AD/HU 269/62 Amdt 1 - Tail Rotor Hub - Inspection and Modification
1AD/HU 269/62 Amdt 1 - Tail Rotor Hub - Inspection and Modification
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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 Schweizer (Hughes) 269 Series Helicopters
AD/HU 269/62
Amdt 1
Tail Rotor Hub - Inspection and Modification 3/82
Applicability: All model 269C with S/Nos. 0004 to 0716.
All model 269A, TH-55A, 269A-1 and 269B with LTS tail rotor assembly P/N 269A6034 Series.
All P/N 369A1725and 369A1725-501 tail rotor hub assemblies. All P/N 369A1725-5 tail rotor assemblies with S/Nos. 001 to 862.
Document: Hughes SIN No. N-153.1.
Compliance: Within 100 hours time in service after 31 March, 1982.
Background: Manufacturer’s SI Notice Revision 1 extends part number effectivity.