STC No. | Subject | PA-15 | PA-17 | PA-16 | PA-20 | PA-22 | Comments |
SA00024NY | Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine | X | | X | X | X | |
SA00068SE | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | X | X | X | X | X | |
SA00081NY | Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. | X | | X | X | X | |
SA00172BO | Installation of Piper PA-18 right wing fuel tank. Limited to installation on PA-16, serial number | | | X | | | Single S/N only |
SA00207AT | Installation of carbon steel brake discs that have melonite surface treatment, P/N AA-67. | | X | X | X | | |
SA00215NY | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | X | X | X | X | X | |
SA00283BO | Installation of Lycoming O-320-A, -A1B, -A2A, -A2B, -A2C, -C1A, -C1B, -C2A or –C2B engine and | | | X | | | |
SA00344BO | Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. | X | X | X | X | X | |
SA00478CH | Installation of Cooper Superflite 102 Fabric. | X | X | X | X | X | |
SA00680SE | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | X | X | X | X | X | |
SA00780SE | Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No | X | X | X | X | X | |
SA00932SE | Installation of the Stewart wing tip assembly in accordance with Stewart Wing Tip Assembly Master | X | X | X | X | X | |
SA01015SE | Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model | X | X | X | X | X | |
SA01026SE | Improved fuel gascolator assembly -Steve's Aircraft | X | X | X | X | X | |
SA01063CH | Installation of a Scott Model 3200 Tail Wheel with the AESI #T.S.05P Tail Spring. | | | X | X | | |
SA01158WI | Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. | | X | X | X | X | |
SA01233SE | Manufacture of Alaskan Bushwheel, Inc. (ABI) tail wheel and fork assembly per ABI Document | X | X | X | X | X | |
SA01240SE | Installation of secondary voltage indication system | X | X | X | X | X | |
SA01251SE | The manufacture of a Sunvisor System. | X | X | X | X | X | |
SA01343WI | Installation of B&C Specialty Products BC400 Alternator. . | | | X | X | X | |
SA01669CH | Installation of Challenger Reusable Air Filter | | X | X | X | X | |
SA01689SE | ONE-ONLY STC: Installation of an 18 gallon right wing fuel tank with electric fuel gauges, | | | X | | | Single S/N only |
SA01704LA | Installation of the Grove Disk Brake System | X | X | X | X | | |
SA01757WI | Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail | X | X | X | X | X | |
SA01765SE | Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels, Part Number (P/N) ABI-1010. | X | X | X | X | X | |
SA01843SE | Installation of Lycoming engine and modified fuel system | | | X | | | |
SA01863SE | Installation of Niagara Oil Cooler in the above model aircraft | | | X | X | X | |
SA01899WI | Installation of Garmin G3X Touch Electronic Flight Instrument System | | | X | X | X | |
SA01944CH | Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index, per ASTM | X | X | X | X | X | |
SA01967WI | Use of GAMI G100UL High Octane Unleaded Avgas | X | X | X | X | X | |
SA01988SE | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) | | | X | X | X | |
SA02033AT | Modification to install an air-oil separator to prevent oil from being aspirated from the engine | X | X | X | X | X | |
SA02093AK | Installation of hourmeter airspeed switch. | X | | X | X | X | |
SA02110CH | Installation of a Time Trac Data Recorder | X | X | X | X | X | |
SA02128LA | Installation of aileron and flap hinge repair bushings | X | X | X | X | X | |
SA02212AK | Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge | X | X | X | X | X | |
SA02241AK | Installation of a Maule Fuel Selector Valve and Associated Fuel System Upgrade in accordance with | | | X | X | X | |
SA02263AK | Fabrication and Installation of a Left Hand Seaplane Door. | | | X | X | X | |
SA02264AK | Fabrication and Installation of a Right Hand Seaplane Door. | | | X | X | X | |
SA02268CH | Installation of Airwolf Filter Corp. Air Oil Separator | X | X | X | X | X | |
SA02283SE | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) | X | X | X | X | X | |
SA02306AK | Installation of a Lycoming O-360-A1A, A1D, A2A, A2D, A2E, A2F, A3A, A3D, A4A, A4M, A4N, or A4P | | | X | X | X | |
SA02345AK | Installation of Piper PA-18 three-inch extended gear & Maule Oleo Strut | | | X | X | X | |
SA02386AK | Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems | X | X | X | X | X | |
SA02402SE | Installation of Electronics International Inc. Glass Panel Engine Monitor | X | X | X | X | X | |
SA02428AK | Installation of a hydraulically actuated ski drag assembly | X | X | X | X | X | |
SA02434NY | Installation of a Digital Engine Monitoring system. | | | X | X | X | |
