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CPZ!!! :-) > Systems Study Guide > Flashcards

Systems Study Guide Flashcards

0
Q

Maximum Takeoff Weight (MTOW)

A

89,000/82,011

89/82

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1
Q

Maximum Ramp Weight (MRW) (175/170)

A

89,352lbs/82,363

89.5/82.5

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2
Q

Maximum Landing Weight (MLW)

A

75,177 / 72,311

75.2/72.3

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3
Q

Maximum Zero Fuel Weight (MZFW)

A

70,547 / 66,447

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4
Q

Cargo Weight Limits - E175

A

Forward Bin: 3,306

Aft Bin: 2,535

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5
Q

Cargo Weight Limits - E170

A

Forward Bin: 3,020

Aft Bin: 2,271

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12
Q

Max Runway Slope

A

+/- 2%

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13
Q

Runway Surface Type

A

Paved

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14
Q

Flaps Maneuvering Load Acceleration Limits, Flaps Up

A

-1.0G to +2.5G

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15
Q

Flaps Maneuvering Load Acceleration Limits, Flaps 1, 2, 3, 4, 5, Full

A

0G to +2.0G

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16
Q

Maximum Operating Altitude

A

41,000 feet

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17
Q

Maximum Takeoff and Landing Altitude

A

8,000 feet

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18
Q

Minimum Takeoff and Landing Altitude

A

-1,000 feet

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19
Q

Max Temperature for Takeoff and Landing

A

ISA +35

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20
Q

Min Temperature Approved for Takeoff

A

M40 C (SAT)

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21
Q

Max Flap Extension Altitude

A

20,000 feet

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22
Q

Hydraulic Warm Up Needed When…

A

<M18 hydraulic temp

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23
Q

Crosswind Limits - Dry

A

28kts sustained, 38kts gusts (28G38)

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24
Q

Crosswind Limits - Wet

A

28kts

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25
Q

Crosswind Limits - Static Takeoff

A

25kts

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26
Q

Crosswind Limits - Compact Snow

A

20kts

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27
Q

Crosswind Limits - Standing Water /Slush

A

18kts

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28
Q

Crosswind Limits - Wet Ice

A

12kts

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29
Q

Maximum Operating Speed - Vmo

A

320kts

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30
Q

Maximum Operating Mach Number - Mmo

A

.82M

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31
Q

Minimum RAT Speed

A

130kts

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32
Q

Maximum Turbulent Airspeed - Below 10,000 feet

A

250kts

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33
Q

Maximum Turbulent Airspeed - At or Above 10,000 feet

A

270kts / 0.76M

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34
Q

Maximum Tire Limit Ground Speed

A

195kts

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35
Q

Maximum Windshield Wiper Operation Speed

A

250KIAS

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36
Q

Maximum Gear Speed - Extension (Vloe), Extended (Vle) AND Retraction (Vlor)

A

250 KIAS

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37
Q

Flap Limitations - Flaps 1

A

230 KIAS

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38
Q

Flap Limitations - Flaps 2

A

215 KIAS

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39
Q

Flap Limitations - Flaps 3

A

200 KIAS

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40
Q

Flap Limitations - Flaps 4

A

180 KIAS

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41
Q

Flap Limitations - Flaps 5

A

180 KIAS

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42
Q

Flap Limitations - Flaps FULL

A

165 KIAS

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43
Q

Max Fuel Capacity (Total)

A

20,785 lbs. (3,071 gallons!)

