Cessna 195 B

Number of Active Aircraft: 124 Active- Map

Description:

Years Produced: 1952-54 The main change in the B model is just a reengining of the airplane to a 275 hp radial engine.

Wikipedia Cessna 190 reference:

218
Fuel Cost ($):
General Stats:
Seat Capacity: 5
Empty Weight: 2050 lbs
Max Weight 3350 lbs
Useful Load: 1300 lbs
Engine Name Jacobs R-755B2
Engine Number 1
Horsepower 275 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 16250 ft
Max Fuel 80 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 143 kts
GPH (75% BHP): 14
MPG (75% BHP) 10.2
Range (75% BHP): 725 nm
Fuel Cost Per Seat Mile 0.12 $
Fuel Cost Per Hour 84 $
MPG per 1000 lbs of Payload 13.28
F-T (Speed^2/FuelBurn) 14.6 HP
F-T Payload 19 kts
MPH To HP: 5.2 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1605 ft

SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00068LA Installation of tail wheel adapter ring. Amended 4/11/2002
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
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
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
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
SA00393SE Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. Issued 12/6/1996
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00412SE Installation of spoilers on the upper wing surface. Issued 2/27/1997
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00680SE (3 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00871WI Produce replacement left and right inboard aileron hinge brackets. Issued 5/25/2000
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
SA01068CH Installation of a BKS Aviation Heating System. Issued 6/29/1999
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
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
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
SA01287WI Installation of Jacobs R-755A and R-755B engines modified for fuel injection in accordance with STC SE01288WI. Data required: (1) Butterfly Aviation Master Drawing List Report BA1002-13 dated August 30 2004 (2) Butterfly Aviation Instructions for Continued Airworthiness Report BA1002-12 dated August 30 2004 and (3) FAA Approved Airplane Flight Manual Supplement dated November 17 2004 or later FAA Approved revisions to (1) (2) or (3).  Reissued 11/23/2004
SA01330LA (PAGE 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01406NY Installation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and );INSERT INTO stc_table VALUES ( rotary wing Amended 10/31/2012
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01458WI Modification involves fabrication and installation of new skins and doublers around the gearboxes and baggage door Issued 11/6/2007
SA01467AT Installation of a Navaid Devices AP-1 autopilot. Issued 9/4/1997
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
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (1 OF 5) Installation of an antenna Amended 2/15/2007
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
SA01801CH Installation of combustion heater kit P/N CD12091K11.  Issued 3/27/2003
SA01861SE (PAGE 1)  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
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
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 2)  Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02212AK (PG 1) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems  Amended 5/4/2011
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
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
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
SA02332AK Installation of a fixed mounted Forward.Vision Enhanced Vision System (EVS) Models 100/600 to include an under-wing conformal fairing with sensor and a glareshield mounted dedicated display monitor Issued 6/24/2009
SA02359AK-D Fabrication and installation of F. Atlee dodge Aircraft Services Cessna Tie-Down clamp  Issued 11/6/2009
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 5) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09167AC-D Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems Model ST-643-40/50. Issued 9/23/1996
SA09197AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-657 with Optional Autotrim System. Amended 10/2/2001
SA09291AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-735-20/30. Issued 10/29/1997
SA09332AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-736. Issued 1/27/1998
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA1005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Issued 7/23/2002
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA120NW Installation of Hartzell HC-B3P20-4/P10160-12E and/or 81HC-B3R20-4/R10160-12E propellers on Jacobs- Page R-755 series engines Amended 4/20/1977
SA1239GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1268SW Installation of Jacobs-Page R-755-S engine. Reissued 11/8/1999
SA1284CE Replacement axles. Issued 10/13/1976
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
SA1413NM Installation of two additional internal belly stringers Issued 4/28/1982
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA147CE Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. Issued 1/1/1960
SA1492WE Installation of Brittain Industries Inc. Model B2C Flight Control System Amended 2/1/2013
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1528GL Install retractable lifting handles Model H. Issued 10/17/1990
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1809SW Installation of Jacobs 6555-1 alternator with associated electrical system changes. Reissued 11/8/1999
SA199GL Installation of oil filter between engine oil gallery and propeller governor/nose case tappet rocker arm supply. Reissued 1/29/2007
SA2067NM Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System Amended 7/11/2012
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA220WE Conversion of aircraft for parachute jumping and aerial photography operations. Issued 1/1/1960
SA2298NM Installation of Cessna SC156001-0110 fuel filler caps. Reissued 7/2/2008
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2388WE Removal of left-hand exit. Issued 7/26/1971
SA2421CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON/2). Issued 10/7/1988
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
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA3-227 ARC L-11 loop and housing ARC ADF receiver R-30A and power unit and ARC control head. Issued 1/1/1960
SA308EA (1 OF 2) Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) Amended 11/20/1978
SA354SW Cargo conversion. Issued 1/1/1960
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4-1075 Full flow lube oil filter 30409A-12 with element 1A0235. Issued 1/1/1960
SA4-1275 Autopilot. Reissued 10/1/1973
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA42WE Eclipse Aviation generator 790-1B. Issued 1/1/1960
SA4302NM (PAGE 1) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4471NM Installation of Silver Instruments FUELTRON digital fuel flow indicating system. Reissued 6/10/2008
SA4546NM Installation of Cleveland Part No. 040-19900 Tail Wheel Assembly and 10 x 3.50  Reissued 6/10/2008
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA54GL Install Cleveland wheel and brake conversion kit P/N 199-61. Amended 4/1/1981
SA5581SW Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. Amended 9/30/2002
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA5658NM  Installation of a BAS Inc. tail pull handle in the aft fuselage.  Amended 12/2/2010
SA5678NM Installation of a fuel cap assembly. Reissued 12/23/1997
SA5715NM Left side passenger door manufactured and installed. Issued 5/13/1992
SA573CE Installation of block swivel action of crosswing gear. Issued 1/1/1960
SA589WE Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. Reissued 10/5/1976
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA630WE Installation of oil filter assemblies. (NAVION A AND B with optional engine) Reissued 8/29/1974
SA71GL Installation of air filters Reissued 6/20/2000
SA8031NM Installation of locking tail wheel strut. Reissued 7/2/2008
SA8150SW Installation of VENTUBE pilot/co-pilot overhead fresh air valves. (195 SERIES LC-126A LC-126B LC-126C) Reissued 12/29/2006
SA8909SW-D Installation of S-TEC System 60 two axis automatic flight guidance system Model St-565 with optional automatic electric trim system. Issued 1/1/1960
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01458WI This modification involves fabrication and installation of new skins and doublers around the gearboxes and baggage door.  Issued 11/6/2007
ST01494LA (PG 1) Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. Reissued 8/30/2011
ST01700NY (1 OF 2) Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature Indicator CHT-100 Cylnder Head Temperature INdicator FL-100 Dual Fuel Level Indicator FP-100 Fuel Pressure and Ammeter Indicator OL-100 Oil Pressure and Temperature Indicator and VA-100 Voltmeter and Ammeter Indicator. Issued 7/8/2003
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)