# TCDS A31CE: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 11
- Revised: November 27, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23, Part 36
- Registered aircraft: 107, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/bc/dd/bcddaa830a074fd224d9e193e24900aabc026454b1ba689e8b43f2dc295d38b7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B7F4C49977E8719E862581EF0060D2FD.0001
- Page: https://openairdocs.org/tcds/A31CE

## Models (1)

As the data sheet lists them.

- F90

## 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 
Rev. No. 11 3 6 3 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
A31CE 
Revision 11 
Textron Aviation  
F90 
November 27, 2017 
 
TYPE CERTIFICATE DATA SHEET NO. A31CE 
 
This data sheet which is part of Type Certificate No. A31CE 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 Textron Aviation Inc. 
 One Cessna Boulevard 
 Wichita, KS  67215 
 
Type Certificate Holder Record: Beech Aircraft Corporation transferred to 
 Raytheon Aircraft Company on April 15, 1996 
 
 Raytheon Aircraft Company transferred to 
 Hawker Beechcraft Corporation on March 26, 2007 
 
 Hawker Beechcraft Corporation transferred to 
 Beechcraft Corporation on April 12, 2013 
 
 Beechcraft Corporation transferred to  
 Textron Aviation Inc. on October 12, 2016 
 
I. Model F90, King Air, 7-10 PCLM (Normal Category), approved May 18, 1979 
 
 Engine Two (2) Pratt & Whitney Aircraft of Canada, Ltd., PT6A-135 (LA-1 through LA-204, 
  except LA-202), PT6A-135A (LA-202, LA-205 and on) (turboprop) per Beech 
  Specification BS 23046 and BS 23549 respectively. 
 
 Fuel JP-4, JP-5 (MIL-T-5624); JP-8 (MIL-T-83133); JET A, JET A-1, and JET B 
  conforming to P&WC S.B. 1244 or ASTM Spec. D1655. 
  See NOTE 6 for emergency fuels. 
 
 Oil (Engine & Gearbox) P&WC PT6 Engine Service Bulletin No. 1001 Lists approved brand oils 
 
 Engine Limits 
  
Shaft 
Horsepower 
 
N1 Gas 
Generator Speed 
 
Prop 
Shaft Speed 
Max. Permissible 
Turbine Interstage 
Temp. (Deg. C.) 
Takeoff (5 min.) 750 101.5% 1900* 805 
Max. continuous 
  (enroute emergency) 
 
750 
 
101.5% 
 
1900* 
 
805 
Starting transient (2 sec.)    1000 
Max. reverse (1 min.) 720 88.0% 1815 805 
 *See NOTE 4    
 
  At low altitude and low ambient temperature, the engines may produce more power at 
  takeoff than that for which the airplane has been certificated.  Under these conditions the 
  placarded torque meter limitations shall not be exceeded. 
 
  Oil temperatures Minus 40° C. minimum starting 
   Minus 40° C. to 99° C. low idle 
     10° C. to 99° C. max continuous

Rev. 11 2 A31CE 
 
I. Model F90 (cont’d) 
 
 Propeller and Two (2) Hartzell HC-B4TN-3B hubs (effective LA-1 through LA-120 except LA-20 and 
   Propeller Limits LA-97), HC-B4TN-3A or HC-B4TN-3B hubs (effective LA-20, LA-97, and LA-121  
  through LA-130) with Hartzell T10173FB-10.5 or T10173FNB-10.5 aluminum alloy  
  blades and Hartzell C-3425P, C-3425-1P, C3425-2P, or C-3425-3P spinner assembly. 
 
  (For Aircraft S/N LA-131 and on) 
  Two (2) Hartzell HC-B4TN-3A or HC-B4TN-3B hubs with Hartzell T10173FK-10.5 
  or T10173FNK-10.5 aluminum alloy blades and Hartzell C-3425-2P or C-3425-3P 
  spinner assembly. 
 
