# TCDS A28CE: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 14
- Revised: April 19, 2024
- Product: Aircraft, Small Airplane
- Certification basis: Part 23, Part 25
- Registered aircraft: 172, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/45/78/4578b295a41511cd458f0fa2633ab69bf6be9465ea789bd78c6307abd792adaa
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188613060720240422132904.0001
- Page: https://openairdocs.org/tcds/A28CE

## Models (1)

As the data sheet lists them.

- 441

## 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. 14 11 10 14 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
 A28CE  
 Revision 14  
Textron Aviation  
 441  
April 19, 2024  
 
TYPE CERTIFICATE DATA SHEET NO. A28CE 
 
This data sheet which is part of Type Certificate No. A28CE 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, Kansas 67215 
 
Type Certificate Holder Record Cessna Aircraft Company transferred to 
   Textron Aviation Inc. on July 29, 2015 
 
I. Model 441, Conquest (Normal Ca tegory), Approved August 19, 1977 
 
 Engines  Two Garrett Turbine Engine  Company TPE331-8 Series Turboprops: 
 
   S/N 441-0001 through 441-0339 
    TPE331-8-401S 
    TPE331-8-402S 
    TPE331-8-403S 
    TPE331-8-404S 
 
   Engines may be interchanged in any combination. 
 
   S/N 441-0340 and On 
    TPE331-8-406S  
 
 Fuel  Aviation turbine fuel ASTM D-1655, Jet A,  Jet A-1 or Jet B; MIL-T-5624, JP-4 or Jp-5.  
   Anti-icing additive per MIL-I-27686D, MI L-T-2768E, or Phillips PFA 55MB must be  
   blended into the aircraft fuel in concen trations not less than 0.060% by volume.  For  
   emergency use of aviation gasoline and fueling procedures, refer to FAA Approved  
   Airplane Flight Manual (AFM). 
 
 Engine Limits  Static sea level ratings 
 
 Shaft 
Horse 
Power 
Gas Gen. 
Speed  
 
(% R.P.M.) 
Indicated 
Torque  
 
(Ft.-lbs.) 
Prop 
Shaft 
Speed  
(R.P.M.) 
Exhaust 
Gas 
Temp. 
(Deg. C) 
Takeoff (5 min) Static 635.5 100 1669 2000 450° 
Max. Continuous 635.5 100 1669 2000 450° 
Starting Limit -- -- -- -- 770° 
   Note: During manual mode operation, refer to OAT gage and AFM for EGT limits.

A28CE 2 Rev. 14  
I. Model 441  (cont’d) 
  
 Propeller and  Two three-bladed fu ll-feathering, reversible propellers: 
  Propeller Limits 1. Manufacturer:  Hartzell 
    Compatible Engines:  TPE331-8-401S or 402S 
    Hub:  Hartzell HC-B3TN-5 
    Blade:  Hartzell T10178B-11 
    Diameter:  not over 90.0 inches, not under 88.5 inches; no further reduction  
    permitted 
    Pitch at 30-inch station: 
    Start locks + 2.0° 
    Flight idle +10.0° 
    Feathered +87.4° 
    Reverse - 8.0° 
 
   2. Manufacturer:  Mc Cauley Accessory Division 
    Compatible Engines:  TPE331-8-403S, 404S, or 406S 
    Hub:  McCauley 3GFR34C601 
    Blade:  McCauley 93JA-3 
    Diameter:  Not over 90.0 inches, not under 88.5 inches; no further reduction  
     permitted 
    Pitch at 30-inch station: 
     Start locks + 2.0° 
     Flight idle + 8.5° 
     Feathered +85.3° 
     Reverse - 8.0° 
 
   Note:  Either two McCauley or two Hartzell Propellers are required. 
 
 Airspeed Limits V MO (Maximum operating) 245 knots 
  (IAS)   Sea level to 21,300 ft. 
   M MO Above 21,300 ft. .55 mach 
   V A  (Maneuvering) 167 knots 
   V FE (Flaps extended) 
    30° (Landing) 180 knots 
    20° (Approach) 200 knots 
    10° (Takeoff) 200 knots 
   V MCA (Minimum control speed) Air 91 knots 
   V LO (Landing gear operating) 180 knots 
   V LE (Landing gear extended) 180 knots 
 
 C.G. Range (Landing (+167.63 in.) to (+178.07 in.) at 6,800 lbs. (12% to 28.5% MAC) 
  Gear Extended) (+173.35 in.) to (+178.07 in.) at 9,850 lbs. (21% to 28.5% MAC) 
   Variation is linear between points 
   Landing gear retracting moment (+1113 in.-lbs.) 
 
