# TCDS A-769: Sky Enterprises Inc. - Type: Type certificate data sheet - Status: Current - Holder: Sky Enterprises Inc. - Revision: 16 - Revised: June 29, 2015 - Product: Aircraft, Small Airplane - Certification basis: CAR 3 - Registered aircraft: 126, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/28/e8/28e88f0837cc1c333cfad0312fa7c277250a0416f6c165ee9539d2c346d39b55 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C679A2C9DFA6CEBD86257E740061FF36.0001 - Page: https://openairdocs.org/tcds/A-769 ## Models (1) As the data sheet lists them. - RC-3 ## 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 REVISION NO. 16 16 16 16 16 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-769 Revision 16 STOL (REPUBLIC) RC-3 June 29, 2015 AIRCRAFT SPECIFICATION NO. A-769 This data sheet which is part of Type Certificate No. A-769 prescribes conditions and limitations under which the product for which the type certificate was issued meet the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder Sky Enterprises, Inc. 10501 Shivalik Circle Anchorage, AK 99507 I - Model RC-3, 4 PCAmM (Normal Category), 2 PCAmM (Utility Category), Approved October 15, 1947 (See NOTES 4, 5 and 6 for flying boat versions). Engine Franklin 6A8-215-B8F Fuel 80 min. octane aviation gasoline Engine limits For all operations, 2500 rpm (215 hp) Airspeed limits (TIAS) Normal Utility Max. structural cruising 117 mph (102 knots) 117 mph (102 knots) Maneuvering 117 mph (102 knots) 117 mph (102 knots) Never exceed 148 mph (129 knots) 159 mph (138 knots) Flaps extended 105 mph ( 91 knots) 105 mph ( 91 knots) C.G. range (+111.5) to (+118.3). Gear retraction moment +2900 in.-lb. (landing gear extended) Empty weight C.G. range None Maximum weight Normal - 3150 lb. Utility - 2810 lb. No. seats 4 (two at +62, two at +96) Maximum baggage 200 lb. (+118) Fuel capacity 75 gal. (tank in hull at +116) Oil capacity 3 gal. (+136) Control surface movements Elevators Up 28° Down 28° Elevator tabs Up 25° Down 25° Ailerons Up 20° Down 20° Rudder Left 30° Right 30° Flaps Up 0° Down 30° Serial Nos. eligible 6 and up 2 A-769 PAGE NO. 1 2 3 4 5 REVISION NO. 16 16 16 16 16 Required equipment In addition to the pertinent required basic equipment specified in CAR 3, the following items of equipment must be installed: 1, 101, 102, 200, 201, 202, 403 and also 300, 301 and 303 when 103 is installed. SPECIFICATIONS PERTINENT TO ALL MODELS Certification basis CAR 03 effective November 13, 1945 Type Certificate No. 769 issued October 15, 1947 Application for Type Certificate dated August 21, 1945 Production basis None. Prior to original certification of each aircraft, an FAA representative must perform a detailed inspection for workmanship, materials, and conformity with approved technical data, and a check of the flight characteristics. Datum Hull Sta. 0, located 97.5 in. forward of wing leading edge. Leveling means Lugs on front and rear left and right-hand door frames. Equipment: A plus (+) or minus (-) sign preceding the weight of an item of equipment 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 (*). This symbol denotes that approval has been obtained by someone other than the aircraft manufacturer. An item so marked may not have been manufactured under an FAA monitored or approved quality control system and therefore conformity must be determined if the item is not identified by a Form FAA-186, PMA or other evidence of FAA production approval. Propeller and Propeller Accessories 1. Controllable and reversible (see NOTE 2 for applicable placards) (a) Hartzell hub HC12x20-2 with blades L8427 or L8433 64 lb. (+178) Diameter: L8427 blades - not over 84 in. not under 82 in. L8433 blades - 84 in. - no cutoff permitted Pitch settings at 30 in. sta.: Blades 8427 - Normal operation +17° to +18° Reverse thrust operation -15° to -14° Note: total angular travel not to exceed 32° Blades 8433 - Low 13-1/2°, high 19-1/2° Reverse -14° (b) Hartzell hub HC-12x20-3, -3A, -3C or -3E with L8427 or +3 lb. (+178) L8433 blades (Similar to 1(a) except for larger operating cylinder and piston) Diameter and pitch limits same as 1(a). Franklin 6A8-215-B8F engines, S/N 23281 and up, and all -B9F engines are equipped with floating or ball thrust bearings for reverse thrust propeller