AD 92-04-03

final rule

Airworthiness Directives; BOEING Model 747 Series Airplanes

AD Number
92-04-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-100B Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-100B SUD Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200B Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200C Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-200F Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-300 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400 Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400D Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747-400F Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747SP Series Airworthiness Directives; BOEING Model 747 Series Airplanes
aircraft The Boeing Company 747SR Series Airworthiness Directives; BOEING Model 747 Series Airplanes

Unsafe Condition

The passenger oxygen system may not activate at the proper altitude due to potential failure of the flow control units.

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

Required Actions

Inspect flow control units to determine serial numbers. Replace units listed in Table 1 of Boeing Service Bulletin 747-35-2074 if not previously reworked, followed by low pressure leak check and simulated automatic actuation test. Units not listed in Table 1 or already reworked require no further action.

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

Compliance Time

within the next 4,000 flight hours after the effective date of this AD, unless accomplished previously

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

Affected Aircraft

Boeing Model 747 series airplanes listed in Boeing Service Bulletin 747-35-2074, dated June 27, 1991

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

Federal Register Abstract

Passenger Oxygen System

Applicability Source Text

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AD Final Rules - DRS_92-04-03.html
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AD Number:
92-04-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BOEING Model 747 Series Airplanes
Subject:
Passenger Oxygen System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/16/1992
Make:
The Boeing Company
Model:
747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 92-04-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-8172

AD NUMBER:   92-04-03

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 16, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-04-03 BOEING: Amendment 39-8172. Docket 91-NM-176-AD.

Applicability: Model 747 series airplanes, as listed in Boeing Service Bulletin 747-35- 2074, dated June 27, 1991, certificated in any category.

Compliance: Required within the next 4,000 flight hours after the effective date of this AD, unless accomplished previously.

To ensure that the passenger oxygen system activates at the proper altitude, accomplish the following:

(a) Inspect the flow control units to determine the serial numbers, in accordance with Boeing Service Bulletin 747-35-2074, Revision 1, dated December 12, 1991.

(1) If the flow control unit serial number is listed in Table 1 of the service bulletin and the unit has not been reworked, prior to further flight, replace the unit and perform a low pressure leak check and a simulated automatic actuation test, in accordance with paragraph III.C. of the Accomplishment Instructions of the service bulletin.

(2) If the flow control unit serial number is not listed in Table 1 of the service bulletin, or if the unit has been reworked in accordance with paragraph III.C. of the Accomplishment Instructions of the service bulletin, no further action is necessary.

(b) An alternative method 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 forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO.

(c) 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.

(d) The inspection, replacement, check, and test required by this AD shall be done in accordance with Boeing Service Bulletin 747-35-2074, Revision 1, dated December 12, 1991. 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 Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC.

(e) This amendment (39-8172, AD 92-04-03) becomes effective on March 16, 1992.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_92-04-03.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
92-04-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BOEING Model 747 Series Airplanes
Subject:
Passenger Oxygen System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/16/1992
Make:
The Boeing Company
Model:
747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 92-04-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-8172

AD NUMBER:   92-04-03

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 16, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-04-03 BOEING: Amendment 39-8172. Docket 91-NM-176-AD.

Applicability: Model 747 series airplanes, as listed in Boeing Service Bulletin 747-35- 2074, dated June 27, 1991, certificated in any category.

Compliance: Required within the next 4,000 flight hours after the effective date of this AD, unless accomplished previously.

To ensure that the passenger oxygen system activates at the proper altitude, accomplish the following:

(a) Inspect the flow control units to determine the serial numbers, in accordance with Boeing Service Bulletin 747-35-2074, Revision 1, dated December 12, 1991.

(1) If the flow control unit serial number is listed in Table 1 of the service bulletin and the unit has not been reworked, prior to further flight, replace the unit and perform a low pressure leak check and a simulated automatic actuation test, in accordance with paragraph III.C. of the Accomplishment Instructions of the service bulletin.

(2) If the flow control unit serial number is not listed in Table 1 of the service bulletin, or if the unit has been reworked in accordance with paragraph III.C. of the Accomplishment Instructions of the service bulletin, no further action is necessary.

(b) An alternative method 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 forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO.

(c) 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.

(d) The inspection, replacement, check, and test required by this AD shall be done in accordance with Boeing Service Bulletin 747-35-2074, Revision 1, dated December 12, 1991. 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 Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at the Office of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC.

(e) This amendment (39-8172, AD 92-04-03) becomes effective on March 16, 1992.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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