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Bombardier Q400 (Cobham) > Limitations > Flashcards

Limitations Flashcards

1
Q

Maximum number of passengers

A

76

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2
Q

Maximum number of occupants

A

85

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3
Q

Max Brakes Release Weight

A

29,574 kg

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4
Q

Max Landing Weight

A

28,123 kg

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5
Q

Max Zero Fuel Weight

A

26,308 kg

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6
Q

Aft 2 Cargo weight limit

A

454 kg

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7
Q

Locker 11 restrictions (3)

A
  • At captain’s discretion
  • Soft-shelled bags
  • No DGs
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8
Q

G-limits

A

Flaps retracted: +2.5g / -1.0g

Flaps extended: +2.0g / 0.0g

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9
Q

Max operating altitude

A

25,000 ft

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10
Q

Max operating temperature

A

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

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11
Q

Min operating temperature

A

-54 degrees

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12
Q

Max tailwind

A

10 kts

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13
Q

Max crosswind

A

32 kts

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14
Q

Max taxi speeds

A

Normally

  • 25 kts in a straight line
  • 15 kts during turns

Narrow taxiways (between 15-18m)

  • 15 kts in a straight line
  • 10 kts during turns
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15
Q

VMO below 8,000ft

A

245 kts

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16
Q

VMO at 25,000ft

A

248 kts

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17
Q

VMO at 10,000ft

A

282 kts

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18
Q

VA

A

204 kts

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19
Q

Rough Air Speed

A

This is a maximum speed to be flown in severe turbulence

210 kts

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20
Q

VLO

A

200 kts

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21
Q

VLE

A

215 kts

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22
Q

Alternate Gear Extension Speed

A

185 kts

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23
Q

Max fuel imbalance

A

272 kg

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24
Q

Engine Intake Bypass Doors Open limitation

A

Max temperature is ISA+25 for:

  • take-off
  • landing
  • MTOP
  • MCP
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25
Q

Max altitude for airstart

A

20,000 ft

26
Q

Max altitude for gear or flap operations

A

15,000 ft

27
Q

Max ITT

A

880 degrees normally

During start it is 920 degrees (for max 20 seconds)

28
Q

Oil pressures

A

_ ENG OIL PRESS Warning Light: 44 to 50 psi

Green: 61 to 72 psi
Amber: 44 to 61 psi – 72 to 100 psi
Red: less than 44 psi – more than 100 psi

29
Q

Oil temperatures

A

PROPS OFF
Normal range: 0 to 107 degrees
Starting: > -40 degrees

PROPS ON/TEST
On ground and on take-off: 55 to 107 degrees
From 3 mins after take-off and in-flight: 65 to 107 degrees

Maximum oil temperature is 125˚ C between discing and flight idle.

30
Q

Usable fuel

A

5,318 kg

31
Q

Auxiliary fuel pumps limitation

A

Must be ON for Take-off and Landing

32
Q

Fuel temperatures

A

0 to 71 degrees

33
Q

Starter cranking limits

A

Start 1: 70 seconds, 2 minutes off
Start 2: 70 seconds 2 minutes off
Start 3: 70 seconds 30 minutes off

34
Q

Max tire speed

A

182 kts

35
Q

Max loadmeter reading for take-off

A

0.1

36
Q

Normal cabin pressure differential

A

5.46 psi

37
Q

Max cabin pressure differential

A

5.95 psi

38
Q

Max cabin altitude

A

8,000 ft

39
Q

Icing conditions are present when?

A

Icing conditions exist when the SAT on the ground and for take-off is 10 .C or below, or SAT in flight is 5 .C 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).

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

Icing conditions also exist when the SAT on the ground and for take-off is 10 .C 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.

40
Q

Autopilot seatbelt rule

A

During autopilot operation, the pilot must be seated at the controls with harness secured.

41
Q

Autopilot single-engine rule

A

The autopilot must be disengaged before descending through 1,000 ft AGL

42
Q

When can you first engage the autopilot after take-off?

A

1,000 ft AGL

43
Q

When must the autopilot be disengaged by on a non-precision approach?

A

200 ft AGL

44
Q

When must the autopilot be disengaged by on a precision approach?

A

160 ft AGL

45
Q

Minimum hydraulic fluid quantities for dispatch

A

System 1 and 2: at least 40%

System 3: at least 45%

46
Q

Minimum oxygen pressure for dispatch

A

1,300 psi (2 crew)

If below 1,800 psi, jump-seater must not use internal oxygen supply

47
Q

APU must not be operated when? (4+1)

A
  • during flight
  • unattended with passengers onboard
  • unattended when pressure refuelling
  • when gravity refuelling
  • APU must not be started or shut-down when pressure refuelling
48
Q

APU starter limits

A

Start 1: 1 minute, 5 minutes off

Start 2: 1 minute, maintenance action

49
Q

Position Error Correction

A

20 ft to be added to a Decision Altitude for a precision approach

50
Q

VFE 5

A

200

51
Q

VFE 10

A

181

52
Q

VFE 15

A

172

53
Q

VFE 35

A

158

54
Q

Holding

Minimum approach speeds (normal ops)

A

190

55
Q

Flap 0

Minimum approach speeds (normal ops)

A

180

56
Q

Flap 5

Minimum approach speeds (normal ops)

A

165

57
Q

Flap 10

Minimum approach speeds (normal ops)

A

155

58
Q 
Flap 15 (Flap 15 landing)
Minimum approach speeds (normal ops)
A

VREF or VREF ICE

59
Q 
Flap 15 (Flap 35 landing)
Minimum approach speeds (normal ops)
A

VREF ICE + 10

60
Q

Flap 35

Minimum approach speeds (normal ops)

A

VREF or VREF ICE

61
Q

Stable approach heights

A

1000ft AGL in IMC or Non-normal conditions

500ft AGL in VMC

Bombardier Q400 (Cobham) (6 decks)

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