Beechcraft 36 B36TC

Number of Active Aircraft: 244 Active- Map

Description:

The Beechcraft Model 36 came about due to the successful production models Cessna and Piper had put out for the heavier single engine market. Thos aircraft being the Cessna 206 and Piper Cherokee Six lines. The Model 36 was there awnser. As the model 35 Bonanza had always been a true four place aircraft with the later models incorporating small seats in the back to bring it up to six seats. The Model 36 Bonanza would be a true six place aircraft. By taking a E model 35 and adjusting the wing position on it was possible to load six people while still maintaing CG tolerance. The first aircraft was introduced in 1968. It wasnt until the 1970 model which was the A36 Bonanza when Beechcraft really made it luxurious aircraft that it took off.

The B36TC has minor modifications from the A model, but some of those modifications included a longer wing as well as range, and an improved takeoff weight.

A Great Bonanza Guide1013
Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 2338 lbs
Max Weight 3850 lbs
Useful Load: 1512 lbs
Engine Name Continental TSIO-520-UB
Engine Number 1
Horsepower 300 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 25000 ft
Max Fuel 102 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 195 kts
GPH (75% BHP): 16.8
MPG (75% BHP) 11.6
Range (75% BHP): 1063 nm
Fuel Cost Per Seat Mile 0.09 $
Fuel Cost Per Hour 100.8 $
MPG per 1000 lbs of Payload 17.55
F-T (Speed^2/FuelBurn) 22.6 HP
F-T Payload 34.2 kts
MPH To HP: 6.5 kts
T/O Roll - T/O over 50 FT OBST 1156 ft / 2364 ft

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. Amended 10/3/2012
SA00035DE Installation of modified engine baffle/cooling louver system. Reissued 10/16/1998
SA00044LA Installation of replacement rudder hinge brackets. Reissued 2/6/2001
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00063LA Installation of Acoustical/Thermal insulation. Reissued 1/5/2005
SA00066WI Installation of global positioning system GPS 150. Issued 5/24/1993
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00068WI Installation of a stretcher on the seat rail. Issued 5/25/1993
SA00070SE Fabrication of Model RD-0050replacement wing-tip position light lens covers. Issued 4/4/1994
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. Amended 10/31/2012
SA00080BO Installation of BB-145 NAV-COMM antenna. Issued 1/21/1998
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00143LA Installation of control yoke retainer lock. Issued 8/2/1996
SA00161BO (3 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00193WI-D Installation of Bendix/King KLN 90A Global Positioning System (GPS). For model F33A approved for serial numbers CE-772 and higher. For model A36 serial numbers E-1241 and higher. Reissued 2/28/2000
SA00195AT Installation of carbon steel brake discs. Reissued 11/14/1994
SA00199SE Modification of Beech 35-950116and/or 35-950118 exhaust stack assemblies by adding a slip joint to the middle riser of each exhaust stack assembly. Amended 10/19/1995
SA00203NY Installation of .312-inch .375-inch or .500-inch thick replacement windshields. Issued 7/15/1994
SA00204NY Installation of .250 inch .312 inch or .375 inch thick one piece windshields (two piece windshield to one piece windshield conversion). Reissued 5/7/1997
SA00206AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00224SE Modification of Beech exhaust stack assemblies. Issued 8/25/1995
SA00238SE Installation of Aviation Development Corporation s sump mounted chip detector Issued 10/31/1995
SA00242WI-D Installation of Bendix/King KLN 90B Global Positioning System (GPS) for IFR enroute and approach operation. For model F33A serial number CE-772 and above model A36 serial number E-1241 and above A36TC and B36TC all serial numbers. Reissued 11/3/2000
SA00243BO (4 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00245SE Installation of the Aviation Research Systems Inc. Locking Fuel Caps Reissued 10/23/2003
