Beechcraft 35 -B35 Bonanza

Number of Active Aircraft: 210 Active- Map

Description:

Known as the Straight 35, was developed as Beechcrafts entrance into the high performance 4 place single after the war. While many of its competitors were developing trainers beechcraft was appealing to the higher performance market. The V tail was decided on, due to its low drag, and ability to reduce the spin tendency of the aircraft. Although there have been susbtantial AD's on the aircraft. It is known and loved by its owners for its efficient and rugged design. Interestingly the propellor on the aircraft was electrically controlled. The pitch on the propellor once set would become in essence a fixed pitch prop, until another setting was selected. So it wasn't a constant speed propeller but it was a variable pitch propellor. Also, the tail included a downspring that would over power the natural trim tab, when the aircraft slowed. Thus providing a protection against inadvertant slow flying. Up from the A model the B model also had very minimal changes, except for the higher powered engine. Update Fuel Cost
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1575 lbs
Max Weight 2650 lbs
Useful Load: 1075 lbs
Engine Name Continental E-185-8
Engine Number 1
Horsepower 196 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 17100 ft
Max Fuel 39 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 147 kts
GPH (75% BHP): 10.5
MPG (75% BHP) 14
Range (75% BHP): 445 nm
Fuel Cost Per Seat Mile 0.11 $
Fuel Cost Per Hour 63 $
MPG per 1000 lbs of Payload 15.05
F-T (Speed^2/FuelBurn) 20.6 HP
F-T Payload 22.1 kts
MPH To HP: 7.5 kts
T/O Roll - T/O over 50 FT OBST 1275 ft / 1515 ft

SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00063LA Installation of Acoustical/Thermal insulation. Reissued 1/5/2005
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
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
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
SA00176SE Installation of FLD-100C self contained hydraulic propeller pitch change system. Amended 1/2/2001
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
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
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
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
SA00246SE Installation of the Aviation Research Systems Inc. Locking Fuel Caps Reissued 10/23/2003
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00460SE Installation of stainless steel battery box. Issued 8/8/1997
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00557AT Installation of carbon steel brake discs. Reissued 1/24/1995
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
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00706LA Installation of a starter engaged light. Issued 11/25/1998
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
SA00839WI Front spar failsafe strap. Amended 7/18/2002
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00901NY Installation of a wing tip recognition lights. Reissued 2/27/2006
SA00954SE (1 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
SA01075SE Installation of the Precise Flight Inc. SpeedBrake 2000 System.  Amended 7/19/2006
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
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
SA01110CH Installation of wing fuel tank quick valve drains. (Listed models with specific serial number applicability) Issued 9/27/1999
SA01120SE Installation of Door Steward. Amended 3/4/2010
SA01155AT Installation of left hand and right hand auxiliary fuel cell assemblies  Reissued 4/27/2009
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
SA01168SE Installation of Teledyne Continental E225-8 engine modified. Amended 10/16/2007
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
SA01330LA (PAGE 2) Installation of alternate avionics support assembly. Reissued 10/6/2010 0:00
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01436SE (2 OF 2) Cockpit sunvisor retrofit kit. Issued 8/2/2004 0:00
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
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
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
SA01683NY Installation of .250 .312 .375 or .500 thick windshield. Issued 6/17/2003
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
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
