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AmericanAirlines Embraer 190 > Limitations > Flashcards

Limitations Flashcards

1
Q

Engine Dry-Motoring Cycle

1st

A

The dry-motoring cycle (with thrust lever at IDLE) may be used for engine ground starts and engine airstarts.

Maximum 90 seconds ON, followed by 5 minutes OFF

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2
Q

*Engine Starter Duty Cycle

3rd through 5th*

A

Maximum 90 seconds ON (ground), 120 seconds ON (in flight)

Followed by…

5 minutes OFF

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3
Q

APU Operational Limits

EGT - Continuous

A

717°C

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4
Q

RVSM Altimeter Tolerance

Standby Altimeter in RVSM

A

Does not meet altimeter accuracy requirements of RVSM.

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5
Q

Maximum Runway Slope for Autolands (up hill, down hill)

A

+1%, -1%

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6
Q

When operating the ICE PROTECTION in manual mode:

A

CAUTION

Do not rely on visual airframe icing cues to select engine anti-ice ON.
Use temperature and visual moisture criteria specified in this section.
Delaying the use of engine anti-ice until ice buildup is visible from the flightdeck may result in severe engine damage and/or flameout.

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7
Q

N1 Max RPM

A

100%

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8
Q

Autopilot Use During Landing

A

Unless executing an autolanding with AUTOLAND 1 engaged, turn off autopilot PRIOR to 50 feet AGL.

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9
Q

APU Operational Limits

Rotor Speed

A

108%

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10
Q

Engine and Wing Anti-Ice Operations

A

During taxi out and takeoff, the MCDU TO DATASET MENU REF A/I must be set to ALL when OAT is 10°c or below and icing conditions exist or are anticipated.

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11
Q

Engine Maximum Continuous Max ITT

A

960°C

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12
Q

APU Operational Limits

Altitude for Start

A

30,000 feet

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13
Q

Turbulent Airspeed (below 10,000 feet)

A

250 KIAS

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14
Q

Maximum Relief Differential Pressure

Above 37,000 feet

A

8.3 psi

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15
Q

Definition of Icing Conditions

A
  • OAT (on the ground and for takeoff) or TAT (inflight) is 10°C or below, and
  • Visibile moisture in any form is present such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals, or
  • When operating on ramps, taxiways, or runways where surface snow, ice, standing water or slush may be ingested by engines and freeze on engines, nacelles, or engine sensor probes.
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16
Q

Autoland Weight Limitations

Maximum

A

97,000 lbs

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17
Q

Maximum Gear Extension Speed (Vlo)

A

265 KIAS

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18
Q

Maximum Weights

Taxi & Ramp

A

114,500 lbs

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19
Q

Engine Caution Range

A

Amber

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20
Q

FMS Bank Angles for Single Engine Operations

A

There is no automatic bank angle protection for an engine out situation.

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21
Q

Maximum Gear Retraction Speed (Vlor)

A

235 KIAS

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22
Q

Turbulent Airspeed (at or above 10,000 feet)

A

270 KIAS/.76M

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23
Q

Maximum Weights

Zero Fuel (MZFW)

A

90,150 lbs

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24
Q

Engine Normal Operating Range

A

Green

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25
Q

Maximum Flap Operating Speeds Vfe(KIAS)

Flaps 2

A

215

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26
Q

Maximum Airspeed for Windshield Wiper Operation Failed in the Non-Parked Position

A

320 KIAS

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27
Q

FMS Speed

A

Not authorized for takeoff.

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28
Q

Engine Normal Takeoff & Go Around Max ITT

A

947°C

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29
Q

Tire Limit Ground Speed

A

195 kts

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30
Q

APU Operational Limits

Altitude for Operation: ELECTRICAL

A

33,000 feet

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31
Q

Approved Fuel

Primary

A

Jet A and A-1

Mixing of fuels is permitted.

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32
Q

Engine Maximum Takeoff & Go Around Max ITT*

*Automatically engaged mode in one engine inoperative or wind shear conditions with the thrust lever in the TOGA position.

A

983 °C

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33
Q

Maximum operating limit speeds (Vmo/Mmo) shall…

A

not be deliberately exceeded in any regime of flight.

