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2016 Gulfstream G650ER
| Overview | |
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2016 Gulfstream G650ER s/n 6188 with 3,323 hours total time and 1,055 landings. 13 passenger forward galley with forward crew rest Hallmark floorplan. One U.S. Fortune 100 owner, always hangared since new, no incidents/stories/damage. Engines on Rolls-Royce CorporateCare; APU on Honeywell MSP Gold. SpaceX Starlink hi-speed internet service & WiFi. FANS 1/A+ / CPDLC, ADS-B Out v2, TCAS 7.1. Block III Baseline completed. Hangared at Morristown Airport (MMU) in Morristown, NJ. |
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| Price: | Contact Seller |
| Offered By: | Leading Edge Aviation Solutions |
| Registration: | N82A |
| S/N: | 6188 |
| Home Airport: | MMU (Airnav) |
| Location: |
Morristown, New Jersey United States 
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| Days Active: | Today |
| Airframe | |
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3,323 Hours Total Time 1,055 Landings Certificate of Airworthiness (CofA): February 2016 Entry Into Service: July 2016 One U.S. Fortune 100 Owner Always Hangared Since New No Incidents/Stories/Damage Basic Empty Weight: 53,322.6 lbs. Basic Operating Weight: 55,121.4 lbs. |
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| Total Time: | 3,323 Hours |
| Landing Cycles: | 1,055 |
| Number of Seats: | 13 |
| Pressurized: | Yes |
| Avionics | |
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Block III Baseline Completed Gulfstream PlaneView Avionics System Triple (3) Flight Management Systems (FMS) Enhanced NAV (FANS-1/A+ w/ CPDLC) Four (4) Large Flat Panel LCD Electronic Display Units (Pilot PFD-MFD & Copilot PFD-MFD) Triple (3) Modular Avionics Units (MAUs) Guidance Panel Dual (2) Standby Multifunction Controllers (SMC) Triple (3) Multi-Function Control Display Units (MCDU) Dual (2) Cursor Control Devices (CCD) Four (4) Multifunction Air Data Probes (MFP) Air Data System Triple (3) Inertial Reference Systems (IRS) Dual (2) Global Positioning Systems (GPS) w/ Wide Area Augmentation System (WAAS) Synthetic Vision - Primary Flight Display (SV-PFD) Head-Up Display (HUD) Enhanced Vision System (EVS) Automatic Flight Guidance System Autothrottle System One (1) Data Loading LAN Management Unit (DLMU) Dual (2) High Frequency (HF) Communications Triple (3) Very High Frequency (VHF) Communications One (1) VHF Communication / Navigation (NAVCOM) Unit VHF Navigation, Instrument Landing System (ILS), and Marker Beacon Dual (2) Mode S Transponders w/ ADS-B Out Capabilities (DO-260B Compliant) Traffic & Collision Avoidance System (TCAS II v7.1) Dual (2) Distance Measuring Equipment (DME) Transceivers Multi-channel Satellite Communications System (SATCOM) - 2 Voice & 1 Data Channel Dual (2) Enhanced Ground Proximity Warning Systems (EGPWS) Flight Data Recorder System (FDR) - Twenty-Five (25) Hour Recording (88 Parameters) Cockpit Voice Recorder (CVR) - Twenty-Five (25) Hour Recording 3-D Color Weather Radar Honeywell IntruVue RDR-4000 Dual (2) Digital Radio Altimeters Central Maintenance Computer (CMC) Emergency Locator Transmitter (ELT) Pilot & Copilot Emergency Vision Assurance Systems (EVAS) Automated Direction Finder (ADF) |
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| Additional Equipment | |
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Starlink Satellite System Jet Connex Ka-band Hi-Speed Internet Honeywell AIS-2000 Multi-Region Airborne Information System Honeywell Inmarsat Satellite Communication System Satcom Direct Router Wireless (Wi-Fi) Local Area Network (LAN) System w/ Shared Network Printer Dual Slot Blu-Ray/DVD/CD Player Gulfstream CabinView Passenger Flight Information System SecuraPlane 500 Aircraft Security System Major Aircraft Service Changes, Enhancements & Upgrades: ASC 003A: Comm. Mgmt. Function (CMF) - SATCOM Direct Datalink Service Provider ASC 004C: AHTMS Health Trend Monitoring Cell Data Transmission ASC 005: Runway Awareness Advisory System (RAAS) - Installation ASC 006: Lightning Sensor System (LSS) - Installation ASC 007: Predictive Windshear (PWS) - Activation ASC 016: Engine Electronic Controller - K7.1.3 Software Upgrade ASC 026: 74,900 Lb. Weight Limitation ASC 027: 90,000 Lb. Weight Limitation ASC 028: 95,000 Lb. Weight Limitation ASC 029: 100,000 Lb. Max Ramp Gross Weight / 99,600 Lb. Max Takeoff Gross Weight ASC 036: ADS-B Out Version 2 - Installation ASC 038A: PlaneView II Avionics Enhancement ASC 048 Part II: Spoiler Joint Anti-Rotation Retention Washer - Installation ASC 051A: Secondary Power Distribution System (SPDS) Software Update ASC 055B: Autobrake System - Installation ASC 065: Main Entrance Door Manual Operation Mechanism ASC 066: Main Entrance Door (MED) - EMED Rigging Improvement ASC 068: Baggage Compartment Grab Handle - Installation ASC 069: Primary Flight Control Actuation Syst. Remote Electronics Unit Software Update ASC 070: Cockpit AIR Ducting - Velocity Reduction ASC 073: Tire Pressure Monitoring Unit (TPMU) Software Upgrade ASC 074: Nose Wheel Steering System - Upgrade