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
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
SA01944CH (1 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004
SA01988SE (PAGE 2) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
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
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
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
SA02203AK (PAGE 2)  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
SA02268CH (PAGE 4) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02293AK (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
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
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
SA02547AT (PG 1) Installation of a Voice Alert System. Amended 8/28/2007
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02722CH Install D Issued 7/1/2009
SA02738CH (PAGE 6) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
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
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
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
SA09141AC-D Installation of S-TEC System 55two axis automatic flight guidance system Model ST-613 with optional autotrim system. Amended 10/24/2001
SA09143AC-D Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System Model ST-614. Amended 9/21/2002
SA09145SC Installation of vortex generators on wing upper surfaces in accordance with J.V.E. Inc. Drawing List JVE-501 Revision IR dated 01/05/96 and Installation Manual JVE-0596 Revision IR dated 01/05/96 or later FAA approved revisions. Reissued 6/17/2011
SA09313AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-757-20/30. Issued 12/5/1997
SA09337SC An increase gross weight of 100lbs for Beech models A35 B35 C35 D35 E35 F35 G35 and 35R when equipped with Vortex Generators per J.V.E. Inc. STC SA09145SC.  Reissued 9/28/2011
SA09345AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-758. Issued 2/25/1998
SA09441AC-D Installation of S-TEC System 40X/50X Single and Two-Axis Automatic Flight Guidance Systems Model ST-787-40X/50X. Issued 3/8/2000
SA09603SC Installation of Teledyne Continental Motors fuel injected engine. Amended 1/30/2001
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 
SA1-368 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
SA1-460 : Installation of auxiliary wing tip fuel tanks in accordance with Drawing Number RB1-001B and Installation Instructions number RB-1 Revision of April 1 1960. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( This wing tip tank installation is acceptable with either the baggage auxiliary tanks or the wing auxiliary tanks. However it is not acceptable with both auxiliary installations incorporated simultaneously. Reissued 8/16/2011
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
SA1-569 Installation of Continental IO-470-J engine (fuel injection) and Hartzell BHC-92ZF-lDl / 8447 propeller in accordance with Stauffer drawing No. 7 dated May 2 1961 and Stauffer Flight Manual Supplement No. 7 FAA approved May 5 1961.  Reissued 6/17/2011
SA1-570 Installation of propeller equipped with 8433 or 8833-4 or V8433 V8834-4 blades respectively. Amended 6/29/1979
SA1-628 External electrical power receptacle. Reissued 10/15/1974
SA1000CE Install cabin and engine compart-fire suppression system. Reissued 12/15/1977
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
SA10236SC (4 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10558SC Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot. Issued 7/27/2006
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
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA10921SC Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators Issued 11/10/2008
SA109WE M-4 autopilot. Issued 1/1/1960
SA1113WE B-4 flight control system. Reissued 10/1/1973
SA1150WE Gyro sense element relocated to remote position. Reissued 10/1/1973
SA115CE Turbo volt Model Three-Five emergency electrical and vacuum system. Issued 5/4/1980
SA1176SO Installation of Aileron and Wing Flap Gap Seals Amended 1/6/2010
SA11GL Installation of Cleveland 6.00-6wheels and brakes conversion kit 199-49. Amended 9/2/1987
SA1211NW Installation of an improved instrument panel Issued 7/24/1981
SA1215NW Installation of a Contintental engine Hartzell propeller Issued 4/20/1981
