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Q400 > Limitations > Flashcards

Limitations Flashcards

0
Q

Maximum Take-Off Weight

High gross
4168, 4181, 4182, 4186

A

64,500lbs

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1
Q

Ramp Weight

High gross
4168, 4181, 4182, 4186

A

64,700lbs

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2
Q

Maximum Landing Weight

High gross
4168, 4181, 4182, 4186

A

61,750lbs

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3
Q

Maximum Zero Fuel Weight

High gross
4168, 4181, 4182, 4186

A

57,000lbs

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4
Q

Ramp weight

Enhanced Gross
4187 and Above

A

65,400lbs

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5
Q

Maximum take-Off Weight

Enhanced Gross
4187 and Above

A

65,200lbs

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6
Q

Maximum Landing Weight

Enhanced Gross
4187 and Above

A

62,000lbs

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7
Q

Maximum Zero Fuel Weight

Enhanced Gross
4187 and Above

A

58,000lbs

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8
Q

Minimum flight crew

A

1 pilot and 1 co-pilot

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9
Q

Kinds of Operations

A

Day and Night VFR
IFR
Icing Conditions

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10
Q

Vmo at 8,000ft

A

245 KIAS

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11
Q

Vmo at 10,000ft

A

282 KIAS

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12
Q

Vmo at 18,000ft

A

286 KIAS

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13
Q

Vmo at 20,000 ft

A

275 KIAS

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14
Q

Vmo at 25,000ft

A

248 KIAS

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15
Q

Flaps 5 Speeds

A

175 - 200 KIAS

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16
Q

Flaps 10 Speeds

A

160 - 181 KIAS

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17
Q

Flaps 15 Speeds

A

150 - 172 KIAS

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18
Q

Flaps 35 Speeds

A

145 - 158 KIAS

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19
Q

Maneuvering Limit Load Factors

Flaps Retracted

A

+2.5g

-1.0g

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20
Q

Maneuvering Limit Load Factors

Flaps Extended

A

+2.0g

-0.0g

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21
Q

Maximum Fuel Imbalance

A

600lbs

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22
Q 
CG Limits 
High Gross (4167, 4181, 4182, 4186)
FWD Limit (up to 53,000lbs)
FWD Limit (53,000 thru 64,500lbs)
AFT Limit
A
  1. 8%
  2. 8% thru 17.4%
  3. 0%

Slopes from 13.8% at 53,000lbs to 17.4% at 64,500 refer to CG Limits chart.

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23
Q

CG Limits
Enhanced Gross
(4187 and Above)

FWD Limit (up to 53,000lbs)
FWD Limit (53,000 thru 65,200lbs)
AFT Limit
A
  1. 8%
  2. 8 thru 17.7%
  3. 0%

Slopes from 13.8% at 53,000lbs to 17.7% at 65,200lbs refer to CG Limits chart.

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24
Q

Landing Gear Operating Speed (Vlo)

A

200 KIAS

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25
Q

Landing Gear Extended Speed (Vle)

A

215 KIAS

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26
Q

Rough Air Speed

A

210 KIAS

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27
Q

Alternate Gear Extension Speed

A

185 KIAS

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28
Q

Maximum Operating Altitude

A

25,000ft

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29
Q

Maximum Altitude for Take-off and Landing

A

10,000ft

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30
Q

Approach Category

A

Category C

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31
Q

Approach Minimums

A

CAT I

32
Q

Maximum Runway Slopes

A

+2% Uphill

-2% downhill

33
Q

Maximum Tailwind Component

Take-off Flaps -0 or 15
Landing Flaps 35

A

20kts

Note: All flaps 35 landings will be done with a maximum flap setting of 15 during the approach to the final segment

34
Q

Maximum Tailwind Component

Take-off Flaps 5
Landing Flaps 10 or 15

A

10kts

35
Q

Minimum Runway Width

A

No Less Than 100ft

36
Q

Maximum Crosswind Component

Hard, Dry or Wet Runway

A

32kts

37
Q

Maximum Crosswind Component

Dry Loose Snow (4.0in take-off, 5.1in landing)

A

18kts (R)

38
Q

Maximum Crosswind Component

Standing water, Slush, or Wet Snow

A

14kts (R)

39
Q

Maximum Operating Ambient Temperature

A

50C or ISA +35C

40
Q

Minimum Operating Ambient Temperature

A

-54C

41
Q

When do you need a warm-up period for the displays?

