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2011 BELL 407S/N 54022
N897KV
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
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
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
*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
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
© 2021 Leviate Air Group. All rights reserved. LAS2021_Bell407_54022_v2
+1 (912) 401-6577 | Andrew Steward | [email protected] | leviatejetsales.com
