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650 > 0. Limits > Flashcards

0. Limits Flashcards

1
Q

Taxi/Ramp

A

48,300

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2
Q

T/O

A

48,200

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3
Q

Landing

A

38,000

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4
Q

Max PA for T/O and L

A

10,000

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5
Q

Max Operating

A

41,000

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6
Q

Max OAT for T/O and L

A

ISA + 35

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7
Q

Min OAT for T/O

A

-40C

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8
Q

Max Runway Slope

A

+/- 2%

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9
Q

Max Tailwind

A

10kts

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10
Q

Max crosswind to use revers thrust

A

24kts

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11
Q

Enroute use of flaps

A

Prohibited

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12
Q

Max altitude with flaps extended

A

15,500

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13
Q

> FL250 at least 1 piot must wear a

A

safety harness

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14
Q

Max gear extend or retract speed

A

197kts/M.6

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15
Q

Max speed for gear down and locked

A

250kts/M.7

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16
Q

Max alt gear down

A

20,000

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17
Q

Tire limit

A

182

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18
Q

Turbulence penetration

A

280 kts/M. 75

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19
Q

Max RVSM cruise speed

A

.83

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20
Q

Max N2 split on ground

A

2%

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21
Q

Flaps 20

A

231

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22
Q

Flaps 30

A

197

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23
Q

Flaps 45

A

189

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24
Q

Pressure Refueling (for gravity)

A

reduce by 7%

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25
Q

Left (Right) Main

A

4860

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26
Q

Aux

A

7168

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27
Q

Tail

A

3112

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28
Q

Total

A

20,000

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29
Q

Max Imbalance between wing tanks

A

800 Cruise/400 Taxi-T/O-Ldg

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30
Q

T/O with <=500 lbs in aux tank permitted, provided that…

A

> = 1500 lbs fuel in each wing tank, and 0 in tail tank

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31
Q

Min Fuel for go-around

A

500 lbs per wing with max 10 degrees NU attitude.

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32
Q

Fuel jettison with…

A

flaps 0 and no lightning

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33
Q

Min engine fuel temp for T/O

A

5 degrees C

34
Q

Bulk fuel temp must remain…

A

above fuel freezing point in flight and be 10 degress C above fuel freezing point on T/O

35
Q

Bleed air 10th stage valves must be closed for T/O and ldg

A

if eng cowl and/or wing a/ice selected on

36
Q

If above 40,000 ft,

A

one ACU or cowl anti-ice must be selected on for each engine.

37
Q

Max AC Gen Loading

A

0-20,000 ft 30 Kva (Main and APU)
20,000-35,000 30 Kva (Main only)
>35,000 ft 25 Kva (Main only)

38
Q

Max load on TRUs

A

100 Amps

39
Q

During ground operation at ambient temps > 40C…

A

operation of electrical /avionics equipment must be limited to 30 mins unless at least one ACU is operating and the passenger door is closed.

40
Q

Continuous Engine Ignition req’d:

A

(CCMMT)

  • T/O and ldg on Contaminated runway
  • T/O with high Crosswind component
  • Flight through Moderate or heavier intensity rain
  • Flight through Moderate or heavier intensity turbulence
  • Flight in vicinity of Thunderstorm
41
Q

Maximum Contamination Depths

A

Standing water .25 Takeoff .5 Land
Slush .25 Takeoff .5 Land
Wet Snow .5 Takeoff 1 Land
Dry Snow 1.2 Takeoff 2.4 Land

42
Q

Taxi&Landing Lights

A

The taxi lights must be selected off whenever the airplane is stationary. During prolonged taxiing, the nose landing lights may be used in place of the taxi lights, if necessary, at the pilot’s discretion. The left and right landing lights must be selected OFF during taxi or when the airplane is stationary. The left and right landing lights must not be used on the ground except for the take-off and landing roll.

