Commonwealth legislation

AD/S-PUMA/34 Amdt 1 - Hoist Arm Lower Fitting Attachment

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive applies to Eurocopter AS 332 C, C1, L and L1 helicopters not modified by AMS 0722955 and requires an inspection of the hoist arm lower‑fitting bolts in accordance with Eurocopter Service Bulletin No. 01.00.58. The inspection must be completed before the next hoisting mission to verify bolt length after a reported bolt failure during load testing, to prevent loss of hoist security.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/S-PUMA/34 Amdt 1 - Hoist Arm Lower Fitting Attachment.

AD/S-PUMA/34 Amdt 1 - Hoist Arm Lower Fitting Attachment

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source
View image in the official source
Eurocopter AS 332 (Super Puma) Series Helicopters

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/S-PUMA/34 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 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.

AD/S-PUMA/34

Amdt 1

Hoist Arm Lower Fitting Attachment 2/2000

Applicability: Models AS 332 C, C1, L and L1 not modified per modification AMS 0722955. Requirement: Inspect in accordance with Eurocopter AS 332 Service Bulletin No. 01.00.58.

Note: DGAC AD 98-487-072(A) R1 refers.

Compliance: Unless already accomplished in accordance with the initial issue of this Directive, before the next hoisting mission after the effective date of this Amendment.

This Amendment becomes effective on 24 February 2000.

Background: During a load test there was a failure of the bolts securing the hoist arm lower fitting. This directive requires checking that the bolts used are the correct length to prevent loss of hoist security during hoist operations.

Amendment 1 reflects the revision status of the DGAC AD, which in turn calls out the definitive Eurocopter Service Bulletin.

The original issue of this Airworthiness Directive became effective on 13 January 1999.

Signature of Eugene Paul Holzapfel Delegate of the Civil Aviation Safety Authority

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 11 January 2000

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 27 January 2000.

Source text

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

1 AD/S-PUMA/34 Amdt 1 - Hoist Arm Lower Fitting Attachment

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

Eurocopter AS 332 (Super Puma) Series Helicopters

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/S-PUMA/34 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 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.

AD/S-PUMA/34

Amdt 1

Hoist Arm Lower Fitting Attachment 2/2000

Applicability: Models AS 332 C, C1, L and L1 not modified per modification AMS 0722955. Requirement: Inspect in accordance with Eurocopter AS 332 Service Bulletin No. 01.00.58.

Note: DGAC AD 98-487-072(A) R1 refers.

Compliance: Unless already accomplished in accordance with the initial issue of this Directive, before the next hoisting mission after the effective date of this Amendment.

This Amendment becomes effective on 24 February 2000.

Amendment 1 reflects the revision status of the DGAC AD, which in turn calls out the definitive Eurocopter Service Bulletin.

The original issue of this Airworthiness Directive became effective on 13 January 1999.

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 11 January 2000

The above AD is notified in the Commonwealth of Australia Gazette on 27 January 2000.