AD 62-07-01

final rule
Data completeness: 70%

Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 and 22M Aircraft

AD Number
62-07-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft D & R Nevada LLC 22 Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 and 22M Aircraft
aircraft D & R Nevada LLC 22M Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 and 22M Aircraft

Unsafe Condition

Failure or cracking of the forward support trunnions for elevator and rudder balance boards P/N 22-14715-7, 9, 15, and 17.

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

Required Actions

Inspect the forward support trunnions for failure or cracking in accordance with Part A(1) of General Dynamics/Convair Alert Service Bulletins 880-A27-55 or 880M-A27-24. Replace any failed or cracked parts before further flight. Replace specific trunnion part numbers with approved equivalents to discontinue repetitive inspections.

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

Compliance Time

within the next 75 hours' time in service after the effective date of this AD and at periods thereafter not to exceed 75 hours' time in service

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

Affected Aircraft

GENERAL DYNAMICS/CONVAIR Models 22 and 22M Aircraft with elevator and rudder balance boards P/N 22-14715-7, 9, 15, and 17.

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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