ASC 076B: Aircraft Health and Trend Monitoring System - Software Update 2 ASC 079: Landing Gear Control Unit Mod D Update ASC 081A: Med Latch Actuator Upgrade ASC 083: Flap Track D Rub Strips - Removal ASC 084A: Main Landing Gear and Brake Assembly - Modification ASC 085: Ka-Band Fin CAP Radome Installation ASC 086: Main Entry Door - Service Door Panel Security Cover - Installation ASC 088A: Engine Electronic Controller - K8.0.2 Software Upgrade ASC 089: Doors (ATA 52), MED - Bottom Folding Step Stop Bolts - Replacement ASC 090A: Hydraulic Filter Monitoring System - Installation and Activation ASC 091A: Acoustic Door Noise Reduction - Modification ASC 092: Primary Flight Control Motor Control Electronic Software Upgrade ASC 093: Flight Controls (ATA 27) - FCC Software Update ASC 095: APU Enclosure Installation - Modification ASC 096: 8.8 KHZ Underwater Acoustic Beacon (UAB) Installation ASC 097: Primary Flight Control Actuation System REU Connector Update ASC 098: Horizontal Stabilizer Control Unit Software Update ASC 099A: Main Entrance Door - Bottom Folding Step Mechanism Improvement ASC 100: Planeview II Avionics Enhancement ASC 101A: Steep Approach to Landing Activation ASC 102: Modification FCC Software v8.2 Update ASC 103: Auxiliary Hydraulic Pump - Grounding Installation ASC 105A: Data LAN Management Unit Harness - Service Loop Installation ASC 110: Flap Electronic Control Unit (FECU) Software Update ASC 113A: APU Exhaust Fairing Drainage - Modification ASC 116A: Battery Charger MODE Control Relays & Elec. Backup Hyd. Actuator Battery Charger No. 2 - Removal ASC 117: Hyd Line Support Bracket Install - Mod to Provide Side Brace Actuator Clearance ASC 118: Aft Equipment Bay Water Shield - Installation ASC 122A: Engine FIRE Extinguishing Bottle Cartridge - Wiring - Modification ASC 123A: APU Electronic Control Unit Software - Update ASC 124A: Pylon Seal Retainer - Modification ASC 125: Heads Up Display (HUD) II Software Update ASC 129: Flap Track D Up-Stop Fitting - Improvement ASC 131: Flap Track C Roller Fitting - Rub PAD Installation ASC 133: Engine Electronic Controller - K9.0.1 Software Modification ASC 134B Part I/II: Wedge Installation - Trailing Edge, Rudder ASC |
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| Engines | |
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Rolls Royce BR700-725A1-12 On Condition & Enrolled on Rolls-Royce CorporateCare Left (#1): SN 25485, 3,323 Total Hours, 1,055 Total Cycles Right (#2): SN 25484, 3,323 Total Hours, 1,055 Total Cycles APU: Honeywell RE220 (G650), Enrolled on Honeywell MSP Gold, SN P-301, 1,754 Hours |
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| Engine 1 Hours: | 3,323 SNEW |
| Engine 2 Hours: | 3,323 SNEW |
| Interior & Exterior | |
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Completed 2016 @ Gulfstream - Savannah, GA The 13 Passenger Forward Galley with Forward Crew Rest Hallmark Interior features a crew jump seat, forward crew lavatory, forward crew rest area, forward main galley, and aft main lavatory. The entry area includes the Left-Hand Side forward crew lavatory, Right-Hand Side forward crew rest area, the Left-Hand Side full-service main galley and Right-Hand Side forward full-service main galley annex. The entry area and forward cabin are separated by an electric pocket door. The interior features a 3-zone cabin with a forward cabin 4-place club with stowable executive writing and dining tables between the opposing club chairs, a mid-cabin 4-place conference group opposite a credenza, followed by an aft room with single 3-place divan opposite a left side 2-place club. There are 26-inch monitors on the forward and aft bulkheads as well as one pop-up 26 inch monitor in the credenza. There are also 12-inch monitors located in the arm rest of each cabin chair. Multiple 115VAC/60Hz outlets are located throughout the cockpit, vestibule, lavatories, cabin, and baggage compartment areas. |
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| Year Interior: | 2016 |
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Completed June 2016 @ Gulfstream - Savannah, GA Overall Matterhorn White with Black Pearl Striping and Gray Cumulus Pearl Accents. |
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| Year Painted: | 2016 |
| Other Info | |
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Inspection Status: Engines are On Condition (Task Oriented) & Enrolled on Rolls-Royce CorporateCare APU Enrolled on Honeywell MSP Gold Aircraft Enrolled on MSG-3 Program and Gulfstream MYCMP Maintenance Tracking Program 12 Month: Last Completed May 2026, Next Due May 2027 24 Month: Last Completed May 2025, Next Due May 2027 36 Month: Last Completed May 2024, Next Due May 2027 48 Month: Last Completed May 2024, Next Due April 2028 72 Month: Last Completed May 2022, Next Due June 2028 96 Month: Last Completed May 2024, Next Due June 2032 144 Month: Next Due June 2028 192 Month: Next Due June 2032 |
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| Damage: | No known current or historical damage |
| Brochure: | View Brochure |
| Aircraft Documents (1) | |
