AD 67-24-03

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AD Number:
67-24-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11-200 and 400 Series Airplanes
Subject:
Rudder Pedal Lock Unit Housing
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/13/1967
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Superseded AD: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Superseded By: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: 67-24-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-442

AD NUMBER:   67-24-03

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

ACTION:  

SUMMARY:  

DATES:   Effective July 13, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-24-03 BRITISH AIRCRAFT: Amdt. No. 39-442, Federal Register July 8, 1967. Applies to Model BAC 1-11-200 and 400 Series Airplanes.

Compliance required as indicated.

To prevent failure of the rudder pedal reach adjuster lock unit housing P/N AB 32-509, accomplish the following:

(a) Within the next 50 hours' time in service after the effective date of this AD, unless already accomplished within the last 200 hours' time in service, and thereafter at intervals not to exceed 250 hours time in service from the last inspection, visually inspect the rudder pedal reach adjuster lock unit housing P/N AB32-509 for cracks in accordance with British Aircraft Corporation BAC 1-11 Alert Service Bulletin No. 27-A-PM 2946, Issue I, or later ARB-approved issue. Cracked housings must be replaced before further flight with an unused or serviceable housing having the same part number or with a new housing P/N AB32-9011 and locking plunger P/N AB32-9013 in accordance with BAC 1-11 Service Bulletin No. 27-PM 2946, or later ARB- approved issue, or FAA-approved equivalent.

(b) If no cracks are detected during the inspection required by paragraph (a), lubricate the housing and conduct a functional check of the lock unit assembly in accordance with BAC 1-11 Alert Service Bulletin No. 27-A-PM 2946 or later ARB-approved issue. Correct defects found before further flight.

(c) Within the next 1200 hours' time in service after the effective date of this AD, replace rudder pedal reach adjuster lock unit housing P/N AB32-509 with new housing P/N AB32-9011 and locking plunger P/N AB32-9013 in accordance with BAC 1-11 Service Bulletin No. 27-PM 2946, or later ARB-approved issue, or FAA-approved equivalent.

(d) The repetitive inspections required by paragraph (a) and the functional checks required by paragraph (b) may be discontinued after the new housing P/N AB32-9011 and locking plunger P/N AB32-9013 are installed in accordance with paragraph (a) or (c) of this AD.

This amendment effective July 13, 1967.

FOOTER: