# TCDS 5A2: Textron Aviation Inc. - Type: Type certificate data sheet - Status: Current - Holder: Textron Aviation Inc. - Revision: 22 - Revised: July 29, 2015 - Product: Aircraft, Small Airplane - Certification basis: CAR 3, CAR 4a - Registered aircraft: 234, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/e6/7a/e67a64e93be785138bfd61dd74824d80260ea6a52bfeab21a4accf9144ea8f8a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BFC5F63870B57E1186257ED2006F214F.0001 - Page: https://openairdocs.org/tcds/5A2 ## Models (1) As the data sheet lists them. - 140A ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 4 5 6 7 Rev No. 22 19 20 18 19 20 21 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 5A2 Revision 22 Textron Aviation Inc. 140A July 29, 2015 TYPE CERTIFICATE DATA SHEET NO. 5A2 This data sheet which is part of Type Certificate No. 5A2 prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Textron Aviation Inc. One Cessna Boulevard Wichita, Kansas 67215 Type Certificate Holder Record Cessna Aircraft Company transferred to Textron Aviation Inc. on July 29, 2015 I. Model 140A, 2 PCLM (Utility Category), Approved April 8, 1949, 2 PCSM, Approved June 17, 1949 Engine Continental C-90-12F (See Items 106 and 107 for optional engines) Fuel 80 min. octane aviation gasoline (See NOTE 3 for alcohol-based fuels warning.) Engine Limits For all operations, 2475 rpm (90 hp) Airspeed Limits Landplane: Maneuvering 106 mph True Ind. Maximum structural cruising 115 mph True Ind. Never exceed 140 mph True Ind. Flaps extended 82 mph True Ind. Seaplane : Level flight or climb 105 mph True Ind. Glide or dive 140 mph True Ind. Flaps extended 82 mph True Ind. 5A2 2 Rev. 22 I. Model 140A (cont’d) C.G. Range Landplane: (+33.5) to (+37.0) at 1500 lbs. (+32.8) to (+37.0) at 1279 lbs. or less Straight line variation between points given. 32 34 36 381200 1400 1600 LBS. INCHES REAR LIMIT FRONT LIMIT Seaplane : (+33.5) to (+35.7) at 1556 lbs. (+32.3) to (+35.7) at 1195 lbs. or less. Straight line variation between points given. 32 33 35 36 1200 1400 1600 LBS. INCHES REAR LIMIT FRONT LIMIT 1300 1500 34 Rev. 22 3 5A2 I. Model 140A (cont’d) Empty Weight C.G. Range Landplane: (+31.2) to (+32.7) (Based on pilot and passenger weight of 190 lbs. (CAR 3.113)). 850 882 900 950 1000 1050 LBS. 31 (+31.2) 32 (+32.7) 33 34 INCHES (+32.9) (+34.2) When Empty Weight C.G. falls within this range computation of critical fore and aft C.G. positions is unnecessary. Range is not valid for non-standard arrangements. Seaplane : None Maximum Weight Landplane or skiplane: 1500 lbs. Seaplane (with item 209a): 1556 lbs. No.of Seats 2 (+40) See item 403 for jump seat. Maximum Baggage 80 lbs. (+64). See item 403 for reduction in baggage when jump seat installed. Fuel Capacity 25 gals. total (Two 12.5 gal. tanks in wings (+42), 10.5 gal. usable in each tank). See NOTE 1 for unusable fuel and Item 108 for optional fuel tanks. Oil Capacity 5 or 6 qts. (-13) Control Surface Movements Elevator Up 20° Down 20° Elevator tab Up 6° Down 33° Rudder Left 16° Right 16° Aileron Up 20° Down 14° Flaps Down 43° Stabilizer Fixed Serial Nos. Eligible 15200 through 15724 Required Equipment In addition to the pertinent required basic equipment specified in the applicable regulations (CAR 3 or 4a) the following items of equipment must be installed: Landplane: Item 1, 102, 201(a), 202(a), 204(a), 401(a). Seaplane : Items 2, 102, 209(a), 401(b). Skiplane : Items 1, 102, 208, 210, 401(a). 