STC SA09505AC-D
FAA DRS lists SA09505AC-D as Current · Issued, held by S-TEC Corporation, for Cessna Aircraft 310, Cessna Aircraft 310A, and Cessna Aircraft 310B, and 1 more aircraft configuration. Recorded change: Installation of S-TEC Manual Electric Trim System, Model ST-883. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA09505AC-D identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Cessna Aircraft 310, Cessna Aircraft 310A, and Cessna Aircraft 310B, and 1 more aircraft configuration. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related flight controls STCs
Installation of flap gap seal per Aircraft Development Co. Drawing List 114-1 stamped FAA approved with a date of April 27, 2005 or later. Conformity data for Drawing List 114-1 is derived from Drawing List 114-1 Revision C and STC s SA1484CE, SA1490CE, SA1491CE, SA1492CE, SA1493CE, SA1494CE, and SA1495CE.
FAA holder: Aircraft Development Co
Installation of aileron gap seal per Aircraft Development Co. Drawing List 115-1 stamped FAA approved with a date of April 27, 2005 or later. Conformity data for Drawing List 115-1 is derived from Drawing List 115-1 Revision D and STC s SA1484CE, SA1490CE, SA1491CE, SA1492CE, SA1493CE, SA1494CE, and SA1495CE.
FAA holder: Aircraft Development Co
Installation of a drag reduction system (including outboard trailing edge extension, leading edge vortilons, and contoured flap) in accordance with Raisbeck Engineering Drawing Number 202L-5700, Revision A, dated August 29, 2004, or later FAA approved revisions.
FAA holder: Raisbeck Engineering
FAA record reference
- STC number
- SA09505AC-D
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- February 23, 2001
- Revision date
- February 27, 2001
- CFR references
- Part 21