# TCDS A-696: Taylorcraft 2000 LLC

- Type: Type certificate data sheet
- Status: Current
- Holder: Taylorcraft 2000 LLC
- Revision: 26
- Revised: March 22, 2022
- Product: Aircraft, Small Airplane
- Certification basis: CAR 4
- Registered aircraft: 1,370, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/bf/4a/bf4a3f697c039356cb8fd87e87c6ee7c9032d4785c17f1b7d89715b14b4c2f97
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/863C2CB5CC20742A862588160050E016.0001
- Page: https://openairdocs.org/tcds/A-696

## Models (14)

As the data sheet lists them.

- BCS
- BC-65
- BC12-D
- BC12-65 ((Army L-2H))
- BCS12-D
- BC
- BCS-65
- BCS12D-4-85
- BC12D-4-85
- BCS12D-85
- BCS12-65
- BC12D-85
- BCS12-D1
- BC12-D1

## 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 8 9 10 11 12 
Rev. No. 25 16 16 16 16 16 16 16 16 16 16 16 
Rev 25 changed TC holder. 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A-696 
Revision 26 
Taylorcraft 2000, LLC 
BC  BCS12-D 
BCS BC12-D1 
BC-65 BCS12-D1 
BCS-65 BC12D-85 
BC12-65 (Army L-2H) BCS12D-85 
BCS12-65 BC12D-4-85 
BC12-D BCS12D-4-85 
March 22, 2022 
 
AIRCRAFT SPECIFICATION NO. A-696 
 
Type Certificate Holder Taylorcraft 2000, LLC 
 Dba Aircraft Taylorcraft Co., LLC 
 815 N Minnesota Avenue 
                                                               Brownsville, TX  78521 
 
Type Certificate Ownership Record Taylorcraft Corporation transferred ownership to Syncron, Inc. on October 19, 1994.  
  Syncrom, Inc. transferred ownership to Airborne Marketing, Inc. on January 8, 1997. 
  Airborne Marketing, Inc. transferred ownership to Lee F. Booth on April 26, 1999. 
Lee F. Booth, dba Taylorcraft Aerospace, transferred ownership to Harvey & Vera 
Patrick Foundation, Inc. on May 10, 2000. 
Harvey & Vera Patrick Foundation, Inc. transferred ownership to Taylorcraft 2000, LLC 
on August 8, 2000 
Taylorcraft 2000 LLC transferred ownership to Taylorcraft Aviation LLC on  
March 5, 2003 
Taylorcraft Aviation LLC, 2124 N. Central Ave., Brownsville, TX 78521 transferred 
ownership to Taylorcraft 2000 LLC on May 21, 2008  
Taylorcraft 2000 LLC transferred to Taylorcraft 2000 LLC Dba Aircraft Taylorcraft Co., 
LLC on October 7, 2009. 
 
I - Model BC, 2 PCLM, Approved August 24, 1938; Model BCS, 2 PCSM, Approved April 5, 1939 
 Engine Continental A-50-1 (see item 114(a) for optional engines) 
 
 Fuel 73 min. grade aviation gasoline 
 
 Engine Limits For all operations, 1900 r.p.m. (50 hp.) 
 Propeller Limits Diameter:  Maximum 83 in. 
 
 Airspeed Limits Landplane: Level flight or climb 105 m.p.h. (91 knots) 
  (True Indicated)  Glide or dive 131 m.p.h. (114 knots) 
  Seaplane: Level flight or climb   95 m.p.h. (83 knots) 
   Glide or dive 129 m.p.h. (112 knots) 
 
 Center of Gravity Landplane: (+14.5) to (+19.7) 
 (C.G.) Range Seaplane: (+15.1) to (+19.4) 
 
 Empty Weight C.G. Range Landplane: (+15.3) to (+18.5) 
  Seaplane: (+15.9) to (+18.3) 
  When empty weight C.G. falls within 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. (S/N 1407 and up are eligible at 1150 lb.)  
  Seaplane: 1228 lb. 
 
 Number of Seats 2 (+23)

A-696, Rev 25 Page 2 of 12 
 Maximum Baggage 30 lb. (+40) 
 Fuel Capacity 12 gal. (-9).  See item 115 for auxiliary tank. 
 Oil Capacity 4 qt. (-21) 
 
 Control Surface Movements Elevators Up 25o Down 27o 
  Rudders Right 26o Left 26o 
  Ailerons (Not available) 
 
 Serial No. Eligible 1001 and up 
 
 Required Equipment Landplane: 1 or 4, 104, 202, 203, 210(a), 401  
  Seaplane: 1 or 4, 104, 205, 401 
 
II - Model BC-65, 2 PCLM, Approved July 22, 1939; Model BCS-65, 2 PCSM, Approved October 7, 1939 
 (Same as Model BC except engine installation) 
 
 Engine Continental A-65-1 (see item 114(b) for optional engines) 
 
 Fuel 73 min. grade aviation gasoline 
 
 Engine Limits For all operations, 2350 r.p.m. (65) hp.) 
 
 Propeller Limits Static r.p.m. at full throttle: 
  A-65-1 engine, not over 2300, not under 2070 
  Optional engines, not over 2250, not under 2070  
  No additional tolerance permitted. 
  Diameter: (landplane) not over 83 in., not under 70 in.  
   (seaplane)   not over 79 in., not under 70 in.  
 