 Empty Wt. C.G. Range None 
 
 Datum  100.0 in. forward of the front face of the forward pressure bulkhead which is sta. +100.0 
 
 Leveling Means Seat rails over main spar (lateral) 
   Leveling screws, R.H. fuselage (longitudinal) 
 
 Maximum Weight Takeoff 9,850 lbs. 
   Landing 9,360 lbs. 
   Zero fuel 8,500 lbs. 
   Ramp 9,925 lbs. 
 
 No. of Seats  1 through 11 (2 at +137.0, 2 at +178. 0, 2 at +209.0, 2 at +249.0, 1 at +285.0, 2 at  
   +296.0) 
   See Manufacturer's Equipment Li st for other seating arrangements

Rev. 14 3 A28CE 
I. Model 441  (cont’d) 
  
 Maximum Baggage Nose compartment: 250 lbs. Sta. + 32.0 
    350 lbs. Sta. + 71.0 
   Aft cabin: 400 lbs. Sta. +281.0 
    400 lbs. Sta. +301.0 
    100 lbs. Sta. +317.0 
 
 Fuel Quantity  3227 lbs. (481. 5 gal.) total in two wing tanks 
   1613.5 lbs. (240.75 gal.) each 
   3183 lbs. (475 gal.) usable total, 1591.5 lbs. (237.5 gal.) in each tank at sta. +181.9.  Fuel  
   weight based on 6.70 lbs./gal. 
   (See NOTE 1 for data on unusable fuel) 
 
 Oil Capacity  3.75 gal. total, 3. 75 gal. usable (1.88 gal. in ea. engine mounted tank at sta. +116.0) 
   (See NOTE 1 for undrainable oil) 
 
 Maximum Operating 33,000 ft. S/N 441-0001 through -0172 (See NOTE 4) 
  Altitude  35,000 ft. S/N 441-0173 and On 
 
 Control Surface Elevator (horn faired) Up 25° Down 15° 
  Movements  Elevator trim tabs Up 4° Down 9° 
   Rudder (perpendicular to Right 32° Left 32° 
    hinge 0° faired with fin) 
   Rudder trim tab Right 11° Left 16° 
    (perpendicular to hinge) 
   Aileron Up 25° Down 15° 
   Aileron trim tab Up 19° from Down 19° from 
      neutral  neutral 
   Wing flap (inboard)   Down 0° to 30° 
   Wing flap (outboard)   Down 0° to 20° 
 
 Serial Nos. Eligible 698 and 441-0001 through 441-0362 
 
Certification Basis:   
Part 23 of the Federal Aviation Regulations (FAR) effective February 1, 1965, as amended by 23-1 through 23-14 except FAR 
23.1385(c) as amended through 23-21; plus Special Conditions 23-74-CE-9; Part 36 of the FAR effective December 1, 1969, as 
amended by 36-1 through 36-6; SFAR 27, fuel venting.  Findings of Equivalent Level of Safety (ELOS) were made for FAR 
23.1189(a), 23.1545, and 23.1583(a). 
 
In addition to the above certification basis, compliance with ice protection has been demonstrated in accordance with FAR 
23.1419 of Amendment 23-14 effective December 20, 1973. 
 
S/N 441-0173 and On 
In addition to the above, certification basis compliance with FAR 25.1447(c)(2) as amended through 25-41 effective September 
1, 1977, is required. 
 
Application for Type Certificate dated October 30, 1974.  Type Certificate No. A28CE issued August 19, 1977, obtained by the 
manufacturer under Delegation Option Procedures. 
 
Production Basis  
Production Certificate No. 312 issued and Delegation Option Manufacturer No. CE-3 authorized to issue airworthiness 
certificates under delegation option provisions of Part 21 of the FAR.  Effective February 15, 1985, and on, Production 
Certificate No. 4 is applicable to all spares production.  See NOTE 6 for specific effectivity of P.C. 4 on new airplane serials.

A28CE 4 Rev. 14  
Equipment:  
Pilot’s Operating Handbook (POH) and FAA Approved AFM required as follows: 
 
 
 
 
 *Or later approved revisions. 
 
