| AD Number | 67-24-03 | Status | Active |
| Effective Date | July 13, 1967 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-442 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Airbus SAS |
| Model(s) | BAC 1-11 200 Series BAC 1-11 400 Series |
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 ServiceBulletin 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.