SA00257BO S/Ns E-111 E-1241 and up ONLY: Installation of air conditioning system. Issued 7/20/2007
SA00269BO (3 OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO ( PAGE 2) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010 0:00
SA00304BO Installation of Approach Aviation Issued 12/23/2010
SA00331BO Installation of Avidyne Corporation Autopilot Issued 5/10/2013
SA00352LA Installation of Aero Sound Shield Acoustical Firewall Blanket Part No. AS-0500. Reissued 1/5/2005
SA00353WI Installation of a modification kit for cold weather operation. Reissued 5/29/2007
SA00358DE Installation of radio telephone system. Issued 10/22/1998
SA00368CH Installation of cooling air baffles Amended 3/27/2008
SA00391NY Installation of second wind auxiliary vacuum system. Reissued 6/18/2002
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00423SE Installation of stainless steel battery box. Reissued 10/23/2003
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00462AT Replacement of Appalachian stainless steel brake discs P/N 75-23 with Appalachian steel brake disk part number AA-47. Reissued 12/7/1994
SA00469NY Installation of Main Landing Gear Auxiliary Landing Lights. Reissued 2/27/2006
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00481AT-D Installation and operation of a United Beechcraft Keyless Entry System. Reissued 4/10/1995
SA00521AT-D Installation of replacement fuel cell assemblies  Reissued 4/16/2009
SA00522AT-D Installation of replacement fuel cell assemblies Reissued 5/5/2009
SA00532NY Installation of Avcheck Corp. Comcheck 422A Radio Reception Indicator. Issued 12/10/1996
SA00557AT Installation of carbon steel brake discs. Reissued 1/24/1995
SA00581CH Installation of a Bendix/King EFS 40 Two Tube EFIS. Issued 11/25/1996
SA00609DE Installation of a nose whell shimmy damper Issued 12/3/2007
SA00625LA Installation of a Concorde Battery Model no RG-35 or RG-35XC. Issued 4/27/1998
SA00638WI Installation of Concorde Battery Corporation (vrsla) Valve Regulated Sealed Acid Battery. Amended 8/10/2012
SA00639SE Installation of Turbine Outlet Temperature Indicator in accordance with Soloy Master Drawing List 887-101 Revision - dated July 30 1998 or later FAA approved revision. This STC is only applicable to aircraft that have been modified in accordance with Soloy STC SA3523NM. Reissued 12/2/2004
SA00667WI-D Installation of Bendix/King KFC 225 Automatic Flight Control System. For model A36 S/N E-1946 E-2104 E-2111 and after. For model B36TC S/N EA-320 EA-389 and after Reissued 2/28/2000
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680NY Installation of Dorsal Fin. Issued 8/14/1997
SA00681NY Installation of tail cone. Issued 8/14/1997
SA00690CH Installation of Great Lakes Aero Products Pilot Side and Door Windows. Amended 2/18/1999
SA00696LA Installation of Sandel Avionics SN3308 Navigation Display. Issued 10/20/1998
SA00697LA Installation of Avionics Innovations Compact Disc Shuttle Inflight Entertainment System. Issued 10/20/1998
SA00718CH Installation of McCauley Propeller Model 3A36C434/80VEA-0. Reissued 9/21/2005
SA00718LA Installation of a Hartzell PHC-C3YF-1RF/F8468A(B K)-8R constant speed propeller. Reissued 2/5/1999
SA00719LA Installation of a Hartzell PHC-C3YF-1RF/F8468A(B K)-6R constant speed propeller. Amended 5/25/2005
SA00724WI Installation of B&C Specialty products BC410-1 Standby Alternator Amended 6/26/2000
SA00735LA Installation of Teledyne Continental Motors O-470-M engine modified by STC SE00736LA in accordance with Michael Adamson Installation Instructions Beech Model 35-A33 Manual #l Revision N/C dated January 4 1999 or later FAA approved revisions. Michael Adamson Airplane Flight Manual Supplement #1 dated February 23 1999 or later FAA approved revision is required with this installation. (Raytheon 35-A33 Serial Number CD-334) Issued 3/19/1999
SA00749AT Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) Amended 12/10/1997
