N321JE - 2004 DIAMOND DA40

2004

DIAMOND

DA40

Used

N321JE

DA40-180 with Garmin G1000, Premium Interior Package, Complete Logbooks The DA40 has accumulated a very low accident record, particularly with regard to stall and spin accidents. Its overall and fatal accident rates are one eighth that of the general aviation fleet and include no stall-related accidents. The level of safe operation is attributed to its high aspect ratio wing, low wing loading and benign flight characteristics in addition to the fuel tanks being placed between two carbon fiber spars. The aircraft can be trimmed full nose up, engine set to idle and it will descend at 600-1200 feet per minute at 48 knots (89 km/h) hands-off, a lower rate of descent than the competitive Cirrus SR22 can achieve with its airframe ballistic parachute deployed. In a 2011 analysis by Aviation Consumer magazine, the DA40 was shown to have a fatal accident rate of 0.35/100,000 hours, the lowest in US general aviation and considerably better that the Cirrus SR20 and SR22 with a combined fatal accident rate of 1.6/100,000 hours, despite its full aircraft parachute system. By comparison, the Cessna 172 has a fatal accident rate of 0.45/100,000 hours. Typical cruise speed is 140 knots burning 9.5 gallons per hours. With fuel fuel, you have 648 lbs. of people and baggage you can put in the cabin, which would give you a range of 448 miles (3.4 hours) with a 1 hour reserve. This is a two owner Diamond DA40 that has seen it?s maintenance treated with an open checkbook. Many desirable features are included with this aircraft include: 1.Increased Gross Weight Mod - 888 lbs. of useful load 2.XE Vision HID landing and taxi light 3.Standard 40 gallons of fuel (no aft CG issues) 4.Two bladed Scimitar propeller (less weight than the 3 bladed non-composite propeller 5.All software and SB?s are up to date on the G1000 (very important)

780.0

Total Time 780

780 Since new on Engine

780 Hours since new Hartzel Scimitar Propeller

DA40-180 with Garmin G1000 including: GDU 1040 Primary Flight Display GDU 1040 Multi-function Display Remote Avionics Equipment Mounting Rack with Line Replaceable Units GDC74 Integrated Digital Air Data Computer GRS77 Attitude & Heading Reference System Dual GNC53 Integrated VHF COM/NAV/ILS/GPS Radio Modules GTX33 Integrated "Mode S" Transponder with Traffic Information System GEA71 Airframe/Engine Interface Unit GMA1347 Digital Audio Controller with Digtal ATC Playback Recording GMU44 Magnetometer KAP 140 Autopilot with Altitude Hold & Preselect w/ G1000 Interface Standby instrumentation Garmin Integrated VFR Terrain Awareness System GDL69A Satellite Data Link - With XM Weather Integrally-lit, laser-etched polycarbonate switch panel overlay Sennheiser "Tip Power" ANR headset Jacks Tanis Engine Preheater System 4-way Baggage Compartment System Premium Care Package

Exterior Trim - Standard DA40 - Copper with Black Accent - Rated a 7.5

Interior Trim: DA40 - 2004 Premium Interior Package - Rated a 8.0

ELT Due 7/2015 IFR Due 7/2015 Annual Due 7/2014 Complete Logbooks Maitenace History: 2013 Update G1000 Soeftware to version 321.22 using STC. AD 2011-14-10 complied with and SB 342F as well 2012 New tires New races and bearings on wheels New emergency battery New G1000 fuses New rubber pad on right gear Complied with nose gear inspection Overhauled MFD 2011 Complied with MSB 40-046 and AD 09-10 nose gear inspection New Battery Complied with AD 10-25-01 rear passenger door retaining bracket Install M20 oil/air seperator AD 09-26-12 N/A ECI Cylinders are not installed Propeller dynamically balanced 2009 New Standby gyro emergency battery New rudder cable kit Completed with Ad 2009-10-04 for nose gear New brakes Complied with MSB 40-054 by reinforcing the pitot, static and stall warning line installation Compled with MSB 40-058 by installation of new circuit board assembly on the auxiliary wire to the alternator. Installed new fuel pump Replaced heater shroud Performed 500 hours mageneto inspeciton. Overhauled left mag, new right mag Compled with MSB 40-433 by inspecting exhaust system 2008 Gross weight increased completed 2 Year Compass calibration completed Nose gear 200 hour/12 month inspection completed Nose gear AD 2007-17-06 and Diamond MSB 40-046 completed no defects noted New landing gear tires Replaced turn coordinator Performed autopilot gyro alignment Replaced PFD Upgraded G1000 operating software from version -08 to -12 Performed transient voltage suppressor inspection per Diamond Removed and installed new alternator and battery scat hoses Complied with AD 2002-26-01 New rocker cover gaskets 2007 AD 07-11-21 Fuel selector shaft U joint completed next due 1302.9 Replace ELT battery Installed XeVision HID lighting for both taxi and landing lights Compled with AD 02-26-01 2006 Replaced insrument back up battery pack Replaced fuel pump Replaced faulty GDC 74A Adjustment to autopilot for heading being 10 degrees off 2005 MSB 40-0301 Fuel Selector U-Joint Inspection Completed Replaced the left and right main gear rubber strips Update G1000 system software SB 0519 Replace aircraft battery Installed GDL 69A Weather Receiver Performed SB 0553 Upgraded IGRF from version 2000.00 to 2005.00 Performed Service Bulletin 0522Replaced defective GDC-74A MSB 40-033 Exhaust Riser Inspeciton comleted Replaced all exhaust risers with improved risers from Diamond 2004 SB 511 on KAP 140 complete SB 0418 on G1000 complete Complied with Garmin Service 46901990 and 46901862 Aircraft Delivered Specifications and/or descriptions are provided as introductory information. They do not constitute representations or warranties of MultiCorp Aviation. The offer for sale of this aircraft is subject to contract and the aircraft may at any time be withdrawn from the market without prior notice. Specification is subject to verification by the purchaser and MultiCorp Aviation is not responsible for errors or omissions in such specifications and/or descriptions.