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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 ____.

25
Engine indication RED
Maximum and minimum limitations
26
Engine indication AMBER
Caution range
27
Engine indication GREEN
Normal operating range
28
Oil, pressure: takeoff power
45 psi minimum
29
After cold start, engine must remain at ___ until oil pressure returns to ___ ___.
Idle; normal range
30
Continuous engine ignition must be used during the following:
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
Starter cranking limits: ground
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
Initiation of the thrust lever movement from SHUTOFF to IDLE: ITT (ground and air)
Ground: 120C Air: 90C
33
During landing, maximum reverse thrust is prohibited below ____, and reverse idol should be achieved by ____.
75KIAS; 60KIAS
34
Slats/Flaps Limitation En route + altitude
En route use of slots/flaps is prohibited. 15,000 ft. max
35
Maximum permissible fuel inbalance between the left and right wing tanks for: Takeoff + All other phases of flight
Takeoff: 300 lbs All other phases of flight: 800 lbs
36
Icing Operations required during taxi when?
Ground Contamination or Visible Moisture OAT 10C or below IAS N/A COWL anti-ice
37
Icing Operations required during takeoff when?
Ground contamination or visible moisture OAT 10C or below -> COWL OAT 5C or below-> WING and COWL IAS N/A
38
Icing Operations required during IN FLIGHT when?
Visible Moisture From TAT 10C to SAT -39C 230 or greater- COWL <230- WING and COWL
39
Icing Operations required during ICE ANNUNCIATED INFLIGHT when?
ON when annunciated WING and COWL
40
Ground contamination definition:
Runways, ramps or taxiways with surface snow, ice, slush or standing water.
41
Visible moisture definition:
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
If __ __ is present below __ft AGL with OAT __ or __ activate __ anti-ice for takeoff. If OAT __ or __activate both __ and __ anti-ice for takeoff.
visible moisture; 400; 10C or below; COWL. 5C or below; COWL and WING.
43
Taxi lights limitation
The taxi lights must be switched OFF whenever the airplane is stationary in excess of 10 minutes.
44
Autopilot operation limitations
*NOT UP TO DATE* need to fix Prohibited below 600’AGL except: Visual/non precision approaches, 80’AGL. Precision approaches (PAR/ILS) or approaches with vertical guidance (APV), 80’AGL
45
Autopilot limitation single engine
*NOT UP TO DATE* need to fix PAR/ILS/APV: 110’AGL
46
Use of __ __ with the flight director or autopilot during approach is ____.
SPEED MODE (DES or IAS); not permitted
47
Use of ___ during climb is ___.
VNAV; not permitted
48
Use of ___ during approaches is only permitted when using ___ or ___ minimums.
VNAV; LPV or LNAV/VNAV
49
FMS limitation
Changes to altitudes in the departure and missed approach procedures are prohibited.
50
Maximum Taxi and Ramp Weight
CR7: 75,250 lbs CR9: 85,000 lbs
51
Maximum Takeoff Weight
CR7: 75,000 lbs CR9: 84,500 lbs
52
Maximum Landing Weight
CR7: 67,000 lbs CR9: 75,100 lbs
53
Maximum Zero Fuel Weight
CR7: 62,300 lbs CR9: 70,750 lbs
54
Braking loss/asymmetry
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
Stab trim runaway
1. Control wheel- assume manual control and override runaway 2. Stab trim disconnect- push, hold, and release
56
Cabin alt message
1. Oxygen mask- don and 100% 2. Crew communications- establish 3. Captain assumes PF duties
57
Smoke/fumes in the cockpit
1. Oxygen mask (if req)- Don and 100% 2. Crew communications- establish

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