Description
FEATURES
• Enrolled on the Evolve Maintenance Program
• Fresh MPIs
• Gross Weight and Zero Fuel Weight Increase
• FDR Equipped
• CVR with RIPS Sentry 120R
• Dual UNS 1 EW/LPV FMS
• Lifeport Medical Interior Provisions
• Concorde Lead Acid Batteries
• Belted Lavatory SeatSpecifications
Year1999
ManufacturerLEARJET
Model45
Serial Number45-020
Registration #C-GVVZ
ConditionUsed
Total Time9,163
Engine Maintenance ProgramMSP
Engine 1 Make/ModelHONEYWELL TFE731-20AR-1B
Engine 1 Time9,095.3
Engine 1 Cycles6,026
Engine 1 NotesTime Since MPI :100.4
Time to MPI: 3399.6
Time to CZI: 3380.4
Engine 2 Make/ModelHONEYWELL TFE731-20AR-1B
Engine 2 Time9,095.3
Engine 2 Cycles6,026
Engine 2 NotesTime Since MPI :100.4
Time to MPI: 3399.6
Time to CZI: 3380.4
APU NotesHoneywell RE100 APU
Avionics/Radios• Honeywell Primus 1000 Avionics System with EICAS
• Dual Micro Data Computers
• 4-tube EFIS Display Including MFD
• Cockpit Voice Recorder (CVR) with RIPS Sentry 120R
• Flight Data Recorder (FDR) -FA2100
• Dual Integrated VHF Comms. UHF / 3rd VHF
• Dual Honeywell AHZ-800 AHRS
• Dual Integrated VHF Nav’s
• Single 2” Standby Altitude Indicator
• Single ADF
• Single 2” Standby Airspeed Indicator
• Aircell
• Dual DMEs
• Single 2” Standby Altimeter
• Dual Mode S Transponders
• TCAS II w/Mode S w/Diversity Transponders
• Dual Universal UNS 1EW/LPV FMS with SCN 1002.2
• Primary Bendix/King KHF-950
• ARTEX ELT 453-5060 ELT
• Honeywell Signal Enhanced EGPWS w/Windshear Alert.
• RVSM Certified with 8.33 Spacing and FM Immunity
• CMNPS Certified
• RNP 5 & 10 Certified
Additional Equipment• GROSS WEIGHT INCREASE 21,500 LBS. ZERO FULL WEIGHT INCREASE 16,500 LBS.
• Allied Signal RE-100 APU,
• Thrust Reversers,
• Triple Rosemont Pitot Static System,
• Pulsating Recognition Light System,
• Inflatable Quick Donning Crew Oxygen Masks,
• Dual Angle of Attack Indicators,
• Ice Detection System,
• Lighted Chart Holders,
• Auxiliary Cockpit Foot Warmers,
• Externally Serviced Electronic Flushing Toilet,
• Cockpit Sunvisors,
• Dual Digital Davtron Clocks,
• Clearance Delivery Unit,
• Belted Lavatory Seat (16G Certified) Digital Variable Position Spoilers,
• Vanity Sink, 40 Amp Ni-cad Batteries,
• (4)-110 Volt A/C Outlets in Cabin, Aircraft Locking Package,
• Wing Ice Detection Light, Floor Tracking,
• Dual 28V Flightbag Outlets
• Cabin and galley AC outlets
Exterior Notes• Painted June 2012
• Matterhorn White with red and blue striping
Interior Notes• Refurbished in 2012
Inspection StatusRecent SB Upgrades:
• A SB45-27-53 R2 – Aileron inspection
• Flight control cable replacement
• SB45-27-44 – Improved flight control cable fairleads
• SB34-3729 – FMS SCN upgrade to 1002.2
• Aircraft incorporated SB45-5-1 – Evolved Maintenance Program (EMP)
Year1999|
ManufacturerLEARJET|
Model45|
Serial Number45-020|
Registration #C-GVVZ|
ConditionUsed|
Total Time9,163|
Engine Maintenance ProgramMSP|
Engine 1 Make/ModelHONEYWELL TFE731-20AR-1B |
Engine 1 Time9,095.3|
Engine 1 Cycles6,026|
Engine 1 NotesTime Since MPI :100.4
Time to MPI: 3399.6
Time to CZI: 3380.4|
Engine 2 Make/ModelHONEYWELL TFE731-20AR-1B |
Engine 2 Time9,095.3|
Engine 2 Cycles6,026|
Engine 2 NotesTime Since MPI :100.4
Time to MPI: 3399.6
Time to CZI: 3380.4|
APU NotesHoneywell RE100 APU|
Avionics/Radios• Honeywell Primus 1000 Avionics System with EICAS
• Dual Micro Data Computers
• 4-tube EFIS Display Including MFD
• Cockpit Voice Recorder (CVR) with RIPS Sentry 120R
• Flight Data Recorder (FDR) -FA2100
• Dual Integrated VHF Comms. UHF / 3rd VHF
• Dual Honeywell AHZ-800 AHRS
• Dual Integrated VHF Nav’s
• Single 2” Standby Altitude Indicator
• Single ADF
• Single 2” Standby Airspeed Indicator
• Aircell
• Dual DMEs
• Single 2” Standby Altimeter
• Dual Mode S Transponders
• TCAS II w/Mode S w/Diversity Transponders
• Dual Universal UNS 1EW/LPV FMS with SCN 1002.2
• Primary Bendix/King KHF-950
• ARTEX ELT 453-5060 ELT
• Honeywell Signal Enhanced EGPWS w/Windshear Alert.
• RVSM Certified with 8.33 Spacing and FM Immunity
• CMNPS Certified
• RNP 5 & 10 Certified|
Additional Equipment• GROSS WEIGHT INCREASE 21,500 LBS. ZERO FULL WEIGHT INCREASE 16,500 LBS.
• Allied Signal RE-100 APU,
• Thrust Reversers,
• Triple Rosemont Pitot Static System,
• Pulsating Recognition Light System,
• Inflatable Quick Donning Crew Oxygen Masks,
• Dual Angle of Attack Indicators,
• Ice Detection System,
• Lighted Chart Holders,
• Auxiliary Cockpit Foot Warmers,
• Externally Serviced Electronic Flushing Toilet,
• Cockpit Sunvisors,
• Dual Digital Davtron Clocks,
• Clearance Delivery Unit,
• Belted Lavatory Seat (16G Certified) Digital Variable Position Spoilers,
• Vanity Sink, 40 Amp Ni-cad Batteries,
• (4)-110 Volt A/C Outlets in Cabin, Aircraft Locking Package,
• Wing Ice Detection Light, Floor Tracking,
• Dual 28V Flightbag Outlets
• Cabin and galley AC outlets|
Exterior Notes• Painted June 2012
• Matterhorn White with red and blue striping|
Interior Notes• Refurbished in 2012|
Inspection StatusRecent SB Upgrades:
• A SB45-27-53 R2 – Aileron inspection
• Flight control cable replacement
• SB45-27-44 – Improved flight control cable fairleads
• SB34-3729 – FMS SCN upgrade to 1002.2
• Aircraft incorporated SB45-5-1 – Evolved Maintenance Program (EMP)|
