E175 Limitations Flashcards

1
Q

Aircraft Length

A

103’ 11”

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2
Q

Aircraft Width

A

93’ 11”

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3
Q

Aircraft Height

A

32’ 4”

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4
Q

Max PAX

A

76

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5
Q

First class seats

A

12

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6
Q

Coach seats

A

64

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7
Q

Cargo FWD compartment weight limit

A

3,307 lbs.

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8
Q

Cargo AFT compartment weight limit

A

2,535 lbs.

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9
Q

Aircraft Weight: MRW

A

85,870 lbs.

(85,800)

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10
Q

Aircraft Weight: MTOW

A

85,517 lbs.

(85,500)

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11
Q

Aircraft Weight: MLW

A

74,957 lbs.

(74,900)

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12
Q

Aircraft Weight: MZFW

A

69,886 lbs.

(69,800)

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13
Q

Minimum Crew

A

Left seat pilot & Right seat pilot

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14
Q

Aircraft Operations

A
  • Day & Night
  • VFR & IFR
  • Icing Conditions
  • CAT I & CAT II
  • RVSM
  • Extended Overwater Operation (EOW equipped)
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15
Q

Max Cabin Differential Overpressure:

A

8.8 psi

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16
Q

Max Cabin Differential Pressure (Above FL370):

A

8.4 psi

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17
Q

Max Cabin Differential for Takeoff & Landing

A

0.2 psi

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18
Q

Max Cabin Differential Negative Pressure

A

-0.5 psi

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19
Q

Max Altitude Depressurized

A

10,000’ or MEA whichever is higher

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20
Q

Mmo (Above FL280)

A

0.82

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21
Q

Vmo (Above 10,000’ to FL280)

A

320 KIAS

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22
Q

Vmo (Below 10,000’)

A

FAA - 250 KIAS
Structural - 300 KIAS

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23
Q

Va

A

240 KIAS

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24
Q

Vle

A

250 KIAS

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25
Q

Vlo

A

250 KIAS

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26
Q

Vlr

A

250 KIAS

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27
Q

Vfe1

A

230 KIAS

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28
Q

Vfe2

A

215 KIAS

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29
Q

Vfe3

A

200 KIAS

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30
Q

Vfe4

A

180 KIAS

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31
Q

Vfe5

A

180 KIAS

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32
Q

Vfefull

A

165 KIAS

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33
Q

Max Turbulent Airspeed (Below 10,000’)

A

250 KIAS

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34
Q

Max Turbulent Airspeed (10,000’ and Above)

A

270 KIAS or .76 Mach (whichever is higher)

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35
Q

Max Crosswind for Takeoff (Dry)

A

35 kts

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36
Q

Max Crosswind for Takeoff (Wet)

A

30 kts

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37
Q

Max Tailwind

A

10 kts

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38
Q

Max DV Window Operation

A

160 KIAS

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39
Q

Max Tire Speed

A

195 KIAS

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40
Q

Max Windshield Wiper Speed

A

250 KIAS

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41
Q

Max Operating Altitude

A

41,000’

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42
Q

Max Altitude with Flaps Extended

A

20,000’

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43
Q

Max Takeoff & Landing (alt)

A

10,000’

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44
Q

Min Takeoff & Landing (alt)

A

-1,000’

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45
Q

Min Takeoff & Landing Temperature (SAT)

A

-40°C

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46
Q

Max Takeoff & Landing Temperature (SAT)

A

52°C

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47
Q

Max altitude display difference in flight for RVSM

A

180’

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48
Q

In the event of a landing below _____°C, …

A

-40°C, the Airplane may not takeoff without further maintenance inspection.

49
Q

APU (brand)

A

Sundstrand APS 2300

50
Q

APU First & Second Start Attempts

A

START/ON then 60 sec. OFF

51
Q

APU Third Start Attempt

A

START/ON then 5 min. OFF

52
Q

APU Minimum Operation Temperature

A

-54°C

53
Q

APU Maximum Operation Temperature

A

ISA + 35°C

54
Q

APU EGT (Start)

A

1032°C

55
Q

APU EGT (Continuous)

A

717°C

56
Q

APU: No time limit in amber on the ground/inflight from ____ to ____

A

662°C to 717°C

57
Q

APU Max Operation Altitude (Electrical)

A

33,000’

58
Q

APU Max Start Altitude

A

30,000’

59
Q

APU Max Operation Altitude (Eng. Start Assist)

A

21,000’

60
Q

APU Max Operation Altitude (ECS Bleed)

A

15,000’

61
Q

APU Max Rotor Speed

A

108%

62
Q

AP Minimum Engagement Altitude on Takeoff or Go Around

A

Above 400’

63
Q

AP minimum Engaged Altitude during Landing

A

Above 50’

64
Q

Engine (Model)

A

GE CF34-8E5

65
Q

Engine: N1 RPM Max

A

99.5%

66
Q

Engine: N2 RPM Max

A

99.4%

67
Q

Engine: Max Start ITT

A

815°C

68
Q

Engine: Max Normal T/O ITT

A

965°C (2 min.)
949°C (3 min.) [Total: 5 min.]