SA1254NW Installation of Beech Model E35 front and rear wing spar center section carry-through members and Beech Model G35 wing panels Issued 6/9/1981
SA1258NW Installation of a modified Aviation Enterprises instrument panel Issued 6/18/1981
SA1262WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1270SW Installation of Mitchell automatic flight system Model AK328 consisting of Century I autopilot with omni tracking system. Reissued 7/9/1984
SA1285NW Installation of a Tactair T3 autopilot Issued 8/11/1981
SA1290NW Installation of a McCauley 3A32C76S-M/S82NB-2 propeller on a Continental IO-520-BA engine Issued 8/14/1981
SA130EA AF-510A AF-512A or AF-512B autopilots. Issued 1/1/1960
SA1315WE Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. Reissued 4/15/2011
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1369WE Installation of Brittain Industries Inc. Model BSA-3 stability augmentation system. Reissued 10/20/1972
SA136WE Autopilot and optional nav-coupler add-on BI-300 BI-301 or BI-304. Reissued 10/1/1973
SA1375WE Installation of Dukes Astronautics Model 4140-00-39 Auxiliary Fuel Pump into fuel system Amended 2/4/1976
SA137WE Beech wing tip kit 35-660. Issued 1/1/1960
SA1387WE Installation of Brittain Industries Model NAV-2A Flight Control System. Reissued 10/1/1973
SA1405NM Installation of a fuel transfer system Issued 1/29/1982
SA1417NM Installation of a Franklin 6AS-350-A or 6AS-350-A1 engine with an AiResearch TE-0657turbosupercharger and Hartzell HC-C2YF-1BF/F8459A-4 to -8 or Hartzell HC-C2YF-1BF/8459A-4Q or -8Q propeller. Reissued 4/9/1999
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1423WE Wing truss reinforcement front spar and change of hinge points for landing gear idler arm. Amended 6/14/1976
SA144EA Approval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG RBI-IDOL) Fiberglass wing Solenoid Fuel System (ref STC SAl-303 dated February 20 1959). No wing or baggage compartment auxiliary tanks are permitted with this system. This STC also places the above aircraft in the Normal and Utility categories using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders Inc. Installation Manual FEI-35 (4A) Rev. D dated February 15 1964 is required. Reissued 8/16/2011
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1476WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 1/23/2013
SA1477WE Installation of Brittain Model B2C Flight Control System. Reissued 10/20/1972
SA147CE Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. Issued 1/1/1960
SA1493WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 2/1/2013
SA1499NM Installation of a General Electric flap indicator Issued 4/19/1982
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA152CE Federal F-200 autopilot. Issued 1/1/1960
SA152NW Installation of deck and glare shield (with or without instrument lights). Amended 5/21/1981
SA1531WE Installation of Brittain Model BSA-4 Stability Augmentation System. Reissued 10/20/1972
SA153EA Install Beryl D Amended 1/30/2013
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1584CE Installation of elevator tail cone fairing per Smith Speed Conversions Drawing List 1005 stamped FAA Approved Reissued 9/28/2011
SA1584GL Install Aero Fabricators shoulder harness and seat belt assembly. Issued 7/1/1991
SA1644SW Installation of Mitchell automatic flight system Model AK415 consisting of Century IIB autopilot with optional radio coupler. (S35 S/N 7841 AND BELOW) Reissued 7/16/1984
SA1650CE Installation of either the Tail Safe support angles or a Stub Spar at the 3% chord station on the root rib of the horizontal stabilizer per Smith Speed Conversions Drawing List No. 1006 with an FAA approved date of May 8 1981 or later. Reissued 9/28/2011
SA165SW Automatic pilot AK121. Issued 1/1/1960
SA1703CE Installation of flap and aileron fairings and seals. Reissued 1/26/1993
SA1722WE Installation of Fiberglass tail fairing. Amended 8/28/2006
SA1736WE Installation of Brittain Industries B-5 Flight Control System. Reissued 10/20/1972
SA173GL Installation of Dukes fuel pump P/N 4140-00-39. Reissued 5/22/1989
SA1775NM Installation of a Teledyne/Continental engine a Beechcraft propeller a Dukes fuel pump a Woodward propeller governor and associated changes Issued 7/12/1983
SA1776NM Installation of standard late model long sloping windshield. (35-33 S/N CD-1 THR E 33 S/N CD118) (C35 S/N D2681 THRU V35 S/N 8598) Issued 7/19/1983