SA00780SE (PAGE 2) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00785SE Installation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics Drawing Package MA2125 Revision IR dated January 18 2000 and Installation Manual MA2126 Revision IR dated January 21 2000 or later FAA approved revisions. Issued 2/29/2000
SA00789LA Installation of Clear View Sunvisor. Amended 11/2/2001
SA00803SE Installation of vortex generators on wings and tail surfaces. Amended 11/7/2008
SA00839WI Front spar failsafe strap. Amended 7/18/2002
SA00849WI Installation of a dual Garmin GNS-430 communications transceiver/VOR/ILS receiver/GPS receiver with single Garmin GI-106A course deviation indicator Mid-Continent Instruments MD41-1468 GPS Annunicator Ps Engineering PMA7000M-S Audio Panel Shadin ADC- 200 Fuel/Air Data Computer and BF Goodrich WX-500 Weather Mapping Sensor. Reissued 3/26/2007
SA00851WI Installation of a Dual Garmin GNS-430 Communications Transceiver/VOR/ILS receiver/GLS receiver with Single Garmin GI-106A course deviation indicator. Issued 2/9/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00874AT-D Installation and operation of a United Beechcraft keyless entry system. Reissued 10/20/2005
SA00899CH Installation of pneumatic luggage door strut on those models with an extended luggage door. Reissued 7/8/1998
SA00901NY Installation of a wing tip recognition lights. Reissued 2/27/2006
SA00902WI Replacement of original main landing gear doors with monolithic machined gear doors. Amended 12/1/2000
SA00911CH Installation of rudder fin cap/strobe fairing. Issued 7/8/1998
SA00954SE (2 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA00982WI Installation of Liese-2xV60 engine exhaust silencer system. This STC is not to be transferred since its issuance was IAW 14 CFR 21.29 and based upon a validation of German LBA EMZ No. 0724/534/534a/627/627a. Issued 8/20/2001
SA00984WI-D Installation of Bendix/King KMH 880 Multi-Hazard Awareness System/KTA 870 Traffic Advisory System and optional Bendix/King KMD 550 Multi-Function Display System. Approved for A36 serial numbers E-1946 E-2104 and E-2111 and for model B36TC serial number EA-320 EA-389 and after. Issued 7/18/2001
SA01010WI-D Installation of the Bendix/King KMH 880 Multi-Hazard Awareness System  Reissued 3/26/2007
SA01033WI Replacement of original outboard main landing gear doors with a one-piece monolithic machined metal door. Amended 1/22/2008
SA01075SE Installation of the Precise Flight Inc. SpeedBrake 2000 System.  Amended 7/19/2006
SA01077SE (PAGE 2) Installation of fluoropolymer film. Reissued 8/20/2003 0:00
SA01078NY Installation of Left and Right Side Windows. Issued 8/25/1999
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
SA01085SE Installation of BAS Inc. of Shoulder Harness per the appropriate BAS Report listed on FAA AML SA01085SE dated May 13 2002 or later FAA approved revision. Amended 12/2/2010
SA01091WI Increase gross weight of Model N35 and P35 Beech Bonanzas by 100 lbs.  Issued 7/10/2002
SA01105WI-D (1 OF 2) Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). Amended 5/31/2007
SA01110CH Installation of wing fuel tank quick valve drains. (Listed models with specific serial number applicability) Issued 9/27/1999
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
SA01116AT Install a freon air conditioning system. Issued 8/21/1996
SA01120SE Installation of Door Steward. Amended 3/4/2010
SA01126WI Replacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632 Issued 12/17/2002
SA01136WI  Installation of the TKS Ice Protection System for flight into known icing conditions. Data Required: );INSERT INTO stc_table VALUES ( 1) Aerospace Systems & Technologies (AS&T) Drawing List No. 10300DL Revision 3 dated February 25 2003 );INSERT INTO stc_table VALUES ( 2) Supplement to Pilot Amended 4/4/2011
SA01152CH Installation of stainless steel passenger step P/N 002-430076-23 with South Seas Ventures Inc. drawing as listed on AML No. SA01152CH or later FAA approved revision. Reissued 11/19/2001
