AD 65-19-01

final rule
Data completeness: 70%

Airworthiness Directives; Air and Space Model 18A Gyroplanes

AD Number
65-19-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
Federal Register: August 25, 1965

Applicability

TypeManufacturerModelDetails
aircraft Air & Space America, Inc. 18A Airworthiness Directives; Air and Space Model 18A Gyroplanes

Unsafe Condition

Failure of main rotor blade retention bolts while supporting the blade near the tip to prevent contact with the droop stops.

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

Required Actions

Replace three main rotor blade retention bolts, P/N RO-U18-2136-11, and nuts, P/N MS-20364-1614, with new bolts and nuts furnished by the manufacturer after August 4, 1965, and torque the nuts to 45-50 foot pounds dry thread torque value.

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

Compliance Time

before further flight unless already accomplished

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

Affected Aircraft

Air & Space America, Inc. Model 18A Gyroplanes, Serial Numbers 18-7 through 18-28.

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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