Cessna 337A

Number of Active Aircraft: 85 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 2615 lbs
Max Weight 4200 lbs
Useful Load: 1585 lbs
Engine Name CONT IO-360-D
Engine Number 2
Horsepower 210 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 20500 ft
Max Fuel 131 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 167 kts
GPH (75% BHP): 21.8
MPG (75% BHP) 7.7
Range (75% BHP): 905 nm
Fuel Cost Per Seat Mile 0.13 $
Fuel Cost Per Hour 130.8 $
MPG per 1000 lbs of Payload 12.14
F-T (Speed^2/FuelBurn) 12.8 HP
F-T Payload 20.3 kts
MPH To HP: 8 kts
T/O Roll - T/O over 50 FT OBST 805 ft / 1435 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
SA00080LA Installation of Teledyne Continental TSIO-520-NB engine and Hartzell three bladed propellers. Reissued 11/10/2009
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
SA00199AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-25A. Reissued 11/14/1994
SA00243BO (3 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
SA00272WI Replacement of hydraulic system pressure switch. Reissued 11/8/2007
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
SA00409AT Installation of Cessna 02A entry door (P/N 1517080-1) and wind deflector. Issued 1/21/1994
SA00410AT Design fabrication and installation of upper and lower windshield retaining gussets. Issued 1/21/1994
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
SA00556AT Installation of Appalachian Accessories carbon steel brake discs P/N AA-27A. Reissued 1/24/1995
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
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
SA00812CH Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. Reissued 6/30/2006
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00897WI Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Issued 8/11/2000
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
SA00972LA Installation of Teledyne Continental Motor Pressurized Magnetos Kit No. EQ6565. T337G s/n P3370001-P3370292 except P3370109 & P3370196 P337H S/N 3370293-3370356 & P3370196 Reissued 11/10/2009
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
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
SA01179AT Installation of an external cargo Pod. Amended 4/2/2001
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
SA01330LA (PAGE 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01344AT Installation of a baggage door on the aft right side of the fuselage. Issued 4/15/1997
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
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 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
SA01888AT Installation of a composite structure baggage door in RH side of the fuselage. Issued 4/27/1999
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
SA01985AT Installation of a fuel jettison system. Issued 11/5/1999
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
SA02017AT Installation of a Wescam FLIR System NSI Microwave System and an Operator s Console. Issued 10/29/1999
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02023AT Installation of a fuel transfer system to transfer fuel from a wing tip extension fuel tank to the main wing fuel tank. Issued 11/7/1999
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
SA02055AT Installation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions Revision D dated January 13 2000 or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII Revision C dated August 17 1999 or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs. Amended 7/3/2003
SA02056AT Installation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions Revision D dated January 13 2000 or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII Revision C dated August 17 or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs. Issued 1/14/2000
SA02094SE  Installation of a CO Guardian 452R Carbon Monoxide Detector per AeroMech Inc. Master Data List document AM0243-DL02-00 Revision A  Issued 1/31/2011
SA02095AK Installation of hourmeter airspeed switch. Issued 12/10/1997
SA02110CH (PAGE 2) 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 (3 OF 5 Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004 0:00
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 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
SA02307AT Installation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions Revision D dated January 13 2000 or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII Revision C dated August 17 or later FAA approved revisions. Amended 12/28/2004
SA02308AT Installation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions Revision D dated January 13 2000 or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII Revision C dated August 17 1999 or later FAA approved revisions.  Amended 12/28/2004
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
SA02510AT Installation of a rear firewall engine accessory access door. Issued 5/14/2002
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02527AT Installation of a landing gear in-transit warning light in 337 models that are equipped with an electric motor to retract landing gear instead of engine driven hydraulic pump. Issued 5/31/2002
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
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
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
