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Envoy > E175 Limitations/Memory Items > Flashcards

E175 Limitations/Memory Items Flashcards

1
Q

Aircraft length

A

103’ 11” (104’)

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2
Q

Aircraft width

A

93’ 11” (94’) (Wingspan)

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3
Q

Aircraft height

A

32’ 4” (33’)

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4
Q

Max PAX

A

76 (12 First/64 Coach)

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5
Q

Max cargo weights

A

FWD 3307 lbs
AFT 2535 lbs

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6
Q

Maximum ramp weight

A

85,800 lbs

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7
Q

Maximum takeoff weight (structural)

A

85,500 lbs

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8
Q

Maximum landing weight (structural)

A

74,900 lbs

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9
Q

Maximum zero fuel weight

A

69,800 lbs

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10
Q

Minimum crew

A

2 pilots (left/right seat)

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11
Q

Aircraft operations

A

Day/night
VFR/IFR
Icing conditions
CAT I/CAT II
RVSM
Extended Overwater Operation (when EOW equipped)

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12
Q

Max cabin differential overpressure (safety valve)

A

8.8 PSI

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13
Q

Max cabin differential pressure above FL 370

A

8.4 PSI

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14
Q

Max cabin differential pressure for T/O and landing

A

0.2 PSI

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15
Q

Max cabin Negative differential pressure

A

-0.5 PSI

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16
Q

Max altitude depressurized

A

10,000’ or MEA whichever is higher

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17
Q

Max altitude for single pack operation

A

31,000’

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18
Q

Mmo (above FL280)

A

.82M

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19
Q

Vmo (above 10,000’ to FL280)

A

320 KIAS

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20
Q

Vmo (below 10,000’) (FAA and structural)

A

250 KIAS FAA regulatory
300 KIAS Structural

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21
Q

Va

A

240 KIAS

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22
Q

Vle

A

250 KIAS

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23
Q

Vlo

A

250 KIAS

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24
Q

Vlr

A

250 KIAS

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25
Q

Vfe1

A

230 KIAS

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26
Q

Vfe2

A

215 KIAS

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27
Q

Vfe3

A

200 KIAS

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28
Q

Vfe4

A

180 KIAS

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29
Q

Vfe5

A

180 KIAS

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30
Q

Vfefull

A

165 KIAS

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31
Q

Max turbulent airspeed (below 10,000’)

A

250 KIAS

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32
Q

Max turbulent airspeed (10,000’ and above)

A

270 KIAS or .76M

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33
Q

Max crosswind for takeoff (dry and wet)

A

Dry 35 kts
Wet 30 kts

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34
Q

Max crosswind for takeoff (RWYCC 4)

A

20 kts

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35
Q

Max crosswind for takeoff (RWYCC 3)

A

15 kts

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36
Q

Max crosswind for landing (RWYCC 6)

A

38 kts

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37
Q

Max crosswind for landing (RWYCC 5)

A

31 kts

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38
Q

Max crosswind for landing (RWYCC 4)

A

20 kts

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39
Q

Max crosswind for landing (RWYCC 3)

A

15 kts

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40
Q

Max crosswind for landing (RWYCC 2)

A

12 kts

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41
Q

Max crosswind for landing (RWYCC 1)

A

8 kts

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42
Q

Max crosswind for landing (RWYCC 0)

A

OPERATIONS PROHIBITED

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43
Q

Unless otherwise required by operational restrictions such as CAT II, MEL, or emergency/abnormal procedures, all landings on runways with an RCC less than 5/5/5 must be at what flap setting?

A

Flaps FULL

44
Q

Max tailwind

A

10 kts

45
Q

Max headwind for CAT II

A

25 kts

46
Q

Max crosswind for landing (RVR less than 4000 or 3/4 mile)

A

15 kts

47
Q

Max DV window operation speed

A

160 KIAS

48
Q

Max tire speed

A

195 KIAS

49
Q

Max windshield wiper speed

A

250 KIAS

50
Q

Max operating altitude

A

41,000’

51
Q

Max altitude with flaps extended

A

20,000’

52
Q

Max altitude for takeoff and landing

A

10,000’

53
Q

Minimum altitude for takeoff and landing

A
  • 1,000’
54
Q

Min SAT for takeoff or landing

A
  • 40 deg C
55
Q

Max SAT for takeoff or landing

A

54 deg C

56
Q

Max altitude display difference in flight for RVSM

A

180’

57
Q

In the event of a landing below ____ , takeoff not authorized without further maintenance inspection