69
Q

Engine: Max T/O & G/A ITT

A

1006°C (2 min)
990°C (3 min.) [Total: 5 min.]

70
Q

Engine: Max Continuous ITT

A

960°C

71
Q

Engine: Min Oil Pressure

A

25 psi

72
Q

Engine: Max Oil Pressure

A

95 psi

73
Q

Engine: Continuous Oil Temperature (Max)

A

155°C

74
Q

Engine: Transient Oil Temperature (Max)

A

163°C (15 min. limit)

75
Q

Engine: Thrust (T/O-1)

A

13,000 lbs.

76
Q

Engine: Thrust (T/O-1) (OEI ATTCS)

A

14,200 lbs.

77
Q

Engine: Thrust (T/O-2)

A

11,800 lbs.

78
Q

Engine: Thrust (T/O-2) (OEI ATTCS)

A

13,000 lbs.

79
Q

Fuel (Brazilian)

A

QAV1

80
Q

Fuel (ATSM)

A

Jet A or A1

81
Q

Fuel (MIL-T)

A

JP8

82
Q

Maximum Fuel Capacity

A

20,934 lbs. (10,467 per tank)

83
Q

Maximum Useable Fuel Quantity

A

20,784 lbs. (10,392 per tank)

84
Q

Unusable Fuel Quantity

A

150 lbs. (75 per tank)

85
Q

Maximum Fuel Imbalance

A

794 lbs.

86
Q

Adopted Fuel Density

A

6.77 lbs./US Gal.

87
Q

Minimum Fuel Tank Temperature

A

-37°C

88
Q

Crossfeed Operation Limitation

A

Crossfeed Knob must be OFF for Takeoff and Landing

89
Q

Starter: 1st Dry Motor

A

Max 90 sec. (5 min. Cool-Down)

90
Q

Starter: 2nd to 5th Dry Motor

A

Max 30sec. (5 min. Cool-Down)

91
Q

Starter: After 5 sequential Dry Motors, the cycle may be repeated following a ____ min. Cool-Down period.

A

15 min.

92
Q

Starter: 1st & 2nd Start (Grd)

A

90 sec. (With 10 sec. Cool-down)

93
Q

Starter: 1st & 2nd Start (Flt)

A

120 sec. (With 10 sec.Cool-down)

94
Q

Starter: 3rd to 5th Start (Grd)

A

90 sec (with 5 min. Cool-down)

95
Q

Starter: 3rd to 5th Start (Flt)

A

120 sec. (With 5 min. Cool-down)

96
Q

Flaps Up Min Speed

A

210

97
Q

Flaps 1 Min Speed

A

180

98
Q

Flaps 2 Min Speed

A

160

99
Q

Flaps 3 Min Speed

A

150

100
Q

Flaps 4/5 Min Speed

A

140

101
Q

Flaps Full Min Speed

A

Vapp

102
Q

Engine: N2 RPM Min.

A

58.5%

103
Q

Wing/Engine Strikes During Landing. Angle:

A

18º at touchdown

16° with gear struts compressed

104
Q

Max Crosswind Landing (Code 6)

A

38

105
Q

Max Crosswind Landing (Code 5)

A

31

106
Q

Max Crosswind Landing (Code 4)

A

20

107
Q

Max Crosswind Landing (Code 3)

A

15

108
Q

Max Crosswind Landing (Code 2)

A

12

109
Q

Max Crosswind Landing (Code 1)

A

8

110
Q

Max Crosswind Takeoff (Dry)

A

35

111
Q

Max Crosswind Takeoff (Wet)

A

30

112
Q

Max Crosswind Takeoff (Compacted Snow)

A

20

113
Q

Max Crosswind Takeoff (Standing Water)

A

18

114
Q

Max Crosswind Takeoff (Slush)

A

18

115
Q

Max Crosswind Takeoff (Wet Snow)

A

18

116
Q

Max Crosswind Takeoff (Dry Snow)

A

18

117
Q

Max Crosswind Takeoff (Ice)

A

12

118
Q

Max Crosswind for Landing in Vis less than 4000 or 3/4

A

15