# TCDS A-761: American Champion Aircraft Corp.

- Type: Type certificate data sheet
- Status: Current
- Holder: American Champion Aircraft Corp.
- Revision: 18
- Revised: January 9, 2009
- Product: Aircraft, Small Airplane
- Certification basis: CAR 4a
- Registered aircraft: 677, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/b8/7c/b87ce72e0d1ff288553303b539c1494a86a59da4842004e951620c672cd37617
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FC049D25CC6B1CD28625753C004E3FA0.0001
- Page: https://openairdocs.org/tcds/A-761

## Models (4)

As the data sheet lists them.

- 11BC
- S11AC
- 11AC
- S11BC

## 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 5 6 7 
Rev No. 17 17 17 17 17 18 17 
Reformatted 3/94. 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
A-761 
Revision 18 
American Champion 
(Bellanca) 
(Trytek) 
(Aeronca) 
11AC 
S11AC 
11BC 
S11BC 
January 9, 2009 
TYPE CERTIFICATE DATA SHEET NO. A-761 
 
Type Certificate Holder:  American Champion Aircraft Corp. 
    P. O. Box 37 
    Rochester, Wisconsin  53167 
 
I - Model 11AC, 2 PCLM, Approved September 28, 1945 
    (See Section III for conversion to model 11BC) 
 
    Engine Continental A-65-8 
 
    Fuel 73 minimum octane aviation gasoline 
 
    Engine Limits For a ll operations, 2300 r.p.m. (65 hp.) 
 
    Airspeed Limits (CAS) Level flight or climb      95 m.p.h.    (83 knots) 
 Glide or dive                128 m.p.h.  (111 knots) 
 
    Propeller Limits Static rpm at maximum permissible throttle setting: 
     (For fixed pitch wood propeller) Not over 2300,  not under 1990.  No additional tolerance permitted 
 Diameter:  not over 72 in., not under 70 in. 
 
    C.G. Range (+12.4) to (+22.0) (Rear limit may be(+23.2) provided intentional spins are prohibited). 
 
    Empty Weight C.G. Range (+12.9) to (+19.6) with standard fuel tank only 
 (+12.9) to (+15.2) with Item 104 installed 
 When the empty weight C.G. falls within these ranges, it is unnecessary to check the 
critical forward and aft C.G. positions.  Ranges are not valid for arrangements other than 
indicated.  
 
    Maximum Weight 1250 lbs. 
 
    No. of Seats 2  (adjustable from +21.5 to +25.5) 
 
    Maximum Baggage 70 lbs. (+48.5).  Placard required on instrument panel: 
 "INTENTIONAL SPINNING PROHIBITED WHEN BAGGAGE IS CARRIED" 
 
    Fuel Capacity 15 gal. (-6) 
 
    Oil Capacity 1 gal. (-32) 
 
    Control Surface Movements Elevator   Up 26° Down 24.5° 
 Elevator Trim Tab  Up 23° Down 31° 
 Ailerons   Up 28° Down 18° 
 Rudder   Right 28° Left 28° 
 
    Serial No. Eligible 11AC-1 and up

-2-  A-761
Rev. 18 
 
   
  Required Equipment In addition to the pertinent requi red basic equipment specified in CAR 4a, the following 
items of equipment must be installed:    1, 101, 102, 201, 202 
 
II - Model S11AC, 2 PCSM, Approved July 22, 1947 
 
    Engine Continental A-65-8F 
 
    Fuel 73 minimum octane aviation gasoline 
 
    Engine Limits For a ll operations, 2300 r.p.m. (65 hp.) 
 
    Airspeed Limits (CAS) Level flight or climb      90 m.p.h.    (78 knots) 
 Glide or dive                122 m.p.h.  (106 knots) 
 
    Propeller Limits Static rpm at maximum permissible throttle setting: 
     (For fixed pitch wood propeller) Not over 2170,  not under 2070.  No additional tolerance permitted 
 Diameter:  not over 72 in., not under 70 in. 
 
    C.G. Range (+17.0) to (+21.9) at 1350 lb. 
 (+14.9) to (+21.9) at 1278 lb. or less.  St raight line variation between points given. 
 
 
LB.
14 15 16 17 18 19 20 21 22
1400
1350
1300
1250
1200
1150
INCHES
FRONT
LIMIT
AFT
LIMIT
 
 
    Empty Weight C.G. Range None 
 
    Maximum Weight 1350 lbs. 
 
    No. of Seats 2  (adjustable from +21.5 to +25.5) 
 
    Maximum Baggage 70 lbs. (+48.5).  Placard required on instrument panel: 
 "INTENTIONAL SPINNING PROHIBITED WHEN BAGGAGE IS CARRIED" 
 
    Fuel Capacity 15 gal. (-6) 
 
    Oil Capacity 1 gal. (-32) 
 
    Control Surface Movements Elevator   Up 26° Down 24.5° 
 Elevator Trim Tab  Up 23° Down 31° 
 Ailerons   Up 28° Down 18° 
 Rudder   Right 28° Left 28° 
 
    Serial No. Eligible 11AC-1 and up 
 
    Required Equipment In addition to the pertinent re quired basic equipment specified in CAR 4a, the following 
items of equipment must be installed:    1, 101, 208, 209

-3-  A-761
Rev. 18 
III - Model 11BC, 2 PCLM, Approved August 26, 1947 
    (Model 11AC eligible for conversion to Model 11BC when accomplished in accordance with Aeronca Service Letter No. 17. 
    The nameplate must be re-stamped with the proper model designation and the letters "CONV" added.  The airplane serial  
    number should not be changed.) 
 
    Engine Continental C-85-8F 
 
    Fuel 80 minimum octane aviation gasoline 
 
    Engine Limits For a ll operations, 2575 r.p.m. (85 hp.) 
 
    Airspeed Limits (CAS) Level flight or climb      95 m.p.h.  (83 knots) 
 Glide or dive                129 m.p.h.  (112 knots) 
 
    Propeller Limits Static rpm at maximum permissible throttle setting: 
     (For fixed pitch wood propeller) Not over 2380,  not under 2160.  No additional tolerance permitted 
 Diameter:  not over 72 in., not under 70.5 in. 
 
    C.G. Range (+12.4) to (+21.5) 
 
    Empty Weight C.G. Range (+12.9) to (+19.1) with standard fuel tank only 
 (+12.9) to (+14.7) with Item 104 installed 
 When the empty weight C.G. falls within these ranges, it is unnecessary to check the 
critical forward and aft C.G. positions.  Ranges are not valid for arrangements, except as 
noted. 
 
    Maximum Weight 1250 lbs. 
 
    No. of Seats 2  (adjustable from +21.5 to +25.5) 
 
    Maximum Baggage 70 lbs. (+48.5). 
 
    Fuel Capacity 15.5 gal. (-6) 
 
    Oil Capacity 4.5 quarts (-32) 
 
    Control Surface Movements Elevator   Up 26° Down 24.5° 
 Elevator Trim Tab  Up 23° Down 31° 
 Ailerons   Up 28° Down 18° 
 Rudder   Right 28° Left 28° 
 
    Serial No. Eligible 11BC-1 and up 
 
    Required Equipment In addition to the pertinent re quired basic equipment specified in CAR 4a, the following 
items of equipment must be installed:    1,  102, 107, 201, 202 
 
IV - Model S11BC, 2 PCSM, Approved September 17, 1948 
    (Same float and fin installation as S11AC) 
 
    Engine Continental C-85-8F 
 
    Fuel 80 minimum octane aviation gasoline 
 
    Engine Limits For a ll operations, 2575 r.p.m. (85 hp.) 
 
