AD 67-15-01

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AD Number:
67-15-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes
Subject:
Stabilizer Link Pin
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/18/1967
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Superseded AD: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Superseded By: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: 67-15-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-401

AD NUMBER:   67-15-01

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

ACTION:  

SUMMARY:  

DATES:   Effective May 18, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-15-01 BRITISH AIRCRAFT: Amdt 39-401 Part 39 Federal Register April 18, 1967. Applies to Model BAC 1-11 200 and 400 Series Airplanes.

Compliance required as indicated, unless already accomplished.

To prevent failure of the link pin, P/N AB 21-6503, installed between the stabilizer pivot lower link assembly and the fin, accomplish the following:

(a) Within the next 200 landings for airplanes with 800 or more landings, and before the expiration of 1,000 landings for airplanes with less than 800 landings, remove P/N AB 21- 6503 from service, and replace with a new P/N AB 21-6679.

(b) After each installation of a new P/N AB 21-6679, conduct a check of the adjustment and torque loading of the horizontal stabilizer side load transfer mechanism and stabilizer link assembly center pivot in accordance with BAC 1-11 Alert Service Bulletin 55-A- PM 2706, Issue 1, dated November 16, 1966, or later ARB-approved issue.

(c) For the purpose of complying with this AD, subject to acceptance by the assigned FAA maintenance inspector, the number of landings may be determined by dividing each airplane's hours' time in service by the operator's fleet average time from takeoff to landing for the airplane type.

This directive effective May 18, 1967.

FOOTER: