- Effective
- March 23, 1962
- Models
- B-2, B-2A, B-2B
- Data sheet
- TCDS2H2
- Registered aircraft
- 53 matched by model
- Product
- Aircraft · Rotorcraft
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 May 30, 2024.
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 | 76773e5f…204d026 | FAA DRS (API key needed) |
On this page
The airworthiness directive
62-06-01 BRANTLY: Amdt. 410 Part 507 Federal Register March 16, 1962. Applies to All Model B-2 Helicopters Equipped With Seat Back Adjustment Wire P/N B2-334-32.
Compliance required within the next 10 hours' time in service after the effective date of this AD.
To prevent the sudden movement of the seat backs to the full aft adjustment position, the following must be accomplished:
Remove the seat back adjustment wire P/N B2-334-32 from the left and right seat backs.
This directive effective March 23, 1962.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 53
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1959 | 1 |
|---|---|
| 1960 | 1 |
| 1961 | 5 |
| 1962 | 2 |
| 1963 | 5 |
| 1964 | 6 |
| 1965 | 1 |
| 1966 | 4 |
| 1967 | 2 |
| 1968 | 2 |
| 1992 | 1 |
| 1997 | 1 |
22 with no year recorded