    Airspeed Limits (CAS) Level flight or climb      90 m.p.h.  (78 knots) 
 Glide or dive                122 m.p.h.  (106 knots) 
 
 
    Propeller Limits Static rpm at maximum permissible throttle setting: 
     (For fixed pitch wood propeller) Not over 2380,  not under 2280.  No additional tolerance permitted

-4-  A-761
Rev. 18 
 Diameter:  not over 72 in., not under 69.5 in. 
 
    C.G. Range (+17.0) to (+21.9) at 1350 lb. 
 (+14.9) to (+21.9) at 1278 lb. or less. 
 Straight line variation between points given. 
 Figure under Model S11AC also applicable here. 
 
    Empty Weight C.G. Range None  
 
    Maximum Weight 1350 lbs. 
 
    No. of Seats 2  (adjustable from +21.5 to +25.5) 
 
    Maximum Baggage 70 lbs. (+48.5). 
 
    Fuel Capacity 15.5 gal. (-6) 
 
    Oil Capacity 4.5 quarts (-32) 
 
    Control Surface Movements Elevator   Up 26° Down 24.5° 
 Elevator Trim Tab  Up 23° Down 31° 
 Ailerons   Up 28° Down 18° 
 Rudder   Right 28° Left 28° 
 
    Serial No. Eligible 11BC-1 and up 
 
    Required Equipment In addition to the pertinent re quired basic equipment specified in CAR 4a, the following 
items of equipment must be installed:    1, 102, 107, 208, 209 
 
Specifications Pertinent to All Models 
 
Datum Wing leading edge at fuselage. 
 
Leveling Means Any portion of the cabin floor to level laterally and longitudinally. 
 
Certification Basis Type Certificate No. 761 (CAR 4a) 
 
Production Basis None.  Prior to original certificati on, an FAA representative must perform a detailed 
inspection for workmanship, materials, and conformity with the approved technical data, 
and a check of the flight characteristics. 
 
Export Eligibility Eligible for export to all countries  subject to the provisions of MOP 2-4 except as 
follows: 
 Canada - Landplane and seaplane - eligible 
  Skipland - not eligible 
 
Equipment A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change 
when that item is installed. 
 
Propeller and Propeller Accessories 
 
1. Propeller - Any fixed pitch wood propeller eligible  for the engine speed and power which meets the 
static r.p.m. and diameter limits specified for the various models.  (11BC cooling test required for 
the installation of a controllable propeller having a higher static low pitch r.p.m. than that specified 
under Section III above). 
10  lb. (-44) 
    
2. Propeller spinner (Aeronca Dwg. 4-710 and 4-711)  (Models 11AC and S11AC only). 1  lb. (-45) 
    
Propeller and Propeller Accessories (contd) 
3. Propeller - McCauley 1A90 with following limits: 26  lb. (-44)

-5-  A-761
Rev. 18 
 (a)  (Model 11AC only)   
       Static r.p.m. at maximum permissible throttle setting:   
       Not over 2250, not under 2100.      No additional tolerance permitted.   
       Diameter:  Not over 74 in., not under 72.5 in.   
    
 (b)  (Model S11BC only)   
       Static r.p.m. at maximum permissible throttle setting:   
       Not over 2380, not under 2280.      No additional tolerance permitted.   
       Diameter:  Not over 71 in., not under 69.5 in.   
    
 (c)  (Model 11BC only)   
       Static r.p.m. at maximum permissible throttle setting:   
       Not over 2380, not under 2160.      No additional tolerance permitted.   
       Diameter:  Not over 71 in., not under 69.5 in.   
    
 (d)  (Model S11AC only)   
       Static r.p.m. at maximum permissible throttle setting:   
       Not over 2170, not under 2070.      No additional tolerance permitted.   
       Diameter:  Not over 74 in., not under 72 in.   
    
