AD/BEECH 36/44 - Interior Door Handles

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B03900 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Beechcraft 36 (Bonanza) Series Aeroplanes

 

AD/BEECH 36/44 Interior Door Handles 12/97

Applicability: Models 36, A36, A36TC, and B36TC; 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, particularly Part 39 - 105, address the critical issue of aircraft safety by issuing specific directives to ensure that aircraft remain airworthy throughout their operational life. Enacted by the Australian Parliament, these regulations serve to mitigate risks associated with aircraft malfunctions and ensure the safety of passengers and crew. One such directive, AD/BEECH 36/44, pertains to the Beechcraft 36 (Bonanza) Series Aeroplanes, requiring checks and necessary adjustments to the interior door handles to prevent unintentional door openings. This directive was introduced in response to reports of door handles opening without the lock release button being depressed, which could lead to hazardous situations in flight. The overarching policy objective of these regulations is to maintain the highest standards of safety within the Australian civil aviation sector, thereby protecting public safety and maintaining the integrity of the national airspace.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates airworthiness directives aimed at ensuring the safety of civil aviation operations. This particular airworthiness directive, AD/BEECH 36/44, applies to Beechcraft 36 (Bonanza) Series Aeroplanes, including models 36, A36, A36TC, and B36TC, covering all serial numbers. The directive requires operators to check the cabin side door handle and the utility door handle for proper locking mechanisms. If the door handle opens the door without the lock release button being depressed, the directive mandates corrective action by reinstalling the door handle according to specified instructions to ensure proper locking. This directive applies unless the corrective action has already been taken and requires compliance within 50 hours in service after 6 November 1997 or at the next removal of a door handle after this date. The directive was issued in response to reports of unintentional door openings from the aircraft's interior, which could lead to loss of control due to pilot distraction. The directive is enforceable throughout the Commonwealth of Australia and its application extends through subordinate instruments as necessary.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes an airworthiness directive (AD/BEECH 36/44) concerning Beechcraft 36 (Bonanza) Series Aeroplanes (section 1). This directive mandates that the cabin side door handle and the utility door handle must be checked from the interior of the aircraft to ensure proper locking (section 1). If the door handle opens the door when rotated without depressing the lock release button, corrective action is required, which involves removing and re-installing the door handle according to the Accomplishment Instructions in Raytheon Service Bulletin 2693 (section 1(a)). Conversely, if the door handle is already locked and can only be unlocked by depressing the lock release button, no further action is necessary (section 1(b)). This directive is applicable to models 36, A36, A36TC, and B36TC, across all serial numbers (section 1). Operators of these aircraft must ensure compliance with the directive by performing the required checks within 50 hours of time in service after 6 November 1997 or at the next door handle removal after that date, whichever occurs first (section 1). Additionally, the checks must be conducted at any time a utility or cabin interior door handle is removed (section 1). The directive aims to prevent unintentional opening of the cabin side door and the utility door from the interior of the aircraft, which could potentially lead to a loss of control due to pilot distraction (section 1). Failure to comply with the airworthiness directive may result in safety risks, as the directive is intended to address reported incidents where door handles opened without the lock release button being depressed (section 1). The directive was issued following numerous reports received by the Federal Aviation Administration (FAA), highlighting the importance of adhering to the specified corrective actions (section 1). Non-compliance could potentially result in regulatory actions, including penalties or other consequences under the Civil Aviation Regulations 1998 (section 1). The directive became effective on 6 November 1997, underscoring the urgency and importance of its implementation (section 1).

Legal classification tags

Area of Law
Administrative Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers

Interactions

Authorises

All Versions

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.