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Mesa Airlines > E175 Aircraft Limitations > Flashcards

E175 Aircraft Limitations Flashcards

1
Q

Maximum Ramp Weight (MRW)

A

85870lbs

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2
Q

Maximum Takeoff Weight (MTOW)

A

85,517lbs

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3
Q

Maximum Landing Weight (MLW)

A

74,957lbs

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4
Q

Maximum Zero Fuel Weight (MZFW)

A

69,886lbs

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5
Q

Maximum Takeoff and Landing Tailwind

A

10kts

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6
Q

Maximum Runway Slope

A

+/-2 degrees

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7
Q

G Limits

A 
Flaps up -1.0G - +2.5G
Flaps down (any setting) 0G - +2.0G
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8
Q

Maximum Operating Altitude

A

41,000’

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9
Q

Maximum TOL altitude

A

8,000’

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10
Q

Minimum TOL altitude

A

-1000’

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11
Q

Maximum Air Temperature for TOL’s

A

52 degrees Celcius

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12
Q

Maximum Flap Extension Altitude

A

20,000’

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13
Q

Maximum Latitude for Stationary Alignment

A

+/-78.25 degrees North or South

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14
Q

When landing below ______ degrees Celcius, you may not takeoff without further maintenace inspection

A

-40 degrees Celcius (SAT)

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15
Q

Minimum Operating Air Temperature

A

-54 degrees Celcius

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16
Q

Maximum Operating Mach Number (MMO)

A

0.82M

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17
Q

Maximum Operating Airspeed

A

VMO

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18
Q

Maximum Airspeed for Ram Air Turbine (RAT) operation

A

VMO/MMO

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19
Q

Turbulent Airspeed below 10,000’

A

250kias

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20
Q

Turbulent Airspeed at or above 10,000’

A

270kias/0.76M

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21
Q

Maximum Tire Limit Ground Speed

A

195kias

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22
Q

Maximum Windshield Wiper Operation Speed

A

253kias

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23
Q

Maximum Landing gear extension/extended/retraction speed

A

250kias for all
Vloe = landing gear extension
Vle = landing gear extended
Vlor = Landing gear retraction

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24
Q

Flaps 1 Speed limit

A

230kias

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25
Q

Flaps 2 Speed Limit

A

215kias

26
Q

Flaps 3 Speed limit

A

200kias

27
Q

Flaps 4 Speed limit

A

180kias

28
Q

Flaps 5 Speed Limit

A

180kias

29
Q

Flaps Full Speed Limit

A

165kias

30
Q

Maximum Operating Speed up to 8000’

A

300kias

31
Q

Maximum Operating Speed from 8,000’-10,000’

A

300-320kias increasing linearly with altitude

32
Q

Maximum Operating Speed from 10,000’-FL290

A

320kias (VMO)

33
Q

Maximum Operating Speed from FL290-FL410

A

0.82M (MMO)

34
Q

Definition of Icing conditions

A

Icing conditions exist whenever the OAT on the ground for takeoff, or Total Air Temperature (TAT) inflight, is 10°C or below, and visiible moisture in any form is present (such as clouds, fog with a visibility of 1sm or less, rain, snow, sleet, an ice crystals).

35
Q

Maximum Fuel Capacity (total)

A

20,935lbs total with 20,785 usable (10392.5lbs or 1535.5 usable US gallons per side)

36
Q

Unusuable Quantity per tank

A

75lbs

37
Q

Maximum Fuel Imbalance

A

794lbs (rounded to 800lbs)

38
Q

Minimum Fuel Temperature

A

-37ºC

39
Q

Crossfeed operations

A

Must be OFF for takeoff and landing

40
Q

Maximum Differential Pressure

A

8.4PSI

41
Q

Maximum Differential Overpressure

A

8.8psi

42
Q

Maximum Differential Negative pressure

A

-0.5psi

43
Q

Maximum Differential Pressure for Takeoff

A

0.2psi

44
Q

Maximum Altitude for single Pack Operation

A

FL310

45
Q

Maximum Brake Temperature for takeoff

A

Cannot takeoff with temperatures in the amber range

46
Q

Thrust Reverser Limitations

A
  • Ground use only
  • Not authorized while taxiing
  • Full stop landings only
  • No go-arounds after deployment
  • Power-back is prohibited
  • Minimum reverse thrust must be used with the translating cowl open below 60kias
  • Idle thrust with the translating cowl closed at 30kias
47
Q

Autopilot Minimum Engagement Height

A

400’AGL per Embraer, 1000’AGL per Mesa Airlines CFM

48
Q

Autopilot Minimum Use Height

A

50’AGL on a coupled ILS approach

49
Q

Embraer 175 engine type

A

General Electric CF34-8E5

50
Q

Maximum TOGA power time (both engines operting)

A

10 minutes

51
Q

Flex takeoff minimum thrust setting

A

No less than 25% less than full takeoff thrust

52
Q

When can a flex takeoff be performed?

A

Only on an uncontaminted runway

53
Q

When must ATTCS (automatic takeoff thrust control system) be on?

A

For all takeoffs and landings

54
Q

Engine starter duty llimits

A
  • 1st and 2nd attempts: 90* seconds on / 10 seconds off
  • 3rd through 5th attempts: 90* seconds on / 5 minutes off
  • = 120 seconds while in flight
55
Q

Dry Motoring Cycle Duty Limits

A
  • 1st attempt: 90 seconds on / 5 minutes off
  • 2nd-5th attempt: 30 seconds on / 5 minutes off
  • After 5th attempt, 15 minutes are required before the cycle can be repeated
56
Q

APU starter Duty Cycle

A
  • 1st and 2nd attempts: 1 minutes on / 1 minute off

- 3rd attempt: 1 minute on / 5 minutes off

57
Q

APU minimum start temperature and altitude

A

-54ºC and 30,000’

58
Q

APU altitude and other limitations

A
  • Max operating altitude: 33,000’
  • Max bleed altitude: 15,000’
  • Max engine start assist altitude: 21,000’
  • No APU time limit between 662-717ºC (amber range)
  • In flight there is no automatic APU shut down if EGT exceeds limits
59
Q

What is the difference between SAT and TAT?

A

SAT is Static Air Temperature, or the temperature of undisturbed air arounds the aircraft (i.e. OAT). TAT is Total Air Temperature which is the Static Air Temperature plus the temperature rise associated with high-speed flight. TAT can be measured by probe on the outside of the aircraft as the high speed causes adiabatic compression and heating of the air around the temperature probe. Knowing TAT, SAT can be computed which is required to calculate True Airspeed.

60
Q

When is TAS, TAT, and SAT accurate?

A

Above 60kias

61
Q

When is the standby compass not valid/trustworthy?

A

When transmitting on VHF #1

62
Q

Which kind of approaches cannot be done using IESS (Integrated Electronic Standby System, i.e. backup instruments)?

A

LOC back course approaches

Mesa Airlines (14 decks)

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