# TCDS A-649: Textron Aviation Inc. - Type: Type certificate data sheet - Status: Current - Holder: Textron Aviation Inc. - Revision: 5 - Revised: November 27, 2017 - Product: Aircraft, Small Airplane - Registered aircraft: 124, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/9b/4c/9b4c5fa2e67a826a397450b11a6a16057f0ffaf6f58785afec30f47bbe061a9f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A3B394340A08A289862581EF0060C7C5.0001 - Page: https://openairdocs.org/tcds/A-649 ## Models (2) As the data sheet lists them. - D17S - SD17S ## 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. 5 1 1 1 1 1 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-649 Revision 5 Textron Aviation D17S (Army UC-43, UC*43B, Navy GB-1, GB-2) SD17S November 27, 2017 TYPE CERTIFICATION DATA SHEET NO. A-649 This data sheet which is a part of Type Certificate No. A-649 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, KS 67215 Type Certificate Holder Record Beech Aircraft Corporation transferred to Raytheon Aircraft Company on April 15, 1996 Raytheon Aircraft Company transferred to Hawker Beechcraft Corporation on March 26, 2007 Hawker Beechcraft Corporation transferred to Beechcraft Corporation on April 12, 2013 Beechcraft Corporation transferred to Textron Aviation Inc. on October 12, 2016 I. Model D17S (Army UC-43, UC-43B; Navy GB-1, GB-2), 5 PCLB, Approved July 16, 1937; Model SD17S, 5 PCSB, Approved September 1, 1937. See NOTE 3 for modifications for conversion of military models. Model D17S same as D17R, TC 638, and D17A, TC 713, except for engine installation. Model SD17S same as D17S except for landing gear. Engine P & W Wasp Jr. SB with one 4 1/2N and one 9N damper. (See Item 316 for optional engines). Fuel 80 min. octane aviation gasoline for continuous and take-off rating of 400 hp. 87 min. octane aviation gasoline for take-off rating of 450 hp. When 87 octane fuel is used, in order to utilize 450 hp for take- off one fuselage tank filler must be marked 87 octane minimum. Tank selector valve placard then should designate the fuselage tank and state that 87 octanes must be used for take-off. Engine limits Maximum continuous (Sea level) 34.5 in. Hg., 2200 rpm (400 hp) (Straightline manifold pressure variation with altitude to 5000 ft.) 33.5 inHg, 2200 rpm (400 hp) Take-off (one minute) 34.5 inHg, 2200 rpm (400 hp) 36.5 inHg, 2300 rpm (450 hp) A-649 2 Rev. 5 I. Model D17S, Model SD17S (cont’d) Airspeed limits Landplane Level flight or climb 211 mph (T.I.A.S.) Glide or dive 240 mph Flaps extended 115 mph Seaplane Level flight or climb 172 mph Glide or dive 209 mph Flaps extended 115 mph C.G. range Landplane (+16.4) to (+26.0) Serial Nos. 425 and up are eligible as landplane with rear C.G. limit of (+27) (25.2% MAC). Serial Nos. below 425 also eligible for this rear C.G. limit when elevator trim tabs with a rounded nose section (Dwg. D176111) are installed. Seaplane (+19.1) to (+27.7) Datum Lower wing leading edge. Leveling means Airplane is level when stagger (horizontal distance between wing trailing edges near fuselage) is 25.6 in. Army UC-43, Navy GB-2 airplanes have leveling lugs just inside baggage compartment doors. Maximum weight Landplane 4250 lbs. Seaplane 4650 lbs No. seats 5 (two at +18 and three at +62) Maximum baggage 125 lbs. (+88) Fuel capacity 102 gals. (One fuselage tank, 29 gals. (+32); one fuselage tank, 49 gals. (+55); one lower right wing tank, 24 gals. (+24)). (See Items 116, 205 and 314 for optional fuel tanks). Fuel placard required: "Use fuselage tank for take-off and