4. Propeller spinner (Aeronca Dwg. 4-708) (Model 11BC only). 1  lb. (-45) 
    
5. Propeller - Hartzell, ground adjustable, hub Model HA-12U, blades 7414 to 6814 or 7214M to 
6814M.  Eligible at diameter and static r.p.m. limits shown for fixed pitch wood models. 
18  lb. (-45) 
    
6. Omitted.   
    
7. Propeller - Koppers Aeromatic F200/00-72D.  Part s List Assembly No. 4324, revised 31  lb. (-45) 
 Feb. 21, 1949 (Eligible on Model 11AC a nd S11AC with A-65 engine only)   
 Low pitch setting 13° measured at 24 in. sta.   
 Static r.p.m. at maximum permissible throttle setting:   
 Not over 2300, not under 2200.      No additional tolerance permitted.   
 Diameter:  Not over 72 in., not under 70.5 in.   
 When this propeller is installed, installation and operation must be accomplished in accordance with 
Kopper's "Installation Procedure and Operating Limitations No. 22A." 
  
    
8. Propeller - Sensenich M74CK, fixed pitch metal 21  lb. (-45) 
    
 (a)  (Model 11AC only)   
       Static r.p.m. at maximum permissible throttle setting:   
       Not over 2250, not under 2100.      No additional tolerance permitted.   
       Diameter:  Not over 74 in., not under 72.5 in.   
    
 (b)  (Model S11AC only)   
       Static r.p.m. at maximum permissible throttle setting:   
       Not over 2170, not under 2070.      No additional tolerance permitted.   
       Diameter:  Not over 74 in., not under 72.5 in.   
    
9. Propeller - Sensenich M74CK-2, fixed pitch metal 21  lb. (-45) 
    
 (a)  (Model 11BC only)   
       Static r.p.m. at maximum permissible throttle setting:   
       Not over 2380, not under 2160.      No additional tolerance permitted.   
       Diameter:  Not over 72 in., not under 70 in.   
 
 
Propeller and Propeller Accessories (contd) 
9. Propeller - Sensenich M74CK-2,  fixed pitch metal (contd)   
 (b)  (Model S11BC only)   
       Static r.p.m. at maximum permissible throttle setting:   
       Not over 2380, not under 2280.      No additional tolerance permitted.

-6-  A-761
Rev. 18 
       Diameter:  Not over 72 in., not under 70 in.   
    
Engine and Engine Accessories - Fuel and Oil Systems 
    
101. Carburetor air heater 1  lb. (-32) 
    
102. Carburetor air scoop (Continental A-5810 or Aeronca 4-601) 2  lb. (-38) 
    
103. Carburetor air cleaner 1  lb. (-38) 
    
104. Auxiliary fuel tank (8 gal. capacity)  S ee NOTE 2(b) for required placard 8  lb. (+61) 
    
105. Cabin heater 2  lb. (-25) 
    
106. Starter - MacDowell (Aeronca Dwg. 7-600) 9  lb. (-39) 
    
107. Hanlon and Wilson mufflers and heaters Aeron ca Dwg. 7-557 (NOTE:  11AC and S11AC, weight 
of exhaust stacks removed to permit the installation -4 lb.) 
13  lb. (-32) 
    
108. Oil filter, Fram PB-5, Kit No. 510, Fram Industries Dwg. No. 61522 or 62399. 4  lb. (-21) 
    
109. Wright winter shutters, installed in accordance w ith Wright Installation Instructions No. 1, dated 
December 24, 1949, issued by Wright Flying Service, Williston, ND. 
2  lb. (-26) 
 
Landing Gear and Floats 
    
201. 6.00-6 wheels with brakes ( Goodyear Mode l L6MBD, Wheel Assembly No. 511413-M, Brake 
Assembly No. 511254-A) with 6.00-6 2 or 4 ply tires or 7.00-6 4-ply tires. 
36  lb. (  0) 
    
