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PSA airlines study June 2020 > POH Ch 3 Bold Limitations (7/9) Revision 27 > Flashcards

POH Ch 3 Bold Limitations (7/9) Revision 27 Flashcards

1
Q

Max xwind TO and LD

A

27 Kts

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2
Q

Max xwind landing CAT II

A

15 Kts

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3
Q

Max headwind landing CAT II

A

16kts

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4
Q

Max tailwind for TO and LD (including gusts)

A

10 Kts

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5
Q

Max operating altitude 7/9

A

41,000 ft

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6
Q

Except in an emergency, takeoff or landing will not be attempted whenever peak wind value exceeds:

A

50 Kts

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7
Q

Max altitude for single pack operation 7/9

A

31,000 ft

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8
Q

Turbulence penetration speed

A

280 KIAS/ .75 M, whichever is lower

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9
Q

Max gear extension speed

A

220 KIAS

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10
Q

Max gear extended speed

A

220 KIAS

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11
Q

Max gear retraction speed

A

200 KIAS

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12
Q

Flaps 1 VFE 7/9

A

230 KIAS

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13
Q

Flaps 8 VFE

A

230 KIAS

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14
Q

Flaps 20 VFE

A

220 KIAS

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15
Q

Flaps 30 VFE

A

185 KIAS

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16
Q

Flaps 45 VFE

A

170 KIAS

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17
Q

7/9
The APU starter motor duty cycle is limited to not more than ____ starts/start attempts in ___ hour with a __ minute delay between cranking attempts.

A

3 starts
1 hour
2 minutes

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18
Q

Bleed air extraction from the APU is not permitted above: (7/9)

A

25,000 ft

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19
Q

With the APU door not closed or the door position is unknown: (7/9)

A

Airplane must be limited to 220 KIAS or the APU must remain in operation.

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20
Q

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

A

5 minutes

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21
Q

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

A

75% N1

2 minutes

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22
Q

Operate Engines at or near idle for ___ prior to shutdown.

A

2 minutes

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23
Q

Takeoff power oil pressure

A

45 PSI minimum

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24
Q

After cold start, engine must ____ until oil pressure returns to normal range

A

Remain at idle

25
Q

Continuous Engine Ignition must be used during the following:

A
  • takeoff and landing on contaminated runways.
  • takeoff with high crosswind components (15 Kts or greater).
  • Flight through moderate or heavier intensity rain.
  • Flight through moderate or easier intensity turbulence.
  • Flight in the vicinity of Thunderstorms.
26
Q

7/9 ground only starter cranking limits

A

Start 1- 90 sec max on followed by 10 sec off
Start 2- 90 sec max on followed by 10 sec off
Start 3- 90 sec max on followed by 5 min off

27
Q

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

A

75 KIAS

60 KIAS

28
Q

(Engine operating limits due to wind direction 7/9)
Within 30° on either direction of the airplane nose- no wind speed limit
-OR-
>30° in either direction of the airplane nose- <5 kts wind speed

A

No limitations- TOGA thrust may be applied before brakes released.

29
Q

(Engine operating limits due to wind direction 7/9)

> 30° in either direction of the airplane nose- between 5 and 30 Kts wind speed

A

Apply maximum of 75% N1 before brake release, then TOGA thrust.

30
Q

(Engine operating limits due to wind direction 7/9)

>30° in either direction of the airplane nose- > 30 Kts wind speed

A

Apply maximum of idle/ taxi thrust before brake release, then TOGA thrust.

31
Q

(7/9) if Static/Standing takeoff data is generated and wind limits prevent a Static/standing takeoff:

A

A.) winds must be entered in ACARS
-OR-
B.) for Aircraft with ACARS INOP, dispatch must manually insert winds into TLR data.

32
Q

Minimum altitude for flight spoiler deployment

A

1,000 ft AGL

33
Q

To ensure adequate maneuver margins, flight spoilers must not be extended inflight at air speeds below the recommended reference speed plus ____

A

17 KIAS

34
Q

(7/9) max fuel imbalance

  • takeoff
  • All other phases of flight
A
  • 300 lbs

- 800 lbs

35
Q

Takeoff with fuel load in excess of ____ in the center tank is not permitted unless each wing tank is above ___

A

500 lbs

4,400 lbs

36
Q

Powered cross flow and gravity cross flow must be ___

A

Off for takeoff

37
Q 
(Operating in icing conditions) 
TAXI
condition: 
Temperature:
IAS:
Anti Ice:
A
  • Ground contamination or visible moisture.
  • OAT 10° C or Below
  • N/A
  • Cowl
38
Q 
(Operating in icing conditions) 
TAKEOFF
condition: 
Temperature:
IAS:
Anti Ice:
A
  • ground contamination or visible moisture
  • OAT 10°C or Below- Cowl.
  • OAT 5°C or below- Wing and Cowl
39
Q 
(Operating in icing conditions)
IN FLIGHT
condition: 
Temperature:
IAS:
Anti Ice:
A
  • Visible Moisture
  • From TAT 10°C to SAT -39° C
  • IAS > or = 230: Cowl
  • IAS <230: Wing and Cowl
40
Q 
(Operating in icing conditions) 
ICE ANNUNCIATED IN FLIGHT
condition: 
Temperature:
IAS:
Anti Ice:
A
  • On
  • N/A
  • N/A
  • Wing and Cowl
41
Q

Ground Contamination definition

A

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

42
Q

Visible Moisture definition

A

Visible moisture or precipitation in any form (such as fog with vis of 1 mile or less, mist, rain, snow, sleet, and ice crystals or clouds inflight).

43
Q

If visible moisture is present below ____ with OAT ___ activate cowl anti ice for TO. If ___ activate both cowl and wing anti ice for TO.

A
  • 400 ft AGL
  • OAT 10°C
  • OAT 5°C
44
Q

Icing conditions exist in flight at a TAT of ____ or below, and visible moisture in any form is encountered (such as clouds, rain, snow, sleet, or ice crystals), except when the SAT is ____ or below.

A

10°C (50°F)

-40°C (-40°F)

45
Q

Do not hold in icing conditions with the _________.

A

Slats and/or flaps extended.

46
Q

Taxi lights must be switched to OFF whenever the airplane is stationary in excess of ____.

A

10 minutes.

47
Q

Minimum brake cooling time is ____, and all BTMS indicators must be _____.

A

15 minutes

- green and not increasing.

48
Q

CAT II approaches are prohibited when the braking action is reported as less than ____.

A

Medium

49
Q

Operation with the autopilot engaged is prohibited at altitudes below ____, except when performing the following:

  • for VIS and non precision approaches, minimum height for autopilot is ____.
  • for (PAR/ILS), the minimum height for autopilot use is _____.
  • (900) for PAR/ILS, one engine inop min height for autopilot is ____.
A
  • 600 ft AGL
  • 400 ft AGL
  • 80 ft AGL, with glide path exceptions (see POH 3.13.1)
  • 110 ft AGL
50
Q

Use of _______ with the flight director or autopilot coupled during approach is not permitted.

A

SPEED MODE (DES or IAS)

51
Q

Use of ____ with the flight director or autopilot coupled during the climb and approach phases of flight is not permitted.

A

VNAV

52
Q

Max Taxi and Ramp weight- 700

A

75,250 lbs

53
Q

Max Taxi and Ramp weight- 900

A

85,000 lbs

54
Q

Max TO weight- 700

A

75,000 lbs

55
Q

Max TO weight- 900

A

84,500 lbs

56
Q

Max landing weight- 700

A

67,000 lbs

57
Q

Max landing weight- 900

A

75,100 lbs

58
Q

Max ZFW- 700

A

62,300 lbs

59
Q

Max ZFW- 900

A

70,750 lbs

PSA airlines study June 2020 (2 decks)

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