AD 67-01-01

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Superseded AD: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Superseded By: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

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-321

AD NUMBER:   67-01-01

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

ACTION:  

SUMMARY:  

DATES:   Effective January 15, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-01-01 BRITISH AIRCRAFT: Amdt. 39-321 Part 39 Federal Register December 16, 1966. Applies to Model BAC 1-11 200 and 400 Series Airplanes.

Compliance required as directed.

To prevent fatigue failures of the flap carriage links, accomplish the following until links, P/N AB09 A943, are replaced with modification PM 2245 links, P/N AB09 A3657:

(a) For 200 Series airplanes having No. 1 flap links with less than 2,500 landings on the effective date of this AD, remove links from service before the accumulation of 3,000 landings.

(b) For 200 Series airplanes having No. 1 flap links with 2,500 or more landings on the effective date of this AD, remove links from service within the next 500 landings after the effective date of this AD.

(c) For 200 Series airplanes having No. 2 flap links with less than 11,500 landings on the effective date of this AD, remove links from service before the accumulation of 12,000 landings.

(d) For 200 Series airplanes having No. 2 flap links with 11,500 or more landings on the effective date of this AD, remove links from service within the next 500 landings after the effective date of this AD.

(e) For 200 Series airplanes having No. 3 flap links with less than 23,500 landings on the effective date of this AD, remove links from service before the accumulation of 24,000 landings.

(f) For 200 Series airplanes having No. 3 flap links with 23,500 or more landings on the effective date of this AD, remove links from service within the next 500 landings after the effective date of this AD.

(g) For 400 Series airplanes having No. 1 flap links with less than 1,500 landings on the effective date of this AD, remove links from service before the accumulation of 2,000 landings.

(h) For 400 Series airplanes having No. 1 flap links with 1,500 or more landings on the effective date of this AD, remove links from service within the next 500 landings after the effective date of this AD.

(i) For 400 Series airplanes having No. 2 flap links with less than 7,500 landings on the effective date of this AD, remove links from service before the accumulation of 8,000 landings.

(j) For 400 Series airplanes having No. 2 flap links with 7,500 or more landings on the effective date of this AD, remove links from service within the next 500 landings after the effective date of this AD.

(k) For 400 Series airplanes having No. 3 flap links with less than 15,500 landings on the effective date of this AD, remove links from service before the accumulation of 16,000 landings.

(l) For 400 Series airplanes having No. 3 flap links with 15,500 or more landings on the effective date of this AD, remove links from service within the next 500 landings after the effective date of this AD.

(m) 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.

(British Aircraft Corporation (Operating) Ltd. (Weybridge Division), Alert Service Bulletin No. 27-A-PM2245 pertains to this subject.)

This directive effective January 15, 1967.

FOOTER: