AD 62-20-02

final rule
Data completeness: 70%

Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M and 30 Series Aircraft

AD Number
62-20-02
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 Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M and 30 Series Aircraft
aircraft D & R Nevada LLC 22M Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M and 30 Series Aircraft
aircraft D & R Nevada LLC 30 Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M and 30 Series Aircraft
aircraft D & R Nevada LLC 30A Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M and 30 Series Aircraft

Unsafe Condition

The aileron override spring may jam in the compressed position if full opposition loads are applied to the lateral control system.

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

Required Actions

Modify the aileron override spring assembly to incorporate a stop in accordance with General Dynamics/Convair Service Bulletins A27-56, A27-25, or A27-26 for Models 22, 22M, or 30 respectively, or an FAA engineering approved equivalent.

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 from 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, 22M, and 30 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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