- Effective
- May 30, 1962
- Models
- 707-100 Long Body, 707-100B Long Body, 707-100B Short Body, 707-200, 707-300 Series, 707-300B Series and 4 more
- Registered aircraft
- 6 matched by model
- Product
- Aircraft · Large 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 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 | d9aa3b07…6590229 | FAA DRS (API key needed) |
On this page
The airworthiness directive
62-13-02 BOEING: Amdt. 446 Part 507 Federal Register May 30, 1962. Applies to 707 and 720 Series Aircraft Listed in Boeing Service Bulletin No. 1698 Dated May 16, 1962.
Compliance required as indicated.
As a result of several cases of damaged wiring in the automatic pilot trim servo wire bundle, accomplish the following one-time inspection:
Within the next 150 hours' time in service after the effective date of this AD unless already accomplished, inspect the wire bundle connected to the autopilot trim servostabilizer limit switches, and stabilizer position transmitter in accordance with Boeing Service Bulletin No. 1698 dated May 16, 1962. If damage is found, repair or replace the wire bundle prior to further flight.
This directive effective May 30, 1962.
Affected TCDS · 3
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 6
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1968 | 1 |
|---|---|
| 1977 | 1 |
4 with no year recorded