Cessna 310R 75

Number of Active Aircraft: 452 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 3417 lbs
Max Weight 5500 lbs
Useful Load: 2083 lbs
Engine Name CONT IO-520-M
Engine Number 2
Horsepower 285 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 19750 ft
Max Fuel 143 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 194 kts
GPH (75% BHP): 26.2
MPG (75% BHP) 7.4
Range (75% BHP): 947 nm
Fuel Cost Per Seat Mile 0.14 $
Fuel Cost Per Hour 157.2 $
MPG per 1000 lbs of Payload 15.42
F-T (Speed^2/FuelBurn) 14.4 HP
F-T Payload 30 kts
MPH To HP: 6.8 kts
T/O Roll - T/O over 50 FT OBST 1335 ft / 1700 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
SA00040LB Installation of a modified exhaust tail pipe. Amended 11/27/1996
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
SA00109BO Installation of Cessna SK310-114-0 electric windshield heated panel kit. Amended 12/3/2001
SA00150SE Installation of TSO shoulder harness assembly with inertia reel and associated mounting brackets in accordance with FAA approved AeroMods Master Drawing List MH010 Rev. B dated October 13 1994 or later FAA approved revision. Reissued 1/17/1995
SA00161BO (1 OF 3) Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005
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
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00215SE Installation of aerodynamic spoilers to the wing. Reissued 7/9/2013
SA00228NY Installation of Sky Harbour Aircraft Refinishing Ltd Ice Damage Prevention Plates. Amended 1/24/1997
SA00243BO (2 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
SA00269BO (1OF 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
SA00280NY Installation of .250 inch thick replacement windshield. Issued 2/7/1995
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 1 ) 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
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00409DE Installation of an aircraft noise control system. Issued 4/3/2000
SA00419NY Installation of cockpit utility light. Reissued 12/31/2002
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00465AT Installation of radar. Issued 5/4/1994
SA00556DE Installation of a left-hand exhaust stack assembly. Issued 9/23/2004
SA00571SE Replacement of certain BF Goodrich pneumatic deicer boots. Reissued 6/13/2001
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (3 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00695SE Replacement of certain Rotomaster and Rayjay scavenge pumps Amended 2/14/2003
SA00709LA Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. Reissued 5/14/2002
SA00729SE Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760 Revision - dated 7/20/99 or later FAA approved revision. Amended 11/30/2005
SA00749AT Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) Amended 12/10/1997
SA00763AT Installation of left hand and right hand fuel cell assemblies. (310 S/N PO240 and up 401 S/N 1 thru B1200 402 S/N 1 thru B1200) Reissued 4/29/2009
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
SA00799CH Installation of Honeywell HC-C2YF-2CUF/FC8468(B)-3 propellers C-2285-4(P) spinners A-2476-8 spinner mounting kits and A-2374-1 anti-ice kits. Issued 11/25/1997
SA00804SE Installation of an engine failure indicator system also referred to as a low Thrust Detector system.  Amended 7/16/2000
SA00823CH Installation of various de-icer wire harnesses. Reissued 10/10/2002
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00873WI Installation of a tailcone assembly. Reissued 11/5/2008
SA00879CH Installation of McCauley Propeller Model 3AF32C528/82NEA-4 spinner and optional anti-ice/deice. Reissued 9/21/2005
SA00880CH Installation of McCauley Propeller Model 3AF32C528/82NEA-X spinner and optional deice. Reissued 9/21/2005
SA00944CH Replace Janitrol/JanAero Combustion Heater Model 81D94-X (XX) with C&D Associates Combustion Heater Model CD45K either P/N RA-81D94-3 or P/N CD81D94-3. (95-B55 S/N TC-1658 and up E55 S/N TE-959 TE-968 and up 58 S/N TH-437 and up) Amended 6/20/2000
SA00948CH Installation of various de-icer wire harnesses. (E90 modified by STC SA3593NM F90 modified by STC SA4131NM B200 modified by STC SA2698NM-S DHC-6 Series modified by STC SA3532NM) Amended 1/29/2004
SA00971CH Remove South Wind 940 series combustion heater and install C&D Asociates TSO-C20 approved heater kit model CD35K or CD45K (310A (USAF U-3A) S/N 35000 trhu 35546 PA-23 S/N 23-1 and up 27-1 thru 27-3049 27-3051 thru 27-3053 PA-30 S/N 30-2 thru 30-401) Amended 3/29/2004
