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E-190 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max Takeoff Weight

A

114,150 lbs

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2
Q

Max Landing Weight

A

97,000 lbs

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3
Q

Max Zero Fuel Weight

A

90,150 lbs

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4
Q

Maximum wind for takeoff and landing

A

50 knots

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5
Q

Maximum crosswind (including gusts) for takeoff and landing

A

28 knots

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6
Q

Maximum headwind for CAT 2/3 approaches

A

25 knots

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7
Q

Maximum crosswind including gusts for autoland

A

15 knots

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8
Q

Maximum crosswind with landing visibility less than 3/4 or 4000 RVR

A

15 knots

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9
Q

Maximum takeoff and landing tailwind component

A

10 knots

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10
Q

Maximum runway slope (uphill, downhill)

A

+2.0%, -2.0%

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11
Q

Maximum runway slope for autolands (uphill, downhill)

A

+1.0%, -1.0%

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12
Q

Flap maneuvering load acceleration limits flaps up

A

-1.0 to +2.5 G

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13
Q

Flap maneuvering load acceleration limits flaps down (1,2,3,4,5, and Full)

A

0.0 to +2.0 G

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14
Q

Maximum operating altitude

A

41,000 feet

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15
Q

Maximum take off and landing altitude

A

8000 feet

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16
Q

Maximum SAT for take off, landing, and ground start

A

52°C

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17
Q

Maximum altitude with flaps extended

A

20,000 feet

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18
Q

Minimum SAT for take off, landing, and ground start

A

-40°C

In the event of a landing below -40°C, the airplane may not take off without further maintenance inspection.

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19
Q

Maximum operating airspeed

A

Vmo

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20
Q

Maximum operating Mach number

A

.82 (Mmo)

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21
Q

Maximum airspeed for RAT operation

A

Vmo/Mmo

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22
Q

Turbulent airspeed (below 10,000 feet)

A

250 KIAS

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23
Q

Turbulent airspeed (at or above 10,000 feet)

A

270 KIAS/.76M

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24
Q

Tire limit groundspeed

A

195 knots

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25
Q

Maximum airspeed for windshield wiper operation

A

250 KIAS

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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

Maximum airspeed to open flight deck window

A

160 KIAS

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28
Q

Maximum gear extension speed (Vlo)

A

265 KIAS

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29
Q

Maximum gear extended speed (Vle)

A

265 KIAS

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30
Q

Maximum gear retraction speed (Vlo)

A

235 KIAS

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31
Q

Maximum flap operating speeds

A 
Flaps 1 - 230
Flaps 2 - 215
Flaps 3 - 200
Flaps 4 - 180
Flaps 5 - 180
Full - 165
32
Q

Design maneuvering speed

A

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

33
Q

Definition of icing conditions

A

OAT (on the ground and for take takeoff) or TAT (in-flight) is 10°C or below, and
Visible moisture in any form is present such as clouds, fog with visibility of 1 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, freeze on engines, nacelles, or engine sensor probe.

34
Q

During taxi out and take off, the MCDU TO DATASET MENU REF

A/I must be set to

A

ALL when OAT is 10°C or below and icing conditions exist or are anticipated

35
Q

Approved Fuels

A

Jet A and A-1
When using Jet A type fuel with ambient temperatures of -30°C or below, the fuel temperature prior to flight must be verified to be above -29°C

36
Q

Maximum usable fuel is

A

14,440 lbs per tank

37
Q

Maximum unusable fuel is

A

101.5 lbs per tank

38
Q

Minimum fuel temperature

39
Q

Maximum permissible fuel imbalance between left and right main tanks during all phases is

40
Q

The XFEED selector must be set to … during takeoff and landing

41
Q

Maximum altitude for a single pack operation

A

31,000 feet

42
Q

Maximum relief differential pressure up to 37,000 feet

43
Q

Maximum relief differential pressure above 37,000 feet

44
Q

Maximum differential Overpressure

45
Q

Maximum negative differential pressure

46
Q

Maximum differential pressure for takeoff and landing

47
Q

Brakes cooling limitation

A

Do not take off with amber brake temperature indicators

48
Q

Max Ramp Weight

A

114,500 lbs

49
Q

Do not hold in icing conditions with

A

Flaps/Slats extended

50
Q

Maximum altitude with flaps/slats extended is

A

20,000 feet

51
Q

During takeoff or go around, do not turn the autopilot on until above

A

400 feet AGL

52
Q

During landing, unless executing an auto landing with AUTOLAND 1 engaged, turn off the autopilot

A

Prior to 50 feet AGL

53
Q

Autoland weight limitations

A

Minimum 69,500 lbs

Maximum 97,000 lbs

54
Q

FMS Speed is

A

Not authorized for takeoff

55
Q

Engine type

56
Q

Starter duty cycle 1st and 2nd

A

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

Followed by
10 seconds OFF

57
Q

Starter duty cycle 3rd through 5th

A

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

Followed by
5 minutes OFF

58
Q

Dry-Motoring Cycle 1st

A

Maximum
90 seconds ON

Followed by
5 minutes OFF

59
Q

Dry-Motoring Cycle 2nd-5th

A

Maximum
30 seconds ON

Followed by
5 minutes OFF

After 5 motorings, a cycle may be repeated following a 15 minute cool down period

60
Q

Maximum reverse thrust is not permitted at airspeeds

A

Below 60 KIAS

Below 60 KIAS reduce to IDLE

61
Q

APU Starter Limits 1st and 2nd

A

APU Control Master START/ON

Followed by 60 seconds OFF

62
Q

APU Starter Limits 3rd cycle

A

APU Control Master START/ON

Followed by 5 minutes OFF

63
Q

APU Operational limit temperature

A

Minimum -54°C

Maximum ISA + 35°C

64
Q

APU Maximum altitude for Start

A

30,000 feet

65
Q

APU Maximum altitude for operation Electrical

A

33,000 feet

66
Q

APU Maximum altitude for operation Bleed

A

15,000 feet

67
Q

APU Maximum altitude for operation to assist engine start

A

21,000 feet

68
Q

Resetting a …. or …. circuit breaker is prohibited

A

Fuel boost pump or fuel indication system

69
Q

On ground, primary altimeters must be within …. feet of each other and within …. feet of field elevation

A

75 feet of both

70
Q

Maximum in flight difference between primary altimeters for RVSM

71
Q

Minimum Turning Width

A

70 ft 3 in

72
Q

Maximum crosswind braking action medium.

73
Q

Maximum crosswind braking action poor.

74
Q

Aircraft Wingspan

75
Q

Aircraft Length

A

118’11”

E-190 (3 decks)

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