The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed 
in the aircraft for certification.  In addition, the following item of equipment is required: 
 
Stall Warning Indicator - Cessna Dwg. 5818008, or as modified by CBQ-34-01, or 
Angle-of-Attack Indicator System - Cessna Dwg. 0800302 
 
NOTE 1. Current weight and ba lance report together with 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. 
 
 The certified empty weight and corresponding center of gravity location must include undrainable oil (not 
included in oil capacity) and unusable fuel as follows: 
 
(a) Fuel  44.0 lbs. (6.5  gal.) at (sta.+186.7) 
(b) Oil   0.0 lbs. 
 
NOTE 2. The placards specified in the FAA Approved AFM must be displayed. 
 
NOTE 3. Service information: 
 
 The airplane maintenance manual contains structural retirement lives, which may not be changed without 
FAA Engineering approval for the following components: 
 
 
 
 
 
 
 
 
NOTE 4. 35,000 ft. S/N 441-0001 through -0172 when modified by SK441-36. 
 
NOTE 5. Model 441 aircraft in compliance with Cessna Drawing 5700018 are eligible for certification in the 
Netherlands. 
 
NOTE 6. Production Certificate No. 4 effective at S/N 441-0347 and On. 
 
 
--- END --- 
Airplane S/N Effectivity POH/AFM Part Numbe r* 
441-0001 through 441-0172 D1561-14-13PH 
441-0173 and On D1586-11-13PH 
 Part Numbers Hours Air plane S/N 
Aileron Hinge 
Bracket 
5824400-3 
5824400-4 
5824400-5 
5824400-6 
5824400-7 
10,000 441-0001 through 441-0362
```

## ADs (28, 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 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009
- [AD 2005-20-25](https://openairdocs.org/ad/2005-20-25): Avionics bus circuit breaker switches · Cessna 401, 401A, 401B and 15 more. Effective Nov 9, 2005
- [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 2003-09-09 R1](https://openairdocs.org/ad/2003-09-09-R1): Fuel pump boost wiring · Cessna 441 and F406. Effective Jan 22, 2004
- [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 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001
- [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 98-04-28](https://openairdocs.org/ad/98-04-28): AFM - Limitations Section - Icing · Cessna 310R, 335, 340A and 12 more. Effective Mar 13, 1998
- [AD 97-25-04](https://openairdocs.org/ad/97-25-04): Airplane Flight Manual (AFM) - Limitations - Power Levers · Cessna 208, 208A, 208B and 2 more. Effective Jan 21, 1998
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 95-25-10](https://openairdocs.org/ad/95-25-10): Outflow/Safety Valve · Cessna 441, 500, 550 and 1 more. Effective Jan 22, 1996
- [AD 92-16-18](https://openairdocs.org/ad/92-16-18): Passenger Seat Reinforcement · Cessna 401, 402, 402A and 9 more. Effective Sep 10, 1992
- [AD 92-16-07](https://openairdocs.org/ad/92-16-07): Horizontal Stabilizer Front Spar · Cessna 441. Effective Aug 30, 1992
- [AD 86-24-13](https://openairdocs.org/ad/86-24-13): POH/AFM Appendix - Icing · Cessna 441. Effective Dec 15, 1986
- [AD 85-25-11](https://openairdocs.org/ad/85-25-11): Nuts - Cessna P/N NAS1291-8 · Cessna 425 and 441. Effective Feb 12, 1986
- [AD 84-20-02](https://openairdocs.org/ad/84-20-02): Nose Landing Gear · Cessna 402C, 404, 414A and 3 more. Effective Nov 1, 1984
- [AD 83-12-03](https://openairdocs.org/ad/83-12-03): Battery Switch Wiring · Cessna 441. Effective Jun 28, 1983
- [AD 80-02-17](https://openairdocs.org/ad/80-02-17): Flight Manual Performance Data · Cessna 441. Effective Jan 29, 1980
- [AD 79-19-13](https://openairdocs.org/ad/79-19-13): Elevator Trim Tab · Cessna 441. Effective Dec 26, 1979
- [AD 79-19-12](https://openairdocs.org/ad/79-19-12): Engine Stoppage · Cessna 441. Effective Oct 1, 1979
- [AD 79-09-02](https://openairdocs.org/ad/79-09-02): Aileron Control Surfaces Drainage · Cessna 441. Effective May 7, 1979
- [AD 79-08-07](https://openairdocs.org/ad/79-08-07): Anti-Icing Propeller Wiring · Cessna 441. Effective Apr 30, 1979
- [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008
- [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008
- [AD 2003-09-09](https://openairdocs.org/ad/2003-09-09) (historical): Fuel Boost Pump Wiring · Cessna Aircraft Company, The 441 and F406. Effective Jun 24, 2003
