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E175 > Limitations > Flashcards

Limitations Flashcards

1
Q

When is T/O-1 thrust required?

A

Altitude at or above 8,000ft or ISA + 35

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2
Q

Máximum headwind for CAT II

A

25 knots

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3
Q

Maximum crosswind for landing visibility < 4000 or 3/4

A

15 knots

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4
Q

Máximum tailwind for takeoff and landing

A

10 knots

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5
Q

Maximum runway slope

A

+2% -2%

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6
Q

Flap maneuvering load limit flaps up

A

-1.0 to +2.5 g

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7
Q

Flap maneuvering load limit flaps down

A

0.0 to 2.0 g

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8
Q

Maximum operating altitude

A

41,000 ft.

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9
Q

Maximum takeoff and landing altitude

A

10,000 ft

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10
Q

Maximum SAT for takeoff, landing and ground start

A

54’c

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11
Q

Maximum altitude with flaps extended

A

20,000 ft

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12
Q

Maximum flight operating latitude

A

78 n
78 s

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13
Q

Minimum SAT for takeoff, landing, and ground start.

A

-40’c

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14
Q

Maximum crosswind for takeoff
Dry runway

A

35

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15
Q

Maximum crosswind for takeoff
Wet runway

A

30

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16
Q

Maximum crosswind for takeoff
Runway with frost

A

31

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17
Q

Maximum crosswind for takeoff
Compacted snow/RWY CC 4

A

20

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18
Q

Maximum crosswind for takeoff
Standing water /slush / wet snow / dry snow

A

18

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19
Q

Maximum crosswind for takeoff
Slippery when wet / RWY CC 3

A

15

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20
Q

Maximum crosswind for takeoff
Ice

A

12

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21
Q

Maximum crosswind for landing
RWYCC 6

A

38

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22
Q

Maximum crosswind for landing
RWYCC 5 good

A

31

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23
Q

Maximum crosswind for landing
RWYCC 4 good to medium

A

20

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24
Q

Maximum crosswind for landing
RWYCC 3 medium

A

15

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25
Q

Maximum crosswind for landing
RWYCC 2 medium to poor

A

12

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26
Q

Maximum crosswind for landing
RWYCC 1 poor

A

8

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27
Q

Maximum crosswind for landing
RWYCC 0 nil

A

Operations prohibited

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28
Q

Unless prohibited by MEL, CAT II, emergency. RCC < 5/5/5

A

Flaps must be full

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29
Q

Maximum operating speed Vmo

A

320

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30
Q

Maximum operating Mach number Mmo

A

.82

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31
Q

Maximum speed for RAT operation

A

Vmo/Mmo

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32
Q

Turbulent airspeed (below 10,000)

A

250 kias

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33
Q

Turbulent airspeed (at or above 10,000)

A

270 kias / .76 mach whichever is lower

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34
Q

Tire limit ground speed

A

195 knots

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35
Q

Maximum airspeed for windshield wiper operation

A

250 kias

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36
Q

Maximum airspeed for windshield wiper failed in the non-parked position

A

320 KIAs

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37
Q

Maximum airspeed to open flight deck window

A

160 kias

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38
Q

Maximum gear operation speed

A

250 kias

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39
Q

Maximum flap operating speed
Flap 1

A

230

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40
Q

Maximum flap operating speed
Flap 2

A

215

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41
Q

Maximum flap operating speed
Flap 3

42
Q

Maximum flap operating speed
Flap 4

43
Q

Maximum flap operating speed
Flap 5

44
Q

Maximum flap operating speed
Flap full

45
Q

Maneuvering speed

46
Q

Icing conditions exist on the ground and takeoff

A

OAT at or below 10’c and
Visible moisture in any form is present such as clouds, fog (vis 1 mile or less) rain, snow, sleet and ice crystal, or
When on ramps, taxiways or runways where surface snow, ice, standing water, or slush may be ingested by engines, freeze on engines nacelles or engine sensor probes.

