AD 90-26-02

final rule

Airworthiness Directives; BOEING Model 747-400 Series Airplanes

AD Number
90-26-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-244-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-400 Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes
aircraft The Boeing Company 747-400D Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes
aircraft The Boeing Company 747-400F Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes
aircraft The Boeing Company 767-200 Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes
aircraft The Boeing Company 767-300 Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes
aircraft The Boeing Company 767-300F Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes
aircraft The Boeing Company 767-400ER Series Airworthiness Directives; BOEING Model 747-400 Series Airplanes

Unsafe Condition

Insufficient cargo fire protection, which could result in significant damage to the airplane in the event of a cargo compartment fire.

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

Required Actions

Inspect cargo compartment fire extinguisher orifices in accordance with specified Boeing Alert Service Bulletins. Replace with correct part if part number does not match specified numbers in the service bulletins. Submit a report of findings within 10 days after inspection if discrepancies are found.

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

Compliance Time

Within 30 days after October 1, 1990 (for Model 747-400 series and Model 767-300 series forward cargo compartments) or within 30 days after the effective date of this amendment (for other Model 767 series).

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

Affected Aircraft

Boeing Model 747-400 Series, 747-400D Series, 747-400F Series, 767-200 Series, 767-300 Series, 767-300F Series airplanes listed in Boeing Alert Service Bulletins 747-26A2170 and 767-26A0068 (Revision 1).

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

Federal Register Abstract

Cargo Compartment Fire Extinguisher

Applicability Source Text

Show captured applicability text from the source AD
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AD Number:
90-26-02
Document Type:
AD Final Rules
Docket Number:
90-NM-244-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747-400 Series Airplanes
Subject:
Cargo Compartment Fire Extinguisher
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/27/1990
Make:
The Boeing Company
Model:
747-400 Series | 747-400D Series | 747-400F Series | 767-200 Series | 767-300 Series | 767-300F Seri...Show more
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:
4/21/2010 - The RGL applicability has been updated to include Boeing 767 series; NCR 8651
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-26-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-244-AD

AMENDMENT:   39-6829

AD NUMBER:   90-26-02

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747-400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 27, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-26-02 BOEING: Amendment 39-6829. Docket No. 90-NM-244-AD.

Applicability: Model 747-400 series airplanes listed in Boeing Alert Service Bulletin 747-26A2170, dated July 5, 1990; and Model 767 series airplanes listed in Boeing Alert Service Bulletin 767-26A0068, Revision 1, dated September 18, 1990; certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent insufficient cargo fire protection, which could result in significant damage to the airplane in the event of a cargo compartment fire, accomplish the following:

A. For Model 747-400 series airplanes, within 30 days after October 1, 1990 (the effective date of Amendment 39-6736, AD 90-19-11), inspect the cargo compartment fire extinguisher orifices in accordance with Boeing Alert Service Bulletin 747-26A2170, dated July 5, 1990. If the part number does not match any number specified as the correct number in the service bulletin, prior to further flight with cargo in that compartment, replace with a correct part.

B. For Model 767-300 series airplanes listed in Boeing Alert Service Bulletin 767- 26A0068, dated July 5, 1990:

1. Within 30 days after October 1, 1990 (the effective date of Amendment 39-6736, AD 90-19-11), inspect the forward cargo compartment fire extinguisher orifices to determine the part number installed, in accordance with Boeing Alert Service Bulletin 767- 26A0068, dated July 5, 1990. If the part number does not match any number specified as the correct number in that service bulletin, prior to further flight with cargo in that compartment, replace with a correct part.

2. Within 30 days after the effective date of this amendment, inspect the aft cargo compartment fire extinguisher orifices to determine the part number installed, in accordance with Boeing Alert Service Bulletin 767-26A0068, Revision 1, dated September 18, 1990. If the part number does not match any number specified as the correct number in that service bulletin, prior to further flight with cargo in that compartment, replace with a correct part.