SA01026SE (PAGE 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
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
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
SA01118WI Installation of the Concorde FLA or VRSLA RG series batteries in the Cessna Single Engine Airplanes listed on the attached FAA Approved Model List (AML) No. SA01118WI dated October 17 2001 Amended 11/30/2013
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 (1 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005
SA01176AT Installation of Composite Spinner. Amended 10/13/2000
SA01205WI-D (1 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
SA01217SE Installation of Zeiss Aerial Survey Camera System.  Issued 5/19/2003
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (2 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
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 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01370SE Installation of BAS Inc. Shoulder Harness in accordance with BAS Inc. Drawing List which includes Installation Instructions and Instructions for Continued Airworthiness listed on FAA AML SA01370SE dated January 26 2004 or later FAA approved revision. Amended 12/2/2010
SA01408AT  Installation of National AirParts Model N300 alternators as replacement for belt-driven generators in accordance with National AirParts Inc. Document Number NAPI310 Cessna 310/320 Alternator Conversion Reissued 6/24/2011
SA01420WI Installation of Garmin GNS 430A / 530A COMM/NAV/GPS Systems. Data required: (1) Scandinavian Avionics Design GmbH Drawing List 2027438-DL-02 Issue 2 or later EASA approved revisions. (2) Scandinavian Avionics Design GmbH Approved Aircraft Flight Manual Supplement Doc. 2027438-AM-02A Issue 1 and Doc. 2027438-AM-02B Issue 2 both approved by EASA under approval No. EASA.A.S.01389 dated 07-09-2005 or later EASA approved revision. );INSERT INTO stc_table VALUES (  Issued 4/6/2007
SA01436SE (1 OF 2) Cockpit sunvisor retrofit kit. Issued 8/2/2004
SA01473SE (2 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
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (2 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
SA01734SE (PG 4) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01828SE Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System Reissued 5/12/2011
SA01847CH Installationof McCauley Propeller Model 3AF32C512/82NEA-5.5.  Reissued 9/23/2005
SA01860NY (3 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 2)  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 (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02003NY Installation of SMR Technologies pneumatic deicer models. Reissued 8/29/2006
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 2) 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
SA02095AK Installation of hourmeter airspeed switch. Issued 12/10/1997
SA02110CH (PAGE 1) 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
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02203AK (PAGE 1) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02217AK (2 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
SA02239SE Installation of a Skymech rear spar replacement kit Issued 8/21/2012
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 2) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02268CH (PAGE 3) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02293AK (1 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02366AT-D Installation of replacement fuel cell assemblies Reissued 4/16/2009
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
SA02546NY Installation of the Lord Corporation Nose Wheel Shimmy Damper Part Number SE-1090-1 Issued 7/9/2008
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02609AT Installation of Enviro Systems Air Conditioner per Air Centers Cool Air Drawings AC-310-062299 dtd 7/24/99 or later FAA approved revision. Issued 1/28/2003
SA02634AT-D Installation of fuel cell modifications consistent Reissued 4/16/2009
SA02655AT (1 OF 2) Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. Amended 9/1/2004
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 4) 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
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
SA09001AC-D Installation of S-TEC System 55 two axis automatic flight guidance system model ST-594 with optional autotrim system. Amended 5/11/2001
