AD/BEECH 1900/16 Amdt 1 - Exterior Operating Instruction Placards for External Doors

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Beechcraft 1900 Series Aeroplanes

 

AD/BEECH 1900/16

Amdt 1


Exterior Operating Instruction Placards for External Doors


1/99

 

Applicability: Model Serial Numbers

 

1900 UA-2 and UA-3

 

1900C  UB-1 through UB-74, and UC-1 through UC-174 1900C (C-12J)              UD-1 through UD-6

1900D UE-1 through UE-268

 

Requirement: Accomplish one of the following in accordance with the Accomplishment Instructions section of Raytheon Aircraft Mandatory Service Bulletin (MSB) 2741, Revision 1, Issued February 1997; Revised May 1997:

 

  1. Modify the existing exterior placards with operating instructions installed in accordance with the original issue of this Directive; or,

 

b.   Remove any existing operating placards and install new exterior placards with operating instructions for the airstair door, cargo door, and emergency exits, as applicable.

 

Installing placards in accordance with Raytheon Aircraft MSB 2741, dated February 1997, and then modifying these placards in accordance with Beechcraft message 52- 0506, dated February 21, 1997, is an alternative method of compliance to the requirements of this Directive.

 

Note: FAA AD 98-21-20 Amdt 39-10829 refers.

 

Compliance: Unless already accomplished, within 200 hours time in service after 28 January 1999.

This Amendment becomes effective on 28 January 1999.

Background: This Directive results from an accident involving a ground collision with another aircraft in which both aircraft were destroyed by fire. Although the occupants of the model 1900C survived the impact, the emergency crew were unable to open the airstair door and all occupants died of smoke inhalation. Investigation revealed that the external instructions for opening the door were either not clearly visible or not easily understandable.

Amendment 1 is issued in response to a new FAA AD which was prompted by reports of the previously installed placards covering the atmospheric vents for the cabin door differential pressure lock.

The original issue of this Airworthiness Directive became effective on 12 March 1997.

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, form a critical component of the regulatory framework aimed at ensuring the safety and efficiency of civil aviation. This piece of legislation was introduced to address safety concerns and to establish uniform standards for the operation and maintenance of aircraft. The Civil Aviation Safety Authority (CASA), as the enacting body, has the mandate to enforce these regulations to protect the public and maintain the integrity of the aviation industry. The policy objective behind these regulations is to enhance the overall safety of civil aviation by ensuring that all aircraft meet specific airworthiness standards, thereby preventing accidents and mitigating risks associated with aviation operations. One specific area addressed by these regulations is the requirement for specific airworthiness directives concerning certain aircraft models. For example, AD/BEECH 1900/16 Amendment 1 pertains to the exterior operating instruction placards for external doors on Beechcraft 1900 series aeroplanes. This directive was introduced following an accident where unclear placards led to the inability to open an airstair door during an emergency, resulting in fatalities. The directive mandates that specific models of the Beechcraft 1900 series must either modify their existing placards or install new ones to ensure they are clearly visible and understandable, in compliance with the requirements set out in Raytheon Aircraft Mandatory Service Bulletin 2741. This directive aims to prevent similar incidents by ensuring that all emergency procedures are easily accessible and comprehensible to flight crew members.

Scope and Application

The Civil Aviation Regulations 1998, as amended, apply to the Beechcraft 1900 Series Aeroplanes specifically within the serial numbers outlined in the Airworthiness Directives. These regulations are enforced by the Civil Aviation Safety Authority (CASA) and have a national reach across Australia, adhering to the overarching framework of civil aviation safety. The legislation mandates that aircraft operators ensure compliance with the Airworthiness Directives concerning exterior operating instruction placards for external doors of the specified Beechcraft 1900 models. Operators must modify or install new placards in accordance with the directives to enhance safety and ensure clear instructions for emergency procedures. This requirement is critical following an incident where visibility and understanding of emergency procedures contributed to fatalities. The directive applies unless the modifications have already been completed, with a compliance deadline set at 200 hours of time in service after the directive's effective date of 28 January 1999. The regulations may be further detailed or modified through subordinate instruments, ensuring adaptability to emerging safety standards and practices.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, establish the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which includes specific directives for various aircraft models. In the case of the Beechcraft 1900 Series Aeroplanes, AD/BEECH 1900/16 Amendment 1 pertains to the exterior operating instruction placards for external doors, effective from 28 January 1999. The directive specifies that for certain model and serial numbers, such as 1900 UA-2 and UA-3, 1900C UB-1 through UB-74, and 1900D UE-1 through UE-268, operators must either modify existing placards or install new ones with clear operating instructions for the airstair door, cargo door, and emergency exits. This requirement is intended to address issues highlighted by a previous accident where unclear placards contributed to fatalities due to smoke inhalation. The obligations imposed by this directive are clear and specific. Operators must ensure that the exterior operating instruction placards are either modified to meet the standards outlined in Raytheon Aircraft Mandatory Service Bulletin (MSB) 2741, Revision 1, or that new placards are installed following the same guidance. This action must be completed within 200 hours of time in service after the effective date of the directive, which is 28 January 1999. The directive underscores the importance of clear and visible instructions to enhance safety during emergency situations. Compliance is mandatory for the specified models and serial numbers to ensure that emergency procedures can be followed without confusion, thereby reducing the risk of fatalities in critical situations. Failure to comply with the requirements of this directive can result in significant consequences. While the specific penalties for non-compliance are not detailed in the excerpt provided, non-compliance with CASA directives generally can lead to severe penalties under the Civil Aviation Act 1988. These penalties may include fines, suspension or revocation of aircraft certificates, and potential criminal charges if the non-compliance leads to accidents or fatalities. The directive references FAA AD 98-21-20 Amendment 39-10829, which indicates that the requirements are aligned with international safety standards and underscore the importance of adhering to such directives to maintain the highest safety standards in aviation.

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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.