mast and pitch bearing case angle using a propeller protractor and rerig if outside 3.9-5.0 degrees. Inspect collective stick for loose rivets; replace assembly if found or reinspect every 25 flight hours if no rivets found.

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

McCulloch Aircraft Corp. Model J-2 Gyroplane, serial numbers 10 and subsequent (for rotor angle requirement) and serial numbers 10 through 54 (for collective stick inspection)

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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