# TCDS A29CE: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 9
- Revised: November 27, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23, Part 36
- Registered aircraft: 151, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/ab/66/ab6672a748666860c0bb3b0189bb9f6d39852511e57ff48387f643c896be8168
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3ED26978567EF1EF862581EF0060D22F.0001
- Page: https://openairdocs.org/tcds/A29CE

## Models (1)

As the data sheet lists them.

- 76

## 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 
Rev. No. 9 4 4 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
A29CE 
Revision 9 
Textron Aviation 
76 
November 27, 2017 
 
TYPE CERTIFICATE DATA SHEET NO. A29CE 
 
This data sheet which is part of Type Certificate No. A29CE 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 76, Duchess, 4 PCLM (Normal Category), Approved January 24, 1978 
 
 Engine Left:  Lycoming O-360-A1G6D 
  Right: Lycoming LO-360-A1G6D 
 
 Fuel 100/130 minimum grade aviation fuel or 100 low lead (blue) 
 
 Oil  1st 50 hours MIL-L-6082C; thereafter MIL-L-22851 
   
 Engine Limits For all operations, 2700 rpm (180 hp.) 
 
 Propeller and  (a) Hartzell constant speed propeller: 
   Propeller Limits   Left:   HC-M2YR-2CEUF/FC7666A, 2 blades aluminum alloy  
    Right:   HC-M2YR-2CLEUF/FJC77666A, 2 blades aluminum alloy 
   Diameter:  76 in. nominal.   
    Minimum allowed for repair 74 in., no further reduction permitted. 
   Pitch setting at 30 in. station: 
    low 12.1° +0.1°, high 17° to 20°, feather 80° to 82° 
  (b) Woodward hydraulic governor L210652 and R210652 
  (c) Hartzell spinner assembly C2285-3P and C2285-3PL 
 
 Airspeed Limits Never exceed 194 knots (223 mph) 
   (IAS) Maximum structural cruising 154 knots (177 mph) 
  Maneuvering 132 knots (152 mph) 
  Flaps extended (35°) 110 knots (127 mph) 
     (20°) 120 knots (138 mph) 
     (15°) 140 knots (161 mph) 
  Maximum landing gear extension  140 knots (161 mph) 
  Maximum landing gear retraction  113 knots (130 mph)

Rev. 9 2 A29CE 
 
I. Model 76  (cont’d) 
 
 C.G. Range (Landing Normal Category 
   Gear Extended) (+110.6) to (+117.5) at 3900 lb. 
  (+106.6) to (+117.5) at 3250 lb. and less  
  Straight line variation between points given 
  Landing gear retraction moment (-1177 in.-lb.) 
 
 Empty Wt. C.G. Range None 
 
 Leveling Means Baggage compartment floor 
 
 Maximum Weight Ramp 3,916 lb. 
  Takeoff 3,900 lb. 
  Landing 3,900 lb. 
  Zero fuel 3,500 lb. 
 
 No. of Seats 4 maximum (2 at +105 forward or +112 aft position, 2 at +142 standard or +144 
  optional) 
 
 Maximum Baggage 200 lb. (+167.0) 
 
 Fuel Capacity Tank Capacity Gal. Usable Gal. Arm 
  L&R main 103 100 +117.0 
  See NOTE 1 for data on unusable fuel. 
 
 Oil Capacity 20 qt. (+75.4) 
  See NOTE 1 for undrainable oil 
 
 Control Surface Movements Wing flaps   Down 35 1 
   Up 20  1 Down 15 1 
  Rudder Right 30  1 Left 30 1 
  Elevator Up 20  +1, -0 Down 15 +1, -0 
  Rudder tab Right 20  1 Left 20  1 
  Elevator tab Up   4  1/2 Down 20  1/2 
    (with elevator neutral) 
   
 Serial Nos. Eligible ME-2 and on  
 
 Datum 103 in. forward of wing leading edge (constant chord section) 
 
 Certification Basis Part 23 of the Federal Aviation Regulations (FAR) effective February 1, 1965, as 
amended by 23-1 through 23-16 and FAR 36 effective June 1974, Amendment 36-1 
through 36-10.  Equivalent safety findings:  FAR 23.621 (S/N ME-2 through ME-437 
only), 23.1545, 23.1583(a). 
 