 Airspeed Limits Landplane:  Level flight or climb   105 m.p.h. (91 knots) 
  (True Indicated)  Glide or dive  131 m.p.h. (114 knots) 
   Seaplane: Level flight or climb    95 m.p.h. (83 knots) 
    Glide or dive  129 m.p.h. (112 knots) 
 
 Center of Gravity (C.G.) Range Landplane: (+14.5) to (+19.7) 
   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. (S/N 1407 and up are eligible at 1150 lb.)  
   Seaplane: 1228 lb. (S/N 1432 and up are eligible at 1278 lb.)  
 
 Number of Seats 2 (+23) 
 
 Maximum Baggage 30 lb. (+40) 
 
 Fuel Capacity 12 gal. (-9).  (See item 115 for auxiliary tank). 
 
 Oil Capacity 4 qt. (-21) 
 
 Control Surface Movements Elevators Up 27o Down 25o 
  Rudders Right 26o Left 26o 
  Ailerons (Not available) 
 
 Serial No. Eligible 1001 and up 
 
 Required Equipment Landplane: Items 1, 2, 3, 4, or *8; 104, 202, 203, 210(a), 401  
   Seaplane: Items 1, 3, 4 or *8; 104, 205, 401

Page 3 of 12 A-696, Rev 25 
III - Model BC12-65 (Army L-2H), 2 PCL-SM, Approved April 7, 1941; Model BCS12-65, 2 PCL-SM, 
 Approved April 7, 1941 
 (Same as Model BC-65 except for minor structural changes and added elevator trim tab). 
 
 Engine Continental A-65-7 (see item 114(c) for optional engines) 
 
 Fuel 73 min. grade aviation gasoline 
 
 Engine Limits For all operations, 2300 r.p.m. (65 hp.) 
 
 Propeller Limits Static r.p.m. at full throttle:  not over 2250, not under 2070.  
   No additional tolerance permitted. 
   Diameter:  not over 72 in., not under 70 in. 
 
 Airspeed Limits Landplane: Level flight or climb 105 m.p.h. 
  (True Indicated)  Glide or dive 140 m.p.h. 
   Seaplane: Level flight or climb   95 m.p.h. 
    Glide or dive 129 m.p.h. 
 
 Center of Gravity (C.G.) Range Landplane: (+14.2) to (+20.0) 
   Seaplane: (+14.2) to (+20.0) with Edo floats (item 205) 
    (+14.6) to (+20.0) with Heath floats (item 211) 
 
 Empty Weight C.G. Range Landplane: (+14.8) to (+17.9) 
   Seaplane: (+14.8) to (+18.3) with Edo floats (item 205) 
    (+15.2) to (+18.3) with Heath floats (item 211) 
 
 Maximum Weight Landplane: 1200 lb. 
   Seaplane: 1278 lb. 
 
 Number of Seats 2 (+23) 
 
 Maximum Baggage Landplane: 50 lb. (+40): 
   Seaplane: 30 lb. (+40) 
 
 Fuel Capacity 18 gal. (12 gal. in fuselage (-9) and 6 gal. in wing (+24)).  See NOTE 3. 
 
 Oil Capacity 4 qt. (-21) 
 
 Control Surface Movements Elevators Up 27o Down 25o 
  Elevator tab Up 25° Down 30° 
  Ailerons  Up 25° Down 25° 
  Rudders Right 26o Left 26o 
 
 Serial No. Eligible 2401, 2501, 2503, 2504, 2529 and up and all USAF numbers.  Use manufacturer’s 
numbers if available. 
 
 Required Equipment Landplane: 1, 2, 4, 5, or *8; 104, 108, 202, 203, 210(a), 401  
   Seaplane: 1 or 4, 104, 108; 205, 401

A-696, Rev 25 Page 4 of 12 
IV - Model BC12-D, 2 PCLM, Approved November 23, 1945; Model BCS-12D, 2 PCSM, Approved February 19, 1946 
 (Same as Model BC12-65 except for alternate tail surface, revised aileron travel, alternate one piece windshield and other 
miscellaneous structural and non-structural changes).  (Model BC12-D1 eligible as Model BC12-D when items 601 and 204 
and 6 gal. right-hand wing tank are installed). 
 
 Engine Continental A-65-8 (see item 114(d) for optional engines) 
 
 Fuel 73 min. grade aviation gasoline 
 
 Engine Limits For all operations, 2300 r.p.m. (65 hp.) 
 
 Propeller Limits Static r.p.m. at full throttle:  not over 2250, not under 2070.  
   No additional tolerance permitted. 
   Diameter:  not over 72 in., not under 70 in. 
 
 Airspeed Limits Landplane: Level flight or climb 105 m.p.h. 
  (True Indicated)  Glide or dive 140 m.p.h. 
  Seaplane: Level flight or climb   95 m.p.h. 
   Glide or dive 129 m.p.h. 
 
 Center of Gravity (C.G. Range) Landplane: (+14.2) to (+20.0) 
  Seaplane: (+14.2) to (+20.0) with Edo floats (item 205) 
   (+14.6) to (+20.0) with Heath floats (item 211) 
 
 Empty Weight C.G. Range Landplane: (+14.8) to (+17.9) 
  Seaplane: (+14.8) to (+18.3) with Edo floats (item 205) 
   (+15.2) to (+18.3) with Heath floats (item 211) 
  When empty weight C.G. falls within pertinent range, computation of critical fore and aft 
C.G. positions is unnecessary.  Ranges are not valid for non-standard arrangements. 
 
 Maximum Weight Landplane: 1200 lb. 
  Seaplane: 1278 lb. 
 
 Number of Seats 2 (+23) 
 
 Maximum Baggage Landplane: 50 lb. (+40) 
  Seaplane: 30 lb. (+40) 
 
 Fuel Capacity 18 gal. (12 gal. fuselage tank at (-9) and 6 gal. wing tank at (+24).  See NOTE 3. 
 
 Oil Capacity 4 qt. (-21) 
 
 Control Surface Movements Elevators Up 27o Down 25o 
  Elevator tab Up 25° Down 30° 
  Ailerons Up 23° Down 23° 
  Rudders Right 26o Left 26o 
 
 Serial No. Eligible 6402 and up 
 
 Required Equipment Landplane: 1, 2, 3, 4, or *8; 104, 108, 202, 203, 210(a), 401  
  Seaplane: 1, 3, 4 or *8; 104, 108, 205, 401

Page 5 of 12 A-696, Rev 25 
V - Model BC12-D1, 2 PCLM-SM, Approved September 10, 1946; Model BCS12-D1, 2 PCL-SM, 
 Approved September 10, 1946 
 (Same as Model BC12-D except for elimination of left hand door (item 601), parking brake (item 204) and 6 gal. R/H wing 
tank)  (Model BC12-D1 eligible as BC12-D when items 601 and 204 and 6 gal. right-hand wing tank are installed) 
 
 Engine Continental A-65-8 (See item 114(d) for optional engines) 
 
 Fuel 73 min. grade aviation gasoline 
 
 Engine Limits For all operations, 2300 r.p.m. (65 hp.) 
 
 Propeller Limits Static r.p.m. at full throttle; not over 2250, not under 2070.  No additional tolerance 
permitted.   
  Diameter:  not over 72 in., not under 70 in. 
  
 Airspeed Limits Landplane: Level flight or climb 105 m.p.h. 
  (True Indicated)  Glide or dive 140 m.p.h. 
  Seaplane: Level flight or climb   95 m.p.h. 
   Glide or dive 129 m.p.h. 
 
 Center of Gravity (C.G.) Range Landplane: (+14.2) to (+20.0) 
  Seaplane: (+14.2) to (+20.0) with Edo floats (item 205) 
   (+14.6) to (+20.0) with Heath floats (item 311) 
 
 Empty Weight C.G. Range Landplane: (+14.8) to (+17.9) 
  Seaplane: (+14.8) to (+18.3) with Edo floats (item 205) 
   (+15.2) to (+18.3) with Heath floats (item 311) 
  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: 1200 lb. 
  Seaplane: 1278 lb. 
 
 Number of Seat 2 (+23) 
 
 Maximum Baggage Landplane: 50 lb. (+40) 
  Seaplane: 30 lb. (+40) 
 
 Fuel Capacity 12 gal. (-9) 
 
 Oil Capacity 4 qt. (-21) 
 
 Control Surface Movements Elevators Up 27o Down 25o 
  Elevator tab Up 25° Down 30° 
  Ailerons Up 23° Down 23° 
  Rudders Right 26o Left 26o 
 
 Serial No. Eligible 6402 and up 
 
 Required Equipment Landplane: 1, 2, 3, 4 or *8; 104, 108, 202, 203, 210(a), 401  
  Seaplane: 1, 3, 4 or *8; 104, 108, 205, 401

A-696, Rev 25 Page 6 of 12 
VI - Model BC12D-85, 2 PCL-SM, Approved September 30, 1948; Model BCS12D-85, PCL-SM, Approved September 30, 1948 
 (Same as Model BC12-D except for increased power and gross weight, fuel system changes, auxiliary wing fuel tank, 
 revised wing fittings and minor structural changes) 
 
 Engines Continental C85-8F 
 
 Fuel 80 min. grade aviation gasoline 
 
 Engine Limits For all operations, 2575 r.p.m. (85 hp.) 
 
 Propeller Limits Static r.p.m. at maximum permissible throttle setting (no additional tolerance permitted): 
  Landplane: not over 2350, not under 2100 
  Seaplane: not over 2310, not under 2010  (exception:  not under 2100 with item 205(a))  
  Diameter: Landplane:  not over 72 in., not under 68 in. 
   Seaplane:    not over 72 in., not under 70 in.  
 
 Airspeed Limits Landplane: Level flight or climb 105 m.p.h. (91 knots) 
  (True Indicated)  Glide or dive 142 m.p.h. (124 knots) 
  Seaplane: Level flight or climb   95 m.p.h. (83 knots) 
   Glide or dive 128 m.p.h. (111 knots) 
 
 Center of Gravity (C.G. Range) Landplane: (+14.2) to (+20.0) 
  Seaplane: (+15.8) to (+17.6) at 1351 lb. 
   (+13.4) to (+17.6) at 1200 lb. or less 
   Straight line variation between points given 
12 13 14 15 16 17 18
1000
1100
1200
1300
1400
LB.
INCHES
BCS12D-85
FRONT
LIMIT
AFTLIMIT
 
Empty Weight C.G. Range Landplane: (+14.8) to (+17.9) 
  Seaplane: (+13.7) to (+15.1) 
  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: 1280 lb. 
  Seaplane: 1351 lb. 
 
