# TCDS A-746: Hangar D LLC

- Type: Type certificate data sheet
- Status: Current
- Holder: Hangar D LLC
- Revision: 9
- Revised: February 18, 2026
- Product: Aircraft, Small Airplane
- Certification basis: CAR 4a
- Registered aircraft: 253, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/de/b3/deb38bcea787572fa9572ae1b0c6bbcc50c6df685a871c6838fecd87f728183c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158728279320260305210627.0001
- Page: https://openairdocs.org/tcds/A-746

## Models (4)

As the data sheet lists them.

- DCO-65 ((Army L-2A, -2B, and -2M))
- DL-65 ((Army L-2D))
- DF-65 ((Army L-2E))
- DC-65 ((Army L-2, L-2C))

## 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  
Rev. No. 9 - - - - - - 9  
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
 A-746   
 Revision 9  
 Hangar D, LLC 
(Army L-2, L-2C) DC-65 
(Army L-2E) DF-65  
(Army L-2D) DL-65  
(Army L-2A, -2B, -2M) DCO-65 
 
   
 Februar y 18, 2026  
 
 
TYPE CERTIFICATE DATA SHEET NO. A-746 
 
This data sheet, which is part of Type Certificate No. A-746, prescribes conditions and limitations under which the product 
for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.  
 
Type Certificate Holder: Hangar D, LLC 
c/o Wheeler and Mitchelson, Chartered 
319 North Broadway Street 
Pittsburg, KS 66762 
 
Type Certificate Holder Record: Taylorcraft Incorporated  transferred A-746 to Robert J. Kuhlow, March 21, 1972  
Marianne Kuhlow assumed ownership, December 7, 2001.  
Marianne Kuhlow transferred A-746 to Arizona Aerospace Foundation, May 27, 2003.  
Arizona Aerospace Foundation, dba Pima Air and Space Museum, transferred to Karl 
M. Gabriel, April 23, 2021. 
Karl M. Gabriel transferred A-746 to Hanger D, LLC, c/o Wheeler and Mitchelson, 
Chartered, October 15, 2024  
 
 
I. Model DC-65 (Army L-2, L-2C) 2-PCLM, Approved November 25, 1941 
(Army L-2 same as DC-65 except for overhead window in cabin) 
 
Engines Continental A-65-8 (See It em 308 for optional engines)  
 
Fuel 73 min. octane aviation gasoline 
 
Engine Limits For all operations, 2300 rpm (65 hp) 
 
Airspeed Limitations Le vel flight or climb 110 mph  ( 96 knots) 
(True Ind.) Glide or drive 140 mph  (122 knots) 
 
Propeller limits Static rpm at maximum permissible throttle setting: 
Not over 2210, not under 2040. 
No additional tolerance permitted. 
Diameter: not over 72 in., not under 70 in.  
 
C.G. Range (+11.8) to (+19.5) 
 
Empty Wt. C.G.  (+12.6) to (+16.7) 
Range  
 
Maximum Weight 1250 lbs. 
 
Number of Seats 2 (+11) and (+40) 
Placard required: "SOLO FROM FRONT SEAT ONLY" 
(See NOTE 3 for swivel type seats)

A-746 Page 2 of 8 Rev. 9 
I. Model DC-65 (Army L-2, L-2C)  (cont’d) 
 
Maximum Baggage 20 lbs. (+60) 
 
Fuel Capacity 14 gal. total (2 gal. fusela ge tank (-18); two 6 gal. wing tanks (+23)) 
 
Oil Capacity 4 quarts (-38) 
 
Control Surface Movements 
 
Elevator Up 28.0 degrees 
 Down 28.0 degrees 
Elevator Trim Tab Up 41.0 degrees 
 Down 41.0 degrees 
Aileron Up 28.0 degrees 
 Down 21.0 degrees 
Rudder Right 25.0 degrees 
 Left 25.0 degrees 
 
Serial Nos. Eligible 4002 and On, and all AAF  numbers.  Use mfg. no., if available. 
 
Required Equipment Items 101, 102, 103, 104, 105 
 
 
II. Model DF-65 (Army L-2E) 2-PC LM, Approved November 25, 1941 
(Same as DC-65 except for engine installations) 
 
Engines Franklin 4AC-176-B2 (See Item 308 for optional engines)  
 
Fuel 73 min. octane aviation gasoline 
 
Engine Limits For all operations, 2200 rpm (65 hp) 
 
Airspeed Limitations Le vel flight or climb 110 mph  ( 96 knots) 
(True Ind.) Glide or drive 140 mph  (122 knots) 
 
Propeller limits Static rpm at maximum permissible throttle setting: 
(1) With Franklin 4AC-176-B2 engine: Not over 2170 
 Not under 2050 
 
(2) With Franklin 4AC-176-BA2 engine: Not over 2315 
 Not under 2150 
 
No additional tolerance permitted. 
Diameter: not over 72 in., not under 70 in.  
 
C.G. Range (+11.8) to (+19.5) 
 
Empty Wt. C.G.  (+12.9) to (+16.8) 
 Range (If empty weight C.G. fall s within this range, it is unnecessary to check critical forward 
and aft C.G. positions.  Range is not valid for non-standard arrangements.)  
 
Maximum Weight 1250 lbs. 
 
Number of Seats 2 (+11) and (+40) 
Placard required: "SOLO FROM FRONT SEAT ONLY" 
(See NOTE 3 for swivel type seats) 
 
Maximum Baggage 20 lbs. (+60) 
 
Fuel Capacity 14 gal. total (2 gal. fusela ge tank (-18); two 6 gal. wing tanks (+23)) 
 
Oil Capacity 5 quarts (-45)

Rev. 9 Page 3 of 8 A-746 
II. Model DF-65 (Army L-2E)  (cont'd) 
 
Control Surface Movements 
 
Elevator Up 28.0 degrees 
 Down 28.0 degrees 
Elevator Trim Tab Up 41.0 degrees 
 Down 41.0 degrees 
Aileron Up 28.0 degrees 
 Down 21.0 degrees 
Rudder Right 25.0 degrees 
 Left 25.0 degrees 
 
Serial Nos. Eligible 4002 and On, and all AAF  numbers.  Use mfg. no., if available. 
 4001 eligible at 1200 lbs., maximum weight. 
 
Required Equipment Items 101, 102, 103, 104, 105 
 
 
III. Model DL-65 (Army L-2D) 2-PC LM, Approved November 25, 1941 
 (Same as DC-65 except for engine installations) 
 
Engines Lycoming O-145-B2 (See Item 308 for optional engines)  
 
Fuel 73 min. octane aviation gasoline 
 
Engine Limits For all operations, 2550 rpm (65 hp) 
 
Airspeed Limitations Le vel flight or climb 110 mph  ( 96 knots) 
Glide or drive 140 mph  (122 knots) 
 
Propeller limits Static rpm at maximum permissible throttle setting: 
Not over 2315, not under 2100. 
No additional tolerance permitted. 
Diameter: not over 70 in., not under 68 in.  
 
C.G. Range (+11.8) to (+19.5) 
 
Empty Wt. C.G.  (+12.9) to (+16.8) 
 Range (If empty weight C.G. fall s within this range, it is unnecessary to check critical forward 
  and aft C.G. positions.  Range is not  valid for non-standard arrangements.)  
 
Maximum Weight 1250 lbs. 
 
Number of Seats 2 (+11) and (+40) 
Placard required: "SOLO FROM FRONT SEAT ONLY" 
(See NOTE 3 for swivel type seats) 
 
Maximum Baggage 20 lbs. (+60) 
 
Fuel Capacity 14 gal. total (2 gal. fusela ge tank (-18); two 6 gal. wing tanks (+23)) 
 
Oil Capacity 5 quarts (-45)

A-746 Page 4 of 8 Rev. 9 
III. Model DL-65 (Army L-2D)  (cont'd) 
 
Control Surface Movements 
 
Elevator Up 28.0 degrees 
 Down 28.0 degrees 
Elevator Trim Tab Up 41.0 degrees 
 Down 41.0 degrees 
Aileron Up 28.0 degrees 
 Down 21.0 degrees 
Rudder Right 25.0 degrees 
 Left 25.0 degrees 
 
