E175 General Limitations Flashcards

1
Q

Max takeoff weight

A

85,517

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2
Q

Max landing weight

A

74,957

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3
Q

Max zero fuel weight

A

69,886

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4
Q

FWD baggage compartment capacity

A

3306

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5
Q

AFT baggage compartment capacity

A

2534

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6
Q

Maximum altitude for flaps extended

A

20,000

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7
Q

Landing gear operation/extended speed (VLO and VLE)

A

250

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8
Q

Maximum speed to open direct vision window

A

160

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9
Q

Max speed flaps 1

A

230

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10
Q

Max speed flaps 2

A

215

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11
Q

Max speed flaps 3

A

200

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12
Q

Max speed flaps 4

A

180

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13
Q

Max ramp weight

A

85,870

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14
Q

Max speed flaps 5

A

180

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15
Q

Max speed flaps full

A

165

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16
Q

Maximum tire ground speed

A

225 mph, 195 kt

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17
Q

Maximum takeoff and landing tailwind component

A

10 kt

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18
Q

Maximum recommended crosswind - dry runway

A

38 kt

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19
Q

Maximum recommended crosswind - wet runway

A

31 kt

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20
Q

Maximum recommended crosswind - runway with compacted snow

A

20 kt

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21
Q

Maximum recommended crosswind - runway with standing water/slush/wet snow/dry snow

A

18 kt

22
Q

Maximum recommended crosswind - runway with ice (including wet ice)

A

12

23
Q

Maximum recommended crosswind - Static takeoff

A

25

24
Q

Maximum usable quantity per tank

A

1535.5 gallons - 10392.5 lbs

25
Q

Unusable quantity per tank

A

11 gallons - 75 lbs

26
Q

Maximum fuel capacity

A

3,094 gallons - 20,935 lbs

27
Q

Maximum permitted fuel imbalance between tanks

A

794

28
Q

Minimum fuel tank temperature

A

-40C

29
Q

Maximum altitude to START the APU

A

30,000

30
Q

Maximum operating altitude for the APU

A

33,000

31
Q

Maximum altitude for the APU for electrical use

A

33,000

32
Q

Maximum altitude to use bleed air from the APU

A

15,000

33
Q

Maximum altitude for the APU to assist engine start

A

21,000

34
Q

APU starter limits - cooling period after first and second attempt

A

60 seconds OFF

35
Q

APU starter limits - cooling period after third attempt

A

5 minutes OFF

36
Q

What is equipment is required for RVSM? CFM 2.27

A

1 Autopilot - Must be operational
Altitude Alerting System - Must be operational
2 Altitude Reporting Transponders - One must be operational
2 Air Data Computers - Two must be operational

37
Q

Autopilot minimum engagement height:

A

400 feet

38
Q

Autopilot minimum use height

A

50 feet

39
Q

Max airspeed for windshield wipers

A

253 Ktus

40
Q

Single pack operational limit

A

FL310

41
Q

Engine type on the E-175

A

CF34-8E5

42
Q

Max runway slope

A

+-2%

43
Q

Positive load factor limits with flaps up or down:

A

Flaps up = 2.5g

Flaps down = 2.0g

44
Q

Negative load factor limits with flaps up and flaps down:

A

Flaps up = -1.0g

Flaps down = 0g

45
Q

Max tire ground speed

A

195 it’s

46
Q

Max N1 with breaks applied:

A

60%

47
Q

Recommended airspeed in turbulence:

A

Below 10,000 = 250 Kts

At or above 10,000 = 270/.76

48
Q

Minimum fuel tank temperature

A

-40 C

49
Q

APU Starter limits:

A

First and second attempts - 1 min on, 1 min off

Third attempt - 1 min on, 5 min off

50
Q

Dry motoring duty cycle limits:

A

Attempt 1 - 90 seconds, 5 min cool down
Attempt 2-5 - 30 seconds, 5 min cool down

After 5 sequential motorings, cycle may be repeated following a 15 min cool down period.