AD/CON/66 Amdt 2 - Fuel Pump Drive Coupling

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Teledyne Continental Motors Piston Engines

 

AD/CON/66

Amdt 2


Fuel Pump Drive Coupling 10/96

 

Applicability: All Teledyne Continental Motors (TCM) piston engines, as listed by model number below, which incorporate a fuel pump as listed by part number (P/N) in TCM Mandatory Service Bulletin Number MSB95-6 or are fitted with a fuel pump, regardless of P/N, which has had a P/N 646176 fuel pump shaft installed.

 

IO-346-A

 

IO-520-B, BA, BB, C, CB, M, MB IO-550-A, B, C, G

TSIO-520-B, BB, D, DB, E, EB, J, JB, K, KB, L, LB, N, NB, UB, VB, WB TSIO-550-B

TSIOL-550-A, B

 

Requirement: To prevent the disengagement of the fuel pump drive coupling which may result in the loss of engine power:

 

1. a. Remove the fuel pump and inspect the fuel pump shaft in accordance with TCM Mandatory Service Bulletin MSB95-6, Figure 1, to determine the part number of the shaft fitted, and

 

  1. b. If a current style P/N 646176 fuel pump shaft is found fitted, ensure only a new style P/N 653359 drive coupling is installed when reassembling the fuel pump to the engine. Fuel pumps incorporating an early style P/N 643689 shaft may continue in service until next engine overhaul with either the old style P/N 631263 or a new style P/N 653359 drive coupling fitted.

 

2.    Replace the old style fuel pump drive coupling P/N 631263 with a new style drive coupling P/N 653359.

 

Note 1: Requirement 2 is only applicable to fuel pumps found, during compliance with Requirement 1, to have the early style P/N 643689 fuel pump shaft incorporated.

 

Note 2: FAA Airworthiness Directive 93-16-15 refers.

 

Compliance: Requirement 1: Unless previously accomplished in accordance with amendment 1 of this directive; within 30 hours time in service effective on 12 September 1996.

 

Requirement 2: At next engine overhaul after 12 September 1996.

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 

Background:  This directive was originally issued on 30 May 1993 to require an inspection of the fuel pump drive coupling for correct engagement. Amendment 1 was issued on 29 February 1996 to include IO-346 engines and fuel pumps incorporating a P/N 646176 shaft. This amendment corrects an ambiguity in the applicability of engines fitted with a fuel pump incorporating the P/N 646176 shaft. Teledyne Continental Motors has confirmed, only "Permold" engine models as listed in TCM MSB95-6 are affected, regardless of the fuel pump configuration.

 

The original issue of this Airworthiness Directive became effective on 30 May 1993. Amendment 1 of this Airworthiness Directive became effective on 29 February 1996.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.