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POH 3 - Limitations Flashcards

1
Q

Max x wind component for takeoff and landing

A

27 knots

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2
Q

Max x wind for landing Cat II

A

15 knots

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3
Q

Max headwind for landing Cat II

A

16 knots

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4
Q

Max tailwind for takeoff and landing

A

10 knots

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5
Q

Max operating altitude

A

41,000 feet

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6
Q

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

A

50 knots

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7
Q

Max altitude for single pack ops

A

31,000 feet

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8
Q

Max severe turbulence penetration speed

A

280 KIAS/.75M - whichever is lower

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9
Q

Max gear extension speed

A

220 knots

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10
Q

Max gear extended speed

A

220 knots

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11
Q

Max gear retraction speed

A

200 knots

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12
Q

Max airspeed for windshield wiper ops

A

250 knots

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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

APU starter motor duty cycle

A

Not more than 3 starts/start attempts in 1 hour with 2 minute delay between cranking attempts

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19
Q

Bleed air extraction from APU is not permitted above

A

25,000 feet

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20
Q

Which engine can be started using APU as bleed air source

A

Either

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21
Q

With APU door not closed or position unknown

A

Aircraft is limited to 220 KIAS

Or

APU must remain in operation

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22
Q

Max permissible time for ground ops with DC power

A

5 minutes - to protect CRT displays

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23
Q

During all starts, do not exceed

A

75% N1 for 2 mins after start

Or

Until all operating indications are in normal range

Whichever is longer

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24
Q

Oil pressure with take off power

A

45 psi minimum

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25
Q

After cold start, engine must

A

Remain at idle until oil pressure returns to normal range

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26
Q

When must use continuous ignition

A

Take off or landing on contaminated runway
Take off with x wind 15 knots or greater
Flight through mod or heavier intensity rain
Flight through mod or heavier intensity turbulence
Flight in vicinity of thunderstorm

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27
Q

Starter cranking limits

A

Start 1 - 90 seconds max time on - followed by 10 seconds off
Start 2 - 90 - 10
Start 3 and subsequent- 90 seconds max time on - 5 minutes off

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28
Q

During landing, max reverse thrust is prohibited below

A

75 KIAS and reverse idle should be achieved by 60 KIAS

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29
Q

FLEX takeoff limitations

A

Anti skid must be operative
No on contaminated runways
No if aircraft has been deiced
No if wing/cowl anti icing bleeds in use
No if warnings of windshear or downdrafts forecast
No with engine that cannot achieve full rated thrust
No when special departure procedure requires full thrust for takeoff

30
Q

Can you use slats/flaps en route?

A

No, prohibited

31
Q

Max slats/flaps extended altitude

A

15,000 feet

32
Q

Minimum altitude for flight spoiler deployment

A

1,000 feet AGL

33
Q

To ensure adequate maneuver margins, flight spoilers must not be extended inflight at airspeeds below the recommended reference speed plus __.

A

10 KIAS

34
Q

Max permissible fuel imbalance between left and right wing tanks

A

Takeoff: 300 lbs
All other phases: 800 lbs

35
Q

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

A

500 lbs
4,400 lbs

36
Q

Powered crossflow and gravity crossflow must be __ for takeoff

A

Off

37
Q

Cowls on temp range

A

Ground: OAT 10C or below
Air: From TAT 10C to SAT -39c

38
Q

Wing and cowls on temp range

A

Ground: Takeoff with OAT 5C or below and contamination/vis moisture
Air: From TAT 10C to SAT -39C below 230 knots

39
Q

Ground contamination definition

A

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

40
Q

Visible moisture definition

A

Precipitation in any form (fog with vis of 1 mile or less, mist, rain, snow, sleet, and ice crystals or clouds in flight)

41
Q

If visible moisture is present below 400 feet AGL with OAT 10C or below:

A

Cowls for takeoff

42
Q

If OAT 5C or below and visible moisture present below 400 feet AGL:

A

Wing and cowl for takeoff

43
Q

Do not hold in icing condition with

A

Slats or flaps extended

44
Q

Taxi lights must be switched off when aircraft is

A

Stationary in excess of 10 minutes

45
Q

Min brake cooling time is

A

15 minutes and all BTMS indicators must been green and not increasing

46
Q

CAT II approaches are prohibited when braking action is reported as

A

Less than medium

47
Q

Ops with autopilot engaged is prohibited below 600 feet AGL except:

A

For visual and non precision approaches (400 feet AGL)
For precision approaches (80 feet AGL)

48
Q

For precision approaches, the minimum height for autopilot use with one engine operating is

A

110 feet AGL

49
Q

Max taxi and ramp weight

A

75,250
85,000

50
Q

Max takeoff weight

A

75,000
84,500

51
Q

Max landing weight

A

67,000
75,100

52
Q

Max zero fuel weight

A

62,300
70,750

53
Q

Max APU starting altitude

A

37,000 feet

54
Q

Max APU operating altitude

A

41,000 feet

55
Q

MEL Categories A

A

Varies

56
Q

MEL Categories B

A

3 days

57
Q

MEL Categories C

A

10 days

58
Q

MEL Categories D

A

120 days

59
Q

Differed MX Class 1

A

10 days max

60
Q

Differed MX Class 2

A

30 days max

61
Q

Max AC Electrical load on Engine or APU driven generator

A

40

62
Q

Max DC Electrical load on each TRU

A

120

63
Q

Max time at TOGA power on 2 engines

A

5 minutes

64
Q

Max ITT for engine start on ground

A

120 C

65
Q

Max ITT for engine start in flight

A

90 C

66
Q

Min oil pressure at idle

A

25 PSI

67
Q

Min oil pressure at TO power

A

45 PSI

68
Q

Min fuel for go around per wing with airplane level and assuming max climb attitude of 10* nose up

A

600 lbs

69
Q

Operation w autopilot engaged is prohibited below __ except with approaches

A

600 AGL

70
Q

Min altitude for autopilot for visual and non-precision approaches

A

400 AGL

71
Q

Min altitude for autopilot for precision approaches

A

80 AGL

72
Q

Min altitude for autopilot on single engine precision approach or approaches with vertical guidance

A

110 AGL

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