- [AD 2002-09-13](https://openairdocs.org/ad/2002-09-13) (historical): Wire Harness and Fuel Boost Pump Lead Wires · Cessna Aircraft Company, The 441. Effective May 31, 2002

## Registered aircraft by registry model (OpenAirDocs)

- [Cessna 441](https://openairdocs.org/model/cessna-441): 172 aircraft (registry code 2076020)

## STCs approved under this data sheet (180, 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 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 SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc.
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners 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 SA118CH](https://openairdocs.org/stc/SA118CH): Installation of TCAS I. Acron Aviation Inc.
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [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 SA00940DE](https://openairdocs.org/stc/SA00940DE): Activation of previously approved Static Source Error Correction (SSEC) software used with the Garmin GSU 75B ADAHRS. West Star Aviation LLC
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [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 SA2496CE](https://openairdocs.org/stc/SA2496CE): Modify the battery compartment and replace the nickel cadmium batteries with Concorde RG 380E lead acid batteries.. Aero-Mach Wilco LLC
- [STC SA644GL](https://openairdocs.org/stc/SA644GL): Wheels and brakes installation199-115 conversion kit.. 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 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 SA04460NY](https://openairdocs.org/stc/SA04460NY): Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-E-C-F-R(G)/CFR210-58( ) or /CFR224-55. MT- Propeller Entwicklung GmbH
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA2057CE-D](https://openairdocs.org/stc/SA2057CE-D): ONE ONLY STC, SN 441-0001: Installation of King KNS 660 Multi-Sensor Flight Management System. Honeywell International 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 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 SA8833SW](https://openairdocs.org/stc/SA8833SW): Installation of a fuselage nose radome shell. The NORDAM Group LLC
- [STC SA02636AT](https://openairdocs.org/stc/SA02636AT): Installation of a Strobe Light System. Reds Aircraft Service Inc.
- [STC SA02669AT](https://openairdocs.org/stc/SA02669AT): Installation choice of magnetic chip detection system part number RAA2002-2-1CL. Reds Aircraft Service Inc.
- [STC SA02863AT](https://openairdocs.org/stc/SA02863AT): Installation of Royal Atlantic Aviation high intensity discharge Landing Light and Recognition Light System. Reds Aircraft Service Inc.
- [STC SA02913AT](https://openairdocs.org/stc/SA02913AT): Installation of a windshield anti-icing system manual control valve. Reds Aircraft Service Inc.
- [STC SA02946AT](https://openairdocs.org/stc/SA02946AT): Installation of a Pitot Heat System Cockpit Indicator Lights. Reds Aircraft Service Inc.
- [STC SA03040AT](https://openairdocs.org/stc/SA03040AT): Royal Atlantic Aviation Engine Oil Filter Bypass Warning System, Kit P/N RAA2003-1-1. Reds Aircraft Service Inc.
- [STC SA00571SE](https://openairdocs.org/stc/SA00571SE): Replacement of certain BF Goodrich pneumatic deicer boots.. SMR Technologies Inc
- [STC SA02935CH](https://openairdocs.org/stc/SA02935CH): Install air ambulance conversion in accordance with Spectrum Aeromed Master Drawing List 6078DL, No Revision, dated February 16, 2010, or later FAA approved revisions.. Spectrum Aeromed LLC dba Spectrum Aeromed
- [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 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 SA04228CH](https://openairdocs.org/stc/SA04228CH): Installation of an Electronics International MVP-50T Engine Monitoring System. Carpenter Avionics, Inc
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA01935LA](https://openairdocs.org/stc/SA01935LA): Installation of external aft body strakes.. Aircraft Performance Modifications
- [STC ST00366WI](https://openairdocs.org/stc/ST00366WI): Installation of Keddeg Company P/N 21BC115 Coalescer Assembly. Purolator Facet, Inc
- [STC SA1494NM](https://openairdocs.org/stc/SA1494NM): Installation of a cargo door.. Textron Aviation Inc
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation

All 180: https://openairdocs.org/tcds/A28CE/stcs.md

---
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