AD 83-14-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-600-1A11 (CL-600) | Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes |
Unsafe Condition
Decompression of the aircraft due to potential cracks in windshield and side window glazing.
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Required Actions
Inspect windshield and side window glazing per Canadair Service Bulletin 600-0147, Rev 2; modify as required. Replace cracked glazing before further flight. Modify per Service Bulletin 600-0225, Rev 1 for applicable serial numbers. Allow alternate compliance with FAA approval and special flight permits for unpressurized operations under specified regulations.
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Compliance Time
within the next 100 hours time in service after the effective date of this AD
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Affected Aircraft
Bombardier Inc. Model CL-600-1A11 airplanes certificated in all categories, with serial numbers listed in Canadair Service Bulletins 600-0147 and 600-0225.
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Federal Register Abstract
Window Glazing Inspection
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_83-14-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-14-10 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes Subject: Window Glazing Inspection Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/28/1983 Make: Bombardier Inc. Model: CL-600-1A11 (CL-600) Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 83-14-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4688 AD NUMBER: 83-14-10 SUBJECT HEADING: Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes ACTION: SUMMARY: DATES: Effective July 28, 1983. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-14-10 CANADAIR: Amendment 39-4688. Applies to Model CL-600-1A11 airplanes certificated in all categories. To prevent decompression of the aircraft, within the next 100 hours time in service after the effective date of this AD, accomplish the following, unless previously accomplished: A. For airplanes with serial numbers listed in Canadair Service Bulletin 600-0147, Revision 2, dated September 24, 1982, modify and inspect the windshield and side window glazing in accordance with the Accomplishment Instructions of this service bulletin. B. If cracks are detected replace the affected glazing prior to further flight except as noted in paragraph E. below. C. For airplanes with serial numbers listed in Canadair Service Bulletin 600-0225, Revision 1, dated September 24, 1982, modify in accordance with the Accomplishment Instructions of this service bulletin. D. 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. E. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes unpressurized to a base for the accomplishment of inspections and/or modifications required by this AD. This amendment becomes effective July 28, 1983. FOOTER:
Document Text
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AD Final Rules - DRS_83-14-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-14-10 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes Subject: Window Glazing Inspection Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/28/1983 Make: Bombardier Inc. Model: CL-600-1A11 (CL-600) 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: 83-14-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4688 AD NUMBER: 83-14-10 SUBJECT HEADING: Airworthiness Directives; CANADAIR Model CL-600-1A11 Airplanes ACTION: SUMMARY: DATES: Effective July 28, 1983. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-14-10 CANADAIR: Amendment 39-4688. Applies to Model CL-600-1A11 airplanes certificated in all categories. To prevent decompression of the aircraft, within the next 100 hours time in service after the effective date of this AD, accomplish the following, unless previously accomplished: A. For airplanes with serial numbers listed in Canadair Service Bulletin 600-0147, Revision 2, dated September 24, 1982, modify and inspect the windshield and side window glazing in accordance with the Accomplishment Instructions of this service bulletin. B. If cracks are detected replace the affected glazing prior to further flight except as noted in paragraph E. below. C. For airplanes with serial numbers listed in Canadair Service Bulletin 600-0225, Revision 1, dated September 24, 1982, modify in accordance with the Accomplishment Instructions of this service bulletin. D. 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. E. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes unpressurized to a base for the accomplishment of inspections and/or modifications required by this AD. This amendment becomes effective July 28, 1983. FOOTER:
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Retrieved: Apr 8, 2026
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