AD 92-06-03

final rule

Airworthiness Directives; BOEING Model 747 Series Airplanes

AD Number
92-06-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-NM-49-AD
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 evacuation system packboard and cover assemblies may have an angle measured at 155 degrees or greater, which could compromise the reliability of the evacuation system.

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

Required Actions

Inspect the evacuation system packboard and cover assemblies within 120 days after the effective date. If the angle is 155 degrees or greater, modify the assemblies before further flight. If the angle is less than 155 degrees, modify within 15 months after the effective date.

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

Compliance Time

Within the next 120 days after the effective date of this AD, and within the next 15 months after the effective date if the angle is less than 155 degrees.

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

Affected Aircraft

Boeing Model 747 series airplanes, line number 696 and subsequent, equipped with specific evacuation system packboards and cover assemblies as per Boeing Service Bulletins 747-25-2807 and 747-25A2889.

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

Federal Register Abstract

Evacuation System

Applicability Source Text

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AD Number:
92-06-03
Document Type:
AD Final Rules
Docket Number:
91-NM-49-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747 Series Airplanes
Subject:
Evacuation System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/21/1992
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: 92-06-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   91-NM-49-AD

AMENDMENT:   39-8183

AD NUMBER:   92-06-03

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 21, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-06-03 BOEING: Amendment 39-8183. Docket 91-NM-49-AD.

Applicability: Model 747 series airplanes, line number 696 and subsequent; equipped with evacuation system packboards and cover assemblies identified in the Boeing Service Bulletin 747-25-2807, Revision 2, dated August 22, 1991, and Boeing Alert Service Bulletin 747- 25A2889, dated November 1, 1990; certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To provide satisfactory reliability of the evacuation system, accomplish the following:

(a) For evacuation system packboard and cover assemblies identified in either Boeing Service Bulletin 747-25-2807, Revision 2, dated August 22, 1991, or Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990: Within the next 120 days after the effective date of this AD, inspect the evacuation system packboard and cover assemblies in accordance with Part III, "Accomplishment Instructions," Paragraph B., of Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990.

(1) If the inspection reveals that the angle measured is 155 degrees or greater, prior to further flight, modify the packboard and cover assemblies in accordance with Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990, and Boeing Service Bulletin 747-25-2807, Revision 2, dated August 22, 1991, as applicable.

(2) If the inspection reveals that the angle measured is less than 155 degrees, within the next 15 months after the effective date of this AD, modify the packboard and cover assemblies in accordance with Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990, and Boeing Service Bulletin 747-25-2807, Revision 2, dated August 22, 1991, as applicable.

(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 and modification shall be done in accordance with Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990; and Boeing Service Bulletin 747-25- 2807, Revision 2, dated August 22, 1991, which contains the following list of effective pages:

Page Number	
Revision Level
	Date
1, 3-4	
2
	August 22, 1991
2, 5, 7, 8,
17-18	
1
	July 25, 1991
6, 9-16	
(original)
	December 7, 1989

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.

This amendment becomes effective on April 21, 1992.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_92-06-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
92-06-03
Document Type:
AD Final Rules
Docket Number:
91-NM-49-AD
Subject Heading:
Airworthiness Directives; BOEING Model 747 Series Airplanes
Subject:
Evacuation System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/21/1992
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: 92-06-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   91-NM-49-AD

AMENDMENT:   39-8183

AD NUMBER:   92-06-03

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 747 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 21, 1992.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
92-06-03 BOEING: Amendment 39-8183. Docket 91-NM-49-AD.

Applicability: Model 747 series airplanes, line number 696 and subsequent; equipped with evacuation system packboards and cover assemblies identified in the Boeing Service Bulletin 747-25-2807, Revision 2, dated August 22, 1991, and Boeing Alert Service Bulletin 747- 25A2889, dated November 1, 1990; certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To provide satisfactory reliability of the evacuation system, accomplish the following:

(a) For evacuation system packboard and cover assemblies identified in either Boeing Service Bulletin 747-25-2807, Revision 2, dated August 22, 1991, or Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990: Within the next 120 days after the effective date of this AD, inspect the evacuation system packboard and cover assemblies in accordance with Part III, "Accomplishment Instructions," Paragraph B., of Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990.

(1) If the inspection reveals that the angle measured is 155 degrees or greater, prior to further flight, modify the packboard and cover assemblies in accordance with Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990, and Boeing Service Bulletin 747-25-2807, Revision 2, dated August 22, 1991, as applicable.

(2) If the inspection reveals that the angle measured is less than 155 degrees, within the next 15 months after the effective date of this AD, modify the packboard and cover assemblies in accordance with Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990, and Boeing Service Bulletin 747-25-2807, Revision 2, dated August 22, 1991, as applicable.

(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 and modification shall be done in accordance with Boeing Alert Service Bulletin 747-25A2889, dated November 1, 1990; and Boeing Service Bulletin 747-25- 2807, Revision 2, dated August 22, 1991, which contains the following list of effective pages:

Page Number	
Revision Level
	Date
1, 3-4	
2
	August 22, 1991
2, 5, 7, 8,
17-18	
1
	July 25, 1991
6, 9-16	
(original)
	December 7, 1989

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.

This amendment becomes effective on April 21, 1992.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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