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    2005 BOMBARDIER GLOBAL 5000 N-NUMBER T7-ALN2005 BOMBARDIER GLOBAL 5000 N-NUMBER T7-ALN
    Photos(9)
    T7-ALN - 2005 BOMBARDIER GLOBAL 5000

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    Aircraft Summary

    General
    Year
    2005
    Manufacturer
    BOMBARDIER
    Model
    GLOBAL 5000
    Serial Number
    9172
    Registration #
    T7-ALN
    Condition
    Used
    Description
    Honeywell 2000 XP Integrated Avionics, MNPS, RNP5, RNP10, RVSM Capable, Artex 406-2 ELT with Nav
Interface
    Airframe
    Total Time
    6190.18
    Total Landings
    2313
    Max Ramp Weight
    87,950 lb
    Max Takeoff Weight
    87,700 lb
    Max Landing Weight
    78,600 lb
    Basic Empty Weight
    49,125 lb
    Basic Operating Weight
    51,429 lb
    Fuel Capacity Mass
    36,187 lb
    Maintenance Tracking
    CAMP
    Engine Program
    Engine Maintenance Program
    Other
    Engine 1
    Engine 1 Manufacturer
    ROLLS ROYCE
    Engine 1 Model
    BR700-710A2-20
    Engine 1 Serial Number
    12455
    Engine 1 Time
    6179.54
    Engine 1 Time Since
    SNEW
    Engine 1 Cycles
    2311
    Engine 1 On Condition
    Yes
    Engine 2
    Engine 2 Serial Number
    12456
    Engine 2 Time
    6179.54
    Engine 2 Time Since
    SNEW
    Engine 2 Cycles
    2309
    Engine 2 Notes
    HSI and Overhaul : On Condition
    Auxiliary Power Unit
    APU
    Yes
    APU Time
    4532
    APU Notes
    Allied Signal RE-220 (GX) s/n P-293
    Avionics
    Flight Deck Manufacturer
    HONEYWELL
    Flight Deck Model
    PRIMUS 2000XP
    RNP
    Yes
    Avionics/Radios
    Six 8”x 7” DU-870 Color EFIS displays, 2 PFD/2 EICAS/2 MFD Triple HG-2001GD03 Inertial Reference Units Triple AZ-840 Micro Air Data Computers (MADC) Quad Ametek DA-810 Data Acquisition Units (DAU) 
Triple FMS NZ-2000 Integrated Flight Management System Dual 12 Channel Honeywell GPS HG-2021 
Triple IC-800 Integrated Avionics Computers (IAC) with EFIS Primus 880 Color Weather Radar with Lightning Sensor System ACSS TCAS 2000 TCAS II (Change 7 incorporated) Central Aircraft Information Maintenance System (CAIMS) Full Authority Digital Engine Control System (FADEC) Engine Indicating Crew Alert System (EICAS) Dual Honeywell Primus II RM-855 Radio Management Units
Dual Honeywell RNZ-851 Integrated NAV Units Radios w/VOR/ILS/MKR/ADF/DME FM Immunity Compliant Dual Honeywell RCZ-833 Integrated COM Units (8.33 Spacing) FM Immunity Compliant Dual Collins ALT-4000 Radio Altimeters Dual Collins HF-9031 HF Communication System Single Coltech CSD-714 SELCAL
    Additional Equipment
    Additional Equipment
    MNPS, RNP5, RNP10, RVSM Capable, Artex 406-2 ELT with Nav Interface HUD Heads Up Display Honeywell Mark V EGPWS Allied Signal SSFDR Digital Flight Data Recorder Allied Signal SSCVR Digital Cockpit Voice Recorder Artex 406-2 ELT ICG-200 Phone system Airshow Network DVD/CD Players
    Exterior
    Year Painted
    2006
    Interior
    Number of Seats
    12
    Interior Notes
    Fireblocked
Twelve (12) passengers plus one jump seat
Fwd cabin features (4) Executive seats w/fold-out tables
Center L/H cabin features a (4) place conference group; Opposite credenza cabinet. 
Aft cabin features (2) 3 place 16g breathable divans. Divans are rated 2 passengers per for takeoff & landing.
    Inspection Status
    Inspection Status
    A check (500 hr /15 mth) due at 6593 hours or Oct 2025
2A check (1000 hr) due at 6593 hours
3A check (1500 hr) due at 7093 hours
1C (15 month) due Oct 2025 
2C (30 month) due Dec 2025


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