Aeronca K Scout

Number of Active Aircraft: 38 Active- Map

Description:



If you feel like you have a particular interest in this model of aircraft you are welcome to submit a brief history and description/points of interest that make this model unique.

Please send descriptions to audriesaircraftanalysis@gmail.com

Or

Have an Update?
Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 590 lbs
Max Weight 1040 lbs
Useful Load: 450 lbs
Engine Name
Engine Number 1
Horsepower 36 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 12500 ft
Max Fuel 10 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 61 kts
GPH (75% BHP): 3
MPG (75% BHP) 20.3
Range (75% BHP): 132 nm
Fuel Cost Per Seat Mile 0.15 $
Fuel Cost Per Hour 18 $
MPG per 1000 lbs of Payload 9.15
F-T (Speed^2/FuelBurn) 12.4 HP
F-T Payload 5.6 kts
MPH To HP: 16.9 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 0 ft

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
SA00478CH (PAGE 1) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA01026SE (PAGE 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
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
SA02033AT (PAGE 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
SA02268CH (PAGE 6) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA1-150 Continental C-85-8 engine Sensenich 75GK-50 propeller and Harrison HE431-9 engine oil cooler. Issued 
SA1-583 Continental A-65-8 engine and Sensenich 72GK42 propeller. Amended 1/1/1961
SA1201GL Authorize gross weight increase from 1150 to 1200 lbs. for Model65-C and from 1253 to 1290 lbs. for Model S-65-C. Issued 7/13/1987
SA1351WE (PG 1) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983
SA2-952 Installation of fiberglass covering. Reissued 9/10/1996
SA4-1210 Installation of Eonnex cover on aircraft surfaces. Reissued 8/19/1980
SA4-1298 Ceconite 101 covering of complete airplane. Issued 1/1/1960
SA4-288 BN-1 propeller spinner. Issued 1/1/1960
SA4503NM Install Ceconite covering material. Reissued 2/25/2011
SA4624NM Installation of F. Atlee Dodge springs 2097 and 2127 to replace bungee cords on ski equipped airplanes. Issued 2/21/1990
SA593CH (1 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009
SA71GL Installation of air filters Reissued 6/20/2000
SA742GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index Surrendered 3/5/2004
SA7965SW Application of fabric and polyurethane finishing system. Amended 7/15/1994
SA8075SW (PAGE 1) Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER) Reissued 11/10/2003
SA928NE Added unleaded automative gasoline. Issued 1/15/1992
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)