| AD Number | 50-42-01 | Status | Active |
| Effective Date | Not specified | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | N/A |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | A35 |
50-42-01 BEECH: Applies to Model A35 Aircraft, Serial Numbers D-1501 to D-2200 Inclusive Not Having the Cambered Elevator Tabs Installed.
Compliance required at next 100 hours inspection but not later than November 15, 1950.
All aircraft should be modified as follows:
(1) Replace the elevator tabs (noncambered) with cambered tabs (lower surface cambered) P/N 35-660040-52 and -53 or,
(2) Restrict rear c.g. limit by appropriate revisions to loading schedules and Airplane Flight Manual to comply with the following c.g. limits:
(plus 83.7) to (plus 84.4) at 2,650 pounds
(plus 75.9) to (plus 84.4) at 2,140 pounds or less
Straight line variation between forward c.g. limits.
(Beech Service Bulletin No. A35-8 dated April 3, 1950, covers this same subject.)