43
Q

Minimum altitude for autopilot use:

A

Take-Off 320, Visual/Non-precision 320, Precision (GP<=3.5 degrees) 80, Precision (GP > 3.5 degrees) 160

44
Q

APU Min temp for start

A

-40C

45
Q

APU Max Alt for in-flight start

A

<= 20,000 ft

46
Q

APU Max Speed for in-flight start and operations

A

290 kts

47
Q

APU Max altitude for bleed air extraction

A

<=15,000 ft

48
Q

In-Flight Eng start with APU–>dble eng fial only

A

<=15,000 ft

49
Q

Engine start during ground ops

A

SL-15,000 ft

50
Q

If both engines started with APU, max N2 for operating engine

A

70%

51
Q

APU Start Cycles - Attempt 1,2, & 3

A

30 SEC, followed by 20 mins OFF

52
Q

APU Start Cycles - Attempt 3 and 4

A

15 SEC, followed by 35 mins OFF

53
Q

COLD-SOAKED AC > 8 hrs

A

For 1st flight of day @ temp <= -30C, motor engines for 60 sec & verify fan rotation prior to start. Reversers must be actuated until deploy and stow cycles are less than 5 sec.

54
Q

Engine Oil (02-05-16)

A

Max oil consumption 189 ml quarts or .05 US Gals/hr. Eng oil level should be checked 15 mins - 2 hrs after engine shutdown. Engines must be motored if replenishment period exceeded. Max refill allowed is 1.9 liters (2 quarts) without dry-motoring engines. Max duration without oil servicing is 16 operating hours.

55
Q

Steady State Idle (min) oil pressure

A

25 psi

56
Q

T/O Power (min)

A

45 psi

57
Q

Oil Temperature min for start

A

-40C

58
Q

Starter not to be used if N2 is

A

> 55%

59
Q

3 consecutive start cycles with….

A

5 mins cooling between additional cycles

60
Q

Fuel introduction Temp and N2 for ground starts

A

ITT <= 120C, N2 >= 20%

61
Q

Fuel introduction for Air Start with starter

A

ITT <= 90C, N2 >= 28%

62
Q

Fuel introduction for Windmill start 10,000 feet and below

A

N2 >= 10%

63
Q

Fuel introduction for Windmill start above 10,000 feet

A

N2 >= 12%

64
Q

Dry motor attempt 1 max time on and cooling

A

90 seconds, 5 mins off

65
Q

Dry motor attempt 2 (and subsequent) max time on and cooling

A

30 seconds, 5 minutes off

66
Q

During landing, application of max reverse thrust is not permitted at airspeeds below…..

A

60 knots

67
Q

Below 60 KIAS revers thrust must be reduced to

A

60% N1 or less.

68
Q

Backing with reverse thrust is

A

prohibited

69
Q

When must cowl anti ice be used on the ground?

A

When OAT <= 10C and (visible moisture and/or contaminated surface)

70
Q

Tactile check required

A

when OAT <= 5C or wing fuel <= 0C or conditions for frost formation exist.

71
Q

Wing anti-ice must be on for final taxi

A

prior to T/O when OAT <= 5C unless Type II,III, or IV anti-icing fluids have been applied.

72
Q

No single-engine taxi when OAT is

A

<=10C

73
Q

Wing anti-ice must be on for T/O when

A

OAT <= 5C and visible moisture below 400 feet AGL, or any precipitation and/or contaminated surface. If type II,III,IV used, leave off until ready for T/O

74
Q

Single Engine taxi operations are prohibited if the OAT is

A

10C or below.

75
Q

ICING conditions exist in flight when

A

TAT <=10C and visible moisture except when SAT <= -40C.

76
Q

Both Cowl and Wing must be on at or above 22000

A
  • When ice indicated by ice detection systerm, or

- When in icing conditions if the ice detector has failed

77
Q

Below 22000

A
  • When in icing conditions

- When ice is indicated by the ice detection system

78
Q

The FMS must not be used for navigation unless it is receiving suitable navigation from:

A
  • 1 GNSS
  • 2DMES
  • 1 VOR/DME, or
  • 1 IRS
79
Q

RNP operations down to LPV minimum must not be commenced or continued unless

A

all required airborne equipment are operation satisfactorily

80
Q

The required airborne equipment are:

A
  • Dual PFD
  • Two GNSS sensors must be available to commence an approach and one GNSS sensor is required to continue an approach
  • Dual FMC
81
Q

FMS as a supplementary navigation source beyond the FAF is permitted when APPR or REF APPR is annunciated on the PFD if

A

the navigation aid referenced in the approach procedure is displayed and monitored by the flight crew during the approach.

82
Q

GNSS sensors must be deselected when on approach in airspace

A

not referenced to WGS84 or NAD83

650 (19 decks)

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