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E175 Study Items > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Takeoff Weight

A

85,517lbs

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2
Q

Max Landing weight

A

74,957lbs

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3
Q

Max Zero fuel weight

A

69,886lbs

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4
Q

Max Aft Cargo

A

2,535lbs

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5
Q

Max Forward Cargo

A

3,306lbs

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6
Q

Minimum runway width

A

100 Feet (SW)

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7
Q

Wing Span

A

93ft 11in

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8
Q

Aircraft length

A

103ft 11in

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9
Q

Tail Hieght

A

32ft 4in

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10
Q

Max Operation Altitude

A

41,000ft

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11
Q

Max Takeoff and landing altitude

A

8,000ft

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12
Q

Max temp takeoff and landing

A

ISA +35•C (52•C)

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13
Q

Min temp takeoff and landing

A

-40•C

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14
Q

Runway Slope

A

+/- 2%

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15
Q

Max Tailwind

A

15kt

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16
Q

Max single pack operation

A

31,000ft

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17
Q

VMO SL-8,000’

A

300

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18
Q

VMO SL-10,000’- Mach Transition

A

320

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19
Q

MMO

A

.82

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20
Q

VA

A

240

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21
Q

VLO EXT

A

250

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22
Q

VLE RET

A

250

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23
Q

VLE

A

250

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24
Q

V Tire

A

195

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25
Q

V RAT Deploy Max

A

VMO/MMO

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26
Q

Vmin (to provide electrical power)

A

130

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27
Q

Vb (below 10,000ft)

A

250

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28
Q

Vb (10,000ft and above)

A

270/.76m (whichever is lower)

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29
Q

Vwiper operation max

A

250 (SW)

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30
Q

Vwindow

A

160

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31
Q

VFE 1

A

230

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32
Q

VFE 2

A

215

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33
Q

VFE 3

A

200

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34
Q

VFE 4

A

180

35
Q

VFE 5

A

180

36
Q

Flaps Full

A

165

37
Q

Dry Runway Croswind

A

38kt

38
Q

Wet Runway Crosswind

A

31kt

39
Q

Runway with compact snow crosswind

A

20kt

40
Q

Runway with standing water, slush, wet snow, dry snow crosswind

A

18kt

41
Q

Runway with ice crosswind

A

12kt

42
Q

Max altitude flaps/ slats extended

A

20,000ft

43
Q

Enroute operation slats/ flaps

A

Prohibited

44
Q

Minimum spoiler speed

A

180kt

45
Q

Cat II approach slats/ flaps

What setting?

A

Mandatory flaps 5

46
Q

Go Around

Landing Flaps Full

A

Go around flaps 4

47
Q

Go Around

Landing flaps 5

A

Go around flaps 2

48
Q

Battery minimum voltage

A

22.5v

49
Q

Engine start temp limit max

A

815c

50
Q

Oil temp start temp minimum

A

-40c

51
Q

Oil pressure start minimum

A

25psi

52
Q

Engine start ground cranking limits

A

Starts 1-2
-90 sec on/ 10 sec off

Starts 3-5
-90 sec on/ 5 min off

53
Q

Starter cranking limits engines (in flight)

A

Starts 1-2
-120 sec on/ 10 sec off

Starts 3-5
-120 sec on/ 5 min off

54
Q

Dry motoring limits

A

Motor 1
-90 sec on/ 5 min off

Motor 2-5
-30 sec on/ 5 min off

After 5 cycles the process may be repeated after 15 minutes

55
Q

No N1 % increase manual abort (ground start)

A

50% N2

56
Q

Fuel capacity total

A

20,935lbs

57
Q

Max fuel imbalance

A

794lbs

58
Q

Minimum fuel tank temp

A

-37c

59
Q

Wait 30 seconds after the EICAS is energized to start the APU

A

True

60
Q

Simultaneous use of the APU bleed and the HP cart is prohibited

A

True

61
Q

APU Starter duty cycles

A

Attempt 1-2
60 sec off

Attempt 3
5 min off

62
Q

APU start temperature min/max

A

-54c/ ISA + 35

63
Q

APU max start altitude

A

30,000 ft

64
Q

APU continuous operation min/ max temps

A

-54c / ISA + 35 (52c)

65
Q

APU operation Max altitude

A

33,000 ft

66
Q

APU GEN use Max altitude

A

33,000 ft

67
Q

APU Max altitude bleed use

A

15,000 ft

68
Q

APU Max altitude engine start

A

21,000 ft

69
Q

Max differential pressure up to FL370

A

7.8psi

70
Q

Max differential pressure above FL370

A

8.34psi

71
Q

Max differential over pressure

A

8.77psi

72
Q

Max differential negative pressure

A

-0.5psi

73
Q

Max differential pressure takeoff and landing

A

0.2 psi

74
Q

Min reservoir temp for engine start (hydraulics)

A

-18c

75
Q

Autopilot minimum engagement height

A

400ft

76
Q

Autopilot minimum use height

A

50ft

77
Q

Autopilot minimum use height on a non precision approach

A

MDA

78
Q

Between 5-10c the MCDU dataset menu must be set to ENG when visible moisture will be encountered up to 1,700 ft or on the ground at all.

A

True

79
Q

The MCDU data set menu must be set to ALL if the OAT is less than 5c. Moisture below 1,700ft or on the ground at all

A

True

80
Q

Max Ramp Weight

A

85,870lbs

81
Q

LL Max Ramp Weight

A

85,450

82
Q

LL Max T/O Weight

A

85,098

83
Q

LL Max Landing Weight

A

74,957

84
Q

LL Max Zero Fuel Weight

A

69,467

E175 Study Items (3 decks)

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