  Diameter:  92.0 in. (maximum) 
  No further reduction permitted. 
  Pitch settings at: 
   Flight idle stop (See NOTE 5(a)) 
   Secondary flight idle stop (See NOTE 5(b)) 
   Reverse   8.5° ± 0.4° 
   Feathered 87.5° ± 0.5° 
  Avoid continuous operation on ground below 1200 rpm.  
 
 Airspeed Limits (IAS)   LA-1 through LA-204 LA-202, LA-205 
        except LA-202       and on 
  Maximum operating speed 253 knots (291 mph) 253 knots (291 mph) 
   up to 12,600 ft. 
  Max operating Mach No. .48 .48 
  Maneuvering speed 171 knots (197 mph) 170 knots (196 mph) 
  Maximum flap extension speed 
    Approach position 32.5% 184 knots (212 mph) 183 knots (211 mph) 
     up to 27,700 ft. 
    100% position 40° 144 knots (166 mph) 146 knots (168 mph) 
  Landing gear extended 184 knots (212 mph) 183 knots (211 mph) 
  Landing gear operation 
    Extension 184 knots (212 mph) 183 knots (211 mph) 
    Retraction 166 knots (191 mph) 165 knots (190 mph) 
 
 C.G. Range (landing gear (+154.8) to (+164.0) at 10,950 lbs.  
   extended) (+150.0) to (+164.0) at 9,484 lbs. or less  
  Straight line variation between points given. 
  Moment change due to retracting landing gear (-5340 in.-lb.) 
 
 Empty Weight C.G. Range None 
 
 Maximum Weight Ramp 11,030 lbs. 
  Takeoff 10,950 lbs. 
  Landing 10,950 lbs. 
  Zero fuel   9,600 lbs. 
  (See NOTE 1) 
 
 Minimum Crew One pilot 
 
 No. of seats Crew (+129), passenger variable, see loading instructions. 
  Maximum passengers:  9 
 
 Maximum Baggage 403 lbs. (+276)

Rev. 10 3 A31CE 
I. Model F90 (cont’d) 
 
 Fuel Capacity Tank Cap. Gal. Usable Gal. Arm 
  Auxiliary LH   41.5       41 +173 
  Auxiliary RH   41.5       41 +173 
  Main LH 195     194 +154 
  Main RH 195     194 +154 
 
  See NOTE 1(a) for data on unusable fuel. 
 
 Oil Capacity 29 qt. total at +92 (includes 12 qt. usable in two integral engine tanks  
  See NOTE 1(b) for data on undrainable oil. 
 
 Maximum Operating Altitude 31,000 ft. 
 
 Control Surface Movements Wing flap Maximum 40°  
  Aileron tab Up 15° Down 15° 
  Aileron Up 16° Down 22° 
  Elevator tabs Up   0° Down 15° 
  Elevator Up 20° Down 17° 
  Rudder tab Right 15° Left 15° 
  Rudder Right 25° Left 25° 
 
 Serial Nos eligible LA-2 and on 
 
 Datum Located 160 in. forward of the wing main (forward) spar centerline. 
 
 Leveling Means Two external screws on left side of fuselage forward of entrance door. 
 
 Certification Basis FAR Part 23 dated February 1, 1965, as amended through 23-16 except 
  FAR 23.967(a)(5) is to be as amended through 23-18; FAR Part 36 dated 
  December 1, 1969, as amended through 36-5; SFAR 27 dated February 1, 
  1974, as amended through 27-2; and Special Conditions 23-85-CE-11, as amended. 
 
  Compliance with ice protection has been demonstrated in accordance with FAR 23.1419  
  when ice protection equipment is installed in accordance with the airplane equipment list. 
 
  Equivalent Safety Findings: 
  FAR 23.621 (S/N LA-2 through LA-186), 23.1323, 23.1545, 23.1583(a),  23.1305(v) 
 
  Application for Type Certificate dated January 12, 1977.   
  Type Certificate No. A31CE issued May 18, 1979, obtained by the manufacturer under  
  delegation option procedures. 
 
 Production Basis Production Certificate No. 8.  Delegation Option Manufacturer No. CE-2 authorized to  
  issue airworthiness certificates under delegation option provisions of Part 21 of the  
  Federal Aviation Regulations.

