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Limitations Flashcards

1
Q

Maximum crosswind for T/O and Landing

A

27 kts

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2
Q

Maximum crosswind for landing from a CAT II

A

15 kts

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3
Q

Maximum headwind for landing from a CAT II

A

16 kts

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4
Q

Maximum tailwind component

A

10 kts

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5
Q

Minimum approved runway width

A

100ft.

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6
Q

Maximum pressure altitude for T/O and landing

A

8,000ft.

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7
Q

Maximum Operating Altitude

A

41,000 ft.

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8
Q

Except in an emergency, takeoff or landing will not be attempted whenever peak wind value exceeds
________. Crosswind components, not including gust factor, are limited to AFM maximum
demonstrated as listed above. Crosswind and tailwind components may be further limited by runway
conditions or Operations Specifications

A

50 kts

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9
Q

Maximum positive pressure differential

A

8.7 psi

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10
Q

Maximum altitude for single pack operation

A

31,000 ft.

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11
Q

Low pressure air must be ____ prior to the main cabin door being closed and secure

A

OFF

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12
Q

EMER DEPRESS switch is prohibited above ________

A

15,000ft

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13
Q

Max Severe Turbulence penetration speed

A

280 KIAS/ .75 Mach whichever is slower

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14
Q

Max Gear Extension speed

A

220 KIAS

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15
Q

Max Gear Extended Speed

A

220 KIAS

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16
Q

Max Gear Retraction Speed

A

200 KIAS

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17
Q

Max Airspeed for windshield operation

A

250 KIAS

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18
Q

Max Cruise Mach in RVSM airspace

A

.82 M

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19
Q

Tire ground limit speed (700)

A

182 kts

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20
Q

Tire ground limit speed (900)

A

195 kts

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21
Q

Flap speeds

A

Flaps 1: 230
Flaps 8: 230
Flaps 20: 220
Flaps 30: 185
Flaps 45: 170

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22
Q

APU Starting limitation

A

The APU starter motor duty cycle is limited to not more than three (3) starts/start attempts in one (1) hour with a
two (2) minute delay between cranking attempts

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23
Q

Max Bleed Air extraction from APU altitude

A

25,000ft.

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24
Q

Max APU starting Altitude

A

37,000ft.

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25
Q

Can the APU be used for bleed air for engine start?

A

yes

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26
Q

APU door limitation

A

With the APU door not closed or the door position is unknown:
* The airplane must be limited to:
220 KIAS
* Or the APU must remain in operation

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27
Q

To protect the flight compartment CRT displays, the maximum permissible time for ground operations with DC
power only is ________.

A

5 minutes

28
Q

During all starts, do not exceed _____ for 2 minutes after start, or until all operating indications are in the normal
range, whichever is longer

A

75% N1

29
Q

Engines must be at idle for ____ prior to shut down

A

2 minutes
(Taxi time with engines stabilized at 80% N2 or below count towards the cool down period)

30
Q

Normal T/O power and max power on 2 engines is limited to______

A

5 minutes

31
Q

APR power (1 engine) is limited to

A

10 minutes

32
Q

ITT must below ____ before start on the ground

A

120 C

33
Q

ITT must below ____ before start in the air

A

90 C

34
Q

Before the first flight of the day, when the airplane is cold-soaked at an ambient temperature of -30°C (-22°F) or below for
more than 8 hours: (Cold Soak)

A
  • The engines must be motored for 60 seconds and fan rotation must be verified before an engine start is initiated
  • Thrust reversers must be actuated until the deploy and stow cycles are 2 seconds or less
35
Q

Oil Pressure Steady State idl

A

25 psi

36
Q

Max Oil pressure for T/O

A

45 psi

37
Q

After cold start, engine must remain at _____ until oil pressure returns to normal range

A

idle

38
Q

Continuous Engine Must be on:

