AD 62-21-02

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AD Number:
62-21-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
GENERAL DYNAMICS/CONVAIR Models 22 and 22M Series Aircraft
Subject:
Rudder
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/25/1962
Make:
D & R Nevada LLC
Model:
22 | 22M
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 62-21-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   62-21-02

SUBJECT HEADING:   GENERAL DYNAMICS/CONVAIR Models 22 and 22M Series Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective October 25, 1962.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
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.

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