# TCDS A-773: Bellanca Aircraft Corporation - Type: Type certificate data sheet - Status: Current - Holder: Bellanca Aircraft Corporation - Revision: 10 - Revised: October 1, 1973 - Product: Aircraft, Small Airplane - Certification basis: CAR 4a - Registered aircraft: 131, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/1b/34/1b34bfb504532184fff082a978ad372c3f107bd6afcf472c4aebf6f6b152fae6 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/24D6631E7E1C971E8525672F006979B0.0001 - Page: https://openairdocs.org/tcds/A-773 ## Models (4) As the data sheet lists them. - 14-13-3W - 14-13-3 - 14-13-2 - 14-13 ## 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 Rev. No. 10 10 10 - Reformatted 2/94. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-773 Bellanca Revision 10 14-13 14-13-2 14-13-3 14-13-3W October 1, 1973 AIRCRAFT SPECIFICATION NO. A-773 Type Certificate Holder Bellanca Aircraft Corporation New Castle, Delaware 19720 I - Models 14-13, 4 PCLM, Approved September 25, 1946; 14-13-2, 4 PCLM, Approved June 2, 1947; 14-13-3, 4 PCLM and 14-13-3W, 2 pclm, Approved October 25, 1948. Model 14-13-2 same as 14-13 except for increased areas of stabilizer and elevators, decreased tip fin area, revised wood construction and revised elevator stops. Model 14-13-3 same as 14-13-2 except for dual landing lights in left wing leading edge, revised oleo struts and nut crackers, adjustable front seat backs and revised instrument panel. Model 14-13-3W same as 14-13-3 except for removal of rear seats. Engine Franklin 6A4-150-B3 Fuel 80 min. grade aviation gasoline. Engine limits For all operations, 2600 r.p.m. (150 hp) Airspeed limits Level flight or climb 160 m.p.h. (139 knots) (True Ind) Glide or dive 216 m.p.h. (187 knots) Flaps extended 85 m.p.h. ( 74 knots) C.G. range (landing gear 14-13: (+16.2) to (+23.6) extended) 14-13-2, 14-13-3, 14-13-3W: (+16.2) to (+24.5) Empty weight C.G. range None. Datum Leading edge of wing at rib No. 1. Rib No. 1 is 24 .in. outboard from fuselage center line. Leveling means Horizontal lugs, sta. 1 and 2. Vertical lugs, sta. 3. Maximum weight 14-13: 2100 lb. 14-13-2, 14-13-3, 14-13-3W: 2150 lb. No. seats 4 (Two at +18 or +20, Two at +50.5). Maximum baggage 60 lb. (+69). When baggage compartment per Dwg. 15086 is installed, maximum is 110 lb. (+80.5). In case of 14-13-3W station wagon compartment maximums are: Fwd. comp't: 260 lb. (+35) Aft. comp't: 413 lb. (+55) Fuel capacity 40 gal. (+29) Oil capacity 2 gal. (-36) Control surface movements 14:13 Elevator - landing gear up 18° up 19° down - landing gear down 23° up 19° down Elevator trim tab 12° up 22° down Rudder 18° left 18° right Aileron 28° up 22° down Flaps 46° down 14-13-2, 14-13-3, and 14-13-3W: Elevator 19° up 19° down Elevator trim tab 12° up 22° down Rudder 18° right 18° left Aileron 25° up 19° down Flaps 46° down A-773 Page 2 Serial Nos. eligible 1060 and up. Serial numbers 1060 through 1385 are Model 14-13. Serial numbers 1386 through 1583 are Model 14-13-2. Serial numbers 1584 and up are Model 14-13-3 and 14-13-3W. Serial numbers 1060 through 1385 are eligible as Model 14-1 3-2 providing they are revised to conform to Bellanca Dwgs. 9989, 9995, 9996 and 9918 and proper control surface movements. Required equipment In addition to the pertinent required basic equipment specified in CAR 4a, the following items of equipment must be installed: Landplane: Items 1, 103, 104, 105, 201(a), 202(a), 204(a). Skiplane: Items 1, 103, 104, 105, 208(a). Specifications Pertinent to all Models Certification basis Type Certificate No. 773 (CAR 4a) Production basis None. 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: 1. Propeller-Sensenich 74RA or any other fixed pitch wood propeller rated for 20 lb. (-56) required hp and rpm and following limits: Static rpm at maximum permissible throttle setting: Not over 2100, not under 2000. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. 2. (a) Propeller-Koppers Aeromatic Hub F200, blades 00-74A, 00-74B or 00-74C. 31 lb. (-56) Parts List Assembly No. 4275. Low pitch setting 14° at 24 in. sta. Static rpm at maximum permissible throttle setting: Not over 2550, not under 2500. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. Installation must be accomplished in accordance with Koppers "Installation Procedure and Operating Limitation No. 1B" (Without Altitude Control). (b) Altitude Control, (optional) Parts List Assembly No. 4379 6 lb. (-44) When Altitude Control is installed, the propeller installation must be made in accordance with Koppers Company Adjustment Instructions and Operating Limitations No. 54, Koppers Installation Dwg. No. 4275H and the engine must be modified in accordance with Aircooled Motors Corporation Dwgs. Nos. 18487, 18218 and SK-582-6. (c) Propeller - Kopper Aeromatic Hub F200, blades 00-74B or 00-74C 31 lb. (-56) Parts List Assembly No. 4275-1 Low pitch setting 14° at 24 in. sta., High pitch setting 26° Static rpm at maximum permissible throttle setting: Not over 2650, not under 2600. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. Installation must be accomplished in accordance with Koppers "Installation Procedure and Operating Limitations No. 84" (Without Altitude Control) Eligible only with item 110 engine. Tachometer must be red-lined at 2650 rpm. A-773 Page 3 3. Propeller - Sensenich, Controllable; Hub model CS3FR5, blade model 37 lb. (-56) PC376B4-2. (eligible with Item 110 engine only) Pitch settings at 3/4 radius: Low 13°; High 19.5°. Diameter: Not over 74 in., not under 72.5 in. 4. Propeller - Koppers Aeromatic; Hub F200H; Blades 00-74B 31 lb. (-56) Parts List Assembly No. 4275AH-1 Altitude Control Parts List Assembly No. 4370 6 lb. (-44) Low pitch setting 14° at 24 in. sta. Static rpm at max. permissible throttle setting: Not over 2650, not under 2600. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. Installation must be accomplished in accordance with Koppers, "Adjustment Instructions and Operating Limitations No. 65" (Eligible only with Item 110 engine. Tachometer must be red-lined at 2650 rpm). Engine and Engine Accessories - Fuel and Oil System 101. Starter - Delco-Remy, part No. 10750 16 lb. (-26) 102. Generator - Autolite, part No. 10119 (15 amp) 12 lb. (-24) 103. Fuel pump - A.C. diaphragm type, part No. 11921 2 lb. (-31) 104. Oil cooler - Fedders (1311H) or heat exchangers (102) 6 lb. (-30) 105. Carburetor heater 2 lb. (-30) 106. Fuel strainer - Koehler K2250-B 107. Two mufflers - Kay Industries - (Bellanca Dwg. 15062) +1 lb. ea. (-34) 108. Generator - Delco-Remy 25 amp., part No. 1101887 +4 lb. (-24) 109. Oil filter - Fram PB5, kit No. K-501 Fram Installation Dwg. 61627 5 lb. (-19) 110. Engine - Franklin, 6A4-165-B3 (Negligible wt. change) Engine limits - 2800 rpm (165 hp) Fuel - 80 minimum octane aviation gasoline (Eligible with Item 2(c), 3 and 4 propellers only) Installation eligible only when original basic Franklin 6A4-150-B3 engine installation components utilized with no changes to aircraft structure. Landing Gear 201. Two main wheel-brake assemblies, 6.00-6, Type III, (a) Goodyear Model 6 IBD, 15 lb. (+8) Wheel Assembly No. 511413-M Brake Assembly No. 511640-M (b) Goodrich Model 605MD, No weight change Wheel Assembly No. D-3-105-MD Brake Assembly No. D-2-524 (c) Firestone Model DFA207, -1 lb. (+8) Wheel Assembly No. DFA180 Brake Assembly No. CFA252 (d) Goodyear Model CL6HBD (Castering wheels) 31 lb. (+8) Wheel Assembly No. 9530375/76 Brake Assembly No. 9530369/68 (Install in accordance with Bellanca Dwg. 18224) 202. Two main wheel, 4-ply rating, Type III tires, with regular tubes, (a) 6.00-6 18 lb. (+8) (b) 7.00-6 +3 lb. (+8) A-773 Page 4 204. Tail Wheel Assembly (a) Firestone Model CFA160, 6x2.00 2 lb. (+192) (b) Same as (a), steerable per Bellanca Dwgs. 15085 and 15091 +4 lb. (+192) (c) Maule Hub and Axle Model SFS-P8 Use actual wt. change General Tire 8.00 SC per Bellanca Dwg. 18222 208. Two Main Skis Use actual wt. change (a) Federal Model A2500, Federal Installation Dwg. 11R185 (b) Federal Model A2500A, Federal Installation Dwg. 11R185 (c) Federal Model A3500, Federal Installation Dwg. 11R185 (d) Federal Model A3500A, Federal Installation Dwg. 11R185 210. One Tail Ski Use actual wt. change Federal Model AT-3500 211. Electric landing gear retraction installation per Bellanca +7 lb. (+18.5) Dwg. No. 15103 Electrical and Radio Equipment 301. Battery - Reading R-24L 24 lb. (-17) 302. Radio equipment 12 lb. (-11) 303. Antenna and mast 1 lb. (+6) 304. Landing light - Grimes ST-250 3 lb. (+21) 305. Dual landing light installation - G.E. No. 4509 2 lb. (+9) Interior Equipment 401. Flares (5 one-minute, International) 17 lb. 