Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.
AIRWORTHINESS DIRECTIVE AIRWORTHINESS DIRECTIVE
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 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.
Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes
AD/CESSNA 170/72 Cigar Lighter Wiring 3/ AD/CESSNA 170/72 Cigar Lighter Wiring 3/2003
AD/CESSNA 170/72 Cigar Lighter Wiring 3/2003
Applicability: Model 170, 172, R172, P172 and 175 series aeroplanes with serial numbers listed in the following table:
Models Models
Models
170
172
R172 P172 175
Serial Numbers Serial Numbers
Serial Numbers
18000 through 20999 and 25000 through 27169
28000 through 29999, 46001 through 47746, 17247747 through
17250572, and 17259224 through 17267584
R1722000 through R1722724 P17257120 through P17257189
55001 through 56777 and 17556778 through 17557119
Cessna 170, 172, F172, FR172 and 175 Ser Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes
Cessna 170, 172, F172, FR172 and 175 Series Aeroplanes
AD/CESSNA 170/72 (Continued)
Compliance: At the next annual inspection, but no later that 100 hours time in service or 12 months after the effective date of this Directive, which ever occurs first.
This Airworthiness Directive becomes effective on 20 March 2003.
Background: Incidents of the cigar lighter unprotected electrical wiring shorting have been reported overseas. This Directive requires either the deactivation of the cigar lighter or the installation of a circuit protection device. These measures are designed to prevent an in-flight electrical system failure, smoke in the cockpit, and/or fire in the wire bundle behind the instrument panel.
James Coyne
Delegate of the Civil Aviation Safety Authority 7 February 2003