5A2 4 Rev. 22 Specifications Pertinent to all Models Datum Front face of firewall Leveling Means Top edge of sheet along fuselage side aft of doors Certification Basis: Type Certificate No. 5A2 Landplane: (CAR 3); Skiplane and Seaplane: (CAR 4a). Production Basis: Production Certificate No. 4 Export Eligibility Eligible for export to all countries, subject to the provisions of MOP 2-4, except as follows: (a) Canada - landplane, skiplane and seaplane - eligible. Equipment: A Plus (+) or minus (-) sign preceding the weight of an optional item indicates the net weight change when that item is installed. Approval for the installation of all items of equipment listed here in has been obtained by the aircraft manufacturer except those items preceded by an asterisk (*). The asterisk denotes that approval has been obtained by other than the aircraftmanufacturer. An item marked with an asterisk may not have been manufactured under a CAA monitored or approved quality control system, and therefore attention should be paid to workmanship and conformity with pertinent data called for in this specification. Propellers and Propeller Accessories for C-90 Engine Installation 1. Propeller-Sensenich 72RK-56, 74FK-51, or any other fixed pitch wood 11 lbs. (-32) propeller which is eligible for the engine power and speed and which meets the following limits: Static rpm at maximum permissible throttle setting: Not over 2160, not under 1900. No additional tolerance permitted. Diameter: Not over 74 in., not under 70.5 in. 2. Propeller McCauley 1A90-CF, IA90-CH, or 1B90-CM with the following limits: 21 lbs. (-32) Static rpm at maximum permissible throttle setting: (No additional tolerance permitted.) Landplane: Not over 2350, not under 2000. Seaplane: Not over 2350, not under 2150. Diameter: Landplane: Not over 71 in., not under 69.5 in. Seaplane: Not over 73 in., not under 69.5 in. Propellers and Propeller Accessories for C-85 Engine Installation 11. Propeller-Sensenich 74FC-47, 74FC-49, 74FK-47, 74FK-49, or 74FK-51 or any 11 lbs. (-32) other fixed pitch wood propeller which is eligible for the engine power and speed and which meets the following limits: Static rpm at maximum permissible throttle setting: Not over 2160, not under 1880. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. 12. Propeller-McCauley 1A90-CF, 1A90-CH or 1B90-CM with the following limits: 22 lbs. (-32) Static rpm at maximum permissible throttle setting: Not over 2350, not under 2050. No additional tolerance permitted. Diameter: Not over 71 in., not under 69.5 in. Rev. 22 5 5A2 Specifications Pertinent to all Models (cont’d) Propellers and Propeller Accessories for C-85 Engine Installation (cont’d) 13. Propeller-Beech Controllable, R002-100 or R003-100 series hub 30 lbs. (-32) R003-201-75 to -72; R003-225-75 to -72; R003-231-75 to -72; or R003-232-75 to -72 blades. (Includes Beech mechanical propeller pitch control). When this item is installed, metal rolls (Cessna P/N 0450103-5 and -6 or equivalent) must be installed along bottom edge of firewall. Low pitch static rpm: Not over or under 2300. No additional tolerance permitted. Pitch settings at 27 in. Station: Low 13°, high 19° * 14. Propeller-Hartzell ground adjustable, HA-12UF-1 hub with 7414, 7214, 18 lbs. (-32) or 7214M blades Static rpm and diameter limits same as for fixed pitch wood propeller. Engine and Engine Accessories - Fuel and Oil System 101. Starter (Delco-Remy 1109565) 16 lbs. (-8) 102. Carburetor air heater and mufflers 8 lbs. (-17) 103. Carburetor air filter 3 lbs. (-24) 104. Winterization equipment (Cessna Dwg. 0450102B) 1 lbs. (-29) Outside air temperature gauge per Cessna Dwg. 0411802B or equivalent required. 105. Oil filter, Fram PB-5, installed in accordance with Fram Corp. Dwg. 61528 4 lbs. (-3) or Cessna Dwg. 0450334. 106. Continental C-85-12, -12F, or -14F engine with the following Use actual weight limitations: (Eligible on landplane only) Fuel 73 min. octane aviation gasoline Engine limits For all operations, 2575 rpm (85 hp) Oil capacity 4 1/2 or 5 quarts (-13) Installation of the C-85-12 or -12F engine is the same as the C-90-12F installation except propellers (See Propellers and Propeller Accessories for C-85 Engine Installation) and power plant instrument markings. In addition, engine mount, Cessna Dwg. 0451111, must be used with C-85-14F engine. 