# TCDS A-766: Swift Museum Foundation Inc. - Type: Type certificate data sheet - Status: Current - Holder: Swift Museum Foundation Inc. - Revision: 19 - Revised: September 4, 2018 - Product: Aircraft, Small Airplane - Certification basis: Part 11, CAR 4a - Registered aircraft: 541, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/b0/8f/b08fcf3518b00c90edf1aee3d33f5a0f197360a98610b1571bff4729d3ed3121 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2A2D9D3DC18E0372862583080047620D.0001 - Page: https://openairdocs.org/tcds/A-766 ## Models (2) As the data sheet lists them. - GC-1A (Globe) - GC-1B (Globe Swift) ## 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 Rev. No. 18 16 11 16 13 16 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-766 Revision 19 SWIFT (Globe, TEMCO) GC-1A GC-1B September 4, 2018 TYPE CERTIFICATE DATE SHEET NO. A-766 Type Cer tificate Holder: Swift Museum Foundation, Inc. 223 County Roa d 552 Athens, T ennessee 37303-6416 Type Cer tificate Holder Record: Globe Aircraft Company transferred TC 766 to Texas Engineering & Manufacturing Company (TEMCO) in 1947. TEMCO transferred TC 766 to Universal Aircraft Industries on May 14, 1956. Universal Aircraft Industries transferred TC 766 to Univair Aircraft Corporation on April 29, 1966. Univair Aircraft Corporation transferred TC 766 to Swift Museum Foundation, Inc. on July 14, 1980. I - Model GC-1A, 2 PCLM, Approved May 7, 1946 Engine Cont inental, C-85-12 or C-85-12F Fuel 73 min. octane aviation gasoline Engine lim its For all operations, 2575 rpm (85 hp) Airspe ed limits Level flight or climb 140 mph (122 knots) True Ind. Glide or dive 185 mph (161 knots) True Ind. Flaps extended 90 mph ( 78 knots) True Ind. C.G. Ran ge (+31.4) to (+35.5) with L.G. extended. Moment change due to retraction of gear +157 in. lbs. Empty we ight C.G. range (+29.3) to (+30.4) If empty weight C.G. falls within pertinent range, it is unnecessary to check critical forward and aft C.G. positions. Ranges are not valid for non-standard arrangements. Maximu m weight 1570 lbs. No. seat s 2 (+42.5) Maximu m baggage 50 lbs. (+60.5) Fuel capaci ty 27.8 gals. (+47) Oil capaci ty 4.5 qts. (-14.5) Control surface movements Flaps Down 39° or 30° Elevators Up 22° Down 20° Elevator trim tab Up 23° Down 17° Ailerons Up 19.5° Down 15° Rudder Right 24° Left 26° A-766 Page 2 of 6 S erial Nos. eligible 2 to 1000, inclusive (also eligible as GC-1B upon completion of conversion according to TEMCO Customer Service Maintenance Bulletin No. 27, dated June 18, 1948.) R equired equipment In addition to the pertinent required basic equipment specified in CAR 4a, the following items of equipment must be installed: Items 1, 101; 105 or 110 and 111; 201, 202, 301, 302, and 303. II - Model GC-1B, 2PCLM, approved September 20, 1946 E ngine Continental C-125-1 or C-125-2 (See NOTE 3 for optional engine) F uel 80 min. octane aviation gasoline En gine limits For all operations, 2550 rpm (125 hp) A irspeed limits Level flight or climb 140 mph (122 knots) True Ind. Glide or dive 185 mph (161 knots) True Ind. Flaps extended 90 mph ( 78 knots) True Ind. C. G. Range (+29.6) to (+34.7) with L.G. extended. (Moment change due to retraction of gear +157 in. lbs.) Em pty weight C.G. range None M aximum weight 1710 lbs. N o. of seats 2 (+42.5) M aximum baggage 100 lbs. (+60.5) F uel capacity 27.8 gals. (+47) O il capacity 2 gals. (-20.3) Control surface movements Flaps Down 