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Q400 Horizon QX 2018 > Memory Items - Limits > Flashcards

Memory Items - Limits Flashcards

Limitzzzz

1
Q

Severe Turbulence Speed

A

200 KIAS

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2
Q

Maneuvering Speed (VA)

A

200 KIAS

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3
Q

Max Flaps Speed 5º (VFE)

A

195 KIAS

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4
Q

Max Flaps Speed 10º (VFE)

A

175 KIAS

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5
Q

Max Flaps Speed 15º (VFE)

A

165 KIAS

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6
Q

Max Flaps Speed 35º (VFE)

A

155 KIAS

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7
Q

Landing Gear Operating Speed (VLO)

A

200 KIAS

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8
Q

Landing Gear Extended Speed (VLE) doors closed

A

215 KIAS

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9
Q

Ambient Temp Max (engine)

A

+50ºC or ISA +35ºC, whichever is lower

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10
Q

Engine Starter Cranking Limits

A

Start: 1, Max Time on: 70 Seconds, Followed by: 2 minutes off

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11
Q

On the ground (taxi and takeoff roll to the point of lift-off):
_____________ or below when precipitation in any form is present, or 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.

A

OAT is 10ºC

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12
Q

In flight (after lift-off to landing):
_____________ or below and _____________ is present in any form. Ice accretion on
aerodynamic surfaces is not considered to exist at temperatures of -40°C or below.

A

SAT is 5ºC, visible moisture

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13
Q

Engine intake bypass doors shall be ________ for engine operations in icing conditions

A

Open

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14
Q

Maximum crosswind component approved for takeoff and landing on a hard, dry, or wet
runway is ______.

A

32 knots

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15
Q

Maximum fuel imbalance between contents of main fuel tanks is ______ (This is an in-flight
limitation only.)

A

600 lb

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16
Q

Standby battery, Auxiliary battery and Main battery maximum loadmeter reading for
takeoff is

A

0.1

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17
Q

Minimum battery temperature for takeoff is

A

-20ºC

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18
Q

Maximum altitude with the landing gear and/or flap extended is

A

15,000 ft

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19
Q

Setting takeoff power prior to brake release, with the nose of the airplane more than ____ out
of wind, is prohibited for wind speeds greater than ____ knots.

A

45°, eight

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20
Q

Tank 1 and tank 2 auxiliary pumps must be ____ for takeoff and landing.

A

on

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21
Q

Maximum operating altitude

A

25,000 ft ASL

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22
Q

Maximum operating altitude for takeoff

A

10,000 ft ASL

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23
Q

Airplane maximum operating ambient temperature limit

A

+50°C or ISA +35°C, whichever is lower

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24
Q

Airplane minimum operating ambient temperature limit is _____.

A

-54°C

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25
Q

Ambient temperature conditions on the ground shall be derived by reference to reported
_____.
Ambient temperature conditions in flight shall be derived by reference to indicated _____.

A

OAT, SAT

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26
Q

Inflight operation of the _____aft of the _____ gate is _____.

A

Power Levers, FLIGHT IDLE, prohibited

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27
Q

Maximum cabin pressure differential limit

A

5.95 psi

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28
Q

Maximum cabin pressure differential limit during takeoff and landing

A

0.5 psi

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29
Q

Bleed air must be _____ for takeoff whenever:
• Tailwind component exceeds _____ knots
• Takeoff is conducted with _____ power selected
• _____ is suspected

A

off, ten, MTOP, Windshear

30
Q

For landing, bleed air must be _____ whenever:
• Tailwind component exceeds _____ knots
• Reported _____ exceeds _____
• _____is suspected

A

off, ten, OAT, 39°C (100°F), Windshear

31
Q

Takeoff in ______ mode is prohibited (AHRS)

A

BASIC, DG

32
Q

Baggage Compartment Fire Extinguishing:
Unless the _____ baggage compartments are empty, the airplane shall not be
operated farther than _____ hour flying time from a suitable airport for landing.

A

forward and aft, one

33
Q

_____ select switches on the Captain and First Officer ARCDU shall be _____ and the
_____ switch on the observer’s Audio Control Panel shall be _____, when using the
flightdeck _____.

A

HOT MIC, OFF, INT/RAD, centered, speakers

34
Q

APU is approved for _____ OPERATION ONLY.