Serial Nos. Eligible 4002 and On  
 
Required Equipment Items 101, 102, 103, 104, 105 
 
 
IV. Model DCO-65 (Army L-2A, L-2B, L-2M) 2-PCLM, Approved February 24, 1942 
(Same as DC-65 except for rear view transparent cabin enclosure, revised cockpit arrangement, and revised fuselage and 
landing gear structure.  Army L-2M is same as Model DCO-65 except for revised rear transparent enclosure, revised 
instrument panel, revised 6 gal., wing tank, closed cowl, revised engine installation, spoiler installation, and operating limits 
as noted below.) 
 
Engines Continental A-65-8   
 
Fuel 73 min. octane aviation gasoline 
 
Engine Limits For all operations, 2300 rpm (65 hp) 
 
Airspeed Limitations Le vel flight or climb 110 mph  ( 96 knots) 
(True Ind.) Glide or drive 140 mph  (122 knots) 
Spoilers extended (L-2M)   90 mph  ( 78 knots) 
 
Propeller limits Static rpm at maximum permissible throttle setting: 
DCO-65 (Army L-2A, L-2B) Not over 2350, not under 2000. 
(Army L-2M) Not over 2325, not under 2135. 
No additional tolerance permitted. 
Diameter: not over 72 in., not under 70 in.  
 
C.G. Range DCO-65 (Army L-2A, L-2B) (+13.2) to (+17.1) 
(Army L-2M) (+13.2) to (+15.3) 
 
Empty Wt. C.G.  DCO-65 (Army L-2A, L-2B) (+12.3) to (+17.1) 
 Range (Army L-2M) (+13.2) to (+15.3) 
 
Maximum Weight DCO-65 (Army L-2A, L-2B) 1300 lbs. 
(Army L-2M) 1325 lbs. 
 
Number of Seats 2 (+11) and (+40) 
Placard required: "SOLO FROM FRONT SEAT ONLY" 
(See NOTE 3 for swivel type seats) 
 
Maximum Baggage DCO-65 (Army L-2A, L-2B) 20 lbs. (+59) 
(Army L-2M) None

Rev. 9 Page 5 of 8 A-746 
IV. Model DCO-65 (Army L-2A, L-2B, L-2M) (cont'd) 
 
Fuel Capacity 14 gal. total (2 gal. fusela ge tank (-18); two 6 gal. wing tanks (+23)) 
(Army L-2M) (+24) 
 
Oil Capacity 4 quarts (-38) 
 
Control Surface Movements 
 
Elevator Up 28.0 degrees 
 Down 28.0 degrees 
Elevator Trim Tab Up 41.0 degrees 
 Down 41.0 degrees 
Aileron Up 28.0 degrees 
 Down 21.0 degrees 
Rudder Right 25.0 degrees 
 Left 25.0 degrees 
Spoilers (Army L-2M) Up 50.0 degrees 
 Left      0 degrees 
 
Serial Nos. Eligible DCO-65 (Army L-2A, L-2B) 4002 and On , and all AAF numbers.  Use mfg. no., if available. 
(Army L-2M) 5166 and On  
 
Required Equipment DCO-65 (Army L-2A, L-2B) Items 101, 102, 103, 104, 105 
(Army L-2M) Items 101, 102, 302(e), 304  
 
 
Data Pertinent to all Models 
 
Datum Leading edge of wing 
 
Leveling Means 3/8 in. above top of stabilizer L.E. , and top of stabilizer rear beam at fuselage. 
 
Certification Basis Type Certificate No. 746 (CAR 4a) 
 
Production Basis None.  Prior to original certificat ion, a CAA 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. 
 
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. Hartzell ground adjustable propeller. 18 lbs. (-58) 
(a) Hub: HA-12U 
(b) Blades: 7414 to 6814 or 7214 to 6814M. 
 Eligible at diameter  
(c) Static rpm limits shown above for fixed pitch wood propellers. 
 