operation. -B8F engines with S/N below 23281 not eligible with HC-12x20-3 propeller unless modified by incorporation of floating or ball thrust bearings as indicated by "F" or "B" affixed to the serial number. See NOTE 4 of Engine Specification E-242 for additional information. Engine and Engine Accessories - Fuel and Oil System 101. Fuel pump AC Spark Plug Model B-F(2) 4 lb. (+148) 102. Oil cooler - Heat Exchange, Inc. model 100 13 lb. (+140) 103. Engine - Franklin 6A8-215-B9F (same as -B8F except S/N 23501 and up equipped with magneto and battery ignition) 104. Oil cooler - United Air Products model U-3170-D-5 22 lb. (+137) Eligible only when installed per Installation Instructions No. 1 dated January 11, 1951, furnished by Kenmore Air Harbor, Inc., Box 64, Kenmore, Washington 3 A-769 PAGE NO. 1 2 3 4 5 REVISION NO. 16 16 16 16 16 Landing Gear 200. Two main wheel-brake assemblies, 7.00-8, Type III (a) Goodrich 6056A, with 4-ply rating 7.00-8 Type III tires & tubes 55 lb. (+93) Wheel assy. G-3-410-A Brake assy. D-2-540 (b) Goodrich 6056AD, with 4-ply rating 7.00-8 Type III tires & tubes 52 lb. (+93) Wheel assy. G-3-410-AD Brake assy. D-2-540 201. Tail wheel assy. 10.00, Type I, with 4-ply rating tire (a) Goodyear PD-173 (b) Bendix 146413 (c) Bendix 146414 (d) Firestone BO-200-F 202. Tail wheel gear with wheel and tire (a) Free swivel lock, S/N 6 thru 875 39 lb. (+225) (b) Steerable, S/N 876 and up, Republic dwg. 17F42001B 42 lb. (+236) and 17F30000G. If this item installed on S/N 6 thru 875, an additional 7 lb. nose ballast must be added. 203. Skis Use actual weight change (a) Federal A3500 (b) Federal AT3500 tail ski Optional when Federal A3500 main skis installed. Remove 30 lb. ballast when skis are installed. Floats may be removed with skis installed. Electrical Equipment 300. Battery (a) Auto Lite CF129 Form 221 52 lb. (+14) (b) Mitchell Type 2SM-9, 12 v. 60 a. hr. 45 lb. (+14) (c) Exide Type 2SM, 12 v. 53 a. hr. at 20 hr. rate 39 lb. (+14) 301. Generator 23 lb. (+126.5) 302. Starter 22 lb. (+128) 303. Voltage regulator (airplane S/N's 6 thru 520) 1 lb. (+110) (airplane S/N's 521 and up) 2 lb. (+22.5) 304. Cross-country instrument panel (optional) +2 lb. (+40) 306. Landing light - Grimes D3150 (optional) 2 lb. (+35) 307. Landing light - Grimes G2900-12 (Land Aviation Corp. Kit RC-3L) 5 lb. (+10) Interior Equipment 400. Anchor equipment (when anchor or line is removed, add equal weight of ballast to anchor compartment cover). (a) Anchor and hemp line 16 lb. (+40) (b) Anchor and cotton braided line 11 lb. (+40) (c) Anchor and nylon line 8 lb. (+40) 401. Life Preservers, front seats 4 lb. (+67) Life Preservers, rear seats 4 lb. (+101.5) (Cushions on backs of front and rear seats are approved life preservers, Republic No. SK17-15944). 402. Fire extinguisher 7 lb. (+65) 403. FAA Approved Airplane Flight Manual (current issue) 404. Stewart-Warner 977-B-1 cabin heater installation (when this heater installed and 23 lb. (+21.5) connected for operation, a hand fire-extinguisher accessible to pilot during flight must be installed. Also, when this heater is installed 20 lb. ballast must be removed). 4 A-769 PAGE NO. 1 2 3 4 5 REVISION NO. 16 16 16 16 16 NOTE 1. Current weight and balance report together with list of equipment included in certificated empty weight and loading instructions when necessary must be provided for each aircraft at the time of original certification. Approximately 53 lb. of ballast required at (+4.5). Actual ballast required should be determined from weight and balance data. NOTE 2. The following placards shall be placed on the instrument panel in full view of pilot: “This airplane must be operated as a Normal or Utility Category airplane in compliance with the FAA Approved Flight Manual applicable in each case.” “All markings and placards on this airplane apply to Normal Category. For Utility Category, refer to the FAA Approved Airplane Flight Manual for airspeed, weight and maneuver limits.” For airplanes with Franklin 6A8-215-B8F engines, S/N's 23001 thru 23280 (only item 1(a) propeller eligible on these engines): “Warning - reversing propeller in flight prohibited. Operate reverse lever in low pitch only. Maximum 1750 r.p.m. in reverse pitch.” For airplanes with Franklin 6A8-215-B8F