AD/CONVAIR/21 - FAA Non-Repetitive ADs (Cth)

Federal Register of Legislation

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AIRWORTHINESS DIRECTIVE For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(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.

Kelowna Flightcraft (General Dynamics/Convair) Series Aeroplanes AD/CONVAIR/21 FAA Non-Repetitive ADs 5/2006

Applicability: General Dynamics (CONVAIR) Model 240, 340 and 440 series aeroplanes. Requirement: 1. Determine the applicability of the AD's listed in Table 1 of this AD.

Table 1 FAA AD Number Effective Date 56-20-04 Upon Receipt 56-24-01 Upon Receipt 56-24-02 Upon Receipt 56-27-01 Upon Receipt 58-01-03 Upon Receipt 59-01-01 Upon Receipt 59-04-02 Upon Receipt 60-14-01 Upon Receipt 63-06-03 20 March 1963 70-10-03 12 May 1970 78-17-04 5 September 1978 78-22-04 1 November 1978 90-13-13 30 July 1990 91-12-05 25 July 1991 93-04-03 19 April 1993 96-03-04 28 February 1996 98-08-17 19 May 1998 Note: Compliance: Within This Background: The CASA 2. If it is determined that an applicable AD has not been accomplished, perform the actions required by the AD. Title Fire Seals Cylinder Carburettors Elevator Servo Tab Rod Carburettor Setting Fire Detector System Pilot's Direct-Vision Window Main Landing Gear Electrical Fault Detection Panel Engine Breather Oil Fumes Emergency Window Release Handle Emergency Exit Window Fuselage Frames Elevator Hinge Pins Horizontal And Vertical Stabilizers Aircraft Flight Manual - Limitation, Icing Conditions Aircraft Flight Manual - Power Levers Prior to 1963 FAA AD's did not have effective dates. 30 days after the effective date of this AD. Airworthiness Directive becomes effective on 11 May 2006. AD's listed in Table 1 of this AD have been evaluated and found to require one-time inspections or modifications as at the effective date of this AD. In addition the compliance period for these AD's has passed. With the introduction of the aeroplane onto the Australian register, the intention of this AD is to ensure compliance with the AD's listed in Table 1. appreciates that not all AD's listed in Table 1 of this AD may be applicable, due to the incorporation of STC's or other modifications.

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Kelowna Flightcraft (General Dynamics/Convair) Series Aeroplanes AD/CONVAIR/21 FAA Non-Repetitive ADs 5/2006

Applicability: General Dynamics (CONVAIR) Model 240, 340 and 440 series aeroplanes. Requirement: 1. Determine the applicability of the AD's listed in Table 1 of this AD.

2. If it is determined that an applicable AD has not been accomplished, perform the actions required by the AD. Table 1 FAA AD Number Effective Date Title 56-20-04 Upon Receipt Fire Seals 56-24-01 Upon Receipt Cylinder 56-24-02 Upon Receipt Carburettors 56-27-01 Upon Receipt Elevator Servo Tab Rod 58-01-03 Upon Receipt Carburettor Setting 59-01-01 Upon Receipt Fire Detector System 59-04-02 Upon Receipt Pilot's Direct-Vision Window 60-14-01 Upon Receipt Main Landing Gear 63-06-03 20 March 1963 Electrical Fault Detection Panel 70-10-03 12 May 1970 Engine Breather Oil Fumes 78-17-04 5 September 1978 Emergency Window Release Handle 78-22-04 1 November 1978 Emergency Exit Window 90-13-13 30 July 1990 Fuselage Frames 91-12-05 25 July 1991 Elevator Hinge Pins 93-04-03 19 April 1993 Horizontal And Vertical Stabilizers 96-03-04 28 February 1996 Aircraft Flight Manual - Limitation, Icing Conditions 98-08-17 19 May 1998 Aircraft Flight Manual - Power Levers Note: Prior to 1963 FAA AD's did not have effective dates. Compliance: Within 30 days after the effective date of this AD. This Airworthiness Directive becomes effective on 11 May 2006. Background: The AD's listed in Table 1 of this AD have been evaluated and found to require one-time inspections or modifications as at the effective date of this AD. In addition the compliance period for these AD's has passed. With the introduction of the aeroplane onto the Australian register, the intention of this AD is to ensure compliance with the AD's listed in Table 1. CASA appreciates that not all AD's listed in Table 1 of this AD may be applicable, due to the incorporation of STC's or other modifications.

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