Commonwealth legislation

AD/ROCK-114/2A - Aileron Hinge Supports - Inspection

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive orders owners of Rockwell/Gulfstream 114 aircraft (S/N 14000–14376) to inspect aileron hinge supports immediately using Rockwell SB-114-14A and to have the pilot perform a visual hinge check before every flight until the permanent modification is done.

The permanent fix required by Part 2 of the Service Bulletin must be carried out within 100 flight hours after 15 August 1978 to prevent possible loss of control.

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Current sections

Direct links to the current provisions in AD/ROCK-114/2A - Aileron Hinge Supports - Inspection.

AD/ROCK-114/2A - Aileron Hinge Supports - Inspection

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Gulfstream (Rockwell) 114 Series Aeroplanes

AD/ROCK-114/2A Aileron Hinge Supports - Inspection 7/78

Applicability: All model 114 aeroplanes with S/Nos. 14000 to 14376. Document: Rockwell International SB No. SB-114-14A.

Compliance: 1. Unless already accomplished as per SB No. 114-14, initially inspect before further flight as per Part 1 of SB No. 114-14A and perform external visual inspection before each subsequent flight until modified.

Note: Pilot in command may perform and certify for visual inspection.

Unless already accomplished as per SB No. 114-14 modify as per Part 2 of SB No. 114-14A within 100 hours time in service after 15 August 1978.

Source text

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