Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
GAF N22 and N24 Series Aeroplanes
AD/GAF-N22/31 Control Wheel Gimbal Support Structure Tie Rod Attachment Plates - Inspection and Modification
Applicability: All N22 and N24 series aeroplanes. Document: Nomad Alert SB ANMD-27-14. Compliance: Unless already accomplished.
Part A - Before further flight.
1/80
Note: For aircraft maintained in accordance with ANO 100.5.1 Part A of this Directive shall be entered on the maintenance release as maintenance required. The inspection may be performed by the pilot in command, in which certification is not required. In all other cases certification may be made on the maintenance release. This inspection may also be performed and certified by any Licensed Aircraft Maintenance Engineer.
Part B - Before further flight if any obstruction to controls experienced during inspection as per Part A. Otherwise not later than 100 hours time in service after 4 December 1979.
Background: Insufficient clearance may exist between the control wheel retaining bolt and control wheel gimbal bearings support brace.
We try to embed the page this law was scraped from. If the site blocks framing, you still get the link and a local excerpt.
Last checked with source on —
Checking whether the official page can be embedded…
Plain-English simplify of this law: a short summary, key points, and both sides of the argument. Generated on first view via Replicate, then cached. Vote on what helps your study.
No study brief is cached for this law yet. Sign up to generate a plain-English brief.
Sign up to generate