AD/G164/18 Amdt 1 - Aileron Bellcrank - Inspection and Modification
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
View image in the official source
Schweizer (Grumman) G-164 (Ag-Cat) Series Aeroplanes
AD/G164/18
Amdt 1
Aileron Bellcrank - Inspection and Modification 8/82
Applicability: All models G-164B with S/Nos. 1B to 656B; G164C with S/Nos. 1C to 44C;
G-164D with S/Nos. 1D to 16D.
Document: Gulfstream American AG-CAT SB No. 75 Revision A.
Note: FAA AD 82-13-06 refers.
Compliance: 1. Unless already accomplished, inspect initially within 100 hours time in service after 31 August 1982, and thereafter at intervals of 300 hours time in service until modified.
- If excessive elongation is found during inspection, modify or replace the bellcrank before further flight.
Background: Conditions continue to exist whereby failure of the aileron cable attachment at the LH and RH aileron bellcrank assemblies may occur.