AMD Alarus CH2000

Number of Active Aircraft: NA Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 1085 lbs
Max Weight 1692 lbs
Useful Load: 607 lbs
Engine Name LYC O-235-N2C
Engine Number 1
Horsepower 116 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 0 ft
Max Fuel 28 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 99 kts
GPH (75% BHP): 5.2
MPG (75% BHP) 19
Range (75% BHP): 446 nm
Fuel Cost Per Seat Mile 0.16 $
Fuel Cost Per Hour 31.2 $
MPG per 1000 lbs of Payload 11.56
F-T (Speed^2/FuelBurn) 18.8 HP
F-T Payload 11.4 kts
MPH To HP: 8.5 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 0 ft

SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA01229SE Page 2 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
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
SA01629LA Installation of AM-Safe Inflatable Restraint System on pilot and co-pilot seats of the Zenair CH-2000 in accordance with FAA Approved AMSAFE Master Data List E508452 Revision B dated April 7 2004 or later FAA approved revision and the FAA Approved Flight Manual Supplement E508440 Revision NC dated April 26 2004 or later FAA approved revisions. Issued 4/28/2004
SA01692SE (Page 2 of 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (5 OF 5) Installation of an antenna Amended 2/15/2007
SA01714WI (Page 2) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
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 (5 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01988SE (PAGE 4) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
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
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02153LA-D (Page 2) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
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
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
SA02283SE Page 2 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 3) 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 2 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA10236SC (1 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
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 (5 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
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Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
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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
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Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
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Instrument Panel
Flight Control
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Heating
Window Defrost
Cooling
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Maximum Climb Profile Speed (KIAS)
Engine
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Cooled
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Propeller Manufacturer
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Maximum Diameter
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Propeller Governor
Fuel System
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Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
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Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
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Electrical System
Power Source
Power Storage
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Alternator Amp
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Limitations
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Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
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Wing Loading (lbs/sq.ft)
Vne (KCAS)
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