- Effective
- October 25, 1962
- Models
- 22, 22M
- Data sheet
- TCDS4A27
- Product
- Aircraft · Large airplane
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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|---|---|---|---|
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The airworthiness directive
62-21-02 GENERAL DYNAMICS/CONVAIR: Amdt. 487 Part 507 Federal Register September 25, 1962. Applies to All Models 22 and 22M Series Aircraft.
Compliance required within the next 350 hours' time in service after the effective date of this AD, unless already accomplished.
With the rudder pedals adjusted to the full forward position and the rudder fully deflected, mechanical interference can make it impossible to apply brakes on the side with the deflected rudder.
To correct this interference problem, P/N's 22-41202-1 LH and 22-41202-2 RH located at fuselage Station 192 shall be reworked in accordance with General Dynamics/Convair Service Bulletin A27-53 for the Model 22 and A27-22 for the Model 22M or in accordance with an FAA engineering approved equivalent modification.
(General Dynamics/Convair Alert Service Bulletin A27-53 for the Model 22 and A27-22 for the Model 22M cover this same subject.)
This directive effective October 25, 1962.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.