  One-engine inoperative stall characteristics tests identified in FAA letter to Beech dated 
May 27, 1976. 
 
  Application for Type Certificate dated October 24, 1975. 
  Type Certificate A29CE issued January 24, 1978, 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. 9 3 A29CE 
I. Model 76  (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 item of equipment is required: 
 
 1. Pilot's Operating Handbook (POH) and FAA Approved Airplane Flight Manual 
(AFM) (P/N 105-590000-5) dated January 1978, revised March 1979, or later. 
 
 
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 20 lb. at +123.2, with 1.6 lb. at +124.8 being undrainable.  
 
  (b) Basic empty weight includes engine oil of 37 lb. at +75.4, with 7.3 lb. being undrainable. 
 
NOTE 2. All placards required in the POH and FAA Approved AFM must be installed in the appropriate locations. 
 
NOTE 3. Mandatory retirement times for all structural components are contained in the AFM (P/N 105-590000-5) 
Limitations Section.  These limitations may not be changed without FAA Approval. 
 
 
 
 
---- END ----
```

## ADs (17, 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 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2021-08-06](https://openairdocs.org/ad/2021-08-06): Landing Gear · Textron 76. Effective May 25, 2021
- [AD 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 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 2004-21-05](https://openairdocs.org/ad/2004-21-05): B-Seires Combustion Heaters · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 41 more. Effective Nov 19, 2004
- [AD 99-05-13 R1 WD](https://openairdocs.org/ad/99-05-13-R1-WD): Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Jul 5, 2000
- [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996
- [AD 80-19-12 R1](https://openairdocs.org/ad/80-19-12-R1): Engine Mount Structure · Textron 76. Effective Jun 14, 1982
- [AD 82-02-03](https://openairdocs.org/ad/82-02-03): Elevator Control Cable · Textron 76. Effective Feb 14, 1982
- [AD 80-07-06](https://openairdocs.org/ad/80-07-06): Rudder and Rudder Trim Tab · Textron 76 and 77. Effective Apr 3, 1980
- [AD 79-23-06](https://openairdocs.org/ad/79-23-06): Replacing Stop Bolt Nuts · Textron 76. Effective Nov 23, 1979
- [AD 79-17-06](https://openairdocs.org/ad/79-17-06): Main Landing Gear Clevis Pin · Textron 76. Effective Aug 27, 1979
- [AD 79-09-04](https://openairdocs.org/ad/79-09-04): Engine Starter Relay Failures · Textron 76. Effective May 7, 1979
- [AD 78-20-08](https://openairdocs.org/ad/78-20-08): Trim Tab Push Rods · Textron 76. Effective Oct 12, 1978
- [AD 99-05-13](https://openairdocs.org/ad/99-05-13) (historical): Fuel Tank Selector · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Apr 19, 1999
- [AD 97-06-10](https://openairdocs.org/ad/97-06-10) (historical): Main Landing Gear "A" Frame Assembly · Hawker Textron 76. Effective May 16, 1997

## Registered aircraft by registry model (OpenAirDocs)

- [Beech 76](https://openairdocs.org/model/beech-76): 151 aircraft (registry code 1153005)

## STCs approved under this data sheet (166, 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 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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc.
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International 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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES 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 SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC
- [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 SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels 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 SA5902NM](https://openairdocs.org/stc/SA5902NM): Installation of locking fuel cap assembly. CheckSix AeroSolutions, LLC
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [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 SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. 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 SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc.
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. 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 SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc.
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA1455CE](https://openairdocs.org/stc/SA1455CE): Installation of KFC200 flight control system (2 axis).. Honeywell International Inc
- [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System.. Honeywell International 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 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [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 SA01828SE](https://openairdocs.org/stc/SA01828SE): Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System. J. P. Instruments
- [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine
- [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 SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [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 SA01114CH](https://openairdocs.org/stc/SA01114CH): Installation of P2 Incorporated 6600 Audio Advisory system. P2 Incorporated
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC 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 166: https://openairdocs.org/tcds/A29CE/stcs.md

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