AD 92-18-10

final rule

Airworthiness Directives; British Aerospace Model ATP Series Airplanes

AD Number
92-18-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
92-NM-34-AD
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited ATP Airworthiness Directives; British Aerospace Model ATP Series Airplanes

Unsafe Condition

Severe structural damage to the airplane due to an internal engine fire within the intercompressor case.

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

Required Actions

Install an intercompressor case (ICC) fire detector system per British Aerospace Service Bulletin ATP-26-5-35225A, revise Section 0.25.0 of the AFM to include Modification No. 35225A, and revise the AFM with operating info via Temporary Revision T/24 Issue 1.

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

Compliance Time

Within 90 days after modification in accordance with Pratt and Whitney Service Bulletin PW100-72-21097, dated November 8, 1991, or within 90 days after the effective date of this AD, whichever occurs later

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

Affected Aircraft

British Aerospace Model ATP series airplanes; serial numbers 2001 through 2045, inclusive; modified per Pratt and Whitney Service Bulletin PW100-72-21097.

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

Federal Register Abstract

Intercompressor Case Fire Detection System ICC

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
92-18-10
Document Type:
AD Final Rules
Docket Number:
92-NM-34-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model ATP Series Airplanes
Subject:
Intercompressor Case Fire Detection System ICC
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/13/1992
Make:
BAE Systems (Operations) Limited
Model:
ATP
Product Type:
Aircraft
Product Subtype:
Large 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Superseded AD: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Superseded By: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: 92-18-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-34-AD

AMENDMENT:   39-8354

AD NUMBER:   92-18-10

SUBJECT HEADING:   Airworthiness Directives; British Aerospace Model ATP Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective on October 13, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-18-10 BRITISH AEROSPACE: Amendment 39-8354. Docket 92-NM-34-AD.
Applicability: Model ATP series airplanes; serial numbers 2001 through 2045, inclusive; which have been modified in accordance with Pratt and Whitney Service Bulletin PW100-72-21097, dated November 8, 1991; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent severe structural damage to the airplane due to an internal engine fire within the intercompressor case, accomplish the following:

(a) Within 90 days after modification in accordance with Pratt and Whitney Service Bulletin PW100-72-21097, dated November 8, 1991, or within 90 days after the effective date of this AD, whichever occurs later:

(1) Install an intercompressor case (ICC) fire detector system, in accordance with British Aerospace Service Bulletin ATP-26-5-35225A, dated October 30, 1991.

(2) Revise Section 0.25.0 of the FAA-approved Airplane Flight Manual (AFM) to include the following statement. This may be accomplished by inserting a copy of this AD in the AFM.

"Modification No.
	
Description

	

35225A
	
Introduction of ICC Fire Detector at the Intercompressor Case."

(3) Revise the FAA-approved AFM to include operating information pertaining to the ICC fire detection systems. This may be accomplished by inserting a copy of Temporary Revision No. T/24, Issue 1, dated February 17, 1992, into the AFM.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) The installation and revision of the AFM shall be done in accordance with Temporary Revision No. T/24, Issue 1, dated February 17, 1992; and British Aerospace Service Bulletin ATP-26-5-35225A, dated October 30, 1991, which contains the following list of effective pages:

Page Number
	
Revision Level
	
Date

1-7, 9, 11, 13,
15, 17, 19, 21,
23, 25, 27, 29,
31, 33, 35, 37,
39, 41, 43	
Original
	
October 30, 1991

		
8, 10, 12, 14, 16,
18, 20, 22, 24, 26,
28, 30, 32, 34, 36,
38, 40, 42	
(These pages are not used)
	
This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, DC 20041-0414. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., Suite 700, Washington, DC.

(e) This amendment becomes effective on October 13, 1992.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_92-18-10.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
92-18-10
Document Type:
AD Final Rules
Docket Number:
92-NM-34-AD
Subject Heading:
Airworthiness Directives; British Aerospace Model ATP Series Airplanes
Subject:
Intercompressor Case Fire Detection System ICC
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
10/13/1992
Make:
BAE Systems (Operations) Limited
Model:
ATP
Product Type:
Aircraft
Product Subtype:
Large 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: 92-18-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-34-AD

AMENDMENT:   39-8354

AD NUMBER:   92-18-10

SUBJECT HEADING:   Airworthiness Directives; British Aerospace Model ATP Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective on October 13, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-18-10 BRITISH AEROSPACE: Amendment 39-8354. Docket 92-NM-34-AD.
Applicability: Model ATP series airplanes; serial numbers 2001 through 2045, inclusive; which have been modified in accordance with Pratt and Whitney Service Bulletin PW100-72-21097, dated November 8, 1991; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent severe structural damage to the airplane due to an internal engine fire within the intercompressor case, accomplish the following:

(a) Within 90 days after modification in accordance with Pratt and Whitney Service Bulletin PW100-72-21097, dated November 8, 1991, or within 90 days after the effective date of this AD, whichever occurs later:

(1) Install an intercompressor case (ICC) fire detector system, in accordance with British Aerospace Service Bulletin ATP-26-5-35225A, dated October 30, 1991.

(2) Revise Section 0.25.0 of the FAA-approved Airplane Flight Manual (AFM) to include the following statement. This may be accomplished by inserting a copy of this AD in the AFM.

"Modification No.
	
Description

	

35225A
	
Introduction of ICC Fire Detector at the Intercompressor Case."

(3) Revise the FAA-approved AFM to include operating information pertaining to the ICC fire detection systems. This may be accomplished by inserting a copy of Temporary Revision No. T/24, Issue 1, dated February 17, 1992, into the AFM.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) The installation and revision of the AFM shall be done in accordance with Temporary Revision No. T/24, Issue 1, dated February 17, 1992; and British Aerospace Service Bulletin ATP-26-5-35225A, dated October 30, 1991, which contains the following list of effective pages:

Page Number
	
Revision Level
	
Date

1-7, 9, 11, 13,
15, 17, 19, 21,
23, 25, 27, 29,
31, 33, 35, 37,
39, 41, 43	
Original
	
October 30, 1991

		
8, 10, 12, 14, 16,
18, 20, 22, 24, 26,
28, 30, 32, 34, 36,
38, 40, 42	
(These pages are not used)
	
This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, DC 20041-0414. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., Suite 700, Washington, DC.

(e) This amendment becomes effective on October 13, 1992.

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.