Number of Seats 2 (+23) 
 
Maximum Baggage Landplane: 50 lb. (+40) 
  Seaplane: 30 lb. (+40) 
Fuel Capacity 18 gal. (12 gal. tank in fuselage at (-9) and 6 gal. tank in wing at (+24)).  See NOTE 3 
 
Oil Capacity 4 1/2 qt. (-21) 
 
Control Surface Movements Elevators Up 27o Down 25o 
  Elevator tab Up 25° Down 30° 
  Ailerons Up 23° Down 23° 
  Rudders Right 26o Left 26o 
 
Serial No. Eligible 12001 and up 
 
Required Equipment Landplane: 1, 4, 6, 7 or *9; 104, 108, 202, 206, 210(a), 401 
  Seaplane: 1, 4, 6, 7 or *9; 104, 108, 205, 401

Page 7 of 12 A-696, Rev 25 
VII - Model BC12-D-4-85, 2 PCL-SM, Approved July 13, 1949; Model BCS12D-4-85, 2 PCL-SM, 
 Approved July 13, 1949 
 (Same as Model BC12D-85 except for engine, baggage compartment , side windows and sky-lights) 
 
 Engine Continental C85-12F 
 
 Fuel 80 min. grade aviation gasoline 
 
 Engine Limits For all operations, 2575 r.p.m. (85 hp.) 
 
 Propeller Limits Static r.p.m. at maximum permissible throttle setting (no additional tolerance permitted): 
  Landplane: not over 2350, not under 2100 
  Seaplane: not over 2310, not under 2010 
   (exception: not under 2100 with item 205(a)) 
  Diameter: Landplane - not over 72 in., not under 68 in. 
   Seaplane - not over 72 in., not under 70 in. 
 
 Airspeed Limits Landplane: Level flight or climb 105 m.p.h. (91 knots) 
  (True Indicated)  Glide or dive 142 m.p.h. (124 knots) 
  Seaplane: Level flight or climb   95 m.p.h. (83 knots) 
   Glide or dive 128 m.p.h. (111 knots) 
 
 Center of Gravity (C.G.) Range Landplane: (+14.2) to (+20.0) 
  Seaplane: (+15.8) to (+17.6) at 1351 lb. 
   (+13.4) to (+17.6) at 1200 lb. or less 
   Straight line variation between points given.  (See Figure under Section VI) 
 
 Empty Weight C.G. Range Landplane: (+14.9) to (+16.3) 
  Seaplane: (+13.8) to (+14.3) 
  When empty weight C.G. falls within the pertinent range, computation of critical fore and 
aft C.G. positions is unnecessary.  Ranges not valid for non-standard arrangements. 
 
 Maximum Weight Landplane: 1280 lb. 
  Seaplane: 1351 lb. 
 
 Number of Seats 2 (+23) 
 
 Maximum Baggage Landplane: 50 lb. (+70) 
  Seaplane: 30 lb. (+70) 
 
 Fuel Capacity 18 gal. (12 gal. tank in fuselage at (-9) and 6 gal. tank in wing at (+24)).  See NOTE 3. 
 
 Oil Capacity 4 1/2 qt.  (-30) 
 
 Control Surface Movements Elevators Up 27o Down 25o 
  Elevator tab Up 25° Down 30° 
  Ailerons Up 23° Down 23° 
  Rudders Right 26o Left 26o 
 
 Serial No. Eligible 4-13010 and up 
 
 Required Equipment Landplane: 1, 4, 6, 7 or *9; 104, 108, 202, 206, 210(a), 401  
  Seaplane: 1, 4, 6, 7 or *9; 104, 108, 205, 401

A-696, Rev 25 Page 8 of 12 
Specifications Pertinent to all Models 
 
 Datum Leading edge of wing 
 
 Leveling Means Upper surface of horizontal stabilizer 
 
 Certification Basis Part 04 of the Civil Air Regulations effective as amended to May 1, 1938.  Type 
Certificate No. 696 issued. 
 
 Production Basis None.  Prior to original certification, 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 Advisory Circular 21-2, 
except as follows: 
  Canada - Landplane and seaplane eligible with the exception of Model BC12-D1.  
Model BC12-D1 eligible provided auxiliary door (item 601) is installed. 
   - Skiplane not eligible; however, structure complies with Canadian 
requirements as follows: 
  (1) At 1100 lb. maximum weight - landing gear per dwg.  B-A50, ski 
height 10 in., tread 72 in. (centerline of ski 5.19 in. out f rom center of 
bolt attaching diagonal streamlined member to axle). 
   (2) At 1150 and 1200 lb. maximum weight - landing gear per dwg. B-
A515, ski height 9 in., tread 72 in. (centerline of ski 5.19 in. out from 
center of bolt attaching diagonal streamline member to axle). 
 