SA03618AT Installation of Teledyne Continental Motors Model IO-550-N engines Hartzell Model PHC-G3YF-2UF/F7663D-2R propeller front Hartzell Model PHC-I3YF-2AL/FLC7663DF-2 propeller rear front and back AirScan engine installations and 5120 pounds Maximum Gross Weight Amended 2/13/2009
SA09120AC-D Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-603 with optional autotrim system. Amended 4/19/2001
SA09419AC-D Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-869-20/30. Issued 10/25/1999
SA1021SW Flap on switch on control wheel. Reissued 9/20/1977
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
SA1205CE 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
SA1258CE Installation of FIQUENCH fire extinguishing system in cabin and/or fire extinghishant system in engine compartments. Reissued 12/15/1977
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1273GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA1356CE Chrome-plated brake disc installation. Issued 1/16/1978
SA1359SW Mitchell automatic flight system FD/AP282-345 consisting of flight director/autopilot with optional automatic pitch trim. Reissued 7/10/1984
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1473CE Installation of Tull microwave landing system with modified King KX175B and KN 73 receivers. Issued 2/12/1979
SA1478SW Mitchell automatic flight system AK345 consisting of Century III autopilot with optional automatic pitch trim radio coupler and glide slope coupler. Reissued 7/10/1984
SA1494SW Installation of Mitchell flight director remote annunciator Model AK375. Amended 7/10/1984
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1520SW Mitchell automatic flight system AK400 consisting of Century IIB autopilot with optional radio coupler. Reissued 7/13/1984
SA1546GL Installation of on-board engine analyzer system. Issued 1/4/1991
SA1558SW Installation of vortex generators wing leading edge cuffs wing tips fairings de-icing boots and stall strips. Amended 1/28/1982
SA1568SO Installation of Sorensen external fuselage insecticide spray tank and associated spray equipment. Issued 1/18/1984
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
SA1627WE Installation of drooped ailerons in flaps down mode recontoured wing leading edge stall fences aileron centering springs conical cambered wing tips and flap actuated elevator trim spring. Reissued 9/8/2005
SA1675WE Installation of exhaust gas temperature monitoring systems EGT-2. Amended 8/28/1974
SA1762NM Installation of a pressurized magneto system on the Continental turbocharged TSIO-360-C F and FB engines. Reissued 3/14/2006
SA1801CE Installation of fire extinguishing system in cabin and/or fire extinguishant system in engine compartments. Amended 5/30/1995
SA1823NM Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4 1983 together with their FAA sealed Installation Instructions dated September 20 1982 or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6 1982 LAS 1013 dated October 5 1982 and LAS 1014 dated October 6 1982 or later FAA approved sealed revisions. Reissued 1/23/2004
SA1877NM Installation of Hoskins Model CFS-2000A -2001A FT-200 fuel flow indicating system. Reissued 1/30/1998
SA190SO Cabin door removed and wind deflector installed. Issued 1/1/1961
SA1922SW Installation of Mitchell automatic flight system AK404 consisting of Century IIB autopilot with optional radio coupler. Reissued 8/1/1984
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
SA2200WE Installation of Brittain Industries Model B2C and BSS Flight Control Systems Reissued 7/2/2013
SA2242SO Installation of external fuselage insecticide spray tank and associated dispersal equipment. Reissued 2/18/1996
SA2335WE Installation of one-piece windshield and relocation of compass. Reissued 8/16/2011
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2364CE Replacement of right front seat with stretcher. Issued 3/18/1988
SA2492SO Installation of Appalachian Accessories stainless steel brake discs P/N 75-25A. Reissued 9/29/1995
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
SA2619WE Installation of Pathfinder Model P1-( ) autopilot system. Reissued 9/30/1998
SA2620WE Installation of Pathfinder Model P2-( ) autopilot system. Reissued 9/30/1998
SA2654WE Installation of Pathfinder Model P2A( ) autopilot. Amended 7/3/1979
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
SA2821CE 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
SA2858SO Installation of a FLIR airborne surveilance system. Reissued 5/5/2010
SA3056WE Installation of fuel flow instruments. Issued 8/15/1975
SA3148SW-D Mitchell automatic flight system AK537 consisting of Century III autopilot with optional radio coupler and glide slope coupler. Reissued 6/6/1984
SA3149SW-D Mitchell automatic flight system AK536 consisting of Century IV autopilot or Model AK536FD consisting of a Century IV flight director autopilot with optional remote annunciator. Reissued 6/6/1984
SA3240SO Removal of main landing gear wheel doors and actuators which are replaced with a fixed composite panel containing a cutout for gear passages. Amended 12/8/1993
SA3250SW-D Mitchell automatic flight system AK404 consisting of Century IIB autopilot with optional radio coupler. Amended 8/12/1993
SA3252SW-D Mitchell automatic flight system AK400 consisting of Century IIB autopilot with optional radio coupler. Reissued 3/28/1984
SA3258NM Installation of ARNAV systems FC-10/FT-10 digital fuel flow indicating system. Issued 6/6/1986
SA32RM Installation of electrically driven freon air-conditioning system. Reissued 5/17/2013
SA3729NM Installation of electric heater and auxiliary alternator. Issued 6/25/1987
