AD/ROCK-114/11 - Rudder Rib Inspection
1AD/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
Image unavailable in extracted text 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.