30° Elevators Up 24° Down 18.5° Elevator trim tab Up 10° Down 22° Ailerons Up 19.5° Down 16° Rudder Right 24° Left 26° S erial Nos. eligible 1001 and up. (GC-1A, serial numbers 2 to 1000 inclusive are eligible as GC-1B upon completion of conversion according to TEMCO Customer Service Maintenance Bulletin No. 27, dated June 18, 1948.) R equired equipment In addition to the pertinent required basic equipment specified in CAR 4a, the following items of equipment must be installed: Items 3, 107, 110, 111, 201, 202, 301, 302, and 303. Specifications Pertinent to All Models D atum Forward face of firewall at bottom Leveling means Window sill between (+37) and (+62) Certification basis Type Certificate No. 766 (CAR 4a) Production basis None. Prior to original certification a CAA agent must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data and a check of the flight characteristics. Export eligibility Eligible for export to all countries subject to the provisions of MOP 2-4, except as follows: Canada - Landplane - eligible. - Skiplane - not eligible. A-766 Page 3 of 6 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 herein has been obtained by the aircraft manufacturer except those items preceded by an asterisk (*). The asterisk denotes that approval has been obtained by someone other than the aircraft manufacturer. 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 GC-1A GC-1B 1 P ropeller - Beech controllable, R002 or R003 with R002-205-72, R003-230-72 or R003-235-72 blades. 30 lbs. (-35) - - - - - Dia. 72 in. Pitch at 26 in. sta.: Low 14°, high 19° 2. Propeller - Koppers Aeromatic, F200 with 00-72C, 29 lbs. (-34) - - - - - 00-72D or 00-72F blades. Dia. 72 in. Pitch at 27 in. sta.: Low 11°, high 23.5° 3. Propeller - Sensenich 73KR59, 73BR54 or any other - - - - - 14 lbs. (-40) fixed pitch wood propeller eligible for the engine speed and power and which meets the following limits: Static rpm at max. permissible throttle setting: Not over 2250, not under 2000. No additional tolerance permitted. Dia: Not over 73 in., not under 71.5 in. 4. Propeller - Koppers Aeromatic, F200 with 00-73D, 00-73E, or 00-73F blades with the following limits: (a) Model GC-1A 29 lbs. (-34) - - - - - Parts List Assembly 4305A. Low pitch setting 11° at 24 in. sta. Static rpm at maximum permissible throttle setting: Not over 2525, not under 2525. No additional tolerance permitted. Dia: Not over 73 in., not under 71.5 in. Installation and operation must be accomplished in accordance with Koppers "Installation and Operation Procedure No. 18C." (b) Model GC-1B - - - - - 29 lbs. (-41) Item 108 required. Parts List assembly 4261 or 4277. Low pitch setting 13.6° at 24 in. sta. Static rpm at maximum permissible throttle setting: Not over 2500, not under 2500. No additional tolerance permitted. Dia: Not under 73 in., not under 71.5 in. Installation and operation must be accomplished in accordance with Koppers "Installation and Procedure No. 9B." 5. Propeller - Beech controllable, R002 or R003 with 29 lbs. (-35) - - - - - R 003-201-72T or R003-231-72T blades. Dia. 72 in. Pitch at 27 in. sta.: Low 14.5°, high 19.5° 6. Propeller - Beech controllable R100-101 hub with - - - - - +26 lbs. (-40) R100-217-73T blades. Static rpm at maximum permissible throttle setting: Not over 2275, not under 2175 No additional tolerance permitted. Pitch at 3/4 radius: Low 15°, high 23°. Item 108 required with this item. A-766 Page 4 of 6 GC-1A GC-1B 