AD/RAD/82 - Prevent GPS Navigation unit from Providing Erroneous Cross-Deviation

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Legislation au F2006B06537 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 CASR 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.


 

Radio Communication and Navigation Equipment

 

AD/RAD/82 Prevent GPS Navigation unit from Providing

Erroneous Cross-Deviation


9/2004

 

 

Applicability: Garmin AT, formerly UPS Aviation Technologies, Apollo GX50/55/60/65 TSO- C129a global positioning system (GPS) navigation units as listed below with software versions 3.0 through 3.4 inclusive:

 

Model

Part Number

Description

Modification Level

GX50

430-6050-400

Approach Certified GPS

With any of the following mods:

(H), (N), (P), (T) or (U);

prior to (V)

 

430-6050-401

Approach Certified GPS

Prior to (V)

 

430-5060-402

Approach Certified GPS

Prior to (V)

GX55

430-6050-200

Enroute/Terminal Certified GPS

With any of the following mods:

(E), (J), (K), (M) or (N);

prior to (R):

 

430-6050-201

Enroute/Terminal Certified GPS

With any of the following mods:

(E), (J), (K), (M) or (N);

prior to (R)

 

430-6050-202

Enroute/Terminal Certified GPS

Prior to (R)

 

430-6050-203

Enroute/Terminal Certified GPS

Prior to (R)

 

GX60

430-6050-600

Approach Certified

GPS/COM

With any of the following

mods:

 

 

 

(H), (N), (S), (AB) or

(AC);prior to (AE)

 

430-6050-601

Approach Certified GPS/COM

With any of the following mods:

(H), (N), (S), (AB) or (AC);

prior to (AE)

 

430-6050-602

Approach Certified GPS/COM

Prior to (AE)

 

430-6050-603

Approach Certified GPS/COM

Prior to (AE)

 

430-6050-604

Approach Certified GPS/COM

Prior to (AE)

GX65

430-6050-800

Enroute/Terminal Certified GPS/COM

With any of the following mods:

(F), (L), (P), (Y) or (AA);

prior to (AC)

 

430-6050-801

Enroute/Terminal Certified GPS/COM

With any of the following mods:

(F), (L), (P), (Y) or (AA);

prior to (AC):

 

430-6050-802

Enroute/Terminal Certified GPS/COM

Prior to (AC)

 

430-6050-803

Enroute/Terminal Certified GPS/COM

Prior to (AC)

 

430-6050-804

Enroute/Terminal Certified GPS/COM

Prior to (AC)

 

Note 1: The above table was sourced from UPS Aviation Technologies Service Bulletin 561-4002-001, dated 19 April 2002, which was referenced in FAA AD 2004- 13-20 and the certification in the table refers to the FAA TSO C-129a class of the unit.

 

Requirement: 1. Modify and test the software for the Apollo GX50/55/60/65 TSO-C129a GPS navigation unit by accomplishing all of the actions specified in paragraphs 3.B. and 3.C. of Service Bulletin (SB) 561-4002-001, dated 19 April 2002.

 

2. Reidentify the modified Apollo GX50/55/60/65 TSO-C129a GPS navigation unit, according to paragraph 3.D. of SB 561-4002-001.

 

Note 2: FAA AD 2004-13-20 Amdt 39-13702 refers.

 

Compliance: For Requirement 1 - Within six months after the effective date of this Directive.

 

For Requirement 2 - Immediately following completion of Requirement 1. This Airworthiness Directive becomes effective on 2 September 2004.

Background: The United States Federal Aviation Administration (FAA) has advised that, under certain conditions, Garmin AT, Apollo GX series GPS navigation units with software versions 3.0 to 3.4 may provide erroneous cross-deviation information, which could result in the aircraft deviating from its intended course for a brief period of time. This erroneous information may place an excessive workload on the flightcrew while they monitor other available navigation data to avoid deviating off course.

 

To prevent the GPS unit from providing erroneous information, this Directive requires modification and testing of the software for the GPS navigation units.


Bernard Malcolm Hole

Delegate of the Civil Aviation Safety Authority 20 July 2004

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 11 August 2004.

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