| AD Number | 85-21-05 | Status | Active |
| Effective Date | November 14, 1985 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-5151 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Nomad TC Pty Ltd |
| Model(s) | N22B N24A |
85-21-05 GOVERNMENT AIRCRAFT FACTORIES (GAF): Amendment 39-5151. Applies to Models N22B and N24A airplanes, (all Serial Numbers) certificated in any category, unless, GAF Service Bulletin (AS/B) ANMD-52-6 dated August 8, 1984, (Mod N627) has been incorporated.
Compliance: Required within 100 hours time-in-service after the effective date of this AD, unless already accomplished.
To prevent restriction of the emergency exit opening, accomplish the following:
(a) Modify the airplane emergency exit door interior trim panel in accordance with Paragraph 2. "Accomplishment Instructions" of GAF Alert Service Bulletin AS/B ANMD-52-6 dated August 8, 1984.
(b) Aircraft may be flown in accordance with Federal Aviation Regulation 21.197 to a location where this AD can be accomplished.
(c) An equivalent method of compliance with this AD, if used, must be approved by the Manager, Western Aircraft Certification Office, ANM-170W, Northwest Mountain Region, FAA, Post OfficeBox 92007, Worldway Postal Center, Los Angeles, California 90009-2007.
All persons affected by this directive may obtain copies of the documents referred to herein upon request to Government Aircraft Factories, 226 Lormier Street, Fisherman's Bend, Port Melbourne, Victoria, Australia 3207, or FAA, Office of Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.
This amendment becomes effective on November 14, 1985.