SA177EA Installation of Monitair angle of attach system Model AA-2. Reissued 2/14/1972
SA1782NM Installation of Precise speedbrake system. Amended 11/7/2003
SA1803CE Installation of fire extinguishing system in cabin and/or fire extinguishant system in engine compartment. Reissued 2/1/1993
SA1811NM Installation of Safe Flight Model SC-150 lift detector system. Reissued 10/31/1984
SA181EA Approval of 200 lb. increase in Maximum gross weight for takeoff and landing when equipped with the following Flight Extenders Inc. Tip tank Installation: 15 gal (RB2-100B) or 14.7 gal (RBI-IOOG RBI-IDOL) Fiberglass wing tip fuel tanks (ref STC SA3OEA Configuration 2 or 3) and Type II or III Kit transfer fuel system. This system eligible with Beech 20 gal wing aux. tanks or baggage compartment tanks but not both. This STC also places the above aircraft in the Normal and Utility categories using the Normal Category as the basic category for purposes of placarding and marking. Flight Extenders Inc. Installation Manual FEI-35 (4A) Rev. C dated February 15 1964 is required. Reissued 8/16/2011
SA184NE Installation of a landing gear protective switch cover. Issued 10/6/1983
SA1850SO Installation of revised instrument panel. Issued 10/16/1985
SA1883WE Installation of Brittain Industries NAV-2B flight control system. Reissued 10/20/1972
SA1902SW Installation of Mitchell automatic flight system Model AK348consisting of Century I autopilot with optional omni tracker. Reissued 8/1/1984
SA197NW Installation of Clark three- light gear position indicator system. Reissued 6/17/2011
SA19GL Install Cleveland 7.00-8 wheels and brakes. Amended 7/24/1987
SA2-1533 Installation of windshield wiper. Reissued 1/31/1997
SA2000SW Dual control wheel. Issued 1/1/1960
SA2029WE Installation of Delta Sigmatronix Emergency Electric Fuel Pump Kit PK-2 in lieu of Beech hand pump P/N 35-924230 (on aircraft equipped with Beech P/N 35-921171 or P/N 35-924065 fuel unit). (C35 S/N D1 THRU D2900) Issued 1/1/1960
SA2045CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index(RON +MON)/2. Amended 5/10/2004
SA2065NM Installation of a Dukes Model 4140-00-39 fuel boost pump under the cabin floor Issued 3/18/1983
SA2081WE Installation of Madras Air Service P/N MAS 102 wing tips. Amended 12/7/1987
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2131WE Installation of Delta Sigmatronix emergency electric fuel pump P/N 29000 in above models equipped with Beech P/N 35-924230 fuel unit. Issued 1/1/1960
SA2144WE Installation of Madras Air Service Part No. MAS 102 wing tips. Issued 1/1/1960
SA2145SO Installation of Appalacian Accessories stainless steel brake discs P/N s 75-25A or75-25B. Reissued 9/29/1995
SA2160NM Installation of the Precise Flight stand-by vacuum system (SVS). Amended 11/7/2003
SA2198NM Installation of a winch and fairlead system for deployment of a trailing drogue (cone). Issued 2/13/1984
SA219EA Installation of Katz integrated flight indicator Model KIFI-2 or KIFI-2A. Amended 5/21/1969
SA2200SW Installation of Teledyne Continental IO-520-B -BA - BB or IO-550-B engine and applicable McCauley Propeller only as listed on STC. Reissued 3/23/2009
SA2201SW Ventral fin. Issued 6/23/1975
SA2208WE Installation of Red-Q-Mark Signet A-MK-100 or A-MK-110 marker assembly. Amended 8/7/1970
SA2219WE Installation of Filtrator Company Engine Crankcase Breather and Vacuum Pump Air-Oil Separator in accordance with the applicable FAA sealed drawing listed on the attached Master Eligibility List Number SA2219WE.Installation of Filtrator Company engine crankcase breather and vacuum pump air-oil separator. Reissued 7/14/2011
SA222CE Reinforce front lower carry- through section & wing attach fittings. Amended 6/2/1980
SA2271WE Installation of long fiberglass tailcone to replace the short factory installed tailcone. Reissued 4/3/1975
SA2286NM Installation of tail stabilizer support. Reissued 3/26/2007
SA22SW AK087 AK087E or AK087R automatic pilot. Issued 1/1/1960
SA232EA Installation of Tactair omni lock model OL-1 and optional installation of Tactair localizer adapter model LA-1 (for use with Tactair model omni lock model OL-1). Reissued 8/7/1972
SA2361SW Installation of Continental IO-470-N engine and McCauley 2A36C23/84B-0 or 2A37C223/90RB-6 or Beech 278-100-11/278-214-82 or 278-100-13/278-214-82 or Flottorp F12A-3/8400-2 propeller Amended 3/7/2013