 Equipment A plus (+) or minus (-) sign preceding the weight of an item indicated 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 (*).  This symbol denotes that approval has 
been obtained by someone other than the aircraft manufacturer.  An item so marked may not have been 
manufactured under an FAA monitored or approved quality control system, and therefore conformity must be 
determined if the item is not identified by a Form FAA-186.  PMA or other evidence of FAA production 
approval. 
 
 Special Note So that all items of equipment might be in their proper categories, the following items were renumbered as 
indicated: 
 
1/ Item 1 was formerly item 103(a) 15/ Item 203 was formerly item 102 
2/ Item 2 was formerly item 103(b) 16/ Item 204 was formerly item 107 
3/ Item 3 was formerly item 103(c) 17/ Item 205 was formerly item 151 
4/ Item 4 was formerly item 103(d) 18/ Item 206 was formerly item 302 
5/ Item 5 was formerly item 103(e) 19/ Item 207 was formerly item 304 
6/ Item  6 was formerly item 103(f) 20/ Item 208 was formerly item 305 
7/ Item 7 was formerly item 103(g) 21/ Item *209 was formerly item *316 
8/ Item *8 was formerly item 103*(h) 22/ Item 210 was formerly item 317 
9/ Item *9 was formerly item 108*(i) 23/ Item *211 was formerly item *320 
10/ Item 114 was formerly item 308 24/ Item *212 was formerly item *321 
11/ Item 115 was formerly item 312 25/ Item 401 was formerly item 105 
12/ Item 116 was formerly item 313 26/ Item 402 was formerly item 306 
13/ Item 117 was formerly item 315 27/ Item 403 was formerly item 314 
14/ Item 202 was formerly item 101 28/ Item 601 was formerly item 106

Page 9 of 12 A-696, Rev 25 
Propellers and Propeller Accessories 
 
1/ 1. Approved wood (fixed or adjustable pitch).  (See Static limits under 
individual models and item 205(a) for minimum static r.p.m. limits for 
Models (BCS12D-85 and BCS12D-4-85) 
 
All Except  
BC12D-4-85 & 
BCS12D-4-85 
10 lb. (-46) 
 
BC12D-4-85  
&  
BCS12D-4-85  
10 lb. (-50) 
2/ 2. Beech R003 controllable, hub R-002-101 or R-003-100, blades R-002-
205-72.  Diameter 72 in.  Pitch at 27 in. sta.:  low 11-3/4° high 17 3/4°.  
(Pitch limits under individual models are not applicable to these 
propellers).  Includes Beech mechanical propeller control. 
 
BC-65, BC12-65, 
BC12-D & BC12-D1 
+20 lb. (-47) 
 
3/ 3. McCauley 1A90 with the following limits: 
Static r.p.m. at maximum permissible throttle setting: 
Landplane: not over 2210, not under 1960 
Seaplane:   not over 2210, not under 2070  
No additional tolerance permitted. 
Diameter:  not over 74 in., not under 72.5 inc 
 
BC-65, BCS-65,  
BC12-D, BCS12-D,  
BC12-D1, BCS12-D1   
+21 lb. (-46) 
 
4/ 4. Hartzell ground adjustable, hub HA-12U, blades 7414 to 6814 or 
7214M to 6814M.  Eligible at diameter and static r.p.m. limits shown 
above for fixed pitched wood models. 
 
All Except BC12D-4-
85 & BCS12D-4-85  
18 lb. (-46) 
BC12D-4-85 &  
BCS12D-4-85 
18 lb. (-50) 
5/ 5. McCauley 1A90 with the following limits:  Static r.p.m. at maximum 
permissible throttle setting:  not over 2250, not under 2070.   
No additional tolerance permitted.   
Diameter:  not over 74 in., not under 72.5 in. 
 
BC12-65   
21 lb. (-46) 
 
6/ 6. Lewis L11CK-45 or any other fixed pitch wood propeller eligible for 
the engine power and speed and meeting static r.p.m. and diameter 
limits noted for the various models eligible. 
 
BC12D-85 & 
BCS12D-85  
+10 lb. (-46) 
BC12D-4-85 & 
BCS12D-4-85 
+10 lb. (-50) 
7/ 7. McCauley 1A90 with the following limits:  Static r.p.m. at maximum 
permissible throttle setting:  not over 2350, not under 2170.   
No additional tolerance permitted.   
Diameter:  not over 71 in., not under 69.5 in. 
 
BC12D-85 &  
BCS12D-85  
+21 lb. (-46) 
BC12D-4-85 & 
BCS12D-4-85 
+21 lb. (-50) 
8/ *8. Sensenich M74CK, fixed pitch metal.   
Static r.p.m. at maximum permissible throttle setting: 
Landplane:  not over 2210, not under 1960  
Seaplane:    not over 2210, not under 2070  
No additional tolerance permitted. 
Diameter:  not over 74 in., not under 72.5 in. 
 
BC-65, BC12-D, 
BC12-D1,  
BC12-65  
21 lb. (-46) 
BCS-65, 
BCS12-D, 
BCS12-D1   
21 lb. (-50) 
9/ *9. Sensenich M74CK-2 fixed pitch metal.  Static r.p.m. at maximum 
permissible throttle setting:  not over 2350, not under 2170.   
No additional tolerance permitted.   
Diameter:  not over 72 in., not under 70 in. 
BC12D-85,  
BCS12D-85   
21 lb. (-46) 
BC12D-4-85, 
BCS12D-4-85, 
21 lb. (-50) 
 
Engines and Engine Accessories 
 No aircraft of these models shall be eligible for original certification with single ignition engines after August 1, 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 August 1, 1941. 
 