A
  • 40 deg C
58
Q

APU model

A

Sundstrand APS 2300

59
Q

APU starter limitations
First and second attempts
Third attempt

A

START/ON then 60 sec OFF
START/ON then 5 min OFF

60
Q

Minimum starting temperature for APU

A
  • 54 deg C
61
Q

Max APU operation temperature

A

ISA + 39 deg C (supplemental info applicable at ISA + 35 deg C)

62
Q

Max EGT APU start

A

1032 deg C

63
Q

Max EGT APU continuous
is there a time limit ground/inflight between 662-717 deg C (amber range)

A

717 deg C
No time limit between 662-717 deg C (amber range)

64
Q

Max APU rotor speed

A

108%

65
Q

Max altitude for APU electrical power

A

33,000’

66
Q

Max altitude for APU start

A

30,000’

67
Q

Max altitude for ENG start assist with APU

A

21,000’

68
Q

Max altitude for APU bleed air

A

15,000’

69
Q

Minimum altitude for autopilot engagement (takeoff/go around)

A

Above 400’

70
Q

Minimum altitude with autopilot engaged during landing

A

above 50’

71
Q

Engine model

A

GE CF34-8E5

72
Q

Max N1 RPM

A

99.5%

73
Q

Max N2 RPM

A

99.4%

74
Q

Max start ITT

A

815 deg C

75
Q

Max normal T/O ITT

A

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

76
Q

Max T/O & G/A ITT

A

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

77
Q

Max continuous ITT

A

960 deg C

78
Q

Min oil pressure

A

25 PSI

79
Q

Max oil pressure

A

95 PSI

80
Q

Max continuous oil temp

A

155 deg C

81
Q

Max transient Oil temp

A

163 deg C (15 min limit)

82
Q

T/O-1 engine thrust

A

13,000 lbs
ATTCS 14,200 lbs

83
Q

T/O-2 engine thrust

A

11,800 lbs
ATTCS 13,000 lbs

84
Q

Fuel types

A

Jet A or A1
JP8
QAV1 (Brazilian)

85
Q

Max fuel capacity

A

20,934 lbs (10,467 lbs/tank)

86
Q

Max useable fuel

A

20,784 lbs (10,392 lbs/tank)

87
Q

Unusable fuel

A

150 lbs (75 lbs/tank)

88
Q

Max fuel imbalance

A

794 lbs

89
Q

Minimum fuel temperature

A

-37 deg C

90
Q

Can you crossfeed fuel during takeoff or landing?

A

NO

91
Q

1st and 2nd engine start limits

A

on ground-90 sec START/10 sec cool-down
in flight-120 sec START/10 sec cool-down

92
Q

3rd-5th attempts engine start limits

A

on ground- 90 sec START/5 min cool-down
in flight-120 sec START/5 min cool-down

93
Q

Dry motoring limits

A

1st dry motor-Max 90 sec followed by 5 min cool-down
2nd-5th dry motor-Max 30 sec followed by 5 min cool-down

94
Q

After __ sequential dry motoring cycles, the sequence may be repeated following a __ min cool-down period.

A

5, 15 min

95
Q

CABIN ALTITUDE HI/RAPID Depressurzation

A

Oxygen masks…..CR…..ON, 100%

96
Q

Jammed Control Column - Pitch

A

Elevator Disconnect…..CR…..PRESS and PULL

97
Q

Jammed Control Wheel - Roll

A

Aileron Disconnect…..CR…..PRESS and PULL

98
Q

Pitch Trim Runaway

A

AP/TRIM Disconnect…..PRESS and HOLD
TRIM PITCH SYS 1 & 2 CUTOUT…..Push IN

99
Q

(Roll or Yaw) Trim Runaway

A

AP/TRIM Disconnect…..PRESS and HOLD

100
Q

Nosewheel Steering Runaway

A

Steering Disconnect…..PRESS

101
Q

Aborted Engine Start

A

Associated Thrust Lever…..IDLE
Associated START/STOP…..STOP

102
Q

Application of reverse thrust is not permitted at airspeeds below __ KIAS during normal operations.

A

60 KIAS

103
Q

Can you single engine taxi with an inoperative APU?

A

NO

104
Q

Dry Ice limit

A

50 lbs in forward compartment only
CAUTION-Not all E170s have forward cargo ventilation fans
dry ice/live animals are prohibited in these aircraft

105
Q

For operations at or above _____’ pressure altitude OR ISA ___ degrees and above, T/O-1 thrust is required.

A

8,000’
ISA +35

Envoy (2 decks)

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