SA236GL Installation of a Continental O-470-G engine and McCauley propeller. Issued 5/4/1978
SA2375CE Installation of B&D Instruments & Avionics Inc. Electronic Tachometer System. Data required: (1) B&D Instruments & Avionics Inc. Installation Manual Part No. 0535-003-011 Rev. B or later FAA Approved Reissued 11/3/2011
SA23CE 210419 governor. Issued 1/1/1960
SA23EA Installation of Third Cabin Window on both sides of Fuselage in accordance with Glenn Floyd Stauffer Drawing Nos. 42601 Revision A dated 31 May 1962 and 42602 Revision A dated 13 June 1962. Reissued 8/16/2011
SA2470WE Installation of anticollision lighting system. Issued 2/8/1972
SA2546WE Installation of Pathfinder Engineering Corp. Model P1-( )autopilot system. Reissued 9/30/1998
SA2547WE Installation of Pathfinder Engineering Corporation Model P2-( ) autopilot system. Reissued 2/20/1974
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2619WE Installation of Pathfinder Model P1-( ) autopilot system. Reissued 9/30/1998
SA2633WE Installation of enlarged window and baggage compartment. Reissued 11/19/2012
SA2653SW Installation of Instrument Panel in accordance with 1998-54 Installation Manual and Drawings 1998A200 1998A300 1998A400 and 1999 all dated July 1 1977 Battery Box Kit per 1998-84 Installation Manual and Drawing 2000 dated July 1 1977 Radio Cooling Kit per 1998-86 Installation Manual and Drawing 2002 each dated July 1 1977. Reissued 8/16/2011
SA2653WE Installation of Beryl D Reissued 7/14/2011
SA2654WE Installation of Pathfinder Model P2A( ) autopilot. Amended 7/3/1979
SA265SO Extension addition to nose landing gear doors. Issued 1/1/1960
SA269WE Pneumatic pitch assist PC-1 and optional installation altitude hold AH-1. Reissued 10/1/1973
SA2700WE Installation of Airborne Electronics solid state automatic propeller control Model 350A. Amended 3/28/1977
SA2753CE Installation of flap actuated landing gear warning system. Reissued 5/7/1997
SA2771WE Installation of Long Fiberglass tailcone to replace the short factory installed tailcone in accordance with FAA Sealed N.E. Coote Tool and Machine Drawing List Report No. 1 dated September 2 1970. Reissued 8/16/2011
SA283EA Installation of Flight Extender Inc. Alternate Fiberglass Fuel Tip Tanks (P/N RB4-100 15 Gal.) on the above aircraft when equipped with 15 gal. or 12 gal. tip fuel systems in accordance with the following STC Reissued 2/6/1975
SA2858WE Installation of right and/or left hand cockpit side windows in accordance with FAA sealed Beryl D Reissued 6/17/2011
SA28EA Installation of 12-gallon fiberglass wing tip fuel tanks. Reissued 8/16/2011
SA292WE Alternator A-14-0 or A-14-5 and voltage regulator A-20. Issued 1/1/1960
SA293CE GUARD System (Gear Up Automatic Response Device). Amended 9/6/1966
SA2941SW Addition to Hydro Seal Fluid Additive to landing gear shock struts. Reissued 8/8/1980
SA294CE GUARD System (Gear Up Automatic Response Device). Amended 9/6/1966
SA3-196 Lear ADF-12C kit complete and LTRA-5 with scope complete. Issued 1/1/1960
SA3-241 Electric motor-driven AN4100 fuel pump. Issued 1/1/1960
SA3-264 Radio rack aft of baggage compartment. Issued 1/1/1960
SA3-276 Scott 8800 oxygen console. Issued 1/1/1960
SA3-298 Electric motor-driven fuel booster pump. Issued 1/1/1961
SA3-3 BC Chinook cabin heater. Issued 1/1/1960
SA3-317 Baggage compartment windows. Issued 1/1/1960
SA3-56 Oxygen equipment Purtain Type E bottles and Scott#8800 console. Issued 1/1/1960
SA3-58 Grimes D-7080-2-12 rotating beacon. Issued 1/1/1960
SA3-673 L-2B autopilot with or without altitude control and/or approach coupler. Issued 1/1/1960
SA3-8 L-2B automatic pilot including approach coupler and altitude control. Issued 1/1/1960
SA3020WE Installation of exhaust silencers in accordance with Top Banana Installation Instructions dated March 12 1975 Revision of October 22 1975. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( Silencer is manufactured in accordance with Top Banana Drawing No. 2-12-A35 G Reissued 7/14/2011
SA30EA Installation of 13.5 gallon fiber-glass wing tip tank assembly. Reissued 8/16/2011
SA3113SW-D Mitchell automatic flight system AK415 cons. Of Century IIB autopilot with optional radio coupler. Reissued 8/16/1984
