AD 91-02-08

final rule

Airworthiness Directives; AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD. Models N22B, N22S, and N24A Airplanes

AD Number
91-02-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-CE-15-AD
FR Citation
This information is not available.
Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

Applicability

TypeManufacturerModelDetails
aircraft Nomad TC Pty Ltd N22B Airworthiness Directives; AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD. Models N22B, N22S, and N24A Airplanes
aircraft Nomad TC Pty Ltd N22S Airworthiness Directives; AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD. Models N22B, N22S, and N24A Airplanes
aircraft Nomad TC Pty Ltd N24A Airworthiness Directives; AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD. Models N22B, N22S, and N24A Airplanes

Unsafe Condition

Overheating of the terminal lugs connected to the generator cables at the wing leading edge engine firewall.

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

Required Actions

Modify the airplane electrical system using Nomad Modification No. N724 in accordance with Part 3 of Nomad Alert Service Bulletin ANMD-24-5, Revision 1. Special flight permits may be issued under FAR 21.197 and 21.199 to operate to a base for compliance. Alternate methods of compliance or adjustments may be approved by the FAA.

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

Compliance Time

within the next 100 hours time-in-service after the effective date of this AD

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

Affected Aircraft

Nomad Models N22B, N22S, and N24A airplanes (all serial numbers), certificated in any category.

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

Federal Register Abstract

Airplane Electrical System

Applicability Source Text

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AD Number:
91-02-08
Document Type:
AD Final Rules
Docket Number:
90-CE-15-AD
Subject Heading:
Airworthiness Directives; AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD. Models N22B, N22S, and N24A Airplanes
Subject:
Airplane Electrical System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/07/1991
Make:
Nomad TC Pty Ltd
Model:
N22B | N22S | 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: 91-02-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-CE-15-AD

AMENDMENT:   39-6842

AD NUMBER:   91-02-08

SUBJECT HEADING:   Airworthiness Directives; AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD. Models N22B, N22S, and N24A Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 7, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-02-08 AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD.: Amendment 39-6842. Docket No. 90-CE-15-AD.

Applicability: Nomad Models N22B, N22S, and N24A airplanes (all serial numbers), certificated in any category.

Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent overheating of the terminal lugs connected to the generator cables at the wing leading edge engine firewall, accomplish the following:

(a) Modify the airplane electrical system using Nomad Modification No. N724, in accordance with the instructions in Part 3 of Nomad Alert Service Bulletin ANMD-24-5, Revision 1, dated August 4, 1989.

(b) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

(c) An alternate method of compliance or adjustment to the compliance time that provides an equivalent level of safety may be approved by the Manager, FAA, Northwest Mountain Region, Los Angeles Aircraft Certification Office, 3229 E. Spring Street, Long Beach, California 90806-2425. The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, FAA, Northwest Mountain Region, Los Angeles Aircraft Certification Office.

(d) All persons affected by this directive may obtain copies of the document referred to herein upon request to Aerospace Technologies of Australia Pty, Ltd., 226 Lorimer Street, Port Melbourne, Victoria 3207, Australia; Telephone 9-011-61-62-68-4142; or may examine this document at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106.

This amendment (39-6842, AD 91-02-08) becomes effective on February 7, 1991.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_91-02-08.html
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Document Versions
 Feedback
Details
AD Number:
91-02-08
Document Type:
AD Final Rules
Docket Number:
90-CE-15-AD
Subject Heading:
Airworthiness Directives; AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD. Models N22B, N22S, and N24A Airplanes
Subject:
Airplane Electrical System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/07/1991
Make:
Nomad TC Pty Ltd
Model:
N22B | N22S | 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: 91-02-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-CE-15-AD

AMENDMENT:   39-6842

AD NUMBER:   91-02-08

SUBJECT HEADING:   Airworthiness Directives; AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD. Models N22B, N22S, and N24A Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 7, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-02-08 AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD.: Amendment 39-6842. Docket No. 90-CE-15-AD.

Applicability: Nomad Models N22B, N22S, and N24A airplanes (all serial numbers), certificated in any category.

Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent overheating of the terminal lugs connected to the generator cables at the wing leading edge engine firewall, accomplish the following:

(a) Modify the airplane electrical system using Nomad Modification No. N724, in accordance with the instructions in Part 3 of Nomad Alert Service Bulletin ANMD-24-5, Revision 1, dated August 4, 1989.

(b) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

(c) An alternate method of compliance or adjustment to the compliance time that provides an equivalent level of safety may be approved by the Manager, FAA, Northwest Mountain Region, Los Angeles Aircraft Certification Office, 3229 E. Spring Street, Long Beach, California 90806-2425. The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, FAA, Northwest Mountain Region, Los Angeles Aircraft Certification Office.

(d) All persons affected by this directive may obtain copies of the document referred to herein upon request to Aerospace Technologies of Australia Pty, Ltd., 226 Lorimer Street, Port Melbourne, Victoria 3207, Australia; Telephone 9-011-61-62-68-4142; or may examine this document at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106.

This amendment (39-6842, AD 91-02-08) becomes effective on February 7, 1991.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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