# AD 67-30-02: Lower Sidestay Pin Retaining Bolt - Type: Airworthiness directive - Status: Current - Products: Airbus BAC 1-11 200 Series and BAC 1-11 400 Series - Effective: December 4, 1967 - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Large airplane - Amendment: 39-507 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B0C160EF75C807078625699F006BC840.0001 - DRS record last changed: May 30, 2024 - Page: https://openairdocs.org/ad/67-30-02 ## The airworthiness directive 67-30-02 BRITISH AIRCRAFT: Amdt. 39-507, Part 39, Federal Register November 4, 1967. Applies to Model BAC 1-11 200 and 400 Series Airplanes which incorporate Modification PM 1558 part (c). Compliance required as indicated unless already accomplished. To prevent fatigue damage of the lower sidestay pin retaining bolt, P/N AC43-267, accomplish the following: (a) Within the next 200 landings after the effective date of this AD or before the accumulation of 5,000 landings, whichever occurs later, and thereafter at intervals not to exceed 5,000 landings from the last inspection, inspect the main landing gear lower sidestay retaining bolts, P/N AC43-267, for cracks, using the magnetic particle procedure or an FAA-approved equivalent, in accordance with British Aircraft Corporation BAC 1-11 Alert Service Bulletin 32- A-PM 2898, Issue 1, dated April 14, 1967, or later ARB-approved issue, or an FAA-approved equivalent. (b) If defective retaining bolts, P/N AC43-267, are found during the inspection required by paragraph (a), before further flight replace the bolts with serviceable bolts of the same part number or new bolts, P/N AC43-399, in accordance with BAC 1-11 Service Bulletin No. 32-PM 2898 Revision 1, dated April 10, 1967, or later ARB-approved issue, or an FAA- approved equivalent. (c) Before the accumulation of 15,000 landings, replace retaining bolts, P/N AC43- 267, with serviceable bolts of the same part number or new bolts, P/N AC43-399. If bolts P/N AC43-267 are used as replacement bolts, inspect the bolts at intervals not to exceed 5,000 landings in accordance with paragraph (a) and replace the bolts at intervals not to exceed 15,000 landings. (d) The repetitive inspections and replacements required by paragraphs (a) and (c) may be discontinued after the new bolts, P/N AC43-399, are installed. Retaining bolt P/N AC43- 399 does not have a service life limitation. (e) 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 amendment effective December 4, 1967. ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A5EU](https://openairdocs.org/tcds/A5EU): Airbus SAS; names 2 of 2 models: BAC 1-11 200 Series, BAC 1-11 400 Series ## Registered aircraft it may apply to (OpenAirDocs) No registered aircraft matched the models it names. ## Related documents - [AC 43-10C](https://openairdocs.org/ac/43-10): United States—Canadian Bilateral Aviation Safety Agreement Maintenance Implementation Procedures. Cited as AC 43 in the AD's requirements - [AC 43-11 CHG 1 Ed Update](https://openairdocs.org/ac/43-11): Reciprocating Engine Overhaul Terminology and Standards. 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Cited as AC 43 in the AD's requirements - [AC 43-6D Ed Update](https://openairdocs.org/ac/43-6): Altitude Reporting Equipment and Transponder System Maintenance and Inspection Practices. Cited as AC 43 in the AD's requirements - [AC 43-7](https://openairdocs.org/ac/43-7): Ultrasonic Testing for Aircraft. Cited as AC 43 in the AD's requirements - [AC 43-9D Ed Update](https://openairdocs.org/ac/43-9): Maintenance Records and FAA Form 8130-3 Return to Service. Cited as AC 43 in the AD's requirements --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.