SA01154CH Install McCauley 3A32C406/82NDB-4 propeller on Beech Model S35 V35 V35A or V35B aircraft equipped with Teledyne Continental Motors Model TSIO-520-D or TSIO-520-DB engines in accordance with D Reissued 6/17/2011
SA01155AT Installation of left hand and right hand auxiliary fuel cell assemblies  Reissued 4/27/2009
SA01156SE Installation of a Pratt & Whitney PT6A-21 engine flat rated at 500 HP 2200 RPM and a Hartzell HC-E4N-3N/D8292 propeller and associated hardware.  Amended 7/16/2007
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01158WI (2 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005 1:00
SA01165CH Install cooling air baffle on Raytheon (Beech) aircraft Model H35 J35 K35 M35 N35 and P35 or aircraft Model A35 B35 C35 D35 E35 F35 G35 H35 J35 K35 M35 35-33 35-A33 35-B33 35-C33 E33 and F33 which are modified by STC SA2660SW SA5635SW SA5527SW SA238GL SA893WE or SA2361SW to use Teledyne Continental Motors engine Models IO-470-C or IO-470-N in accordance with Castlegar Trust L. L. C. Installation manual as listed on AML No. SA01165CH or later FAA Approved revisions. Reissued 6/7/2011
SA01170NY Installation of NPX138N-XXX FM Transceiver. Amended 1/17/2007
SA01204AT Installation of left-hand side and right-hand side main fuel tank fuel cell assemblies. Reissued 4/29/2009
SA01205WI-D (2 OF 2) Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. );INSERT INTO stc_table VALUES (  Amended 11/20/2007
SA01224AT Installation of wheel hub cabs with valve stem access door. Amended 4/17/1998
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (3 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01330LA (PAGE 2) Installation of alternate avionics support assembly. Reissued 10/6/2010 0:00
SA01373NY Installation of landing lights IAW Arrow Light Company Adaptation and Installation Instructions and drawing number 2002-A-1 Rev IR dtd 7/10/01. Amended 4/27/2004
SA01422AT-D Installation of lower cabin door stiffener. Amended 2/10/1999
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01436AT Installation of alternator replacement of belt-driven generator in accordance with National AirParts Document Number NAPI-3533 Initial Release dated 12/29/96 or later FAA approved revisions. );INSERT INTO stc_table VALUES (  Reissued 6/24/2011
SA01436SE (2 OF 2) Cockpit sunvisor retrofit kit. Issued 8/2/2004 0:00
SA01455WI Modification to install a Honeywell KR 87 Automatic Direction Finder (ADF) System and the Honeywell KA 44B ADF Antenna interfaced with the previously installed Garmin 1000 Avionics System. Issued 10/15/2007
SA01473SE (5 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01548CH Installation of Hartzell Model PHC-(C L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Continental six-cylinder engines in accordance with D Reissued 6/17/2011
SA01560WI-D Installation of the Honeywell KFD 840 Primary Flight Display System. );INSERT INTO stc_table VALUES ( REQUIRED DATA: AML No. 159-08325-0002 Revision - dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. Amended 7/22/2010
SA01561CH Installation of Hartzell Model PHC-(C L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Teledyne Continental Motors six-cylinder engines in accordance with D Reissued 6/17/2011
SA01595SE Installation of the Garmin G1000 integrated avionics system including GFC700 Automated Flight Control. Reissued 3/26/2007
SA01595WI-D G1000 Integrated Avionics System Update with options Reissued 5/13/2013
SA01639NY Replacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B. Amended 6/1/2004
SA01655LA Installation of ignition switch. Reissued 4/1/2008
SA01668CH Installation of Hartzell Model PHC-(C L)3YF-1RF/F8068 three bladed propeller in accordance with D Reissued 3/21/2011
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01671WI Installation of interior configurations Amended 2/11/2013
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (4 OF 5) Installation of an antenna Amended 2/15/2007
SA01698LA Installation of interior sidewall/armrest panels per drawing DT1-1-02 Revision B dated December 6 2004 and later FAA approved revisions as listed on AML No. SA01698LA. Reissued 2/14/2005
