- Effective
- July 20, 1970
- Model
- SC-7 Skyvan Series 3
- Data sheet
- TCDSA15EU
- Product
- Aircraft · Small airplane
- Amendment
- 39-1032
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 | 20 KB | f69438c9…aec72aa | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-15-05 SHORT BROTHERS AND HARLAND, LIMITED: Amdt. 39-1032. Applies to Model SC-7, series 3 airplanes.
To alert the pilot to hazardous errors in the indicated altitude and airspeed when the stand-by static system is used, within the next 25 hours' time in service from the effective date of this AD, unless already accomplished, accomplish the following:
(a) Install the altimeter stand-by correction label P/N SC7-18-5365 on the instrument panel above the pilot's altimeter in accordance with Shorts Service Bulletin No. 31-53, dated January 9, 1970, or later ARB-approved issue or an FAA-approved equivalent.
(b) Replace the existing airspeed indicator placard P/N SC7-18-5093 on the 1 D panel with a new placard, P/N SC7-18-5409, in accordance with Shorts Service Bulletin No. 31- 51, dated January 9, 1970, or later ARB-approved issue or an FAA-approved equivalent.
This amendment becomes effective July 20, 1970.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.