Limitations Flashcards

1
Q

Max Crosswind for take off and landing normal

A

27 kts

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2
Q

Max crosswind for CAT II approach

Max Headwind for CAT II approach

A

15kts crosswind and 16kt headwind

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3
Q

Max tailwind for take off and landing

A

10th

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4
Q

Max operating alt

A

FL410

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5
Q

Max pressure alt for t/o and landing

A

8000ft

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6
Q

Max temp for t/o and landing

A

ISA +35

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7
Q

Max alt for single pack ops

A

FL310

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8
Q

Max severe turbulence speed

A

280kts/ M.75 which ever is lower

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9
Q

Max gear extension speed

A

220

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10
Q

Max gear extended speed

A

220

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11
Q

Max gear retraction speed

A

200

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12
Q

Max windshield wiper speed

A

250kts

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13
Q

Max tire speed for CR7 and CR9

A

CR7 is 182 and CR9 is 195

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14
Q

Flap extension speeds

A

Flaps 1- 230kts
Flaps 8- 230kts
Flaps 20-220kts bold text
Flaps 30- 185kts
Flaps 45- 170

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15
Q

Min temp to start APU

A

-40C

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16
Q

APU starter duty cycle

A

No more than 3 starts in 1 hour, respecting 2 min delay between start attempts

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17
Q

Max APU start altitude

A

FL370

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18
Q

Max APU bleed air use

A

FL250

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19
Q

Max alt to starter assisted in flight engine start using APU bleed air

A

FL210

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20
Q

Scenario: APU door will not close. What limitations apply?

A

Speed limited to 220kts or APU must remain in operation

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21
Q

Max APU and engine gen AC load

A

40kVA to FL410

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22
Q

Max continuous load on TRU

A

120A

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23
Q

On the ground with DC power only. What time limitation is in play and why?

A

5 min only and because of CRT display cooling

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24
Q

During engine start do not exceed 75% N1 until…

A

For 2 minutes or until all operating indications are in the normal range, whichever is longer

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25
Q

How long do the engines need to be at idle before shutdown?

A

2 minutes at or near idle, taxi time counts towards this

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26
Q

Max ITT for ground start?

A

815C

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27
Q

Normal Take off power and maximum power is limited to how long?

A

5 minutes

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28
Q

What is considered to be a cold soak airplane?

A

FFOD, plane exposed to -30C or below for more than 8 hours

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29
Q

Minimum oil pressure when at take off power?

A

45 psi minimum

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30
Q

When is continuous ignition required?

A

T/O and landing on contaminated runways
T/O with 15kt or greater crosswind
Mod or heavier rain
Mod or heavier turb
Vicinity of TS

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31
Q

Starter Cranking limits?

A

1: 90 seconds on 10 seconds off
2: 90 seconds on 10 seconds off
3+: 90 seconds on 5 min off

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32
Q

When is Max thrust reverse prohibited and when must they be idle?

A

Thrust reversers must be below max below 75kts and idle by 60kts

33
Q

Flex Take off limitations

A

Anti skid must be operative
Prohibited if:
Contaminated runways
De iced
Wing and cowls on
Wind shear
Engine cannot achieve full power
Required by SID

34
Q

Max slats/flaps alt?

A

15000ft and cannot be used enroute.

35
Q

Minimum speed for spoilers, minimum alt for spoilers

A

VREF +10 and 1000ft agl

36
Q

Max fuel imbalance for T/O? And for all other phases

A

300lbs for T/O and 800lbs for all other phases of flight

37
Q

Total Pressure refueling

A

19,594lbs

38
Q

Total gravity refueling 700

A

14,580lbs

39
Q

Total gravity refueling 900

A

14,810lbs

40
Q

Powered and gravity crossflow must be…

A

off for take off

41
Q

Minimum fuel for go around per wing tank?

A

600lbs

42
Q

Take off with engine fuel temps below what are prohibited?

A

temperature below 5*C

43
Q

Minimum braking cooling time

A

15 minutes and all BTMS must be green and not increasing

44
Q

APU door not closed or unknown…

A

220kts or APU must remain in operation

45
Q

Maximum ITT for engine start in flight

A

90*C

46
Q

Minimum oil pressure at idle

A

25psi

47
Q

Minimum oil pressure at take off power

A

45psi

48
Q

EMER DEPRES is prohibited above what alt?

A

15000ft

49
Q

Low Pressure must be removed prior to…

A

MCD closed

50
Q

APU min temp for start?

A

-40*C

51
Q

Max Oil Pressure engine start

A

182psi

52
Q

Max oil pressure during normal ops

A

95psi

53
Q

If an engine is cold soaked, how long to dry motor?

A

60 seconds and must see n1 rotation

54
Q

What is considered Ground contamination?

A

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

55
Q

What is the definition of visible moisture?

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.

56
Q

What Braking action prohibits a CAT II approach?

A

Less than medium

57
Q

RVSM Required Equipment:

A

Autopilot with altitude hold
Altitude alerting system
Altitude reporting transponder (2) one must be operational
Air data computer (2)

58
Q

What is the max RVSM speed?

A

0.82M

59
Q

Auto pilot limits:

A

600ft unless:
Visual or non precision= 400ft
Precision approach or approached with vertical guidance= 80ft (CR7 3.5 to 4.0 and AFE less than or equal to 4000ft is 120ft. If its greater than 4000ft AFE its prohibited.)

60
Q

Maximum positive differential psi?

A

8.7psi

61
Q

When oil temp transient is <60*C what is the maximum pressure?

A

156psi

62
Q

Can you do an ILS approach with a glide path greater than 4.0 in a CR7?

A

no it is prohibited greater than 4.0 degrees

63
Q

Can you do an ILS approach with a glide slope greater than 3.5 in a CR9?

A

no it is prohibited greater than 3.5 degrees.

64
Q

What is the minimum alt for AP during single engine on a precision approach or APV?

A

110ft agl

65
Q

Can you use speed mode during an approach?

A

NO

66
Q

Can you use VNAV during the climb?

A

no

67
Q

When can you use VNAV?

A

during approach when using LPV or LNAV/VNAV minimums only

68
Q

CR7 maximum taxi and ramp weight

A

75,250lbs

69
Q

CR7 Maximum Take off weight

A

75,000lbs

70
Q

CR7 Maximum Landing weight

A

67,000lbs

71
Q

CR7 Maximum zero fuel weight

A

62,300lbs

72
Q

CR7 Minimum flight weight

A

42,000lbs

73
Q

CR9 Maximum Taxi and Ramp weight

A

85,000lbs

74
Q

CR9 Maximum Take off weight

A

84,500lbs

75
Q

CR9 Maximum Landing weight

A

75,100lbs

76
Q

CR9 Maximum Zero fuel weight

A

70,750lbs

77
Q

CR9 Minimum flight weight

A

45,000lbs

78
Q
A