SA09354AC-D Installation of S-TEC system 20/30 single and two axis automatic flight guidance systems. Issued 4/14/1998
SA09356AC-D Installation of S-TEC System 30 alt altitude hold system. Issued 4/13/1998
SA09458AC-D Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-790-40X/50X. Issued 6/30/2000
SA09505AC-D Installation of S-TEC Manual Electric Trim System Model ST-883. Issued 2/27/2001
SA09511AC-D Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems model ST-888-20/30. Issued 6/19/2001
SA09519AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-896-20/30. Issued 1/24/2002
SA09655SC Installation of RAM Induction Equalized Fuel Nozzle Set. Amended 9/20/2002
SA09774AC Replacement of certain Goodrich pneumatic deicer boots Issued 11/9/2012
SA09971SC-D Installation of Hartzell model PHC-C3YF-2UF/FC7693DF or PHC-C3YF-2UF/FC7693DFB propellers Reissued 9/11/2008
SA1-124 Lube oil filter BP55-1. Issued 
SA1-185 Installation of Tactair T-3 auto- matic pilot and optional installa- tion of Tactair AH-1 altitude hold device (for use with Tactair T-3 autopilot). Reissued 8/7/1972
SA1-21 Federal autopilot F-400. Issued 
SA1-293 Lightweight reservoir pneumatic deicing system. Reissued 3/1/1996
SA1-506 Electrothermal propeller deicing system. Reissued 3/1/1996
SA1-579 Taxi lamp in right outboard cowling. Amended 1/1/1960
SA1-620 Kit No. 2014X for 12-inch RCA AVQ-45 AVQ-47 AVQ-50 AVQ-55 and 12-inch Collins WP-103 radar antenna. Reissued 7/6/2005
SA1007NW Installation of a low thrust detector system. Reissued 3/6/1998
SA1018SW Bendix M4-C autopilot. Issued 1/1/1961
SA10224SC Installation of a Chelton Aviation Corp. AP-3C autopilot.  Amended 2/1/2006
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA103GL Install Norton Company radome Part No. 4096X. Amended 6/12/1989
SA103RM Installation of exhaust turbo connector P/N 30477-3 Amended 11/28/1990
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA107GL Conversion of oil lubricated de-ice pumps and related hardware to Airborne dry air pump 400 series conversion kits. Issued 1/23/1976
SA1081CE-D Installation of Collins Radio Group AP-106 3-axis autopilot system. Amended 6/27/1975
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1082CE-D Installation of Collins Radio Group AP-107 3-axis autopilot system. Amended 6/27/1975
SA1083CE-D Installation of Collins Radio Group AP-107 2-axis autopilot system. Amended 6/27/1975
SA1084CE-D Installation of Collins Radio yaw damper system. Amended 6/27/1975
SA1090NE Install auxiliary ignition switch between magneto control switch and engine start switch. Amended 8/9/1993
SA109EA Pump type pneumatic deicing system. Reissued 3/1/1996
SA110RM Modify Cessna exhaust system by replacement of the inter-cylinder expansion joints with a slip fit joint. Issued 8/17/1977
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA111GL Install Cleveland conversion kit P/N 199-64. Amended 4/1/1981
SA1142SW Mitchell automatic flight system AK300 consisting of Century III autopilot with optional automatic pitch trim radio and glide slope coupler. Reissued 7/9/1984
SA1175WE Installation of one-piece windshield. Reissued 6/25/2001
SA1190SW Mitchell automatic flight system FD/AP282-300 consisting of flight director/automatic pilot and automatic pitch trim. Reissued 7/9/1984
SA119CE L-2C autopilot. Issued 1/1/1960
SA1250NW Installation of Cessna 310D propeller alcohol de-ice system Issued 5/29/1981
SA1273CE Installation of King KFC 200 2-axis(3 optional) flight control system with a King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller. Reissued 2/28/2000
SA128GL Replace existing asbestos or bellows exhaust seal with slip joint. Reissued 10/9/1987
SA1301CE Installation of Enk Aviation fire suppression system. Amended 7/28/1981
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
SA1359CE Chrome-plated brake disc installation. Issued 1/16/1978
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1374GL Installation of a Cooling Shroud on engine driven dry air pumps. Amended 5/1/2007
SA137NW Installation of Collins AP-107 low profile automatic flight control system (FCS) including yaw damper system. Amended 12/12/1974
SA1387SW Installation of liquid nitrogen air conditioner. Reissued 11/29/1984
SA138NW Installation of Collins low profile yaw damper system. Amended 12/12/1974
SA1406NW Installation of late model Cessna control wheels (P/N 1260243-2) and adapter (P/N 0760017-3) Issued 12/22/1981
