- Model
- A35
- Data sheet
- TCDSA-777
- Registered aircraft
- 159 matched by model
- Product
- Aircraft · Small airplane
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed January 21, 2026.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | eca67f1b…02978d1 | FAA DRS (API key needed) |
On this page
The airworthiness directive
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.)
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 159
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1947 | 2 |
|---|---|
| 1948 | 81 |
| 1949 | 42 |
| 1957 | 1 |
33 with no year recorded