# TCDS A-675: Thomas Gores

- Type: Type certificate data sheet
- Status: Current
- Holder: Thomas Gores
- Revision: 9
- Revised: February 23, 2022
- Product: Aircraft, Small Airplane
- Registered aircraft: 235, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/28/32/28323ac6e060a2a9f028f9c557444bf433b1b3c0b8885f841852450f07b279ab
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CE651BC352A4A32F862587FF004B33B1.0001
- Page: https://openairdocs.org/tcds/A-675

## Models (7)

As the data sheet lists them.

- 50-C
- KCA
- S-65-C
- S-65-CA
- 65-CA (Army L-3F)
- S-50-C
- 65-C

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
 
TYPE CERTIFICATE DATA SHEET NO. A-675 
 
 
Type Certificate Holder: Thomas Gores 
 12008 W Belmar Dr. 
Franklin, Wisconsin 53132 
Type Certificate Holder Record: Mr. William J. Gores 
12008 Belmar Dr. 
Franklin, Wisconsin 53132 
 
1- Model KCA, 2 PCLM, Approved April 26, 1938. 
Model 50-C, 2 PCLM, Approved August 11, 1938 (Same as KCA except for wider cabin and modified engine 
cowling). 
Model S-50-C, 2 PCSM, Approved August 11, 1938 (Same as 50-C except for the landing gear). 
 
 KCA 2 PCLM 50-C 2 PCLM S-50-C 2 PCSM 
Engines Continental A-50-1 Continental A-50-1 Continental A-50-1 
(See Item 307 (a), (b), (c), (d), and (e)) 
 
Fuel 
 
73 min. octane av. gas 
 
73 min. octane av. gas 
 
73 min. octane av. gas 
Engine Limits (for all operations) 1900 r.p.m (50 h.p) 1900 r.p.m (50 h.p) 1900 r.p.m (50 h.p) 
Airspeed Limits (CAS) 
Level flight or climb 
 
100 m.p.h ( 87 knots) 
 
100 m.p.h ( 87 knots) 
 
95 m.p.h  ( 82 knots) 
Glide or dive 135 m.p.h (117 knots) 135 m.p.h (117 knots) 129 m.p.h  (112 knots) 
Propeller Limits 
Maximum permissible diameter 
 
81 in. 
 
81 in. 
 
76 in. 
C.G.Range (+13.4) to (+20.5) (+13.4) to (+20.7) (+14.1) to (+21.1) 
Empty Weight C.G. Range (+13.9) to (+20.3) with  
standard fuel tank only. 
(+13.9) to (+17.4) with 
Item 312(a) installed. 
(+14.3) to (+20.5) with 
standard fuel tank only. 
(+14.3) to (+17.6) with 
Item 312(a) installed. 
(+15.1) to (+21.2) with  
standard fuel tank only. 
(+15.1) to (+18.3) with 
Item 312(a) installed. 
When the empty weight C.G. falls within these ranges, it is unnecessary to 
check critical C.G. positions. Ranges are not valid for non-standard 
arrangements. 
 
Maximum Weight 1150 lbs. 1150 lbs. 1253 lbs. 
No. of Seats 2 (+21) 2 (+21) 2 (+21) 
 
Page No. 1 2 3 4 5 6 
Rev No. 9 7 7 7 8 7 
Reformatted 7/94. 
A-675 
Revision 9 
AERONCA 
KCA 
50-C 
S-50-C 
65-C 
S-65-C 
(L-3F) 65-CA 
S-65-CA 
 
February 23, 2022

A-675 Page 2 
 
 
 KCA 2 PCLM 50-C 2 PCLM S-50-C 2 PCSM 
Maximum Baggage 40 lbs. (+45) 40 lbs. (+45) 40 lbs. (+45) 
Fuel Capacity (see Item 312 (a)) 10 gal. (-10) 12 gal. (-10) 12 gal. (-10) 
Oil Capacity 1 gal. (-21) 1 gal. (-21) 1 gal. (-21) 
Control Surface Movements Elevators 30°up; 30°down 
Rudder 30° right; 30° left 
Ailerons not available 
Elevators 30°up; 30°down 
Rudder 30° right; 30° left 
Ailerons not available 
Elevators 30°up; 30°down 
Rudder 30° right; 30° left  
Ailerons not available 
Serial No. Eligible KCA-1 and up C-1018 and up C-1018 and up 
Required Equipment Items 101(a), 102, 103 
104, and 105 
Items 101(a), 102, 103 
104, and 105 
Items 103, 104, 105, and 
151 
Not eligible for original certification with single ignition engines after August 1, 1941. 
 
II – Model 65-C, 2 PCLM, Approved June 7, 1939 (Same as 50-C except for the engine installation). 
Model S-65-C, 2 PCSM, Approved June 7, 1939 (Same as 65-C except for the landing gear). 
 65-C 2 PCLM S-65-C 2 PCSM 
Engines Continental A-65-1 Continental A-65-1 
(See Item 307 (f), (g), and (h)) 
 
Fuel 
 
73 min. octane av. gas 
 
73 min. octane av. gas 
Engine Limits (for all operations) 2350 r.p.m. (65 hp.) 2350 r.p.m. (65 hp.) 
Airspeed Limits (CAS) 
Level flight or climb 
 
100 m.p.h. ( 87 knots) 
 
95 m.p.h. ( 82 knots) 
Glide or dive 135 m.p.h (117 knots) 129 m.p.h. (112 knots) 
Propeller Limits 
Maximum permissible diameter 
 
81 in. 
 
76 in. 
C.G. Range (+13.4) to (+20.7) (+14.1) to (+21.1) 
Empty Weight C.G. Range (+14.3) to (+20.5) with standard fuel 
tank only. 
(+14.3) to (+17.6) with Item 312(a) 
installed. 
(+15.1) to (+21.2) with standard fuel 
tank only. 
(+15.1) to (+18.3) with Item 312(a) 
installed. 
When the empty weight C.G. falls within these ranges, it is unnecessary to check 
critical C.G. positions. Ranges are not valid for non-standard arrangements. 
 
Maximum Weights 
 
1150 lbs. 
 
1253 lbs. 
No. of Seats 2 (+21) 2 (+21) 
Maximum Baggage 40 lbs. (+45) 40 lbs. (+45) 
Fuel Capacity (see Item 312(a)) 12 gal. (-10) 12 gal. (-10) 
Oil Capacity 1 gal. (-21) 1 gal. (-21)

Page 3 A-675 
 
 
 65-C 2 PCLM S-65-C 2 PCSM 
Control Surface Movements Elevators 30°up;  30°down 
Rudder 30° right;  30° left  
Ailerons not available 
Elevators 30°up;  30°down 
Rudder 30° right;  30° left  
Ailerons not available 
Serial No. Eligible C-1018 and up C1018 and up 
Required Equipment Items 101(a), 102, 103, 104, and 105 Items 103, 104, 105, and 151 
Not eligible for original certification with single ignition engines after 
August 1, 1941. 
 
III – Model 65-CA (L-3F), 2 PCLM, Approved September 11, 1940 (Same as 50-C except for minor structural changes, 
equipment changes, and the engine installation). 
Model S-65-CA, 2 PCSM, Approved November 15, 1940 (Same as 65-CA except for the landing gear). 
 
