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Envoy E175 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Ramp Weight

A

85,870lb

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2
Q

Max Takeoff Weight (MTOW)

A

85,517lb

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3
Q

Max Landing Weight (MLW)

A

74,957lb

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4
Q

Max Zero Fuel Weight (MZFW)

A

69,886lb

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5
Q

Max Cargo Weight (FWD)

A

3,307lb

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6
Q

Max Cargo Weight (AFT)

A

2,535lb

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7
Q

Aircraft Dimensions

A

Length — 103’ 11”
Width (Wingspan) — 93’ 11”
Height — 32’ 4”

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8
Q

Cabin Loading

A

Max PAX = 76

12 First / 64 Coach

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9
Q

Kinds of Operations (7)

A
  1. Day and Night
  2. VFR
  3. IFR
  4. Icing Conditions
  5. Cat I & II
  6. RVSM
  7. Extended Overwater Operation (when equipped)
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10
Q

Pressure Altitude / Temp where T/O-1 requried

A

At or above 8,000’ PA
Or
At or above ISA +35°C

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11
Q

Minimum flight crew

A

Pilot and First Officer

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12
Q

Maximum headwind for CAT II

A

25 kts

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13
Q

Max crosswind for landing vis < 4000 or 3/4

A

15 kts (E)

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14
Q

Max takeoff and landing tailwind component

A

10 kts

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15
Q

Max runway slope (uphill, downhill)

A

+ / - 2%

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16
Q

Flap manuevering load acceleration limits (up and down)

A

Up: -1.0 to +2.5 G

Down: 0.0 to +2.0 G

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17
Q

Max operating altitude

A

41,000’

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18
Q

Max takeoff & landing altitude

A

10,000’

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19
Q

Max SAT for takeoff, landing, and ground start

A

54°C

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20
Q

Max altitude with flaps extended

A

20,000’

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21
Q

Max flight operating latitude

A

78° North (E)

78° South (E)

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22
Q

Min SAT for takeoff, landing, and ground start

A

-40°C

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23
Q

Max crosswind for T/O—Dry runway

A

35 kts (E)

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24
Q

Max crosswind for T/O—Wet runway

A

30 kts (E)

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25
Q

Max crosswind for T/O—Runway w/ frost

A

31 kts

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26
Q

Max crosswind for T/O—Compacted snow RWYCC 4

A

20 kts

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27
Q

Max crosswind for T/O—standing water / slush / wet snow / dry snow

A

18 kts

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28
Q

Max crosswind for T/O—slippery when wet runway / RWYCC 3

A

15 kts

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29
Q

Max crosswind for T/O—ice

A

12 kts

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30
Q

Max crosswind for landing—RWYCC 6

A

38 kts

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31
Q

Max crosswind for landing—RWYCC 5

A

Braking Action: Good

31 kts

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32
Q

Max crosswind for landing—RWYCC 4

A

Braking action: Good to Medium

20 kts

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33
Q

Max crosswind for landing—RWYCC 3

A

Braking action: Medium

15 kts

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34
Q

Max crosswind for landing—RWYCC 2

A

Braking action: Medium to Poor

12 kts

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35
Q

Max crosswind for landing—RWYCC 1

A

Braking action: Poor

8 kts

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36
Q

Max crosswind for landing—RWYCC 0

A

Braking action: Nil

Operations Prohibited

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37
Q

Vmo (above 10,000’ MSL to FL280)

A

Max operating airspeed

320 KIAS

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38
Q

Mmo (above FL280)

A

Max operating mach number

.82

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39
Q

Max airspeed for RAT (Ram Air Turbine) operation

A

Vmo / Mmo

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40
Q

Turbulent airspeed (below 10,000’ MSL)

41
Q

Vmo (below 10,000’ MSL)

A

FAA — 250 KIAS

Structural limitation — 300 KIAS

42
Q

Va

43
Q

Turbulent airspeed (at or above 10,000’ MSL)