SA01711CH Installation of Proscan Avionics FSM2000 Flight Systems Monitor. Issued 10/10/2002
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01725SE Installations of TAWS functionality  Reissued 8/14/2007
SA01727AT Installation of archangel avionics cockpit display system. Issued 12/3/1998
SA01770SE ONE-ONLY: Installation of a SAGEM Electronic Displays S/N EA-524 Issued 6/29/2007
SA01800SE (PG 3) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01807AT Installation of a Basic Type BAE 14/28 Model 2025 Air Driven Alternator. Issued 1/14/1999
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
SA01860NY (1 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 4)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01880CH Installation of a Three Point Torso Restraint System. Issued 9/5/2003
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (4 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01939CH Install Coller on the front landing gear strut. Issued 1/28/2004
SA01988SE (PAGE 1) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02033AT (PAGE 4) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008 0:00
SA02110CH (PAGE 3) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02135CH Installation of L-3 Communications Avionics Systems Inc. SkyWatch Traffic Advisory System Model SKY497. Reissued 3/26/2007
SA02149AK Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. Reissued 5/17/2013
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 2) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005 0:00
SA02168AK (PG 1) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001
SA02192CH Increase of maximum gross weight from 3600/3650 lb. to 4010 lb. for normal category operation. Reissued 6/17/2011
SA02203AK (PAGE 1) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02217AK (4 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004 0:00
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 4) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02276AK Installation of AMSAFE Aviation Inflatable Restraints Amended 3/12/2013
SA02279AT Installation of a Boom Beam bulb starter and ballast IAW LoPresti Master Drawing List Report No. 43 Rev D dtd 8/25/00 or later FAA approved revision. Amended 2/14/2003
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02293AK (1 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02314AT-D Installation of a stainless steel exhaust system. Required as part of this STC is Atlantic Aero Document 19593010 Instructions for Continued Airworthiness Rev B dtd 3/27/02 or later FAA approved revision. Amended 5/25/2010
SA02363CH Installation of Chuck Ney Enterprises Inc. CNE IO-470-C/N-MOD Model Engine (STC SE02261CH)  Issued 12/18/2006
SA02387AK Fabrication and installation of the LSI Exterior LED Lightning Suite Reissued 3/27/2013
SA02412CH-D Installation of Hartzell propeller de-ice components. Issued 5/7/2007
SA02424AT-D Installation of replacement fuel cell assemblies Reissued 4/16/2009
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02460CH Install Genesis Aero LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanks Reissued 11/19/2012
SA02461CH Install Genesis Aero LLC. 20-gallon fiberglass auxiliary wing-tip fuel tanks Reissued 11/19/2012
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02532AT Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. Issued 6/5/2002
SA02535CH Installation of M-T Propeller Inc model MTV-9-D/205-58 or MTV-9-D/210-58 propeller Reissued 1/1/2009
SA02547AT (PG 1) Installation of a Voice Alert System. Amended 8/28/2007
SA02556CH-D Installation of a Hartzell PHC-C3YF-1RF/F8068(K) propeller. Issued 4/18/2008
SA02625CH Installation of corrugated aluminum elevator skins in place of corrugated magnesium elevator skins. Issued 9/24/2008
SA02631AT Replace Lord Isolating Mounting Assemblies P/N J-10520-I with Lord Assembly P/N J-23135-1 four each. Reissued 3/12/2007
