AD/CESSNA 170/66 - Fuel Selector Valve

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Legislation au F2006B04995 In force Legislative Instrument

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Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes

 

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 39.1 (1) of CAR 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 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.

 

AD/CESSNA 170/66 Fuel Selector Valve 3/2000 TX

Applicability: Model 170, 172, F172, FP172, FR172, P172, R172 and 175 series aeroplanes as,

 

(a)     listed below by serial number; and

 

(b)     equipped with Fuel Selector Valve Cam part number 0513123, or Fuel Selector Valve part number 0513120-5, 0513120-6, 0513120-8, 0513120-9, or 0513120- 200 that Cessna shipped from 6 December 1998 through 10 May 1999.

 

Model

Serial Numbers

Model

Serial Numbers

170B

609,19401, 20267 through 20999,

25000 through 27169

172

610, 612, 615, 28000 through

29999, 36000 through 36999, 46001

through 46754

172A

622, 625, 46755 through 47746

172B

630, 17247747 through 17248734

172C

17248735 through 17249544

172D

17249545 through 17250572

172E

639, 17250573 through 17251822

172F

17251823 through 17253392

172G

17253393 through 17254892

172H

638, 17254893 through 17256492,

17256494 through 17256512

172I

17256513 through 17257161

172K

17257162 through 17259223

172L

17259224 through 17260758

172M

17256493,17260759 through

17261444, 17261446 through

17261577, 17261579 through

17263458

F172D

F172-0001 through F172-0018

F172E

F172-0019 through F172-0085

F172F

F172-0086 through F172-0179

F172G

F172-0180 through F172-0319

F172H

F172-0320 through F172-0654 F17200655 through F17200754

F172K

F17200755 through F17200804

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 

 

 

F172L

F17200805 through F17200904

F172M

F17200905 through F17201234

FP172

FP172-0001 through FP172-0003

 

 

FR172E

FR17200001 through FR17200060

FR172F

FR17200061 through FR17200145

FR172G

FR17200146 through FR17200225

FR172H

FR17200226 through FR17200350

FR172J

FR17200351 through FR17200590

FR172K

FR17200591 through FR17200675

P172D

P17257120 through P17257188

 

 

R172E (T41)

R172-0001 through R172-0335

R172F (T41)

R172-0336 through R172-0409

R172G (T41)

R1720410 through R1720444

R172H (T41)

R1720445 through R1720620

R172J

R17257189

R172K

680, R1722000 through R1723454

175

28700A

175A

619

175C

17557003 through 17557119

 

 

 

Note 1: The assessment of applicability may be made by the Certificate of Registration Holder by a review of maintenance records.

 

Requirement: (a) Replace any installed Fuel Selector Valve Cam part number 0513123, or Fuel Selector Valve part number 0513120-5, 0513120-6, 0513120-8, 0513120-9, or

0513120-200, that Cessna shipped from 6 December 1998 through 10 May 1999, in accordance with Cessna Service Bulletin SEB99-7 dated June 7, 1999.

 

(b) A fuel selector valve cam or fuel selector valve, as identified in paragraph (a) of the Requirement, must not be installed as a replacement part on an aeroplane applicable to this AD, after the effective date of this AD.

 

Note 2: FAA AD 99-27-02 refers.

 

 

 

Compliance: Within the next 10 hours time in service after the effective date of this AD. This Airworthiness Directive becomes effective on 27 January 2000.

Background: The affected fuel selector valve cams or fuel selector valves, when installed, could result in an inadequate supply of fuel to the engine. This could then result in an emergency landing or loss of control of the aeroplane.


 

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 24 January 2000

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 27 January 2000.

Overview

The Civil Aviation Regulations 1998, which were enacted to ensure the safety of civil aviation in Australia, have been supplemented by the Airworthiness Directive (AD) issued under subregulation 39.1 (1) of the Civil Aviation Regulations 1998 (CAR 1998). This particular AD, titled AD/CESSNA 170/66, was issued on 24 January 2000 by Eugene Paul Holzapfel, a delegate of the Civil Aviation Safety Authority (CASA), to address a safety issue with specific Cessna 170, 172, F172, FR172, and 175 series aeroplanes. The AD targets a specific unsafe condition related to the fuel selector valve, which could potentially lead to an inadequate fuel supply to the engine, thereby risking emergency landings or loss of control. The directive requires the replacement of certain fuel selector valve components shipped between 6 December 1998 and 10 May 1999 and prohibits the installation of these components as replacements post the AD's effective date of 27 January 2000.

Scope and Application

This Airworthiness Directive (AD) applies specifically to the Cessna 170, 172, F172, FR172 and 175 series aeroplanes that are listed by serial number and equipped with certain fuel selector valves or valve cams manufactured and shipped by Cessna between 6 December 1998 and 10 May 1999. The AD mandates that these specific parts be replaced or that the identified parts not be used for replacements in applicable aircraft. This directive applies to the entire Commonwealth of Australia and is issued under the Civil Aviation Regulations 1998 (CAR 1998). Compliance with this AD must occur within the next 10 hours of flight time after its effective date, which is 27 January 2000. The AD does not specify any exclusions or exemptions and applies to all relevant aircraft regardless of ownership or operational context within Australia. The directive may be extended or modified through subordinate instruments issued by the Civil Aviation Safety Authority (CASA).

Key Provisions

The main operative sections of this Airworthiness Directive (AD) are the applicability, requirement, and compliance sections. The applicability section specifies the Cessna aircraft models and serial numbers affected by this directive, particularly those equipped with certain fuel selector valves shipped between 6 December 1998 and 10 May 1999. The requirement section mandates that any installed fuel selector valve cam part number 0513123 or fuel selector valve part numbers 0513120-5, 0513120-6, 0513120-8, 0513120-9, or 0513120-200 must be replaced, in accordance with Cessna Service Bulletin SEB99-7 dated 7 June 1999. Additionally, it prohibits the installation of these specified valves as replacements after the AD's effective date. The compliance section requires that the specified actions be completed within the next 10 hours of time in service after the AD becomes effective, which is 27 January 2000. The AD imposes specific obligations on the parties it governs. Aircraft owners and operators must review their maintenance records to determine if their aircraft fall within the applicability section. If they do, they must replace the specified fuel selector valves as per the requirement section. Failure to comply with this AD could result in an unsafe condition that could lead to an emergency landing or loss of control of the aircraft. The AD also prohibits the installation of the specified fuel selector valves as replacements after the effective date of the AD. Failure to comply with the requirements of this AD can result in serious safety consequences. The AD clearly states that the affected fuel selector valve cams or valves, when installed, could result in an inadequate supply of fuel to the engine, potentially leading to an emergency landing or loss of control. While the AD does not specify particular offences, penalties, or consequences for non-compliance, it is clear that non-compliance poses significant risks to the safety of the aircraft and its occupants. The AD underscores the importance of adhering to the specified requirements to maintain the airworthiness of the affected aircraft.

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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.