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73855 33500 139 146 147 142 146 147 144 147 147 146 148 148
74958 34000 141 147 148 143 148 148 145 148 148 147 149 149 19 3 14 1 12 6
76060 34500 142 148 149 145 149 149 147 149 150 148 150 150
77162 35000 144 149 151 146 150 151 148 150 151 149 151 151 19 6 14 3 12 7
78265 35500 145 150 152 147 151 152 149 151 152 150 152 152
79367 36000 146 151 153 148 152 153 150 153 153 150 153 153 19 8 14 5 12 8
80469 36500 147 153 154 150 153 154 151 154 154 149 154 154
81571 37000 149 154 155 151 154 155 153 155 155 148 155 155 20 1 14 7 12 9
82674 37500 150 155 156 152 155 156 154 156 156 147 157 157
E190 --- Takeoff V-Speeds --- Flap 4 --- Mode T/O-1
Pressure Alt.
(ft.)
Static Air Temperature (°C)
SL → -40 to 34 35 to 40 41 to 46 47 to 50
1000 → -40 to 29 30 to 36 37 to 43 44 to 48
2000 → -40 to 26 27 to 31 32 to 38 39 to 45 46 to 46
3000 →
-40 to 27 28 to 34 35 to 41 42 to 44
4000 →
-40 to 22 23 to 29 30 to 36 37 to 42
5000 →
-40 to 24 25 to 32 33 to 40
6000 →
-40 to 19 20 to 27 28 to 38
7000 →
-40 to 21 22 to 36
8000 →
-40 to 15 16 to 34
9000 →
-40 to 32
10000 → -40 to 30
Weight ↓ ↓ ↓ ↓ ↓ Flap 4 Full
LBS KG V1 VR V2 V1 Vfs Vac Vref VR V2 V1 VR V2 V1 VR V2 Vfs Vac Vref
66139 30000 97 105 116 95 101 112 92 97 107 92 96 104 95 98 104 157 119 103
68344 31000 97 104 114 95 100 110 93 98 107 95 98 106 98 100 106 160 121 104
70548 32000 97 103 113 95 100 110 96 100 108 98 101 108 101 103 108 162 122 106
72753 33000 97 102 112 97 102 110 99 102 110 100 103 110 103 105 109 164 124 107
74958 34000 98 103 112 99 104 112 101 104 111 102 105 111 105 107 111 168 127 110
77162 35000 100 105 113 102 105 113 103 106 113 104 107 113 107 108 113 170 128 111
79367 36000 103 107 115 104 107 115 105 108 114 106 109 114 109 110 114 172 130 113
81571 37000 105 108 116 106 109 116 107 110 116 108 111 116 111 112 116 174 132 114
83776 38000 107 110 118 108 111 117 109 112 117 110 113 117 112 114 117 176 133 115
85981 39000 109 112 119 110 113 119 111 114 119 113 114 119 115 115 119 179 136 117
88185 40000 111 114 120 112 114 120 113 115 120 115 116 120 117 117 120 181 137 119
90390 41000 113 116 122 114 116 122 115 117 122 117 118 122 119 119 122 183 139 120
92595 42000 115 117 123 116 118 123 118 119 123 120 120 123 - - - 186 140 122
94799 43000 117 119 125 118 120 125 120 121 125 121 121 125 - - - 188 142 123
97004 44000 119 121 126 120 122 126 122 122 126 - - - - - - 190 144 125
99209 45000 121 123 128 122 123 128 124 124 128 - - - - - - 192 146 126
101413 46000 123 124 129 125 125 129 - - - - - - - - - 194 147 127
103618 47000 125 126 130 126 126 130 - - - - - - - - - 196 149 129
105822 48000 127 128 132 - - - - - - - - - - - - 199 151 130
108027 49000 129 129 133 - - - - - - - - - - - - 201 152 132
110232 50000 131 131 134 - - - - - - - - - - - - 203 154 133
E-170 Fuel Planning Charts:
Flightplan MZFW Fuel Break Climb: Cruise: Descend:
Fuel only 66.447 lbs Consumed Release to 250 / 300 kt M 0.78 M 0.78
ISA, no Wind (lbs) Landing M 0.78 300 / 250 kt
E170 max. Range at MZFW: ≈ 1500 nm
Fuelburn (lbs) per hour ≈ 3500 Fuelburn per 1nm ≈ 7,78
Distance
(nm)
Payload * Fuel (lbs) at Fuel (lbs) at Fuel (lbs) at Fuel (lbs) at
% / lbs FL 290/300 FL 310/320 FL 330/340 FL 350 - 410
100**
100 / 21100
1578
≈ 97% of
FL290
≈ 94% of FL
290
≈ 91% of FL 290
200 2356
300 3133
400 3911
500 4689
600 5467
700 6244
800 7022
900 7800
1000 8578
1500 12467
After 1500nm Payload has to be traded for fuel. ***
2000 76 / 16200 16356 ≈ 97% of
FL290
≈ 94% of FL
290
≈ 91% of FL 290
2100 72 / 15400 17133
* Maximum Payload to MTOW (including pilots at 640lbs). (Max Fuel = 20580 lbs)
** For a distance of 100nm altitudes of 15000ft maximum are assumed.
*** Flying in higher altitudes - consuming less fuel - it is possible to carry the same payload over a
longer range with the trade-off between the fuel, range and payload affecting the aircraft
after a longer distance.
Basic Operating Weight (OEW) 046.385 LBS
Fuel planning notes E170:
= Zero Fuel Weigh (ZFW) XXX.XXX LBS (max 66.447 LBS)
+ Payload (passengers & cargo) XXX.XXX LBS
+ Minimum Landing Fuel 001.000 LBS
+ Alternate Fuel (200nm distance) 001.500 LBS
= Planned Landing Weight (PLW) XXX.XXX LBS (max 72.312 LBS)
+ Contingency Fuel (holding, taxi, etc.) 001.000 LBS
= Planned Takeoff Weight (PTOW) XXX.XXX LBS (max 80.012 LBS)
　
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