AD 83-10-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
The bus-to-bus electrical resistance of the windshield NESA coat may be outside acceptable limits due to windshields produced in 1979 and 1980 with serial numbers beginning with 9-H and 0-H manufactured by P.P.G. Industries, Inc.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Check the windshield NESA coat's bus-to-bus electrical resistance within 200 hours time in service or 28 days, whichever comes first, using British Aerospace Alert Service Bulletin 56-A-PM5836. Depending on resistance values, perform actions from paragraphs 2.2, 2.3, or 2.4 of the service bulletin. Alternate means of compliance may be approved by the FAA.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 200 hours time in service or 28 days, whichever occurs first, after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
British Aerospace Model BAC 1-11 200 and 400 Series airplanes fitted with pilots windshield No. 1, left and right-hand part numbers AB31A705 and AB31A706 respectively, produced in 1979 and 1980 with serial numbers beginning with 9-H and 0-H, manufactured by P.P.G. Industries, Inc.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Windshields
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_83-10-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-10-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes Subject: Windshields Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/31/1983 Make: Airbus SAS Model: BAC 1-11 200 Series | BAC 1-11 400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 83-10-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4651 AD NUMBER: 83-10-02 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective May 31, 1983. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-10-02 BRITISH AEROSPACE: Amendment 39-4651. Applies to BAC 1-11 200 and 400 series airplanes, certificated in all categories. Compliance is required as indicated. For airplanes fitted with pilots windshield No. 1, left and right-hand part numbers AB31A705 and AB31A706 respectively, produced in 1979 and 1980 with serial numbers beginning with 9-H and 0-H, manufactured by P.P.G. Industries, Inc., accomplish the following, unless already accomplished: A. Check the bus-to-bus electrical resistance of the windshield NESA coat within the next 200 hours time in service or 28 days, whichever occurs first, after the effective date of this AD in accordance with paragraph 2.1 of the Accomplishment Instructions of British Aerospace Alert Service Bulletin 56-A-PM5836, dated March 19, 1982. NOTE: If windshield is replaced with another windshield produced in 1979 or 1980, repeat paragraph A after 200 hours time in service but not later than 300 hours time in service on the replacement windshield. B. Accomplish the actions of paragraph 2.2, 203, or 2.4 of the service bulletin based upon the resistance values obtained in the check done in paragraph A. C. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. D. 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 inspections and/or modifications required by this AD. This amendment becomes effective May 31, 1983. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_83-10-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-10-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes Subject: Windshields Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/31/1983 Make: Airbus SAS Model: BAC 1-11 200 Series | BAC 1-11 400 Series 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: 83-10-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4651 AD NUMBER: 83-10-02 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective May 31, 1983. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-10-02 BRITISH AEROSPACE: Amendment 39-4651. Applies to BAC 1-11 200 and 400 series airplanes, certificated in all categories. Compliance is required as indicated. For airplanes fitted with pilots windshield No. 1, left and right-hand part numbers AB31A705 and AB31A706 respectively, produced in 1979 and 1980 with serial numbers beginning with 9-H and 0-H, manufactured by P.P.G. Industries, Inc., accomplish the following, unless already accomplished: A. Check the bus-to-bus electrical resistance of the windshield NESA coat within the next 200 hours time in service or 28 days, whichever occurs first, after the effective date of this AD in accordance with paragraph 2.1 of the Accomplishment Instructions of British Aerospace Alert Service Bulletin 56-A-PM5836, dated March 19, 1982. NOTE: If windshield is replaced with another windshield produced in 1979 or 1980, repeat paragraph A after 200 hours time in service but not later than 300 hours time in service on the replacement windshield. B. Accomplish the actions of paragraph 2.2, 203, or 2.4 of the service bulletin based upon the resistance values obtained in the check done in paragraph A. C. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. D. 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 inspections and/or modifications required by this AD. This amendment becomes effective May 31, 1983. 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.