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ERJ 170 Limitations
Limitation flash cards
| Question | Answer |
|---|---|
| Maximum Ramp Weight (MRW) E170 | 82,364 lbs. |
| Maximum Takeoff Weight (MTOW) E170 | 82,011 lbs. |
| Maximum Landing Weight (MLW) E170 | 72,310 lbs. |
| Maximum Zero Fuel Weight (MZFW) E170 | 65,256 lbs. |
| Maximum Zero Fuel Weight (MZFW) E170 N646RW and higher: | 66,446 lbs. |
| Maximum Ramp Weight (MRW)E175 | 85,870 lbs. |
| Maximum Takeoff Weight (MTOW) E175 | 85,517 lbs. |
| Maximum Landing Weight (MLW) E175 | 74,957 lbs. |
| Maximum Zero Fuel Weight (MZFW) E175 | 69,886 lbs. |
| Maximum takeoff and landing tailwind component: | 10 knots |
| Max. Runway Slope | +/- 2.0% |
| Flap maneuvering load acceleration limits; Flaps Up: Flaps Down: | Up: -1 G to +2.5Down: 0.0G to +2.0 G |
| Max operating altitude: | 41,000 ft |
| Max. takeoff and landing altitude: | 8,000 ft |
| Max. ambient air temperature for T/O and landing: | 52*C |
| Max. flap extension altitude: | 20,000 ft. |
| Max. flight operating latitude: | 78*N to 78*S |
| Min. ambient temperature approved for takeoff: | -40*C |
| Min. ambient temperature for operation: | -54*C |
| Maximum Difference Between Altitudes:ADS 1 to ADS 2; ADS 1 to ADS 3/IESS; ADS 2 to ADS 3/IESS: -2000 up to 10000 ft. | 50 Feet |
| Maximum Difference Between Altitudes:ADS 1 to ADS 2; ADS 1 to ADS 3/IESS; ADS 2 to ADS 3/IESS: 10000 up to 20000 ft. | 120 Feet |
| Maximum Difference Between Altitudes:ADS 1 to ADS 2; ADS 1 to ADS 3/IESS; ADS 2 to ADS 3/IESS: 20000 up to 41000 ft. | 180 Feet |
| When the altitude between the Captain's and First Officer's display exceed ____FT., use PFD 1 as the selected source for autopilot. | 100 |
| Maximum operating airspeed: | Vmo |
| Maximum operating mach number: | .82 (Mmo) |
| Maximum airspeed for RAT operation: | Vmo/Mmo |
| Turbulent airspeed (below 10,000ft) | 250 KIAS |
| Turbulent airspeed (at or above 10,000ft) | 270 KIAS/.70M |
| Maximum tire limit ground speed: | 195 knots (225mph) |
| Maximum windshield wiper operation speed: | 250 KIAS |
| Design Maneuvering Speed - VA | 240 KIAS |
| Maximum operating speed KIAS at 8,000 ft. | 300 KIAS |
| Maximum operating speed KIAS at 10,000 ft. | 320 KIAS |
| Fuel Quantity: Maximum usable quantity per tank: | 10367 lbs |
| Fuel Quantity: Unusable quantity per tank: | 100 lbs |
| Fuel Quantity: Aircraft maximum fuel capacity (usable + unusable fuel) | 20,935 lbs |
| Approved Fuels: | Jet A, Jet A-1, JP-8, QAV1 (Brazilian Specification) |
| Min. Fuel Tank Temperature: | -40C |
| Fuel Imbalance: | 800 lbs |
| Maximum Differential Pressure: -Up to 37,000ft | 7.8 psi |
| Maximum Differential Pressure: -Above 37,000ft | 8.34 psi |
| Maximum differential overpressure: | 8.77 psi |
| Maximum differential negative pressure: | -.5 psi |
| Maximum differential pressure for takeoff and landing: | .20 psi |
| Maximum altitude for single pack operation: | 31,000 ft. |
| Brake Limitation for takeoff: | Do not takeoff with amber brake temperature indication. |
| Maximum altitude with flaps extended: | 20,000 ft. |
| Two Flap limitations: | 1. Enroute use of flaps is prohibited.2. Do not hold in icing conditions with flaps extended. |
| TAS, TAT, and SAT are only valid above ___KIAS | 60 KIAS |
| Standby magnetic compass indication is not valid while transmitting on VHF #___ | VHF #1 |
| LOC Backcourse approaches using _____ is not authorized. | IESS |
| Power Plant Type: | Two General Electric CF-34-8E5 Engines. |
| Engine Operational Limits: -N1 max. | 99.5% |
| Engine Operational Limits: -N2 min/max | 58.5% - 99.4% |
| Engine Operational Limits: Max temp. for start: | 815C |
| Engine Operational Limits: -Normal takeoff and Go Around | 965C first 2 minutes/ 949C for the remaining 3 minutes. |
| Engine Operational Limits: -Maximum Takeoff and Go Around | 1006C for the first 2 minutes/990C for the remaining 3 minutes. |
| Engine Operational Limits: -Maximum Continuous Temp. | 960C |
| Oil pressure Limits: min/max | 25 psi to 95 psi |
| Oil Temperature continuous: | 155C |
| Oil Temperature Transient: | 163C (Time limited to 15 minutes for transient peration above 155C) |
| Engine Starter Duty Cycle Limits: | 1st and 2nd starts, 90sec (gnd) 120sec (in flight) 10 seconds OFF. 3rd - 5th starts 90/120 then 5 minutes OFF. |
| Engine Starter Dry Motoring Duty Cycle Limits: | 1st 90 seconds ON/5 minutes OFF. 2nd-5th 30 seconds ON/5 minutes OFF. |
| APU Limits: Min/max ambient temps. for start. | -54C to ISA + 35C |
| APU Limits: Max Start Altitude | 30,000 ft. |
| APU operating temperature range: | -62C to ISA + 35C |
| APU Operating altitude limits: -Electrical | 33,000 ft |
| APU Operating altitude limits: -Bleed | 15,000 ft |
| APU Operating altitude limits: -To assist engine start | 21,000 ft |
| APU Operating limits: -Rotor Speed | 108% |
| APU Operating limits: -EGT START/Continuous | 1032C/717C |
| APU starter duty cycle: | 1st and 2nd - 60 seconds ON/60 seconds OFF3rd cycle - 60 seconds ON/5 minutes OFF |
| Four Required Items for RVSM above FL290: | 2 RVSM Compliant Air Data Systems1 autopilot with altitude hold mode operative1 altitude alerter1 transponder |
Created by:
RBadley
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