202. Tail wheel assemblies   
 (a)  6 x 2.00 steerable Scott Model AST-8, with leaf spring 11  lb (+181) 
 (b)  Maule Model SFS-12, SAFS-12 or SAFS-14 6  lb. (+181) 
 (c)  Scott Model 3-24B steerable 7  lb. (+181) 
 (d)  Imperial Model B-100 6  lb. (+181) 
 (e)  Decker steerable Model D-501 7  lb. (+181) 
    
203. Parking brake (Aeronca Dwg. 7-527) 1  lb. (  -1) 
    
204. 6.00-6 wheels with brakes ( Cleveland M odel 6:00 DMB, Wheel Assembly No. C-38500,  
Brake Assembly No. C-7000) with 6.00-6 2 or 4 ply tires or 7.00-6 4-ply tires. 
No weight change 
    
205. Skis   
 (a)  Federal A-1500 (Federal Instal. Dwg. 11R241) 37  lb. (  0) 
 (b)  Federal CA-1850-6 (Federal Instal. Dwg. 11R241) 48  lb. (  0) 
 (c)  Federal A-2000A (Federal Instal. Dwg. 11R241) 49  lb. (  0) 
 (d)  Federal A-2000 (Federal Instal. Dwg. 11R241) 41  lb. (  0) 
 (e)  Federal A-1850 (Federal Instal. Dwg. 11R241) 38  lb. (  0) 
 (f)  Federal A-1500A (Federal Instal. Dwg. 11R241) 39  lb. (  0) 
 (g)  Federal Model AWB-1500 wheel skis when installed in accordance with Federal Instal. 
      Dwg. 11R471.  Placard required on ski position selector box: 
      "SKI CONTROL" 
      "UP-NEUTRAL-DOWN" 
  75  lb. 
Retracted 
   (-6) 
 
Extended 
(-3.5) 
 
 
Landing Gear and Floats (contd) 
205. Skis (contd)   
 (h)  Federal Model AWB-1500A wheel skis when installed in accordance with Federal 
       Instal. Dwg. 11R471.  Placard required on ski position selector box: 
      "SKI CONTROL" 
      "UP-NEUTRAL-DOWN" 
  84  lb. 
Retracted 
   (-6) 
 
Extended 
(-3.5)

-7-  A-761
Rev. 18 
206. Toe brakes (Aeronca Dwg. 7-554) 2  lb. (  -5) 
    
207. Wheel pants (Aeronca Dwg. 7-606B and 7-607A) 6  lb. (   0) 
    
208. Edo 92-1400 float installation 167 lb. (+19) 
    
209. Auxiliary ventral fin (Aeronca Dwg. 4-657) 4  lb. (+161) 
    
210. Consolidair Model 17 wheel fenders (Consolid air Installation Dwg. No. 0036) 10  lb. (   0) 
 
Electrical Equipment 
    
301. Generator - wind-driven (Champion 8 amp.) 8  lb. ( +9) 
    
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 and at all times thereafter 
(except in the case of air carrier operations having an approved weight control system). 
 
NOTE 2.  (a) On models 11AC and S11AC, the following placard must  be installed on the instrument panel in plain view of the 
pilot. 
 
 "INTENTIONAL SPINNING PROHIBITED WHEN BAGGAGE IS CARRIED." 
 
                (b) For airplanes equipped with the aux iliary fuel tank, the following placard, or equivalent, must be displayed near 
the fuel shut-off valve and in view of the pilot. 
 
 "TRANSFER FUEL IN LEVEL FLIGHT OR GLID E ONLY AND WHEN MAIN TANK IS HALF FULL OR 
LESS.  VALVE IS TO BE CLOSED EXCEPT WHILE TRANSFERRING FUEL." 
 
