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ENY-175 Study Guide > Limitations, Memory Items, and Extra > Flashcards

Limitations, Memory Items, and Extra Flashcards

1
Q

Maximum Ramp Weight

A

85,800 lbs

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2
Q

Maximum Takeoff Weight (MTOW)

A

85,500 lbs

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3
Q

Maximum Landing Weight (MLW)

A

74,900 lbs

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4
Q

Maximum Zero Fuel Weight (MZFW)

A

69,800 lbs

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5
Q

Maximum Forward Cargo Compartment Loading Weight

A

3,307 lbs

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6
Q

Maximum Aft Cargo Compartment Loading Weight

A

2,535 lbs

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7
Q

Aircraft Height

A

32’ 4” (33’)

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8
Q

Aircraft Width

A

93’ 11” (94’)

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9
Q

Aircraft Length

A

103’ 11” (104’)

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10
Q

Maximum Headwind for CAT II Approaches

A

25 knots

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11
Q

Maximum Crosswind for Landing (vis < 4000 or 3/4)

A

15 knots (E)

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12
Q

Maximum Takeoff and Landing Tailwind Component

A

10 knots

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13
Q

Maximum Operating Altitude

A

41,000

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14
Q

Maximum Altitude with Flaps Extended

A

20,000

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15
Q

Passenger Carrying Capacity

A

76 (12 First Class and 64 Coach)

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16
Q

Minimum Number of Crew

A

2 Pilots

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17
Q

Authorized Aircraft Operating Conditions

A

Day and Night
VFR and IFR
Icing Conditions
CAT I and CAT II
RVSM

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18
Q

Maximum Cabin Differential Overpressure

A

8.8 psi

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19
Q

Maximum Cabin Differential Pressure Above FL370

A

8.4 psi

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20
Q

Maximum Cabin Differential Pressure During Takeoff and Landing

A

0.2 psi

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21
Q

Maximum Negative Cabin Differential Pressure

A

-0.5 psi

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22
Q

Maximum Operating Altitude While Depressurized

A

10,000 or MEA, whichever is higher

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23
Q

Maximum Operating Altitude for Single Pack Operation

A

31,000

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24
Q

MMO Above FL280

A

0.82 M

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25
Q

VMO Between 10,000 and FL280

A

320 knots

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26
Q

VMO Below 10,000

A

300 (structural)
250 (FAA speed limit)

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27
Q

VA

A

240

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28
Q

VLE

A

250

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29
Q

VLO

A

250

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30
Q

VLR

A

250

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31
Q

VFE1

A

230

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32
Q

VFE2

A

215

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33
Q

VFE3

A

200

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34
Q

VFE4

A

180

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35
Q

VFE5

A

180

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36
Q

VFEFULL

A

165

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37
Q

Maximum Turbulent Airspeed Below 10,000

A

250

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38
Q

Maximum Turbulent Airspeed 10,000 and Above

A

270 or .76M, whichever is lower

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39
Q

Maximum Crosswind for Takeoff (DRY)

A

35 knots

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40
Q

Maximum Crosswind for Takeoff (WET)

A

30 knots

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41
Q

Maximum Tailwind

A

10 knots

42
Q

Maximum Direct View Window Operation

A

160

43
Q

Maximum Tire Speed

A

195

44
Q

Maximum Speed for Windshield Wiper Operation

A

250

45
Q

Aircraft Maximum Operating Altitude

A

41,000

46
Q

Maximum Takeoff and Landing Altitude

A

10,000

47
Q

Minimum Takeoff and Landing Altitude

A

-1,000

48
Q

Min/Max Takeoff and Landing Temperature (SAT)

A

-40°C | 54°C

note: In the event of a landing below -40°C, takeoff not authorized without further maintenance inspection

49
Q

Maximum Altitude Display Difference in Flight for RVSM

A

180 ft

50
Q

APU Make and Model

A

Sundstrand APS 2300

51
Q

APU Starting Time Limits

A

1st and 2nd Attempt: 60 secs off

3rd Attempt: 5 mins off

52
Q

APU Minimum Starting Temperature

A

-54°C

53
Q

APU Maximum Operating Temperature

A

ISA + 39°C

note: Supplemental restrictions applicable > ISA + 35°C

54
Q

APU Maximum EGT (Start)

A

1032°C

55
Q

APU Maximum EGT (Continuous)

A

717°C

note: No time limit for amber indications on ground or inflight between 662°C - 717°C

56
Q

APU Maximum Operating Altitude

A

33,000

57
Q

APU Maximum Altitude for Electrical Demand

A

33,000

58
Q

APU Maximum Starting Altitude

A

30,000

59
Q

APU Maximum Altitude for Engine Start Bleed

A

21,000

60
Q

APU Maximum Altitude for ECS (Pack) Bleed Demand

A

15,000

61
Q

Minimum Battery Temperature for APU Start

A

-20°C (Battery #2)

note: This does not prevent starting the APU via DC power if a DC GPU is available and utilized

62
Q

Minimum Autopilot Engagement Altitude on Takeoff and Go Around

A

Above 400’

63
Q

Minimum Altitude for Autopilot Disconnect During Landing

A

50’

64
Q

Engine Make and Model

A

GE CF34-8E5

65
Q

N1 Maximum RPM

A

99.5%

66
Q

N2 Maximum RPM

A

99.4%

67
Q

Engine Maximum Takeoff and Go Around ITT (Dual Engine)

A

965°C (2 mins)
949°C (3 mins)

note: Total of 5 mins

68
Q

Engine Maximum Takeoff and Go Around ITT (Single Engine)

A

1006°C (2 min)
990°C (3 min)

note: Total of 5 mins

69
Q

Engine Maximum Continuous ITT

A

960°C

70
Q

Min/Max Engine Oil Pressure

A

25 psi | 95 psi

71
Q

Engine Continuous Oil Temperature

A

155°C

72
Q

Engine Transient Oil Temperature

A

163°C

note: 15 min time limit

73
Q

Engine Thrust T/O-1

A

13,000 lbs
ATTCS = 14,200 lbs

74
Q

Engine Thrust T/O-2

A

11,800 lbs
ATTCS = 13,000 lbs

75
Q

Maximum Fuel Capacity

A

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

76
Q

Maximum Usable Fuel Capacity

A

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

77
Q

Unusable Fuel Amount

A

75 lbs per tank (150 total)

78
Q

Maximum Fuel Tank Imbalance

A

794 lbs

79
Q

Fuel Pounds to Gallon Conversion Ratio

A

6.767 lbs / US Gallon

80
Q

Minimum Fuel Tank Temperature

A

-37°C

81
Q

Engine Starting Time Limits

A

1st and 2nd Attempt:
GND: 90 sec START / 10 sec Cool-down
FLT: 120 sec START / 10 sec Cool-down

3rd - 5th Attempt:
GND: 90 sec START / 5 min Cool-down
FLT: 120 sec START / 5 min Cool-down

82
Q

Engine Dry Motoring Time Limits

A

1st Attempt: 90 sec maximum / 5 min Cool-down

2nd - 5th Attempt: 30 sec maximum / 5 min Cool-down

note: After 5 sequential dry motoring attempts, the sequence may be repeated following a 15 min cool-down period

83
Q

Cabin Altitude HI / Rapid Depressurization

A
  1. Oxygen Masks …… CR ….. ON, 100%
84
Q

Jammed Control Column - Pitch

A

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

85
Q

Jammed Control Wheel - Roll

A

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

86
Q

Pitch Trim Runaway

A
  1. AP/TRIM Disconnect ………………………………… PRESS and HOLD
  2. TRIM PITCH SYS 1 & 2 CUTOUT ………………… Push IN
87
Q

(Roll or Yaw) Trim Runaway

A

AP/TRIM Disconnect …………………………………….. PRESS and HOLD

88
Q

Nosewheel Steering Runaway

A

STEER DISC ……………. PRESS and HOLD

89
Q

Aborted Engine Start

A
  1. Associated Thrust Lever …………………………. IDLE
  2. Associated START/STOP …………………………. STOP
90
Q

Minimum Airspeed for Maximum Reverse Thrust

A

60 KIAS

note: Below 60 KIAS reduce reverse thrust to idle

91
Q

Definition of Icing Conditions

A

10°C or below (OAT on ground or TAT in flight) AND at least one of:

  1. Visible moisture in any form including clouds or fog (one mile or less visibility).
  2. When operating on ramps, taxiways, or runways with snow, ice, or standing water contamination.
92
Q

Before Start, REF A/I on the MCDU must be set to:

A

“ENG” when the OAT is between 5°C and 10°C or “ALL” when OAT is below 5°C

and icing conditions exist or are anticipated prior to reaching 1,700 ft above field elevation

93
Q

All landings on runways with an RCC less than 5/5/5 must be at what flap setting?

A

Flaps FULL

note: Unless otherwise required by operational restrictions such as CAT II, MEL status, or Emergency/Abnormal procedures

94
Q

The green towing light illuminates when:

A

Steering is disengaged.
Parking brake is not on.
Main brakes are not applied.

95
Q

A rejected takeoff should only be initiated between 80 knots and V1 for the following:

A
  1. Fire or fire warning
  2. Engine failure
  3. Stagnant airspeed or sudden negative wind change
  4. If the airplane is unsafe or unable to fly
96
Q

The T/O Config button checks what items?

A

Flaps (not in takeoff position or disagrees with FMS takeoff page 2/2)

Parking Brake (brakes are on)

Pitch Trim (outside of green range)

Spoilers (any panel is deployed)

97
Q

What happens when an Engine Fire Handle is pulled?

A
  1. Fuel shutoff valve closes
  2. Hydraulic shutoff valve closes
  3. Engine bleed air valve closes
98
Q

Items in the accessory gearbox

A

Integrated Drive Generator (IDG)
Hydraulic Pump
Permanent Magnet Alternator (PMA)
Air Turbine Starter (ATS)

note: Radial drive shaft connects to the N2 rotor

99
Q

Maximum Crosswind for Landing

A

38 knots

100
Q

Engine Start Maximum ITT

A

815°C

ENY-175 Study Guide (1 decks)

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