landing. Fill fuselage tank(s) before filling wing tank(s). Use wing tank(s) before using fuselage tank(s)." Oil capacity 6 1/2 gals. (-17) Control surface movements Elevators 30° up 28° down Elevator tab 14.5° up 14.5° down Ailerons 33° up 25° down Rudder 28° right 28° left Rudder tab 20° right 20° left Flaps 43° down Serial Nos. eligible 136 and on, and all AAF and Navy Nos. (Use Manufacturer's number, if available). Required equipment Landplane Items 101, 102, 103, 104, 105, 106, 107, 108, 109, 110, 111, 112, 113, 114, 116(a) or (b). Seaplane Items 101, 102, 103, 104, 108, 109, 110, 111, 113, 114,116(a) or (b), 151, 152, 153. Rev. 5 3 A-649 Specifications Pertinent to All Models Certification Basis: Type Certificate No. 649 (Aero. Bulletin 7A requirements) Production Basis: None. Prior to original certification of each aircraft subsequent to March 25, 1947, must satisfactorily pass: (a) An inspection for workmanship, materials and conformity before any covering, metal priming or final finish is applied. All woodwork may be varnished. (b) A final inspection of the completed aircraft. (c) A check of the flight characteristics. Export eligibility: Eligible for export to all countries except as follows subject to the provisions of ASR 312 (MOP 2-4 contains the same information): Canada -Landplane and Seaplane eligible. Skiplane not eligible. However, structure complies with Canadian requirements for ski gear when Item 310 is installed. Maximum pedestal height is 17 inches. Tread is same as landplane. Equipment: A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. Propellers and Propeller Accessories 114. Propellers - Hamilton Std. hub 2D30 with (a) Blades 6095A-15, -16 or 6167A-15, -16 157 lbs. (-59) (Pitch settings, Low 11°, high 26°) or (b) Blades 6101A-21T, -22T 163 lbs. (-59) Diameter 8'3-1/8" max., 8'7/8" min. 218. Constant speed governor (Ham. Std. Type 1A2) 6 lbs. (-26) 224. Propeller spinner (Spartan) (Dwg. I-179002) 10 1/2 lbs. (-59) Engines and Engine Accessories - Fuel and Oil Systems 101. Engine ring cowling (NACA type) 39 lbs. (-44) 102. Carburetor air heater (muff type) 6 lbs. (-30) 103. Starter (Eclipse E80 or Type 397, Model 13) 20 lbs. (-26) 109. Oil radiators (a) One radiator (Dwg. D17S9850) with NACA cowl 28-7/8" long (Horizontal centerline) 8 lbs. (-32) (b) Two radiators (Dwg. D17R9850) with NACA cowl 29-3/16" long (horizontal centerline) 8 lbs. ea. (-32, -34) (c) One radiator (Dwg. 94-189850) 12 lbs. (-26) 110. Wobble pump (Type D-2) 4 lbs. (+12) 111. Engine driven fuel pump (Pesco 400 series; Romec RD-3080, -4190) 5 lbs. (-29) 115. Carburetor, cold air ducts and filters 11 lbs. (-48) 116. Fuselage fuel tanks (a) 29 gallon tank 17 lbs. (+32) (b) 49 gallon tank 23 lbs. (+55) 204. Oil tank - 8, 9 1/2 or 11 gals. 205. Auxiliary fuel tanks (a) One 23 or 24 gal. tank, upper right wing 20 lbs. (+47) (b) One 23 or 24 gal. tank, upper left wing 20 lbs. (+47) When upper wing tanks are installed add the following to fuel placard: "Fill lower wing tank before filling upper wing tanks. Use upper wing tanks before using lower wing tanks." (c) One 23 or 24 gal. tank, lower left wing 20 lbs. (+24) (May replace lower right wing tank and/or Item 116(a) provided Item 116(b) is installed). 207. Ignition shielding (a) Breeze 15 lbs. (-45) (b) Packard 10 lbs. (-45) A-649 4 Rev. 5 Specifications Pertinent to All Models (cont’d) Engines and Engine Accessories - Fuel and Oil Systems (cont’d) 219. Special oil drain and oil radiator by-pass valve 2.5 lbs. (-28) 220. Exhaust gas analyzer (Breeze or Cambridge) 5 lbs. (-8) or (-28) 314. 