# TCDS A-699: Taylorcraft Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Taylorcraft Inc.
- Revision: 6
- Revised: August 11, 1971
- Product: Aircraft, Small Airplane
- Registered aircraft: 33, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/98/66/9866e4fc9d1d030c0ad73d9fc4de29a31ae177e8e42f0c40df65e7f9c60109fc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3D4F3589CFDB308086257D7E00552C52.0001
- Page: https://openairdocs.org/tcds/A-699

## Models (8)

As the data sheet lists them.

- BFS-60
- BF
- BFS-65
- BF12-65
- BF-65
- BFS
- BFS12-65
- BF-60

## 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. 6 5 6 5 5 5 5 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A-699 
Revision 6 
TAYLORCRAFT 
(Army L-2G) BF 
BFS 
BF-60 
BFS-60 
BF-65 
BFS-65 
(Army L-2K) BF12-65 
BFS12-65 
 
August 11, 1971 
 
AIRCRAFT SPECIFICATION NO. A-699 
 
Type Certificate Holder: Taylorcraft, Inc. 
  Connellsville Airport 
  Connellsville, Pennsylvania  15425 
 
I - Model BF (Army L-2G), 2 PCLM, Approved 19 September 1938; Model BFS, 2 PCSM, Approved 5 April 1939 
 
 Engine Franklin 4AC-150 Series 50 (Single ignition - Scintilla magneto). 
  (See Item 308 for optional engines.) 
 
 Fuel 70 min. octane aviation gasoline. 
 
 Engine limits For all operation, 2300 r.p.m. (50 hp.). 
 
 Airspeed limits Landplane: Level flight or climb 105 m.p.h. 
   (True Ind.)  Glide or dive 131 m.p.h. 
  Seaplane: Level flight or climb    95 m.p.h. 
    129 m.p.h. 
 
 Propeller limits Landplane: maximum diameter 83 in. 
  Seaplane: maximum diameter 79 in. 
 
 Center of Gravity Landplane: (+14.5) to (+19.5) 
   (C.G.)  range Seaplane: (+15.1) to (+19.4) 
 
 Empty weight C.G. range Landplane: (+15.3) to (+18.4) 
  Seaplane: (+15.9) to (+18.3) 
  When empty weight C.G. falls within the pertinent range, computation of critical  
  fore and aft C.G. positions is unnecessary.  Ranges are not valid for  
  non-standard arrangements. 
 
 Maximum weight Landplane: 1100 lb. (Serial No. 1407 and up are eligible at 1150 lb.).  
  Seaplane: 1228 lb. 
 
 Number of seats 2 (+23) 
 
 Maximum baggage 30 lb. (+40) 
 
 Fuel capacity 12 gal. (-9) (See item 312 for auxiliary tank).

A-699  Page 2 
 
 Oil capacity 1 gal. (-34) 
 
Control surface movements Elevators 27° up 25° down 
 Ailerons 25° up 25° down 
 Rudder 26° right 26° left 
 
 Serial Numbers eligible 1001 and up. 
 
 Required equipment Landplane: Items 101, 102, 103, 104 and 105 
  Seaplane: Items 103, 104, 105, and 151. 
 
II - Model BF-60, 2 PCLM, Approved 22 July 1939; Model BFS-60, 2 PCSM, Approved 7 October 1939 
   (Same as BF and BFS except for engine installation.) 
 
 Engine Franklin 4AC-171 (See Item 308 for optional engines). 
 
 Fuel 70 min. octane aviation gasoline. 
 
 Engine limits For all operations, 2350 r.p.m. (60 hp.). 
 
 Airspeed limits Landplane: Level flight or climb 105 m.p.h. 
   (True Ind.)  Glide or dive 131 m.p.h. 
  Seaplane: Level flight or climb   95 m.p.h. 
   Glide or dive 129 m.p.h. 
 
 Propeller limits Static r.p.m. at maximum permissible throttle setting: 
   Not over 2330, not under 2120.  No additional tolerance permitted.  
  Diameter -  Landplane: Not over 83 in., not under 72 in. 
    Seaplane: Not over 79 in., not under 72 in. 
 
