AD 92-25-04

final rule

Airworthiness Directives; BOEING Model 737 Series Airplanes

AD Number
92-25-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
92-NM-108-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 737-100 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 737-200 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 737-200C Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 737-300 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 737-400 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 737-500 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 737-600 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 737-700 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 737-800 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 757-200 Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 757-200CB Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 757-200PF Series Airworthiness Directives; BOEING Model 737 Series Airplanes
aircraft The Boeing Company 757-300 Series Airworthiness Directives; BOEING Model 737 Series Airplanes

Unsafe Condition

Maintenance test stop plungers may interfere with proper deployment of oxygen masks.

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

Required Actions

Modify the test stop plungers in oxygen box assemblies in lavatories and modular lavatory 'A' per Boeing Service Bulletins 737-35A1037 and 737-35A1038. Alternative methods may be used if approved by FAA PMI.

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

Compliance Time

Within 900 flight hours or 6 months 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

Boeing Model 737 series airplanes listed in Boeing Alert Service Bulletins 737-35A1037 and 737-35A1038, and Model 757 series listed in 757-35A0010.

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

Federal Register Abstract

Test Stop Plungers

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_92-25-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
92-25-04
Document Type:
AD Final Rules
Docket Number:
92-NM-108-AD
Subject Heading:
Airworthiness Directives; BOEING Model 737 Series Airplanes
Subject:
Test Stop Plungers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/23/1992
Make:
The Boeing Company
Model:
737-100 Series | 737-200 Series | 737-200C Series | 737-300 Series | 737-400 Series | 737-500 Series...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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 92-25-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-108-AD

AMENDMENT:   39-8419

AD NUMBER:   92-25-04

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 737 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 23, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-25-04 BOEING: Amendment 39-8419. Docket No. 92-NM-108-AD.

Applicability: Model 737 series airplanes, as listed in Boeing Alert Service Bulletin 737- 35A1037, dated February 13, 1992, and Boeing Alert Service Bulletin 737-35A1038, dated March 19, 1992; and Model 757 series airplanes, as listed in Boeing Alert Service Bulletin 757- 35A0010, dated February 13, 1992; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent maintenance test stop plungers from interfering with proper deployment of oxygen masks, accomplish the following:

(a) For Model 737 series airplanes: Within 900 flight hours or 6 months after the effective date of this AD, whichever occurs later, accomplish the requirements of paragraphs (a)(1) and (a)(2) of this AD.

(1) Modify the test stop plungers in the oxygen box assemblies in the lavatories in accordance with Boeing Alert Service Bulletin 737-35A1037, dated February 13, 1992.

(i) As an alternative action, operators may accomplish the modification of the test stop with the oxygen box assembly removed from the airplane.

(ii) In lieu of the method for reidentification of the test stop prescribed in the service bulletin, operators may use an alternative method of reidentification if it is approved by the cognizant FAA Principal Maintenance Inspector (PMI).

(2) Modify the oxygen box assemblies in modular lavatory "A" in accordance with Boeing Alert Service Bulletin 737-35A1038, dated March 19, 1992.

(b) For Model 757 series airplanes: Within 900 flight hours or 6 months after the effective date of this AD, whichever occurs later, modify the test stop plungers in the oxygen box assemblies in the lavatories and at doors 1 and 4 flight attendant seats in accordance with Boeing Alert Service Bulletin 757-35A0010, dated February 13, 1992.

(1) As an alternative action, operators may accomplish the modification of the test stop with the oxygen box assembly removed from the airplane.

(2) In lieu of the method for reidentification of the test stop prescribed in the service bulletin, operators may use an alternative method of reidentification if it is approved by the cognizant FAA Principal Maintenance Inspector (PMI).

(c) 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, Seattle Aircraft Certification Office (ACO), 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, Seattle ACO.

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

(d) 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.

(e) The modifications shall be done in accordance with Boeing Alert Service Bulletin 737-35A1037, dated February 13, 1992; Boeing Alert Service Bulletin 737-35A1038, dated March 19, 1992; or Boeing Alert Service Bulletin 757-35A0010, dated February 13, 1992; as applicable. 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, 800 North Capitol Street, NW., suite 700, Washington, DC.

(f) This amendment becomes effective on December 23, 1992.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_92-25-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
92-25-04
Document Type:
AD Final Rules
Docket Number:
92-NM-108-AD
Subject Heading:
Airworthiness Directives; BOEING Model 737 Series Airplanes
Subject:
Test Stop Plungers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/23/1992
Make:
The Boeing Company
Model:
737-100 Series | 737-200 Series | 737-200C Series | 737-300 Series | 737-400 Series | 737-500 Series...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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 92-25-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   92-NM-108-AD

AMENDMENT:   39-8419

AD NUMBER:   92-25-04

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 737 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 23, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-25-04 BOEING: Amendment 39-8419. Docket No. 92-NM-108-AD.

Applicability: Model 737 series airplanes, as listed in Boeing Alert Service Bulletin 737- 35A1037, dated February 13, 1992, and Boeing Alert Service Bulletin 737-35A1038, dated March 19, 1992; and Model 757 series airplanes, as listed in Boeing Alert Service Bulletin 757- 35A0010, dated February 13, 1992; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent maintenance test stop plungers from interfering with proper deployment of oxygen masks, accomplish the following:

(a) For Model 737 series airplanes: Within 900 flight hours or 6 months after the effective date of this AD, whichever occurs later, accomplish the requirements of paragraphs (a)(1) and (a)(2) of this AD.

(1) Modify the test stop plungers in the oxygen box assemblies in the lavatories in accordance with Boeing Alert Service Bulletin 737-35A1037, dated February 13, 1992.

(i) As an alternative action, operators may accomplish the modification of the test stop with the oxygen box assembly removed from the airplane.

(ii) In lieu of the method for reidentification of the test stop prescribed in the service bulletin, operators may use an alternative method of reidentification if it is approved by the cognizant FAA Principal Maintenance Inspector (PMI).

(2) Modify the oxygen box assemblies in modular lavatory "A" in accordance with Boeing Alert Service Bulletin 737-35A1038, dated March 19, 1992.

(b) For Model 757 series airplanes: Within 900 flight hours or 6 months after the effective date of this AD, whichever occurs later, modify the test stop plungers in the oxygen box assemblies in the lavatories and at doors 1 and 4 flight attendant seats in accordance with Boeing Alert Service Bulletin 757-35A0010, dated February 13, 1992.

(1) As an alternative action, operators may accomplish the modification of the test stop with the oxygen box assembly removed from the airplane.

(2) In lieu of the method for reidentification of the test stop prescribed in the service bulletin, operators may use an alternative method of reidentification if it is approved by the cognizant FAA Principal Maintenance Inspector (PMI).

(c) 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, Seattle Aircraft Certification Office (ACO), 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, Seattle ACO.

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

(d) 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.

(e) The modifications shall be done in accordance with Boeing Alert Service Bulletin 737-35A1037, dated February 13, 1992; Boeing Alert Service Bulletin 737-35A1038, dated March 19, 1992; or Boeing Alert Service Bulletin 757-35A0010, dated February 13, 1992; as applicable. 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, 800 North Capitol Street, NW., suite 700, Washington, DC.

(f) This amendment becomes effective on December 23, 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.