Limitations Flashcards

1
Q

Maximum Cargo Compartment Loads

E175

A

Forward: 3307

Aft: 2535

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2
Q

Maximum Cargo Compartment Loads

E170

A

Forward: 3020

Aft: 2271

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3
Q

Max tailwind component:

A

10 knots

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4
Q

Max Runway Slope

A

+/-2%

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5
Q

Acceleration Load Limits

Flaps Up

A

-1.0G to +2.5G

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6
Q

Acceleration Load Limits

Flaps 1, 2, 3, 4, 5, and full

A

0.0G to +2.0G

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7
Q

Max Operating Altitude

A

FL410

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8
Q

Max Takeoff and Landing Altitude

A

8,000

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9
Q

Max Ambient Air Temperature for Takeoff and Landing

A

52°C

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10
Q

Max Flap Extension Altitude

A

FL200

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11
Q

Max Operating Latitude

A

78°N to 78°S

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12
Q

Min Ambient Temperature for Takeoff and Landing

A

-40°C

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13
Q

Maximum Landing Gear Extended Speed

A

250 KIAs

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14
Q

Maximum Gear Retraction Speed

A

250 KIAs

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15
Q

Maximum Gear Extended Speed

A

250 KIAs

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16
Q

VFE Flaps 1

A

230 KIAs

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17
Q

VFE Flaps 2

A

215 KIAs

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18
Q

VFE Flaps 3

A

200 KIAs

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19
Q

VFE Flaps 4

A

180 KIAs

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20
Q

VFE Flaps 5

A

180 KIAs

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21
Q

VFE Flaps Full

A

165 KIAs

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22
Q

Design Maneuvering Speed

A

240 KIAs

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23
Q

Definition of Icing Conditions?

A

10°C or below; and

-Visible moisture in any form is present;

or

When operating on contaminated surfaces.

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24
Q

Fuel Quantity per Tank

A

10,393 lbs

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25
Q

Unusable Fuel Quantity per Tank

A

75 lbs

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26
Q

Aircraft Maximum Fuel Capacity (Usable + unusable)

A

20,936 lbs

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27
Q

Maximum Windshield Wiper Operation Speed

A

250 KIAs

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28
Q

Fuel Imbalance

A

790 lbs

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29
Q

Crossfeed Limitations

A

XFEED Selector must be set to OFF during takeoff and landing.

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30
Q

Minimum Fuel Tank Temperature

A

-37°C

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31
Q

Brake Cooling Limitation

A

Do not take off with amber brake temperature indicators.

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32
Q

Landing Gear Retraction (Activation of landing gear downlock release button)

A

Prohibited for all takeoffs except when obstacle clearance is required.

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33
Q

What is prohibited regarding flaps use?

A

Holding in Icing conditions with flaps extended
Using Flaps 4 during approach and landing
Enroute use of flaps

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34
Q

Thrust Reverser Limitations

A

Ground use only
Do not attempt go around after thrust reverser deployment
Power back operations prohibited
Must be stowed below 60 knots
Once deployed, do not move thrust reversers into the forward thrust range until the REV is shown green on EICAS

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35
Q

When must thrust reversers be stowed?

A

Below 60 knots.

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36
Q

When are TAS, TAT and SAT valid?

A

Above 60 knots

37
Q

When are LOC back courses N/A?

A

Using IESS

38
Q

What equipment is required to operate in RVSM airspace?

A

2 RVSM Compliant Air Data systems
1 Autopilot ENGAGED with altitude holding mode operative
1 altitude alerter
1 Transponder

39
Q

What is the maximum allowable altitude difference between PFD 1 and PFD 2 for RVSM operations?

40
Q

What is the maximum altimeter difference allowed between altimeter indications on the ground?