 104. Carburetor air heater (dwg. BC-L601)  
 108. Enclosed engine cowl (all except BC, BCS, BC-65, BCS-65)  
 109. McDowell starter  installation (BC-12D, BC12D-85)  (BC-A6014 nose cowl must be 
installed) 
   11 lb. (-34) 
 110. McDowell starter installation using horizontal operating handle (BC12-D, BCS12-D)    13 lb. (-34) 
 111. Exhaust muffler, Ryan Aero. Co. dwg. 52112 (with items 114(b)(1) and (2) only)      2 lb. (-40)

A-696, Rev 25 Page 10 of 12 
 
 112. Oil filter, Fram PB-5, Kit No. 510.  Weight includes 1 qt. oil 
(a) Fram Installation dwg. No. 61544 (BC, BCS, BC12-65, BCS12-65) 
(b) Fram Installation dwg. No. 61524 (BC12-D, BCS12-D, BC12-D1, BCS12-D1) 
     4 lb. (-20) 
 113. Starter (Delco-Remy 1109656) (BC12D-4-85 only)   16 lb. (-24) 
10/ 114. Engines (Continental, see Engine Specs. No. 190 and 205) 
(a) Models BC, BCS 
 (1) A-50-2 
 (2) A-50-3 or A-50-8 
 (3) A-50-4 
 (4) A-50-5 
 (5) A-50-7 
(b) Models BC-65, BCS-65 
 (1) A-65-3, A-65-3J, A-65-8 or A-65-8J 
  Engine limits:  For all operations, 2300 r.p.m.  (65 hp.) 
 (2) A-65-7 or A-65-7J 
  Engine limits same as (b)(1) 
(c) Models BC12-65 
 (1) A-65-7J, A-65-8, A-65-8F, A-65-8J 
  Engine limits same as (b)(1) 
(d) Models BC12-D, BCS12-D, BC12-D1, BCS12-D1 
 (1) A-65-8F, A-65-8J 
  Engine limits same as (b)(1) 
            (-33) 
 
+  6 lb. 
+10 lb. 
+  3 lb. 
+13 lb. 
No weight change 
 
+10 lb. 
 
No weight change 
 
 
No weight change 
 
 
No weight change 
 
 115. Auxiliary 6 gal. fuselage fuel tank installation (fuel arm +35) 
(BC, BCS, BC-65, BCS-65) 
8 lb. (+30) 
 116. Enclosed type engine cowl (dwg. BL-L628) (BC, BCS, BC-65, BCS-65) 9 lb. (-18) 
 117. Revised engine mount (dwg. BC65-A128) (for engines incorporating integral rubber 
bushings) 
Negligible weight 
 
Landing Gear and Floats 
 201. Two main wheel-brake assemblies, 6.00-6, Type III 
(a) Cleveland Aircraft Products Co. Model 6.00 DHB  
      Wheel assembly No. C-38500HMA   
      Brake assembly No. C-7000 
 
  +4 lb. (+2) 
14/ 202. Two main wheels, 6.00-6, Type III, Firestone 604     9 lb. (+2) 
15/ 203. Tail skid  
16/ 204. Parking brake     1 lb. (-9) 
17/ 205. Edo float installation 
(a) Model 60-1320 floats 
 Auxiliary fin (required on all models except BCS12D-85 and BCS12D-4-85 unless the 
seaplane aft C.G. limit for maximum weight is reduced to +18.9).  (When propeller 
item 1 or 6 is installed on Models BCS12D-85 or BCS12D-4-85 the minimum static 
r.p.m. limit is increased to not under 2100 r.p.m.) 
 As an alternate method of installing these floats, Taylorcraft clamp-on fuselage 
fittings, P/N 2554, 2555 and 2556 may be used. 
(b) Model 92-1400 floats 
 Auxiliary fin (required on all model except BCS12D-85 and BCS12D-4-85) 
 
165 lb. (+20)   
    4 lb. (+176) 
 
 
 
 
 
181 lb. (+19)  
    4 lb. (+176) 
18/ 206. Tail wheel assemblies 
(a) 6 x 2.00 steerable with brake (Baxter) 
(b) 6 x 2.00 steerable (Aircraft Associates) 
(c) 6 x 2.00 full swiveling (Firestone Industrial) 
(d) 6 x 2.00 steerable (Lake State Products 5-40-31) 
(e) 6 x 2.00 steerable (Heath) 
(f) Maule SFS-12, SS-12, SAFS-1-2-P8 
(g) Steerable (Lang D-501, formerly Decker) 
(h) Scott Model 3-24B, Steerable, full swiveling 
            (+193) 
  +5 lb. 
  +3 lb. 
  +3 lb. 
  +4 lb. 
  +4 lb. 
  +4 lb. 
    6 lb. 
    6 lb. 
19/ 207. Two main wheel-brake assemblies, 6.00-6, Type III Firestone Model 6C3HB   +4 lb. (+2) 
20/ 208. Wheel streamlines (dwg. A-9015 or A-9016)     6 lb. (+2)

