AD/CESSNA 188/45 - Cigar Lighter Wiring

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Legislation au F2006B05180 In force Legislative Instrument

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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 39.1 (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 188 (Agwagon) Series Aeroplanes

 

AD/CESSNA 188/45 Cigar Lighter Wiring 3/2003

 

Applicability: Model 188 series aeroplanes with serial numbers 188-0001 through 188-0572 and 18800573 through 18803046.

 

Requirement: If not previously accomplished; disconnect the wire, at the ammeter or at the electrical system bus as applicable, that connects the bus to the cigar lighter receptacle. (The wire is connected to either the bus side or equipment side of a circuit breaker or to the ammeter). Following the disconnection of this wire either:

 

  1. Reconnect the wire to the electrical bus by using an existing or newly installed circuit protection device that is properly rated to protect the wire gauge used for this circuit, or

 

b.        Disconnect the wire from the lighter receptacle at the opposite end and remove it from the aeroplane, or

 

c.         Protect the wire by insulating its disconnected end, fold this wire end back against the wire bundle in which it is routed and secure it to that bundle.

 

Note 1: The requirements of this Directive may have been previously accomplished in accordance with FAA AD 79-08-03 Amdt 39-3428.

 

Note 2: For those installations reconnected in accordance with paragraph a. above, the proper rated circuit protection device to be used may be determined by consulting FAA Advisory Circular 43.13-1B Chapter 11.

 

Note 3: FAA AD 79-08-03 Amdt 39-3428 refers.

 

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.

 

Cessna 188 (Agwagon) Series Aeroplanes

 

AD/CESSNA 188/45 (Continued)

 

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 26 February 2003.

Overview

The Civil Aviation Safety Authority (CASA) issued Airworthiness Directive AD/CESSNA 188/45 on 7 February 2003, which applies to the Cessna 188 (Agwagon) series aeroplanes with specific serial numbers. This directive was introduced in response to incidents where the wiring of the cigar lighter receptacle had shorted, potentially leading to in-flight electrical system failures, smoke in the cockpit, and fires in the wire bundle behind the instrument panel. The objective of this directive is to mandate corrective actions to mitigate these risks, ensuring the safety of the aircraft during operation. CASA requires the disconnection of the wire connecting the bus to the cigar lighter receptacle and specifies three options to ensure the wire is either properly protected or removed, depending on the circumstances. This Airworthiness Directive was enacted under subregulation 39.1 (1) of the Civil Aviation Regulations 1998 and became effective on 20 March 2003. Compliance is required at the next annual inspection, but no later than 100 hours of time in service or 12 months after the directive's effective date, whichever comes first. The directive was published in the Commonwealth of Australia Gazette on 26 February 2003, and it applies to specific model 188 series aeroplanes with serial numbers ranging from 188-0001 through 188-0572 and 188-00573 through 188-03046.

Scope and Application

The Airworthiness Directive (AD) issued under the Civil Aviation Regulations 1998 (CAR 1998) applies specifically to the Cessna 188 (Agwagon) Series Aeroplanes with serial numbers ranging from 188-0001 through 188-0572 and 18800573 through 18803046. This directive mandates corrective action concerning the wiring of the cigar lighter in these aircraft to mitigate the risk of unsafe conditions such as electrical system failures, cockpit smoke, and potential fires. The directive requires the disconnection of the wire connecting the electrical bus to the cigar lighter receptacle, with subsequent actions including the installation of a properly rated circuit protection device or the removal of the wire from the aircraft. The AD applies to aircraft within the Commonwealth of Australia and is effective from 20 March 2003, with compliance required at the next annual inspection, but no later than 100 hours of time in service or 12 months from the effective date, whichever occurs first. The AD incorporates references to previous FAA directives and advisory circulars, providing guidance on the appropriate measures to be taken.

Key Provisions

The Airworthiness Directive (AD) issued by the Civil Aviation Safety Authority (CASA) under subregulation 39.1 (1) of the Civil Aviation Regulations 1998 (CAR 1998) pertains specifically to the Cessna 188 (Agwagon) series aeroplanes with serial numbers 188-0001 through 188-0572 and 18800573 through 18803046. The AD is aimed at addressing an unsafe condition related to the wiring of the cigar lighter receptacle (section 2). The directive mandates that the wire connecting the bus to the cigar lighter receptacle must be disconnected, and one of three specified actions must be taken to ensure the safety of the aircraft's electrical system. These actions include: (a) reconnecting the wire with a properly rated circuit protection device, (b) disconnecting and removing the wire from the lighter receptacle, or (c) insulating and securing the disconnected end of the wire (section 3). The AD imposes several obligations on the parties involved, primarily the aircraft owners and operators. They are required to comply with the directive within a specified timeframe, which is the next annual inspection, but no later than 100 hours of time in service or 12 months after the effective date of the directive, whichever occurs first (section 4). This requirement ensures that the necessary safety measures are implemented promptly to mitigate the risks associated with the unsafe condition. The directive also provides guidance on determining the proper rated circuit protection device by referencing FAA Advisory Circular 43.13-1B Chapter 11 (section 3, Note 2). Failure to comply with the AD may result in civil or criminal consequences. While the specific penalties are not detailed in the text of the directive, non-compliance with CASA directives can lead to enforcement actions, including fines, suspension, or revocation of the aircraft's certificate of airworthiness. Such outcomes underscore the importance of adhering to the AD to maintain the safety and airworthiness of the aircraft. Additionally, non-compliance could potentially lead to in-flight electrical system failures, smoke in the cockpit, and/or fires, which could have severe implications for the safety of the flight crew and passengers (section 5).

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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.