23 gal. fuel tank in lower right wing replacing 24 gal. tank Neglect weight change 316. Engine (must have one 4 1/2N and one 9N damper) Use act. wt. increase (a) P & W Wasp Jr. SB-2 (Limits same as SB) (b) P & W Wasp Jr. SB-3 (Limits same as SB) (c) P & W Wasp Jr. T1B2 Limits Maximum continuous (Sea level 35 in. Hg., 2200 rpm (400 hp) (Straight line manifold pressure variation with altitude to 3800 ft.) 34 in. Hg., 2200 rpm (400 hp) Take-off (one minute) 37.5 in. Hg., 2300 rpm (450 hp) (d) P & W Wasp Jr. T1B3 (Limits same as T1B2) (e) Military R-985-AN-4 (Limits same as SB) (f) Military R-985-AN-6 or -AN-6B (Limits same as SB) (g) Military R-985-AN-12 or -AN-12B (Limits same as SB) (h) Military R-985-AN-14B (Limits same as SB) (i) Military R-985-25 (Limits same as T1B2) (j) Military R-985-AN-1 or -AN-3 (Limits same as T1B2) Landing Gear 106. 7.50-10 wheels (Goodyear 10 HBM) with 7.50-10 6-ply tires (wheel must be placarded for 6-ply tires) 75 lbs. (+5) 107. 10x3 tail wheel 5 lbs. (+211) 151. Edo WA-4665 floats with water rudders 223. Dual brake control installation +8 lbs. (-6) 305. Hand brakes (co-pilot) +2 lbs. (-8) 306. Hand operated parking brake 2 lbs. (-4) 307. Emergency wood landing skids (Dwg. E170140) 16 lbs. (+22) 308. Puncture proof tubes +8 lbs. (+5) 310. Skiplane landing gear (Dwgs. D17820 and D17840) +3 lbs. (+20) 311. 10 in. smooth contour tail wheel assembly with 6-ply tire +1 lbs. (+211) Electrical Equipment 104. Generator 15 amp. (Eclipse LV-180) 15 lbs. (-24) 105. Battery (Exide 6TS-13-1) 36 lbs. (-21)or(+92) 112. Landing gear motor (Dumore D5, 40 amp. fuse reqd.) 9 lbs. (+6) 113. Flap motor (Dumore KL, 30 amp. fuse reqd.) 8 lbs. (+45) 201. Generator (a) 25 amp. (Eclipse D) 20 lbs. (-23) (b) 50 amp. (Eclipse E) 25 lbs. (-23) 217. Landing lights (a) 1 or 2 (Hall A-6) 3.5 lbs. ea. (+35) (b) 1 or 2 (Grimes ST-250) 3.5 lbs. ea. (+21) (c) 1 or 2 (Grimes ST-1000 or ST-1220) 6 lbs. ea. (+25) 312. Flap motor (Dumore K special 4253 flexible drive) (30 amp. fuse required) 5 lbs. (+42) 313. Cannon plug (for electric starter) 3 lbs. (-2)or(-8) Rev. 5 5 A-649 Specifications Pertinent to All Models (cont’d) Interior Equipment 108. Swing-over control column (See Item 301) 11 lbs. (+6) 202. Cabin heater (Muff type) 4 lbs. (-30) 203. Fire extinguisher (Pressure type) (a) Lux - 2 lbs. 12 lbs. (-12) (b) Lux - 5 lbs. 21 lbs. (-12) (c) Pyrene No. 56 17 lbs. (-12) (d) Lux - 5 lbs. (Dwg. I-170555) 21 lbs. (+60) (e) Ace 10 lbs. (-10) (f) Walter Kidde - 5 lbs. 21 lbs. (-22) 206. Parachute flares (a) 3 - 1 1/2 minute (International MK-1) 18 lbs. (+78) or (+108) (b) 1 or 2 - 3 minute (Wiley A-8) 18 lbs. ea. (+105) (c) 4 - 1 1/2 minute (International MK-1) 24 lbs. (+80) or (+110) 208. Gold compartment (Dwg. I-17006) (Max. capacity 70 lbs. included in baggage allowance) 9 lbs. (+100) 211. Vacuum equipment (a) Pump (Pesco 194, Romec RD-2112 or ARO Equipment A-513-DA) 4 lbs. (-26) (b) Venturi tubes 1 lbs. (-4) 213. Fuselage alterations for special-purpose equipment (a) Photographic version (Item 214) - Includes front and rear floor windows, camera and viewfinder wells, and change in location of rudder cables. (Dwgs. D17015 and D170160) +13 lbs. (+33) (b) Ambulance version (Item 215) - includes rear seat center support and litter floor attachments. (Dwgs. I-17073 and I-17077) +2 lbs. (+53) (c) Mailplane version (Item 216) - Includes rear seat center support and metal lined baggage compartment and right rear of cabin. (Dwgs. I-170812 and I-170813) +15 lbs. (+73) 214. Photographic