2. McCauley propeller, with the following limits.  
(a) Model 1A90 21 lbs. (-58) 
(b) Diameter: not over 74 in., not under 72.5 in. (eligible on DCO-65 model only) 
(c) Static rpm at maximum permissible throttle settings: 
 Not over 2250, not under 2070. 
 
 101. Propeller.  Wood (fixed or adjustable pitch) 11 lbs. (-58)

A-746 Page 6 of 8 Rev. 9 
Data Pertinent to all Models 
 
Engine and Engine Accessories - Fuel and Oil System 
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 original 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. 
 
 Engine limits: for all operations, 2300 rpm (65 hp). 
 
 102. Carburetor air heater. 1 lbs. (-51) 
 
 105. Muffler (No. D-A624) 6 lbs. (-36) 
 
 106. Carburetor air intake & filter (Continenta l A-5810) (Models DCO-65 & DO-65 only) 3 lbs. (-49) 
 
 107. Carburetor air scoop & filter (Skinner Modifi ers Model S-300A scoop & F-300A filter) 3 lbs. (-47) 
 (Models DCO-65 (L-2 series) only) (Filter  must always be installed on air scoop) 
 
 108. AC air filter No. 1529265 (Aircooled Motors Dwg. SK-534-4) (Model DF-65 only) 1 lbs. (-41) 
 
 110. Oil Filter, Fram PB -5, weight includes 1 quart oil  4 lbs. (-30) 
a. Kit No. 510, Fram Installation Draw ing No. 61544 (Models DC-65, DCO-65) 
b. Kit No. 520, Fram Installation Drawing No. 61550 (Model DL-65) 
c. Kit No. 501, Fram Installatio n Drawing No. 61564 (Model DF-65) 
 
 308. Engines 
a. Model DC-65 (Continental, per Engine Specification No. 205) 
(1) A-65-7 -11 lbs. (-34) 
(2) A-65-9 3 lbs. (-34) 
 
b. Model DL-65 (Lycoming, per Engine Specification No. 210) 
(1) 0-145-B1 -11 lbs. (-45) 
 
c. Model DF-65 (Franklin, per Engine Specification No. 221) 
(1) 4AC-176-BA2 Negligible weight increase 
Engine limits: for all operations, 2300 rpm (65 hp) 
 
Landing Gear and Floats 
 
 103. 6.00-6 wheels (Model Shinn 6C4) with 6.00-6 2-ply tires 22 lbs.  (+0) 
 
 104. Tailskid, Spring 5 lbs. (+190) 
 
 302. Tail wheel  (+198) 
a. Omitted 
b. 6x2.00 steerable (Aircraft Assc.) +3 lbs. 
c. 6x2.00 full swiveling (Taylorcraft) +3 lbs. 
d. 6x2.00 steerable (Lake State Products 5-40-31) +4 lbs. 
e. 6x2.00 steerable (Taylorcraft)  +4 lbs. 
f. 6x2.00 steerable (Scott Model TA-8B) +4 lbs. 
 
 303. Parking brake 3 lbs. (-13) 
 
 304. 6.00-6 wheels (Model Shinn 6C4HB) with brakes +6 lbs.  (+0) 
 
 307. 6.00-6 4-ply tires Negligible with increase

Rev. 9 Page 7 of 8 A-746 
Data Pertinent to all Models 
 
Landing Gear and Floats (cont'd) 
 
 313. Skis (eligible on any airplane of these mo dels provided installation meets the minimum  
9 in. ground clearance requirements.  The maximum weight for the skiplane will be the  
same as for the corresponding landplane of that shown in parenthesis after each ski model,  
whichever is less.) Use actual weight change 
a. Federal SC-1  maximum 1400 lbs. 
b. Heath 725 or 725A  maximum 1450 lbs. 
c. Air Transport 1224-580-1 maximum 1220 lbs. 
d. Jacobson (formerly Escanaba) EAS-100 maximum 1200 lbs. 
e. Federal A-1500; Installation Draw ing No. 11R232 maximum 1500 lbs. 
f. Federal A-1500A; Installation Dr awing No. 11R232 maximum 1500 lbs. 
g. Federal A-1850; Inst allation Drawing No. 11R232 maximum 1850 lbs. 
h. Federal A-2000; Inst allation Drawing No. 11R232 maximum 2000 lbs. 
i. Federal A-2000A; Installation Dr awing No. 11R232 maximum 2000 lbs. 
j. Federal CA1850-6; Installation Drawing No. 11R232 maximum 1850 lbs. 
 