7. Hampton Spinner Model No. 1B, Dwg. No. 100 - - - - - 2 lbs. (-40) (Opt ional with Koppers Aeromatic F-200 propeller) 8. Propeller - McCauley 1A170 (a) Model 1A170-DM7357 - - - - - 33 lbs. (-40) Static rpm at maximum permissible throttle setting: Not over 2050, not under 1950. No additional tolerance permitted. Diameter: Not over 73 in., not under 71.5 in. Approved on Continental C125-2 engine only (b) Model 1A170-DM7359 - - - - - - 33 lbs. (-40) Static rpm at maximum permissible throttle setting: Not over 2180, not under 2080. No additional tolerance permitted. Diameter: Not over 73 in., not under 71.5 in. Approved on Continental C125-2 engine only *9. Propeller - Sensenich M74DR-1, fixed pitch metal - - - - - - 30 lbs. (-40) Static rpm at maximum permissible throttle setting: Not over 2250, not under 2000. No additional tolerance permitted. 10. - - - - - - 46 lbs. (-40) 11. - - - - - - 51 lbs . (-40) Diameter: Not over 73 in., not under 71.5 in. Approved on Continental C125-2 engine only. Propeller – Hartzell BHC-C2YF-1BF/7663DR, constant speed Pitch settings at 30” station: low 12.8° + 0.2º high 30.0º + 1.0º Diameter: Not ov er 76”, not under 72”, in one inch increments Spinners: Hartzell A-2298-2(P), D-4798P Maintain propeller in acco rdance with Hartzell Owners Manual #115N and Hartzell Maintenance Manual #113B Approved on Continental I O-360 series engine installed per STC SA53NW only. Propeller – Hartzell HC-C2YK-1BF or HC-C2YR-1BF with F7666A-2, c onstant speed (See NOTE 4) Pitch settings at -30 station: low 12. 8° + 0.2º high 35.9º + 1.0º Diameter: Not over 74”, not under 72”, in one inch increments Spinners: Hartzell A-2298-2(P), D-4798P Maintain propeller in acco rdance with Hartzell Owners Manual #115N and Hartzell Maintenance Manual #113B Only approved on Lycoming O-36 0-A1A engine installed per S TC SA803SO. See NOTE 2. Engines and Engine Accessories - Fuel and Oil System 101. Carburetor air heater 2 lbs. (-15) - - - - - 102. Cabin air heater 2 lbs. (-11) - - - - - 103. Oil radiator 4 lbs. (-13) - - - - - 104. Starter - Delco-Remy 1109656 16 lbs. (- 8) - - - - - 105. Two engine-driven fuel pumps 4 lbs. (-26) - - - - - (Upper AC10538-III or Continental 40585-III, lower Continental 40452) 106. Carburetor air filter X X 107. Carburetor air heater - - - - - 1 lb. (-19) 108. Oil radiator (Harrison 3875) - - - - - 4 lbs. (-13) Required when item 4 or 6 is installed. 109. Starter - Delco-Remy A-40098 - - - - - 15 lbs. (- 7) 110. Engine-drive fuel pump (AC1523066) 2 lbs. (-26) 2 lbs. (-33) 111. (a) Wobble pump (Air Corps. Type D-2) 3 lbs. (+34) 3 lbs. (+34) (b) Wobble pump (Aero Supply No. 54609) 1 lb. (+34) 1 lb. (+34) A-766 Page 5 of 6 GC- 1A GC-1B 112. 9-gallon auxiliary fuel tank installation GC-1B - - - - - 14 lbs. (+61) eligible for this installation in the baggage compartment in accordance with Texas Engineering & Manufacturing Company Drawing No. 11-420-5016, Rev A. 113. Fuel tank venting system (TEMCO Drawing No. 11-420-5060). GC-1A (except serial nos. 2 thru 128) and GC-1B below serial no. 3501 eligible for this item in accordance with TEMCO Customer Service Maintenance Bulletin No. 25 dated December 10, 1947. GC-1A, Serial Nos. 2 through 128 eligible for this item in accordance with TEMCO Customer Service Maintenance Bulletin No. 25 Supplement No. 1 dated June 18, 1948. 