AD/CESSNA 188/16 Amdt 1 - Fuselage Lower Longerons
1AD/CESSNA 188/16 Amdt 1 - Fuselage Lower Longerons
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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 Cessna 188 (Agwagon) Series Aeroplanes
AD/CESSNA 188/16
Amdt 1
Fuselage Lower Longerons 11/86
Applicability: All models A188 excluding those with an aircraft serial number with a “T” suffix and those which have been modified in accordance with a scheme approved by the Secretary.
Requirement: Inspect the fuselage lower longerons for cracks in the vicinity of the main landing gear supports.
Compliance: Within 100 hours time in service for all aeroplanes with more than 1500 hours total time in service and thereafter at intervals not exceeding 500 hours time in service, after 1 September 1971.
Background: This amendment distinguishes between the configuration differences of the “Agwagon” and the “Agtruck” aircraft.