65-CA (L-3F)  2 PCLM S-65-CA 2 PCSM 
 
Engines Continental A-65-8 Continental A-65-8 
(See Item 307 (f), (i), and (j)) 
 
Fuel 73 min. octane av. gas 73 min. octave av. gas 
Engine Limits (for all operations) 2300 r.p.m. (65 hp) 2300 r.p.m. (65 hp.) 
Airspeed Limits (CAS)   
Level flight or climb 100 m.p.h. ( 87 knots) 95 m.p.h. ( 82 knots) 
Glide or dive 135 m.p.h. (117 knots) 129 m.p.h. (112 knots) 
Propeller Limits   
Static r.p.m. at full throttle 
Maximum 
 
2150 
 
2070 
Minimum 2050 1970 
No additional tolerance permitted 
Diameter: 
Maximum 
 
 
78 in. 
 
 
76 in. 
Minimum 70 in. 74 in. 
 
C. G. Range (+13.9) to (+21.2) (+14.1) to (+21.1) 
 
Empty Weight C. G. Range (+15.7) to (+20.5) with standard fuel 
tank only. 
(+15.9) to (+20.4) with standard fuel 
tank only. 
 (+15.7) to (+19.0) with Item 312(b) (+15.9) to (+19.0) with Item 312(b) 
 installed. installed. 
When the empty weight C.G. falls within these ranges, it is unnecessary to check 
critical C.G. positions. Ranges are not valid for non-standard arrangements. 
 
Maximum Weight 
 
1250 lbs. 
 
1320 lbs. 
No. of Seats 2 (+21) 2 (+21) 
Maximum Baggage 70 lbs. (+48) 70 lbs. (+48)

A-675 Page 4 
 
 
 65-CA (L-3F) 2 PCLM S-65-CA 2 PCSM 
Fuel Capacity (see Item 312(b)) 17 gal. (-8) 17 gal. (-8) 
Oil Capacity 1 gal (-32) 1 gal (-32) 
Control Surface Movements Elevators 30° up; 30° down 
Rudder 30° right; 30° left 
Ailerons not available 
Elevators 30° up; 30° down 
Rudder 30° right; 30° left 
Ailerons not available 
Serial No. Eligible C-10010 and up and all AAF Nos. C-10010 and up 
Required Equipment Items 101(b), 102, 103, 104, and 105 Items 103, 104, 105, and 151 
Not eligible for original certification with single ignition engines after 
August 1, 1941. 
 
Specifications Pertinent to All Models 
 
Datum Wing leading edge. 
Leveling Means Incidence of No. 2 wing rib is (-1½°) when aircraft is level. 
Certification Basis Type Certificate No. 675 (Aeronautical Bulletin 7-A) 
 
Production Basis None. Prior to original certification of each aircraft manufactured subsequent to 
August 24, 1949, 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 (no longer listed on Specification Sheet) 
 
Equipment A plus (+) or minus (-) sign preceding the weight of an item indicates net weight changes 
when that item is installed. 
 
KCA, 50-C, S-50-C 65-CA 
Propeller and Propeller Accessories 65-C, S-65-C S-65-CA 
103. Propeller 
(a) Wood, fixed or adjustable pitch, including hub 15 lb. (-44) 15 lb. (-44) 
(b) Fixed pitch metal, McCauley 1A90 (Models 65-C, with Items 307 (f), 26 lb. (-44) 26 lb. (-44) 
(g), and (h) and 65-CA only) with following limits; 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. 
 
Engine and Engine Accessories – Fuel and Oil Systems 
104. Carburetor Air Heater 4 lb. (-28) 1 lb. (-28) 
106. Oil Filter, Fram PB-5, Kit No. 510 (weight includes 1 qt. of oil) 
(a) Fram installation Dwg. 61538. All except KCA 
 
4 lb. (-19) 
 
--- --- 
KCA (only) 4 lb. (-31) --- --- 
(b) Fram installation Dwg. 61540 (models with engine starter). --- --- 4 lb. (-19)

