TaylorCraft F19

Number of Active Aircraft: 124 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 860 lbs
Max Weight 1500 lbs
Useful Load: 640 lbs
Engine Name
Engine Number 1
Horsepower 85 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 17000 ft
Max Fuel 24 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 95 kts
GPH (75% BHP): 3.8
MPG (75% BHP) 25
Range (75% BHP): 503 nm
Fuel Cost Per Seat Mile 0.12 $
Fuel Cost Per Hour 22.8 $
MPG per 1000 lbs of Payload 16
F-T (Speed^2/FuelBurn) 23.8 HP
F-T Payload 15.2 kts
MPH To HP: 11.2 kts
T/O Roll - T/O over 50 FT OBST 300 ft / 400 ft

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. Amended 10/3/2012
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
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. Amended 10/31/2012
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00139LA Installation of a replacement S & S Propeller model W7448A1-2. Issued 12/7/1995
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00478CH (PAGE 2) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00680SE (4 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA01015SE Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. Amended 10/4/2012
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01227SE Farication of Vortex Generator Kit. Amended 11/12/2008
SA01233SE Manufacture of Alaskan Bushwheel Inc. (ABI) tail wheel and fork assembly per ABI Document ABI-3200B Revision A dated April 28 2005 or later FAA approved revision.  Amended 5/22/2012
SA01240SE (5 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01800SE (PG 4) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01861SE (PAGE 5)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01944CH (2 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004 0:00
SA01988SE (PAGE 5) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02033AT (PAGE 5) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008 0:00
SA02168AK (PG 2) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001 1:00
SA02212AK (PG 4) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Amended 5/4/2011
SA02268CH (PAGE 5) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 2 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02300AK Installation of FAA approved sealed lift struts in accordance with Airframes Inc. Master Drawing List No. 315 Revision B dated October 2 2007 or later FAA approved revision and Airframes Inc. Installation Instructions AFI-II-TCSTRUT Revision A dated October 8 2007 or later FAA approved revision. Reissued 6/9/2008
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-95 Wing lift struts to include a hydraulic-pneumatic shock absorber. Issued 1/1/1961
SA10077SC Installation of push-button starter system. Amended 4/26/2005
SA1008WE Installation of Poly-Fiber covering material. Reissued 5/27/2003
SA1070SO Installation of Aqua Model 1500 floats. Amended 5/25/2004
SA10921SC Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators Issued 11/10/2008
SA1129EA Installation of PK Model 1800 or B1800 (TSO-C27) seaplane floats. Reissued 12/23/1980
SA1454GL Surrendered and incorporated into STC SA00478CH. Surrendered 6/14/2002
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1745SO Installation of Appalachian Access. stainless steel brake rotors P/N 75-20. Reissued 2/6/1995
SA191NE Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. Reissued 10/4/1984
SA2076CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON)/2. Intermixing with aviation gasoline also approved. Issued 1/24/1985
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2230SO Installation of stainless steel brake discs P/N 75-20. Reissued 2/6/1995
SA2350NM Page 2 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA24CH Installation of Baumann Model 1420 floats. Reissued 6/2/2006
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2649NM Installation of EDO 92-1400 seaplane floats. Issued 8/31/1984
SA2683NM Installation of Precise Flight Inc. stand-by vacuum system (SVS) Amended 3/10/2005
SA308EA (1 OF 2) Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) Amended 11/20/1978
SA345NW Removal of one or two main cabin doors Amended 4/14/1978
SA3630NM Application of polyurethane finishing system. Issued 7/15/1987
SA3862NM Page 2 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4-1200 Delco-Remy generator 1101879 and regulator 1118384. Issued 1/1/1960
SA4005NM (PG 5) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4302NM (PAGE 3) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989 0:00
SA489EA Installation of ARP Inc. carburetor ice detection system Models 107AP (-12 -R-12 -24 and -R-24 series) in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Precision A ir-Motive (Facet or Marvel-Schebler) MA-2 MA-3 MA-3SPA MA-4 MA-4-5 MA-4SPA MA-5 MA-6 MA-6AA and HA-6 series carburetors. Amended 12/5/2002
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5581SW Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. Amended 9/30/2002
SA5755NM Installation of a propeller anti theft device. Issued 8/5/1992
SA593CH (4 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA71GL Installation of air filters Reissued 6/20/2000
SA769GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
SA8075SW (PAGE 1) Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER) Reissued 11/10/2003
SA90NW Installation of a Continental O-200-A engine McCauley 1A100 MCM/6950 propeller Cessna 150 exhaust system Cessna 150 oil cooler and engine colwing Issued 2/26/1974
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Limitations
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)