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34
Q

Engine and Wing Anti-Ice Temperature Limits

A

There is no temperature limitation for anti-ice system automatic operation.

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35
Q

Fuel Density

A

6.77 lbs/gal

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36
Q

APU Starter Limit

3rd Start cycle

A

5 minutes OFF

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37
Q

APU Starter Limit

1st and 2nd Start cycle

A

60 seconds OFF

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38
Q

Reverse Thrust Use

A

Reverse thrust is for GROUND USE only.

Thrust reverser are intended for use during full stop landings.

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39
Q

Crossfeed Operation

A

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

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40
Q

Maximum Airspeed for Windshield Wiper Operation

A

250 KIAS

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41
Q

Flaps Maneuvering Load Acceleration Limits

Flaps UP

A

-1.0 to 2.5 G

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42
Q

TAS, TAT and SAT

A

Information are only valid above 60 KIAS.

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43
Q

*Engine Starter Duty Cycle

1st and 2nd*

A

Maximum 90 seconds ON (ground), 120 seconds ON (in flight)

Followed by…

10 seconds OFF

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44
Q

“When using Jet A type of fuel with ambient temperatures of _______ , the fuel temperature prior to flight must be verified to be ________ “

A

-30°C (-22°F) is below

At or above -29°C (-21°F)

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45
Q

Maximum Headwind for CAT II/III Approaches

A

25 kts

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46
Q

Maximum Relief Differential Pressure

Up to 37,000 feet

A

7.8 psi

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47
Q

Brakes Cooling Limitation

A

Do NOT takeoff with amber brake temperature indicators.

48
Q

Maximum Crosswind for Landing Vis <4000 or 3/4

A

15 kts (A)

49
Q

Flaps Maneuvering Load Acceleration Limits

Flaps Down (1,2,3,4,5 and Full)

A

0.0 to 2.0 G

50
Q

Maximum Wind for Takeoff and Landing (including gusts)

A

50 kts (A)

51
Q

Minimum Fuel Temperature

52
Q

Maximum Airspeed to Open Flightdeck Window

53
Q

Maximum Takeoff and Landing Altitude

A

8,000 feet

54
Q

Evacuation Slides

A

Whenever occupants are in the cabin, the escape slides must be armed during taxi, takeoff, and landing.

55
Q

Electrical Circuit Breaker Reset

A

There is no operational situation in which it would be necessary to reset a tripped fuel boost pump or fuel indicating system circuit breaker.

WARNING

Resetting a tripped fuel boost pump or fuel indicating system circuit breaker is prohibited.

56
Q

Unusable Fuel

A

101.5 lbs per tank

57
Q

Maximum Runway Slope (up hill, down hill)

A

+2.0%, -2.0%

58
Q

Minimum Operating Limit Speed

A

Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for non-routine flight or training operations.

59
Q

APU Operational Limits

Temperature (min and max)

A

Min: -54°C

Max: ISA + 35°C

60
Q

Maximum Operating Altitude

A

41,000 feet

61
Q

Minimum SAT for Takeoff, Landing and Ground Start

62
Q

Maximum Flap Operating Speeds Vfe(KIAS)

Flaps 5

63
Q

Engine Type

64
Q

Maximum Flight Operating Latitude

A

72° North (A)

59° South (A)

65
Q

“During takeoff or go around, do NOT turn the autopilot on until …”

A

Above 400 feet AGL

66
Q

Maximum Operating Mach Number

67
Q

Reverse Thrust Go Around WARNING

A

Do NOT attempt a go around maneuver after deployment of the thrust reversers.

68
Q

Engine Dry-Motoring Cycle

2nd through 5th

A

The dry-motoring cycle (with thrust lever at IDLE) may be used for engine ground starts and engine airstarts.

Maximum 30 seconds ON, followed by 5 minutes OFF

69
Q

Maximum Flap Operating Speeds Vfe(KIAS)

Flaps 1

70
Q

RVSM Altimeter Tolerance

Maximum Allowable In-Flight Difference Between Captain and First Officer Displays for RVSM Operation

71
Q

Terrain/Obstacle Awareness Alerting functions …

A

Should be manually inhibited within 15nm on approach to an airport that is not in the EGPWS airport database to avoid unwanted alerts.

