| AD Number | 74-20-12 | Status | Active |
| Effective Date | October 04, 1974 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-1979 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Twin Commander Aircraft LLC |
| Model(s) | 690A |
74-20-12 COMMANDER AIRCRAFT DIVISION, ROCKWELL INTERNATIONAL: Amendment 39-1979. Applies to Rockwell Model 690A series airplanes, S/N 11100 through 11197.
Compliance required as indicated unless already accomplished.
1. Before the first flight of each day after the effective date of this A.D., check the cutout around the openable pilot's and co-pilot's side windows for cracks.
2. If cracks are found in either side window, replace the openable side window with a non-openable side window, P/N 360012-501, before further flight, except flight with cabin unpressurized may be made in accordance with FAR 21.197 to a base where the replacement can be accomplished.
3. Within 50 hours' time in service after the effective date of this A.D., unless already accomplished, replace all openable side windows, with a non-openable side window, P/N 360012-501, in accordance with Rockwell Service Bulletin 143 dated September 10, 1974, or an equivalent method approved by the Chief,Engineering and Manufacturing Branch, Flight Standards Division, Southwest Region, Fort Worth, Texas.
This amendment becomes effective October 4, 1974.