 
 
 
 
 
...END...
```

## ADs (13, in force first)

- [AD 2000-25-02 R1](https://openairdocs.org/ad/2000-25-02-R1): Wood Spars · American Champion 11AC, 11BC, 11CC and 27 more. Effective Jul 13, 2001
- [AD 47-20-01](https://openairdocs.org/ad/47-20-01): Gascolator Bowl Cleaning · American Champion 11AC, 7AC and 7BCM (Army L-16A). Effective Mar 18, 1980
- [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 47-20-02](https://openairdocs.org/ad/47-20-02): Oleo Piston · American Champion 11AC and 7AC
- [AD 47-30-01](https://openairdocs.org/ad/47-30-01): Lift Strut Wing Attach Fittings · American Champion 11AC and 7AC
- [AD 47-30-05](https://openairdocs.org/ad/47-30-05): Exhaust Stack Inspection · American Champion 11AC and 7AC
- [AD 48-04-02](https://openairdocs.org/ad/48-04-02): Wing Rib Rework · American Champion 11AC, 11BC and 7AC
- [AD 48-08-02](https://openairdocs.org/ad/48-08-02): Cleveland Wheels · American Champion 11AC, 11BC, 11CC and 33 more
- [AD 48-13-07](https://openairdocs.org/ad/48-13-07): Turnbuckle Fork Replacement · American Champion 11AC and S11AC
- [AD 49-11-02](https://openairdocs.org/ad/49-11-02): Wing Attach Fitting · American Champion 11AC, 11BC, 11CC and 4 more
- [AD 49-15-01](https://openairdocs.org/ad/49-15-01): Seat Anchorage Rework · American Champion 11AC, 11BC and S11AC
- [AD 52-28-01](https://openairdocs.org/ad/52-28-01): Fuel Transfer Placard · American Champion 11AC and S11AC
- [AD 2000-25-02](https://openairdocs.org/ad/2000-25-02) (historical): Wood Wing Spars · American Champion 11AC, 11BC, 11CC and 15 more. Effective Jan 19, 2001

## Registered aircraft by registry model (OpenAirDocs)

- [Aeronca 11AC](https://openairdocs.org/model/aeronca-11ac): 603 aircraft (registry code 0191102)
- [Aeronca 11BC](https://openairdocs.org/model/aeronca-11bc): 65 aircraft (registry code 0191106)
- [Aeronca S11AC](https://openairdocs.org/model/aeronca-s11ac): 6 aircraft (registry code 0191104)
- [Aeronca S11BC](https://openairdocs.org/model/aeronca-s11bc): 1 aircraft (registry code 0191108)
- [Aeronca/Miller/Delaney 11AC](https://openairdocs.org/model/aeronca-miller-delaney-11ac): 1 aircraft (registry code 0191105)
- [Champion 11BC](https://openairdocs.org/model/champion-11bc): 1 aircraft (registry code 21101P6)
- [Champion 11AC](https://openairdocs.org/model/champion-11ac): 0 aircraft (registry code 21101P4)
- [Champion S11AC](https://openairdocs.org/model/champion-s11ac): 0 aircraft (registry code 21101P5)
- [Champion S11BC](https://openairdocs.org/model/champion-s11bc): 0 aircraft (registry code 21101P7)

## STCs approved under this data sheet (94, first 50)

- [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, 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 SA00079NY](https://openairdocs.org/stc/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.. Airwolf Filter Corporation
- [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC
- [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC
- [STC SA345CE](https://openairdocs.org/stc/SA345CE): Remove right door. Install following placard in front of and in clear view of pilot.. Stephen D. Woodin
- [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC
- [STC SA03898NY](https://openairdocs.org/stc/SA03898NY): Installation and maintenance of ORATEX covering and coating material. Aircraft Design & Certification Ltd
- [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc.
- [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc.
- [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC
- [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA04301CH](https://openairdocs.org/stc/SA04301CH): Attachment of fabric covering and wing leading edge. C William Pancake Jr
- [STC SA2710WE](https://openairdocs.org/stc/SA2710WE): Installation of carburetor heat box bearings.. Del-Air