SA3116SW-D Installation of Mitchell automatic flight system AK325 consisting of Century I autopilot with optional omni tracker. Reissued 6/5/1984
SA312WE Beech pneumatic pitch assist PC-1and optional altitude hold AH-1. Reissued 10/1/1973
SA3191WE Installation of wing tip fences. (A35 B35 C35 D35 E35 F35 G35 UTILITY CATEGORY) (35 NORMAL OR UTILITY CATEGORY) Issued 5/11/1976
SA319NW Installation of a Continental IO-520-BA engine Hartzell HC-C3YF-1RF/8468A-8R propeller and associated systems Amended 9/17/1976
SA321SO Tank type wing tip plates. Issued 1/1/1960
SA321WE Beech pneumatic pitch assist PC-1and optional altitude hold AH-1. Reissued 10/1/1973
SA322WE Pneumatic pitch assist PC-1 and optional altitude hold AH-1. Reissued 10/1/1973
SA323WE Beech pneumatic pitch assist PC-1and optional altitude hold AH-1. Reissued 10/1/1973
SA3260WE Installation of electric driven fuel pump. Issued 9/8/1976
SA3267SW-D Mitchell automatic flight system AK727 consisting of Century III autopilot with optional and glide slope couplers. Reissued 3/29/1984
SA3268SW-D Mitchell automatic flight system AK728 consisting of Century IV autopilot or AK728FD consisting of Century IV flight director autopilot with optional remote annunciator. Reissued 3/29/1984
SA3271SW-D Mitchell yaw damper system YK631. Reissued 3/29/1984
SA3286SW-D Mitchell automatic flight system AK732 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 3/29/1984
SA332EA Electronic voltage alarm. Amended 1/1/1960
SA3337WE Installation of ventral air skeg. Amended 4/2/1979
SA334SW Installation of InterAv Alternator. Reissued 7/20/1981
SA3365NM Install a Continental IO-470-K Engine McCauley 2A36C23/84B-0 Propeller and an M35 Bonanaza nose section structure Issued 4/28/1986
SA33SW Beech T-24 ailerons 45-135050-3with servo attach fittings 45-115090. Issued 1/1/1960
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3584NM Installation of aileron and flap gap seals. Reissued 10/23/2003
SA358GL Carburetor air filter (dry type). Issued 1/1/1960
SA358WE One-piece windshield. Reissued 6/25/2001
SA359WE Supercharged Continental engine E225-8. Issued 1/1/1960
SA361EA A. Installation of monitair angle of attack and stall warning kit number 92-107 and B. Installation of Monitair angle of attack and stall warning kit number 92-105. Reissued 2/14/1972
SA3650NM Cockpit sun visor installation. Amended 7/7/2004
SA3678WE Installation of air/oil separator. Reissued 9/28/2001
SA374SW Automatic pilot AK131 AK131E and AK131E-3 pitch trim system AK132 and federal lateral guidance radio AK123. Issued 1/1/1960
SA380SW A-C generator. Issued 1/1/1960
SA384WE Installation of adjustable pilot and co-pilot seat Amended 6/27/2012
SA387SO Installation of Aviation Elec. Omni bearing tester Model OBT-X in accordance with AET Drawing Nos. 1001 1002 1003. Issued 1/1/1960
SA4-1146 Hartzell HC-12X20-7C/8433-0propeller. Issued 1/1/1960
SA4-1239 Autopilot and optional nav-coupler add-on BI-300 BI-301 or BI-304. Reissued 10/1/1973
SA4-1245 Installed Flightcraft ski bag compartment. Reissued 1/31/1986
SA4-1260 Autopilot and optional nav-coupler add-on BI-300 BI-301 or BI-304. Reissued 10/1/1973
SA4-1305 Hartzell HC-12X20-7E/8433-0propeller. Issued 1/1/1960
SA4-133 Automatic rudder control. Issued 1/1/1960
SA4-1437 Leece-Neville alternator A001-2002AA and regulator A001-3533RA. Issued 1/1/1960
SA4-1538 Oil-air separator. Issued 1/1/1960
SA4-1611 Anticollision beacon Roto- Lite X5000 either 12 or 24- volt on the top or bottom of fuselage. Issued 1/1/1960
SA4-1629 Installation of wing tip fuel tanks. Reissued 9/29/2009
SA4-190 Automatic rudder control. Issued 1/1/1960
SA4-191 L-2 automatic pilot. Issued 1/1/1960
SA4-238 Thompson TF 2800 engine- driven fuel pump installation on Continental O-470-G engine. Issued 1/1/1960
SA4-280 Ceco CE-9136 AN-4100 or AN-4101 electric fuel pump. Issued 1/1/1960
SA4-282 Tactair T-3 automatic pilot. Issued 1/1/1960
SA4-344 B arcon system. Issued 1/1/1960
SA4-393 Fiberglas reinforced plastic wing tips incorporating positions. Issued 1/1/1960
SA4-435 Automatic rudder control Model B. Issued 1/1/1960
SA4-436 L-2 autopilot. Issued 1/1/1960
SA4-489 Automatic rudder control. Issued 1/1/1960
SA4-550 Standard Beech A-35 Fuel System modified. Reissued 3/5/1998
SA4-559 20-gallon auxiliary fuel tank. Issued 1/1/1960
SA4-562 Federal F-200 autopilot. Issued 1/1/1960
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)