AD 90-19-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A | Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (C-29A) | Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes |
| aircraft | Textron Aviation Inc. | BAe.125 Series 800A (U-125) | Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes |
Unsafe Condition
Fatigue cracks in the windscreen center pillar and subsequent rapid decompression of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install reinforcing straps on the bottom aft portion of the upper and lower web sections of the windscreen center pillar assembly in accordance with British Aerospace Service Bulletin 53-65-3168A, Revision 1, dated March 9, 1989. An alternate means of compliance or adjustment of the compliance time may be used when approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 6,000 landings since new or within 30 days after the effective date of this AD, whichever occurs later, unless previously accomplished.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Model BAe 125-800A series airplanes, Serial Numbers 258001 through 258090, inclusive, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Windscreen Pillar Assembly
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_90-19-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 90-19-04 Document Type: AD Final Rules Docket Number: 90-NM-84-AD Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes Subject: Windscreen Pillar Assembly Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/16/1990 Make: Textron Aviation Inc. Model: BAe.125 Series 800A | BAe.125 Series 800A (C-29A) | BAe.125 Series 800A (U-125) Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 90-19-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 90-NM-84-AD AMENDMENT: 39-6721 AD NUMBER: 90-19-04 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes ACTION: Final rule SUMMARY: DATES: Effective October 16, 1990. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 90-19-04 BRITISH AEROSPACE: Amendment 39-6721. Docket No. 90-NM-84-AD. Applicability: Model BAe 125-800A series airplanes, Serial Numbers 258001 through 258090, inclusive, certificated in any category. Compliance: Required prior to the accumulation of 6,000 landings since new or within 30 days after the effective date of this AD, whichever occurs later, unless previously accomplished. To prevent fatigue cracks in the windscreen center pillar and subsequent rapid decompression of the airplane, accomplish the following: A. Install reinforcing straps on the bottom aft portion of the upper and lower web sections of the windscreen center pillar assembly in accordance with British Aerospace Service Bulletin 53-65-3168A, Revision 1, dated March 9, 1989. 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, Transport Airplane Directorate. NOTE: The request should be submitted directly to the Manager, Standardization Branch, ANM-113, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Manager, Standardization Branch, ANM-113. 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. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041-0414. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington. This amendment (39-6721, AD 90-19-04) becomes effective October 16, 1990. FOOTER:
Document Text
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AD Final Rules - DRS_90-19-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 90-19-04 Document Type: AD Final Rules Docket Number: 90-NM-84-AD Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes Subject: Windscreen Pillar Assembly Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/16/1990 Make: Textron Aviation Inc. Model: BAe.125 Series 800A | BAe.125 Series 800A (C-29A) | BAe.125 Series 800A (U-125) 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: 90-19-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: 90-NM-84-AD AMENDMENT: 39-6721 AD NUMBER: 90-19-04 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model BAe 125-800A Series Airplanes ACTION: Final rule SUMMARY: DATES: Effective October 16, 1990. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 90-19-04 BRITISH AEROSPACE: Amendment 39-6721. Docket No. 90-NM-84-AD. Applicability: Model BAe 125-800A series airplanes, Serial Numbers 258001 through 258090, inclusive, certificated in any category. Compliance: Required prior to the accumulation of 6,000 landings since new or within 30 days after the effective date of this AD, whichever occurs later, unless previously accomplished. To prevent fatigue cracks in the windscreen center pillar and subsequent rapid decompression of the airplane, accomplish the following: A. Install reinforcing straps on the bottom aft portion of the upper and lower web sections of the windscreen center pillar assembly in accordance with British Aerospace Service Bulletin 53-65-3168A, Revision 1, dated March 9, 1989. 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, Transport Airplane Directorate. NOTE: The request should be submitted directly to the Manager, Standardization Branch, ANM-113, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Manager, Standardization Branch, ANM-113. 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. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, D.C. 20041-0414. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington. This amendment (39-6721, AD 90-19-04) becomes effective October 16, 1990. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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