Commonwealth legislation

AD/B737/137 Amdt 1 - LE Slat Actuator Rod End

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive requires operators of Boeing 737-300/400/500 aeroplanes (line numbers 1001–3132) to carry out the inspection/repair actions set out in FAA AD 2003-03-05 to address fractured leading-edge slat actuator rod ends caused by fatigue. Amendment 1 adds checks for vibro-engraving part markings that create stress risers and shorten rod-end fatigue life. It matters because fractured rod ends can cause uncontrolled slat deployment and reduced aircraft controllability, and operators must follow the FAA/Boeing technical instructions within the stated compliance times.

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Current sections

Direct links to the current provisions in AD/B737/137 Amdt 1 - LE Slat Actuator Rod End.

AD/B737/137 Amdt 1 - LE Slat Actuator Rod End

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source

AIRWORTHINESS DIRECTIVE

View image in the official source

View image in the official source
For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/B737/137 and issues the following 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.

Boeing 737 Series Aeroplanes

AD/B737/137

Amdt 1

LE Slat Actuator Rod End 4/2003

Applicability: Model 737-300, -400, and -500 series aircraft, line numbers 1001 through 3132. Requirement: Action in accordance with the technical requirements of FAA AD 2003-03-05 Amdt

39-13029

Note: Boeing Service Bulletins 737-27A1211, 737-27A1211 Revision 1, 737- 27A1211 Revision 2, and 737-27A1243 refer.

Compliance: As specified in the Requirement document, with a revised effective date of 17 April 2003.

This Amendment becomes effective on 17 April 2003.

Background: The FAA received reports of fractured rods on leading edge slat actuators.

Investigation revealed the rod ends fractured as a result of fatigue cracking. Fractured leading edge slat actuator rod ends could result in uncontrolled deployment of the slat and consequent reduced controllability of the aircraft.

Amendment 1 is issued in response to a new FAA AD which was prompted by

reports indicating that vibro-engraving was found on new rod ends during installation. Such part markings create stress risers that reduce the fatigue life of the rod ends.

The original issue of this Airworthiness Directive became effective on 23 March 2000.

Signature of David Villiers, Delegate of the Civil Aviation Safety Authority.

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 28 February 2003

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 26 March 2003.

Page 1 of 1

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

1 AD/B737/137 Amdt 1 - LE Slat Actuator Rod End

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/B737/137 and issues the following 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.

Boeing 737 Series Aeroplanes

AD/B737/137

Amdt 1

LE Slat Actuator Rod End 4/2003

Applicability: Model 737-300, -400, and -500 series aircraft, line numbers 1001 through 3132. Requirement: Action in accordance with the technical requirements of FAA AD 2003-03-05 Amdt

39-13029

Note: Boeing Service Bulletins 737-27A1211, 737-27A1211 Revision 1, 737- 27A1211 Revision 2, and 737-27A1243 refer.

Compliance: As specified in the Requirement document, with a revised effective date of 17 April 2003.

This Amendment becomes effective on 17 April 2003.

Background: The FAA received reports of fractured rods on leading edge slat actuators.

Amendment 1 is issued in response to a new FAA AD which was prompted by

reports indicating that vibro-engraving was found on new rod ends during installation. Such part markings create stress risers that reduce the fatigue life of the rod ends.

The original issue of this Airworthiness Directive became effective on 23 March 2000.

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 28 February 2003

The above AD is notified in the Commonwealth of Australia Gazette on 26 March 2003.