STC SA3239NM
FAA DRS lists SA3239NM as Current · Reissued, held by Advanced Instrument Incorporated, for Cessna Aircraft A185E and Cessna Aircraft A185F. Recorded change: Relocate battery to forward of fire wall, add cowl flap extensions and relocate cylinder head temperature probe to cylinder number 3. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA3239NM 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 A185E and Cessna Aircraft A185F. 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
- SA3239NM
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- January 26, 1979
- Revision date
- August 18, 2006
- CFR references
- Part 3, Part 21