- Model
- Viscount 810
- Data sheet
- TCDSA-814
- 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 | aaf5bc51…89eb711 | FAA DRS (API key needed) |
On this page
The airworthiness directive
59-06-06 VICKERS: Applies to All Viscount 810 Series Aircraft.
Compliance required as indicated.
In order to rectify a manufacturing error on bearing channel 81003-1063, Vickers- Armstrongs recommends the following corrective action: Inspect for signs of distortion or cracks on vertical bearing channel 81003-1061 on upper side of chassis pivot support block at wheel bay side of outer rib of inboard nacelles. The inspection must be made within 135 flying hours and every subsequent 135 flying hours until the outer rib reinforcement is incorporated. The outer rib reinforcement must be incorporated by July 1, 1959. The British Air Registration Board considers this mandatory. The FAA concurs with this action and considers compliance therewith mandatory.
(Vickers-Armstrongs Modification Bulletin G.1656 covers this subject.)
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.