Condition: Pre-Owned
Year: 2013
Hours: 633
Airframe:
TTAF: 633
Landings: 296
Weights:
MAX RAMP WEIGHT: 100,000 Lbs.
MAX TAKE-OFF WEIGHT: 99,600 Lbs.
MAX LANDING WEIGHT: 83,500 Lbs.
BOW: 54,178 Lbs.
EMPTY WEIGHT: 52,040 Lbs.
MAX FUEL LOAD: 44,200 Lbs.
MAX ZERO FUEL: 60,500 Lbs.
Note: ASC027 compliant permitting Max Takeoff Weight reduction to 90,000 pounds.
ASC030 compliant permitting Max Zero Fuel Weight reduction to 60,000 pounds.
Avionics / Radios:
Gulfstream PlaneView™II/ Honeywell Primus Epic
AIR DATA COMUTERS: Four independent multifunction probes (MFP) with self-contained computing platforms
AUTOMATIC DIRECTION FINDER: Single Honeywell DF-855 ADF Module
AUTO FLIGHT CONTROL: Dual Pitch/Roll Autopilot Servos with FADEC Interfaced Auto Throttle System and Automatic Emergency Descent Mode
COCKPIT VOICE RECORDER: Single Honeywell Solid State CVR
COMMUNICATIONS: Triple Honeywell VHF Receivers w/8.33 kHz spacing
Triple Digital Audio Control Panels
DISTANCE MEASURING EQUIPMENT: Dual Honeywell DM-855 DME Module
ELECTRONIC FLIGHT INSTRUMENT SYSTEM: Four Honeywell large 14” adaptive LCD displays
EMERGENCY LOCATOR TRANSMITTER: 406 MHz with Navigation Interface
ENHANCED GROUND PROXIMETY WARNING SYSTEM: Dual Honeywell Mark V EGPWS with RAAS and Predictive Wind Shear Warning
ENHANCED VISION SYSTEM: Gulfstream EVS II System
FLIGHT DATA RECORDER: Single Digital FDR (88 Parameters)
FLIGHT MANAGEMENT SYSTEM: Triple Honeywell NEXTGEN Multifunction Display Units (Block Point 1 compliant)
FLY-BY WIRE: Fly-by-wire flight controls with 5 channel redundancy
GLOBAL POSITIONING SYSTEM: Dual GPS With Wide Area Augmentation System (WAAS) / LPV
HEADS UP DISPLAY: Gulfstream Enhanced Vision System II (HUD and Infared Camera)
HIGH FREQUENCIES: Dual VDL Mode A and Mode 2 Capabilities with SECAL
LONG RANGE NAVIGATION: Triple Honeywell LASEREF VI
RADIO ALTIMETER: Dual Honeywell KRA-405B Radio Altimeter System
TRAFFIC COLLISION ALERT AND AVOIDANCE SYSTEM: Honeywell TCAS II 7.1
SYNTHETIC VISION: Honeywell SmartView™SV-PFD
TRANSPONDER: Dual Honeywell Mode S Enhanced
WEATHER RADAR: RDR-4000 3-D Weather Radar
Engine(s):
Rolls Royce BR-725A1-12
Engine 1: S/N 25195
633 HSN, 296 CSN
Overhaul Due: 10,000 hours / Oct 2032
Engine 2: S/N 25194
633 HSN, 296 CSN
Overhaul Due: 10,000 hours / Oct 2032
Engines are “Operated per Hard Time & Calendar”
Engines on Rolls-Royce Corporate Care
APU: Honeywell RE-220 (G650) S/N: P-150
596.5 HSN, 296 CSN
HSI Due: On Condition
APU Enrolled on MSP
Interior:
Original Interior, Completion at Gulfstream, Appleton, WI
14 Passenger Executive Interior featuring a forward 4-Place Club, a 4-Place conference table facing a credenza in the mid cabin and a double divan in the aft cabin. The aircraft is equipped with forward and aft lavatories, a forward galley as well as a forward crew rest.
Galley Description
Dynamo Galley Refrigerator
Enflite Convection Oven
Dynamo Aviation Microwave
Espresso Coffee Maker
Wine Chiller (located in mid-cabin credenza)
Lavatory Description
Vacuum Lavatory System
Gulfstream G650 Cabin Entertainment & Communications
Original Paint, June 2013 at Gulfstream, Long Beach, CA
Matterhorn White, Gray, Forest Jade Green, Orange, Dark Gray and Jet Stream Gray
The airplane will be delivered with new Registration Number N829JV
Maintenance tracked by CMP
No Damage History
Standard Warranty
Airframe 20 years/20,000 hours (labor included)
Structural Airframe 20 years/20,000 hours (labor included)
Production Non-structural 5 years (labor included)
Standard Avionics – 5 years (labor included)
Optional Avionics – 2 years (labor included)
Engines – 6 years/3,500 hours
APU – 5 years (labor included)
Paint – 2 years (labor included)
Interior Completion – 2 years (labor included)
Gulfstream Capabilities:
FANS/1A
CPDLC
ADS-B (OUT)
HUD w/EVS
TCAS 7.1
WAAS/LPV
BRNAV
MNPS
VNAV
RVSM
Auto Throttles
TAWS
Enhanced Navigation
Emergency Descent Mode
CAT1 Approaches
RNP-10, 5, 4
RNAV-1
Data Link Recording