Commonwealth legislation

AD/ROCK-114/11 - Rudder Rib 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This Act has been repealed and is no longer in force. It is retained for historical reference.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

2/10 complexity

Owners/operators of Gulfstream/Rockwell Model 114 aircraft (serials 14000–14500) must inspect the rudder tip rib around the balance-weight attachment hole for cracks, following Gulfstream American Service Bulletin SB 114‑20.

If not inspected within the last 100 flight hours, inspect before next flight and repeat every 100 hours until the required Part II repair/modification is done—cracks could weaken the rudder and risk loss of control.

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Current sections

Direct links to the current provisions in AD/ROCK-114/11 - Rudder Rib Inspection.

AD/ROCK-114/11 - Rudder Rib 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-114/11 Rudder Rib Inspection 2/82

Applicability: All model 114 with S/Nos. 14000 to 14500. Document: Gulfstream American SB No. SB 114-20.

Compliance: Unless already accomplished within the last 100 hours time in service inspect in accordance with Part 1 before further flight and thereafter at intervals not exceeding 100 hours time in service until Part II is accomplished.

Background: In service reports of cracks in rudder tip rib at balance weight attachment hole have been received by the manufacturer.

Source text

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