A

270 KIAS / .76M

whichever is lower

44
Q

Max airspeeed for windshield wiper operation

45
Q

Max airspeeed for windshield wiper operation in the non-parked position

46
Q

Max airspeed to open flight deck window

47
Q

Vlo (down)

A

Max gear extension speed

250 KIAS

48
Q

Vlo (up)

A

Max gear retraction speed

250 KIAS

49
Q

Vle

50
Q

Vfe 1

51
Q

Vfe 2

52
Q

Vfe 3

53
Q

Vfe 4

54
Q

Vfe 5

55
Q

Vfe Full

56
Q

Max altitude flaps / slats can be extended

A

20,000’ MSL

57
Q

Approved Fuels

A

ASTM – Jet A or A1 (Primary)

Brazilian – QAV1 (Secondary)
American – JP8 (Secondary)

58
Q

Max Cabin Differential Overpressure

59
Q

Max Cabin Differential Pressure (Above FL370)

60
Q

Max Cabin Differential for T/O & Landing

61
Q

Max Cabin Differential Negative Pressure

62
Q

Max Altitude Depressurized

A

10,000 or MEA (whichever is higher)

63
Q

Max altitude display difference in flight for RVSM

64
Q

What must occur prior to takeoff in the event that the airplane was landed below -40°C?

A

Maintenance inspection

65
Q

What APU do we have?

A

Sundstrand APS 2300

66
Q

First & Second APU Start Attempts

A

START/ON then 60 sec. OFF

67
Q

Third APU Start Attempt

A

START/ON then 5 min. OFF

68
Q

APU Minimum Operation Temperature

69
Q

APU Maximum Operation Temperature

A

ISA + 35°C

70
Q

APU EGT (Start)

71
Q

APU EGT (Continuous)

72
Q

APU Max Operation Altitude (Electrical)

A

33,000 ft.

73
Q

APU Max Start Altitude

A

30,000 ft.

74
Q

APU Max Operation Altitude (Eng. Start Assist)

A

21,000 ft.

75
Q

APU Max Operation Altitude (ECS Bleed)

A

15,000 ft.

76
Q

APU Max Rotor Speed

77
Q

When can autopilot be engaged on T/O or go around?

A

Above 400’ AFE

78
Q

When must autopilot be disconnected during landing?

A

Above 50’ AFE

79
Q

Engine Model

A

GE CF34-8E5

80
Q

N1 RPM Max

81
Q

N2 RPM Max

82
Q

Max Start ITT

83
Q

Max Normal T/O ITT

A

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

84
Q

Max T/O & G/A ITT

A

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

85
Q

Max Continuous ITT

86
Q

Min / Max Oil Pressure

A

25 psi / 95 psi

87
Q

Continuous Oil Temperature

88
Q

Transient Oil Temperature

A

163°C (15 min. limit)

89
Q

Engine Thrust

A 
T/O-1 = 13,000 lbs.  /  OEI ATTCS = 14,200 lbs.
T/O-2 = 11,800 lbs.  /  OEI ATTCS = 13,000 lbs.
90
Q

Maximum Fuel Capacity

A

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

91
Q

Maximum Useable Fuel Quantity

A

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

92
Q

Unusable Fuel Quantity

A

150 lbs. (75 lbs. per tank)

93
Q

Maximum Fuel Imbalance

94
Q

Fuel density

A

6.767 lbs. / US gallon

95
Q

Minimum Fuel Tank Temperature

96
Q

Crossfeed Operation

A

Crossfeed Knob must be OFF for T/O and Landing

97
Q

Dry Motoring Time Limits

A

1st – Max 90 sec. ON, followed by 5 min. OFF

2nd through 5th – Max 30 sec. ON, followed by 5 min. OFF

(After 5 attempts, may be repeated following 15 min. cooldown period)

98
Q

Starter Time Limits

A

1st and 2nd – Max 90 sec. (ground) / 120 sec. (flight) ON, following by 10 sec. OFF

3rd through 5th – Max 90 sec. (ground) / 120 sec. (flight) ON, followed by 5 min. OFF

Envoy E175 (5 decks)

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