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44
Q

Minimum Fuel Tank Temperature

A

M40C

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45
Q

Maximum Fuel Imbalance

A

794 lbs

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46
Q

Crossfeed Operations (Must be off when…)

A

During takeoff and landing

47
Q

Maximum Differential Pressure (up to 37,000 feet)

A

7.8 PSI

48
Q

Maximum Differential Pressure (above 37,000 feet)

A

8.3 PSI

49
Q

Maximum Differential Overpressure

A

8.7 PSI

50
Q

Maximum Differential Negative Pressure

A

-0.5 PSI

51
Q

Max Differential Pressure for Takeoff and Landing

A

0.2 PSI

52
Q

Maximum Altitude for Single Pack Operation

A

31,000 feet

53
Q

Thrust Reverser Limitations - engines must be idle by:

A

60 KIAS

54
Q

Thrust Reverser Limitations - Engines Must Be Out Of Reverse By:

A

30 KIAS

55
Q

Cockpit Crew Oxygen:

3 Crewmembers, 2 Crewmembers, No Dispatch

A

3=Green, 2=Cyan, No Dispatch= Amber

56
Q

Autopilot Limitations: Minimum Engagement Height

A

Acceleration Altitude

57
Q

Autopilot Limitations: Minimum En Route Height

A

500’ AGL

58
Q

Autopilot Limitations: Minimum Height to Engage on Go-Around

A

400’ AGL

59
Q

Autopilot Limitations: Minimum Height for a Precision Approach

A

70’ AGL

60
Q

Autopilot Limitations: Minimum Height for a Non-Precision Approach

A

MDA

61
Q

Autopilot Limitations: Special Instrument Approach

A

As specified in the procedure

62
Q

Crosswind Limits - Max Tail Wind

A

10kts

63
Q

CAT II - Max Headwind

A

25kts

64
Q

CAT II - Max Crosswind

A

12kts

65
Q

CAT II - Max Tailwind

A

10kts

66
Q

Max Taxi Speed - Straight Dry/Wet

A

30kts

67
Q

Max Taxi Speed - Straight Contaminated

A

15kts

68
Q

ITT Max Start Temp

A

815C

69
Q

For takeoff, ATTCS must be:

A

On

70
Q

Engine warm-up and cool down period:

A

2 minutes

71
Q

Powerback Operations are:

A

Prohibited!

72
Q

Engine Starter Duty Limits - Ground

A

1-2: 90 seconds on, 10 seconds off
3-5: 90 seconds on, 5 minutes off

*After five sequential motorings, the cycle may be repeated following a 15 minute cool down.

73
Q

Engine Starter Duty Limits - In Flight

A

1-2: 120 seconds on, 10 seconds off
3-5: 120 seconds on, 5 minutes off

*After five sequential motorings, the cycle may be repeated following a 15 minute cool down.

74
Q

Engine Starter Duty Limits - Dry Motoring

A

1: 90 seconds on, 5 minutes off
2-5: 30 seconds on, 5 minutes off

*After five sequential motorings, the cycle may be repeated following a 15 minute cool down.

75
Q

No Flex - Reduced Thrust Takeoff if:

A
  1. Standing water, slush, snow, or ice
  2. Anti-skid INOP
  3. TLR - No Flex Data
  4. Flex prohibited airport (10-7)
  5. PIC deems unsafe
76
Q

RVSM requirements

A

2 - ADS
1 - Autopilot with altitude hold
1 - Altitude alerter
1 - Transponder

77
Q

Air Temperature for Start

A

-54C to ISA +35C

78
Q

Minimum Battery Voltage to Start the APU

A

21V

79
Q

Minimum Battery Temperature for APU Start

A

-20C

80
Q

Max Altitude for APU:

  • Generator
  • Starting the APU
  • Assisted Engine Start
  • Bleed Air
A
  • Generator - 33,000’
  • Starting the APU - 30,000’
  • Assisted Engine Start - 21,000’
  • Bleed Air - 15,000’
81
Q

APU Starter Duty Cycle

A

1: 1 minute on, 1 minute off

2-3: 1 minute on, 5 minutes off

82
Q

Icing Conditions on Ground and for Takeoff -

MCDU TO DATASET MENU - set to ENG when:

A
  1. SAT is 5C to 10C and visible moisture will be encountered up to 1,700’ AFE or:
  2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engine nacelles, or engine sensor probes.
83
Q

