AD 62-21-02

final rule
Data completeness: 70%

GENERAL DYNAMICS/CONVAIR Models 22 and 22M Series Aircraft

AD Number
62-21-02
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 GENERAL DYNAMICS/CONVAIR Models 22 and 22M Series Aircraft
aircraft D & R Nevada LLC 22M GENERAL DYNAMICS/CONVAIR Models 22 and 22M Series Aircraft

Unsafe Condition

Mechanical interference between rudder pedals in full forward position and rudder fully deflected can prevent application of brakes on the side with deflected rudder.

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

Required Actions

Rework parts P/N 22-41202-1 LH and 22-41202-2 RH at fuselage Station 192 per General Dynamics/Convair Service Bulletin A27-53 (Model 22) or A27-22 (Model 22M), or an FAA-approved equivalent modification.

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

Compliance Time

within the next 350 hours' time in service after the effective date of this AD

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

Affected Aircraft

GENERAL DYNAMICS/CONVAIR Models 22 and 22M Series Aircraft

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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