 Center of Gravity Landplane: (+14.5) to (+19.7) 
   (C.G.)  range Seaplane: (+15.1) to (+20.1) 
 
 Empty weight C.G. range Landplane: (+15.3) to (+18.5) 
  Seaplane: (+15.9) to (+19.0) 
  When empty weight C.G. falls within the pertinent range, computation of critical  
  fore and aft C.G. positions is unnecessary.  Ranges are not valid for non-standard  
  arrangements. 
 
 Maximum weight Landplane: 1100 lb. (Serial No. 1407 and up eligible at 1150 lb.).  
  Seaplane: 1228 lb. (Serial No. 1432 and up eligible at 1278 lb.).  
 
 Number of seats 2 (+23) 
 
 Maximum baggage 30 lb. (+40) 
 
 Fuel capacity 12 gal. (-9) (See item 312 for auxiliary tank). 
 
 Oil capacity 1 gal. (-34) 
 
Control surface movements Elevators 27° up 25° down 
 Ailerons 25° up 25° down 
 Rudder 26° right 26° left 
 
 Serial Numbers eligible 1001 and up. 
 
 Required equipment Landplane: Items 101, 102, 103, 104 and 105 
  Seaplane: Items 103, 104, 105, and 151.

A-699  Page 3 
 
III - Model BF-65,2 PCLM, and Model BFS-65, 2 PCSM, Approved 21 August 1941 
    (Same as BF and BFS except for engine installation). 
 
 Engine Franklin 4AC-176-B2  
  (See Item 308 for optional engines.) 
 
 Fuel 73 min. octane aviation gasoline. 
 
 Engine limits For all operations, 2200 r.p.m. (65 hp.). 
 
 Airspeed limits Landplane: Level flight or climb 105 m.p.h. 
   (True Ind.)  Glide or dive 131 m.p.h. 
  Seaplane: Level flight or climb    95 m.p.h. 
   Glide or dive 129 m.p.h. 
 
 Propeller limits Static r.p.m. at maximum permissible throttle setting: 
   Not over 2040, not under 1930.  No additional tolerance permitted.  
 
  Diameter:  Not over 72 in., not under 70 in. 
 
 Center of Gravity Landplane: (+14.5) to (+19.7) 
   (C.G.)  range Seaplane: (+15.1) to (+20.1) 
 
 Empty weight C.G. range Landplane: (+15.3) to (+18.5) 
  Seaplane: (+15.9) to (+19.0) 
  When empty weight C.G. falls within the pertinent range, computation of critical  
  fore and aft C.G. positions is unnecessary.  Ranges are not valid for non-standard 
  arrangements. 
 
 Maximum weight Landplane: 1100 lb. (Serial No. 1407 and up eligible at 1150 lb.).  
  Seaplane: 1228 lb. (Serial No. 1432 and up eligible at 1278 lb.). 
 
 Number of seats 2 (+23) 
 
 Maximum baggage 30 lb. (+40) 
 
 Fuel capacity 12 gals. (-9) (See item 312 for auxiliary tank). 
 
 Oil capacity 5 qts. (-34) 
 
Control surface movements Elevators 27° up 25° down 
 Ailerons 25° up 25° down 
 Rudder 26° right 26° left 
 
 Serial Numbers eligible 1001 and up. 
 
 Required equipment Landplane: Items 101, 102, 103, 104, 105 
  Seaplane: Items 103, 104, 105, 151. 
 
IV - Model BF12-65 (Army L-2K),2 PCLM and Model BFS12-65, 2 PCSM, Approved 1 May 1941 
   (Same as BF and BFS except for engine installation). 
 
 Engine Franklin 4AC-176-B2  
  (See Item 308 for optional engines.) 
 
 Fuel 73 min. octane aviation gasoline. 
 
 Engine limits For all operations, 2200 r.p.m. (65 hp.).

A-699  Page 4 
 
 Airspeed limits Landplane: Level flight or climb 105 m.p.h. 
   (True Ind.)  Glide or dive 140 m.p.h. 
  Seaplane: Level flight or climb    95 m.p.h. 
   Glide or dive 129 m.p.h. 
 
 Propeller limits Static r.p.m. at maximum permissible throttle setting: 
  Not over 2040, not under 1930.  No additional tolerance permitted. 
 
