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Q400 > Basic Limitations 01 > Flashcards

Basic Limitations 01 Flashcards

1
Q

What is the Q400’s maximum operating ambient temperature limit? 


A

+50° C
or
ISA +35

*whichever is lower

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2
Q

What is the Q400’s minimum operating ambient temperature limit?

A

-54°C

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3
Q

What is the maximum operating altitude of the aircraft? 


A

25,000 ft.

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4
Q

What is the maximum operating altitude for takeoff? 


A

10,000 ft.

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5
Q

What is Severe Turbulence Speed?

A

200 knots

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6
Q

What is Maneuvering Speed (VA)?

A

200 knots.

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7
Q

What is Maximum Flaps Extended Speed (VFE) for

Flaps 5 degrees? 

Flaps 10 degrees? 

Flaps 15 degrees? 

Flaps 35 degrees? 


A

Flaps 0 - Vmo - 10 knots

Flaps 5 - 195 KIAS


Flaps 10 - 175 KIAS

Flaps 15 - 165 KIAS

Flaps 35 - 155 KIAS

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8
Q

What is Landing Gear Operating Speed (VLO)? 


A

200 KIAS

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9
Q

What is Landing Gear Extended Speed (VLE)? 


A

215 KIAS

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10
Q

What must the temperature be (OAT) on the ground for icing conditions to exist? 


A

10°C

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11
Q

What must the temperature be (SAT) in flight for icing conditions to exist? 


A

5°C

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12
Q

True or False: The engine intake bypass doors shall be open for engine operation in icing conditions.

A

True, bypass doors shall be open for engine operation in icing conditions.

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13
Q

What is the maximum crosswind component approved for takeoff and landing on a hard, dry, or wet runway?

A

32 knots

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14
Q

What is the maximum fuel imbalance between contents of main fuel tanks in flight?

A

600lbs.

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15
Q

True or False: Tank 1 and Tank 2 auxiliary fuel pumps are required to be on for landing but not for takeoff.

A

False

Auxiliary Pumps 1 & 2 must be on for both landing and takeoff.

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16
Q

What is the maximum loadmeter reading for takeoff of the Standby battery, Auxiliary battery, and the Main battery?

A

.1

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17
Q

What is the minimum battery temperature for takeoff?

A

-20 C

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18
Q

What is the maximum operating altitude with the landing gear and/or flap extended?

A

15,000

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19
Q

Setting takeoff power prior to brake release, with the nose of the airplane more than 45 degrees out of wind, is prohibited for wind speeds greater than _____ kts. 


A

8 knots

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20
Q
  1. True or False: Inflight operation of the POWER levers aft of the FLIGHT IDLE gate is prohibited. 

A

True, it is prohibited.

21
Q

What is the maximum cabin pressure differential limit?

A

5.96

22
Q

What is the maximum cabin pressure differential limit during takeoff/landing? 


A

.5

23
Q

Bleed air must be off for takeoff whenever _____.

A
  • Tailwind component exceeds ten knots
  • Windshear is suspected
  • Takeoff is conducted with MTOP power selected
24
Q

For landing, bleed air must be off whenever _____.

A
  • Tailwind component exceeds ten knots
  • Windshear is suspected
  • Reported OAT exceeds 39°C (100°F)
25
Q

True or False: Takeoff in the BASIC mode (AHRS) is prohibited, but takeoff in DG mode is allowable. 


A

False

AHRS Basic is PROHIBITED
DG Mode is PROHIBITED

FOR TAKEOOFF

26
Q

Unless the forward and aft baggage compartments are empty, the airplane shall not be operated farther than _____ from a suitable airport for landing. 


A

1 Hour Flying Time

27
Q

True or False: HOT MIC select switches on the Captain and First Officer ARCDU shall be OFF and the INT/RAD switch on the observer’s Audio Control Panel shall be centered, when using the flight-deck speakers. 


A

True

28
Q

True or False: The APU is approved for GROUND OPERATIONS ONLY.

A

True

29
Q

True or False: The APU shall be shutdown prior to takeoff unless it is needed airborne. 


A

False

30
Q

True or False: The APU may be operated unattended with passengers on board if OAT exceeds 30 degrees C.

A

False

31
Q

True or False: The APU shall not be operated during gravity (overwing) refueling

A

True

32
Q

`True or False: The APU shall not be started during refueling. 


A

True

33
Q

What are the APU ambient temperature limitations?

A

(Upper) - +50oC or ISA +35oC, whichever is lower

(Lower) -54oC
whichever is lower

34
Q

True or False: The APU Bleed Air shall be selected off when the aircraft is being deiced/anti-iced. 


A

True

35
Q

What are the APU starter cranking limits?

A

1 - 60 seconds
5 minutes off

2 - 60 seconds
Maintenance action required

36
Q

True or False: During autopilot operation, the pilot shall be seated at the controls with harness secured. 


A

True

37
Q

Autopilot (coupled) and Flight Director (manual) approaches are approved from a nominal glideslope angle of _____ to maximum of _____.

A

2.5°to maximum of 4°

38
Q

AFCS is approved for autopilot coupled approaches to _____.

A

CAT I Only

39
Q

Autopilot coupled approaches are approved for all flap configurations except _____.

A

If one engine operative and use of 35° flaps

40
Q

Autopilot coupled approaches have been demonstrated in crosswind components up to _____ kts. 


A

18 knots. This is not considered limiting though.

Page 9

41
Q

The minimum height for autopilot engagement after takeoff/go-around is _____ feet AFE

A

1,000 AFE

42
Q

Autopilot shall be disengaged at or above _____ feet AFE for

-HGS approaches flown in AIII mode —

-approaches flown with an inoperative
engine

-approaches flown with Flaps 0 degrees. 


A

1,000 AFE

43
Q

For coupled approaches (non-CAT III), the autopilot shall be disengaged at or above _____ feet AFE

A

200 ft. AFE

44
Q

True or False: The autopilot shall be disengaged in severe icing and severe/extreme atmospheric turbulence.

A

True

45
Q

Maximum Alternate Gear Extension Speed

A

185KIAS

46
Q

Maximum Tire Speed

A

182 KIAS

*max tire ground speed touchdown may exceed 182 knots in abnormal flap configuration

47
Q

Icing Conditions on the Ground (taxi and takeoff roll to the point of lift-off):

A

 OAT is 10°C or below AND
o Precipitation in any form is present,

OR
o Fog with visibility of one mile or less;

ALSO

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

48
Q

Icing Conditions in Flight (after lift-off to landing):

A

 SAT is 5°C or below and visible moisture is present in any form.

 Ice accretion on aerodynamic surfaces is not considered to exist at temperatures of
-40°C or below.

Q400 (31 decks)

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