AD/FSM/29 Amdt 2 Precision Airmotive Corporation Carburettors (Cth)

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/FSM/29 Amdt 1 and issues the following AD under subregulation 39.1 (1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Fuel Supply and Metering Equipment

AD/FSM/29 Amdt 2 Precision Airmotive Corporation Carburettors 2/2005

Applicability:

Precision Airmotive Corporation (PAC, formerly Facet Aerospace Products Corporation and Marvel-Schebler Corporation) Model MA-3, MA-3A, MA-3PA, MA-3SPA, MA-4SPA carburettors installed on but not limited to Textron Lycoming O-235, O-290, and O-320 series engines, and Teledyne Continental Motors (TCM) A-65, A-75, C-75, C-85, C-90, C-115, C-125, C-145, O-200, and O-300 series engines.

Requirement:

Model MA-3A, MA-3PA, MA-3SPA, and MA4-SPA carburettors:

1.    Inspect the carburettor to determine if a two-piece venturi is installed. If a two-piece venturi is installed, inspect the carburettor to determine if the primary venturi is loose or missing.

2.    If a two-piece venturi is installed and the primary venturi is found loose or missing, repair the carburettor by installing a serviceable two-piece venturi or by installing a one-piece venturi as per provisions of Precision Airmotive Service Bulletin (SB) No. MSA-2, Revision 1, 2, 3 or later FAA approved revision.

Note 1:  Carburettors that have the letter "V" stamped or etched on the lower portion of the data plate, or that have a black, yellow, or blue data plate showing the Precision Airmotive Corporation (PAC) name and logo, or that have a black Facet Aerospace Products data plate with a serial number beginning with 750, are already equipped with a one-piece venturi and no further action is necessary provided the engine does not subsequently run rough or experience power loss.

3.    If a one-piece venturi is already installed, or installed in accordance with the requirement 2 of this Airworthiness Directive (AD) and engine subsequently runs rough or experiences power loss, accomplish either of the following:

a.     Install a carburettor containing a two-piece venturi and resume the inspections as per requirement 1 and 2 of this AD; OR

b.    Modify the carburettor in accordance with paragraphs 3.b.(i), 3.b(ii), or 3.b.(iii) of this Directive, as applicable:

(i)    For PAC Model MA-3SPA series carburettors with part numbers (P/N) 10-4894 or 10-4115-1, installed on TCM Model O-200A series engines modified by installing a one-piece venturi, install a new fuel nozzle in accordance with PAC SB MSA-7, dated 30 September 1994.

(ii)   For PAC Model MA-3SPA series carburettors with P/Ns 10-4895, 10-4439, or 10-3237, installed on TCM Model O-300 or C-145 series engines modified by installing a one-piece venturi, install a new fuel nozzle in accordance with PAC SB No. MSA-8, dated 10 July 1995.

(iii)  For PAC Model MA-3SPA series carburettors with P/Ns 10-4240, 10-4252, 10-4252-1, or 10-4457, installed on TCM Model C-75, C-85, or C-90 series engines modified by installing a one-piece venturi, install a new fuel nozzle in accordance with PAC SB No. MSA-9, dated 10 October 1995.

Note 2:  Installing a one-piece venturi constitutes terminating action for the repetitive inspection as per requirement 1 of this AD.

Model MA-3 series carburettors:

4.    Inspect the carburettor to determine if the primary venturi is loose or missing.

5.    If primary venturi is found loose or missing, repair the carburettor by installing a serviceable two-piece venturi, or replace the entire carburettor with a serviceable carburettor.

Note 3:  FAA AD 98-01-06 Amendment 39-10270 refers.

Compliance:

1.    Unless accomplished earlier, within 50 flight hours or 30 days from the effective date of this Directive, whichever comes first and repetitively there after, at each annual or 100-hourly inspection, whichever comes first.

2.    Before further flight, following inspection per requirement 1 of this Directive.

3.    Before further flight, if a one-piece venturi is installed and engine subsequently runs rough or experiences power loss, as indicated in requirement 3 of this Directive.

4.    Unless accomplished earlier, within 50 flight hours or 30 days from the effective date of this Directive, whichever comes first and repetitively there after, at each annual or 100-hourly inspection, whichever comes first.

5.    Before further flight, following inspection per requirement 4 of this Directive.

This Amendment becomes effective on 17 February 2005.

Background:

Disruption of fuel flow to the engine may result in the failure to attain rated power, power loss in flight, and forced landings.  This AD addresses the identified unsafe condition associated with the power loss in flight.

Amendment 2 of the AD reflects requirements of FAA AD 98-01-06.

Amendment 1 of this AD became effective on 1 January 1998 and made reference to now superseded FAA AD 93-18-03.

The original issue of this AD became effective on 6 January 1994.

James Coyne
Delegate of the Civil Aviation Safety Authority

23 December 2004

The above AD is notified in the Commonwealth of Australia Gazette on 26 January 2005.