Aeronca 11CC Super Chief

Number of Active Aircraft: 95 Active- Map


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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 820 lbs
Max Weight 1350 lbs
Useful Load: 530 lbs
Engine Name
Engine Number 1
Horsepower 85 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 12300 ft
Max Fuel 23 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 83 kts
GPH (75% BHP): 8.3
MPG (75% BHP) 10
Range (75% BHP): 169 nm
Fuel Cost Per Seat Mile 0.3 $
Fuel Cost Per Hour 49.8 $
MPG per 1000 lbs of Payload 5.3
F-T (Speed^2/FuelBurn) 8.3 HP
F-T Payload 4.4 kts
MPH To HP: 9.8 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 475 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
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00232SE Installation of vortex generators on the wings and tail surfaces. Amended 4/12/2005
SA00478CH (PAGE 1) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00823SE  );INSERT INTO stc_table VALUES ( Fabrication and Installation of Rainbow Flying Service front and rear wing spars and modified wing ribs Amended 8/8/2006
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 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
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
SA01944CH (1 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
SA01988SE (PAGE 1) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009
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
SA02110CH (PAGE 1) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02212AK (PG 1) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems  Amended 5/4/2011
SA02268CH (PAGE 1) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02370AK Option (1) Installation of a replacement main tank fuel valve Reissued 5/13/2010
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02566CH Installation of the Custom Fiberglass Molding Inc. (CFMI) Model 1500 Aircraft Main Landing Gear Skis. Amended 3/6/2009
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA1189GL Installation of Ceconite 102 fabric. Limited to installation on model 11CC serial number 11CC-121 ONLY. Amended 7/19/2002
SA1351WE (PG 1) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983
SA150SO Installation of surface fabric attachment clip. Reissued 6/3/1991
SA2078CE 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. Amended 6/23/1992
SA217AL Install L-1650A or L-2000A skis. Issued 1/1/1960
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA262CE Manufacture parts and install 12-30A electrical system. (Requires alteration of engine per STC SE3CE.) Issued 1/1/1960
SA2683NM Installation of Precise Flight Inc. stand-by vacuum system (SVS) Amended 3/10/2005
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA2710WE Installation of carburetor heat box bearings. Issued 6/15/1973
SA3-115 Model 3000 main ski and Model 1000 tail ski. Reissued 2/16/1993
SA3-424 Installation of Wiparie Skis Model CTF-2200 (Acft Skis) (FluiDyne) (Federal) tail ski on airplanes equipped with Scott Model 3000 tail wheel. Reissued 2/16/1993
SA3-670 Install Pee-Kay Model 1500 floats with Edo struts and fittings. Reissued 12/23/1980
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
SA3358NM Production of aircraft wing ribs as specified in W. N. Kutner s Report #1 STC Request for Wing Ribs.  Reissued 12/5/2008
SA3829NM Installation of aluminum wing spars in accordance with FAA Approved Drawing List No. 001 Revision C dated March 6 1986 and installation instructions BHM-000 Revision E dated April 21 1987 or later FAA-approved revision. Amended 9/9/2004
SA4-1270 Ceconite 101 covering of complete airplane. Issued 1/1/1960
SA4005NM (PG 1) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4302NM (PAGE 1) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
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
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA535AL Fabrication and installation of Stoddard Aero Service wing auxiliary fuel tanks per Stoddard Aero Service Drawing List No. 89 dated February 7 1975 or later Federal Aviation Administration approved revision. Reissued 1/26/2012
SA57RM Installation of Lycoming O-235-C1 -C1A -C1B -C1C -C2A -C2B -C2C -H2C -K2A -K2B -L2A or L2C series engines. Reissued 7/8/2009
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA593CH (1 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009
SA69SO Installation of Continental C85-12F Series engine less starter and generator per C. W. Lasher Report L-100 dated April 23 1963. Reissued 9/21/2012
SA734GL Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. Surrendered 3/5/2004
SA73CH Installation of Wing Strut Fittings P/N SAR 2-893 or SAR 2-893-1 and stiffeners P/N 2-5009 in accordance with Safe Air Repair Installation Instructions SAR 2-5007 no revisions dated April 30 1993 or later FAA approved revisions. Reissued 4/22/2005
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
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
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
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
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)


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