AD 67-23-03

AD Final Rules - DRS_67-23-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
67-23-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes
Subject:
Reverse Thrust Plunger Unit Rods
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/04/1967
Make:
Airbus SAS
Model:
BAC 1-11 200 Series | BAC 1-11 400 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Superseded AD: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Superseded By: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: 67-23-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-461

AD NUMBER:   67-23-03

SUBJECT HEADING:   Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 4, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-23-03 BRITISH AIRCRAFT: Amdt. 39-461, Part 39, Federal Register August 4, 1967. Applies to Model BAC 1-11 200 and 400 Series Airplanes.

Compliance required as indicated.

To prevent failure of the reverse thrust plunger unit rods P/N AC 39-117, accomplish the following:

(a) Within the next 155 hours' time in service after the effective date of this AD and thereafter at an interval not to exceed 600 hours' time in service from the initial inspection, remove and dismantle reverse thrust plunger units P/N AC 39A 111 and visually inspect plunger rods P/N AC 39-117 for cracks, distortion, or other defects in accordance with British Aircraft Corporation Alert Service Bulletin No. 76-A-PM 2837 or later ARB-approved issue, or FAA- approved equivalent.

(b) Replace cracked, distorted, or defective plunger rods, P/N AC 39-117, with serviceable plunger rods of the same part number before further flight.

(c) Within the next 1,000 hours time in service after the effective date of this AD, replace reverse thrust plunger units P/N AB 39 A 111 with plunger units P/N AB 39 A 3477 in accordance with British Aircraft Corporation Service Bulletin No. 76-PM 2837 or later ARB- approved issue or FAA-approved equivalent.

(d) The inspections required by paragraph (a) may be discontinued after reverse thrust plunger units P/N AB 39 A 111 have been replaced with plunger units P/N AB 39 A 3477 in accordance with paragraph (c).

This amendment effective August 4, 1967.

FOOTER: