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Dash 8 Q400 MILM > Limitations > Flashcards

Limitations Flashcards

1
Q

Rough air speed

A

210 KIAS

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2
Q

Landing gear operating speed (Vlo)

A

200 KIAS

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3
Q

Takeoff or landing with the bypass doors open is prohibited at or above a maximum ambient temperature limitation of ___.

A

ISA +25C

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4
Q

Minimum Oil PSI

MaxStart Oil PSI

Normal Oil PSI

Transient (low ) Oil PSI

A

44 PSI

100 PSI

61 to 72 PSI

44 to 61 PSI

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5
Q

Minimum portable oxygen pressure for dispatch (2 crew/3crew)…and gives x hours?

A

1300 PSI (2 crew)

1800 PSI (3 crew)

2 Hours

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6
Q

AFCS is approved for autopilot approaches to… (what Category)

A

CAT I limits only.

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7
Q

Maximum operating altitude for takeoff and landing

A

10,000 ft

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8
Q

Maximum altitude for landing gear or wing flaps

A

15,000 ft

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9
Q

Maximum fuel imbalance

A

600 lbs

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10
Q

What ice is detected the AIRFRAME MODE SELECT selector must be…

A

positioned at FAST.

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11
Q

Autopilot must be disengaged…(conditions)

A

in severe icing. in severe atmospheric turbulence.

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12
Q

For all approaches the autopilot must be disengaged at or above

A

200 ft agl

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13
Q

Maximum operation speed (Vmo)245 KIAS

0 to 8,000 ft

8 to 10,000

10 to 18,000

18 to 20,000

20 to 25,000

A

0 to 8,000 ft 245

8 to 10,000 282

10 to 18,000 286

18 to 20,000 275

20 to 25,000 248

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14
Q

Airplane min / max operating ambient temperature limit

A

-50c to 50c or (ISA +35c)

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15
Q

The aircraft is only authorized for Cat __ approach minimums

A

I

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16
Q

Starting Max ITT

&

Max ITT normal

A

920 (20 seconds maximum)

880 Normal Max

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17
Q

Max reverse Max torque

A

35%

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18
Q

On a Single Engine approach the AP must be off …..

A

past the final approach fix or 1000 feet agl, whichever is lower

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19
Q

Fuel heater outlet temp limitation

A

operation with fuel heater outlet temperature below 0C or above 71 C is prohibited

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20
Q

Normal cabin pressure

differential limit

A

5.46 +/- 0.1 psi

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21
Q

APP mode, autopilot engaged approaches, is approved for what flap settings:

A

Flap 0, 5, 10, 15, and 35

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22
Q

Minimum SAT for engine relight

A

-40C

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23
Q

APU is approved for…

A

ground operations only.

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24
Q

Max reverse Max ITT

A

880C

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25
Q

Wheel brake cooling limits apply when….and shorted time is…..

A

between a landing or a low-energy rejected takeoff and a subsequent takeoff to ensure that sufficient brake energy is available

15 Minutes min

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26
Q

Standby, Auxiliary, and Main Battery Maximum load meter reading for takeoff

A

0.1

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27
Q

With and Cargo in any compartment the airplane must no be…..

A

the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.

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28
Q

Minimum Nh% ground operation

A

64.2%

29
Q

Definition of icing conditions

A

Icing conditions exist when the SAT on the ground and for takeoff is 10C or below, or SAT in flight is 5C or below, and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, or ice crystals). Icing conditions also exist when the SAT on the ground and for takeoff is 10C or below 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.

30
Q

Engine intake bypass doors must be…(closed/open) in what conditions

A

open for engine operation in icing conditions.

31
Q

APU ambient temperature limits

A
  • 35 to +50C or (ISA +35C)
32
Q

Maximum altitude for air-start

A

20,000 ft

33
Q

Integrated Standby Instrument limitation (flight time)

A

With the ISI installed the airplane must not be operated further than 1 hour flying time from a suitable airport for landing.

34
Q

Maximum runway slopes approved for takeoff and landing

A

+ 2% to - 2%

35
Q

Maximum cabin pressure differential limit during taxiing, takeoff and landing

A

0.5 psi

36
Q

Maximum cabin altitude (pressurized flight)

A

8,000 ft

37
Q

Standby, Auxiliary, and Main Battery Minimum battery temperature for takeoff

A

-20C

38
Q

Route limitation (this is the general…how far/how long can you be ?)

A

The route of flight must be within ONE hour flight time of a suitable airport in still air at normal cruising speed with one engine inoperative.

39
Q

Maximum tailwind component

A

10 kts

40
Q

Minimum flight crew

A

One Pilot and One copilot

41
Q

Starting Oil temperature

A

-40C min

42
Q

Oil Temps
Minimum for Starting

Normal

Icing

A

-40c

0 - 107c

55c; 65c in 3 min

43
Q

Maximum cabin pressure

differential limit

A

5.95 psi

44
Q

Propeller make and model

A

Dowty Aerospace R408

45
Q

Maximum tire speed

A

182 kts

46
Q

For approach minimums on straight in and circle approaches the DHC-8-402 is a category __ aircraft.

A

C

47
Q

Landing gear extended speed (Vle)

A

215 KIAS

48
Q

Powerplant ambient temperature limitation

A

-54C to +50C or (ISA +35C)

49
Q

Normal takeoff (NTOP) Max torque

A

(NTOP torque indication will be 90% or 91%)

50
Q

APU starter cranking limits

A

60 secs on, 5 mins off

60 secs on, maintenance action is required

51
Q

AC Gen, DC Gen, and TRU Maximum load air/ground

A

1.0

52
Q

Powerplant starter cranking limits

A

70 secs on, 2 mins off

70 secs on, 2 mins off

70 secs on, 30 mins off

53
Q

Center of gravity limits Fore and Aft

A

17% MAC

36% MAC

54
Q

Maximum wind speed for ground operation with the nose of the airplane more than 30 degrees out of the wind

A

50 kts

55
Q

Alternate gear extension speed

A

185 KIAS

56
Q

Maneuvering speed (Va)

A

204 KIAS

57
Q

FLAP Extension Speeds

5

10

15

35

A

5 200

10 181

15 172

35 158

58
Q

Maximum Ramp weight

Maximum takeoff weight

Maximum Landing weight

Maximum zero fuel weight

A

65,400 lbs

65,200 lbs

62,000 lbs

58,000 lbs

59
Q

After takeoff or go around the minimum height for autopilot engagement is _____.

A

1000 ft agl

60
Q

Autopilot and flight director only approaches are approved for glideslope angles of ___ to a maximum of ___.

A

2.5 degrees to a maximum of 4 degrees

61
Q

Tank 1 and 2 auxiliary fuel pumps must be…

A

….on for takeoff and landing.

62
Q

Max takeoff (MTOP) (limited to x mins)

A

10 Minute Engines

63
Q

Maneuvering G limit load factors

Flaps retracted

Flaps extended

A

+ 2.5 g - 1.0 g

+ 2.0 g - -0.0 g

64
Q

Contaminated runway definition

A

More than 25% of surface is covered by any standing water, ice, slush, or snow

65
Q

Automatic takeoff power uptrim is ….TQ?

A

10% torque (nominal)

66
Q

Powerplant make and model

Horse Power

A

Pratt & Whitney PW150A

5071,

67
Q

APU must not be operated unattended…

APU must be of for….

A

with passengers onboard. during pressure refueling.

Off for Gravity…

68
Q

Maximum operating altitude

A

25,000 ft

Dash 8 Q400 MILM (17 decks)

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