SA1407NW Relocation of Pitch Servo from the position directed in Edo-Aire Centruy III Installation manual to position aft of the baggage compartment Issued 12/22/1981
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1452WE Installation of Brittain Model B-4A flight control system. Reissued 7/2/2013
SA147CE Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. Issued 1/1/1960
SA1490WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 2/1/2013
SA1494SW Installation of Mitchell flight director remote annunciator Model AK375. Amended 7/10/1984
SA14GL Installation of detachable lead strap propeller deicers. Reissued 3/1/1996
SA150GL Install Norton Company radome Kit No. 4131X. Amended 3/28/1978
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1555CE-D Installation of King KAS 297 altitude selector option in airplanes equipped with KFC 200 Flight Control System with Flight Director.. Reissued 2/28/2000
SA1576GL Installation of on-board engine analyzer system. Issued 3/25/1991
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1604WE Installation of Brittain B-5 flight control system. Reissued 6/14/2013
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1642WE Modification of exhaust system components. Amended 12/7/1973
SA1675WE Installation of exhaust gas temperature monitoring systems EGT-2. Amended 8/28/1974
SA1686WE Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. Amended 10/17/2002
SA1799WE Installation of Brittain Industries B-5 flight control system. Reissued 6/14/2013
SA181SO Installation of Turbosupercharged Continental IO-470- U engines  Reissued 6/26/2006
SA1847WE Installation of Brittain Up-Command Signal Adapter Kit. Reissued 10/20/1972
SA1880WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 2/6/2013
SA1883SW Install Hartzell synchrophase system. Reissued 11/29/1984
SA1896WE Installation of Brittain Industries NAV-2B Flight Control System Reissued 6/14/2013
SA1904SW Installation of additional auxiliary transfer tanks. Reissued 11/29/1984
SA192RM New slip joint exhaust manifold. Issued 12/20/1979
SA1BO Installation of Safeway Model7009-1 deicer kit. Reissued 5/9/2003
SA2-1272 Installation of revised hat rack. Reissued 11/29/1984
SA2-1533 Installation of windshield wiper. Reissued 1/31/1997
SA2-1578 Installation of Teledyne Continental Motors 0-470-BI or 0-470-MI engines modified for fuel injection. Reissued 12/29/1986
SA2-695 Installation of one-piece instrument panel and related equipment. Reissued 8/31/2000
SA2-698 Installation of Bendix 50 ampere generators type 30E22 and related equipment. Reissued 8/31/2000
SA2-712 Installation of auxiliary fuel tanks saddle type and fuel cross-feed system. Reissued 11/29/1984
SA2-871 Installation of engine mounts to accommodate lord mount assemblies J6545-1. Reissued 8/31/2000
SA2-872 Installation of exhaust muffler and nacelle modifications. Reissued 8/31/2000
SA2-880 Installation of nacelle changes and exhaust system changes using existing O-470-B or O-470-M engines Reissued 5/1/1973
SA2-903 Manufacture and installation of 1/4 inch thick plexiglass windshield Reissued 5/1/1973
SA2-904 Installation and manufacture of engine shock mounts for Teledyne0-470-M and IO-470-D engines. Reissued 11/29/1984
SA2-909 Installation of full shock mounted instrument panel. Reissued 11/29/1984
SA202SW Cessna 0895000-8 -9 aft cowling doors. Issued 1/1/1960
SA2082WE Installation of two Lycoming TIO-540-A2B or  Reissued 7/31/2012
SA2093CE Reinstallation of original Cessna manually operated alternate engine induction );INSERT INTO stc_table VALUES ( air system on airplanes previously modified in accordance with STC SA2242SW Reissued 7/31/2012
SA20GL Installation of Woodward Type II electronic propeller synchronizer or synchrophaser system. (G-44A MODIFIED COLEMILL - STC 2-13) (500-A modified - Colemill STC SA340SO) Reissued 4/30/2007
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA212SO Installation of Lycoming IO-540- A1A5 engines and Hartzell HCA3XK-2B/7636D propellers. Reissued 11/29/1984
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2203WE Installation of air conditioning system. Reissued 5/17/2013
SA2207SO Installation of two Teledyne Continental Motors Model IO-550-A engines in accordance with Colemill Enterprises Installation Instructions for Modification of Cessna model 310R in Accordance with Colemill Enterprises Inc. Drawing AC6200 Reissued 2/10/2011
