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
Max altitude for airstart
20,000 ft
26
Max altitude for gear or flap operations
15,000 ft
27
Max ITT
880 degrees normally | During start it is 920 degrees (for max 20 seconds)
28
Oil pressures
Green: 61 to 72 psi Amber: 44 to 61 psi -- 72 to 100 psi Red: less than 44 psi -- more than 100 psi #_ ENG OIL PRESS Warning Light: 44 to 50 psi
29
Oil temperatures
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
Usable fuel
5,318 kg
31
Auxiliary fuel pumps limitation
Must be ON for Take-off and Landing
32
Fuel temperatures
0 to 71 degrees
33
Starter cranking limits
Start 1: 70 seconds, 2 minutes off Start 2: 70 seconds 2 minutes off Start 3: 70 seconds 30 minutes off
34
Max tire speed
182 kts
35
Max loadmeter reading for take-off
0.1
36
Normal cabin pressure differential
5.46 psi
37
Max cabin pressure differential
5.95 psi
38
Max cabin altitude
8,000 ft
39
Icing conditions are present when?
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
Autopilot seatbelt rule
During autopilot operation, the pilot must be seated at the controls with harness secured.
41
Autopilot single-engine rule
The autopilot must be disengaged before descending through 1,000 ft AGL
42
When can you first engage the autopilot after take-off?
1,000 ft AGL
43
When must the autopilot be disengaged by on a non-precision approach?
200 ft AGL
44
When must the autopilot be disengaged by on a precision approach?
160 ft AGL
45
Minimum hydraulic fluid quantities for dispatch
System 1 and 2: at least 40% | System 3: at least 45%
46
Minimum oxygen pressure for dispatch
1,300 psi (2 crew) If below 1,800 psi, jump-seater must not use internal oxygen supply
47
APU must not be operated when? (4+1)
- 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
APU starter limits
Start 1: 1 minute, 5 minutes off | Start 2: 1 minute, maintenance action
49
Position Error Correction
20 ft to be added to a Decision Altitude for a precision approach
50
VFE 5
200
51
VFE 10
181
52
VFE 15
172
53
VFE 35
158
54
Holding | Minimum approach speeds (normal ops)
190
55
Flap 0 | Minimum approach speeds (normal ops)
180
56
Flap 5 | Minimum approach speeds (normal ops)
165
57
Flap 10 | Minimum approach speeds (normal ops)
155
58
``` Flap 15 (Flap 15 landing) Minimum approach speeds (normal ops) ```
VREF or VREF ICE
59
``` Flap 15 (Flap 35 landing) Minimum approach speeds (normal ops) ```
VREF ICE + 10
60
Flap 35 | Minimum approach speeds (normal ops)
VREF or VREF ICE
61
Stable approach heights
1000ft AGL in IMC or Non-normal conditions | 500ft AGL in VMC