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Envoy E175 > Limitations Memory > Flashcards

Limitations Memory Flashcards

1
Q

Maximum headwind for Cat II approaches

A

25 knots

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2
Q

Maximum crosswind for landing vis less than 4000 RVR or 3/4

A

15 knots

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3
Q

Maximum takeoff and landing tailwind component

A

10 knots

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4
Q

Maximum crosswind for takeoff on dry runway

A

35 knots

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5
Q

Maximum crosswind for takeoff Wet runway

A

30 knots

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6
Q

Maximum operating altitude

A

41,000 feet

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7
Q

Maximum altitude with flaps extended

A

20,000 feet

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8
Q

Maximum operating airspeed (Vmo)

A

320

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9
Q

Maximum operating Mach number (Mmo)

A

.82

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10
Q

Turbulent airspeed (below 10,000 feet)

A

250 knots

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11
Q

Turbulent airspeed (at or above 10,000 feet)

A

270 KIAS/.76

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12
Q

Maximum airspeed for windshield wiper operation

A

250 Knots

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13
Q

Eng. Starter duty cycles

1st and 2nd

A

Maximum 90 seconds on (ground)120 seconds on (in flight)

Followed by 10 seconds off

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14
Q

Eng. Starter Duty Cycle
3rd though 5th

A

Maximum 90 seconds on (ground)120 seconds on (in flight)

Followed by 5 minutes off

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15
Q

Eng. Dry-Motoring Cycle
1st start 90 seconds on
2nd though 5th start 30 seconds on

A

Followed by 5 minutes off

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16
Q

Reverse Thrust is used….

A

For ground use only

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17
Q

Landing with reverse thrust..

A

Maximum reverse thrust is not permitted at air speeds below 60 knots.
Below 60 Knots set reverse thrust to idle.

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18
Q

Apu starter limits
1st and 2nd attempt

A

60 seconds off

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19
Q

Apu Starter Limits
3rd attempt

A

5 minutes off

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20
Q

Apu maximum altitude for APU start

A

30,000 feet

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21
Q

Apu maximum altitude for electrical use

A

33,000 feet

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22
Q

Apu maximum altitude for bleed use

A

15,000 feet

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23
Q

Apu maximum altitude for assist engine start

A

21,000 feet

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24
Q

Aircraft Dimensions

A
  • Length – 103’ 11” (104’)
  • *Width – 93’ 11 ” (94’)
  • Height – 32’ 4” (33’)
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25
Q

Cabin Loading

A

• Max PAX - 76

12 First / 64 Coach

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26
Q

Minimum Crew

A

• Left Seat Pilot and Right Seat Pilot (i.e. Captain and First Officer)

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27
Q

Aircraft Operations

A 
• Day & Night
• VFR & IFR
• Icing Conditions
• CAT I & CAT II
• RVSM
Extended over water operations if equipped
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28
Q

Max Cabin Differential Over-pressure

A

8.8 psi

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29
Q

Max Cabin Differential Pressure (Above FL370)

A

8.4 psi

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30
Q

Max Cabin Differential Negative Pressure

A

-0.5 psi

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31
Q

Max Cabin Differential for Takeoff/Landing

A

0.2 psi

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32
Q

Max Altitude Depressurized

A

10,000’ or MEA whichever is Higher

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33
Q

Vmo (Below 10,000’)

A

250

*FAA Regulatory Speed / Structural Speed Limit is 300 KIAS

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34
Q

Va

A

240

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35
Q

Vle

36
Q

Vlo

37
Q

Vlr

38
Q

Vfe1

39
Q

Vfe2

40
Q

Vfe3

41
Q

Vfe4

42
Q

Vfe5

43
Q

VfeFull

44
Q

Max Crosswinds for Landing

A

Braking action/Max crosswind
6/38 5/31 4/20 3/15
2/12 1/8

45
Q

Max DV Window Operation

46
Q

Max Tire Speed

47
Q

Max Windshield Wiper Speed

48
Q

MAX Takeoff/Landing Altitude

49
Q

MIN Takeoff/Landing Altitude

50
Q

Min Takeoff /Landing Temperature (SAT)

A

-40°C

Note: In the event of a landing below -40°C, the Airplane may not takeoff without further maintenance inspection.

51
Q

APU Brand

A

Sundstrand APS 2300

52
Q

APU Minimum Operation Temperature

53
Q

APU Maximum Operation Temperature

A

ISA + 35°C

54
Q

APU EGT (Start)

55
Q

APU EGT (Continuous)

A

717°C

Note: No time limit in amber on the ground/in-flight from 662°C to 717°C

56
Q

APU Max Rotor Speed

57
Q

Autopilot Minimum Engagement Altitude on Takeoff or Go Around

58
Q

Autopilot Minimum Engaged Altitude during Landing

A

Above 50 Feet

59
Q

Engine Type

A

GE CF34-8E5

60
Q

N1 Max

61
Q

N2 Max

62
Q

Max Start ITT

63
Q

Max Normal T/O ITT

A

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

64
Q

Max T/O & G/A ITT

A

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

65
Q

Max Continuous ITT

66
Q

Min/Max Oil Pressure

A

25 psi / 95 psi

67
Q

Continuous Oil Temperature

68
Q

Transient Oil Temperature

A

163°C (15 min. limit)

69
Q

Engine Thrust T/O-1

A

13,000 lbs. / OEI ATTCS = 14,200 lbs

70
Q

Engine Thrust T/O-2

A

11,800 lbs. / OEI ATTCS = 13,000 lbs

71
Q

Fuel Types Allowed

A
  • Brazilian – QAV1
  • ASTM – Jet A or A1
  • American – JP8
72
Q

Maximum Fuel Capacity

A

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

73
Q

Maximum Useable Quantity

A

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

74
Q

Unusable Quantity

A

150 lbs. (75 lbs. per tank)

75
Q

Maximum Fuel Imbalance

76
Q

Minimum Fuel Tank Temperature

77
Q

Crossfeed Operation

A

Crossfeed Knob must be OFF for Takeoff and Landing

78
Q

Max difference allowed between FO and CA altimeter in RSVM is:

79
Q

Aircraft Dimensions

A

Length – 103’ 11” (104’)
• Width – 93’ 11” (94’) (Wingspan)
• Height – 32’ 4” (33’)

80
Q

Cargo Compartment Max Weight Limits

A
  • FWD – 3,306 lbs.
  • AFT – 2,535 lbs
81
Q

Max Ramp Weight

82
Q

Max Takeoff Weight

83
Q

Zero Fuel Weight

84
Q

Max Landing Weight

85
Q

Max Takeoff/Landing Tempature SAT

Envoy E175 (3 decks)

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