COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes
AD/BEECH 33/42 Interior Door Handles 12/97
Applicability: Models E33, F33, G33, E33A, F33A, E33C, and F33C; all serial numbers.
Requirement: Check the cabin side door handle and the utility door handle from the interior of the aircraft for proper locking (rotating the door handle clockwise without depressing the lock release button) in accordance with the Accomplishment Instruction section of Raytheon Service Bulletin 2693.
(a) If the door handle opens the door when rotated, without depressing the handle’s lock release button, correct the door handle lock by removing the door handle, and re-installing the door handle so that the lock release button locks the door in accordance with the Accomplishment Instructions section in Raytheon Service Bulletin 2693.
(b) If the door handle is locked and will only unlock by depressing the door handle lock release button, then no further action is necessary.
Note: FAA AD 97-14-15 Amdt 39-10073 refers.
Compliance: Unless already accomplished, within 50 hours time in service after 6 November 1997 or at the next door handle removal after 6 November 1997, whichever occurs first; and thereafter at any time a utility or cabin interior door handle is removed.
This airworthiness directive becomes effective on 6 November 1997.
Background: The FAA received numerous reports of the utility and cabin door handle opening from the interior of the aircraft without depressing the lock release button. The actions specified by this Directive are intended to prevent unintentional opening of the cabin side door and the utility door from the interior of the aircraft. This could result in a loss of control caused by the distraction to the pilot.
Overview
The Civil Aviation Regulations 1998, as amended, address various safety concerns related to aircraft operations in Australia. Specifically, Part 39 of these regulations contains airworthiness directives designed to ensure the safety of aircraft in service. One such directive is AD/BEECH 33/42, which was enacted to address issues with the interior door handles of Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes. The problem this directive seeks to resolve involves the cabin side door and utility door handles potentially opening from the interior of the aircraft without the lock release button being depressed, which could lead to loss of control due to pilot distraction. This directive is issued by the Civil Aviation Safety Authority, under the authority of the Civil Aviation Act 1988, with the policy objective of enhancing flight safety and preventing accidents through mandatory maintenance actions.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to airworthiness directives issued by the Civil Aviation Safety Authority (CASA). This particular directive applies to Beechcraft 33 and 35-33 (Debonair/Bonanza) Series aeroplanes, including models E33, F33, G33, E33A, F33A, E33C, and F33C, with all serial numbers falling within its scope. The directive mandates that the cabin side door handle and the utility door handle be checked for proper locking mechanisms to prevent unintentional opening from the interior of the aircraft. This requirement involves rotating the door handle clockwise without depressing the lock release button, and if necessary, correcting the door handle lock by following the instructions provided in Raytheon Service Bulletin 2693. Compliance with this directive must be achieved within 50 hours of time in service after 6 November 1997 or at the next removal of a door handle after this date, and subsequently whenever a door handle is removed. The directive aims to prevent potential loss of control due to pilot distraction from unintentional door openings.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, includes an airworthiness directive (AD/BEECH 33/42) that pertains to Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes. This directive mandates that the cabin side door handle and the utility door handle must be checked for proper locking functionality (section 1). If the door handle opens the door when rotated without depressing the lock release button, it must be corrected by removing and reinstalling the door handle according to the Accomplishment Instructions in Raytheon Service Bulletin 2693 (section 1(a)). If the door handle is already functioning correctly, no action is required (section 1(b)).
The directive applies to models E33, F33, G33, E33A, F33A, E33C, and F33C, covering all serial numbers. Compliance with this directive is necessary unless the action has already been taken. It must be completed within 50 hours of time in service after 6 November 1997 or at the next door handle removal after that date, whichever comes first. Additionally, the check must be performed every time a utility or cabin interior door handle is removed (section 3). The directive became effective on 6 November 1997, following reports of door handles opening unintentionally from the interior, which could cause loss of control due to pilot distraction.
The obligations imposed by this airworthiness directive require operators of the specified Beechcraft models to ensure that the door handles are properly locked and functional. Operators must follow the instructions provided in Raytheon Service Bulletin 2693 to check and, if necessary, correct the door handle lock. Failure to comply with these requirements could result in the door opening unintentionally, posing a significant safety risk during flight.
In the event of non-compliance with the airworthiness directive, there may be serious consequences. Although specific penalties are not detailed within the directive, non-compliance could lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions might include fines, operational restrictions, or other regulatory measures to ensure the safety of the aircraft and its occupants. The potential for loss of control due to an improperly functioning door handle underscores the importance of adhering to these requirements.