Page 5 A-675 
 
KCA, 50-C, S-50-C 65-CA 
65-C, S-65-C S-65-CA 
 
307. Engines (Continental) (Note – Airplane not eligible for original 
 certification with single ignition engines after August 1, 1941.  
(a) A -50-2: Limits for all operations – 1900 r.p.m. (50 hp) +6 lb. (-23) --- --- 
(b) A-50-3 or A-50-8: Limits for all operations -1900 r.p.m. (50 hp) +10 lb. (-23) --- --- 
(c) A-50-4 or A-50-7: Limits for all operations -1900 r.p.m. (50 hp) Neglect wt. incrse --- --- 
(d) A-50-5 or A-50-9: Limits for all operations – 1900 r.p.m. (50 hp) +13 lb. (-23) --- --- 
(e) A-50-6: Limits for all operations – 1900 r.p.m. (50 hp) +16 lb. (-23) --- --- 
(f) A-65-7 or A-65-7J: Limits for all operations – 2300 r.p.m. (65 hp) Neglect wt. incrse -10 lb. (??) 
(g) A-65-3, A-65-8, A-65-8F (Add 1 lb), or A-65-3J: +10 lb. (-23) --- --- 
Limits for all operations – 2300 r.p.m. (65 hp)   
(h) A-65-6, A-65-9, A-65-6J, or A-65-9J: +13 lb. (-23) --- --- 
Limits for all operations – 2300 r.p.m. (65 hp)    
 (i) A-65-8J: Limits for all operations – 2300 r.p.m. (65 hp) +10 lb. (-23) Neglect wt. inc. 
 (j) A-65-9 or A-65-9J: Limits for all operations – 2300 r.p.m. (65 hp) --- --- +3 lb. (-23) 
312. (a) 5 gal. aux. fuel tank (fuel arm is (+48)) 10 lb. (+29) --- --- 
 (b) 8 gal. aux. fuel tank and 5 qt. oil sump (fuel arm is (+55)). --- --- --- --- 
5 qt. oil sump is required with this fuel tank. 
Placard fuel valve as follows: “Drain aux. tank in glide or level flight after using half of main tank”. 
320. Revised engine mount (Dwg. 4-72, change B) to accommodate rubber Neglect wt. change --- --- 
 bushed engine.   
325. Oil radiator (Continental) --- --- 5 lb. (-37) 
328. Hummer starter --- --- +14 lb. (+21) 
 
Landing Gear and Floats 
101. 6.00-6 wheels with tires  
 (a) (Shinn 654) 21 lb. (-1) --- --- 
 (b) (Shinn 6C5) --- --- 23 lb. (-1) 
102. Tail skid Neglect weight Neglect Weight 
151. Edo 60-1320 float installation including auxiliary fin (169 lb.) +112 lb. (+28.6) +106 lb. (+27) 
301. Wheels   
 (a) 3 in. (Goodyear 3-LMBM) with brakes +10 lb. (-1) --- --- 
 (b) 6.00-6 (Shinn 6C4B or 6C4HB) with brakes +5 lb. (-1) --- --- 
 (c) 3 in. (Goodyear 3-LNBM) 1 lb. (-1) --- --- 
 (d) 6.00-6 (Shinn 605HB) with brakes --- --- +5 lb. (-1) 
 (e) 6.00-6 (General Airmotive Corp. MBA) with brakes (requires --- --- +7 lb. (-1) 
 axle 3-180)   
 (f) 6.00-6 (Goodyear L6MBM) with brakes --- --- +5 lb. (-1) 
302. Tires   
 (a) 18x8-3 with tube +4 lb. (-1) --- --- 
 (b) 16x7-3 with tube Neglect wt. incrse --- --- 
303. Tail wheel installation   
 (a) Shock cord type with 6x2.00 wheel and pneumatic tire +1 lb. (+174) --- --- 
 (b) Leaf spring type with 6 in. wheel and solid tire +2 lb. (+180) +2 lb. (+180) 
 (c) 6x2.00 steerable +3 lb. (+179) +3 lb. (+179) 
 (d) Maule Model SFS-12, or SS12, or SAFS-12 6 lb. (+179) 6 lb. (+179) 
309. Wheel streamliners 8 lb. (-1) 6 lb. (-1) 
317. Ski type axle struts (Dwg. 3-43 or 3-44) Neglect wt. incrse --- --- 
318. Seaplane fitting Neglect wt. incrse --- --- 
321. Parking brake installation +1 lb. (-6) +1 lb (-6)

