2005 LEARJET 45XR | SN 45-0275

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HIGHLIGHTS

WAAS / LPV Equipped
BR Engines
TCAS 7.1

Capabilities

RVSM
RNP 10/5/4/1
TCAS 7.1
8.33 SPACING
BRNAV
FM IMMUNITY
VNAV
MNPS
WAAS / LPV
Engines & APU on MSP Gold

Airframe

8,346 Hours Total Time
6,130 Landings

Engines

(2) Honeywell TFE-731-20BR-1B
Enrolled on MSP Gold

Engine #1
SN: P-116617C
8,311 Hours Total Time
6,101 Total Cycles

Engine #2
SN: P-116616C
8,311 Hours Total Time
6,101 Total Cycles

APU

Enrolled on MSP Gold
SN: P-305
1,957 Hours Total Time

Avionics

AIR DATA COMPUTER: Dual Honeywell AZ-950 ADC
ATTITUDE HEADING REFERENCE SYTEM: Dual Honeywell AH-800 AHRS Computers
AUDIO CONTROL PANEL: Dual Honeywell AV-850A
AUTOMATIC DIRECTION FINDER: Honeywell RNZ-850 with ADF
AUTOPILOT: Honeywell IC-600 Autopilot
COCKPIT VOICE RECORDER: Honeywell SSCVR CVR120 (120 minutes)
COMMUNICATIONS: Dual Honeywell RCZ-851G VHF Comm/ATC Units
ELECTRONIC STANDBY INSTRUMENT SYSTEM: Honeywell DU-870 Display Units
EMEGENCY LOCATOR TRANSMITTER: Artex C406-2 ELT
DISTANCE MEASURING EQUIPMENT: Integrated w/ Dual Honeywell RNZ-851 Navigation Units
FLIGHT GUIDANCE SYSTEM: Honeywell GC-550
FLIGHT MANAGEMENT SYSTEM: Dual Universal UNS-1Ew FMS
HIGH FREQUENCY RADIO: Bendix King KHF-950 with SELCAL
MAINTENANCE DIAGNOSTIC COMPUTER: MCOS
NAVIGATION: Honeywell RNZ-850 with ADF and RNZ-851 Navigation Units
RADIO ALTIMETER: Honeywell RT-300 Radar Altimeter
RADIO MANAGEMENT UNIT: Dual Honeywell RM-855
SELCAL: CSD-10 Selcal Decoder
STANDBY ATTITUDE INDICATOR: L3 AI-804BZ Standby Indicator
TERRAIN AWARENESS WARNING SYSTEM: Honeywell Mark V EGPWS Computer
TRAFFIC COLLISION AVOIDANCE SYSTEM: Honeywell TCAS 2000 TCAS II with Change 7.1
TRANSPONDERS: Integrated with Dual Honeywell VHF Comm/ATC Units with ADS-B Out Version 2
WEATHER RADAR: Honeywell Primus WU-660

Additional Features

Iridium Satellite Phone System
Thrust Reversers
115V Outlets
Pilot Sun Visors
LED Navigation Lights

Interior

This executive 9 passenger interior is configured with both forward cabin and aft cabin double club seating and belted toilet. A very functional forward galley and full aft lavatory complete the cabin.

Exterior

Overall white with black and gray accent stripes. Original paint at Bombardier, Wichita.

MAINTENANCE & INSPECTIONS

Phase A (300 Hours) last completed 10/2021 (Next Due 10/2022)
Phase B (600 Hours) last completed 7/2021 (Next Due 6/2023)
Phase C (1,200 Hours) last completed 6/2019 (Next Due 6/2023)
Phase D (2,400 Hours) last completed 7/2017 (Next Due 7/2025)
4,800 Hour Check last completed 7/2013 (Next Due @ 9,378 Hours)
9,600 Hour Check Due @ 9,600 Hours

WEIGHTS

MAX RAMP WEIGHT: 21,750 LBS
MAX LANDING WEIGHT: 19,200 LBS
EMPTY WEIGHT: 13,826 LBS
MAX USABLE FUEL: 6,062 LBS
MAX TAKEOFF WEIGHT: 21,500 LBS
MAX ZERO FUEL: 16,000 LBS
MIN FLIGHT WEIGHT: 14,000 LBS
SB 45-11-4 R2 complied with on 11/2004 increases MAX TAKEOFF WEIGHT to 21,500 LBS

Aircraft specifications are always subject to verification by purchaser.