107. Continental C-90-14F engine (Limits same as for C-90-12F engine) Use actual weight Engine mount, Cessna Dwg. 0451111, necessary when this engine installed. 108. Two 21 gal. fuel tanks in wings (replaces two 12.5 gal. tanks) +8 lbs. (+41) installed per Cessna Dwg. 0426004. With this item installed, fuel capacity is 42 gals. total at (+41) (18.5 gals. usable in each tank). Fuel selector valve placard, Cessna Dwg. 0511167 or equivalent, and Item 401(c) required when this item installed. Eligible only on airplanes equipped with engines having 6 qt. capacity oil sump. (See NOTE 1 for weight of unusable fuel.) 109. Oil dilution system (Cessna Dwg. 0450336) No weight change * 110. Controllable cowl flaps - SerVair Accessories Model SAC-100A, installed in 2 lbs. (-6) accordance with instructions dated November 8, 1950, Amendment No. 1 dated January 24, 1951, supplied by SerVair Accessories, P.O. Box 557, Williston, North Dakota. Eligible on Serial No. 15200 and up unless Item 13 installed. Landing Gear 201. Two main wheel-brake assemblies, 6.00-6 Type III: (a) Goodyear Model LF6HBD 12 lbs. (+18) Wheel assembly No. 511960-M Brake assembly No. 9520517 (b) Goodyear Model CL6HBM (Castering) 30 lbs. (+18) Wheel Assembly No. 9530242 and 3 Brake Assembly No. 9530368 and 9 Installed in accordance with Cessna Dwg. 0441150 202. (a) Two main 4-ply rating tires, 6.00-6, Type III, with regular tubes 18 lbs. (+18) (b) Two main 4-ply rating tires, 7.00-6, Type III, with regular tubes +1 lb. (+18) (c) Two main wheel 4-ply rating tires, 8.00-6, Type III, with regular +10 lbs. (+18 tubes. Items 202(a), (b) and (c) eligible for use with 201(b). 5A2 6 Rev. 22 Specifications Pertinent to all Models (cont’d) Landing Gear (cont’d) 204. Tail wheel and tire (a) Scott 3-24B steerable 5 lbs. (+217) (b) Maule SFS-1-2 6 lbs. (+217) * (c) Scott Model 3200, steerable, swiveling (installed in accordance 8 lbs. (+217) with Scott Bulletin No. I-168) * (d) Maule Model SFS-1-2-P8 7 lbs. (+217) (e) Goodyear Model 95-0843 8-inch wheel with pneumatic tire in 6 lbs. (+217) accordance with Cessna Dwg. No. 0542110 208. Ski installations: (a) Two Federal A-1500 according to Cessna Dwg. No. 0441102 32 lbs. (+15) * (b) Two Woychik R-1 according to Woychik Dwgs. Nos. 1, 2, and 3 42 lbs. (+14.5) (22 psi tire pressure required) * (c) Federal AWA-1500 Wheel-Ski, Federal Instl. Dwg. 11R395A +35 lbs. Eligible with mechanical conversion on ground only. Retracted Extended Note: Weight and balance shall be checked with ski in retracted and (+16) (+19.5) extended positions. Not eligible with Item 202(c) installed. * (d) Federal AWB-1500 Wheel-Ski, Federal Instl. Dwg. 11R549 76 lbs. Eligible with hydraulic conversion on ground and in flight. Retracted Extended Note: Weight and balance shall be checked with ski in (+11.5) (+14) retracted and extended positions. Not eligible with Item 202(c) installed. Placard required: "Do Not Extend or Retract Skis While in Motion on the Ground." * (e) Federal AWB-1500A Wheel-Ski, Federal Instl. Dwg. 11R896 84 lbs. Eligible with hydraulic conversion on ground and in flight. Retracted Extended Note: Weight and balance shall be checked with ski in retracted (+11.5) (+14) and extended positions. Not eligible with Item 202(c) . Placard required: "Do Not Extend or Retract Skis While in Motion on the Ground." * (f) Woychik Model R-1A according to Woychik Aircraft Equipment 58 lbs. (+13) (Middleton, Wisc.) Dwgs. 1 through 5 (32 psi tire pressure required). Airplane Flight Manual Supplement dated February 27, 1952 is required * (g) Federal AWB-2100 Wheel-Ski, Federal Instl. Dwg. 11R1100 93 lbs. Eligible with hydraulic conversion on ground and in flight. Retracted Extended Note: Weight and balance shall be checked with ski in (+11) (+14.5) retracted and extended positions. Not eligible with Item 202(c). Placard required: "DO NOT EXTEND OR RETRACT SKIS WHILE IN MOTION ON THE GROUND." 