Icing Conditions on Ground and for Takeoff -

MCDU TO DATASET MENU - set to ENG when:

A
  1. SAT is less than 5C and visible moisture will be encountered up to 1,700’ AFE or,
  2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engine nacelles, or engine sensor probes.
84
Q

Icing conditions exist in flight whenever static air temperature (SAT) on the ground (taxi or takeoff), or the Total AirTemperature (TAT) in flight is:

A

Equal to or less than 10C and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals)

85
Q

If either one or both ice detectors are failed,

A

The crew must set the mode selector to ON when icing conditions exist or are anticipated with a TAT of 10C or below with visible moisture.

86
Q

Random Limitations: when the airplane is stopped on the ground,

A

The taxi and landing lights must be OFF

87
Q

Random Limitations: for takeoff and in flight the taxi nose light must be:

A

Off.

88
Q

How long should you wait after the GPU switch is pushed in, or the APU power is available before shutting down the engine(s)?

A

10 seconds

89
Q

Minimum Flight Speed - All Altitudes, exceptions

A

Except as described in the normal/abnormal/emergency procedures, the airplane may never be operated below the “green dot” speed.

90
Q

Baro altimeter minimums

A

Must be used for all Cat I approaches

91
Q

VOR flight director mode:

A

Is prohibited/inhibited. VOR navigation using the FD must be predicated on HDG mode and VHF (green) needles or LNAV mode (magenta).

92
Q

Back course approaches are prohibited using:

A

IESS

93
Q

Before stopping the APU after engine start:

A
  1. Engine N2 must be stabilized for 5 seconds, OR

2. Power transfer is confirmed on the Electrical Synoptic Page

94
Q

Before starting the APU after an engine is shutdown:

A
  1. Wait for the engine to go below 30% N2
95
Q

Minimum distance for a 180 degree turn: (175/170)

A

175: 59’2”
170: 54’8”

96
Q

MEMORY ITEM: Smoke (fire, fumes, LAV smoke, and cargo smoke)

A
  1. Oxygen Mask - DON, 100% AS REQUIRED

2. Crew Communications - ESTABLISH

97
Q

MEMORY ITEM: LOSS OF CABIN PRESSURE (Cabin altitude high)

A
  1. Oxygen mask - DON, 100%

2. Crew Communication - ESTABLISH

98
Q

MEMORY ITEM: JAMMED CONTROL COLUMN (Pitch)

A
  1. Elevator Disconnect Handle (CONFIRM) - PRESS & PULL
99
Q

MEMORY ITEM: JAMMED CONTROL WHEEL (ROLL)

A
  1. Aileron Disconnect Handle (CONFIRM) - PRESS & PULL
100
Q

MEMORY ITEM: PITCH TRIM RUNAWAY

A
  1. Autopilot Disconnect Button - PRESS & HOLD

2. Pitch Trim Systems 1 & 2 Cut-out Buttons - PRESS IN

101
Q

MEMORY ITEM: ROLL (YAW) TRIM RUNAWAY

A
  1. Autopilot Disconnect Button - PRESS & HOLD
102
Q

MEMORY ITEM: STEERING RUNAWAY

A
  1. Steering Disconnect Switch - PRESS

2. Differential Braking and Rudder - USE TO STEER

103
Q

MEMORY ITEM: ENGINE START MALFUNCTION

A

Affected Engine:

1. START / STOP Selector - STOP

104
Q

How many networks make up the electrical system on the airplane? Why?

A

2 independent networks, to provide redundancy and fault isolation.

105
Q

What happens if a power generating source fails?

A

Bus ties automatically connect to provide no system degradation.

106
Q

What components power the AC system?

A 
2 integrated drive generators (IDG)
Auxiliary Power Unit (APU)
Inverter
Ram Air Turbine (RAT)
AC GPU receptacle
107
Q

What components power the DC system?

A

3 transformer rectifiers
2 NiCAD batteries
1 DC GPU

CPZ!!! :-) (4 decks)

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