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02722CH Install D Issued 7/1/2009
SA02723CH Install D Reissued 9/23/2011
SA02737AT Installation of a Hartzell model PHC-C3YF-1RF propeller with F8468AK-8R blades in accordance with Mike Stohler Issued 10/2/2003
SA02738CH (PAGE 6) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA03122CH Increase Maximum Gross weight to 4011 pounds for Normal Category operations Issued 6/6/2012
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03286CH Install an electronic engine ignition system Issued 1/13/2014
SA03913AT Installation of the Astronics LED Replacement Lighting Bulbs in accordance with Chippewa Aerospace Master Drawing List (MDL) No. P23-3340-01-0001 Rev. 1 Dated November 01 2010 or later FAA approved revision. Issued 3/21/2011
SA08998AC-D Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-582 with optional automatic electric trim. Amended 1/18/2002
SA08999AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-583 with Optional Autotrim System. Issued 4/27/1995
SA09005SC Installation of Trimble 2000 Approach Navigator for nonprecision approach approval. Reissued 12/21/2001
SA09006AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-584 with Optional Autotrim System. Also eligible on model V35B when modified by STC SA1035WE (turbocharged engine). Amended 10/9/2001
SA09074SC Installation of vortex generators on wing upper surface and vertical stabilizer Amended 1/23/2013
SA09137AC-D Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-611 with Optional Autotrim System. Amended 4/11/2001
SA09203AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems. Amended 12/27/2001
SA09206AC-D Installation of S-TEC System 30 ALT altitude hold system Model ST-672. Issued 5/9/1997
SA09254SC Increase in maximum takeoff and landing gross weight by 100lbs. when equipped with vortex generators per STC SA09074SC. Amended 2/21/2013
SA09255SC Increase in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E. Inc. STC SA09074SC. Reissued 6/17/2011
SA09256SC Increase in maximum takeoff and landing gross weight by 100 lbs. when equipped with vortex generators per J.V.E. Inc. STC SA09074SC. Reissued 6/17/2011
SA09311AC-D Installation of S-TEC system 30 alt altitude hold system. Issued 11/21/1997
SA09312AC-D Installation of S-TEC System 30 alt altitude hold system. Issued 11/21/1997
SA09318AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-747-20/30. Issued 12/29/1997
SA09334SC Installation of Magellan Skynav 5000 GPS with Avionics Intl ACF100 and ACF528 cooling fans and AIS80-1 and AIS240-35 switching units Reissued 1/18/2011
SA09342AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-773-20/30. Issued 2/20/1998
SA09343AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-774. Issued 2/24/1998
SA09344AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-749-20/30. Issued 2/26/1998
SA09361SC Installation of Trimble 2000 Approach Plus GPS Navigator. Reissued 4/5/2002
SA09371AC-D Installation of S-TEC System 20/30 Single and Two Axis automatic flight guidance systems Model ST-824-20/30. Issued 6/10/1998
SA09372AC-D Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems Model ST-827-20/30. Issued 6/11/1998
SA09373AC-D Installation of S-TEC System 30 ALT altitude hold system Model ST-828 according to Bulletin No. 928 dated 6/8/98. Issued 6/12/1998
SA09374AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-825. Issued 6/18/1998
SA09375AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-833-20/30. Amended 1/17/2002
SA09376AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-834. Issued 7/3/1998
SA09410AC-D Installation of S-TEC System 50XP Two Axis Automatic Flight Guidance System Model ST-775. Issued 8/17/1999
SA09416AC-D Installation of S-TEC System 40X/50X single and two axis automatic flight guidance systems Model ST-866-40X/50X. Issued 10/1/1999
SA09418AC-D Installation of S-Tec system 40X/50X single and two axis automatic flight guidance systems model ST-778-40X/50X. Issued 2/22/2000
