Number of Active Aircraft: 3 Active- Map


If you feel like you have a particular interest in this model of aircraft you are welcome to submit a brief history and description/points of interest that make this model unique.

Please send descriptions to


Have an Update?
Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 2608 lbs
Max Weight 4300 lbs
Useful Load: 1692 lbs
Engine Name Lycoming TIO-540-AE2A
Engine Number 1
Horsepower 350 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 25000 ft
Max Fuel 120 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 225 kts
GPH (75% BHP): 24
MPG (75% BHP) 9.4
Range (75% BHP): 994 nm
Fuel Cost Per Seat Mile 0.11 $
Fuel Cost Per Hour 144 $
MPG per 1000 lbs of Payload 15.86
F-T (Speed^2/FuelBurn) 21.1 HP
F-T Payload 35.7 kts
MPH To HP: 6.4 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 2375 ft

SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00063LA Installation of Acoustical/Thermal insulation. Reissued 1/5/2005
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
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 (3 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
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
SA00185WI Remove existing headliner in cockpit and cabin and replace with new headliner. Issued 8/10/1994
SA00243BO (4 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00269BO (3 OF 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
SA00282BO Installation of Avidyne Corporation Entegra Integrated Flight Display System Amended 4/4/2013
SA00290BO ( PAGE3) 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 0:00
SA00310BO  Issued 11/7/2011
SA00380AT Replace TCM TSIO-520-BE with Continental TSIO-550C. Reissued 2/18/2003
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00520SE Installation of Precise Flight Speedbrake System. Amended 1/8/2008
SA00590CH Installation of BFGoodrich Aerospace SMARTboot system. Amended 6/27/1997
SA00656WI-D Installation of Bendix/King KFC 225 Automatic Flight Control System. Reissued 2/28/2000
SA00680SE (5 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00780SE (PAGE 1) 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
SA00859AT Installation of an additional fuel filler opening and cap outboard of the standard filler cap to allow the carriage of 10 additional gallons per side. Reissued 2/18/2003
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA01006WI-D Installation of Bendix/King KMD 850 Multi-Function Display System and the optional Bendix/King KMH 980/KMH 880 Multi-Hazard Awareness Systems/KTA 870 Traffic Awareness System/KTA 970 Traffic Alert and Collision Avoidance System and KDR 510 VHF Datalink System. Amended 6/6/2002
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
SA01079NY Installation of Eventide Argus 7000CE Moving Map Display with the ALT-1001-00 Altitude Encoder Adapter. Issued 9/8/1999
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
SA01147WI Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Reissued 7/30/2012
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01205WI-D (2 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
SA01224AT Installation of wheel hub cabs with valve stem access door. Amended 4/17/1998
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (4 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 3) Installation of alternate avionics support assembly. Reissued 10/6/2010 0:00
SA01340CH Installation of a Hartzell HC-13YR-1E/7890(K)propeller and D-6750-(P) spinner. Issued 11/20/2000
SA01435DE Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine.  Reissued 5/25/2011
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01473SE (4 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 2) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01533WI-D Synthetic Vision and Pathways Upgrade to the G1000 Integrated Avionics System Amended 12/11/2009
SA01542AT Modify PA-46-310P aircraft equipped with TCM TSIO-550-C engines per STC SA00380AT by replacing Hartzell 2 Blade Propeller Model BHC-C2YF-1BF/F8052 and Spinner Assembly with MT 4 Blade Propeller MTV-14-D/195 30a and spinner assembly. Reissued 11/13/2002
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
SA01616CH Installation of Hartzell PHC-G3YF-1E/7890(K) Propeller and C3535-3(P) spinner. Issued 1/24/2002
SA01625SE Cockpit Sun Visor installation Issued 12/15/2005
SA01654AT Installation of MT-Propeller four blade model MTV-14-B/195-30a. Reissued 11/13/2002
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (4 OF 5) Installation of an antenna Amended 2/15/2007
SA01705WI Installation of the Garmin G950 Integrated Flight Deck Installation Issued 12/20/2012