  Diameter:  Not over 72 in., not under 70 in. 
 
 Center of Gravity Landplane: (+14.2) to (+20.0) 
   (C.G.)  range Seaplane: (+14.2) to (+20.0) with EDO floats, Item 151. 
   (+14.6) to (+20.0) with Heath floats, Item 319. 
 
 Empty weight C.G. range Landplane: (+14.8) to (+17.3) 
  Seaplane: (+14.8) to (+19.1) with EDO floats, Item 151. 
   (+15.2) to (+19.1) with Heath floats, Item 319. 
 
 Maximum weight Landplane: 1200 lb.  
  Seaplane: 1278 lb. 
 
 Number of seats 2 (+23) 
 
 Maximum baggage Landplane: 50 lb. (+40) 
  Seaplane: 50 lb. (+40) 
 
 Fuel capacity 18 gal. (12 gal. in fuselage at -9 and 6  gal. in wing at +24).   
  (See NOTE 3). 
 
 Oil capacity 5 qt. (-34) 
 
Control surface movements Elevators 27° up 25° down 
 Ailerons 25° up 25° down 
 Rudder 26° right 26° left 
 Elevator trim tab 25° up 30° down 
 
 Serial Numbers eligible 2401, 2501, 2503, 2504, 2529 and up and all Air Force numbers.  
  Use manufacturer's number when available. 
 
 Required equipment Landplane:  Items 101, 102, 103, 104, 105 and 108. 
  Seaplane: Items 103, 104, 105, 108 and 151. 
 
Specification Pertinent to All Models 
 Datum Leading edge of wing. 
 
 Leveling means Upper surface of horizontal stabilizer. 
 
 Certification basis Type Certificate No. 699 (CAR 4a). 
 
 Production basis None.  Prior to original certification, an FAA representative must perform detailed  
  inspection for workmanship, materials and conformity with the approved technical data,  
  and a check of the flight characteristics.

A-699  Page 5 
 
Equipment: A plus (+) or minus ( -) sign preceding the weight of an item of equipment indicates net weight change when that 
item is installed. 
 
  Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer 
except those items preceded by an asterisk (*).  The asterisk denotes that approval has been obtained by other than 
the aircraft manufacturer.  An item marked with an asterisk may not have been manufactured under a CAA 
monitored or approved quality control system, and therefore attention should be paid to workmanship and 
conformity with pertinent data called for in this specification. 
 
Propellers and Propeller Accessories 
 
103. Propeller - wood (fixed or adjustable pitch) 10 lb. (-46) 
 
Engines and Engine Accessories - Fuel and Oil System 
No aircraft of these models shall be eligible for original certification with single ignition engines after  
1 August 1941.  In addition, no aircraft of these models shall be eligible for recertification with single ignition  
engines unless such aircraft were either previously certificated with single ignition engines or were originally  
certificated prior to 1 August 1941. 
 
104. Carburetor air heater (BF-L600) 
108. Enclosed engine cowl (BF12-65) 
109. AC air filter 1529265 (Aircooled Motors Dwg. SK-534-4) 1 lb. (-23) 
 (Models BF-65 and BF12-65 only) 
110. Oil Filter PB-5, weight includes 1 qt. of oil 4 lb. (-20) 
 (a) (BF, BFS, BF-60, BFS-60) Kit No. 500, Fram Installation Dwg. 500 
 (b) (BF-12-65, BFS12-65) Kit No. 501 Fram Installation Dwg. 61564 
308. Engines, Franklin (See Engine Specification No. 194, 206 and 221)  
 A. 4AC-150 Series 50 (for Models BF & BFS) (-34) 
  (a)  Scintilla SF-4L or -4R (Dual ignition) +11 lb. 
  (b)  Wico AP-953 (Dual ignition) +4 lb. 
 B. 4AC-176-BA2 (for Models BF-65 and BF12-65) Neglect weight change 
  Engines limits - for all operations, 2300 r.p.m. (65 hp.) 
  Propeller limits - Static r.p.m. at maximum permissible  
   throttle setting - not over 2250, not under 2140.   
   No additional tolerance permitted. 
  Diameter - not more than 72 in., not less than 70 in. 
 C. 4AC-150 Series A (Engine mount Dwg. BF-A13 or BF-A130) 
  (For Model BF-60, Serial No. 1001 to 1406 incl., only) 
  Fuel - 73 min. oct., Engine limits - For all operations,  
  2400 r.p.m. (60 hp.); Prop. limits under BF-60. 
312. Auxiliary 6 gal. fuselage fuel tank installation 8 lb. (+30) 
 (Fuel arm (+35)) (BF, BFS, BF-60, BFS-60, BF-65 and BFS-65) 
318. Exhaust muffler and carburetor heater installation Neglect weight change 
 (BF12-L68) (This item may replace Item 104) 
 