Rev. 11 4 A31CE 
 
I. Model F90 (cont’d) 
 
 Equipment The basic required equipment as prescribed in applicable airworthiness regulations  
  (see Certification Basis) must be installed in the aircraft for certification. 
 
  In addition, the following items of equipment are required: 
 
  1. Stall warning lift transducer, P/N 101-380005-9, and lift computer, 
   P/N 101-380005-17. 
  2. Maximum allowable airspeed indicator, P/N 109-384003-3, Pilot's and 
   Copilot's sides. 
  3. Pilot's Operating Handbook, P/N 109-590010-3, S/N LA-2 through LA-204, 
   except LA-202. 
  4. Pilot's Operating Handbook, P/N 109-590010-57, S/N LA-202, LA-205 and on. 
 
 
Data Pertinent to All Models 
 
NOTE 1. Current weight and balance data, loading information and a list of equipment included in basic empty weight must 
be provided for each airplane at the time of original certification. 
 
  (a) Basic empty weight includes unusable fuel of 41 lbs. at (+157) in.) with 9 lbs. being undrainable. 
  (b) Basic empty weight includes engine oil of 58 lbs. at (+92 in.) 
 
NOTE 2. All placards required in the FAA Approved Airplane Flight Manual (AFM) must be installed in the appropriate 
location. 
 
NOTE 3. Mandatory retirement times for all structural components are contained in the Limitation Section, Chapter 4, of 
the FAA Approved Beechcraft F90 Maintenance Manual.  These limitations may not be changed without FAA 
Approval. 
 
NOTE 4. The maximum propeller shaft overspeed limit is 110 percent (2090 rpm).  100 percent propeller shaft speed is 
defined as 1900 rpm and is the normal steady state operating limit.  Gas generator speeds up to 102.6 percent are 
permissible for 2 seconds and to 101.5 percent for unlimited periods subject to applicable temperature and other 
limits.  100 percent gas generator speed is defined as 37,500 rpm. 
 
NOTE 5. (a) Flight idle propeller low pitch is set so that at 1800 rpm there shall be an indicated 600 ±40 ft. -lb. torque 
   corrected to sea level standard day. 
  (b) Secondary flight and ground low pitch stop is set so that at 1800 rpm there shall be an indicated torque  
   of 350 ±40 ft.-lb. torque corrected to sea level standard day. 
 
NOTE 6. Emergency use of MIL-G-5572: 
  Grades 80/87, 91/98, 100/130 and 115/145 are permitted for a total time period not to exceed 150 hours’ time 
between engine overhaul periods.  It is not necessary to purge the unused fuel from the system when switching 
fuel types. 
 
 
 
