EFTA00617516.pdf

Gulfstream Comparison of the Gulfstream G650ER, G500, and G600 EFTA00617516 Gulfstream Cabin Layouts G650ER G500 G600 Interior Dimension Comparison G650ER G500 G600 6' 5" 6' 4" 6' 4" Cabin Height 1.96 m 1.93 m 1.93 m 8' 6" 7'11" 7' 11" Cabin Width 2.59 m 2.41 m 2.41 m 46' 10" 41'6" 45' 2" Cabin Length 14.27 m 12.65 m 13.77 m 2,138 ft3 1,715 ft3 1,884 ft3 Cabin Volume 60.54 m3 48.56 m3 53.35 m3 Net Usable 195 ft3 175 ft3 175 ft3 Baggage Volume 5.52 m3 4.96 m3 4.96 m3 Gulfstream Proprietary Information, April 2017 1 G500 / G600 data is preliminary and subject to change EFTA00617517 Gulfstream Cabin Cross Section Finished Dimensions G650ER G500 / G600 80 00" 73.W 2.03 m 1.85 m Interior Comparison G650ER G500 G600 Living Areas 4 3 4 Passenger Capacity 19 19 19 Typical Outfitting 13-18 12-15 14-18 Flat Bed Berthing 6 6 6 Temperature Control 3 3 3 Zones Lavatories 2 2 2 Lavatory System Vacuum Vacuum Vacuum Galley Location Forward or Aft Forward or Aft Forward or Aft Yes Yes Yes Cold Food Storage (refrigerator) (refrigerator) (refrigerator) In-Flight Access to Yes Yes Yes Baggage Gulfstream Proprietary Information, April 2017 2 G500 / 6600 data is preliminary and subject to chance EFTA00617518 Gulfstream Cabin Comparison Continued G650ER G500 G600 Flexible Floor Plans Yes Yes Yes Gulfstream Quality Completions Materials Yes Yes Yes and Processes Gulfstream Audio / Video Distribution System Standard Standard Standard (GAVDS) Gulfstream Cabin Management System Standard Standard Standard (GCMS) 26" HD 24" HD 24" HD FWD Bulkhead Monitor widescreen LCD widescreen LCD widescreen LCD Credenza Monitor 26" HD LCD 26" HD LCD 26" HD LCD Entertainment Cabinet Option 32" HD LCD 32" HD LCD Cabin Altitude at FL450 4,030 ft 4,030 ft 4,030 ft Cabin Altitude at FL510 4,850 ft 4,850 ft 4,850 ft 6' 3" 6' 3" 6' 3" Main Entry Door Height 1.91 m 1.91 m 1.91 m Windows 16 14 14 450 in2 450 in2 450 in2 Window Area 2,903 cm2 2,903 cm2 2,903 cm2 Total Window Area 7,200 in2 6,300 in2 6,300 in2 46,452 cm2 40,645 cm2 40,645 cm2 100% Fresh Air Yes Yes Yes Gulfstream Proprietary Information, April 2017 3 G500 / G600 data is preliminary and subject to change EFTA00617519 Gulfstream Flight Deck Comparison PlaneView IITM Symmetry Flight Deck' Gulfstream Proprietary Information, April 2017 4 G500 / G600 data is preliminary and subject to change EFTA00617520  Gulfstream Flight Deck Comparison PlaneView II TM Symmetry Flight Deck' PlaneView II"' Feature Symmetry Flight Deck"' Honeywell Primus Epic Basis Honeywell Primus Epic Yoke and Rudder Pedals Primary Flight Control Active Sidesticks Cursor Control Devices and Cursor Control Device Avionics Control 10 Touchscreen Interfaces Dual Multifunction Digital Units Standby Displays Dual Digital Touchscreen Units EVS II and HUD II EVS & HUD EVS III and HUD II Four Multi-Function 14" Main Displays Four Multi-Function 14" G650 Type Rating Same between G500 and G600 Triplex FMS, Triple VHF Nav/Com, Yes Yes Dual 24 channel GPS, Triple IRS LPV, WAAS, Standard Standard RNP AR Honeywell RDR400 IntuVue TM Weather Radar Honeywell RDR400 IntuVueTM Gulfstream Proprietary Information, April 2017 5 G500 / G600 data is preliminary and subject to change EFTA00617521 Gulfstream System Comparison