- [STC SA02529AK](https://openairdocs.org/stc/SA02529AK): Installation of the GSD Landing Gear System, Aeronca/American Champion 7 & 11 series
airplanes. Mr. Ernie Broten
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [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 SA02503AK](https://openairdocs.org/stc/SA02503AK): Installation of AMSAFE State of the Art Restraint System (SOARS) inflatable restraints. AMSAFE Inc.
- [STC SA04202AT](https://openairdocs.org/stc/SA04202AT): Replacement of either a 65 horsepower Continental A65-8 or A65-8F engine with a 85 horsepower Continental C85-12F or a C85-12 which have provisions for an electrical starter. C William Pancake Jr
- [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 SA10077SC](https://openairdocs.org/stc/SA10077SC): Installation of push-button starter system.. Hartzell Engine Technologies, LLC
- [STC SA4773NM](https://openairdocs.org/stc/SA4773NM): Installation of replacement metal leading edge.. MILMAN Engineering Inc
- [STC SA02566CH](https://openairdocs.org/stc/SA02566CH): Installation of the Custom Fiberglass Molding, Inc. (CFMI) Model 1500, 2250-001, or 2250-002 Aircraft Main Landing Gear Skis. Silveraire LLC
- [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc.
- [STC SA01768SE](https://openairdocs.org/stc/SA01768SE): Installation of an oil cooler system.. Steve's Aircraft
- [STC SA4305WE](https://openairdocs.org/stc/SA4305WE): Installation of GAR-AERO wheel adapters and tundra type tires on the main landing gear. Seaplanes North LLC
- [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 SA02428AK](https://openairdocs.org/stc/SA02428AK): Installation of a hydraulically actuated ski drag assembly. Northern Airframes LLC
- [STC SA02295SE](https://openairdocs.org/stc/SA02295SE): Installation of an alternate method of fastening aluminum wing ribs to wood spars. Rainbow Flying Service LLC
- [STC SA01765SE](https://openairdocs.org/stc/SA01765SE): Installation of Alaskan Bushwheel TSO-C26d wheels, Part Number (P/N) ABI-1010. ABI, LLC
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft
- [STC SA217AL](https://openairdocs.org/stc/SA217AL): Installation of Airglas Engineering Co. Inc. Model L-1650A or L-2000A skis. Airglas Inc.
- [STC SA535AL](https://openairdocs.org/stc/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.. Cub Crafters Inc
- [STC SA02370AK](https://openairdocs.org/stc/SA02370AK): Option (1) Installation of a replacement main tank fuel valve. Burl's Aircraft LLC
- [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated
- [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories.. Electronics International Inc.
- [STC SA57RM](https://openairdocs.org/stc/SA57RM): Installation of Lycoming O-235-C1, -C1A, -C1B, -C1C, -C2A, -C2B, -C2C, -H2C, -K2A, -K2B, -L2A, or L2C series engines.. Coleman T. Wagner
- [STC SA01988SE](https://openairdocs.org/stc/SA01988SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.. Electronics International Inc.
- [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC
- [STC SA3358NM](https://openairdocs.org/stc/SA3358NM): Production of aircraft wing ribs as specified in W. N. Kutner's 'Report #1 STC Request for Wing Ribs.'. Coleman T. Wagner
- [STC SA02033AT](https://openairdocs.org/stc/SA02033AT): Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.. M-20 Oil Separators LLC
- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc
- [STC SA00823SE](https://openairdocs.org/stc/SA00823SE): Fabrication and Installation of Rainbow Flying Service front and rear wing spars and modified wing ribs. Rainbow Flying Service
- [STC SA241CH](https://openairdocs.org/stc/SA241CH): Install Ceconite 101 fabric.. Aviation Products Systems Inc.
- [STC SA73CH](https://openairdocs.org/stc/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.. Aero Fabricators Co

All 94: https://openairdocs.org/tcds/A-761/stcs.md

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