Electrical Equipment 
 
 301. Position Lights (Grimes B) 2 lbs. (+24) 
 
 305. Battery  
a. 6-volt Willard Model No. SYR-7-3 (10 A.H.) with box 9 lbs. (-30) 
b. 12-volt Reading Model No. 333LD (33 A.H.) 14 lbs. (-25) 
c. 6-volt Willard Model No. SYR-7-6 (10 A.M.) with box 16 lbs. (-25) 
d. 6-volt Reading Model No. 324L (24 A.H.) with box 12 lbs. (-24) 
 
 311. Generator, wind driven 
a. 6-volt General Armature Co. 10 lbs. (0) 
b. 12-volt Lear Model No. 1030-A 10 lbs. (+5) 
c. 6-volt Champion Model No. W612-6V with rotor brake 10 lbs. (+1) 
d. 6-volt Champion Model No. W612B 9 lbs. (0) 
 
Interior Equipment 
 
 306. Cabin Heater Negligible with increase 
 
 309. Taylorcraft compass (Carwell) 2 lbs.  
 
 401. Cabin Heater 
a. Surface Combustion Model AAV-15N-12, fuel burning heater 5 lbs. (-37) 
b. Duct for above heater in stallation (Model DCO-65 (L-2 series) only) 2 lbs. (+20) 
 
 402. Cabin Heater 
a. Stewart Warner Model No. 24809  10 lbs. (-32) 
b. Duct for above heater in stallation (Model DCO-65 (L-2 series) only) 2 lbs. (+5)

A-746 Page 8 of 8 Rev. 9 
 
NOTE 1. Current weight and balance information, including list of equipment included in certificated empty 
  weight and loading instructions, when  necessary, must be in each airplane at the time of original certification, 
and always thereafter (except in the case of air carrier operators having an approved weight control system). 
 
NOTE 2. Placard required: "SOLO FROM FRONT SEAT ONLY" 
 
NOTE 3. The swivel type rear seats with folding backs on all Taylorcraft L-2 series aircraft must be permanently 
fastened so that there is no possibility of interference with the rear control stick.  The back should be bolted 
or welded in place and the seat should be permanently locked in the forward-facing position. 
 
NOTE 4. The following parts from TG-6 gliders can be us ed directly on Taylorcraft L-2 series aircraft.  The 
replacement of such complete component parts is considered a minor repair, in accordance with Cam 
18.3006. 
 
1. Tail surfaces, except the fin. 
2. Landing gear tires and wheels. 
3. Tail wheels 
4. Wings.  Wings with the spoiler installation should be used only on the model Army L-2M.  The spoiler 
installation should be removed and suitable covering placed over the upper surface opening on wings for 
use in other Model D series airplanes. 
5. Certain parts and assemblies of the control sy stem from, and including, the middle occupant aft. 
6. Wing struts. 
7. Instruments, same as or equivale nt to, those used on powered aircraft. 
 
The fuselage primary structure of the TG-6 glider aft of the firewall station can be used on Taylorcraft D 
series airplanes.  However, the use of such parts entails a major repair and must be handled in accordance 
with CAM 18. 
 