72
Q

Flight Load Acceleration Limitation WARNING

A

Rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large side slip angles) may result in structural failures at any speed.

73
Q

Reverse Thrust During Landing

*Application of __________, is not permitted at airspeeds _________.

Below _____ _______ reverse thrust to _____.”

A

Maximum reverse thrust; below 60 KIAS

60 KIAS; reduce; IDLE

74
Q

Maximum Altitude for Single Pack Operation

A

31,000 feet

75
Q

APU Operational Limits

Altitude for Operation: BLEED

A

15,000 feet

76
Q

Pressurization Door Opening WARNING

A

Prior to opening any of the aircraft doors, the aircraft must be completely depressurized.

77
Q

Autoland Weight Limitations

Minimum

A

69,500 lbs

78
Q

Maximum Flap Operating Speeds Vfe(KIAS)

Flaps 3

79
Q

RVSM Altimeter Tolerance

Primary Altimeter Readings

A

On the ground, must be within 75 feet of each other and within 75 feet of field elevation.

80
Q

Maximum Altitude With Flaps Extended

A

20,000 feet

81
Q

APU Operational Limits

Altitude for Operation: To Assist ENGINE START

A

21,000 feet

82
Q

Maximum SAT for Takeoff, Landing and Ground Start

83
Q

Maximum Weights

Landing (MLW)

A

97,000 lbs

84
Q

Maximum Crosswind (including gusts) for Autoland

A

15 kts (A)

85
Q

Maximum Useable Fuel

A

14,400 lbs, per tank

86
Q

Maximum Fuel Imbalance

A

Between left and right main tanks during all phases is 800 lbs.

87
Q

Oil Temperature Max

88
Q

Maximum Flap Operating Speeds Vfe(KIAS)

Flaps Full

89
Q

Reverse Thrust WARNING

A

After applying thrust reverser, do not move the throttle back to the forward thrust range, unless the REV icon on the EICAS is shown in amber or green.

90
Q

Maximum Airspeed for RAT Operation

91
Q

Enroute Use of Flaps/Slats …

A

Is prohibited.

92
Q

Maximum Takeoff and Landing Tailwind Component

93
Q

Engine Dry Motoring Cycle After 5th Start

A

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

94
Q

Design Maneuvering Speed

A

Full application of rudder and aileron controls, as well as maneuvers that involve angle of attack near the stall, must be confined to speeds below

240 KIAS

95
Q

“In the event of a landing below ____ , the aircraft may not takeoff without further maintenance inspection.”

96
Q

Minimum Flight Crew

A

Captain and First Officer

97
Q

Maximum Operating Airspeed

98
Q

Engine Maximum and Minimum Limitations

99
Q

APU Operational Limits

EGT - Start

100
Q

Normal and Maximum Takeoff & Go Around Engine Temperature Limit

A

Are limited to 5 minutes during a 10 minute period.

101
Q

Icing Conditions with Flaps/Slats Extended…

A

Do NOT hold in icing conditions with flaps/slats extended.

102
Q

N2 Max RPM

103
Q

Approved Fuels

Alternate

A

JP-8

Mixing of fuels is permitted.

104
Q

Maximum Differential Overpressure

105
Q

Maximum Gear Extended Speed (Vle)

106
Q

Maximum Crosswind (including gusts) for Takeoff and Landing

A

28 kts (A)

107
Q

Maximum Differential Pressure for Takeoff and Landing

108
Q

Maximum Flap Operating Speeds Vfe(KIAS)

Flaps 4

109
Q

Maximum Weights

Take (MTOW)

A

114,150 lbs

110
Q

Maximum Negative Differential Pressure

111
Q

Oil Pressure Minimum

112
Q

Flightdeck Door Access System Check

A

Must be accomplished prior to the first flight of the day.

113
Q

Memory Item

(YAW or ROLL) TRIM Runaway

A

AP/TRIM DISC … PRESS and HOLD

114
Q

Memory Item

Nosewheel Steering Runaway

A

STEER DISC … PRESS

115
Q

Memory Item

PITCH TRIM Runaway

A

AP/TRIM DISC … PRESS and HOLD

AmericanAirlines Embraer 190 (2 decks)

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