A-675 Page 6 
 
  KCA, 50-C, S-50-C 65-CA 
  65-C, S-65-C S-65-CA 
326. Shock strut special attachment bolt (Dwg. 1-875) --- --- Neglect weight 
327. Skis   
 (a) Washington Aircraft 1200 Use actual wt. --- --- 
 (b) Federal SA-1 Use actual wt. --- --- 
 (c) Federal SA-2 Use actual wt. --- --- 
 (d) Federal SC-1 Use actual wt. Use actual wt. 
 (e) Federal SC-2 Use actual wt. --- --- 
 (f) Marston MFS-1200 Use actual wt. --- --- 
 (g) Marston MFS-1600 Use actual wt. --- --- 
 (h) Jennings TY-2 Use actual wt. --- --- 
 (i) Richards I-B Use actual wt. --- --- 
 (j) Graf-Shupe A Use actual wt. --- --- 
 (k) Aero sales and Service AS-6.00-6 Use actual wt. --- --- 
 (l) Heath 655 Use actual wt. --- --- 
 (m) Federal SA-1A Use actual wt. Use actual wt. 
 (n) Heath 725 Use actual wt. Use actual wt. 
 (o)  Jack Carr 16 (Max. 1600 lb.) Use actual wt. Use actual wt. 
 (p) Heath 725A (Max. 1450 lb.) Use actual wt. Use actual wt. 
 (q)  Federal CA-1850-6 (Federal Instal. Dwg. 11R241) 48 lb. (0) 48 lb. (0) 
 (r) Federal A-2000-A (Federal Instal. Dwg. 11R241) 49 lb. (0) 49 lb. (0) 
 (s) Federal A-2000 (Federal Instal. Dwg. 11R241) 41 lb. (0) 41 lb. (0) 
 (t) Federal A-1850 (Federal Instal. Dwg. 11R241) 38 lb. (0) 38 lb. (0) 
 (u Federal A-1500 (Federal Instal. Dwg. 11R241) 37 lb. (0) 37 lb. (0) 
 (v) Federal A-1500A (Federal Instal. Dwg. 11R241) 39 lb. (0) 39 lb. (0) 
 
Electrical Equipment 
310. Battery Max. 20 lb. (+48) Max. 20 lb. (+48) 
319. Landing lights (Grimes ST-250) (one or two) 5 lb. ea. (+17) 5 lb. ea. (+17) 
323. Generator – wind driven (Air Associates G-6 or G-12) 8 lb. (+9) 8 lb. (+9) 
 
Interior Equipment 
 
 
 
 
M 
105. Wheel Type control column (Dwg. 7-35) 
201. Flare installation (three 1½ min.) 
305. Cabin heater 
322. Stick type control column (replacing wheel) 
X 
---   --- 
2 lb. (-25) 
Neglect wt. change 
X 
23 lb. (+50) 
2 lb. (-16) 
--- --- 
 
iscellaneous (not listed above) 
311. Extra Door 2 lb. (+21) 2 lb. (+21) 
316. Anchor and rope 7 lb. (+2) 7 lb. (+2) 
324. Steps (two) Neglect weight Neglect Weight 
  