209. Float installation (a) Two Edo 88-1650 according to Cessna Dwg. No. 0441100 208 lbs. (+32) * (b) Two Edo 92-1400 according to Edo Dwgs. No. 06704 and No. 06822. 174 lbs. (+33) This item eligible for approval for a maximum weight of 1474 lbs. only. 210. Tail ski installation, one Federal AT-1500 according to Cessna Dwg. No. 0441102 3 lbs. (+214) 211. Two wheel streamlines per Cessna Dwg. 0441143. Not eligible with Item 202(b) or 202(c) 6 lbs. (+18) * 212. Two "no drag" wheel fenders per Liquid Tool Co., Box 299, Morrow, Ohio,Dwg. 105 8 lbs. (+19) * 213. Geisse Safety Gear according to St. Louis Machine Co. Dwgs. 1 and 2 and instructions dated May 5, 1953 (Revised October 8, 1953). Not eligible with Items 201(b), 208, 209, 210, 211 02 212 installed. 12 lbs. (0) Electrical Equipment 301. Generator (Delco-Remy 1101876) 10 lbs. ( -7) 302. Battery - 12 volt, 24 amp. hr. 24 lbs. (+75) 303. Landing light - G.E. 4509, Cessna Dwg. 0426000 2 lbs. (+28) Rev. 22 7 5A2 Specifications Pertinent to all Models (cont’d) Interior Equipment 401. CAA Approved Airplane Flight Manual and pertinent revisions applicable to the particular model and serial number. (a) Landplane and skiplane (b) Seaplane (c) Pipeline Patrol Version (Item 406) Approved September 13, 1949. 402. Cabin heater 403. Jump seat installation, Cessna Dwg. 0413202 (Kit No. 52-3-103C). 2 lbs. (-10) The compartment must be placarded for the weight determined by the 6 lbs. (+64) weight and balance computations except that the total weight shall not exceed 80 lbs. C.G. of passenger in jump seat is at (+64) 404. International flares, 3 Mark I - 1 1/2 min. 18 lbs. (+67) 405. Blind flight cover, Cessna Dwg. 0413267 4 lbs. (+5) 406. Provision for pipeline patrol according to Cessna Dwg. 0411914, Door Assembly (addition of lower window), +1 lb. at (+37); Dwg. 0411915, Message Drop Tube +1 lb. at (+18), and 21 gal. Fuel Tanks, Item 108, +8 lbs. at (+41). Miscellaneous (Not Listed Above) 601. Two stabilizer abrasion boots, Cessna Dwg. 0432161, installed per 2 lbs. (+181) Cessna Dwg. 0432000. * 602. Woychik retractable lifting handles according to Woychik Aircraft Equipment (Middleton, Wisc.) Dwgs. 50 & 50A. 13 ozs. (+134) NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions, when necessary, must be in each aircraft at the time of original certification and at all times thereafter (except in the case of air carrier operators having an approved weight control system). The certificated weight empty and corresponding center of gravity location must include unusable fuel of 24 lbs at (+42) when two 12.5 gal. tanks are installed or 30 lbs. at (+39) when two 21 gal. tanks (Item 108) are installed. (Above values are included in total fuel capacity.) NOTE 2. The following placards must be displayed in front of and in full view of the pilot: (a) "THIS AIRPLANE MUST BE OPERATED AS A UTILITY CATEGORY AIRPLANE IN COMPLIANCE WITH THE FLIGHT MANUAL. - UTILITY - NO ACROBATIC MANEUVERS APPROVED EXCEPT THOSE LISTED IN THE FLIGHT MANUAL" (b) "RETRACT WATER RUDDER BEFORE TAKE-OFF AND LANDINGS" (Applicable seaplane only.) (c) For those aircraft with Item 208(d) or (e) installed: "Do Not Extend or Retract Skis While in Motion on the Ground." NOTE 3. WARNING: Use of alcohol-based fuels can cause serious performance degradation and fuel system component damage, and is therefore prohibited on Cessna airplanes. --- END --- ``` ## ADs (13, in force first) - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2022-08-03](https://openairdocs.org/ad/2022-08-03): Flight Compartment Equipment · Textron 120, 140 and 140A. Effective May 17, 2022 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2004-19-01](https://openairdocs.org/ad/2004-19-01): Upper shoulder harness adjusters · Cessna F150G, F150H, F150J and 129 more. Effective Nov 1, 2004 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [AD 79-10-14 R1](https://openairdocs.org/ad/79-10-14-R1): Fuel Tank Venting · Cessna 140A, 150, 150A and 172 more. Effective May 30, 1988 - [AD 