G650ER G500 G600 BR725 PW814GA PW815GA Engines (Thrust) 16,900 lb 15,144 lb 15,680 lb 75.2 kN 67.4 kN 69.7kN TBO (hr) 10,000 On-Condition (2) 40 kVA engine driven generators, (2) 40 kVA engine driven generators, Electric Power (1) 40 kVA APU (1) 40 kVA APU generator, Generation (AC) generator, (1) 15 kVA Ram Air Turbine (RAT) (1) 15 kVA Ram Air Turbine (RAT) 5 Transformer DC Power Rectifier Units 5 Transformer Rectifier Units (TRUs) (TRUs) 3-axis digital fly-by- 3-axis digital fly-by-wire with active Flight Controls wire with central control sidesticks mounted yoke Data Concentration N/A Yes Network Auto Brakes Yes Yes 2 separate systems with 2 separate systems with engine driven Hydraulics engine driven pumps pumps 40 US Gal, hot and Potable Water Capacity 30 US Gal, hot and cold pressurized cold pressurized Aircraft Health and Trend 10,000 parameters 15,000 Parameters Monitoring Gulfstream Proprietary Information, April 2017 6 G500 / G600 data is preliminary and subject to change EFTA00617522 Gulfstream Exterior Dimensions G500 G650ER G600 oa% Exterior Dimension G650ER G500 G600 99' 9" 91' 2" 96' 1" Length 30.40 m 27.78 m 29.29 m 25' 8" 25' 6" 25' 3" Height 7.82 m 7.78 m 7.70 m 99' 86' 3" 94' 1" Overall Span 7 30.35 m 26.30 m 26.68 m Gulfstream Proprietary Information, April 2017 7 G500 / G600 data is preliminary and subject to change EFTA00617523 Gulfstream Performance Comparison G650ER G500 G600 Normal Cruise M0.90 M0.90 M0.90 Long Range Cruise M 0.85 M 0.85 M 0.85 Mmo M 0.925 M 0.925 M 0.925 Range at LRC 7,390 nm 5,000 nm 6,200 nm 8 Pax, ISA, NBAA IFR Reserves 13,686 km 9,260 km 11,482 km Range at Normal Cruise 6,320 nm 3,800 nm 4,800 nm 8 Pax, ISA, NBAA IFR Reserves 11,705 km 7,038 km 8,890 km Takeoff Distance 6,299 ft 5,200 ft 5,700 ft SL, ISA, MTOW 1,920 m 1,585 m 1,737 m Landing Distance 3,000 ft 3,100 ft 3,100 ft SL, ISA, MLW 914 m 945 m 945 m Initial Cruise Altitude FL410 FL430 FL410 Maximum Cruise Altitude FL510 FL510 FL510 Performance Assumption Range assumes 8 passengers at 225 lb per person and a typical operating weight for the G650ER. Performance based on the noted assumptions. Actual performance will be affected by ATC routing. operating speed. weather. outlining options. and other factors. Weights G650ER G500 G600 103,600 lb 76,850 lb 91,600 lb Maximum Takeoff 46,992 kg 34,859 kg 41,549 kg 83,500 lb 64,350 lb 76,800 lb Maximum Landing 37,875 kg 29,189 kg 34,836 kg 6,000 lb 5,500 lb 6,000 lb Maximum Payload 2,722 kg 2,495 kg 2,722 kg 1,300 lb 1,800 lb 1,800 lb Max Payload/Full Fuel 590 kg 816 kg 816 kg Gulfstream Proprietary Information, April 2017 8 G500 / G600 data is preliminary and subject to change EFTA00617524 Gulfstream Range Performance Gulfstream Fleet Maximum Range Departing Boston Range Performance Assumptions • Great Circle Distance • Boeing 85% Annual Winds • Cruise Speed as Noted • 8 Passengers • NBAA IFR Reserves • ISA Conditions • G500: 3 Crew. G650ER, G600: 4 Crew Theoretical performance based on the noted assumptions. Actual performance wit( be affected byATC routing. operating speed. weather. outfitting options. and other factors. Gulfstream Proprietary Information, June 2017 9 G500 / G600 data is preliminary and subject to change EFTA00617525  Gulfstream 