Performance STC Modifications
R172K (‘HAWK XP)
SA1437CE Increases horsepower from 195 to 210. Approved in combination with SE1436CE which approves the Continental IO-360-K and –KB to 210 horsepower. This STC is available from Isham Inc. at this link.
STC Modification Listing
Installation of flap and aileron gap seals.
Fabrication of interchangeable float spreader bars.
SA00161BO (1 OF 3)
Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.
Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface
Installation of carbon steel brake discs that have melonite surface treatment.
SA00243BO (2 OF 5)
Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n
Installation of fiberglass replacement wing tips.
Installation of replacement flap trailing edge bulbs. (R172K XP)
SA00680SE (3 OF 6
Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.
Installation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2, no rev, both
Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate
Installation of Baumann Model BF-2550 floats.
Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun
Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery.
Installation of replacement wing tip fairing assembly.
Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model, s/n 67042 and up) (For Cessna
Installation of flap gap seal per Aircraft Development Co. Drawing List 114-1 stamped FAA approved
Installation of aileron gap seal per Aircraft Development Co. Drawing List 115-1 stamped “FAA
SA01436SE (1 OF 2)
Cockpit sunvisor retrofit kit.
SA01695SE (1 OF 5)
Installation of an antenna
Installation of Baumann Model BF2550A floats. For models 172I through 172P, a gross weight of 2350
Installation of hourmeter airspeed switch.
Installation of Lord Corporation nose wheel shimmy damper part number SE-1051-2/3.
SA02217AK (2 OF 5)
Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL
12/01/2004 12:00:00 AM
SA02655AT (1 OF 2)
Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type
Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems, Model
Installation of airflow register into baggage compartment cover and insert a screened vent into
SA10236SC (2 OF 4)
Installation of a GDC 31 Roll Steering Converter
Installation of a Shadin Co. fuel flow indicating system.
Installation of an adjustable nine-inch trim tab on left aileron.
Continental IO-360-K or KB engine installation rerated to 210 hp (2800 rpm) at takeoff and 195
Installation of flap and aileron gap seals.
Installation of on-board engine analyzer system.
Installation of flap gap seals.
Installation strut/wing and strut/fuselage fairings, lightning hole covers, and aerodynamic putty.
Installation of Lompoc Aero Specialties inner plexiglass pane
in swing out window frames presently
Installation of flap gas fairing.
Installation of aileron and/or flap gap seals.
Installation of steering rod boots.
Leading edge cuffs, stall fences, aileron seals, wing tips.
Installation of seaplane safety covers.
Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system.
Installation of Auto-Vac-2 manifold vacuum system per certain engine STC's.
Add sheet metal flap seals and/or flexible fabric aileron gap seals.
Installation of PeeKay model 2300 or B2300 seaplane floats and associated hardware
Installation of FluiDyne A2500A or AT2500A skis.
Installation of Aero Ski Manufacturing Co. Model M3000H fixed skis. (172M LANDING GEAR MODIFIED PER
Installation of Aero Ski Manufacturing Co. Model R2800 retractable skis. (172N LANDING GEAR
Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator
Installation of an engine electronic tachometer, Model P-1000.
Installation of S-TEC Manual Electric Trim System Model ST-447.
Installation of S-TEC System 65 two axis automatic flight guidance system, model ST-470.
Installation of an R25400 alternator control unit
Installation of V25101 overvoltage sensor.
Installation of S-TEC System 55 two axis automatic flight guidance system, Model ST-563, with
Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne
Installation of Grimes aviation white anti-collision strobe light system two light or three light
STOL kit installation (wing leading edge cuffs, drooped tips, stall fences, and aileron gap seals).
ST01700NY (1 OF 2)
Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature
ST02547AT (1 OF 2)