Landing Gear and Floats 
 
101. 6.00-6 wheels (Firestone 604) with 2-ply tires 21 lb.  (+2) 
102. Tail skid 
107. Parking brake (BF12-65) 1 lb.  (-9) 
151. EDO 60-1320 float installation 169 lb. +115 lb. (+22) 
 (including auxiliary fin 4 lb. (+176) 
 As an alternate method of installing Item 151, Taylorcraft  
 clamp-on fuselage fittings, Part Numbers 2554, 2555, and 2556  
 may be used.

A-699  Page 6 
 
302. Tail wheel assembly 
 (a) 6x2.00 steerable with brake (Baxter) +5 lb.      
 (b) 6x2.00 steerable (Aircraft Associates) +3 lb.      
 (c) 6x2.00 full swiveling (Firestone Industrial) +3 lb.      
 (d) 6x2.00 steerable (Lake State Products 5-40-31) +4 lb.      
 (e) 6x2.00 steerable (Heath) +4 lb.      
 (f) Steerable (Decker D-501) 6 lb.      
304. 6.00-6 wheel (Firestone 6C4HB) with brakes +6 lb. (+1) 
305. Wheel streamlines (Dwg. A-9015 or A9016) 6 lb. (+2) 
309. Parking brake (BF and BF-60) 1 lb. (-9) 
*314. Skis (Eligible on any airplane of these models provided  Use actual weight change 
 the propeller installation meets the minimum 9 in. ground  
 clearance.  The maximum weight for the skiplane will be the  
 same as for the corresponding landplane or that shown in  
 parenthesis after each ski model, whichever is less.) 
 (a) Marston 1200 (Maximum 1200 lb.) 
 (b) Air Transport 1220-480 (Maximum 1220 lb.) 
 (c) Air Transport 1224-580-1 (Maximum 1220 lb.) 
 (d) Federal SC-1 (Maximum 1400 lb.)  
 (e) Piper S-1000 (Maximum 1200 lb.)  
 (f) Jennings TY-2 (Maximum 1200 lb.) 
 (g) Federal SA-1 (Maximum 1200 lb.) 
 (h) Aviation Service B (Maximum 1650 lb.) 
 (i) Richards 1-B (Maximum 2220 lb.) 
 (j) Washington Aircraft 1200 (Maximum 1200 lb.) 
 (k) Heath 655  (Maximum 1210 lb.) 
 (l) Federal SC-2 (Maximum 1650 lb.) 
 (m) Aviation Service A (Maximum 1100 lb.) 
 (n) Federal SA-1A (Maximum 1300 lb.) 
 (o) Jacobsen (Formerly Escanaba) EAS-100 (Maximum 1200 lb.) 
 (p) Richards 1-A (Maximum 2800 lb.) 
 (q) Marston MFS-1600 (Maximum 1600 lb.) 
 (r) Heath 725  (Maximum 1450 lb.) 
 (s) Aero, Sales & Service AS-6.00-6 (Maximum 1320 lb.) 
 (t) Jack Carr Service 16 (Maximum 1600 lb.) 
 (u) Fairbanks MF-5  (Maximum 1310 lb.) 
 (v) Heath 725 A (Maximum 1450 lb.) 
 (w) Federal SKT-1 (Maximum 1400 lb.) 
 (x) Call S2 (Maximum 1800 lb.) 
 (y) Federal A-1500 (Maximum 1500 lb.), Federal Instal. Dwg. 11R232 
 (z) Federal A-1500A (Maximum 1500 lb.), Federal Instal. Dwg. 11R232 
 (aa) Federal A-1850 (Maximum 1850 lb.), Federal Instal. Dwg. 11R232 
 (ab) Federal A-2000 (Maximum 1500 lb.), Federal Instal. Dwg. 11R232 
 (ac) Federal A-2000A (Maximum 2000 lb.), Federal Instal. Dwg. 11R232 
 (ad) Federal CA-1850-6 (Maximum 2000 lb.), Federal Instal. Dwg. 11R232 
 (ae) Wesco A-15, Western Aircraft Equipment Co. Dwgs. 148, 202, 203. 
 (af) Wesco A-20, Western Aircraft Equipment Co. Dwgs. 148, 202, 203. 
315. 6.00-6 4-ply tires  Neglect weight change 
319. Heath 1460A float installation, 172 lb., incl. aux. fin, +122 lb. (+25) 
 4 lb. (+176) (BFS12-65 only) 
*320. Consolidair Model 16 Wheel Fenders (per airplane) 10 lb.  (+2) 
 Consolidair installation Dwg. 0029