---- END ----
```

## ADs (33, in force first)

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2020-25-01](https://openairdocs.org/ad/2020-25-01): Wings · Textron 100, 65-90, 65-A90 and 17 more. Effective Jan 11, 2021
- [AD 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008
- [AD 2006-12-25](https://openairdocs.org/ad/2006-12-25): Actuator nut assembly · General Machine - Diecron Actuator nut assembly, 100, 200 and 15 more. Effective Jul 28, 2006
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2005-01-04](https://openairdocs.org/ad/2005-01-04): Fuel hose · Textron 100, 200, 200C and 29 more. Effective Feb 22, 2005
- [AD 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004
- [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004
- [AD 2004-08-15](https://openairdocs.org/ad/2004-08-15): TAWS8000 terrain awareness warning systems (TAWS) · Cessna 421, 500, 501 and 18 more. Effective Jun 7, 2004
- [AD 2003-13-16](https://openairdocs.org/ad/2003-13-16): Aft Pressure Bulkhead of Fuselage · Textron 100, 200, 200C and 33 more. Effective Aug 25, 2003
- [AD 2003-02-03](https://openairdocs.org/ad/2003-02-03): Airstair door and emergency exits · Textron 100, 200, 2000 and 46 more. Effective Mar 7, 2003
- [AD 2002-23-11](https://openairdocs.org/ad/2002-23-11): Elevator Balance Weight Attachment Screws · Textron 1900, 1900C, 1900C (C-12J) and 30 more. Effective Jan 10, 2003
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 99-10-07](https://openairdocs.org/ad/99-10-07): Elevator Control Cable · Textron 65-90, 65-A90, 65-A90-1 and 9 more. Effective Jun 8, 1999
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-04-24](https://openairdocs.org/ad/98-04-24): AFM - Limitations Section - Icing · Textron 100, 300, 58 and 13 more. Effective Mar 13, 1998
- [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998
- [AD 97-25-01](https://openairdocs.org/ad/97-25-01): Outflow/Safety Valve · Textron 100, 200, 2000 and 38 more. Effective Jan 11, 1998
- [AD 97-23-17](https://openairdocs.org/ad/97-23-17): Pneumatic Tubing · Textron 200, 200C, 200CT and 30 more. Effective Dec 29, 1997
- [AD 97-06-06](https://openairdocs.org/ad/97-06-06): Pilot and Copilot Chairs Locking Pins · Textron 100, 1900, 1900C and 43 more. Effective May 9, 1997
- [AD 96-03-13](https://openairdocs.org/ad/96-03-13): Main Landing Gear Drag Leg Lock Link · Textron 100, 200, 200C and 24 more. Effective Apr 1, 1996
- [AD 95-13-03](https://openairdocs.org/ad/95-13-03): Electrical Landing Gear Motor · Textron 100, 200, 200C and 22 more. Effective Jul 28, 1995
- [AD 92-15-01](https://openairdocs.org/ad/92-15-01): Truss-To-Firewall Bolts · Textron 100, 200, 200C and 40 more. Effective Aug 21, 1992
- [AD 91-12-11](https://openairdocs.org/ad/91-12-11): Side Windows · Textron 200, 200C, 200CT and 7 more. Effective Jul 15, 1991
- [AD 90-08-17](https://openairdocs.org/ad/90-08-17): Fuselage Moisture Drain System · Textron 100, 200, 200C and 32 more. Effective May 7, 1990
- [AD 89-22-14](https://openairdocs.org/ad/89-22-14): Aileron Flutter · Textron 200, 200C, 200CT and 9 more. Effective Nov 17, 1989
- [AD 87-04-24](https://openairdocs.org/ad/87-04-24): Elevator Trim Cable System · Textron 1900, 1900C, 200 and 28 more. Effective Apr 14, 1987
- [AD 85-22-05](https://openairdocs.org/ad/85-22-05): Nuts and Bolts Replacement · Textron 100, 200, 200C and 60 more. Effective Nov 12, 1985
- [AD 83-07-14](https://openairdocs.org/ad/83-07-14): One-Ply Window Replacement · Textron 200, 200C, 200CT and 4 more. Effective Apr 18, 1983
- [AD 80-07-05](https://openairdocs.org/ad/80-07-05): Bolt and Nut, Wing Section · Textron 200, 200C, 200T and 10 more. Effective Apr 3, 1980
- [AD 98-15-13](https://openairdocs.org/ad/98-15-13) (historical): Fuel Hose · Raytheon 100 Model or Series (all), 200 Model or Series (all), 200C and 32 more. Effective Aug 28, 1998
- [AD 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989

## Registered aircraft by registry model (OpenAirDocs)

- [Beech F90](https://openairdocs.org/model/beech-f90): 107 aircraft (registry code 1152909)

## STCs approved under this data sheet (195, first 50)

- [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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc.
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA4132NM](https://openairdocs.org/stc/SA4132NM): Installation of Raisbeck Mark VIII wing lockers.. Raisbeck Engineering Inc.
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc.