A

Parking in Temps

< -15 (5F) for > 3hrs

42
Q

When is setting take-off power prior to break release prohibited?

A

When the nose is > 45 degrees out of wind and the wind speed is > 8kts

43
Q

Can you single-engine or reverse taxi?

A

No

44
Q

When must the tank 1 and tank 2 auxiliary fuel pumps be on?

A

Take-Off and Landing

45
Q

Fuel Heater Temperature Limitation

A

Continuous operation prohibited when temperature is:

71C

46
Q

Minimum Oil Pressure

A

44 psi

47
Q

Normal Oil Pressure Operating Range

A

61 to 72 psi

48
Q

Minimum Teansient Oil Pressure

A

44 to 61 psi

49
Q

Minimum Oil Temp for Start

A

-40C

50
Q

Minimum Oil Temp Above Flight Idle

A

0C

51
Q

Maximum Oil Temp at Ground Idle

A

-40C

52
Q

Maximum Oil Temp PLA Between DISC and FLT IDLE

A

125C

53
Q

Minimum Oil Temp Above Ground Idle

A

0C

54
Q

Maximum Oil Temp Above Ground Idle

A

107C

55
Q

Maximum Continuous Oil Temp

A

107C

56
Q

Minimum Oil Temp to ensure engine air inlet ice protection, prior to take-off.

A

55C

57
Q

Minimum Oil Temp to ensure engine air inlet ice protection, in flight and within 3 minutes of setting take-off power.

A

65C

58
Q

APU Limitations

A

-Ground Operations Only
-Shutdown Prior to Takeoff
-Not Operated Unattended with PAX
-Not Operated Unattended During Pressure Refuelling
-

59
Q

APU Minimum Ambient Temp

A

-35C

60
Q

APU Maximum Ambient Temp

A

50C or ISA + 35C. Whichever is lower

61
Q

Maximum APU Ambient Temp with Louvres Installed

A

21C

62
Q

APU Starter Limitations

A

Max Time On Followed By
60 sec 2 min off
60 sec 2 min off
60 sec 30 min off

Note: if APU does not start in the 3rd attempt, maintenance action is required.

63
Q

Engine Starter Limitations

A

Max Time On Followed By
70 sec 2 min off
70 sec 2 min off
70 sec 30 min off

64
Q

Propeller Manufacturer and Model

A

Dowry Aerospace

R408

65
Q

Power plant Manufacturer and Model

A

Pratt and Whitney

PW150A

66
Q

Powerplant maximum Ambient Temp

A

50C or ISA + 35C, whichever is lower

67
Q

Power plant Minimum Ambient Temp

A

-54C

68
Q

Maximum Ambient Temp with Bypass Doors Open, Takeoff, Landing and Setting MTOP and MCP

A

ISA +25C

69
Q

Maximum Altitude for Airstart

A

20,000ft

70
Q

Automatic Take-Off Power Uptrim

A

10% Torque (Nominal)

71
Q

Wide Cut Type Fuels

A

Prohibited

72
Q

Mixing of Fuels

A

Permitted

73
Q

Usable Fuel

A

11,724lbs (5,862lbs/side)

74
Q

Maximum Engine Torque for Ground

A

100%

75
Q

Minimum Ground Nh

A

64.2%

76
Q

Maximum wind speed for ground operation with the nose >30 degrees out of wind

A

50kts

77
Q

For wind speed > 8kts with the nose > 30 degrees out of wind

A

GND Man. GND Static

9-20kts FLT IDLE. PLA 60 deg

21-35kts. FLT IDLE FLT IDLE

36-50kts. FLT IDLE DISC

78
Q

Ground Operations when the wind speed is > 50kts

A

Must be recorded and the maximum wind speed provided to maintenance within 24hrs (flying day)

Q400 (1 decks)

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