41
Q

Minimum Autopilot Engagement Height

A

400 ft AGL

42
Q

Minimum Autopilot Use Height: ILS Approach

43
Q

Minimum Autopilot Use Height: Non-Precision Approach

44
Q

Minimum Autopilot Use Height: Visual Approach

A

400 ft AGL (C)

45
Q

Maximum Crosswind Component for Cat II Approach

46
Q

CAT II Required Equipment

A
  • 2 Intertial Reference Systems
  • 2 ADS
  • 2 PFDs
  • 1 EGPWS
  • SPOILER FAULT message not presented
  • 2 VOR/ILS Nav Systems
  • 1 VHF/COMM System
  • Autothrottles
  • Rudder in normal mode
  • 1 Radar Altimeter
  • 2 Flight Director Systems
  • 1 Autopilot with 1 operating channel
  • Windshield Wipers
  • 1 CAT II Engagement Logic
47
Q

What flaps setting is required for CAT II Approach?

48
Q

Minimum Use Height for CAT II approach

49
Q

Engine N1 Maximum

50
Q

Engine N2 Minimum

51
Q

Engine N2 Maximum

52
Q

ITT Start Maximum

53
Q

ITT Max Continuous

54
Q

Oil Pressure Operating Range

55
Q

Oil Temperature Continuous

56
Q

Oil Temperature Transient

A

163°C (Time limited to 15 minutes above 155°C.

57
Q

How long is the engine warm up/ cool down periods?

58
Q

When is reduced thrust takeoff not authorized?

A

Runway contaminated with standing water, slush, snow or ice
Windshear present or suspected
Performance mandates NO FLEX

59
Q

Engine Starter Duty Cycle Limits
Attempts 1-2
Ground and Inflight

A

Ground: 90 Seconds ON/ 10 seconds OFF

In flight: 120 Seconds ON/ 10 seconds OFF

60
Q

Engine Starter Duty Cycle Limits
Attempts 3-5
Ground and Inflight

A

Ground: 90 seconds ON/ 5 minutes OFF
Inflight: 120 seconds on/ 5 minutes OFF

61
Q

Engine Starter Dry Motoring Duty Cycle Limits
1st Attempt
Ground and Inflight

A

90 seconds ON/ 5 minutes OFF

62
Q

Engine Starter Dry Motoring Duty Cycle Limits
Attempts 2-5
Ground and Inflight

A

30 seconds ON/ 5 minutes OFF

63
Q

When is single engine taxi not authorized?

A

Braking Action Less than Good

RVR <1200

64
Q

APU Start Min Temperature

65
Q

APU Max Start Altitude

A

30,000 feet

66
Q

APU Max Operating Altitude

A

33,000 feet

67
Q

APU Bleed Max Altitude

A

15,000 feet

68
Q

APU Max Altitude Engine Start

A

21,000 feet

69
Q

APU Max Rotor Speed

70
Q

APU Continuous Max Temp

71
Q

APU Max Start Temp

72
Q

Max Differential Pressure

73
Q

Max Differential Overpressure

74
Q

Max altitude for single pack operation

75
Q

Max differential negative Pressure

76
Q

Maximum Differential Overpressure for Takeoff and Landing

77
Q

Maximum Recommended Crosswind

78
Q

Maximum Speed to Open the Direct Vision Window

79
Q

Maximum Tire Ground Speed

80
Q

Maximum Recommended Crosswind

RCC 6

81
Q

Maximum Recommended Crosswind

RCC 5 Good

82
Q

Maximum Recommended Crosswind

RCC 4 Good to Medium

83
Q

Maximum Recommended Crosswind

RCC 3 Medium

84
Q

Maximum Recommended Crosswind

RCC 2 Medium to Poor

85
Q

Maximum Recommended Crosswind

RCC 1 Poor

86
Q

Max Ramp Weight

A

E175: 85,870
E170: 82,364

87
Q

Maximum Takeoff Weight

A

E175: 85,517
E170: 82,011

88
Q

Max Landing Weight

A

E175: 74,957
E170: 72,310

89
Q

Max Zero Fuel Weight

A

E175: 69,886
E170: 65,256