SA2242SW Installation of Continental TSIO-520J engines Reissued 7/31/2012
SA2292WE Modification of waste gate controls. Issued 1/20/1971
SA2306CE Install Sperry MLZ-910 microwave landing system - MLS. Issued 11/12/1987
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
SA234CH Installation of Hartzell PHC-C3YF- FC7663D-2R with the associated spinner model C-4558-2P or C-4558-3(P). Amended 4/14/1997
SA234EA Installation of Chamberlain 2310K-B series radome kit. Amended 3/11/1970
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA237SO Modification of the control wheel. Reissued 11/29/1984
SA2383WE Installation of turbocharged Continental IO-470-D engine Reissued 7/3/2006
SA2404WE Consolidation of STC Reissued 9/30/2011
SA2406SW Addition of hydro seal fluid additive to nose and main gear shock strut. Amended 8/8/1990
SA240WE Consolidation of STCs SA355CE and SA362CE into one STC having MASTER ELIGIBILITY LIST - amended to include improved power supply assembly and subchassis timer assembly for Twilighter MK III high intensity supplementary lighting system. Issued 8/16/1971
SA248SO Increase takeoff gross weight to4 830 pounds. Reissued 11/29/1984
SA2504CE Installation of wing nacelle locker tanks and fuel transfer system. Reissued 10/15/1997
SA250CE Installation of Woodward electronic propeller synchraphaser system. Reissued 4/30/2007
SA2534WE Installation of Cessna 310P-type fiberglass tail stinger and yaw reduction adapter. Amended 5/30/1973
SA254SO Installation of swept vertical tail. Reissued 11/29/1984
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2586NM (PAGE 2) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA26SO Aerodynamic clean-up cabin sound- proofing new interior and cooling duct changes. Reissued 11/29/1984
SA2712 Installation of auxiliary fuel tanks saddle type and fuel cross-feed system.  Reissued 8/22/1974
SA272EA Installation of Chamberlain 2014K-B radome kit as follows: Kit No. 2014K-B for Bendix RDR-100 or RDR-110 radar systems with 12-inch antenna and transmitter receiver unit. Reissued 7/6/2005
SA2750SW Installation of Continental TSIO-520-E or -EB engine. Amended 9/20/2002
SA2784WE Installation of Ontrac II VLF 1000 very low frequency navigation system. Amended 12/3/1973
SA2832SO Installation of a combination radio/throttle/gust lock. Amended 12/3/2001
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2862SW CFS-2000 electronic fuel flow metering system. Reissued 1/30/1998
SA2872SW Installation of wing nacelle locker tanks. Reissued 7/5/1990
SA2880 Installation of nacelle changes and exhaust system changes using existing 0-478-B or 0-470-M engines. Reissued 5/1/1973
SA2903 Manufacture and installation of 1/4 inch thick plexiglass windshield.  Reissued 5/1/1973
SA294SO Installation of turbocharged Continental I0-470-D engines. S Reissued 7/3/2006
SA2960NM Install stay put (seat position locking device). Amended 3/14/1986
SA2996SO Installation of McCauley propeller governor (as shown in table on Page 2) in accordance with Colemill Enterprises installation instructions CM900-15 Rev. A dated July 5 1991. Reissued 2/10/2011
SA3-440 L-3 autopilot. Issued 1/1/1960
SA3-475 Full feathering constant speed propellers hubs 2AF36C26 blades90MF-10. Reissued 8/15/2006
SA3-55 Radio equipment. Issued 1/1/1960
SA3-636 M-4 flight control system with altitude controller. Issued 1/1/1960
SA3-643 Transa-Strobe beacon B-7228. Issued 1/1/1970
SA3-662 Installation of Woodward propeller unfeathering accumulator kit number210341. Reissued 3/20/1992
SA3-665 Cabin air temperature control system on Southwind (Stewart- Warner) 8240-A heater. Issued 1/1/1960
SA300CE Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) Amended 5/14/1992
SA3018SW-D Installation of Mitchell automatic flight system AK442 consisting of Century III autopilot with optional command/automatic electronic pitch trim system radio and glide slope coupler. Reissued 8/1/1984
SA3019SW-D Installation of Mitchell automatic flight system AK443 consisting of Century IV autopilot or AK443FD consisting of Century IV flight director autopilot with optional remote annuciator. Reissued 8/1/1984
SA3020SW-D Installation of Mitchell automatic flight system Model YK444 consisting of yaw damper. Amended 8/1/1984
SA302CE Installation of Hoskins High Intensity Position Light system. A supplemental condenser discharge (strobe) lighting system. Consists of red/green/white wing tip and tail position lights with or without white top and bottom fuselage lights plus a power supply.  Reissued 9/30/2011