81-15-03](https://openairdocs.org/ad/81-15-03): Engine Inlet Air Filters · Replace existing engine induction air filter (Brackett Aero Filters STC SA693CE or SA71GL). Effective Jul 20, 1981 - [AD 79-08-03](https://openairdocs.org/ad/79-08-03): Electrical System · Cessna 120, 140, 140A and 152 more. Effective Jun 6, 1979 - [AD 62-24-03](https://openairdocs.org/ad/62-24-03): Cabin Heat System · Lycoming O-235-C1, O-235-C2C, O-290-D, O-290-D2, O-320 engine (Luscombe STC SA4-173 or 5 others). Effective Nov 21, 1962 - [AD 61-25-01](https://openairdocs.org/ad/61-25-01): Met-Co-Aire Landing Gear · Cessna 120, 140 and 140A. Effective Dec 20, 1961 - [AD 50-31-01](https://openairdocs.org/ad/50-31-01): Fin Spar Reinforcement · Cessna 120, 140 and 140A - [AD 51-21-01](https://openairdocs.org/ad/51-21-01): Rudder Rib Flanges · Cessna 120, 140 and 140A - [AD 86-26-04](https://openairdocs.org/ad/86-26-04) (historical): Shoulder Harness Adjuster · Cessna Aircraft Company, The 120, 140, 140A and 134 more. Effective Jan 6, 1987 ## Registered aircraft by registry model (OpenAirDocs) - [Cessna 140A](https://openairdocs.org/model/cessna-140a): 234 aircraft (registry code 2071604) ## STCs approved under this data sheet (173, first 50) - [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc. - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA5581SW](https://openairdocs.org/stc/SA5581SW): Installation of ALCOR true-flow/ totalizer system. Alcor LLC - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd. - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC - [STC SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc. - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc. - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine - [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA00897WI](https://openairdocs.org/stc/SA00897WI): Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery.. Aero-Mach Wilco LLC - [STC SA3-423](https://openairdocs.org/stc/SA3-423): Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels.. F.Atlee Dodge Aircraft Services - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA13GL](https://openairdocs.org/stc/SA13GL): Installation of Cleveland wheel No. 40-97A and brake No. 30-63A. Kaman Corporation Aircraft Wheel & Brake LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc. - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc - [STC SA04382CH](https://openairdocs.org/stc/SA04382CH): Installation of seat rail supports and Cessna 150 seats in accordance with Lowe Aviation Aircraft Maintenance instructions as listed on AML No. SA04382CH, issued July 18, 2019, or later approved FAA revision.. David Lowe dba Lowe Aviation Aircraft Maintenance - [STC SA1398SO](https://openairdocs.org/stc/SA1398SO): Remove drain plug AN-806-6 from fuel line drain in belly of aircraft and replace with drain valve MT-101-1. (See limitations). Saf-Air Products Inc. - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA01139CH](https://openairdocs.org/stc/SA01139CH): Installation of W.D. Davis V.I.C.C.L. Cessna Cowl Latch.. Kenneth E. Morris and Lorraine R. Morris - [STC SA4-376](https://openairdocs.org/stc/SA4-376): Installation of a Lycoming O-235-C1 or O-235-C2C engine. John P. Warren - [STC SA4-581](https://openairdocs.org/stc/SA4-581): Installation of a Lycoming O-290-D engine and Sensenich M76AM-2 or Sensenich CS3FM4 propeller. John P. Warren - [STC SA4-640](https://openairdocs.org/stc/SA4-640): Installation of a Lycoming O-290-D2 engine and Sensenich M74DM propeller. John P. Warren - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC - [STC SA01838WI](https://openairdocs.org/stc/SA01838WI): Installation of a FreeFlight 1201 GPS receiver, with an Avidyne AXP340 Transponder, for ADS-B Out. Trego Dugan Aviation - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation All 173: https://openairdocs.org/tcds/5A2/stcs.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.