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
Relocate battery to forward of fire wall, add cowl flap extensions and relocate cylinder head temperature probe to cylinder number 3.
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.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Cessna Aircraft A185E and Cessna Aircraft A185F model, serial range, and configuration?
- 02Which control configuration, rigging, limitations, and inspections apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
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