SA303CE Installation of Bendix Model M-4B/C autopilot flight control system. Amended 2/20/1969
SA3078SW-D Auto flight system AK556 Century IV autopilot or AK556FD Century IV flight director. Reissued 10/14/1983
SA3079SW-D Mitchell yaw damper system YK 558. Reissued 6/19/1984
SA3082SW-D Installation of Mitchell automatic flight system AK557 consisting of Century III autopilot with optional radio and glide slope couplers. Amended 11/8/1984
SA3105SW-D Mitchell automatic flight system AK584 consisting of Century IIB autopilot with optional radio coupler. Reissued 5/24/1984
SA3235WE Installation of recognition light assembly on horizontal stabilizer. Issued 7/13/1976
SA3243WE Installation of pilot s and co- pilot s side vent windows. Issued 8/13/1976
SA325CE GUARD system (Gear Up Automatic Response Device). Issued 1/1/1960
SA3266WE Installation of ONTRAC III VLF/ Omega navigation system. Reissued 3/5/1998
SA3287WE Installation of Ontrac III or LRN-80 VLF/Omega navigation system as a means of VFR/IFR navigation enroute Rnav navigation. Reissued 2/10/1998
SA338SW Automatic pilot AK125. Issued 1/1/1960
SA3453SW-D Installation of Century Automatic Flight System Model AK958 consisting of a Century 2110/2130/2131/2150/2151 autopilot. Amended 1/26/1998
SA3454SW-D Installation of Century automatic flight Model YK959 consisting of a Century yaw damper installation. Issued 1/25/1987
SA347SW Cowling and exhaust system. Issued 1/1/1960
SA348WE Installation of air induction system in accordance with FAA Sealed Rajay Drawing list No. RJ1039. Reissued 7/3/2006
SA3522NM Installation of Precise flight series 400 speedbrake system. Amended 3/10/2005
SA3539NM Installation of ARNAV Systems FC-10/FT-10 digital fuel flow indicating system. Amended 7/9/1987
SA3602WE Installation of vapor cycle airconditioning system. Issued 3/6/1978
SA362CE Description of Type Design Change: Install Hoskins Twilighter  Reissued 9/30/2011
SA3671WE Installation of Fueltron IIIG or IIIP digital fuel flow indicating system. Reissued 4/29/1991
SA3729SW Install vacuum pump cooling shroud. Reissued 10/8/2001
SA3789WE Installation of 36-gallon auxiliary fuel tanks in each wing. (THRU S/N 310Q-0600) Reissued 7/5/1990
SA37SO Fuselage access holes in bottom skin of fuselage. Issued 1/1/1960
SA385WE Installation of turbocharged Lycoming IO-540-A1A5 engines in accordance with FAA sealed Rajay Drawing List No. RJ1000-100. Reissued 7/3/2006
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA3903WE Installation of Hoskins Model CFS-2000 or -2001 fuel flow indicating system. Reissued 1/30/1998
SA390WE Pitch assist PC-1 and optional altitude hold AH-1. Reissued 10/1/1973
SA391GL Installation of Great Lakes Aero Products windshield P/Ns W-2070 W/T-2070 or W/G-2070. Reissued 1/25/2007
SA3924WE Installation of ONTRAC IIIA or LRN-70 VLF/Omega navigation system as a means of VFR/IFR en route Rnav navigation. Reissued 2/10/1998
SA396EA Installation of Radome Kit No. 2310X-R. Reissued 4/15/1976
SA3RM Modification of engine exhaust stacks by replacement of expansion joint with slip fit joint. Reissued 10/1/1973
SA4-1217 Extension of augmenter tubes to trailing edge of wing. Issued 1/1/1960
SA4-127 56-gallon auxiliary fuel tank in hat rack compartment. Issued 1/1/1961
SA4-1400 SP-3 autopilot. Issued 1/1/1960
SA4-1598 Autopilot. Reissued 10/1/1973
SA4-239 Thompson TF2800 engine-driven fuel pump. Issued 1/1/1960
SA4-3 32-gallon auxiliary fuel tank in baggage compartment. Issued 1/1/1961
SA4-306 Roto-Nav bracket and Grimes D 7080 anti-collision light on vertical fin. Issued 1/1/1960
SA4-702 Full flow lube oil filter 30409A with element 1A0235. Issued 1/1/1960
SA4005NM (PG 2) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4011SW Installation of TSIO-520-N or TSIO-520-NB engines. Reissued 1/8/2001
SA4012SW Installation of dual camera port view finder hole camera mount for RMKA8.5/23 and RMKA 15/23 intervalometer and autopilot servo relocation. Reissued 10/8/2001
SA4024NM Replace the standard Cessna oil drain plug with a Bogert Aviation quick drain. Amended 4/12/1989
SA4055WE Installation of 81.6 gallon auxiliary wing fuel tanks Reissued 11/1/2012
SA407NW Installation of a Brittian Model B-4 flight control system Issued 2/11/1977
SA409SW Automatic pitch trim AK137. 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)