EFTA00617516.pdf

Gulfstream Comparison of the Gulfstream G650ER, G500, and G600 EFTA00617516 Gulfstream Cabin Layouts G650ER G500 G600 Interior Dimension Comparison Cabin Height Cabin Width Cabin Length Cabin Volume Net Usable Baggage Volume G650ER G500 G600 6' 5" 6' 4" 6' 4" 1.96 m 1.93 m 1.93 m 8' 6" 7'11" 7' 11" 2.59 m 2.41 m 2.41 m 46' 10" 41'6" 45' 2" 14.27 m 12.65 m 13.77 m 2,138 ft3 1,715 ft3 1,884 ft3 60.54 m3 48.56 m3 53.35 m3 195 ft3 5.52 m3 175 ft3 4.96 m3 175 ft3 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 Living Areas Passenger Capacity Typical Outfitting Flat Bed Berthing Temperature Control Zones G650ER 4 G500 3 G600 4 19 19 19 13-18 12-15 14-18 6 6 6 3 3 3 Lavatories 2 2 2 Lavatory System Vacuum Vacuum Vacuum Galley Location Forward or Aft Forward or Aft Forward or Aft Cold Food Storage In-Flight Access to Baggage Yes Yes Yes (refrigerator) (refrigerator) (refrigerator) Yes Yes Yes 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 (GAVDS) Gulfstream Cabin Management System (GCMS) FWD Bulkhead Monitor Standard Standard 26" HD Standard Standard Standard Standard 24" HD 24" HD 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 Main Entry Door Height Windows Window Area Total Window Area 100% Fresh Air Yes Yes Yes 6' 3" 6' 3" 6' 3" 1.91 m 1.91 m 1.91 m 16 14 14 450 in2 450 in2 450 in2 2,903 cm2 2,903 cm2 2,903 cm2 7,200 in2 6,300 in2 6,300 in2 46,452 cm2 40,645 cm2 40,645 cm2 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 Yoke and Rudder Pedals Cursor Control Device Dual Multifunction Digital Units EVS II and HUD II Four Multi-Function 14" G650 Yes Standard Honeywell RDR400 IntuVue TM Basis Primary Flight Control Avionics Control Standby Displays EVS & HUD Main Displays Type Rating Triplex FMS, Triple VHF Nav/Com, Dual 24 channel GPS, Triple IRS LPV, WAAS, RNP AR Weather Radar Honeywell Primus Epic Active Sidesticks Cursor Control Devices and 10 Touchscreen Interfaces Dual Digital Touchscreen Units EVS III and HUD II Four Multi-Function 14" Same between G500 and G600 Yes Standard Honeywell RDR400 IntuVueTM Gulf stream Proprietary Information, April 2017 G500 / G600 data is preliminary and subject to change 5 EFTA00617521 Gulfstream System Comparison Engines (Thrust) TBO (hr) Electric Power Generation (AC) DC Power Flight Controls Data Concentration Network Auto Brakes Hydraulics Potable Water Capacity G650ER BR725 16,900 lb 75.2 kN 10,000 (2) 40 kVA engine driven generators, (1) 40 kVA APU generator, (1) 15 kVA Ram Air Turbine (RAT) 5 Transformer Rectifier Units (TRUs) 3-axis digital fly-by- wire with central mounted yoke N/A Yes 2 separate systems with engine driven pumps 40 US Gal, hot and cold pressurized Aircraft Health and Trend 10,000 parameters Monitoring G500 PW814GA 15,144 lb 67.4 kN G600 PW815GA 15,680 lb 69.7kN On-Condition (2) 40 kVA engine driven generators, (1) 40 kVA APU generator, (1) 15 kVA Ram Air Turbine (RAT) 5 Transformer Rectifier Units (TRUs) 3-axis digital fly-by-wire with active control sidesticks Yes Yes 2 separate systems with engine driven pumps 30 US Gal, hot and cold pressurized 15,000 Parameters Gulf stream Proprietary Information, April 2017 6 G500 / G600 data is preliminary and subject to change EFTA00617522 Gulfstream Exterior Dimensions G500 Exterior Dimension Length Height G600 oa% G650ER 99' 9" 30.40 m 