engines, S/N's 23001F thru 23280F and 23281 and up and all B9F engines (see NOTE 4, Spec. E-242) and (a) HC-12x20-3 or -3A propellers: “Warning - reversing propeller in flight prohibited. Operate reverse lever in low pitch only. Maximum 2300 r.p.m. in reverse pitch,” or (b) HC-12x20-2, -3C or -3E propellers: “Warning - reversing propeller in flight prohibited. Operate reverse lever in low pitch only. Maximum 2500 r.p.m. in reverse pitch.” NOTE 3. Alternate pitot tube installation above pilot's compartment per dwg. 17F81030 is also acceptable. NOTE 4. Amphibian may be converted to flying boat by removing complete main gear and tail wheel assemblies, including actuating mechanism (approximate decrease in empty weight 196 lb. at +119) provided following is accomplished: (a) Plug unused hydraulic lines and provide watertight seal at hull openings resulting from removal of main landing gear. (b) Check weight and balance, and adjust weight of nose ballast to maintain most forward and aft C.G. locations within the specified limits. (Loading schedule in flight manual is not applicable to flying boat). (c) Replace present takeoff and landing procedure placard with the following: Takeoff Landing Flaps down Mixture - full rich Propeller - low pitch Flaps down Mixture - full rich Propeller - low pitch Carburetor Heat - off NOTE 5. Eligible as 5-place flying boat when converted per “Flyers Service Seabee Five-Place Conversion Kit No. 1” and R. G. Hunt, Middlebury Airport, Middlebury, Vermont Kit Instructions dated April 10, 1950. NOTE 6. Amphibian may be converted to flying boat by unbolting the main landing gear only (approximate decrease in empty weight 115 lb. at +93) provided the following is accomplished: (a) A self-sealing hydraulic coupling is used for each brake line at the hull surface. (b) An adequate seal or seaplane corrosion proofing is used for main landing gear supporting tube. (c) Check weight and balance and adjust weight of nose ballast to maintain most forward and aft C.G. locations within the specified limits. (Loading schedule in flight manual is not applicable to flying boat). .....END..... ``` ## ADs (25, 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 47-21-11](https://openairdocs.org/ad/47-21-11): Firewall Stud Bushings · Sky Enterprises RC-3 - [AD 47-21-12](https://openairdocs.org/ad/47-21-12): "No Smoking" Placard · Sky Enterprises RC-3 - [AD 47-21-13](https://openairdocs.org/ad/47-21-13): Elevator Push-Pull Tube Rivets · Sky Enterprises RC-3 - [AD 47-21-14](https://openairdocs.org/ad/47-21-14): Elevator Control Cable Guide · Sky Enterprises RC-3 - [AD 47-21-15](https://openairdocs.org/ad/47-21-15): Radio Filters · Sky Enterprises RC-3 - [AD 47-21-16](https://openairdocs.org/ad/47-21-16): Fuel Strainer Drain · Sky Enterprises RC-3 - [AD 47-21-17](https://openairdocs.org/ad/47-21-17): Backfire Screen · Sky Enterprises RC-3 - [AD 47-21-18](https://openairdocs.org/ad/47-21-18): Mixture Control Support Bracket · Sky Enterprises RC-3 - [AD 47-21-19](https://openairdocs.org/ad/47-21-19): Control Clamps or Brass Ferrules · Sky Enterprises RC-3 - [AD 47-21-20](https://openairdocs.org/ad/47-21-20): Oil Pressure Gage Line Restrictor · Sky Enterprises RC-3 - [AD 47-21-21](https://openairdocs.org/ad/47-21-21): Tip Float Struts · Sky Enterprises RC-3 - [AD 47-21-22](https://openairdocs.org/ad/47-21-22): Engine Mounting Bolt Lock Washers · Sky Enterprises RC-3 - [AD 47-21-23](https://openairdocs.org/ad/47-21-23): Engine Cooling Fan · Sky Enterprises RC-3 - [AD 47-47-10](https://openairdocs.org/ad/47-47-10): Float Strut Rework · Sky Enterprises RC-3 - [AD 47-47-11](https://openairdocs.org/ad/47-47-11): Propeller Reverse Control Spring · Sky Enterprises RC-3 - [AD 47-47-12](https://openairdocs.org/ad/47-47-12): Carburetor Antiswirl Vanes · Sky Enterprises RC-3 - [AD 47-47-13](https://openairdocs.org/ad/47-47-13): Hartzell Propeller Hub Counterweight · Sky Enterprises RC-3 - [AD 47-47-14](https://openairdocs.org/ad/47-47-14): Oil Screen Inspection · Sky Enterprises RC-3 - [AD 47-51-08](https://openairdocs.org/ad/47-51-08): Tailwheel Horns · Sky Enterprises RC-3 - [AD 48-01-03](https://openairdocs.org/ad/48-01-03): Elevator Trim Tab Bushing · Sky Enterprises RC-3 - [AD 48-11-04](https://openairdocs.org/ad/48-11-04): Hydraulic