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E170

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E170

Product catalog summary

Weight Specifications

Maximum Takeoff Weight: LR: 37,200 kg (82,012 lb), AR: 38,600 kg (85,098 lb)
Maximum Landing Weight: LR: 32,800 kg (72,312 lb), AR: 33,300 kg (73,414 lb)
Basic Operating Weight (standard): LR: 21,137 kg (46,599 lb), AR: 21,157 kg (46,643 lb)
Maximum Zero Fuel Weight: LR: 30,140 kg (66,447 lb), AR: 30,900 kg (68,123 lb)
Maximum Payload: LR: 9,003 kg (19,848 lb), AR: 9,743 kg (21,480 lb)
Maximum Usable Fuel: 9,335 kg (20,580 lb) or 11,625 l (3,071 gal)

Performance Specifications

Max Cruise Speed: Mach 0.82 for both LR and AR
Time to Climb to FL350: 16 minutes for both LR and AR
Takeoff Field Length: For 500 nm, full PAX: 1,151 m (3,776 ft); MTOW: LR: 1,582 m (5,190 ft), AR: 1,644 m (5,394 ft)
Landing Field Length: LR: 1,228 m (4,029 ft), AR: 1,241 m (4,072 ft)
Service Ceiling: 41,000 ft for both LR and AR
Range: LR: 2,100 nm (3,889 km), AR: 2,150 nm (3,982 km)

Fuel and Passenger Details

Fuel Density: 0.803 kg/l (6.70 lb/gal)
Passenger Weight Assumption: 100 kg (220 lb) per passenger

Seating Configurations

Single Class Configuration: 72 seats at 32” pitch
High Density Configuration: 78 seats at 33”/31”/30” pitch
Dual Class Configuration: 66 seats at 40” and 32” pitch

Catalog excerpts

E170 E170 DUAL CLASS CONFIGURATION 66 SEATS AT 40” AND 32” PITCH E170 SINGLE CLASS CONFIGURATION 72 SEATS AT 32” PITCH E170 HIGH DENSITY CONFIGURATION 78 SEATS AT 33”/31”/30” PITCH Maximum Takeoff Weight Maximum Landing Weight Basic Operating Weight (std) Maximum Zero Fuel Weight Maximum Payload Maximum Usable Fuel* Maximum Usable Fuel * Fuel Density: 0.803 kg/l (6.70 lb/gal) Time to climb to FL350 TOW for 500 nm, full PAX* Takeoff Field Length TOW for 500nm, full PAX*, ISA, SL, E5 engines Takeoff Field Length MTOW, ISA, SL - E5 engines for LR; E5A1 engines for AR version Landing Field Length...

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E170

E170

Catalog excerpts

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