 
 
----- END -----
```

## ADs (1, 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

## Registered aircraft by registry model (OpenAirDocs)

- [Taylorcraft DCO-65](https://openairdocs.org/model/taylorcraft-dco-65): 195 aircraft (registry code 8850408)
- [Taylorcraft DC-65](https://openairdocs.org/model/taylorcraft-dc-65): 49 aircraft (registry code 8850402)
- [Taylorcraft DF-65](https://openairdocs.org/model/taylorcraft-df-65): 7 aircraft (registry code 8850416)
- [Taylorcraft DL-65](https://openairdocs.org/model/taylorcraft-dl-65): 1 aircraft (registry code 8850420)
- [Taylorcraft/Marek DCO-65](https://openairdocs.org/model/taylorcraft-marek-dco-65): 1 aircraft (registry code 8850409)
- [Taylorcraft/Barkmann DCO 65](https://openairdocs.org/model/taylorcraft-barkmann-dco-65): 0 aircraft (registry code 8850407)

## STCs approved under this data sheet (57, first 50)

- [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 SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc.
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc.
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [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 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 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 SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft
- [STC ST00961LA](https://openairdocs.org/stc/ST00961LA): Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29, 2000, or later FAA approved revisions.  These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1, "Slug Thrower Cartridges Master Drawing List", Revision N/C, dated
June 26, 2000, or later FAA approved revisions.. AMETEK AMERON LLC d/b/a MASS Systems
- [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc.
- [STC SA02164LA](https://openairdocs.org/stc/SA02164LA): Removal of Teledyne Continental Motors A-65-8 engine and installing one of the following Teledyne Continental Model engines: C85-8, C85-8F, C85-12, C85-12F, C85 (Modified per STC # SE00979AT), C90-8F, C90-12F OR 0-200A.. Certified Aeronautical Products
- [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 SA02047LA](https://openairdocs.org/stc/SA02047LA): S/N L4413 ONLY: Installation of a Teledyne Continental Motors model C85-12 engine (modified by STC SE00979AT) and a McCauley model 1B90 propeller.. Anctil Gary
- [STC SA00402SE](https://openairdocs.org/stc/SA00402SE): Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed). Aviation Development Corporation
- [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International
- [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 SA770GL](https://openairdocs.org/stc/SA770GL): 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 SA1421SW](https://openairdocs.org/stc/SA1421SW): Installation of EDO-60-1320 floats. Robert Picard
- [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 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
- [STC SA71GL](https://openairdocs.org/stc/SA71GL): Installation of air filters. Brackett Aero Filters Inc.
- [STC SA1-86](https://openairdocs.org/stc/SA1-86): McCauley metal fixed-pitch propeller 1B90-CM on aircraft powered by Continental A-65 engine.. Beth-Air Consulting
- [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 SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc
- [STC SA5755NM](https://openairdocs.org/stc/SA5755NM): Installation of a propeller anti theft device.. Davis Ray G
- [STC SA3192SO](https://openairdocs.org/stc/SA3192SO): Installation of a Teledyne Continental Motors model O-200 engine and a McCauley model 1A101 propeller.. Collier John
- [STC SA3193SO](https://openairdocs.org/stc/SA3193SO): Installation of Cleveland brakes and wheels.. Collier John
- [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 SA1677NM](https://openairdocs.org/stc/SA1677NM): Installation of a Continental O-200A engine, fiberglass cowling, two 12- gallon wing tanks, and McCauey1A101DCM/6948 propeller.. Clover Park Vocational/Technical Institute
- [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 SA4-302](https://openairdocs.org/stc/SA4-302): Installation of BN-1 propeller spinner.. ACS Products Co, Inc
- [STC SA2086CE](https://openairdocs.org/stc/SA2086CE): 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 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 SA4-1210](https://openairdocs.org/stc/SA4-1210): Installation of Eonnex cover on aircraft surfaces.. 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 SA3202WE](https://openairdocs.org/stc/SA3202WE): ONE ONLY STC, SN L-5830: Installation of Continental C-85-12F engine, McCauley 1890 propeller, modified trim and spoiler control systems, and associated changes.. David B. Kratzer
- [STC SA69NW](https://openairdocs.org/stc/SA69NW): Installation of Matney's engine charge air-air filter assembly. (AA-1B, AA-1, AA-1A 1969 AND ON) (AA-5 1972, 1973 AND 1974 ONLY). Matney D H
- [STC SA798EA](https://openairdocs.org/stc/SA798EA): Installation of Monitair exhaust gas combustion monitor kit.. Rosemount Engineering Co

All 57: https://openairdocs.org/tcds/A-746/stcs.md

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