AD/GAF-N22/12 Amdt 1 - Rudder Control System - 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
GAF N22 and N24 Series Aeroplanes
AD/GAF-N22/12
Amdt 1
Rudder Control System - Inspection and Modification
4/77
Applicability: All models N22 and N22B with S/Nos. as listed in SB No. N22.27.7.
Requirement: 1. Inspect the mounting of the rudder pulley bracket at FUS. STA. 67.95 in accordance with GAF ALERT SB No. N22.27.6.
- Modify the mounting of the rudder pulley bracket at FUS. STA. 67.95 and affix towbar maximum deflection indication in accordance with GAF SB No. N22.27.7.
Note 1: Flight restrictions referred to in Alert SB Telex N22.27.5 must be adhered to until compliance with para. 2 is completed.
Note 2: Incorporation of MODIFICATION N137 is an acceptable means of compliance with para. 2.
Compliance: 1. Within 50 hours time in service after 24 December 1976 and thereafter at intervals not exceeding 50 hours time in service until modified.
- Within 200 hours time in service after 1 April 1977.