AD 87-03-05

final rule

Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes

AD Number
87-03-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. BAe.125 Series 800A Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes
aircraft Textron Aviation Inc. BAe.125 Series 800B Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes

Unsafe Condition

The fuselage canopy upper rail may fail, leading to possible rapid loss of cabin pressurization.

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

Required Actions

Modify the fuselage canopy upper rail in accordance with Section 2 of British Aerospace Service Bulletin 53-59-(3031B), dated June 5, 1986. An alternate means of compliance or adjustment of compliance time may be used if approved by the FAA Manager, Standardization Branch, ANM-113.

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

Compliance Time

Prior to the accumulation of a total of 3,000 flight cycles or within the next 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 BAe 125-800A and -800B series airplanes listed in Service Bulletin 53-59 (3031B), dated June 5, 1986.

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

Federal Register Abstract

Fuselage Canopy Rail

Applicability Source Text

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Details
AD Number:
87-03-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes
Subject:
Fuselage Canopy Rail
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/19/1987
Make:
Textron Aviation Inc.
Model:
BAe.125 Series 800A | BAe.125 Series 800B
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Superseded AD: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Superseded By: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: 87-03-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5516

AD NUMBER:   87-03-05

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 19, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   87-03-05 BRITISH AEROSPACE: Amendment 39-5516. Applies to Model BAe 125- 800A and -800B series airplanes, listed in British Aerospace Service Bulletin 53-59 (3031B), dated June 5, 1986, certificated in any category. Compliance is required prior to the accumulation of a total of 3,000 flight cycles, or within the next 90 days after the effective date of this AD, whichever occurs later. To prevent the possible rapid loss of cabin pressurization, accomplish the following, unless previously accomplished:

A. Modify the fuselage canopy upper rail in accordance with Section 2, "Accomplishment Instructions," of British Aerospace Service Bulletin 53-59-(3031B), dated June 5, 1986.

B. 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, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of the modification required by this AD.

All persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to British Aerospace, Inc., Librarian for Service Bulletins, Box 17414, Dulles International Airport, Washington, D.C. 20041. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective February 19, 1987.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_87-03-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-03-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes
Subject:
Fuselage Canopy Rail
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
02/19/1987
Make:
Textron Aviation Inc.
Model:
BAe.125 Series 800A | BAe.125 Series 800B
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: 87-03-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5516

AD NUMBER:   87-03-05

SUBJECT HEADING:   Airworthiness Directives; BRITISH AEROSPACE Model BAe 125- 800A and -800B Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective February 19, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   87-03-05 BRITISH AEROSPACE: Amendment 39-5516. Applies to Model BAe 125- 800A and -800B series airplanes, listed in British Aerospace Service Bulletin 53-59 (3031B), dated June 5, 1986, certificated in any category. Compliance is required prior to the accumulation of a total of 3,000 flight cycles, or within the next 90 days after the effective date of this AD, whichever occurs later. To prevent the possible rapid loss of cabin pressurization, accomplish the following, unless previously accomplished:

A. Modify the fuselage canopy upper rail in accordance with Section 2, "Accomplishment Instructions," of British Aerospace Service Bulletin 53-59-(3031B), dated June 5, 1986.

B. 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, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of the modification required by this AD.

All persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to British Aerospace, Inc., Librarian for Service Bulletins, Box 17414, Dulles International Airport, Washington, D.C. 20041. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.

This amendment becomes effective February 19, 1987.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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