Description
2016 Delivery * Forward Crew Rest * Forward Galley * Immediately Available * ADS-B Out Version 2
Airframe
Total Hours: 32.1
Total Landings: 13
Date of Manufacture: 2015
Entry Into Service: 2016
Engine(s)
Rolls Royce BR725A1-12
Left Engine:
22.1 TT - 6 Cycles - SN 25421
Right Engine:
22.5 TT - 6 Cycles - SN 25420
APU:
Honeywell RE220 - 47.0 TT - SN P-5279
Avionics/Radios
The Gulfstream G650 is equipped with an integrated, Honeywell PlaneView avionics suite. A general summary of this avionics suite is as follows:
– 3-Axis Quadruple-Redundant Fly-By-Wire Automatic Flight Control System with Automatic Emergency Descent Mode, Auto Throttle, and Dual Cursor Control Devices
– Four (4) Honeywell Adaptive LCDs EFIS
– Gulfstream Enhanced Vision System II (Head-Up Display + Infrared Camera) and Honeywell SmartView Synthetic Vision System
– Triple Honeywell Primus Epic Flight MC-850 Model Management System with WAAS /LPV capability
– Triple Honeywell Multifunction Computer Display Units
– Two Honeywell Model AH-1000 Attitude Heading Reference Units
– Honeywell Communications Management Function (Satcom Direct Service Provider)
– PlaneConnect HTM Aircraft Health Trends Monitoring System
– Triple Honeywell Micro Air Data Computers
– Triple Honeywell Model TR-866B VHF Communication Receivers with 8.33 kHz Spacing VDL Mode A and Mode 2 Capabilities
– Triple Honeywell Model NC-860A VHF Navigation receivers
– Dual HF Rockwell Collins model HF-9034A Communication System with Dual SELCAL
– Triple Digital Audio Control Panels
– Honeywell MCS-7210 Inmarsat Satellite Communication System (SATCOM 1)
– Iridium Satellite Telephone System (SATCOM 2)
– Dual Honeywell Model DM-855DME Receivers
– Dual Honeywell Model DF-855 ADF Receivers
– Honeywell IntuVue 3-D Weather Radar System with Honeywell LSZ-860 Lightning Sensor System and Predictive Windshear
– Dual Honeywell Model KRA-405B Radio Altimeter System
– Dual Honeywell MK V EGPWS (Class A TA WS)
– Honeywell TCASS II Surveillance Processor Computer with Change 7.1
– Dual Honeywell Mode S EHS & ADS-B Out (DO-260A Compliant) Transponders
– Universal Avionics Solid State Flight Data Recorder Combined CVR & FDR w/embedded RIPS (FAR 135 Compliant)
– Universal Avionics Systems CVFDR Solid State Cockpit Voice Recorder 120-minute with Data link Recorder capability
– RVSM certified
– Three (3) Apple iPad tablets (PlaneBook electronic manual suites – one (1) year subscription)
Additional Equipment
Part 135 Compliance
Crew Rest Compartment
ASC-036 Automatic Dependent Surveillance—Broadcast (ADS-B) Out Version 2 Installation
12.1” Monitors in the inboard armrest of each single seat in the main cabin.
Two JetBed Self-Inflating Mattresses
SecuraPlane 500 Security System
Exterior
Chevron White Upper and Medium Grey Lower separated by Charcoal Gray and Chevron White Stripes.
Interior
Eleven (11) Place Executive Configuration, Fwd Galley, Fwd Crew Lavatory, Fwd Four-Place and Mid Four-Place Club Seating and an Aft, Left-Hand Area Three-Place Berthable Divan with Opposing Customized Credenza. Aft Executive Lavatory, In addition, the cabin is configured with One Fwd Facing Seat in “Crew Rest Area” as well as a Certified Jumpseat.