A-699  Page 7 
 
Electrical and Radio Equipment 
310. Battery and box  9 lb. (+10) 
311. Radio installations 
 (a) Receiver (BF, BFS, BF-60 and BFS-60) 9 lb. (+39) 
 (b) Receiver (BF12-65 and BFS12-65)  11 lb. (+12) 
 (c) Transmitter (BF12-65 and BFS12-65) 9 lb.  (+8) 
 (d) Reel type trailing antenna (BF12-65 and BFS12-65) 3 lb. (+61) 
 (e) "T" type antenna 1 lb. (+40) 
 (f) Lear Loop Rotator AML-1 (BF12-65 and BFS12-65) 2 lb. (+25) 
 (g) Lear receiver complete, including receiver AMR-1 5 lb. 
  (+2), dry battery and cable 6 lb. (+20), antenna 1 lb. 
  (+40) (B12 series only) 12 lb. (+14) 
 (h) Lear receiver and transmitter complete, including receiver 
  AMR-1 5 lb. (+2), receiver antenna 1 lb. (+40), transmitter 
  AMT-1 5 lb. (+2), trailing antenna 3 lb. (+61), dry battery  23 lb. (+18) 
  and cable 9 lb. (+20) (B12 series only) 
 (i) Heath receiver complete, including receiver MA-4 7 lb. 
  (+2), dry battery and cable 6 lb. (+20), antenna 1 lb. 
  (+40) (B12 series only) 14 lb. (+13) 
317. Position lights (Grimes B) 2 lb. (+77) 
 
Interior Equipment 
105. Wheel type control 
306. Cabin heater (Taylorcraft Dwg. BF-L607) 2 lb. (-22) 
313. Stick type control  Neglect weight change 
 
Miscellaneous (not listed above) 
106. Auxiliary door (BF12-65) 
303. Auxiliary door (BF, BFS, BF-60, BFS-60) +5 lb. (+17) 
316. Special instruments (B12 series only) 
 (a) Bank and turn 4 lb.   (0) 
 (b) Rate of climb 2 lb. (-4) or (-9) 
 (c) Compass  2 lb.  (+4) 
 
 
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 operators having an approved weight control  
 system). 
 
NOTE 2. Reserved. 
 
NOTE 3. Refill main tank in level flight and only when main tank is less than 1/2 full. 
 
 
 
 
 