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 at all times thereafter (except in the case of air carrier operators having an approved weight control system). NOTE 2. The following placards must be installed in full view of the pilot: (a) "Intentional Spinning Prohibited." (b) "Front seats must be occupied when used as three place." (Applicable to Model 14-13). ...END... ``` ## 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 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 79-19-05](https://openairdocs.org/ad/79-19-05): Aileron Control System · Bellanca 14-13, 14-13-2, 14-13-3 and 1 more. Effective Sep 10, 1979 - [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979 - [AD 76-20-07](https://openairdocs.org/ad/76-20-07): Wood Decayed Wing Spars · Bellanca 14-12F-3, 14-13, 14-13-2 and 11 more. Effective Oct 8, 1976 - [AD 63-20-01](https://openairdocs.org/ad/63-20-01): Brake Cylinder Support Bracket · Bellanca 14-13, 14-13-2, 14-13-3 and 1 more. Effective Oct 21, 1963 - [AD 63-17-01](https://openairdocs.org/ad/63-17-01): Main Landing Gear · Bellanca 14-13, 14-13-2, 14-13-3 and 1 more. Effective Sep 13, 1963 - [AD 63-06-02](https://openairdocs.org/ad/63-06-02): Rudder Bellcrank · Alexandria 14-19, 14-19-2, 14-13 and 3 more. Effective Mar 19, 1963 - [AD 46-41-01](https://openairdocs.org/ad/46-41-01): Rudder Bellcrank Replacement · Bellanca 14-13 and 14-13-2 - [AD 46-41-02](https://openairdocs.org/ad/46-41-02): Aileron Control Bushing · Bellanca 14-13 and 14-13-2 - [AD 46-41-03](https://openairdocs.org/ad/46-41-03): Control Wheel Universal Joints · Bellanca 14-13 and 14-13-2 - [AD 47-07-01](https://openairdocs.org/ad/47-07-01): Fuel Selector Valve Indexing · Bellanca 14-13 and 14-13-2 - [AD 47-14-01](https://openairdocs.org/ad/47-14-01): Flap Hinge Bracket · Bellanca 14-13 and 14-13-2 - [AD 47-32-17](https://openairdocs.org/ad/47-32-17): Landing Gear Inspection Covers · Bellanca 14-13 and 14-13-2 - [AD 47-32-18](https://openairdocs.org/ad/47-32-18): Sprocket Cotter Pin · Bellanca 14-13 and 14-13-2 - [AD 47-51-13](https://openairdocs.org/ad/47-51-13): Cabin Heat Control Valve · Bellanca 14-13, 14-13-2, 14-13-3 and 1 more - [AD 48-05-03](https://openairdocs.org/ad/48-05-03): Trim Tab Bracket Bolts · Bellanca 14-13 and 14-13-2 - [AD 48-13-06](https://openairdocs.org/ad/48-13-06): Engine Cowl Brackets · Bellanca 14-13 and 14-13-2 - [AD 49-13-02](https://openairdocs.org/ad/49-13-02): Landing Gear Drag Strut · Bellanca 14-13, 14-13-2 and 14-13-3 - [AD 51-16-01](https://openairdocs.org/ad/51-16-01): Trim Tab Modification · Bellanca 14-13 and 14-13-2 - [AD 52-17-01](https://openairdocs.org/ad/52-17-01): Landing Gear Chain Guard · Bellanca 14-13, 14-13-2, 14-13-3 and 1 more - [AD 52-28-02](https://openairdocs.org/ad/52-28-02): Fuel Pump Relief Valve · Bellanca 14-13, 14-13-2 and 14-13-3 ## Registered aircraft by registry model (OpenAirDocs) - [Bellanca 14-13-2](https://openairdocs.org/model/bellanca-14-13-2): 77 aircraft (registry code 1201004) - [Bellanca 14-13](https://openairdocs.org/model/bellanca-14-13): 43 aircraft (registry code 1201002) - [Bellanca 14-13-3](https://openairdocs.org/model/bellanca-14-13-3): 11 aircraft (registry code 1201006) - [Bellanca 14-13-3W](https://openairdocs.org/model/bellanca-14-13-3w): 0 aircraft (registry code 1201008) - [Bellanca/Peteani 14-13-2](https://openairdocs.org/model/bellanca-peteani-14-13-2): 0 aircraft (registry code 1201005) ## STCs approved under this data sheet (107, first 50) - [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 SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC - [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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC - [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 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 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 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 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 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 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 SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [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 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 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 SA4-1421](https://openairdocs.org/stc/SA4-1421): Installation of Brittain Model B2D and BSS Flight Control Systems. Brittain Industries, Inc - [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 SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International 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 SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International 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 - [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): 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 SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc - [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC - [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft - [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc - [STC SA5156NM](https://openairdocs.org/stc/SA5156NM): Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System. AvTek All 107: https://openairdocs.org/tcds/A-773/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.