CTHIn ForceLegislation
AD/GC-1/2 Main Landing Gear Retraction System - Inspection
© 2026 Zoe. All rights reserved.
Zoe is a legal information platform. Always consult the Federal Register of Legislation for authoritative text.
AD/GC-1/2 Main Landing Gear Retraction System - Inspection
Start here
Turn the raw legal text into a practical explanation grounded in AD/GC-1/2 Main Landing Gear Retraction System - Inspection.
| AD/GC-1/2 | Main Landing Gear RetractionSystem - Inspection | 18/2020 |
|---|
| Applicability: | All Swift Museum Foundation GC-1A and GC-1B model aircraft. |
|---|---|
| Requirement: | 1. Inspect the main landing gear retraction system to determine that adjustments are as follows:a. When the side brace is against the down stop the middle joint is 1/8 inch to 1/4 inch above dead centre (3/16 inch to 5/16 inch when measured from edges of links in accordance with Globe Customer Service Maintenance Bulletin No. 7, as in force from time to time).b. When the side brace is against the down stop and the down lock plunger is fully extended, covering at least 1/2 of the adjustment screw head, the clearance between the plunger and the screw head is from 0.001 inch to 0.005 inch.c. When the side brace is against the down stop the limit switch plunger is depressed approximately 1/32 inch beyond the cutoff point.d. The turnbuckle in the emergency extension cable is positioned so that on manual extension of the gear, both down locks operate before the handcrank has been wound to the full down position. After it has been determined that the turnbuckle position is satisfactory in this respect it should be determined that with the handcrank wound to the full up position the cable length is sufficient to permit the up limit switches to cut off.Note 1: United States of America Federal Aviation Administration (FAA) AD 47‑06‑01 is the source document for the requirements of this AD.Note 2: The words “as in force from time to time” require compliance with the most recent version of the referenced document. |
| Compliance: | 1. Unless previously accomplished, within 6 months after the commencement date of this AD and thereafter at intervals not to exceed 100 hours’ time in service. |
| This AD commences on 17 September 2020. | |
| Background: | An audit of the Australian Aircraft Register found that Swift Museum Foundation GC-1B aircraft have been on the register for some time and that requirements equivalent to the applicable FAA ADs have not previously been mandated in Australia for these aircraft. |
| This AD is issued to mandate requirements equivalent to FAA AD 47-06-01. |
A drawing of a face Description automatically generated
Pieter van Dijk
Delegate of the Civil Aviation Safety Authority
25 August 2020