Limitations Flashcards

1
Q

The E-170/5 is approved for day and night operations in the following conditions…

A

VFR

IFR

Icing

CAT 1&2

RVSM

EOW

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2
Q

Max takeoff weight is limited by the most restrictive of the following…

A

Max takeoff weight (climb limited)

Max field length limited TO weight

Max certificated takeoff weight

Obstacle clearance, en route, and LDG limits

Brake energy limit weights

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3
Q

Maximum landing weight is limited by the most restrictive of the following…

A

Max approach and landing weight (rwy length plus obstacle, altitude, temperature, and i op equipment limits)

Max landing weight (climb limited)

Max certificated landing weight

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4
Q

E-170 Max ramp weight

A

82,364

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5
Q

E-175 Max ramp weight

A

85,870

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6
Q

E-170 Max takeoff weight

A

82,011

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7
Q

E-175 Max takeoff weight

A

85,517

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8
Q

E-170 Max landing weight

A

72,310

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9
Q

E-175 Max landing weight

A

74,957

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10
Q

E-170 Max zero fuel weight

A

65,256

66,446

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11
Q

E-175 Max zero fuel weight

A

69,886

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12
Q

E-170 Max cargo weights

A

3020 FWD

2271 AFT

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13
Q

E-175 Max cargo load

A

3307 FWD

2535 AFT

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14
Q

E-170 Max amount of dry ice

A

300 lbs

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15
Q

E-175 Max amount of dry ice

A

440 lbs

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16
Q

Where is dry ice not allowed to be carried?

A

Aft cargo compartment

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17
Q

Max takeoff and landing tailwind component

A

10 KTS

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18
Q

Max runway slope

A

+-2%

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19
Q

Flaps up load limit

A

-1.0 to +2.5

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20
Q

Flaps down load limits

A

0.0 to 2.0

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21
Q

Max altitude

A

41,000’

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22
Q

Max takeoff/landing altitude

A

8,000’

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23
Q

Max ambient temp for TO and landing

A

52C

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24
Q

Max flap extension altitude

A

20,000’

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25
Q

Max latitudes

A

78N to 78S

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26
Q

Min ambient temp for TO and landing

A

-40C

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27
Q

Max turbulent air penetration speed < 10,000’

A

250 KIAS

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28
Q

Max turbulent air penetration speed at or above 10,000’

A

270 KIAS/0.76 M

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29
Q

Max gear speed

A

250 KIAS

30
Q

Max tire groundspeed

A

195 KTS

31
Q

Flaps 1

A

230 KIAS

32
Q

Flaps 2

A

215 KIAS

33
Q

Flaps 3

A

200 KIAS

34
Q

Flaps 4

A

180 KIAS

35
Q

Flaps 5

A

180 KIAS

36
Q

Flaps FULL

A

165 KIAS

37
Q

Max speed for direct vision window

A

160 KIAS

38
Q

Va

A

240 KIAS

39
Q

Definition of icing conditions

A

10C or below; and

Visible moisture present (clouds, fog w/ < 1 mile vis, mist, rain, snow, sleet, and ice) or

When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines; or freeze on engines, nacelles, or engine sensor probes

40
Q

When must MCDU DATASET MENU be set to ALL during taxi out and takeoff?

A

When SAT 10C or < and icing conditions exist or are anticipated to be encountered < 1700 AFE

41
Q

Max windshield wiper speed

A

250 KIAS

42
Q

Max fuel capacity

A

20,936 lbs

43
Q

Min fuel tank temp

A

-37C

44
Q

Max fuel imbalance

A

790 lbs

45
Q

Can you takeoff or land with crossfeed on?

A

No

46
Q

Max altitude for single pack

A

31,000’

47
Q

Four flap operation limitations

A

Max altitude 20,000’

No en route use of flaps

Do not hold in icing conditions with flaps out

No flaps 4 for landing

48
Q

Thrust reversers must be stowed by

A

60 KIAS

49
Q

Standby mag compass is not valid when…

A

Transmitting on VHF #1

50
Q

Which approaches are prohibited using the IESS?

A

LOC backcourse

51
Q

RVSM required equipment

A

2 RVSM compliant ADS

1 autopilot (engaged), with operative altitude hold

1 altitude alerter

1 transponder

52
Q

Which ADS are RVSM approved?

A

1,2, and 3

53
Q

ADS3 is not considered RVSM compliant when ADS3 SLIPCOMP FAIL is displayed

A

FYI

54
Q

Max PFD altimeter difference -2000 up to 10,000’

A

50’

55
Q

Max PFD altimeter difference 10,000’ up to 20,000’

A

120’

56
Q

Max PFD altimeter difference 20,000’ up to 41,000’

A

180’

57
Q

When are FMS speeds prohibited during approach?

A

After the aircraft is in the landing configuration (final flap setting)

58
Q

Minimum AP engagement height

A

400 AGL

59
Q

Minimum AP use height for ILS

A

50 AGL

60
Q

Minimum AP use height for non-precision approach

A

MDA (DA)

61
Q

Required flap setting for CAT 2

A

5

62
Q

Max CAT 2 crosswind component

A

12 KTS

63
Q

What kind of engine is on the E-170/5?

A

CF34-8E5

64
Q

Before applying takeoff thrust, allow the engines to warm up for a minimum of…

A

2 minutes

65
Q

Allow the engines a minimum of long to cool before shutting down?

A

2 minutes

66
Q

Use of FLEX takeoff is not allowed on runways contaminated with…

A

Standing water

Slush

Snow

Ice

67
Q

FLEX takeoff is not allowed on wet runways unless…

A

Suitable performance accountability is made for the increased stopping distance

68
Q

Single engine taxi is not authorized when…

A

Freezing rain, freezing drizzle, freezing fog, or heavy snow is anticipated

Braking action < good

RVR < 1200’

Power out is required

69
Q

APU max altitude for start

A

30,000’

70
Q

APU max altitude

A

33,000’

71
Q

APU max altitude for bleed

A

15,000’

72
Q

APU max altitude for air start

A

21,000’