SA3818WE Installation of Fueltron IIIG or IIIP digital fuel flow and totalizer system. Reissued 4/29/1991
SA385GL Installation of Norton radome kit No. 4231X. Reissued 4/17/1981
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA3863NM Installation of American intercooled engines as modified by STC SE3864NM. Amended 11/1/1998
SA4005NM (PG 2) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4024NM Replace the standard Cessna oil drain plug with a Bogert Aviation quick drain. Amended 4/12/1989
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
SA4166NM Installation of Fairchild voltage regulator No. UA78 GUIC to replace the original voltage regulator in Cessna turn coordinator P/N 0661003-0506. Issued 1/25/1988
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4504NM Installation of an Intercooler in the air induction system of both engines. (T337G S/N P3370001 - P3370292 EXCEPT P3370109 AND P3370196) (P337H S/N P3370293 - P3370356 AND P3370196) Reissued 11/10/2009
SA4526NM Limited to installation on serial number P3370109 ONLY. Installation of intercoolers in air induction system of both engines. Issued 1/27/1989
SA478NW Installation of Bendix RDR 160 weather radar system. Amended 9/25/1979
SA482SO Installation of Bendix FCS-810 automatic flight control system including manual electric trim and flight director indicator. Amended 7/2/1976
SA491SW Automatic pilot AK135 automatic pitch trim AK156 and lateral guidance radio coupler AK123. Issued 1/1/1960
SA4961NM Installation of a NSA sunvisor system for the pilot and copilot. Reissued 3/24/2003
SA5017NM Installation of an inflatable door seal. Reissued 11/10/2009
SA5033NM Installation of Teledyne Continental Motor pressurized magnetos kit no. EQ6565. (T337G S/N P3370001-P3370292 except P3370109 and P3370196) (P337H S/N P3370293-P3370356 and P3370196) Reissued 11/10/2009
SA5090NM Installation of a nineteen and a half(19.5 U.S.) gallons wing tip fuel tank on each wing tip. Reissued 2/25/2000
SA5114NM Installation of spoiler system. Reissued 7/9/2013
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5176NM Installation of an ADC Corporation Model 5001A engine pre-oiler system Issued 8/10/1991
SA5495NM Installation of an engine driven air conditioning system. Reissued 11/10/2009
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
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
SA593CH (2 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
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
SA638GL Installation of a Shadin Co. 910516 fuel flow indicating system. Reissued 6/8/2006
SA660WE Installation of HRD-type fire extinguishing system. (AND STC SA111WE) Reissued 2/4/1987
SA668SW Installation of Mitchell automatic flight system Model AK210 consisting of Century III autopilot automatic pitch trim automatic aileron stabilizer and radio coupler. Reissued 6/25/1984
SA672CE Install auxiliary fuel tank in rear baggage area. Reissued 6/23/2006
SA678CE Install fuselage top emergency exit door. Reissued 6/23/2006
SA704NW Installation of a Hoskins CFS 2000 computerized fuel system Issued 1/15/1979
SA71GL Installation of air filters Reissued 6/20/2000
SA7203SW-D Installation of S-TEC System 65 Two axis Automatic Flight Guidance System Model ST-313. Reissued 2/27/1990
SA7208SW-D Installation of S-TEC system 65 two axis automatic flight guidance system Model ST-313. Issued 2/27/1990
SA7209SW-D Installation of S-TEC System 60 Two Axis Automatic /Flight Guidance System with Optional Autotrim System Model ST-314. Issued 4/6/1990
SA7774SW-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems model ST-317-40/50. Issued 6/15/1990
SA7808SW-D Installation of S-TEC System 60 pitch stabilization system model ST-478 with optional automatic electric trim system. Issued 1/1/1960
SA798EA Installation of Monitair exhaust gas combustion monitor kit. Reissued 2/14/1972
SA8008SW Installation of Zeftronics alternator control units P/N s R25101 (27.7V systems) or R25102 (28.8V systems). Reissued 5/12/1998
SA801SW Mitchell automatic flight system AK244 Century II autopilot with optional radio coupler. Reissued 6/29/1984
SA808SW Installation of Mitchell Model AK246 omni-tracker. Applicable only to aircraft modified by STC SA615SW. Reissued 6/29/1984
SA8367SW-D Installation of System 65 two axis automatic flight guidance system Model ST-506. Issued 3/25/1993
SA8368SW-D Installation of System 65 two axis automatic flight guidance system Model ST-506. Issued 3/25/1993
SA8371SW-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-510. Issued 8/17/1993
SA8372SW-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-510. Issued 8/17/1993
SA842SW Mitchell automatic flight system AK252 consisting of Century III autopilot with optional automatic pitch trim automatic aileron stabilizer and radio coupler. Reissued 6/29/1984
SA8533SW-D Installation of a Century Automatic Flight System. Amended 8/8/2003
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
SA937CE Installation of leading edge cuffs stall fences droop wing tips and vortex generators on rear engine lower cowling. Amended 10/4/1990
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
ST01548LA Installation of external landing gear position verification mirrors and aft engine cowl observation mirrors. Reissued 8/16/2004
ST02307CH Installation of Rudder Pedal Extensions. Amended 10/13/2006
ST02547AT (1 OF 2) Installation of a voice alert system. Amended 5/13/2003
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)