- [STC SA02133SE](https://openairdocs.org/stc/SA02133SE): Installation of a Luma Technologies LT-4500 Series Integrated Light\Emitting Diode (LED) Display Panel and LT-3500 LED light modules. Luma Technologies LLC
- [STC SA12345IB](https://openairdocs.org/stc/SA12345IB): Replacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC SA01638WI](https://openairdocs.org/stc/SA01638WI): Part Fabrication and Installation of Arm Ledge System and Table Assembly for aircraft cabin interior. Aviation Fabricators Inc.
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc.
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS  (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc.
- [STC SA9210SC-D](https://openairdocs.org/stc/SA9210SC-D): Installation of the L-3 Communications Avionics Systems Infrared Imaging System (IRIS). Acron Aviation Inc.
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc.
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc.
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft.. Michelin North America Inc.
- [STC SA01800CH](https://openairdocs.org/stc/SA01800CH): Installation of Butterfield Industries Oil Residue Collection System, kit Part Number BI 2001-1. Raisbeck Engineering Inc.
- [STC SA02215SE](https://openairdocs.org/stc/SA02215SE): Fabrication of Inspection Panel Kit BI 9501-001. Raisbeck Engineering Inc.
- [STC SA3683NM](https://openairdocs.org/stc/SA3683NM): Installation of exhaust stack fairings.. Raisbeck Engineering Inc.
- [STC SA4130NM](https://openairdocs.org/stc/SA4130NM): Installation of lower aft fuselage strakes.. Raisbeck Engineering Inc.
- [STC SA4131NM](https://openairdocs.org/stc/SA4131NM): Installation of Hartzell/Raisbeck Quiet Turbofan Propeller. Raisbeck Engineering Inc.
- [STC SA4944NM](https://openairdocs.org/stc/SA4944NM): Installation of fully enclosed main landing gear door system for high-flotation-gear-equipped aircraft. Raisbeck Engineering Inc.
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA00741WI](https://openairdocs.org/stc/SA00741WI): Installation of the Concorde RG-380E/K series VRSLA batteries in airplanes listed on the attached FAA approved Model List (AML). Aero-Mach Wilco LLC
- [STC SA1242GL](https://openairdocs.org/stc/SA1242GL): Replace existing nose wheel with Cleveland nose wheel P/N 40-204by installing Parker Hannifin conversion kit 199-126.. KAMAN Corporation Aircraft Wheel and Brake LLC
- [STC SA1510GL](https://openairdocs.org/stc/SA1510GL): Installation of Cleveland Main wheels and brakes.. KAMAN Corporation Aircraft Wheel  Brake LLC
- [STC SA650GL](https://openairdocs.org/stc/SA650GL): Installation of Cleveland brake conversion kit 199-110.. KAMAN Corporation Aircraft Wheel and Brake LLC
- [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc.
- [STC SA00186LA](https://openairdocs.org/stc/SA00186LA): Installation of Alternate Main Landing Gear Tires, Michelin P/N 026-335-0.. Metrea Special Aerospace ISR Inc.
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC SA04634NY](https://openairdocs.org/stc/SA04634NY): Modification of the Brake Master Cylinder. Marsh Brothers Aviation Inc
- [STC SA01672WI](https://openairdocs.org/stc/SA01672WI): Installation of Window Shade Assembly as the replacement for OEM polarized window assemblies. Aviation Fabricators Inc
- [STC SA04062NY](https://openairdocs.org/stc/SA04062NY): Installation of Garmin G600 Avionics System. airplus engineering GmbH
- [STC SA01748WI](https://openairdocs.org/stc/SA01748WI): Installation of Cabin LED Downwash Lighting. PWI Inc.
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA09760DS](https://openairdocs.org/stc/SA09760DS): Installation of an S-TEC 01326 Digital Flight Control System (DFCS). S-TEC Corporation
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA00273WI](https://openairdocs.org/stc/SA00273WI): Installation of Stretcher, Patient Loading, and Support system.. Lifeport Inc
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit.. Med-Pac Inc.
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA01867WI](https://openairdocs.org/stc/SA01867WI): CoolView Flight Compartment Side and Storm Windows Installation.  See attached AML No. SA01867WI for required data.. Lee Aerospace, Inc.
- [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc.
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA02673LA](https://openairdocs.org/stc/SA02673LA): Automatic Dependent Surveillance  Broadcast (ADS-B) Out Integration. Universal Avionics Systems Corp

All 195: https://openairdocs.org/tcds/A31CE/stcs.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.