S /N 54022

2011 BELL 407S/N 54022

N897KV

+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com

mailto:[email protected][email protected]&subject=%202011%20Bell%20407%20-SN:54022%20Inquiry

https://iada.aero/

*Specifications as of 07/01//2021. Specifications are subject to verification upon inspection and should not provide a basis for reliance or create any other binding obligation.

HIGHLIGHTS

201 1 BELL 407 | SN 54022

ENGINE STATUS

AIRFRAME STATUS

SERIAL NO: 54022REGISTRATION: N897KVMFR YEAR: 2010DELIVERY YEAR: 2011TOTAL TIME: 1,376TOTAL LANDINGS: 2,154

Rolls-Royce Model 250-C47BGas Turboshaft Engine w/ FADEC (Full Authority Digital Electronic Control) and Direct Reversion to ManualGovernor

TSN: 1,376CSN: 1,706TBO: 2,000Program: -

MAINTENANCE


ADS-B OUT COMPLIANT

GARMIN GPSMAP® 696

OPTIONAL HIGH SKIDGEAR W/ AAI FLIGHTSTEPS

CORPORATE SEATING

CORPORATESOUNDPROOFING

MARKINGS FOR HIGHVISIBILITY M/R BLADES(WHITE & ORANGE)

Paint: Passion Red, BlackStripes, White Rear-BottomInterior: 2 PilotsCorporate Seating

2 Extra Wide ForwardFacing Outboard Seatsand a Middle Seat forOccasional Use Acrossthe Rear of the Cabin(w/fold-down armrestbetween the outboardseats)2 Individual RearwardFacing Seats Aft of theCockpit.

INTERIOR & EXTERIOR

FL IGHT & ENGINE INSTRUMENTSGARMIN GPSMAP® 696GARMIN GNS 430Clock, Digital w/ OAT & Volt MeterCompass, MagneticDual Tachometer (Rotor and Engine)InclinometerIndicator, Airspeed.Indicator, Altimeter.Indicator, IVSIIndicator LCD, Engine Oil Pressure /TemperatureIndicator LCD, Fuel Quantity with Forward CellQuantity SwitchIndicator LCD, Fuel Pressure / Generator LoadMeterIndicator LCD, NG Speed w/ EXCEEDANCEMONITERINGIndicator LCD, Torque w/ EXCEEDANCEMONITERINGIndicator LCD, Transmission Oil / TemperatureIndicator LCD, T.O.T. w/ EXCEEDANCEMONITERINGHour Meter (Located in Battery Compartment)Maintenance Download Ports (FADEC & LCDInstruments

ROTORS AND CONTROLS

Main Rotor, soft in-plane flex beam hud withfour fiberglass blades, Tail Rotor: two fiberglass blades, semirigidHydraulic boost system for Main & Tail Rotor(separate pump and reservoir) Mechanical Flight Control Linkage throughoutAirspeed Activated Pedal Stop (AAPS) withbuilt-in test function, electrical overriderelease switch, and manual override release.

TRANSMISSION DRIVE SYSTEM

Soft Mounted Pylon Isolation SystemFreewheeling unit (between the engine andmain transmission)Kaflex Input Drive ShaftGearbox, Tail Rotor, 90 Deg Reduction. Main TransmissionOil CoolerOil Filter with Replaceable Type CartidgeOil Pump, Constant Pressure

ADDIT IONAL EQUIPMENT

Optional High Skid Gear w/ AAI FlightstepsCorporate SeatsCorporate SoundproofingGARMIN GPSMAP® 696GARMIN GNS 430Snow Deflector Kit BHT-407-II-4Dual Control Quick Disconnect Kit BHT-407-II-9

10-15hr T/R D/S Side Pack Retorque - Completed08/202150hr/3 Month Lube Items - Completed 08/2021

12 Month Inspection - Due Nov 2021150 hr. AD 2015-05-04, due at ACTT 1496.8


https://aircraftexchange.com/aircraft-by-broker/160/leviate-air-group

*Specifications as of 07/01//2021. Specifications are subject to verification upon inspection and should not provide a basis for reliance or create any other binding obligation.

201 1 BELL 407 | SN 54022


DIMENSIONS

Length: Height: Width:

Length:Height: Width:Cabin Volume:Baggage Volume:

R a n g eRange: 328 nm - 607 km

Normal: Ceiling: (HOGE) Out of Ground Effect:(HIGE) In-Ground Effect:

Standard: Standard: Optional: Optional:

Max. Takeoff: Empty Operating Weight (EOW): Basic Operating: Max Baggage Weight

PERFORMANCE

C l i m b

F u e l C a p a c i t y

W e i g h t

1,940 f/m - 9.9 m/s20,000 ft. - 6,096 m10,400 ft. - 3.170 m12,200 ft. - 3,719 m

858 lbs. - 389 kg.128 gals. - 485 ltr.127 lbs. - 58 kg.19 gals. - 72 ltr.

5' 0" ft. - 1.5 m3' 8" ft. - 1.2 m3' 9" ft. - 1.2 m

85 cu ft. - 2.4 m^316 cu ft. - .45 m^3

34.2 ft. - 10.4 m11.8 ft. - 3.6 m

7.5 ft. - 2.3 m

5,000 lbs. - 2,268 kg.2,598 lbs. - 1,178 kg.3,798 lbs. - 1,723 kg.

250 lbs. - 113 kg.

F u s e l a g e

C a b i n

MONITORING SYSTEM

Caution Indication LightsAuto RelightBaggage DoorBattery HotBattery RelayCheck InstrumentsCyclic CenteringEngine Anti-IceEngine Chip DetectorEngine Out and Low Rotor RPM Warning Lightsand Horn w/ Mute Switch. (Low RPM or EngineOut)Engine OverspeedFuel Boost Pump Inoperative, Left & RightFuel Transfer Pump Inoperative, Left & RightFuel Filter Bypass IndicatorFuel Valve in TransitFuel FlowFADEC FaultFADEC FailPedal StopFADEC DegradedFADEC ManualGenerator FailureHydraulic SystemLitter DoorRestart FaultStartTail Rotor Gearbox Chip DetectorTransmission Oil PressureTransmission Oil TemperatureTransmission (& Freewheeling unit) ChipDetector

ELECTRICAL

28 Volt DC SystemBattery, 17 amp-hr Nickel CadmiumExternal Power and Grounding ReceptacleLights:

Anticollision StrobeCockpit/mapInstrumentAft CabinLanding (Two 250 Watt)Position

Starter-Generator (180 Ampere)Solid State Voltage Regulator28 Volt Outlet in CabinHeated Pilot Tube & Static Ports



*Specifications as of 07/01/2021. Specifications are subject to verification upon inspection and should not provide a basis for reliance or create any other binding obligation.

201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022





201 1 BELL 407 | SN 54022




© 2021 Leviate Air Group. All rights reserved. LAS2021_Bell407_54022_v2



http://www.iada.aero/

Documents

S /N 54022