114. Fram oil-filter (CAA Approved Fram Installation Sheet No. 62604 and 62605) 5 lbs. (- 3) 5 lbs. (- 3) 115. "CODA" exhaust silencers - - - - - 3 lbs. (-22) 116. Davis Model W-125 exhaust silencer installed in accordance - - - - - +8 lbs. (-18) with Davis Installation Dwg. No. W-125-C and Davis Photograph No. P-125-1 (with Item 401 only) 117. Hanlon-Wilson Model 193 muffler -heater exhaust system - - - - - +6 lbs. (-25) per TEMCO Dwg. No. 11-440-5046 "C". Landing Gear and Floats 201. 6.00-6 wheels and brakes (Goodyear L6H/MBL 31 lbs. (+24) 31 lbs. (+24) or LF6H/MDB) with 6.00-6 tires 202. Tail wheel assemblies (a) Scott 6x2.00 4 lbs. (+179) 4 lbs. (+179) (b) 6x2.00, steerable, installed in accordance with 4 lbs. (+179) 4 lbs. (+179) Firestone Dwg. DFA-277. (Item 203 required). (c) 6x2.00, steerable, installed in accordance with 5 lbs. (+179) 5 lbs. (+179) TEMCO Dwg. 11-350-5002. (Item 203 required.) (d) 6x2.00, steerable, TEMCO Assy. No. 11-350-5120. 5 lbs. (+179) 5 lbs. (+179) (Item 203 required) (e) Scott 3250, steerable, installed in accordance with 7 lbs. (+179) 7 lbs. (+179) TEMCO Dwg. 11-351-3630, C change. (Item 203 required) 203. Tail wheel steering mechanism 2 lbs. (+170) 2 lbs. (+170) 204. Copilot brake pedal installation. 5 lbs. (+9) 5 lbs. (+9) Electrical and Radio Equipment 301. (a) Reading R-24 battery and battery box - 26 lbs. (-4) 24 lbs. (-4) 12-volt, 23 amp. hr., 5 hr. rate (b) Willard AW-12-25 manifold vent-battery 12-volt, 24 lbs. (-4) 24 lbs. (-4) 25 amp. hr., 5 hr. rate (c) Concorde RG-35A battery12-volt, 29 amp. hr., 29.5 lbs. (-4) 29.5 lbs. (-4) 5 hr. rate 302. Engine -driven generator (Delco Remy 1101876) 10 lbs. (-8) 10 lbs. (-7) 303. Hydraulic system energizer (Adel model N-15668) 6 lbs. (-3) 6 lbs. (-3) 304. Two-way radio (General Electric AS-1B) 12 lbs. (+16) 12 lbs. (+16) 305. Deleted (equipment same as Item 302) 306. (a) Dual fixed landing lights per TEMCO Dwg. 5 lbs. (+21) 5 lbs. (+21) No. 11-552-R3718, change "B" (b) "CODA" landing lights (Gordon Beach Aircraft 2.5 lbs. (+35) 2.5 lbs. (+35) Service, Installation Dwg. No. S-125-1102) 307. Safe flight stall warning indicator per TEMCO Dwg. No. 11-600-5101, change "B". 1 lb. (+19) 1 lb. (+19) Interior Equipment 401. Draft seal bulkhead, TEMCO part 11-210-5014 No wt. change No wt. change A-766 Page 6 of 6 GC-1A GC-1B Miscellaneous (not listed above) 601. (a) Cabin window installation TEMCO +4 lbs. (+73) +4 lbs. (+73) Dwg. 11-213-5096, Assembly Fuselage "New Look" Kit-without turnover ring. (b) Cabin window and turnover structure installation +7.5 lbs. (+68) +7.5 lbs. (+68) TEMCO dwg. 11-213-5095 change "A" fuselage window and Ring Turnover Structure "New Look" kit. *602. Hydraulic systems modified in accordance with Ruleto, Use actual Ruleto Industries, Inc., 4823 Rosecrans Avenue, weight change Hawthorne, CA, Drawing Nos. R-1004, R-1005, R1006 and installation instructions SHK-1. NOTE 1. Weight and ba lance 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). NOTE 2. Placard ins trument panel: (a) "INTENTIONAL SPINS PROHIBITED." (b) "DO NOT LOWER LANDING GEAR ABOVE 100 MPH." (c) For GC-1B aircraft modified per STC SA803SO and utilizing Hartzell Propeller as provided in Item 11 above, Add placard “AVOID CONTINUOUS OPERATIONS BETWEEN 2000 AND 2250 RPM” NOTE 3. Optional Engine – Teledyne Continental Motors (TCM) model IO-360-D installed in accordance with STC SA53NW. Eligible for installation on model GC-1B. Engine Limits – For all operations: 2800 RPM, FT (210 HP) Fuel, minimum octane – 100LL, B95/130CIS or