SA09421AC-D Installation of S-TEC system 40X/50X single and two axis automatic flight guidance systems Model ST-780-40X/50X. Issued 2/21/2000
SA09438AC-D Installation of S-Tec system 40X/50X single and two axis automatic flight guidance systems Model ST-784-40X/50X. Issued 2/23/2000
SA09446AC-D Installation of S-TEC GPSS ARINC 429 converter/interface Model ST-901. Issued 3/30/2000
SA09504AC-D Installation of S-TEC Altitude Vertical Speed Selector/Altitude Alerter Model ST-360. Issued 3/5/2001
SA09528SC Installation of a 23-volt 100 ampere alternator. Reissued 5/17/2013
SA09553SC Modification of the ECS s in Bonanza Models F33a A36 and B36TC to convert R12 vapor cycle systems into R134A refrigerant systems. Issued 6/1/1999
SA09561AC Installation of Pilot-side Meggitt EFIS. Issued 4/22/2002
SA09603SC Installation of Teledyne Continental Motors fuel injected engine. Amended 1/30/2001
SA09619SC Installation of Teledyne Continental Motors IIO-550-B engine cooling baffles and propeller. Issued 8/1/2000
SA09852SC Installation of Continental IO-550B engine. Amended 6/16/2005
SA1-27 Installation of Tactair T-3 auto-matic pilot and optional installation of Tactair AH-1 altitude hold device (for use with Tactair T-3autopilot). Reissued 8/7/1972
SA1-303 Auxiliary wing tip fuel tanks. Reissued 2/14/1975
SA1-341 Oil-free vacuum pump PA-201. Issued 
SA1-343 Oil-free vacuum pump. Issued 
SA1-354 Auxiliary wing tip fuel tanks. Reissued 2/14/1975
SA1-368 Installation of auxiliary wing tip fuel tanks in accordance with Safe Flight Extenders Company Reissued 8/16/2011
SA1-377 Replacement of d.c. belt- driven generator and regulator with Leece-Neville belt-driven alternator with built-in silicon rectifier. Issued 
SA1-379 Lube oil filter PB55-1 on aircraft with Continental E-185-1 through -11 engines. Amended 9/11/1967
SA1-381 Installation of Fram oil filter Model PB55-1. Amended 9/11/1967
SA1-478 Griswold lateralizer. Amended 
SA1-491 Flare rack modification to include radio equipment mount. Amended 
SA1-55 Federal F-200 automatic pilot. Amended 1/1/1960
SA1-584 External electrical power receptacle. Reissued 10/15/1974
SA1-587 External electrical power receptacle. Reissued 10/15/1974
SA1-628 External electrical power receptacle. Reissued 10/15/1974
SA1-636 Install 300 Series dry vacuum pump conversion kits. Reissued 10/30/1985
SA10004SC Installation of Hartzell PHC-C3YF-1RF/F8068 propeller on Raytheon Model S35 V35 V35A V35B 36 A36 35-C33A E33A F33A F33C or G33 with Teledyne Continental Model IO-520-B -BA or  Reissued 3/14/2013
SA1000CE Install cabin and engine compart-fire suppression system. Reissued 12/15/1977
SA10074SC Installation of CMI FADEC IOF-550 engine Reissued 11/6/2013
SA10080SC Installation of Hartzell model PHC-C3YF-1RF/F8068 propeller. Aircraft must be equipped with Teledyne Continental Motors IO-520-B IO-550-B or IOF-550-B model engine. Issued 4/3/2003
SA10126SC (1 OF 2) Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.  Amended 10/23/2003
SA10135SC Installation of Hartzell model PHC-C3YF-1RF/F8068 propeller. Must be equipped with Teledyne Continental Motors IO-520-B IO-520-BA IO-520-BB or IO-550-B model engine. Issued 4/3/2003
SA10145SC Installation of Teledyne Continental Motors Model IO-550-R engine. Reissued 9/23/2005
SA10145SC-D Installation of a Teledyne Continental Motors Model IO-550-R engine Amended 5/20/2010
SA1022NW Installation of a late model instrument panel  Issued 9/12/1980
SA10236SC (4 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1028NW Installation of a camera bay in aft cabin (between F.S. 118.5 and 151)and associated systems. Amended 10/10/1980
SA1033GL Installation of Pamco emergency back-up pneumatic system. Amended 10/12/1989
SA1034GL Installation of cooling shroud on engine driven dry air pumps. Amended 5/1/2007
SA1035WE Installation of Continental TSIO-520-D engine in accordance with FAA Sealed AiResearch Drawing No. 101-S35-209. Reissued 4/25/2011
SA1036EA Installation of vertical tail floodlights on upper surfaces of the horizontal stabilizer. Reissued 2/28/1980