Page 11 of 12 A-696, Rev 25 
 
21/ 209. Skis (eligible on any airplane of these models provided 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 (max. 1200 lb.) 
(b) Air Transport 1220-480 (max. 1220 lb.) 
(c) Air Transport 1224-580-1 (max. 1220 lb.) 
(d) Federal SC-1 (max. 1400 lb.) 
(e) Piper S-1000 (max. 1200 lb.) 
(f) Jennings TY-2 (max. 1200 lb.) 
(g) Federal SA-1 (max. 1200 lb.) 
(h) Aviation Service B (max. 1650 lb.) 
(i) Richards 1-B (max. 2220 lb.) 
(j) Washington Aircraft (max. 1200 lb.) 
(k) Heath 655 (max. 1210 lb.) 
(l) Federal SC-2 (max. 1650 lb.) 
(m) Aviation Service A (max. 1100 lb.) 
(n) Federal SA-1A (max. 1300 lb.) 
(o) Jacobsen (formerly Escanaba) EAS-100 (max. 1200 lb.) 
(p) Richards 1-A (max. 1600 lb.) 
(q) Marston MFS-1600 (max. 1600 lb.) 
(r) Heath 725 (max. 1450 lb.) 
(s) Aero. Sales & Service AS-6.00 (max. 1320 lb.) 
(t) Jack Carr Service 16 (max. 1600 lb.) 
(u) Fairbanks MF-5 (max. 1310 lb.) 
(v) Heath 725A (max. 1450 lb.) 
(w) Federal SK4-1 (max. 1400 lb.) 
(x) Call S2 (max. 1800 lb.) 
(y) Federal A-1500 (max. 1500 lb.), Federal Instln. dwg. 11R232 
(z) Federal A-1500A (max. 1500 lb.), Federal Instln. dwg. 11R232 
(aa) Federal A-1850 (max. 1850 lb.), Federal Instln. dwg. 11R232 
(ab) Federal A-2000 (max. 2000 lb.), Federal Instln. dwg. 11R232 
(ac) Federal A-2000A (max. 2000 lb.), Federal Instln. dwg. 11R232 
(ad) Federal CA-1850-6 (max. 1850 lb.), Federal Instln. dwg. 11R232 
(ae) Wesco A-15, Western Aircraft Equipment Co. dwg. 148, 202, 203 
(af) Wesco A-20, Western Aircraft Equipment Co. dwg. 148, 202, 203 
Use act. wt. change 
22/ 210. Two main-wheel tires, 6.00-6, Type III with regular tubes 
(a) 2-ply rating 
(b) 4-ply rating 
 
    12 lb.(+2) 
    +5 lb. (+2) 
23/ *211. Heath 1460A float installation, 172 lb. including auxiliary fin, 4 lb. (+176)  (BCS12 -D 
and BCS12-D1 only) 
+122 lb. (+25) 
24/ *212. Wheel fenders, Consolidair Model 16 
(Consolidair instln. dwg. 0029). 
    10 lb. (+2) 
 
Electrical Equipment 
310. Battery and box 
(a) 6v. 
(b) 12 v. 
(c) 12 v. (BC12D-4-85 and BCS12-D-4-85) 
 
    9 lb. (+10) 
  15 lb. (+10) 
  16 lb. (+70) 
319. Position lights 
(a) Grimes B (6 v.) 
(b) Grimes D (6 v.) (BC12-D, BC12D-85 and BCS12-D only) 
(c) Grimes D (12 v.) (BC12-D, BC12D-85, BCS12D-85, BC12D-4-85 and BCS12D-4-85) 
    2 lb. (+77) 
322. Generator (Delco-Remy 1101876) (BC12D-4-85 and BCS12D-4-85 only)   10 lb. (-24) 
323. Voltage regulator (Delco-Remy 1118323) (BC12D-4-85, BCS12D-4-85)     1 lb. (-18)

A-696, Rev 25 Page 12 of 12 
Interior Equipment 
25/ 401. Wheel type control  
26/ 402. Cabin heater (Taylorcraft BC-L606 or BC-L630)     2 lb. (-22) 
27/ 403. Stick type control Negligible weight 
 
Miscellaneous (not listed above) 
28/ 601. Auxiliary door   +5 lb. (+25) 
 
NOTE 1. Weight and balance report including list of equipment included in certificated empty weight and loading 
instructions when necessary must be provided for each aircraft at the time of original certification. 
NOTE 2. Left hand wing tank eligible as 6 gal. auxiliary on all models except BCS-65 and BC12D-85. 
NOTE 3. Required placard adjacent to shutoff valve of right and left wing tanks:  “Refill main tank in level flight 
only”. 
 
