| AD Number | 83-14-10 | Status | Active |
| Effective Date | July 28, 1983 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-4688 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Bombardier Inc. |
| Model(s) | CL-600-1A11 (CL-600) |
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 theManager, 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.