SA02483AK | Installation of : (1) Cleveland 199-62 or 199-62A wheel and brake kit or ABI LLC AB-199-62 or | | | X | X | X | |
SA02484AK | Installation of Sensenich W80CM8 wood propeller | | | X | X | X | |
SA02520AT | Installation of M-20 Oil Separator, model 600-WP. | X | X | X | | | |
SA02525LA | Installation of Wheel and Brake Assemblies | X | X | X | X | | |
SA02553AK | Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener | X | X | X | X | X | |
SA02594SE | SkyView HDX Instrumentation and Autopilot System manufactured | | | X | X | X | |
SA02734CH | Installation of Lightweight Battery and Circuit Breaker Master Switch in lieu of original | | | X | X | X | |
SA02738CH | Installation of L-3 Communications Avionics Systems | X | X | X | X | X | |
SA02751CH | Installation of McCauley Propeller model 1A200FA824X | | | X | X | X | |
SA02825NY | Installation of Aerospace Logic Aircraft Instruments | X | X | X | X | X | |
SA02846CH | Installation of MT Propeller model MTV-15-B/210-58 on Piper Aircraft models PA-20 and PA-22, | | | X | X | X | |
SA02929CH | Installation of Lycoming O-360 engine in accordance with Installation Instructions, Report SA300 | | | X | X | X | |
SA02987CH | Installation of the Electroair Electronic Ignition System | | X | X | X | X | |
SA04032CH | Install rocker switch assemblies | | X | X | X | X | |
SA04112CH | Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder | | | X | | | |
SA04378CH | Installation of an engine modified per STC SE04349CH on an aircraft listed on FAA approved model list #SA04378CH dated 1/13/19 or later FAA approved revision, IAW SureFly installation instructions listed on the AML. | | | X | X | | |
SA04474CH | Installation of Rubbert Exhaust Assembly RR-1210, RR-1210-HR, RR-1212 and RR-1212-HR on Piper Aircraft models PA-12, PA- 14, PA-16, PA-18, PA-19, PA-20 and PA-22, in accordance with Installation Instructions, document number RR-120, revision Org., dated 04/24/2020 and Instruct 1201, revision Org., dated July 27, 2020 or later FAA approved revision. | | | X | X | X | |
SA04776NY | The HIPEC Covering and Finishing System must be performed and maintained | X | X | X | X | X | |
SA09470SC | Installation of Starter Indicator light system. | | | X | X | X | |
SA1005NW | Installation of a Lycoming O-290-D engine, a Sensenich 74DM-0-55 propeller, a right wing auxiliary | | | X | | | |
SA1008WE | Installation of Poly-Fiber covering material. | X | | X | X | X | |
SA10682SC | Installation of alternator and voltage regulator | | | X | X | X | |
SA11RM | Installation of modified axles, wheels and brakes | X | X | X | X | | |
SA126SO | Installation of wing fabric attachment clips. | X | | X | X | X | |
SA1-282 | Replacement of fabric covering with metal skins. | | | X | X | X | |
SA1-327 | Replacement of fabric covering with metal skins. | | | X | X | X | |
SA1351WE | Replace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 | X | X | X | X | X | |
SA144AL | Remote compass bracket. | X | X | X | X | X | |
SA1455NM | Installation of a flame proof auxiliary heater-dryer, Model12-1600. | X | X | X | X | X | |
SA147AL | Electric fuel quantity gauge system. | | | X | | | |
SA1-510 | Installation of Sur-Vent fuel tank filler cap manufactured. | | | X | X | X | |
SA1511SO | Remove the 12 gallon fuselage fuel tank and install an 18 gallon fuel tank in the right wing. | | | X | | | |
SA1520NM | Installation of stamped aluminum wing ribs. | | | X | | | |
SA1-577 | Installation of Sensenich controllable pitch propeller Model CS3FM4/C374E. | | | X | | | |
SA1590NM | Installation of replacement long-life lift strut. | | | X | | | |
SA1626NM | Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series) | X | X | X | X | X | |
SA1637SO | Installation of Lycoming O-320(150 hp) engine. Sensenick Model74DM6-0-57 propeller and Harrison | | | X | | | |
SA2082CE | Operation of airplane on unleaded automotive gasoline, 87 minimum antiknock index and leaded | | | X | | | |
SA2127WE | Installation of Madras Air Service Model 104 wing tips. | X | | X | X | X | |
SA2167NM | Installation of the Precise Flight stand-by vacuum system (SVS). | X | X | X | X | X | |
SA2190NM | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | X | X | X | X | X | |
SA22RM | Manufacture of exact replacement parts, front and rear lift strut assembly. | | | X | X | X | |
SA2350NM | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | X | X | X | X | X | |
SA24EA | Conversion of aircraft for parachute jumping and aerial photography. | | | X | | | |
SA2508SO | Replacement of Cleveland brake discs, No. 164-67 or 164-167, with Appalachian Accessories' | X | X | X | X | | |
SA2687NM | Installation of Truboplus/ Electronics Int'l gauges and switches. | X | X | X | X | X | |
