AD 85-21-05

final rule

Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes

AD Number
85-21-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
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

Restriction of the emergency exit opening due to improper modification of the emergency exit door interior trim panel.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Modify the emergency exit door interior trim panel per GAF Alert Service Bulletin AS/B ANMD-52-6 dated August 8, 1984. Aircraft may be flown under FAR 21.197 to a location where this AD can be accomplished. Equivalent compliance methods must be approved by the FAA.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within 100 hours time-in-service after the effective date of this AD, unless already accomplished

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A airplanes (all Serial Numbers)

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Emergency Exit Door Trim

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_85-21-05.html
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Details
AD Number:
85-21-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes
Subject:
Emergency Exit Door Trim
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/14/1985
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Superseded AD: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Superseded By: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: 85-21-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5151

AD NUMBER:   85-21-05

SUBJECT HEADING:   Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 14, 1985.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
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 Office Box 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.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_85-21-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
85-21-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes
Subject:
Emergency Exit Door Trim
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/14/1985
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: 85-21-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5151

AD NUMBER:   85-21-05

SUBJECT HEADING:   Airworthiness Directives; GOVERNMENT AIRCRAFT FACTORIES (GAF) Models N22B and N24A Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective November 14, 1985.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
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 Office Box 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.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.