C. For Model 767 series airplanes listed in Boeing Alert Service Bulletin 767- 26A0068, Revision 1, dated September 18, 1990, other than those that are subject to paragraph B. of this AD, within 30 days after the effective date of this amendment, inspect the cargo compartment fire extinguisher orifices to determine the part number installed, in accordance with that service bulletin. If the part number in the service bulletin does not match any number specified as the correct number in the service bulletin, prior to further flight with cargo in that compartment, replace with a correct part.

D. Within 10 days after the inspection required by paragraph A., B., or C. of this AD, if configuration discrepancies are discovered, submit a report of findings to the Manager, Seattle Manufacturing Inspection District Office, ANM-108S, FAA, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington 98055-4056. The report must include the airplane serial number.

E. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO.

F. 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.

All persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington.

Airworthiness Directive 90-26-02 supersedes AD 90-19-11, Amendment 39-6736.
This amendment (39-6829, AD 90-26-02) becomes effective on December 27, 1990.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-26-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-26-02
Document Type:
AD Final Rules
Docket Number:
90-NM-244-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747-400 Series Airplanes
Subject:
Cargo Compartment Fire Extinguisher
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/27/1990
Make:
The Boeing Company
Model:
747-400 Series | 747-400D Series | 747-400F Series | 767-200 Series | 767-300 Series | 767-300F Seri...Show more
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:
4/21/2010 - The RGL applicability has been updated to include Boeing 767 series; NCR 8651
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-26-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-244-AD

AMENDMENT:   39-6829

AD NUMBER:   90-26-02

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747-400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 27, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-26-02 BOEING: Amendment 39-6829. Docket No. 90-NM-244-AD.

Applicability: Model 747-400 series airplanes listed in Boeing Alert Service Bulletin 747-26A2170, dated July 5, 1990; and Model 767 series airplanes listed in Boeing Alert Service Bulletin 767-26A0068, Revision 1, dated September 18, 1990; certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent insufficient cargo fire protection, which could result in significant damage to the airplane in the event of a cargo compartment fire, accomplish the following:

A. For Model 747-400 series airplanes, within 30 days after October 1, 1990 (the effective date of Amendment 39-6736, AD 90-19-11), inspect the cargo compartment fire extinguisher orifices in accordance with Boeing Alert Service Bulletin 747-26A2170, dated July 5, 1990. If the part number does not match any number specified as the correct number in the service bulletin, prior to further flight with cargo in that compartment, replace with a correct part.

B. For Model 767-300 series airplanes listed in Boeing Alert Service Bulletin 767- 26A0068, dated July 5, 1990:

1. Within 30 days after October 1, 1990 (the effective date of Amendment 39-6736, AD 90-19-11), inspect the forward cargo compartment fire extinguisher orifices to determine the part number installed, in accordance with Boeing Alert Service Bulletin 767- 26A0068, dated July 5, 1990. If the part number does not match any number specified as the correct number in that service bulletin, prior to further flight with cargo in that compartment, replace with a correct part.

2. Within 30 days after the effective date of this amendment, inspect the aft cargo compartment fire extinguisher orifices to determine the part number installed, in accordance with Boeing Alert Service Bulletin 767-26A0068, Revision 1, dated September 18, 1990. If the part number does not match any number specified as the correct number in that service bulletin, prior to further flight with cargo in that compartment, replace with a correct part.

C. For Model 767 series airplanes listed in Boeing Alert Service Bulletin 767- 26A0068, Revision 1, dated September 18, 1990, other than those that are subject to paragraph B. of this AD, within 30 days after the effective date of this amendment, inspect the cargo compartment fire extinguisher orifices to determine the part number installed, in accordance with that service bulletin. If the part number in the service bulletin does not match any number specified as the correct number in the service bulletin, prior to further flight with cargo in that compartment, replace with a correct part.

D. Within 10 days after the inspection required by paragraph A., B., or C. of this AD, if configuration discrepancies are discovered, submit a report of findings to the Manager, Seattle Manufacturing Inspection District Office, ANM-108S, FAA, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington 98055-4056. The report must include the airplane serial number.

E. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO.

F. 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.

All persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington.

Airworthiness Directive 90-26-02 supersedes AD 90-19-11, Amendment 39-6736.
This amendment (39-6829, AD 90-26-02) becomes effective on December 27, 1990.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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