Systems Limitations Flashcards

0
Q

Max engine temp during start

A

815C

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1
Q

Min battery voltage

A

22.5 V

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2
Q

Min oil temp for engine start

A

-40C

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3
Q

Min oil pressure for engine start

A

25 psi

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4
Q

Starter cranking limits on the ground

A

1&2 - 90 sec on, 10 sec off

3-5 - 90 sec on, 5 min off

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5
Q

Starter cranking limits in flight

A

1&2 - 120 sec on, 10 sec off

3-5 - 120 sec on, 5 min off

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6
Q

On the ground, what is the max cumulative starter run time per start attempt

A

90 sec

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7
Q

In flight, what is the max cumulative starter run time per start attempt

A

120 sec

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8
Q

Dry motoring cycle limits

A

1 - 90 sec on, 5 min off

2-5 - 30 sec on, 5 min off

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9
Q

When starting engine with tail wind, when must start be manually aborted

A

If no positive increase of N1 prior to starter cutout (50% N2)

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10
Q

When does starter cut out

A

50% N2

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11
Q

Can you takeoff with Automatic Takeoff Thrust Control System (ATTCS) OFF

A

No

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12
Q

How long must you wait after EICAS is energized prior to starting APU

A

30 sec

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13
Q

How long can you leave the aircraft unattended with APU running

A

5 min (sw)

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14
Q

Can you use APU and High Pressure air cart at the same time

A

Nope

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15
Q

Min hydraulic reservoir temp for engine start

A

-18C

16
Q

What must brake temp indication be for takeoff

A

In green range

17
Q

After selecting reverse thrust, when can you move thrust levers into forward thrust range

A

When REV icon on EICAS is shown in amber or green

18
Q

Min engagement height for autopilot

A

400 ft

19
Q

Min use height for autopilot

A

50 ft

20
Q

Min use height for autopilot on non-precision approach

A

MDA

21
Q

At what speed do TAS, TAT, and SAT info become valid

A

Above 60kts

22
Q

When is standby mag compass indication not valid

A

When transmitting on VHF 1

23
Q

Which minimums must be used for all CAT I approaches

A

Barometric altimeter minimums

24
Q

Can you use IESS on back course approaches

A

No

25
Q

When should you manually inhibit predictive EGPWS functions

A

When landing at an airport not in database

And

During QFE ops if GPS data is unavailable or inoperative

26
Q

Can we do RNP approaches

A

No (sw)

27
Q

When can we not use FMS speed mode

A

During engine failure

28
Q

During power up, what must be done if one or both batteries are between 21-22.5 V

A

Recharge the batteries prior to takeoff through any AC source including engines during taxi.

29
Q

What must you do if, during startup, one or both batteries are below 21V

A

Report irregularity and do not depart

30
Q

To allow the flight controls built in test to complete, how long must you wait before turning on any hydraulic pump

A

3 mins

31
Q

For APU to start, how must the batteries be set

A

BATT 1 must be ON

BATT 2 must be AUTO

32
Q

While doing a Flex thrust takeoff, when will REF ATTCS automatically give you maximum available thrust

A
  • Difference between both engine N1 values is greater than 15%
  • OEI (one engine inoperative)
  • Associated thrust lever is moved to MAX detent
  • Windshear is detected
33
Q

When is use of Flex Thrust Takeoff prohibited

A
  • Takeoff on Contaminated runways
  • Reported or forecast windshear
  • when a special departure procedure specifies full thrust for takeoff
34
Q

If armed on the ground, when will LNAV automatically engage

A

200 ft AGL

35
Q

With all engines operating, what guidance will the flight director have you maintain

A

V2 + 10 to 15 kts

36
Q

What is the flight director’s guidance range during engine failure in flight

A

Based on weight and flap setting.

Min 8 degrees, max 18 degrees

37
Q

With one engine inop, limit bank angles to:

A

15 degrees at V2
20 degrees at V2+5
25 degrees at V2+10