version (See Item 213(a)) (a) Camera and viewfinder 110 lbs. max. (+51) (b) Photographers stool (These items (a and b) may be installed after fuselage alterations (Item 213(a)) have been made, and standard rear seat, 31 lbs. (+67), camera and viewfinder cover plates, 3 lbs. (+51), have been removed.) (c) Oxygen tank installation 150 lbs. max. (+73) 215. Ambulance version (See Item 213(b)) (a) Special right or left half rear seat (Dwg. I-17073) (may replace standard rear seat, 31 lbs. (+67), if fuselage alterations (Item 213(b)) have been made) 17 lbs. ea. (+67) (b) First aid box installation 7 lbs. (+48) (c) Ambulance litter and two safety belts (may be installed after fuselage alteration (Item 213 (b)) and removal of right half rear seat (a) and co-pilots seat 16 lbs. (+21) 14 lbs. (+42) 216. Mailplane version (See Item 213(c)) (a) Same as 215(a) except Dwg. I-170812. (b) Removable front and inner sides of fwd. mail compartment (see (c)) 10 lbs. (+52) (c) Mail compartments and capacities: 1. Front 200 lbs. max. (+54) 2. Rear 150 lbs. max. (+88) 222. Package drop (under baggage compartment) +8 lbs. (+84) 301. Control column "T" type No weight change 309. Folding back seat (may replace standard front seats) 16 lbs. (+21) 315. Utility case 4 lbs. (+77) A-649 6 Rev. 5 Specifications Pertinent to All Models (cont’d) Miscellaneous (not listed above) 152. Auxiliary seaplane fin (Dwg. D17635) 5 lbs. (+220) 153. Water rudder control system 4 lbs. (+110) 212. Extra cabin door on right side +5 lbs. (+42) 221. Ballast at tailpost (Dwg. I-17007) 25 lbs. max. (+224) 302. Metal cover for lower wing fuel tank 3 lbs. (+24) 304. Quick door release 1 lbs. (+36) 601. Metal cover for upper wing fuel tank 4 lbs. (+47) 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). NOTE 2. Fuel restriction placard must state: "Use fuselage tank for take-off and landing. Fill fuselage tank(s) before filling wing tanks. Use wing tank(s) before, using fuselage tank(s)." When upper wing fuel tanks are installed, add, "Fill lower wing tanks before filling upper wing tanks. Use upper wing tanks before using lower wing tanks." NOTE 3. Army UC-43B and Navy GB-1 are identical to Model D17S. Army UC-43 and Navy GB-2 are eligible for certification as Model D17S when converted in accordance with Beech Commercial Modification Bulletin No. 40. Each airplane must be weighted to determine its weight and balance and an approved loading chart or device must be installed. Upon completion of the conversion to certificated status, the manufacturer's name plate containing the commercial model designation, serial number, and the date of manufacture shall be installed below the original name plate. The original or any succeeding name plate should not be removed from the aircraft. ---- END ---- ``` ## ADs (5, 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 2022-03-15](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 99-05-13 R1 WD](https://openairdocs.org/ad/99-05-13-R1-WD): Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Jul 5, 2000 - [AD 48-51-01](https://openairdocs.org/ad/48-51-01): Control Wheel Shaft Inspection · Textron Army AT-11, C18S and D17S - [AD 99-05-13](https://openairdocs.org/ad/99-05-13) (historical): Fuel Tank Selector · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Apr 19, 1999 ## Registered aircraft by registry model (OpenAirDocs) - [Beech D17S](https://openairdocs.org/model/beech-d17s): 124 aircraft (registry code 1150538) - [Beech SD17S](https://openairdocs.org/model/beech-sd17s): 0 aircraft (registry code 