47
Q

Icing conditions exist inflight

A

TAT at or below 10’c and
Visible moisture in any form is present such as clouds, fog (vis 1 mile or less) rain, snow, sleet and ice crystals

48
Q

Set REF A/I to ALL for takeoff when

A

Outside temperature is at or below 10’c and ceiling is at or below 1,700 ft AFE

49
Q

Maximum usable fuel per tank is

A

10,392 lbs

50
Q

Unusable fuel per tank is

51
Q

Minimum fuel temperature

52
Q

Maximum fuel imbalance

53
Q

Maximum altitude for single pack operation

54
Q

Pressurization limitations
Maximum differential pressure

55
Q

Pressurization limitations
Maximum differential over pressure

56
Q

Pressurization limitations
Maximum negative differential pressure

57
Q

Pressurization limitations
Maximum differential pressure for takeoff and landing

58
Q

Maximum altitude with flaps extended

59
Q

Minimum Engagement altitude for the autopilot during takeoff or go around

A

400 ft AFE

60
Q

Minimum altitude for the autopilot on landing

61
Q

Maximum engine ITT
Normal takeoff and go around

A

965 (2min)
949 (3min)

62
Q

Maximum engine ITT
Maximum takeoff and go around

A

1006 (2 min)
990 (3 min)

63
Q

Maximum engine ITT
Maximum continuos

64
Q

Maximum engine ITT
Engine starts

65
Q

Engine RPM limits
N1

A

Min ——. Max 99.5%

66
Q

Engine RPM limits
N2

A

Min 58.5 Max 99.4

67
Q

Oil temperature
Continues

68
Q

Oil temperature
Transient

A

163’c
15 min limit

69
Q

Oil pressure
Min

70
Q

Oil pressure
Max

71
Q

Starter time limits
1st and 2nd

A

90 seconds on (ground) 10 sec off
120 seconds on (flight). 10 sec off

72
Q

Starter time limits
3rd thru 5th

A

90 seconds on ( ground) 5 min off
120 seconds on (flight) 5 min off

73
Q

Dry motoring time limits
1st

A

90 seconds on 5 min off

74
Q

Dry motoring time limits
2nd thru 5th

A

30 seconds on 5 min off

75
Q

APU STARTER TIME LIMITS
1st and 2nd

A

Start on / 60 seconds off

76
Q

Apu starter limits
3rd

A

Start on / 5 minutes off

77
Q

Apu operational limits starting
Minimum temperature

78
Q

Apu operational limits starting
Maximum temperature

79
Q

Apu operational limits starting
Maximum altitude

80
Q

Apu operational limits for operation
Electrical

81
Q

Apu operational limits for operation
Bleed

82
Q

Apu operational limits for operation
To assist engine start

83
Q

Apu operational limits for operation
Rotor speed

84
Q

Apu operational limits for operation
EGT START

85
Q

Apu operational limits for operation
EGT CONTINUOUS

86
Q

Circuit breaker resets

A

Tripped fuel boost or fuel indicating system is prohibited

87
Q

Minimum battery temperature for Apu starting

A

Batt #2 - 20 c

88
Q

Maximum altimeter difference CA FO for RVSM

89
Q

operations at ISA +35c - +39c
Apu starter limits 1st

A

Start/on 60 seconds off

90
Q

operations at ISA +35c - +39c
Apu starter limits 2nd

A

Start / on 5 minutes off

91
Q

operations at ISA +35c - +39c
Electrical

A

After engine start at least 2 AC power sources are required.

92
Q

operations at ISA +35c - +39c
Single engine taxi

A

APU ON
APU generator ON
single engine taxi without APU is prohibited

93
Q

Dry ice

A

Must be carried in the forward cargo

94
Q

Dry ice quantity

A

E70 no fan prohibited
E70 / 75 …. 50 lbs

95
Q

Cabin altitude HI / rapid depressurization

A
  1. Oxygen Mask ………… on, 100%
96
Q

Jammed control column - pitch

A
  1. Elevator disconnect ….. press and pull
97
Q

Jammed control wheel - roll

A

Aileron disconnect… press and pull

98
Q

Pitch trim runaway

A
  1. AP / trim disc ……. Press and hold
  2. TRIM PITCH SYS 1&2 cutout…push in
99
Q

(Roll or yaw) trim runaway

A
  1. AP/trim DISC ….. press and hold
100
Q

Nosewheel steering runaway

A
  1. STEER DISC ……. Press
101
Q

Aborted engine start

A
  1. Associated thrust lever …… IDLE
  2. Associated START/stop ….. stop

E175 (1 decks)

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