SA10393SC Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot Amended 8/28/2006
SA1056WE BSA-2 stability augmentation system and optional rudder add-on kit. Reissued 10/1/1973
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA1069SO Installation of Bendix FCS-870automatic flight control system including manual electric pitch trim and optional flight director. Issued 5/3/1979
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1093CE Installation of AP-107 (2 axis)autopilot system and interface with Collins 329A-4V indicator. Issued 4/1/1975
SA1095CE Installation of AP-106 autopilot system and interface with Collins 329A-4V indicator. Amended 7/1/1975
SA10960SC Installation of a built-in oxygen system installed Issued 11/10/2009
SA1096CE Installation of yaw damper system. Issued 4/1/1975
SA1097CE Installation of AP-107 autopilot system and interface with Collins 329A-4V indicator. Issued 4/1/1975
SA1099GL Installation of Pamco emergency backup pneumatic system. (A36TC S/N EA-1 THRU EA-241 EA-243 THRU EA-272 B36TC S/N EA-242 EA-273 THRU EA-439) Amended 4/11/1989
SA109WE M-4 autopilot. Issued 1/1/1960
SA1103NW Installation of a Contental engine Hartzell propeller and associated systems Issued 11/19/1980
SA1106SO Installation of Bendix FCS-870automatic flight control system including manual electric pitch trim and option yaw damper and flight director. Issued 10/11/1979
SA1112NW Installation of a cabin heat boost pump fan Reissued 11/27/2001
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1113WE B-4 flight control system. Reissued 10/1/1973
SA11151SC Installation of an Electromech EM6025 Heat Duct Blower Issued 9/30/2013
SA1118NW Installation of a camera port and an optical port Issued 12/19/1980
SA112EA AF-510A AF-512A or AF-512B autopilots. Issued 1/1/1960
SA1140CE Installation of a 2-axis autopilot system with a King compass and a flight command indicator or an altitude horizon indicator with a mode controller. Reissued 2/28/2000
SA1145CE Installation of King Model KFC-200 2 axis (3 optional) or stand alone yaw damper for Beech Model A36S/N E572 and later autopilot system with a King KI-255(KI-256optional) flight command indicator with the KC-292 mode controller. Reissued 2/28/2000
SA1150WE Gyro sense element relocated to remote position. Reissued 10/1/1973
SA1154NW Approval of a gross weight increase to 3400 pounds Issued 1/9/1981
SA115CE Turbo volt Model Three-Five emergency electrical and vacuum system. Issued 5/4/1980
SA1163NW Installation of a camera port and a view finder hole Issued 2/2/1981
SA1164CE Installation of King KFC-200 two axis autopilot system with King KI-255 (or -256) flight command indicator or King KG-258 altitude horizon indicator with a KC-292mode controller. Reissued 2/28/2000
SA1166GL Installation of McCauley Model 3A32C406/82NDB-2 propeller in accordance with the appropriate installation instruction drawing as determined by Master Eligibility List No. PR0P406 Rev. A dated February 5 1987 or later FAA approved revision. Reissued 6/17/2011
SA1176SO Installation of Aileron and Wing Flap Gap Seals Amended 1/6/2010
SA1185CE Installation of Collins AP-107 (2 axis) autopilot system and interface with Collins FD-112V flight director. Issued 4/1/1976
SA1186CE Installation of Collins AP-107(2 axis) autopilot system and interface with Collins FD-112V flight director. Issued 4/1/1976
SA11GL Installation of Cleveland 6.00-6wheels and brakes conversion kit 199-49. Amended 9/2/1987
SA1204NW Installation of a recalibrated dial face on the United Instruments Fuel Flow Gauge Issued 3/27/1981
SA1211SO Installation of an adjustable trim tab on left aileron. Amended 11/23/1994
SA1218SW Automatic flight system AK306cons. of Century I and optional tracking system. Reissued 7/9/1984
SA1219NW Installation of an extended baggage compartment and hat shelf Issued 4/30/1981
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Limitations
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)