Pump Handle · Sky Enterprises RC-3 - [AD 49-03-01](https://openairdocs.org/ad/49-03-01): AC Fuel Pump · Sky Enterprises RC-3 - [AD 49-31-02](https://openairdocs.org/ad/49-31-02): Fuel Placard · Sky Enterprises RC-3 - [AD 53-23-03](https://openairdocs.org/ad/53-23-03): Strut Fitting Corrosion · Sky Enterprises RC-3 ## Registered aircraft by registry model (OpenAirDocs) - [Republic RC-3](https://openairdocs.org/model/republic-rc-3): 122 aircraft (registry code 3080202) - [Downer RC-3](https://openairdocs.org/model/downer-rc-3): 2 aircraft (registry code 3080206) - [Republic Aviation Corp USA SEABEE RC-3](https://openairdocs.org/model/republic-aviation-corp-usa-seabee-rc-3): 1 aircraft (registry code 3080205) - [Simuflight Seattle-1-Stol RC-3](https://openairdocs.org/model/simuflight-seattle-1-stol-rc-3): 1 aircraft (registry code 5410103) - [Stol Amphibian RC-3](https://openairdocs.org/model/stol-amphibian-rc-3): 0 aircraft (registry code 8670102) ## STCs approved under this data sheet (138, first 50) - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc. - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc. - [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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc. - [STC SA3968NM](https://openairdocs.org/stc/SA3968NM): Installation of fuel cell.. Aerosport Fuel Cells, LLC - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc. - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [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 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 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 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 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 SA537NW](https://openairdocs.org/stc/SA537NW): Installation of a Motorola model 12N55 alternator and Model R2-2 voltage regulator, Stewart Warner Model 240-D-12 priming pump (electric) and an EDO Float (hull) booster (scallop). Kenmore Air Harbor LLC - [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 SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments - [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc. - [STC SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE 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 SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems.. J P Instruments - [STC SA02560SE](https://openairdocs.org/stc/SA02560SE): Installation of a Lycoming Engines IO-540- K1B5 and an MT-Propeller Entwicklung GmbH MTV-9-B-C-R(M)/CRLD203-58 propeller. Transitions Aircraft, Inc - [STC SA1293NW](https://openairdocs.org/stc/SA1293NW): Installation of a Lycoming IO-540-K1B5 engine, Hartzzell HC-E3YR-7LF/LFC8468-4R propeller, and associated systems. Randy Michael Komko - [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [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 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 - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA00194BO](https://openairdocs.org/stc/SA00194BO): Installation of Aircraft Components, Inc. Landing Gear Warning System for Amphibian Aircraft, P/N 2042. Aircraft Components Inc - [STC SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [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 - [STC SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.. Garmin International Inc - [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments - [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments - [STC SA00656SE](https://openairdocs.org/stc/SA00656SE): Installation of a Lycoming TIO540-A2C engine, a Hartzell HC-E3YR-7LF/FLC8468-4R propeller, and a manual waste gate control system. Mr. Henry Ruzakowski - [STC ST00961LA](https://openairdocs.org/stc/ST00961LA): Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29, 2000, or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1, "Slug Thrower Cartridges Master Drawing List", Revision N/C, dated June 26, 2000, or later FAA approved revisions.. AMETEK AMERON LLC d/b/a MASS Systems - [STC SA1315WE](https://openairdocs.org/stc/SA1315WE): Installation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision.. Universal Corporation All 138: https://openairdocs.org/tcds/A-769/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.