E-JETS FAMILY EMBRAER 175
E-JETS FAMILY
170
175
190
195
SPECIFICATIONS
WEIGHTS Maximum Takeoff Weight Maximum Landing Weight Maximum Zero Fuel Weight Basic Operation Weight Maximum Payload Maximum Fuel*
*Fuel Density: 0.803 kg/l (6.70lb/gal)
STD & LR Versions STD LR 82,673 lb 85,517 lb 74,957 lb 69,887 lb 47,664 lb 22,223 lb 20,580 lb 37,500 kg 38,790 kg 34,000 kg 31,700 kg 21,620 kg 10,080 kg 9,335 kg
AR Version 89,000 lb 75,178 lb 70,548 lb 47,708 lb 22,840 lb 20,580 lb 40,370 kg 34,100 kg 32,000 kg 21,640 kg 10,360 kg 9,335 kg
EMBRAER 175
PERFORMANCE (AR Version) Maximum Operating Speed Time to Climb to FL 350, TOW for 500 nm Takeoff Field Length, ISA, SL MTOW Takeoff Field Length, ISA, SL TOW to 500 nm Landing Field Length, ISA, SL MLW Range 78 PAX @ 220 lb (100 kg), LRC EXTERNAL DIMENSIONS Wingspan Length Overall Height Overall Horizontal Stabilizer Span Fuselage Width Fuselage Height INTERNAL DIMENSIONS Cabin Length (excluding cockpit) Cabin Width (at armrest) Cabin Height Aisle Width Seat Width 69 ft 7 in 9 ft 0 in 6 ft 7 in 19.75 in 18.25 in 21.20 m 2.74 m 2.00 m 0.50 m 0.46 m 85 ft 4 in 103 ft 11 in 31 ft 11 in 32 ft 10 in 9 ft 11 in 11 ft 0 in 26.00 m 31.68 m 9.73 m 10.00 m 3.01 m 3.35 m M 0.82 18 min 7,362 ft 4,137 ft 4,278 ft 2,000 nm M 0.82 18 min 2,244 m 1,261 m 1,304 ft 3,706 km
VIEWS
31 ft 11 in (9.73 m)
103 ft 11 in (31.68 m)
31 ft 11 in (9.73 m)
103 ft 11 in (31.68 m)
32 ft 10 in (10.00 m) 31 ft 11 in (9.73 m)
103 ft 11 in (31.68 m)
32 ft 10 in (10.00 m)
85 ft 4 in (26.00 m) 32 ft 10 in (10.00 m)
85 ft 4 in (26.00 m)
85 ft 4 in (26.00 m)
June 2007
E-JETS FAMILY EMBRAER 175
A NEW CABIN CONCEPT
A double-bubble fuselage design means passengers enjoy an extraordinary amount of personal space. The widest seat and the widest aisle in the category add to passenger comfort. Four-abreast seating eliminates the undesirable middle seat, easing access and making boarding and deplaning smoother and faster.
PERFORMANCE
Short field capability, superior hot and high performance, and 2,000 nm range combine to deliver maximum operational versatility.
(kg) 12,000 AR LR
88 PAX @ 100 kg
PAYLOAD
(lb) 30,000
10,000 STD
25,000
8,000
Carry-on Bag Size 24 x 16 x 10 in 61 x 40 x 25 cm
78 PAX @ 100 kg
20,000
30.80 in 0.78 m
EMBRAER 175 INTERIOR LAYOUTS
SINGLE CLASS 78 seats at 32 pitch
6,000
15,000
FLY- BY- WIRE (FBW)
Pilot workload is reduced and aircraft performance is optimized with integrated flight control systems guided by fly-by-wire technology. FBW and 100% cockpit commonality minimize crew transition costs between any aircraft in the E-Jets family.
4,000
10,000
2,000
5,000 0 0 500 1,000 1,500 2,000 2,500 3,000 RANGE (nm)
18.25 in 0.46 m 4 ft 9 in 1.44 m 39
6 ft 7 in 2.00 m
ENGINE
FADEC-controlled diagnostics, fully
COCKPIT
ASSUMPTIONS Typical Mission Reserves - Cruise at M 0.78 - Passengers @ 100 kg (220 lb) each
SINGLE CLASS 86 seats at 31 pitch
11 ft 0 in 3.35 m
interchangeable right and left engines, environmental enhancements, and 30minute LRU replacement efficiency make General Electrics CF34-8E the most comprehensive, value-added propulsion system in the industry.
Engine Characteristics GE CF34-8E
ECONOMICS
The cost-effective use of the latest technologies makes the EMBRAER 175 the most efficient aircraft available in the 78 to 88 seat segment. The best structural efficiency, excellent fuel burn, and outstanding aircraft maintainability characteristics provide significant cost advantages to airlines.
01. Audio Control Panel 02. Speed Brake 03. Cursor Control Device (CCD) 04. EICAS 05. Integrated Electronic 09. Primary Flight Display (PFD) 10. Multi-Function Display (MFD) 11. Multi-Function Control Display Unit (MCDU)
19.75 in 0.50 m 3 ft 1 in 0.94 m
HIGH CAPACITY 88 seats 30 pitch
Sea Level Flat Rating 86F/30C APR Thrust Installed NTO Thrust Installed Length Weight Dry Engine Maximum Diameter Thrust-to-Weight Ratio Fan Bypass Ratio Noise 14,200 lb 13,800 lb 121.2 in / 307.8 cm 2,627 lb / 1,192 kg 53.4 in / 136 cm 5.41 5:1 Stage III and IV Compliant
BREAK-EVEN*
58%
9 ft 0 in 2.74 m 9 ft 11 in 3.01 m
DUAL CLASS 78 seats (6F/72Y) at 38/31 pitch
Standby System 12. Engine Panel (IESS) 13. Ram Air Turbine 06. Lights Panel 07. Guidance Panel 08. Landing Gear
*
PROFIT
14. Flap 15. Thrust Lever
Based on Total Operation Costs; 500 sm sector