SA01750SE Fabrication of Dahlia Doubler. Reissued 8/24/2011
SA01751SE Fabrication of Panida Doubler. Reissued 8/24/2011
SA01752SE Fabrication of Panida Doubler. Reissued 8/24/2011
SA01770CH Installation of a Teledyne Continental TSIO-550-C1B model engine Hartzell PHC-G3YF-1E/7890K propeller with a spinner assembly C-3535-3P and engine cooling kit. Reissued 2/27/2009
SA01800SE (PG 3) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01843CH Replacement of certain BFGoodrich pneumatic deicer boots. Amended 6/2/2008
SA01848AT Installation of Cockpit Display System. Issued 3/2/1999
SA01860NY (2 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 4)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01896CH Installation of engine cooling kit. Amended 4/28/2009
SA01933LA-D Page 2 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (4 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01969SE Installation of a Mid-Continent MD302 Standby Attitude Module Issued 1/17/2014
SA01988SE (PAGE 6) 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
SA02018SE-D (PAGE 2) Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) SA02018SE-D dated January 4 2011 or later FAA approved revision and FAA Approved GPS/XM Antenna STC Master Drawing List Document No.: 005-00638-01 Revision 1 Issued 1/4/2011 0:00
SA02019SE-D Page 2 Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/19/2012
SA02033AT (PAGE 4) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008 0:00
SA02033AT (PAGE 6) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008 0:00
SA02079CH Installation of a vacuum system upgrade. Issued 12/20/2004
SA02093AK Installation of hourmeter airspeed switch. Issued 10/17/1997
SA02110CH (PAGE 3) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02154AK (PAGE 2) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005 0:00
SA02168AK (PG 1) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001
SA02203AK (PAGE 3)  Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02217AK (4 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004 0:00
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 5) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02276AK Installation of AMSAFE Aviation Inflatable Restraints Amended 3/12/2013
SA02283SE Page 2 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
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02532AT Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. Issued 6/5/2002
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02677CH-D Installation of Hartzell HC-I3YR-1N/N7605(K)+2 or HC-I3Y1R-1N/N7605(K)+2 propellers Issued 3/13/2009
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 2) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02779AT Modification of the Engine Mount Assembly Amended 12/3/2013
SA03148NY (PAGE 2 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03188CH Installation of LED Taxi Light Assemblies Issued 2/27/2013
SA03308AT Installation of a Light Assembly to Illuminate the Right Horizontal Stabilizer for the Inspection by the Pilot of Ice Accumulation  Issued 8/7/2006
SA03825AT-D Installation of a Forward Vision EVS-100 and EVS-600 Infrared Camera System in the Piper PA-46-310P PA-46-350P and PA-46-350T Models Reissued 3/9/2010
SA04005AT  Installation of Garmin GSR 56 System Issued 5/13/2013
SA09021SC-D Installation of TSIO-520-BE. Reissued 8/11/2008
SA09354SC Installation of a heated pilot s windshield. Issued 7/23/1997
SA09402AC-D Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance Systems Model ST-854 with Autotrim System Yaw Damper System and Flight Director/Steering Horizon. Amended 12/12/2000
SA09430AC-D Installation of S-TEC System 550 Flight Director/Autopilot with trim yaw damper and altitude selector alerter Model ST-845. Issued 9/27/2000
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09521AC-D Installation of S-TEC Digital Flight Control System (autopilot) Part No. 01298-01-01-001 or 01304-01-01-001 1500 Autopilot with Autotrim and Yaw Damper System per Report 97-13001-003 Revision 2 dated 9/23/2003  Reissued 12/10/2008
SA09524SC Conversion of existing Piper air conditioning system from R12 to R134a refrigerant. Amended 3/26/2002
SA09830SC Installation of an entertainment cabinet. Issued 9/25/2000
SA10107SC Installation of a #2 direct drive vacuum pump using installation instruction document number 0001 dtd 2/2/02. Reissued 3/15/2005
SA10196SC Modification of engine mount part number 89137-041 to improve nose landing gear actuator attach point. Issued 10/7/2003
SA10220SC Installation of EFG-proprietary modified J.P. Instruments EDM-700/800 engine monitor and replacement of factory-installed TIT probes to be used as the aircraft Amended 6/8/2005
