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E170 > Limitations > Flashcards

Limitations Flashcards

1
Q

VMO

A

300

320 @ 10,000

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2
Q

MMO

A

.82

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3
Q

Max Turbulent air below 10,000

A

250

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4
Q

Max Turbulent air Above 10,000

A

270 / .7M

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5
Q

Max Tire Limit GS

A

195

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6
Q

Max Wiper Speed

A

250

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7
Q

VLO

A

250

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8
Q

VA

A

240

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9
Q

VLE

A

250

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10
Q

VLO

A

250

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11
Q

VFE 1

A

230

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12
Q

VFE 2

A

215

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13
Q

VFE 3

A

200

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14
Q

VFE 4

A

180

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15
Q

VFE 5

A

180

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16
Q

VFE FULL

A

165

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17
Q

Auto Flight Takeoff limit

A

400 ft

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18
Q

Auto Flight Coupled ILS Limit

A

50 ft

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19
Q

APU Starter limits 1st and 2nd

A

60 seconds on then 60 seconds off

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20
Q

APU Starter limits 3rd cycle

A

60 seconds on then 5 5inutes off

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21
Q

Engine Starter Duty Cycle Limits 1st and 2nd

A

Ground: 90 seconds on 10 seconds off
Flight: 120 seconds on 10 seconds off

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22
Q

Engine Starter Dry Motoring 1st attempt

A

90 seconds on 5 minutes off

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23
Q

Engine Starter Dry Motoring 2nd through 5th attempt

A

30 seconds on 5 minutes off

24
Q

APU Altitude Start limit

A

30,000

25
Q

APU Altitude Electric use limit

A

33,000

26
Q

APU Altitude Bleed use

A

15,000

27
Q

Altitude Engine Start

A

21,000

28
Q

Definition of Icing Conditions

A

10 degrees and below and….

a. Visible Moisture or
b. Surface Snow, Slush, Ice, or Standing Water

29
Q

EICAS Engine Limit Max and Min markings

A

Red

30
Q

EICAS Engine Limit Caution Range

A

Amber

31
Q

EICAS Engine Limit Normal Range

A

Green

32
Q

Engine Thrust: Use of reduced takeoff thrust procedures is not allowed….

A

On runways contaminated with standing water, slush, snow, or ice.

33
Q

Max Land Weight

A

170 72,310

175 74,957

34
Q

Max Tail Wind component

A

10 kts

35
Q

Max Operating Altitude

A

41,000

36
Q

Max Flap Extension Altitude

A

20,0000

37
Q

Fuel Tank Min Temp

A

-40 C

38
Q

Max Fuel Imbalance

A

800 lbs

39
Q

Air Conditioning Max Alt for single pack Ops

A

31,000

40
Q

Flap Max Altitude Extended

A

20,0000

41
Q

Single Engine Taxi is not authorized when….

A

1) Braking action is less than good.
2) RVR is reported less than 1200
3) Power out is required (no pushback)
4) After Landing
a) If starting the APU, do not shut down an engine until the APU has stabilized at 95% or greater for a Min of 3 sec.
b) A 2 minute cool down must be observed prior to shutting down an engine.
c) Wait a Min of 1 additional minute after shutting an engine down prior to starting the APU.

42
Q

Engine Starter Duty Cycle Limits 3rd through 5th

A

Ground: 90 seconds on 5 minutes off

In Flight: 120 seconds on 5 minutes off

43
Q

Max Takeoff and Landing Altitude

A

8,000 ft

44
Q

Min Takeoff and Landing Altitude

A

-1,000 ft

45
Q

Min Ambient Temp for Takeoff

A

-40 C (SAT)

46
Q

Min Ambient Temp for Operation

A

-54 C (SAT)

47
Q

Max Ramp Weight

A

170 82,364

175 85,870

48
Q

Max Takeoff Weight

A

170 82,011

175 85,517

49
Q

Fuel Quantity Capacity (Total)

A

20,935

50
Q

Unusable Quantity per Tank

A

100lbs

51
Q

Crossfeed Operations during takeoff and landing

A

Must be OFF

52
Q

Max Differential Pressure

A

< 37,000 ft 7.80 psi

>37,000 ft 8.34 psi

53
Q

Brake Temps in Amber?

A

Do not take off.

54
Q

Thrust Reversers….

A
  • Ground use only
  • Full stop landings
  • Do not attempt go-around after deployment
  • Powerback is prohibited
  • IDLE thrust below 60 KIAS
  • After selecting Reverse Thrust, do not move the thrust levers forward of the detent until the REV icon on the EICAS is amber or green.
55
Q

APU Min start temp

A

-54 C

E170 (15 decks)

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