RH95/130 Oil – 10 quarts (-21) Maximum Weight – 1710 lbs. Airplane CG Limits: (+29.6) to (+33.0) with L.G. extended (moment change due to retraction of gear +157 in. lbs.) .....END.... NOTE 4. When the Lycoming O-360-A1A is installed on the GC-1B per STC SA803SO, Hartzell hub models HC-C2YK-1BF or HC-C2YR-1BF can be used interchangeably with Hartzell blade model F7666A-2 per TC P-920 and the Hartzell Standard Practices Manual 202A 61-01-02 Volume 3 Section 12 Subsection A (Rev 35, dated July 2015) . ``` ## ADs (22, in force first) - [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 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996 - [AD 64-05-06](https://openairdocs.org/ad/64-05-06): Engine Mount · Swift Museum Foundation GC-1B. Effective Feb 27, 1964 - [AD 46-23-04](https://openairdocs.org/ad/46-23-04): Addition of Rivets in Wing Skin · Swift Museum Foundation GC-1A and GC-1B - [AD 46-33-02](https://openairdocs.org/ad/46-33-02): Fuselage Bulkhead Flange Stiffener · Swift Museum Foundation GC-1A and GC-1B - [AD 46-42-01](https://openairdocs.org/ad/46-42-01): Cabin Heater Valve Replacement · Swift Museum Foundation GC-1A and GC-1B - [AD 47-06-01](https://openairdocs.org/ad/47-06-01): Main Landing Gear Retraction System · Swift Museum Foundation GC-1A and GC-1B - [AD 47-06-02](https://openairdocs.org/ad/47-06-02): Landing Gear Retraction Placard · Swift Museum Foundation GC-1A and GC-1B - [AD 47-06-03](https://openairdocs.org/ad/47-06-03): Elevator Cable Collars · Swift Museum Foundation GC-1A and GC-1B - [AD 47-06-04](https://openairdocs.org/ad/47-06-04): Landing Gear Washers · Swift Museum Foundation GC-1A and GC-1B - [AD 47-06-05](https://openairdocs.org/ad/47-06-05): Battery Vent Plugs · Swift Museum Foundation GC-1A and GC-1B - [AD 47-06-06](https://openairdocs.org/ad/47-06-06): Engine Breather Line · Swift Museum Foundation GC-1A and GC-1B - [AD 47-25-06](https://openairdocs.org/ad/47-25-06): Carburetor Flexible Air Duct · Swift Museum Foundation GC-1A and GC-1B - [AD 47-25-07](https://openairdocs.org/ad/47-25-07): Oil Radiator Outlet Sleeve · Swift Museum Foundation GC-1A and GC-1B - [AD 48-28-01](https://openairdocs.org/ad/48-28-01): Fuselage Bulkhead Rework · Swift Museum Foundation GC-1A and GC-1B - [AD 51-02-02](https://openairdocs.org/ad/51-02-02): Asbestos Cloth Removal · Swift Museum Foundation GC-1A and GC-1B - [AD 51-08-03](https://openairdocs.org/ad/51-08-03): Stabilizer Spar Attachment · Swift Museum Foundation GC-1A and GC-1B - [AD 51-10-05](https://openairdocs.org/ad/51-10-05): Fuselage Reinforcement Rework · Swift Museum Foundation GC-1A and GC-1B - [AD 51-11-04](https://openairdocs.org/ad/51-11-04): Landing Gear Rework · Swift Museum Foundation GC-1A and GC-1B - [AD 56-16-04](https://openairdocs.org/ad/56-16-04): Landing Gear Torque Knees · Swift Museum Foundation GC-1A and GC-1B - [AD 58-10-03](https://openairdocs.org/ad/58-10-03): Landing Gear Stop Ring · Swift Museum Foundation GC-1A and GC-1B ## Registered aircraft by registry model (OpenAirDocs) - [Globe GC-1B](https://openairdocs.org/model/globe-gc-1b): 395 aircraft (registry code 9230104) - [Temco GC-1B](https://openairdocs.org/model/temco-gc-1b): 115 aircraft (registry code 9230108) - [Globe GC-1A](https://openairdocs.org/model/globe-gc-1a): 31 aircraft (registry code 9230102) - [Temco GC-1A](https://openairdocs.org/model/temco-gc-1a): 0 aircraft (registry code 9230106) ## STCs approved under this data sheet (176, first 50) - [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [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 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 SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. 