HIGHLIGHTS

In Service December 2012
U.S Registered
Forward Galley
Forward Crew Rest Compartment
Engines Enrolled on Rolls Royce Corporate Care
APU Enrolled on MSP
42″ Monitor in Aft Stateroom
Honeywell Swift Broadband
Satellite Direct TV
One Owner Since New

AIRFRAME

Certificate of Airworthiness: January 2012
Entry Into Service: 21st December 2012

Total Time: 1312.3 Hours
Cycles: 605

Home Base: L as Vegas, Nevada, USA
Certification: FAR 91.409 (f)(3)
Maintenance Tracking: G ulfstream Computerized Maintenance Program (CMP)

(as of 01st July 2015)

ENGINES

Description: BR700-725A1-12

Engine 1 (Left) Engine 2 (Right)
Serial Number: 25189 25188
Total Time: 1279.3 Hours 1279.3 Hours
Cycles: 590 590

Program Coverage: Rolls Royce Corporate Care

APU

Description: Honeywell RE220 (G650)
Serial Number: P-106
Total Time: 1050 Hours

Program Coverage: Honeywell MSP

AVIONICS

The Gulfstream G650ER is equipped with an integrated, Honeywell PlaneViewTM avionics suite with Block Point upgrade. A general summary of this avionics suite is as follows:

– TCAS 7.2
– FANS 1/A compliant
– Enhanced Vision System
– Synthetic Vision
– Predictive Windshear
– Part 135 DFDR 88-Parameters
– RAA
– 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 Management System with WAAS / LPV
– Triple Honeywell Multifunction Computer Display Units
– Honeywell Communications Management Function (ARINC Direct Datalink Service
Provider) + PlaneConnectHTM Aircraft Health Trends Monitoring System
– Triple Honeywell Micro Air Data Computers
– Triple Honeywell VHF Receivers with 8.33 kHz Spacing VDL Mode A and
Mode 2 Capabilities
– Dual HF Communication System with Dual SELCAL
– Triple Digital Audio Control Panels
– Honeywell MCS-7210 Inmarsat Satellite Communication System (SAT COM 1)
– Iridium Satellite Telephone System (SAT COM 2)
– Multi-Function Printer
– Triple Honeywell Navigation Receivers
– Dual Honeywell DME Receivers
– Dual Honeywell ADF Receivers
– Honeywell IntuVue 3-D Weather Radar System with Honeywell LSZ-860 Lightning Sensor
System and Predictive Windshear
– Dual Honeywell Radio Altimeter System
– Honeywell MK V EGPWS (Class A TA WS)
– Honeywell TCASS II with Change 7.1
– Dual Honeywell Mode S EHS & ADS-B Out (DO-260A Compliant) Transponders
– Solid State Flight Data Recorder (FAR 135 Compliant)
– Solid State Cockpit Voice Recorder
– RVSM Capable

ADDITIONAL EQUIPMENT

G650 ASC 14 – Extended Range Mod
42″ Monitor in aft stateroom

INTERIOR

Number of Seats: 14 (11 certified for take-off & landing)
Number of Berthable Seats: 5
Galley Location: Forward
Crew Rest: Forward / Left
Fwd Cabin Configuration: Four (4) Place Club
Mid Cabin Configuration: 4 place conference group opposite credenza
Aft Cabin Configuration: Stateroom with opposing dual 4 place divans
(1 divan not certified for take-off & landing)
Divan modified with 42″ monitor
Lavatory Location(s): Forward and Aft
Jump Seat: Yes

GALLEY EQUIPMENT:
Dynamo DMO-1000 Microwave
High Temp Oven
Two TIA 1604 Coffee Makers

ENTERTAINMENT:
Dual Slot Blu-Ray DVD/CD
Satellite TV
Satellite Communications
Fax Machine

Honeywell Wireless LAN system

INSPECTION STATUS

Recent 24 MO (2C) & 12 MO (1C) c/w at GAC Dallas
C1 & C3 due by October 2015

WARRANTIES

Commenced: 12th December 2012
Expires: 12th December 2022