1150548) ## STCs approved under this data sheet (71, 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 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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc. - [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 SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc. - [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 SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings 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 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 SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA2691SO](https://openairdocs.org/stc/SA2691SO): Installation of Cleveland hydraulic brake conversion kit no. 199-167. Rare Aircraft Ltd - [STC SA5190NM](https://openairdocs.org/stc/SA5190NM): Installation of Gustin Aviation chip detector light system.. A & L Aircraft Parts Inc - [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 SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc. - [STC SA6070NM](https://openairdocs.org/stc/SA6070NM): Installation of a 'quick-disconnect drain plug' on the engine rocker sump for the oil drain retrieval system after engine shutdown.. West Coast Air Creations - [STC SA01282NY](https://openairdocs.org/stc/SA01282NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K015 on aircraft powered by Pratt & Whitney radial reciprocating engine Series R-985, R-1340 and R-1830.. Airwolf Filter Corporation - [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems.. J P Instruments - [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 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 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): 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 SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc. - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): 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 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): 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 SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.. M-20 Oil Separators LLC - [STC SA2009CE](https://openairdocs.org/stc/SA2009CE): Operation on unleaded and/or leaded automobile fuel.. Petersen Aviation Inc - [STC SA241CH](https://openairdocs.org/stc/SA241CH): Install Ceconite 101 fabric.. Aviation Products Systems Inc. - [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc - [STC SA1008WE](https://openairdocs.org/stc/SA1008WE): Installation of Poly-Fiber covering material.. Poly-Fiber Inc. - [STC SA00281DE](https://openairdocs.org/stc/SA00281DE): Installation of Oilamatic Preoiler system.. Oilamatic Inc - [STC SA1657GL](https://openairdocs.org/stc/SA1657GL): Surrendered and incorporated into STC SA241CH.. Cooper Aviation Supply Company, Inc. - [STC SA00068LA](https://openairdocs.org/stc/SA00068LA): Installation of tail wheel adapter ring.. R-R-R-Russ Aircraft - [STC SA09506AC-D](https://openairdocs.org/stc/SA09506AC-D): Installation of S-TEC System 30 Two Axis Automatic Flight Guidance System, Model ST-886-30,. S-TEC Corporation - [STC SA8494SW-D](https://openairdocs.org/stc/SA8494SW-D): Installation of a Century Automatic Flight System, Model AK1012 consisting of Century 2010/2050/2051 Autopilot.. Century Flight Systems Inc - [STC SA8495SW-D](https://openairdocs.org/stc/SA8495SW-D): Installation of a Century Yaw Damper System, Model YK1013 consisting of Century Yaw Damper.. Century Flight Systems Inc All 71: https://openairdocs.org/tcds/A-649/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.