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10270SC Installation of EFG Model 1074 aerodynamic two-piece composite fairings in accordance with and type inspection data is contained in Master Drawing List No. 12010-0000 Revision A dated 05/04/2004 or later FAA approved revision. Required instruction for continued airworthiness is contained in installation instructions referenced in Master Drawing List No. 12010-0000 Revision A dated 05/04/2004 or later FAA approved revision.  Issued 7/28/2004
SA1067NE Installation of a capacitance based ice detection system. Issued 3/10/1993
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1538GL Installation of on-board engine analyzer system. Issued 11/23/1990
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 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1778CE-D Installation of KAP 100 single-axis KAP 150 two-axis or KFC 150 two-axis flight control system. Reissued 2/28/2000
SA1793CE-D ONE ONLY STC SN 46-8508024: Installation of King KNS 660 Multi-Sensor Mangement System. Reissued 2/28/2000
SA2167NM Installation of the Precise Flight stand-by vacuum system (SVS). Amended 11/7/2003
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 4) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2687NM (PAGE 2) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000 0:00
SA2787NM Installation of photovoltaic battery charging system. Reissued 7/24/1987
SA3202NM Installation of Hoskins Model CFS 1222 fuel flow indicating system. Reissued 1/30/1998
SA3639SW Installation of ARNAV Systems Loran C Model R-40 with remote data base. Issued 7/31/1986
SA3781SW Installation of ARNAV Systems Model FC-10 or FT-10 fuel flow system. Issued 5/7/1987
SA3862NM Page 2 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5156NM (PG 2) Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 7/29/2010 0:00
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA5196NM Installation of spoilers system. Reissued 7/9/2013
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
SA593CH (3 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA5982SW Installation of Texas Instruments TI9200 Loran C navigation system. Amended 10/31/1985
SA6018NM Installation of an electronic digital engine tachometer Model P-1000 P/N P100074-. Reissued 1/14/2002
SA7515SW Installation of tail floodlights on horizontal stabilizer. Amended 3/7/1990
SA7642SW Camera hole installation. Reissued 6/1/2011
SA824GL Installation of digital fuel management system. Reissued 6/8/2006
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
SA8961SW-D Installation of Slick 6320 pressurized magnetos. Approved for serial numbers 46-8408001 through 46-8608067 and 4608001 through 4608140 only. Reissued 9/11/2008
SA8962SW-D Installation of RAM baffle material. Reissued 9/11/2008
SA8963SW-D Modification of a Piper Malibu nose wheel door for better engine cooling Reissued 9/11/2008
ST00541SE Installation of a Pratt & Whitney PT6A-34 engine rated at 560 HP 2200 RPM or as an option a Pratt & Whitney PT6A-35 engine rated at 560 HP 2190 RPM or as an option a Pratt & Whitney PT6A-21 engine rated at 550 HP 2200 RPM and an eligible propeller from Table 1 Page 3 and associated hardware in accordance with Rocket Engineering Master Drawing List 560.00.000 Revision AP dated September 14 2007 or later approved revision. Amended 5/16/2011
ST00961LA Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29 2000 or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1 Slug Thrower Cartridges Master Drawing List Reissued 7/13/2011
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01468CH Installation of various SMR Technologies electrical propeller deicer models. Amended 7/25/2006
ST01851NY Installation of Piper Mirage PA46-350P Pilot s Heated Windshield. Issued 12/31/2003
ST02547AT (2 OF 2) Installation of a voice alert system. Amended 5/13/2003
ST09524SC Piper conversion of air conditioning systems from using R12 to R134a refrigerant on aircraft models listed. For PA-31-300 s/n 31-660 31-712 thru 31-900 31-7300901& up. For PA-31-325 sns 31-7400990 & up. PA-31-350 sns 31-5001& 31-5003 31-7305005 up Amended 3/28/2000
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
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
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
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
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)


Subscribe To Our Newsletter

Join our mailing list to receive the latest news and updates from our team.

You have Successfully Subscribed!