AD/AMD 50/23 - Electronic Flight Instrument System Displays

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

Legislation au F2006B02390 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.

 

AMD Falcon 50 and 900 Series Aeroplanes

 

AD/AMD 50/23 Electronic Flight Instrument System Displays 12/2001

DM

 

Applicability: Mystère Falcon 900 aeroplanes, serial numbers 1 to 178 inclusive, except 169, equipped with an SPZ 8000 avionics system.

 

Requirement: 1. Identify the part numbers and modification status of the Electronic Flight Instrument System (EFIS) Symbol Generators.

 

2.        If, as a result of Requirement 1, the following symbol generators are identified:

 

Symbol Generator

Part Number

Modification Status

SG-820

7007356-901 or -902 or

7007356-903 or -904

 

without Mod S

MG-820

7009289-801 or -802 or

7009289-803 or -804

 

without Mod V

 

  1. Insert Temporary Change No 86 in the Aircraft Flight Manual.

 

b.        Modify the Symbol Generators in accordance with Dassault Aviation Service Bulletin F900-281 dated 21 March 2001.

 

Note: DGAC AD 2001-466-033(B) refers.

 

Compliance: For Requirement 1 - Before 14 November 2001.

 

For Requirement 2.a. - Immediately any of the EFIS Symbol Generators listed in Requirement 2 are identified.

 

For Requirement 2.b. - Within 18 months after the effective date of this Directive. This Airworthiness Directive becomes effective on 17 October 2001.

Background:  The Direction Générale de L’Aviation Civile of France has advised that during certain phases of flight the quantity of data to be processed by the EFIS Symbol Generators may lead to the saturation of the processor’s computing capability. This saturation may result in the EFIS display ether flashing or going off altogether.

 

AMD Falcon 50 and 900 Series Aeroplanes

 

AD/AMD 50/23 (Continued)

 

This Directive initially requires a temporary Flight Manual change that introduces measures designed to decrease the load on the processor, followed by a modification that increases the computing speed of the display processors.


 

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 9 October 2001

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 17 October 2001.

Overview

The Airworthiness Directive (AD) issued under the Civil Aviation Act 1988 aims to ensure the continued airworthiness of specific aircraft within the Australian aviation industry. The Civil Aviation Safety Authority (CASA) issued AD/AMD 50/23 on 9 October 2001 to address an issue identified in Mystère Falcon 900 aeroplanes, serial numbers 1 to 178 inclusive, except 169, equipped with an SPZ 8000 avionics system. This AD responds to concerns raised by the Direction Générale de L’Aviation Civile of France about potential data processing saturation in the Electronic Flight Instrument System (EFIS) Symbol Generators, which could result in display malfunctions during certain phases of flight. The policy objective of this AD is to mitigate the identified unsafe condition by requiring modifications to the aircraft's EFIS Symbol Generators and updating the Aircraft Flight Manual to ensure continued safe operation of the affected aircraft.

Scope and Application

This Airworthiness Directive (AD) applies specifically to Mystère Falcon 900 aeroplanes, serial numbers 1 to 178 inclusive, excluding serial number 169, that are equipped with an SPZ 8000 avionics system. The AD was issued under the authority of the Civil Aviation Safety Authority (CASA) and is effective from 17 October 2001. It requires the identification of the part numbers and modification status of the Electronic Flight Instrument System (EFIS) Symbol Generators, followed by a series of corrective actions if certain specified generators are identified without the required modifications. The corrective actions include inserting a Temporary Change in the Aircraft Flight Manual and modifying the Symbol Generators in accordance with a specified Service Bulletin. These actions must be completed within specified timeframes, with some requirements needing immediate attention and others within 18 months from the effective date of the AD. The directive aims to address an unsafe condition identified in the EFIS Symbol Generators, which can lead to display malfunctions during certain phases of flight.

Key Provisions

The Airworthiness Directive AD/AMD 50/23, issued by the Civil Aviation Safety Authority (CASA) under subregulation 39.1(1) of the Civil Aviation Regulations 1998, applies specifically to Mystère Falcon 900 aeroplanes with serial numbers ranging from 1 to 178, excluding serial number 169, and must be equipped with an SPZ 8000 avionics system (Applicability). This AD mandates that the action set out in the requirement section must be taken in the specified circumstances and according to the instructions set out, by the dates mentioned in the compliance section. The main requirement of the directive is to identify the part numbers and modification status of the Electronic Flight Instrument System (EFIS) Symbol Generators (Requirement 1). If certain Symbol Generators without specific modifications are identified, the directive requires the insertion of Temporary Change No 86 into the Aircraft Flight Manual and the modification of the Symbol Generators in accordance with Dassault Aviation Service Bulletin F900-281 dated 21 March 2001 (Requirement 2). The AD imposes specific obligations on the operators and maintainers of the Mystère Falcon 900 aeroplanes covered by this directive. Firstly, they must identify the part numbers and modification status of the EFIS Symbol Generators before 14 November 2001 (Compliance for Requirement 1). Once the specific Symbol Generators without required modifications are identified, the operators must immediately insert Temporary Change No 86 into the Aircraft Flight Manual (Compliance for Requirement 2.a). Additionally, within 18 months after the effective date of this directive, the operators must modify the Symbol Generators in accordance with the Dassault Aviation Service Bulletin F900-281 (Compliance for Requirement 2.b). Failure to comply with the requirements of this AD may lead to safety issues, including potential processor saturation and subsequent display malfunctions, as identified by the Direction Générale de L’Aviation Civile of France. The AD does not explicitly state any specific offences, penalties, or consequences for non-compliance within the text. However, non-compliance with CASA directives can generally lead to enforcement actions by the CASA, including potential fines, grounding of the aircraft, and other regulatory measures to ensure compliance with aviation safety standards. The severity of the penalties may depend on the nature and extent of the non-compliance, as well as any resulting safety implications.

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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.