AD/ENST 28/7 Amdt 1 - Main Rotor Transmission Attachment Bolts - Inspection and Replacement
1AD/ENST 28/7 Amdt 1 - Main Rotor Transmission Attachment Bolts - Inspection and Replacement
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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 Enstrom F-28 Series Helicopters
AD/ENST 28/7
Amdt 1
Applicability: All models.
Main Rotor Transmission Attachment Bolts - Inspection and Replacement
4/77
Requirement: 1. Inspect the 4 bolts attaching the main rotor transmission assembly to the fuselage frame for a torque preloading of 100-110 inch pounds.
- Modify the attachment of the main rotor transmission assembly to fuselage attachment as per Enstrom Service Information Letter No. 0057.
Compliance: For Para. 1: At intervals not exceeding 50 hours time in service until modified and then once only within 100 hours time in service after modification as per SIL No. 0057.
For Para. 2: Modify within 300 hours time in service after 1 June 1977.