AD 87-03-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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.
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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.
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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.
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Affected Aircraft
British Aerospace Model BAe 125-800A and -800B series airplanes listed in Service Bulletin 53-59 (3031B), dated June 5, 1986.
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Federal Register Abstract
Fuselage Canopy Rail
Applicability Source Text
Show captured applicability text from the source AD
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Model: BAe.125 Series 800A | BAe.125 Series 800B Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 87-03-05 CITATION: This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:
Document Text
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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:
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