2005 Bombardier Global 5000

Maintenance ConditionOn CAMP Maintenance Tracking Program
2A Check c/w @ 986 Hours, Next Due @ 2,000 Hours
3A Check Due @ 1,500 Hours
6A Check Due @ 3,000 Hours
9A Check Due @ 4,500 Hours
1C Check c/w October 2011, Next Due March 2013
2C Check c/w November 2011, Next Due June 2014
4C Check c/w February 2012, Next Due December 2016
8C Check due December 2016
Fuselage/Structure until 2025
This Aircraft was Manufactured in 2005 and Placed into Service in 2006

Weight & BalanceEmpty: 50,517 Lbs
Basic Operating: 51,026 Lbs
Max Takeoff: 92,500 Lbs (SB 11-008)
Max Landing: 78,600 Lbs
Max Zero Fuel: 56,000 Lbs
Max Ramp: 87,950 Lbs

AvionicsCOM: Triple Honeywell RCZ 833 /835
NAV: Dual Honeywell NV 850
FDS: Honeywell Primus 2000XP
A/P: Honeywell Primus 2000XP
Xpndr: Dual Honeywell RNZ 851 Mode S Diversity - Enhanced Flight ID
ADF: Dual Honeywell Primus DF 850 Integrated
DME: Dual Honeywell Primus DM 850 Integrated
ADC: Triple Honeywell Micro AZ 840 MADC
FMS: Triple Honeywell NZ 2000 with CDU 820s
GPS: Dual Honeywell GPS 550 12 Channel GPS
AFIS: HST 2100 Digital Data Link and SATCOM High Speed data /ADLS
STCOM: Collins SAT 6100 (3) channel
HFCOM: Dual Collins 9031A with SELCAL
FFONE: Aerocom A 3000B Iridium & ICS 100 - (5) Cabin Handsets & (1) Cockpit
EFIS: Six Honeywell 8" x 7" DU870 Displays
Radar: Primus 880 with dual control heads & LSZ 860 Lightning Processor
Radalt: Dual Collins ALT 4000
TCAS: Honeywell TCAS 2000 with Change 7
EGPWS: Honeywell Mark V
LRNAV: Triple Honeywell HG-2001GD03 Inertial Reference Systems
FDR: Honeywell SSFDR
CVR: Honeywell SSCVR
ELT: Artex 406 MHGZ with NAV Interface