| AD Number | 77-13-05 | Status | Active |
| Effective Date | June 29, 1977 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2930 |
| 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-215-1A10 CL-215-6B11 (CL-215T Variant) CL-215-6B11 (CL-415 Variant) |
77-13-05 CANADAIR: Amendment 39-2930. Applies to CL-215 Airplanes, Serial Numbers 1001 through 1040 and 1046, certificated in all categories.
Compliance required prior to U.S. airworthiness certification, unless already accomplished:
(a) Inspect the right hand canopy sill for missing rivets forward and aft of bulkhead 234.5 as indicated in Figures 1 and 3 of the Canadair Information Circular (S.I.C.) No. 129-CL- 215 dated May 12, 1976, or an approved equivalent inspection.
(b) If rivets have been omitted forward of the bulkhead, between stations 223 and 229, install three NAS 1103-4 bolts with MS2104L3 Nuts and Strip Washer as shown in Figure 2 of the S.I.C. or an approved equivalent alteration.
(c) If rivet spacing aft of the bulkhead is greater than 1.25 inch install intermediate rivets as indicated in Figure 3 of the S.I.C. or an approved equivalent alteration.
(d) Equivalent inspections, alterations or parts must be approved by Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
This Amendment becomes effective June 29, 1977.