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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels 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 SA2GL](https://openairdocs.org/stc/SA2GL): Installation of wheel and brake assemblies and axle spacer.. Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc. - [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): 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 SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA04362CH](https://openairdocs.org/stc/SA04362CH): Installation of the uAvionix skyBeacon Automatic Dependent Surveillance-Broadcast (ADS-B) Out. uAvionix Corporation - [STC SA169NW](https://openairdocs.org/stc/SA169NW): Installation of Merlyn Products motor, part number 06-6001. Merlyn Products Inc. - [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments - [STC SA803SO](https://openairdocs.org/stc/SA803SO): Installation of a Lycoming O-360-A1A engine, equipped with either a McCauley Model 2D34C53-A/74E-0 propeller or a Hartzell Model HC-C2YK-1BF/F7666A-2 propeller. Swift Museum Foundation Inc - [STC SA00184BO](https://openairdocs.org/stc/SA00184BO): Installation of an electric elevator trim system. Swift Museum Foundation Inc - [STC SA00185BO](https://openairdocs.org/stc/SA00185BO): Installation of McCauley 2A34C209/78CCA-2 Propeller. Swift Museum Foundation Inc - [STC SA00910AT](https://openairdocs.org/stc/SA00910AT): Installation of control sticks.. Swift Museum Foundation Inc - [STC SA1-326](https://openairdocs.org/stc/SA1-326): Installation of Teledyne Continental Mode IO-300-A engine with McCauley Model 1A170-DM7359 propeller and Cessna spinner AK7053-3.. Swift Museum Foundation Inc - [STC SA2098SO](https://openairdocs.org/stc/SA2098SO): Installation of a pneumatic squat switch on the landing gear retraction system. Swift Museum Foundation Inc - [STC SA345SO](https://openairdocs.org/stc/SA345SO): Replaced hand operated wobble pump with electric fuel pump. Swift Museum Foundation Inc - [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [STC SA00433NY](https://openairdocs.org/stc/SA00433NY): Installation of Airwolf remote mounted engine oil filter model AFC-500 or AFC-600 on multi engine fixed wing light aircraft incorporating Franklin reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation - [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 SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems.. J P Instruments - [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley - [STC SA10077SC](https://openairdocs.org/stc/SA10077SC): Installation of push-button starter system.. Hartzell Engine Technologies, LLC - [STC SA2996SW](https://openairdocs.org/stc/SA2996SW): Install Brittain Model BSS Stability Augmentation System. Brittain Industries, Inc - [STC SA01768SE](https://openairdocs.org/stc/SA01768SE): Installation of an oil cooler system.. Steve's Aircraft - [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc. - [STC SA02930NY](https://openairdocs.org/stc/SA02930NY): Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. Insight Instrument Corporation All 176: https://openairdocs.org/tcds/A-766/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.