2009 BOMBARDIER LEAR 45XR

$3,850,000

SN 0388 · REG LV-BTO

AIRFRAME
(As of August 27, 2019)
Total Time Since New 1,516.3 Hours
Total Landings Since New 1,664 Landings
C of A Issue Date 17 January, 2009
Entry into Service Date 27 August, 2009
Home Base Buenos Aires, Argentina
Certification Currently Op. FAR 135 Equivalent

Airframe enrolled on Smartparts Program

ENGINES
Honeywell TFE731-20BR-1B
Left Eng. Right Eng.
Serial Number(s) P-116538C P-116539C
Total Hours Since New 1,516.3 Hrs. 1,516.3 Hrs.
Total Cycles Since New 1,664 Cyc. 1,664 Cyc.

Engines enrolled on MSP Gold Program

APU
Description Honeywell RE100 (LJ)
Serial Number P-162
Total Time Since New 1,317.7 Hours
Total Cycles Since New 2,151

APU enrolled on MSP Gold Program

AVIONICS
The Bombardier Lear 45XR is equipped with an integrated, Honeywell Primus 1000 avionics suite.
A general summary of this aircraft’s avionics suite is as follows:
EFIS (Electronic Flight Instrument System) Four Tube Honeywell Primus 1000 (DU870 Displays)
FMS (Flight Management System) Dual Universal UNS-1E (SCN 802.2) with PRNAV Compliance
FLT DIR (Flight Director) Dual Honeywell IC-600
NAV (VOR / ILS / DME / ADF) Dual Honeywell RNZ-851 & RNZ-851B
FGC (Flight Guidance Computer) Honeywell GC-550
ADC (Air Data Computer) Dual Honeywell AZ-950
AHRS (Aircraft Heading Reference Sys.) Dual Computers
DTU (Data Transfer Unit) Universal Avionics DTU-100
A/P (Autopilot) Single Honeywell IC-600
RMU (Radio Management Unit) Dual Honeywell RM-855
ICU (Integrated Comm. Unit) Dual Honeywell RCZ-833K with 8.33 KHz Spacing and Mode S
HF Radio (High Frequency) Honeywell KAC 1052 w SELCAL
SATCOM (Satellite Comm.) Single Iridium ICS-200
RADAR Single Honeywell WU-880
RADAR ALT (Radar Altimeter) Single Honeywell RT-300
EGPWS (Enhance Ground Prox Warn Sys.) Single Honeywell Mark V
TCAS (Traffic Collision Avoidance Sys.) Single ACSS TCAS 2000 RT-951
CVR (Cockpit Voice Recorder) Single Honeywell SSCVR (30 min)
ELT (Emergency Locater Transmitter) Single Artex C406-2

INTERIOR
Number of Passengers: Eight (8) Passenger Seats in Double Club Configuration
Galley Location: Forward Right Hand Side
Lavatory Location(s): Aft Belted Lav and Vanity with Sink
Executive Seating: Townsend Classic Amber Leather
Headliner: Ultra leather
Cabinetry, Tables & Trim: High Gloss Figured Walnut
Plating: Brushed Nickel
Other Notable Features: Fire blocked Interior
Last Interior Date: Original

GALLEY EQUIPMENT
High Temp Oven
Coffee/Espresso Maker Hot Water / Coffee

CONNECTIVITY
Iridium ICS-200 Dual Channel In Flight Phone System with two Handsets
110 Volt Cab Pwr Sys. w/ 5 Outlets in Cockpit (1), Cabin (3) and Lav (1)

ENTERTAINMENT
Display/TV Monitor(s) 2 ea. 10.4″ Forward and Aft Monitors
Airshow System 1 ea. Airshow 410
DVD/CD Player(s) 1 ea. Audio International

EXTERIOR
Base Paint Color(s) Original – Overall Matterhorn White with Beige and Grey Toned Accent Striping.

WEIGHTS
Gross Weight (Ramp) 21,500 lbs Max Zero Fuel Weight 16,000 lbs
Max Takeoff Weight 21,500 lbs Empty Weight 13, 690 lbs
Max Landing Weight 19,200 lbs Current BasicOperating Weight 14,200 lbs

NAVIGATION & COMPLIANCE
RVSM
8.33 COM
VOR / ILS / RNAV / PRNAV

MAINTENANCE / PEDIGREE
Inspection Last Performed Next Due
Phase A1-A6 (12 Month Tasks) November 2018 November 2019
Phase B1-B6 (24 Month Tasks) November 2017 November 2019
Phase C1-C6 (48 Month Tasks) October 2016 October 2020
Phase D1-D6 (96 Month Tasks) October 2016 October 2024

One Owner Since New / Part 91 Operated Only
Maintained at Bombardier ASF Since New
Fuselage Skin Replaced by Bombardier, FLL in 2014

Maintenance Tracking enrolled on CAMP Program

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