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 185 Series Aeroplanes
AD/CESSNA 185/47 Cigar Lighter Wiring 3/2003
Applicability: Model 185 series aeroplanes with serial numbers 18500968 through 18503458.
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:
- 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 185 Series Aeroplanes
AD/CESSNA 185/47 (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 Airworthiness Directive (AD) AD/CESSNA 185/47 issued in 2003 by the Civil Aviation Safety Authority (CASA) under subregulation 39.1 (1) of the Civil Aviation Regulations 1998, addresses the identified safety concern related to the unprotected electrical wiring of the cigar lighter in Cessna 185 series aeroplanes. This directive applies to aircraft within the specified serial number range and aims to prevent unsafe conditions that could lead to in-flight electrical system failures, cockpit smoke, or fires. The directive mandates that the wiring connecting the electrical bus to the cigar lighter receptacle must be disconnected and either replaced with a properly rated circuit protection device, removed entirely, or otherwise insulated and secured. This action must be taken by the next annual inspection, but no later than 100 hours of service or 12 months from the directive's effective date, whichever comes first. The policy objective of this directive is to enhance the safety of the aircraft by mitigating the risks associated with the reported incidents of electrical shorting.
Scope and Application
The Airworthiness Directive issued under the Civil Aviation Regulations 1998 pertains specifically to the Cessna 185 series aeroplanes with serial numbers ranging from 18500968 to 18503458. The directive mandates the disconnection of the wire connecting the electrical bus to the cigar lighter receptacle if certain conditions are met. This can be done either by reconnecting the wire with a properly rated circuit protection device, disconnecting and removing the wire from the aeroplane, or insulating and securing the wire's disconnected end. The directive requires compliance either at the next annual inspection or within 100 hours of time in service, whichever occurs first, from the effective date of 20 March 2003. The directive aims to mitigate risks of electrical system failures, cockpit smoke, and potential fires by addressing issues with unprotected wiring in the cigar lighter system. The directive applies across the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority (CASA), with potential extensions or restrictions through subordinate instruments as necessary.
Key Provisions
This Airworthiness Directive (AD), issued under the Civil Aviation Regulations 1998, applies to Cessna 185 series aeroplanes with specific serial numbers, namely those ranging from 18500968 through 18503458. The primary directive, outlined in the requirement section, mandates the disconnection of the wire that connects the electrical bus to the cigar lighter receptacle. This can be achieved by either reconnecting the wire with a properly rated circuit protection device, disconnecting the wire from the lighter receptacle and removing it from the aeroplane, or insulating the disconnected end of the wire and securing it to the wire bundle. It is essential to note that the action must be taken if it has not been previously accomplished, as indicated in Note 1, which refers to FAA AD 79-08-03 Amdt 39-3428. Additionally, Note 2 advises consulting FAA Advisory Circular 43.13-1B Chapter 11 for determining the proper rated circuit protection device.
The AD imposes specific obligations on the parties or entities it governs. Owners and operators of the affected aircraft must ensure that the required action is taken in accordance with the instructions set out in the requirement section and at the time mentioned in the compliance section. This means that the action must be carried out during the next annual inspection, but no later than 100 hours of time in service or 12 months after the effective date of this Directive, whichever occurs first. The directive also highlights the importance of adhering to the specified instructions to maintain the airworthiness of the aircraft and prevent potential hazards such as electrical system failures, smoke in the cockpit, and fires in the wire bundle behind the instrument panel.
Failure to comply with this Airworthiness Directive may result in civil and/or criminal consequences. The maximum penalties for non-compliance with the Civil Aviation Regulations 1998 include fines and imprisonment. However, the specific penalties for breaching this AD are not stated in the text. It is crucial for the parties and entities governed by this AD to take the required action to ensure the safety and airworthiness of the aircraft and to avoid any potential legal ramifications.