25' 8" 7.82 m ' Overall Span 99 7 30.35 m Gulfstream Proprietary Information, April 2017 7 G500 / G600 data is preliminary and subject to change G650ER G500 G600 91' 2" 27.78 m 25' 6" 7.78 m 86' 3" 26.30 m 96' 1" 29.29 m 25' 3" 7.70 m 94' 1" 26.68 m EFTA00617523 Gulfstream Performance Comparison Normal Cruise Long Range Cruise Mmo Range at LRC 8 Pax, ISA, NBAA IFR Reserves Range at Normal Cruise 8 Pax, ISA, NBAA IFR Reserves Takeoff Distance SL, ISA, MTOW Landing Distance SL, ISA, MLW Initial Cruise Altitude Maximum Cruise Altitude G650ER M0.90 M 0.85 M 0.925 7,390 nm 13,686 km 6,320 nm 11,705 km 6,299 ft 1,920 m 3,000 ft 914 m FL410 FL510 G500 M0.90 M 0.85 M 0.925 5,000 nm 9,260 km 3,800 nm 7,038 km 5,200 ft 1,585 m 3,100 ft 945 m FL430 FL510 G600 M0.90 M 0.85 M 0.925 6,200 nm 11,482 km 4,800 nm 8,890 km 5,700 ft 1,737 m 3,100 ft 945 m FL410 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 Maximum Takeoff Maximum Landing Maximum Payload Max Payload/Full Fuel Gulf stream Proprietary Information, April 2017 G500 / G600 data is preliminary and subject to change G650ER G500 G600 103,600 lb 76,850 lb 91,600 lb 46,992 kg 34,859 kg 41,549 kg 83,500 lb 64,350 lb 76,800 lb 37,875 kg 29,189 kg 34,836 kg 6,000 lb 2,722 kg 1,300 lb 590 kg 8 5,500 lb 2,495 kg 1,800 lb 816 kg 6,000 lb 2,722 kg 1,800 lb 816 kg 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 NBAA IFR Range (nm) with 8 Passengers 8,000 7,500 7,000 6,500 6,000 5,500 5,000 4,500 4,000 3,500 3,000 0.80 7,000 6,000 5,000 :a- 4,000 crs O 5, Ct a_ 3,000 2,000 1,000 0 0.83 0.87 0.85 Cruise Speed (M) 0.90 0 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 NBAA IFR Range (nm) Gulf stream Proprietary Information, April 2017 10 G500 / G600 data is preliminary and subject to change See Page 8 for assumptions EFTA00617526 Gulfstream Takeoff Distance (ft) Takeoff Distance (ft) 7,000 6,500 6,000 5,500 5,000 4,500 4,000 3,500 3,000 12,000 11,000 10,000 9,000 8,000 7,000 6,000 5,000 4,000 3,000 G650ER M0.85 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 NBAA IFR Range (nm) G600 G500 M0.85 M0.85 G650ER M0.85 5,000 ft ISA+20°C 0 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 NBAA IFR Range (nm) Gulf stream Proprietary Information, April 2017 11 G500 / G600 data is preliminary and subject to change See Page 8 for assumptions EFTA00617527 Gulfstream Gulfstream Safety Features Enhanced Vision and Head-up Display Auto Throttles Automatic Descent Mode Synthetic Vision 100% fuel in wing Secondary pressure bulkhead G650ER G500 G600 EVS II and HUD II EVS III and HUD II EVS III and HUD II Standard Standard Standard Yes Yes (2) 40 kVA engine driven generators, (1) 40 kVA APU Redundant power sources generator, (1) 15 WA Ram Air Turbine (RAT) Gulfstream Cost of Operations Comparison Fuel at $4 per gallon Maintenance Labor, Parts, Engine and APU Reserves Miscellaneous Flight Expenses Standard Standard Standard Yes Yes Standard Standard Standard Yes Yes (2) 40 WA engine driven generators, (1) 40 kVA APU generator, (1) 15 kVA Ram Air Turbine (RAT) 'EVS III has 4 times the resolution of EVS II (640 x 512) G650ER G500 G600 $1,516 $1,352 $1,440 $1,385 $1,335 $1,395 $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. Gulf stream Proprietary Information, April 2017 13 G500 / G600 data is preliminary and subject to change EFTA00617529