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