Bold Limitations Flashcards

1
Q

Maximum crosswind component for takeoff and landing

A

27 knots

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2
Q

Maximum crosswind component for landing from a category II approach

A

15 knots

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3
Q

Maximum headwind component for landing from a category II approach

A

16 knots

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4
Q

Maximum tailwind component for takeoff and landing

A

10 knots

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5
Q

Maximum operating altitude

A

41,000 ft.

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6
Q

Except in an emergency, takeoff or landing, will not be attempted whenever peak wind values exceeds ____. Crosswind components, not including ____, are limited to AFM maximum demonstrated as listed above. Crosswind and tailwind components may be further limited by runway conditions or ops specs.

A

50 knots; gust factor

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7
Q

Maximum altitude for single pack operation

A

31,000 ft.

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8
Q

Maximum severe turbulence penetration speed

A

280 KIAS/.75M, whichever is lower

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9
Q

Maximum gear extension speed

A

220 KIAS

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10
Q

Maximum gear extended speed

A

220 KIAS

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11
Q

Maximum gear retraction speed

A

200 KIAS

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12
Q

Maximum airspeed for windshield wiper operation

A

250 KIAS

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13
Q

Flaps 1

A

230 KIAS

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14
Q

Flaps 8

A

230 KIAS

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15
Q

Flaps 20

A

220 KIAS

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16
Q

Flaps 30

A

185 KIAS

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17
Q

Flaps 45

A

170 KIAS

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18
Q

The APU starter motor duty cycle is limited to not more than…

A

3 starts/start attempts in 1 hour with a 2 minute delay between cranking attempts

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19
Q

Bleed air extraction from the APU is not permitted above:

A

25,000 ft.

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20
Q

Each engine may be started using the ___ as a bleed air source

A

APU

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21
Q

APU indication RED

A

Maximum and minimum limitations

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22
Q

APU indication GREEN

A

Normal operating range

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23
Q

With the APU door not closed or the door position is unknown:

A

The airplane must be limited to 220 KIAS

Or the APU must remain in operation

24
Q

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

A

5 minutes

25
Q

Engine indication RED

A

Maximum and minimum limitations

26
Q

Engine indication AMBER

A

Caution range

27
Q

Engine indication GREEN

A

Normal operating range

28
Q

Oil, pressure: takeoff power

A

45 psi minimum

29
Q

After cold start, engine must remain at ___ until oil pressure returns to ___ ___.

A

Idle; normal range

30
Q

Continuous engine ignition must be used during the following:

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

31
Q

Starter cranking limits: ground

A

Start 1, 90 seconds ON, 10 seconds OFF
Start 2, 90 seconds ON, 10 seconds OFF
Start 3 and subsequent, 90 seconds ON, 5 minutes OFF

32
Q

Initiation of the thrust lever movement from SHUTOFF to IDLE: ITT (ground and air)

A

Ground: 120C
Air: 90C

33
Q

During landing, maximum reverse thrust is prohibited below ____, and reverse idol should be achieved by ____.

A

75KIAS; 60KIAS

34
Q

Slats/Flaps Limitation
En route + altitude

A

En route use of slots/flaps is prohibited.
15,000 ft. max

35
Q

Maximum permissible fuel inbalance between the left and right wing tanks for:
Takeoff + All other phases of flight

A

Takeoff: 300 lbs
All other phases of flight: 800 lbs

36
Q

Icing Operations required during taxi when?

A

Ground Contamination or Visible Moisture
OAT 10C or below
IAS N/A
COWL anti-ice

37
Q

Icing Operations required during takeoff when?

A

Ground contamination or visible moisture
OAT 10C or below -> COWL
OAT 5C or below-> WING and COWL
IAS N/A

38
Q

Icing Operations required during IN FLIGHT when?

A

Visible Moisture
From TAT 10C to SAT -39C
230 or greater- COWL
<230- WING and COWL

39
Q

Icing Operations required during ICE ANNUNCIATED INFLIGHT when?

A

ON when annunciated
WING and COWL

40
Q

Ground contamination definition:

A

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

41
Q

Visible 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).

42
Q

If __ __ is present below __ft AGL with OAT __ or __ activate __ anti-ice for takeoff. If OAT __ or __activate both __ and __ anti-ice for takeoff.

A

visible moisture; 400; 10C or below; COWL.
5C or below; COWL and WING.

43
Q

Taxi lights limitation

A

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

44
Q

Autopilot operation limitations

A

Prohibited below 600’AGL except:
Visual/non precision approaches, 400’AGL.
Precision approaches (PAR/ILS) or approaches with vertical guidance (APV), 80’AGL

45
Q

Autopilot limitation single engine

A

PAR/ILS/APV: 110’AGL

46
Q

Use of __ __ with the flight director or autopilot during approach is ____.

A

SPEED MODE (DES or IAS); not permitted

47
Q

Use of ___ during climb is ___.

A

VNAV; not permitted

48
Q

Use of ___ during approaches is only permitted when using ___ or ___ minimums.

A

VNAV; LPV or LNAV/VNAV

49
Q

FMS limitation

A

Changes to altitudes in the departure and missed approach procedures are prohibited.

50
Q

Maximum Taxi and Ramp Weight

A

CR7: 75,250 lbs
CR9: 85,000 lbs

51
Q

Maximum Takeoff Weight

A

CR7: 75,000 lbs
CR9: 84,500 lbs

52
Q

Maximum Landing Weight

A

CR7: 67,000 lbs
CR9: 75,100 lbs

53
Q

Maximum Zero Fuel Weight

A

CR7: 62,300 lbs
CR9: 70,750 lbs

54
Q

Braking loss/asymmetry

A
  1. Wheel brakes- release momentarily
  2. PM will select antiskid to off
  3. Wheel brakes- reapply as required
  4. Reverse thrust- apply maximum until stopping assured
55
Q

Stab trim runaway

A
  1. Control wheel- assume manual control and override runaway
  2. Stab trim disconnect- push, hold, and release
56
Q

Cabin alt message

A
  1. Oxygen mask- don and 100%
  2. Crew communications- establish
  3. Captain assigned PF duties
57
Q

Smoke/fumes in the cockpit

A
  1. Oxygen mask (if req)- Don and 100%
  2. Crew communications- establish