SA2693NM | Installation of Electronics International digital volt/amp gauges and accessories. | X | X | X | X | X | |
SA2844CE | Installation of a plastic cap enclosure over the anti-collision strobe light system. | X | X | X | X | X | |
SA293AL | Installation of Stoddard improved brake system. | X | X | X | X | | |
SA2-952 | Installation of fiberglass covering. | X | | X | | | |
SA2NE | Installation of Cleveland wheels and brakes, 7.00-6 or 6.00-6, C38500-HA, 40-6, in accordance with | X | X | X | X | | |
SA308EA | Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single | X | | X | X | X | |
SA318NW | Removal of the left-hand cabin door | | | X | | | |
SA3215WE | Installation of George M. Adams DGA-2000 or Bodell BMI-2000 wheelsand Bodell BMI-252 brakes. | | | X | | | |
SA334SW | Installation of InterAv Alternator. | | | X | X | X | |
SA3518NM | Installation of a skylight, in accordance with Steve’s Aircraft Drawing No. SP-3200, Sheet 1 | X | X | X | X | X | |
SA3531NM | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | | X | X | X | |
SA3605NM | Installation of landing gear fueling step. | | | X | | | |
SA3606NM | Installation of landing gear fueling step. | X | | X | X | X | |
SA3862NM | Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and | X | X | X | X | X | |
SA399AL | Conversion of 4-inch wheels and brakes to 6-inch wheels and brakes. | | | X | | | |
SA4005NM | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND | | X | X | X | X | |
SA4-1210 | Installation of Eonnex cover on aircraft surfaces. | X | | X | X | X | |
SA412NW | Installation of #40-97A Cleveland wheels and #30-63A brakes | | | X | | | |
SA4172NM | Installation of Aviation Development oil filter. | | | X | X | X | |
SA4-302 | Installation of BN-1 propeller spinner. | | | X | | X | |
SA4302NM | Installation of Electronics Int'l digital automatic engine analyzer. | X | | X | X | | |
SA4305WE | Installation of GAR-AERO wheel adapters and tundra type tires on the main landing gear | X | X | X | X | X | |
SA447AL | Fabrication and installation of Stoddard Aero Service Model 15 auxiliary fuel tank in the right | | | X | | | |
SA4503NM | Install Ceconite covering material. | X | X | X | X | X | |
SA460SW | Install wing tips in accordance with Cub Crafters, Inc. Master Drawing List., MDL102400, Revision C, | X | X | X | | | |
SA4635NM | Modification of wing lift struts. | | | X | X | X | |
SA478AL | Installation of fiberglass wing tips. | | | X | | | |
SA489EA | Installation of ARP Inc. carburetor ice detection system | X | X | X | X | X | |
SA4-900 | Ceconite 101 covering of wings, fuselage, ailerons, elevator and rudder. | | | X | | | |
SA4-977 | Installation of Fiberglass rudder post mount for either Grimes or Whelen WRM rotating beacons. | X | X | X | X | X | |
SA5-13 | Installation of 8.50x6 tires and tubes with Hayes 6-inch wheels. | | | X | X | X | |
SA5159NM | Installation of chip detector system. | X | X | X | X | X | |
SA573SW | Installation of Plane Booster wing tip kit 101-250. | X | X | X | X | X | |
SA5778NM | Installation of Lycoming O-290-D2 engine and Sensenich M74DM6-0-56 propeller | | | X | | | |
SA589WE | Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. | | | X | | X | |
SA5924NM | Installation of RPM instrument. | X | X | X | X | X | |
SA5925NM | Installation of oil pressure/temperature instrument. | X | X | X | X | X | |
SA593CH | Install Champion SlickSTART magneto booster system. | X | X | X | X | X | |
SA615EA | Installation of Whelen Anti-Collision Strobe Light Systems, Part Number 01-0770006-( ), | X | X | X | X | X | |
SA630WE | Installation of oil filter assemblies. (NAVION A AND B with optional engine) | | | X | | | |
SA71GL | Installation of air filters | | X | X | X | X | |
SA786NW | Installation of a Lycoming engine | | | X | | | PA-16 S/N 16-505 only |
SA7965SW | Application of fabric and polyurethane finishing system. | X | X | X | X | | |
SA800EA | Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429, A430, A434, A450, | X | X | X | X | X | |
SA8075SW | Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER) | | | X | | | |
SA840NW | Installation of a lycoming engine, Sensenich propeller, PA-22 balanced elevators and an overhead | | | X | | | PA-16 S/N 16-543 only |
SA8438SW | Installation of dual toe brakes including rudder pedals, linkages and torque tubes. | | | X | X | X | |
SA95AL | Maule SFS-1-4-P8 tail wheel; Hayes D-15-26 brake assembly using Kennedy Air Service adapter 64-1; | X | X | X | X | | |
SA99AL | Installation of six-inch wheels and brakes. | X | X | X | X | | |
ST01700NY | Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature | | X | X | X | X | |
ST02291AK-A | Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener | X | X | X | X | X | PA-22 when converted |