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89 Cards in this Set
- Front
- Back
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Min. Ambient Temperature For Takeoff
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-40ºC
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APU Start Temperature Min. / Max.
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-54ºC to +35 ISA
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EMB 175 MLW
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74957
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APU Operation Temperature Min. / Max.
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-62ºC / +35ºC ISA
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ITT Normal Takeoff & Go Around MAX.
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965ºC - 2 minute limit 949ºC - 3 minute limit 5 minute limit total
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EMB 175 MTOW
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85517
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Engine Starter Dry Motoring Limits
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1st - 90 sec. on - 5 min. off 2-5 - 30 sec. on - 5 min. off 5 - 30 sec. on - 15 min. off
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Engine Starter Duty Cycle Limits
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Always 90 sec. on (ground) Always 120 sec. on (flight) 1-2 - 10 sec. off 3-5 - 5 min. off
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EMB 175 MRW
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85870
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EMB 175 MZFW
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69886
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Oil Temperature Continuous
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155ºC
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Min. Ambient Temperature for Operation
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-54ºC
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Max. Differential Pressure Above 37,000
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8.34 psi
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Max. Differential Pressure Up to 37,000
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7.8 psi
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Max. Ambient Air Temperature for T/O & Landing
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ISA +35
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APU Altitude Bleed MAX.
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15,000 ft
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Oil Temperature Transient
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163ºC Limit 15 min. above 155ºC
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Max. Differential Overpressure
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8.77 psi
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APU Type
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Sunstrand APS 2300
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Max. Takeoff & Landing Altitude
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8,000 ft
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Max. Operating Altitude
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41,000 ft
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APU Starter Cycle
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1-2 - 60 sec. on - 60 sec. off 3 - 60 sec. on - 5 min. off
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VLO
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250 KIAS
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VLE
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250 KIAS
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Max. Windshield Wiper Operation Speed
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250 KIAS
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Max. Tire Limit Groundspeed
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195 kts
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Max. Altitude With Flaps Extended
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20,000 ft
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Min. Takeoff & Landing Altitude
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-1,000 ft
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Max. Flight Operating Latitude
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78 degrees North to 78 degrees South
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Unusable Quantity per Tank
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100 lbs
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Va
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240 KIAS
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Runway Surface Type
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Paved
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Max. Runway Slope
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+/- 2%
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Max. Tailwind Component
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10 kts
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Min. Autopilot Engagement Height
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400 ft
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Max. Airspeed For RAT Operation
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Vmo / Mmo
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Vfe Flap 1
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230 kts
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VLO Retraction
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250 KIAS
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Vfe Flap 3
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200 kts
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Vfe Flap 2
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215 kts
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Vfe Flap 4
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180 kts
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Vfe Flap 5
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180 kts
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Vfe Flap Full
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165 kts
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ITT Max. Continuous
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960 c
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Max. Turbulent Airspeed below 10,000 ft
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250 KIAS
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Max. Operating Airspeed
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Vmo
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Max. Operating Mach #
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0.82
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Max. Turbulent Airspeed at & above 10,000 ft
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270 KIAS / .70 Mach whichever is less
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Max. Differential Negative Pressure
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-0.5 psi
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Max. Fuel Imbalance
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800 lbs
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Powerplant
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G.E. CF-34-8E5
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APU Max. Rotor speed
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108.00%
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APU EGT Start Temperature Max.
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1,032ºC
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N2 Min / Max
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58.5% / 99.4%
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Vmo
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0 - 8,000 = 300 kts 8,000 - 29,000 = 320 kts 29,000 - 41,000 = .82 m
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N1 Min / Max
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- / 99.5%
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Max. Difference between ADS's -2,000 to 10,000
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50 ft
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Flap Maneuvering Load Accl. Limits Up
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-1.0g - +2.5g
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Max. Difference between ADS's 10,000 to 20,000
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120 ft
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Max. Differential Pressure for Takeoff & Landing
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.20 psi
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Min. Autopilot Height for Approaches
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200 ft 50 ft - ILS
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Max. Temperature at 41,000
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-21.5ºC
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Oil Pressure Min. / Max.
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25 psi / 95 psi
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Flap Maneuvering Load Accl. Limits Down
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0.0 - +2.0g
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Min. Temp at 41,000 ft
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-65ºC
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ITT Start Max.
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815ºC
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APU EGT Continuous Temp. Max.
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717ºC
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APU Altitude Assit Engine Start Max.
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21,000 ft
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APU Start Altitude Max.
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30,000 ft
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Max. Difference Between ADS's 20,000 to 41,000 ft
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180 ft
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170 MRW
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82364
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170 MTOW
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82011
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170 MZFW
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65,256 646RW & higher 66,446
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170 MLW
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72310
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Max. Usable Quantity per Tank
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10,367 lbs
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Aircraft Max. Fuel Capacity
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20,935 lbs
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APU Altitude Electrical Max.
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33,000 ft
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ITT Max. Takeoff & Go Around Max.
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1,006 ºC - 2 min. limit 990 ºC - 3 min. limit 5 min. limit total
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Min. Fuel Tank Temperature
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-40 ºC
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Minimum Temperature for Takeoff, Landing & Ground Start?
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-40 ºC SAT
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Types of Operations
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Visual
Night Instrument Icing CAT1 RVSM |
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Takeoff weight is limited by the most restrictive of the following:
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Max TO weight (Climb Limited)
Max field length limited TO weight Max Certificated TO weight Obstacle clearance, enroute, and landing limitations. Brake energy limit weights |
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Max landing weight is limited by the most restrictive of the following
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Max approach and landing weight(runway length plus obstacle, altitude,and temperature, and includes limitations for inoperative equipment)
Max landing weight (climb limited) Max certificated landing weight |
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Altimeter Miscompare tolerances
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Altitude Max difference
-2000' up to 10,000' 50 10,000' up to 20,000' 120 20,000' up to 41,000' 180 |
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Restrictions on flap use
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Enroute use of flaps is prohibited
Do not hold with flaps extended in icing conditions |
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Cooling limitation on brakes
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Do not take off with brakes in amber
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Thrust Reverse Limitations
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Ground use only
Full stop landings only Do not attempt a go-around after deployment Power back prohibited Landing roll-out below 60kts- a. Max reve not permitted b. Reduce rev to IDLE After selecting rev thrust, do not move thrust levers into the forward thrust range until the REV icon on EICAS is amber or green. |
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Engine starter duty cycle limits
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1st and 2nd starts -
90 seconds ON - 10 seconds OFF 3rd through 5th starts- 90 seconds ON - 5 minutes OFF (90 seconds on ground/ 120 seconds in flight) |
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Engine dry motor duty cycle limits
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1st
90 seconds ON - 5 minutes OFF 2nd through 5th 30 seconds ON - 5 minutes OFF After 5th sequential motoring, cycle may be repeated following a 15 minute cool down period. |