...END...
```

## ADs (5, in force first)

- [AD 2008-09-18](https://openairdocs.org/ad/2008-09-18): Wing strut attach fittings · Taylorcraft A, BF, BF-60 and 34 more. Effective Jun 6, 2008
- [AD 2008-04-09](https://openairdocs.org/ad/2008-04-09): Left and right wing front and aft lift struts · Taylorcraft 2000 19, BC, BC-65 and 35 more. Effective Mar 28, 2008
- [AD 47-16-03](https://openairdocs.org/ad/47-16-03): Wing Strut Fittings · Taylorcraft 2000 BC, BC-65, BC12-65 and 25 more
- [AD 50-41-01](https://openairdocs.org/ad/50-41-01): Elevator Horn Bolt · Taylorcraft 2000 BC, BC-65, BC12-65 and 25 more
- [AD 51-09-03](https://openairdocs.org/ad/51-09-03): Fuel Shutoff Valve Clip · Taylorcraft A, Army TG-6 Conversions, BF and 37 more

## Registered aircraft by registry model (OpenAirDocs)

- [Taylorcraft BF12-65](https://openairdocs.org/model/taylorcraft-bf12-65): 14 aircraft (registry code 8850340)
- [Taylorcraft BF](https://openairdocs.org/model/taylorcraft-bf): 9 aircraft (registry code 8850326)
- [Taylorcraft BF-65](https://openairdocs.org/model/taylorcraft-bf-65): 9 aircraft (registry code 8850336)
- [Taylorcraft BF-60](https://openairdocs.org/model/taylorcraft-bf-60): 1 aircraft (registry code 8850332)
- [Taylorcraft BFS](https://openairdocs.org/model/taylorcraft-bfs): 0 aircraft (registry code 8850330)
- [Taylorcraft BFS-60](https://openairdocs.org/model/taylorcraft-bfs-60): 0 aircraft (registry code 8850334)
- [Taylorcraft BFS-65](https://openairdocs.org/model/taylorcraft-bfs-65): 0 aircraft (registry code 8850338)
- [Taylorcraft BFS12-65](https://openairdocs.org/model/taylorcraft-bfs12-65): 0 aircraft (registry code 8850344)

## STCs approved under this data sheet (45)

- [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of  existing instrument panel lights dimmer control.. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, 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 SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector.. Alcor LLC
- [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 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 SA2057SO](https://openairdocs.org/stc/SA2057SO): Installation of shoulder harness.. Alpha Aviation Inc
- [STC SA00433NY](https://openairdocs.org/stc/SA00433NY): Installation of Airwolf remote mounted engine oil filter model AFC-500 or AFC-600 on multi engine fixed wing light aircraft incorporating Franklin reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc.
- [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 SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc.
- [STC SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc.
- [STC SA02402SE PAGE 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): 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 SA02825NY PAGE 2](https://openairdocs.org/stc/SA02825NY%20PAGE%202): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc.
- [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc.
- [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated
- [STC SA01227SE](https://openairdocs.org/stc/SA01227SE): Farication of Vortex Generator Kit.. Micro AeroDynamics Inc
- [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 SA02300AK](https://openairdocs.org/stc/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.. Northern Airframes LLC
- [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International
- [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc
- [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP.. M-20 Oil Separators LLC
- [STC SA666NW](https://openairdocs.org/stc/SA666NW): Installation of Teflon control yoke bail or control yoke bushings.. Johnson George O
- [STC SA00140LA](https://openairdocs.org/stc/SA00140LA): Installation of a replacement S & S Propeller model W7448A1-2.. S & S Propellers Inc
- [STC SA1626NM PAGE 2](https://openairdocs.org/stc/SA1626NM%20PAGE%202): Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series). Electronics International
- [STC SA2350NM PAGE 2](https://openairdocs.org/stc/SA2350NM%20PAGE%202): Installation of Electronics International Inc digital carburetor/outside air temperature gauges. Electronics International
- [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International
- [STC SA3862NM PAGE 2](https://openairdocs.org/stc/SA3862NM%20PAGE%202): Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories.. Electronics International
- [STC SA2190NM PAGE 2](https://openairdocs.org/stc/SA2190NM%20PAGE%202): Installation of electronics International Digital Volt/Amp Gauges and Accessories.. Electronics International
- [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 SA308EA](https://openairdocs.org/stc/SA308EA): 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.). Alfred R Puccinelli
- [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co
- [STC SA4-1438](https://openairdocs.org/stc/SA4-1438): Eronite covering of fuselage.. Lott William C
- [STC SA4-906](https://openairdocs.org/stc/SA4-906): Ceconite 101 covering of complete airframe.. Cooper Engineering Corporation
- [STC SA4-1346](https://openairdocs.org/stc/SA4-1346): Fiberglas covering of airplane surfaces.. Quentin Laywell
- [STC SA2350NM](https://openairdocs.org/stc/SA2350NM) (historical): Installation of Electronics International Inc digital carburetor/outside air temperature gauges listed on the attached continuation sheet and the associated accessories.. Electronics International

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