…END…
```

## ADs (2, in force first)

- [AD 96-09-06](https://openairdocs.org/ad/96-09-06): Air Filter Assemblies · Maule Aerospace Technology 7ACA, 7ECA, 7FC and 180 more. Effective Jun 7, 1996
- [AD 47-30-08](https://openairdocs.org/ad/47-30-08): Seat Modification · Gores, William 65-CA (Army L-3F), 65-LA and S-65-CA. Effective Sep 30, 1947

## Registered aircraft by registry model (OpenAirDocs)

- [Aeronca 65-CA](https://openairdocs.org/model/aeronca-65-ca): 141 aircraft (registry code 0190922)
- [Aeronca 65-C](https://openairdocs.org/model/aeronca-65-c): 72 aircraft (registry code 0190920)
- [Aeronca KCA](https://openairdocs.org/model/aeronca-kca): 8 aircraft (registry code 0190406)
- [Aeronca 50-C](https://openairdocs.org/model/aeronca-50-c): 7 aircraft (registry code 0190712)
- [Aeronca S-65-C](https://openairdocs.org/model/aeronca-s-65-c): 4 aircraft (registry code 0190926)
- [Aeronca S-65-CA](https://openairdocs.org/model/aeronca-s-65-ca): 2 aircraft (registry code 0190928)
- [Aeronca/Browne 65-CA](https://openairdocs.org/model/aeronca-browne-65-ca): 1 aircraft (registry code 0190923)

## STCs approved under this data sheet (31)

- [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 SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels 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 SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc.
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc.
- [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc.
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft
- [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC
- [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 SA01944CH](https://openairdocs.org/stc/SA01944CH): 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.. Experimental Aircraft Association Inc.
- [STC SA742GL](https://openairdocs.org/stc/SA742GL): Superseded by STC SA01944CH.  Modify airplane to fly on unleaded automotive gasoline, 87 minimum antiknock index. EAA Aviation Foundation
- [STC SA8075SW](https://openairdocs.org/stc/SA8075SW): Installation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER). Razorback Fabrics Inc
- [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP.. M-20 Oil Separators LLC
- [STC SA00279LA](https://openairdocs.org/stc/SA00279LA): Installation of Ameri-King AK-950 Global Positioning System Navigation Switching/Annunciator Panel and Associated Equipment. Ameri-King Corporation
- [STC SA71GL](https://openairdocs.org/stc/SA71GL): Installation of air filters. Brackett Aero Filters Inc.
- [STC SA2-952](https://openairdocs.org/stc/SA2-952): Installation of fiberglass covering.. Razorback Fabrics Inc
- [STC SA928NE](https://openairdocs.org/stc/SA928NE): Added unleaded automative gasoline.. Lovett Charles J
- [STC SA4624NM](https://openairdocs.org/stc/SA4624NM): Installation of F. Atlee Dodge springs 2097 and 2127 to replace bungee cords on ski equipped airplanes.. F Atlee Dodge Aircraft Service
- [STC SA1351WE](https://openairdocs.org/stc/SA1351WE): Replace existing fabric on wings, fuselage, empennage, and/or control surfaces, with Ceconite101 material. (262A Series -12). Ceconite Inc
- [STC SA4-1210](https://openairdocs.org/stc/SA4-1210): Installation of Eonnex cover on aircraft surfaces.. Ceconite, Inc
- [STC SA1-583](https://openairdocs.org/stc/SA1-583): Continental A-65-8 engine and Sensenich 72GK42 propeller.. Oldfield A H
- [STC SA4-1298](https://openairdocs.org/stc/SA4-1298): Ceconite 101 covering of complete airplane.. Cooper Engineering Corporation
- [STC SA4-288](https://openairdocs.org/stc/SA4-288): BN-1 propeller spinner.. Raymond M Stits
- [STC SA1-150](https://openairdocs.org/stc/SA1-150): Continental C-85-8 engine, Sensenich 75GK-50 propeller, and Harrison HE431-9 engine oil cooler.. North American Flying Srvc
- [STC SA1201GL](https://openairdocs.org/stc/SA1201GL) (historical): Authorize Gross Weight Increase from 1150 lbs to 1200 lbs. Lawrence F. Diedrich

---
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