AD 80-12-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Nomad TC Pty Ltd | N22B | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes |
| aircraft | Nomad TC Pty Ltd | N24A | Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes |
Unsafe Condition
Loss of horizontal stabilizer trim tab due to failure of the replacement trim tab hinge, part number MS 20001-4.
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Required Actions
Visually inspect and modify the attachment of the right-hand and left-hand trim tab hinges to the horizontal stabilizer in accordance with GAF Nomad Alert Service Bulletin ANMD-27-16 or an FAA-approved equivalent. Aircraft may be flown under FAR 21.197 and 21.199 to a location where the modification can be accomplished.
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Compliance Time
Within the next 25 hours time in service after the effective date of this AD
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Affected Aircraft
GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B (Serial Nos. N22B-5 and up) and N24A (Serial Nos. N24A-42 and up)
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Federal Register Abstract
Trim Tab Hinge
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_80-12-12.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 80-12-12 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes Subject: Trim Tab Hinge Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/26/1980 Make: Nomad TC Pty Ltd Model: N22B | N24A Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 80-12-12 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-3798 AD NUMBER: 80-12-12 SUBJECT HEADING: Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes ACTION: SUMMARY: DATES: Effective June 26, 1980. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 80-12-12 GOVERNMENT AIRCRAFT FACTORIES (GAF): Amendment 39-3798. Applies to Models N22B (Serial Nos. N22B-5 and up) and N24A (Serial Nos. N24A-42 and up), certificated in all categories, which have had a replacement trim tab hinge, P/N MS 20001-4, installed. Compliance required as indicated. To prevent loss of horizontal stabilizer trim tab, accomplish the following: (a) Within the next 25 hours time in service after the effective date of this AD, unless already accomplished, visually inspect and modify, as necessary, the attachment of the right-hand and left-hand trim tab hinge to horizontal stabilizer in accordance with GAF Nomad Alert Service Bulletin ANMD-27-16, dated February 12, 1980, or an FAA-approved equivalent. (b) Aircraft may be flown in accordance with FAR 21.197 and FAR 21.199 to a location where the modification can be accomplished. (c) For purposes of complying with this AD, an FAA-approved equivalent must be approved by the Chief, Engineering and Manufacturing District Office, FAA, Pacific-Asia Region, Honolulu, Hawaii. NOTE: All persons affected by this directive who have not already received these documents from the manufacturer, may obtain copies upon request from the Government Aircraft Factories, 226 Lorimer Street, Port Melbourne, 3207 Vic., Australia. These documents may also be examined at the FAA, Engineering and Manufacturing District Office, 300 Ala Moana Blvd., Room 7321, Honolulu, Hawaii, 96850, and Rules Docket, Room 916, FAA, 800 Independence Avenue, S.W., Washington, D.C. 20591. This amendment becomes effective June 26, 1980. FOOTER:
Document Text
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AD Final Rules - DRS_80-12-12.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 80-12-12 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes Subject: Trim Tab Hinge Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 06/26/1980 Make: Nomad TC Pty Ltd Model: N22B | N24A Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 80-12-12 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-3798 AD NUMBER: 80-12-12 SUBJECT HEADING: Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes ACTION: SUMMARY: DATES: Effective June 26, 1980. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 80-12-12 GOVERNMENT AIRCRAFT FACTORIES (GAF): Amendment 39-3798. Applies to Models N22B (Serial Nos. N22B-5 and up) and N24A (Serial Nos. N24A-42 and up), certificated in all categories, which have had a replacement trim tab hinge, P/N MS 20001-4, installed. Compliance required as indicated. To prevent loss of horizontal stabilizer trim tab, accomplish the following: (a) Within the next 25 hours time in service after the effective date of this AD, unless already accomplished, visually inspect and modify, as necessary, the attachment of the right-hand and left-hand trim tab hinge to horizontal stabilizer in accordance with GAF Nomad Alert Service Bulletin ANMD-27-16, dated February 12, 1980, or an FAA-approved equivalent. (b) Aircraft may be flown in accordance with FAR 21.197 and FAR 21.199 to a location where the modification can be accomplished. (c) For purposes of complying with this AD, an FAA-approved equivalent must be approved by the Chief, Engineering and Manufacturing District Office, FAA, Pacific-Asia Region, Honolulu, Hawaii. NOTE: All persons affected by this directive who have not already received these documents from the manufacturer, may obtain copies upon request from the Government Aircraft Factories, 226 Lorimer Street, Port Melbourne, 3207 Vic., Australia. These documents may also be examined at the FAA, Engineering and Manufacturing District Office, 300 Ala Moana Blvd., Room 7321, Honolulu, Hawaii, 96850, and Rules Docket, Room 916, FAA, 800 Independence Avenue, S.W., Washington, D.C. 20591. This amendment becomes effective June 26, 1980. FOOTER:
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