A

GROUND

35
Q

APU shall be _____ prior to takeoff

A

shutdown

36
Q

APU shall not be operated _____ with _____ on board

A

unattended, passengers

37
Q

APU shall not be operated during _____ refueling.

A

gravity (overwing)

38
Q

To maintain steady electrical state, the APU _____ be started during _____.

A

shall not, refueling

39
Q

APU ambient temperature limitations (max)

A

+50ºC or ISA +35ºC, whichever is lower

40
Q

APU ambient temperature limitations (min)

A

-54ºC

41
Q

When the APU has been shut down in _____ below _____ for greater than
_____ hour, it must be preheated prior to start in accordance with applicable maintenance
procedures.

A

outside air temperature, -35ºC, one

42
Q

The APU Bleed Air shall be selected _____ when the aircraft is being _____.

A

off, deiced/anti-iced

43
Q

APU starter cranking limits (Start 1)

A

Max Time on: 60 seconds, Followed By: 5 minutes off

44
Q

APU starter cranking limits (Start 2)

A

Max Time on: 60 seconds, Followed By: Maintenance action required

45
Q

(APU) Including the time taken for maintenance action following the second start attempt, a
minimum of _____ minutes must elapse prior to the next start attempt.

A

30

46
Q

During autopilot operation, the pilot shall be seated at the _____ with _____ secured.

A

controls, harness

47
Q

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

A

2.5°, 4°

48
Q

AFCS is approved for autopilot coupled approaches to _____ limits only.

A

CAT I

49
Q

______ approaches are approved for _____ flap configurations.

A

Autopilot coupled, all

50
Q

Use of Flaps _____, autopilot coupled is prohibited with _____

A

35°, one engine inoperative

51
Q

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

A

18, This is not considered limiting

52
Q

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

A

1,000 feet AFE

53
Q

Autopilot shall be disengaged at or above _____ for:

  • HGS approaches flown in _____ mode
  • Approaches flown with an _____
  • Approaches flown with Flap _____
A

1,000 feet AFE, AIII, inoperative engine, 0°

54
Q

For coupled approaches, the autopilot shall be disengaged at or above _____.

A

200 feet AFE

55
Q

Autopilot shall be disengaged in _____ icing.

A

severe

56
Q

Autopilot shall be disengaged in _____ atmospheric turbulence

A

severe or extreme

57
Q

Max Flaps Speed 0º (VFE)

A

Vmo-10kts

58
Q

Maximum Tire Speed

A

182 KIAS

59
Q

Maximum Alternate Gear Extension Speed

A

185 KIAS

60
Q

Min Flaps Speed 5º (Vmin)

A

160 KIAS

61
Q

Min Flaps Speed 0º (Vmin)

A

180 KIAS

62
Q

Min Flaps Speed 15º (Vmin)

A

145 KIAS

63
Q

Min Flaps Speed 10º (Vmin)

A

150 KIAS

64
Q

Abort engine start if

A
  • Engine ITT approaches or exceeds 920ºC
  • NH is not in the green arch within 70 seconds of selecting Condition Lever to START & FEATHER
  • Engine Oil Pressure fails to reach 44 psi by start SELECT switch reset
65
Q

Takeoff Abort required when

A
  • Takeoff warning horn
  • Failure of the A/F ARM message to illuminate on ED
  • Engine fire or failure
  • MASTER WARNING
  • Takeoff torque not obtained on either engine
  • Exceeding engine limitations
  • Windshear encounter
  • HGS failure, “TO WARN,” or loss of HGS symbology during takeoff below 500 RVR when the runway centerline is not in sight
66
Q

O2 required when either pilot detects a situation

A
  • Which could introduce smoke or fumes in the flightdeck, shall state. “Smoke - Don mask,”
  • Results in loss of cabin pressure above 10,000 MSL, shall state, “Oxygen - Don mask.”
67
Q

Max ramp weight

A

65, 400 lbs

68
Q

Maximum takeoff weight

A

65,200 lbs

69
Q

Maximum landing weight

A

62,000 lbs

70
Q

Maximum zero fuel weight

A

58,000 lbs

71
Q

Minimum structural design weight

A

31,753 lbs

Q400 Horizon QX 2018 (7 decks)

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