AD 63-21-01

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AD Number:
63-21-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GENERAL DYNAMICS Model 30 Aircraft
Subject:
Landing Gear Anti-Skid
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/28/1963
Make:
D & R Nevada LLC
Model:
30 | 30A
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Superseded AD: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Superseded By: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: 63-21-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   63-21-01

SUBJECT HEADING:   Airworthiness Directives; GENERAL DYNAMICS Model 30 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective October 28, 1963.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   63-21-01 GENERAL DYNAMICS: Amdt. 623 Part 507 Federal Register September 26, 1963. Applies to All Model 30 Aircraft.

Compliance required within 500 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent a ground fault in the landing gear ground safety switch which causes the loss of braking without a warning indication, modify the aircraft landing gear anti-skid wiring system as follows in accordance with Convair Service Bulletin No. 32-37A revised February 26, 1963, or an FAA Western Region Engineering approved equivalent:

(a) Add a test switch, relay socket, relay and harnesses;

(b) replace the antiskid and light plastic panel, circuit board and plate; and

(c) reroute the wiring.

(Convair Service Bulletin No. 32-37A pertains to this same modification.)

This directive effective October 28, 1963.

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