# AD 62-21-02: Rudder

- Type: Airworthiness directive
- Status: Current
- Products: D & R Nevada 22 and 22M
- Effective: October 25, 1962
- Superseded by: Nothing supersedes this AD
- Product type: Aircraft, Large airplane
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D1D6286AA9C3167A86256A3B006D6B1E.0001
- DRS record last changed: May 30, 2024
- Page: https://openairdocs.org/ad/62-21-02

## 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 data sheets (1) (OpenAirDocs)

The type certificate data sheets whose models the AD names.

- [TCDS 4A27](https://openairdocs.org/tcds/4A27): CV Nevada, LLC; names 2 of 2 models: 22, 22M

## Registered aircraft it may apply to (OpenAirDocs)

No registered aircraft matched the models it names.

Its text cites no advisory circulars or STCs.

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