A
  • Takeoff and landing on contaminated runways
  • Takeoff with high crosswind components (15 knots or greater)
  • Flight through moderate or heavier intensity rain
  • Flight through moderate or heavier intensity turbulence
  • Flight in the vicinity of thunderstorms
39
Q

Starter Cranking Limits (on ground)

A

1: 90 Seconds 10 Seconds OFF
2: 90 Seconds 10 Seconds OFF
3: and Subsequent 90 Seconds 5 Minutes OFF

40
Q

During landing, maximum reverse thrust is prohibited below ______, and reverse idle should be achieved by _____

A

75 KIAS, 60KIAS

41
Q

Reduced Thrust (FLEX) Takeoff

A

The following limitations apply to reduced thrust takeoff:
1. Anti-skid must be operative
2. PROHIBITED on contaminated runways
3. PROHIBITED if the airplane has been de-iced
4. PROHIBITED if wing and/or cowl anti-icing bleeds are in use
5. PROHIBITED if warnings of windshear or downdrafts have been forecast
6. PROHIBITED with an engine that cannot achieve full-rated thrust
7. PROHIBITED when a special departure procedure specifies full thrust for takeoff

42
Q

En Route use of Slats/ Flaps

A

PROHIBITED

43
Q

Max slats and or/ flaps extended

A

15,00ft.

44
Q

Minimum flight spoiler deployment

A

1,000 ft. AGL

45
Q

To ensure adequate maneuver margins, flight spoilers must not be extended inflight at airspeeds below the recommended ________

A

Vref +10

46
Q

Max fuel imbalance for T/O

A

300 lbs

47
Q

Max Fuel imbalance all other phases of flight

A

800lbs

48
Q

Gravity Refueling (700)

A

14,580

49
Q

Gravity Refueling (900)

A

14,810

50
Q

Pressure Refueling

A

19,594

51
Q

Engine fuel temperature cannot be below

A

5C

52
Q

Ground contamination definition

A

Runways, ramps or taxiways with surface snow, ice, slush or standing water

53
Q

Visual moisture definition

A

Visible moisture or precipitation in any form (such as fog with visibility of one mile or less, mist, rain, snow, sleet,
and ice crystals or clouds inflight)

54
Q

Taxi: Anti Ice

A

10 C or below: Cowl

55
Q

Take off: Anti-ice

A

10 C or below :cowl
5 C or below: wing and cowl

56
Q

InFLight: Anti Ice

A

OAT 10C to SAT -39C
greater than or equal to 230: cowl
Less than 230: wing and cowl

57
Q

When is Single engine Taxi Prohibited?

A

when ramps or taxiways are contaminated with snow, slush, or ice, or when snow or other
freezing/frozen precipitation is present

58
Q

When is a Tactile Check required?

A
  • The OAT is 10°C or less, or
  • The bulk fuel temperature is 0°C or less, or
  • The atmospheric conditions have been conducive to frost formation.
  • Ice and frost may continue to adhere to wing surfaces for some time even at outside air temperatures above 10°C.
59
Q

Taxi light limitation

A

The taxi lights must be switched OFF whenever the airplane is stationary in excess of 10 minutes

60
Q

Minimum brake cooling time

A

15 minutes, and all BTMS indicators must be green and not increasing

61
Q

Category II approaches are prohibited when the braking action is reported as less than

A

Medium

62
Q

Where can live animals not be transported?

A

Fwd Cargo

63
Q

Autopilot limitations

A

Prohibited below:
-600 ft. AGL except:
+non- precision approach 400 AGL
+precision and APV 80 ft. AGL
+precision app single engine 110 ft. AGL

64
Q

Max Taxi & Ramp Weight

A

700: 75,250
900: 85,000

65
Q

Max T/O weight

A

700: 75,000
900: 84,500

66
Q

Max Landing weight

A

700: 67,000
900: 75,100

67
Q

Max zero fuel weight

A

700: 62,300
900: 70,750

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