8,000 NBAA IFR Range (nm) with 8 Passengers 7,500 7,000 6,500 6,000 5,500 5,000 4,500 4,000 3,500 3,000 0.80 0.83 0.85 0.87 0.90 Cruise Speed (M) 7,000 6,000 5,000 :a- 4,000 crs O 5, 3,000 Ct a_ 2,000 1,000 0 0 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 NBAA IFR Range (nm) Gulfstream Proprietary Information, April 2017 10 G500 / G600 data is preliminary and subject to change See Page 8 for assumptions EFTA00617526  Gulfstream 7,000 G650ER 6,500 M0.85 6,000 Takeoff Distance (ft) 5,500 5,000 4,500 4,000 3,500 3,000 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 NBAA IFR Range (nm) 12,000 G650ER M0.85 11,000 10,000 G600 Takeoff Distance (ft) 9,000 G500 M0.85 M0.85 8,000 7,000 5,000 ft ISA+20°C 6,000 5,000 4,000 3,000 0 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 NBAA IFR Range (nm) Gulfstream Proprietary Information, April 2017 11 G500 / G600 data is preliminary and subject to change See Page 8 for assumptions EFTA00617527 Gulfstream Gulfstream Safety Features G650ER G500 G600 Enhanced Vision and EVS II and HUD II EVS III and HUD II EVS III and HUD II Head-up Display Auto Throttles Standard Standard Standard Automatic Descent Mode Standard Standard Standard Synthetic Vision Standard Standard Standard 100% fuel in wing Yes Yes Yes Secondary pressure Yes Yes Yes bulkhead (2) 40 kVA engine driven generators, (1) 40 kVA APU (2) 40 WA engine driven generators, Redundant power sources generator, (1) 40 kVA APU generator, (1) 15 WA Ram Air (1) 15 kVA Ram Air Turbine (RAT) Turbine (RAT) 'EVS III has 4 times the resolution of EVS II (640 x 512) Gulfstream Cost of Operations Comparison G650ER G500 G600 Fuel at $4 per gallon $1,516 $1,352 $1,440 Maintenance Labor, Parts, Engine and $1,385 $1,335 $1,395 APU Reserves Miscellaneous Flight Expenses $616 $583 $600 Total Direct Operating Costs Per Hour $3,517 $3,270 $3,435 Cost Assumption Fuel burn calculated for a 1.000 nm stage length with NBAA IFR Reserves (no fuel tankering) at LRC (G650ER/G500/G600 = M0.85). typical BOW and typical payload. Actual fuel burns will vary with cruise speed, payload. BOW. fuel tankering. cruise altitudes. wether. and other conditions. Engine maintenance costs are based on engine manufacturer maintenance plans. Rolls Royce engine cost data is based on the "on•condition" 2017 Corporate Care rates. APU maintenance costs are based on the 2017 Honeywell MSP rate. All other costs are from the Fall 2016 issue of Conklin 8 de Decker. Default fuel price is based on a nominal value from Spring 2017. All costs are theoretical estimates based on assumptions noted. Actual costs will vary by aircraft depending on operations, maintenance practices, environmental conditions, and other factors. Gulfstream Proprietary Information, April 2017 12 G500 / O600 data is preliminary and subject to change EFTA00617528 Gulfstream PROPRIETARY NOTICE THIS DATAAND INFORMATION CONTAINED HEREIN IS PROPRIETARY DATA OF GULFSTREAM AEROSPACE CORPORATION. NEITHER THIS DATA NOR THE DATA CONTAINED HEREIN SHALL BE REPRODUCED, USED, OR DISCLOSED TO OTHERS WITHOUT THE EXPRESS WRITTEN AUTHORIZATION OF GULFSTREAM AEROSPACE CORPORATION. Gulfstream Proprietary Information, April 2017 13 G500 / G600 data is preliminary and subject to change EFTA00617529