TaylorCraft BL65

Number of Active Aircraft: 197 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 640 lbs
Max Weight 1150 lbs
Useful Load: 510 lbs
Engine Name
Engine Number 1
Horsepower 65 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 15000 ft
Max Fuel 18 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 78 kts
GPH (75% BHP): 4.8
MPG (75% BHP) 16.3
Range (75% BHP): 221 nm
Fuel Cost Per Seat Mile 0.18 $
Fuel Cost Per Hour 28.8 $
MPG per 1000 lbs of Payload 8.29
F-T (Speed^2/FuelBurn) 12.7 HP
F-T Payload 6.5 kts
MPH To HP: 12 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 0 ft

SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00140LA Installation of a replacement S & S Propeller model W7448A1-2. Issued 12/7/1995
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
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
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
SA01988SE (PAGE 5) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02110CH (PAGE 3) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
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
SA1236NW Installation of Scintilla S4LN20 magnetos carbueretor heat box and exhaust system a 6 gallon auxiliary fuel wing tank an enlarged baggage compartment a Scott 3000 tail wheel dual brake installation and Stits polyfiber covering Issued 5/20/1981
SA1351WE (PG 2) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983 0:00
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2350NM Page 2 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA3-640 Removed Lycoming O-145-B2 engine motor mount baffles and exhaust system. Installed Continental A-65-8 engine motor mount baffles and Champion 7AC exhaust system. Engine cowling modified to accomadate exhaust stacks. Issued 5/9/1961
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
SA3862NM Page 2 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4-1210 Installation of Eonnex cover on aircraft surfaces. Reissued 8/19/1980
SA4-1346 Fiberglas covering of airplane surfaces. Issued 1/1/1960
SA4-1438 Eronite covering of fuselage. Issued 1/1/1970
SA4-162 Glass cloth applied over old fabric with the exception of all flight control surfaces. Issued 1/1/1960
SA4-302 Installation of BN-1 propeller spinner. Reissued 10/30/1985
SA4-906 Ceconite 101 covering of complete airframe. Amended 12/15/1966
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
SA637AL Installation of Plexiglass Skylight in fuselage cabin. Reissued 2/22/2008
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
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)