Cessna 336 SL

Number of Active Aircraft: 55 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 2320 lbs
Max Weight 3900 lbs
Useful Load: 1580 lbs
Engine Name CONT IO-360-C
Engine Number 2
Horsepower 210 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 19000 ft
Max Fuel 131 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 150 kts
GPH (75% BHP): 20.6
MPG (75% BHP) 7.3
Range (75% BHP): 864 nm
Fuel Cost Per Seat Mile 0.14 $
Fuel Cost Per Hour 123.6 $
MPG per 1000 lbs of Payload 11.5
F-T (Speed^2/FuelBurn) 10.9 HP
F-T Payload 17.2 kts
MPH To HP: 7.1 kts
T/O Roll - T/O over 50 FT OBST 790 ft / 1145 ft

SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
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
SA00192AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
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
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
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
SA00462AT Replacement of Appalachian stainless steel brake discs P/N 75-23 with Appalachian steel brake disk part number AA-47. Reissued 12/7/1994
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (4 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
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
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
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
SA01090AT Manufacture of flap gap seals. Issued 7/24/1996
SA01091AT Manufacture of mechanical cowl flap control system. Amended 2/20/2001
SA01093AT Manufacture of short takeoff and landing (STOL) kit and tail boom to vertical fin fairings. Amended 5/13/1997
SA01094AT Manufacture of modified Lightning Wingtips. Issued 7/24/1996
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
SA01158WI (1 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005
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
SA01215SE Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer and on both vertical stabilizers. Issued 5/13/2003
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
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
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 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
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 (1 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006
SA01933LA (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 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
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 2)  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
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 (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02446CH Installation of the Courtesy Light Kit. Issued 6/25/2007
SA02460AT Replace propellers with MT-Propeller Company model MTV-12 propellers per Coastal Planes installation manual. No intermixing of propellers is allowed. Amended 5/16/2006
SA02655AT (1 OF 2) Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. Amended 9/1/2004
SA02686AT Installation of air intake louvers on the rear engine lower cowl in accordance with Aviation Enterprises Installation Instructions dated June 15 2003 or later FAA approved revision.  Issued 7/21/2003
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
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
SA03100AT Installation of Wing Auxiliary Fuel Tanks. Issued 6/15/2005
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1056SW Revise wing contours leading edge and redesign landing light deflector plates. Reissued 4/27/1984
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1260CE Install FiQuench extinguishing system in cabin and/or fire extinguishant system in engine compartments. Reissued 12/15/1977
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
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
SA1355CE Chrome-plated brake disc installation. Issued 8/19/1977
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1675WE Installation of exhaust gas temperature monitoring systems EGT-2. Amended 8/28/1974
SA1800CE Installation of fire extinguishing system in cabin and/or fire extinguishant system in engine compartments. Reissued 2/1/1993
SA1875SW Wing edge leading cuffs wing tips vortex generators on fuselage and fairing on vertical tails. Reissued 9/15/1979
SA203SW Right front seat replaced with stretcher. Reissued 8/21/1987
SA2067NM Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System Amended 7/11/2012
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
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA250CE Installation of Woodward electronic propeller synchraphaser system. Reissued 4/30/2007
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
SA2820CE Installation of wing tips. Issued 4/17/1992
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
SA286NW Installation of drooped ailerons in flaps down mode recontoured wing leading edge stall fences aileron centering springs and conical cambered wing tips. Reissued 9/8/2005
SA3000SO Installation of Appalachian stainless steel brake discs No. 75-15A. Reissued 9/29/1995
SA3205SO Installation of Appalachian stainless steel brake discs. Reissued 9/29/1995
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4005NM (PG 2) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA406CE Installation of Hoskins Supplemental Position Light System which includes Model (A) Wing Tip Lights Model 2 Fuselage Light used as a Tail Light or the Model L Tail Light.  Reissued 9/30/2011
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA445SW Automatic pilot AK140 pitch trim system AK141 and lateral guidance radio coupler AK123. Issued 1/1/1960
SA5137NM Installation of sun visor. Amended 2/22/2005
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
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
SA615EA (PAGE 2) Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. Reissued 7/6/2010
SA71GL Installation of air filters Reissued 6/20/2000
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
SA8922SW Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) Issued 7/21/1994
SA917EA Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail P/N 30-0555-( ). Reissued 6/4/2007
SA936CE STOL Kit installation. Reissued 5/1/1977
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
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
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)