-END-
```

## ADs (10, 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 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 87-03-08](https://openairdocs.org/ad/87-03-08): Oil Pressure Gauge Hose · Taylorcraft 2000 19, BC, BC-65 and 8 more. Effective Mar 1, 1987
- [AD 78-20-11](https://openairdocs.org/ad/78-20-11): Aileron Control Malfunction · Taylorcraft 2000 BC12-D and F19. Effective Oct 16, 1978
- [AD 47-13-02](https://openairdocs.org/ad/47-13-02): Fuel Hose · Taylorcraft 2000 BC-65, BC12-65, BC12-D and 4 more
- [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
- [AD 2007-16-14](https://openairdocs.org/ad/2007-16-14) (historical): Left and right wing front and aft lift struts · Taylorcraft 2000 BC, BC-65, BC12-65 and 11 more. Effective Aug 20, 2007

## Registered aircraft by registry model (OpenAirDocs)

- [Taylorcraft BC12-D](https://openairdocs.org/model/taylorcraft-bc12-d): 1,011 aircraft (registry code 8850316)
- [Taylorcraft BC-65](https://openairdocs.org/model/taylorcraft-bc-65): 109 aircraft (registry code 8850306)
- [Taylorcraft BC12-65](https://openairdocs.org/model/taylorcraft-bc12-65): 104 aircraft (registry code 8850310)
- [Taylorcraft BC12-D1](https://openairdocs.org/model/taylorcraft-bc12-d1): 76 aircraft (registry code 8850320)
- [Taylorcraft BC12D-85](https://openairdocs.org/model/taylorcraft-bc12d-85): 28 aircraft (registry code 8850322)
- [Taylorcraft BC](https://openairdocs.org/model/taylorcraft-bc): 17 aircraft (registry code 8850302)
- [Taylorcraft BCS12-D](https://openairdocs.org/model/taylorcraft-bcs12-d): 11 aircraft (registry code 8850318)
- [Taylorcraft BC12D-4-85](https://openairdocs.org/model/taylorcraft-bc12d-4-85): 6 aircraft (registry code 8850323)
- [Taylorcraft BCS12D-4-85](https://openairdocs.org/model/taylorcraft-bcs12d-4-85): 5 aircraft (registry code 8850324)
- [Taylorcraft BCS-65](https://openairdocs.org/model/taylorcraft-bcs-65): 2 aircraft (registry code 8850308)
- [Taylorcraft BCS12-65](https://openairdocs.org/model/taylorcraft-bcs12-65): 1 aircraft (registry code 8850314)
- [Taylorcraft BCS](https://openairdocs.org/model/taylorcraft-bcs): 0 aircraft (registry code 8850304)
- [Taylorcraft BCS12-D1](https://openairdocs.org/model/taylorcraft-bcs12-d1): 0 aircraft (registry code 8850321)
- [Taylorcraft/Mcbee BC-12D](https://openairdocs.org/model/taylorcraft-mcbee-bc-12d): 0 aircraft (registry code 8850319)
- [Taylorcraft/Peterson BC12-D](https://openairdocs.org/model/taylorcraft-peterson-bc12-d): 0 aircraft (registry code 8850317)
- [Vaughn/Taylorcraft BC12-D](https://openairdocs.org/model/vaughn-taylorcraft-bc12-d): 0 aircraft (registry code 8850315)

## STCs approved under this data sheet (91, first 50)

- [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 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 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 SA661AL](https://openairdocs.org/stc/SA661AL): Installation of Plexiglass Skylight in fuselage cabin. Terry L. Bowden, President Certified Aeronautical Products LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA24CH](https://openairdocs.org/stc/SA24CH): Installation of Baumann Model 1420 floats.. Baumann Floats LLC
- [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 SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [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 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 SA02604CH](https://openairdocs.org/stc/SA02604CH): Installation of a battery powered engine starting system.. SafeStart Starter System
- [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 SA10921SC](https://openairdocs.org/stc/SA10921SC): Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators. Hartzell Engine Technologies, LLC
- [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 SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft
- [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 SA1-210](https://openairdocs.org/stc/SA1-210): Conversion of Taylorcraft Model BC or Model BC12D to the equivalent of aircraft models BC12D85 and BC12D-4-85 or Model 19.. Certified Aeronautical Products
- [STC SA02110CH](https://openairdocs.org/stc/SA02110CH): Installation of a Time Trac Data Recorder. P2 Incorporated
- [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 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 SA241CH](https://openairdocs.org/stc/SA241CH): Install Ceconite 101 fabric.. Aviation Products Systems Inc.
- [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International
- [STC SA2085CE](https://openairdocs.org/stc/SA2085CE): 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.. Petersen Aviation Inc
- [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 SA768GL](https://openairdocs.org/stc/SA768GL): Superseded by STC SA01944CH.. 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 SA1008WE](https://openairdocs.org/stc/SA1008WE): Installation of Poly-Fiber covering material.. Poly-Fiber Inc.
- [STC SA489EA](https://openairdocs.org/stc/SA489EA): Installation of ARP Inc. carburetor ice detection system. Aircraft & Rotorcraft Products (ARP) Inc
- [STC SA1398GL](https://openairdocs.org/stc/SA1398GL): Surrendered and incorporated into STC SA241CH.. Cooper Aviation Supply Company, Inc.
- [STC SA02520AT](https://openairdocs.org/stc/SA02520AT): Installation of M-20 Oil Separator, model 600-WP.. M-20 Oil Separators LLC
- [STC SA02168AK](https://openairdocs.org/stc/SA02168AK): Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated.. Avalaska Inc

All 91: https://openairdocs.org/tcds/A-696/stcs.md

---
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