AD 67-31-02

AD Final Rules - DRS_67-31-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
67-31-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 203/AE, 204/AF and 212/AR Airplanes
Subject:
Fuel Leak At Station 630
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/18/1967
Make:
Airbus SAS
Model:
BAC 1-11 200 Series
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Superseded AD: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Superseded By: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: 67-31-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-512

AD NUMBER:   67-31-02

SUBJECT HEADING:   Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 203/AE, 204/AF and 212/AR Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 18, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-31-02 BRITISH AIRCRAFT: Amdt. 39-512, Part 39, Federal Register November 18, 1967. Applies to Model BAC 1-11 203/AE, 204/AF and 212/AR Airplanes.

Compliance required within the next 3,000 hours' time in service after the effective date of this AD, unless already accomplished. To avoid the possibility of a fuel leak within the pressurized area, relocate the left and right fuel line couplings from Station 630 to a point 3 inches forward, in accordance with British Aircraft Corporation BAC 1-11 Service Bulletin No. 28-PM 2914, dated May 12, 1967, or later ARB-approved issue, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.

This amendment effective December 18, 1967.

FOOTER: