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LCA > Limitations > Flashcards

Limitations Flashcards

1
Q

Minimum flight crew

A

One Captain and one First Officer

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2
Q

Maximum crosswind component for takeoff and landing

A

27 knots

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3
Q

Maximum crosswind component for landing from a Category II Approach

A

15 knots

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4
Q

Maxximum headwind component for landing from a Category II Approach

A

16 knots

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5
Q

Maxximum tell when component for takeoff and landing

A

10 knots

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6
Q

Maximum runway slope approved for takeoff and landing

A

+2.0% uphill
-2.0% downhill

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7
Q

Maximum Runway width approved for takeoff and landing

A

100 feet

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8
Q

Maximum operating altitude

A

41,000 ft

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9
Q

Maximum pressure altitude for takeoff and landing

A

8,000 feet

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10
Q

Maximum ambient temperature for takeoff and landing

A

ISA +35°C limited to a maximum OAT of 51°C

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11
Q

Minimum ambient temperature approved for takeoff

A

-40°C

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12
Q

Maneuvering limit load factors – Flaps Retracted

A

-1.0 to +2.5 G

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13
Q

Maneuvering load limit factor – Flaps Extended

A

0.0 to +2.0 G.

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14
Q

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

A

50 knots

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15
Q

Maxximum positive differential pressure

A

8.7 psi

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16
Q

Maximum negative differential pressure

A

-0.5 psi

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17
Q

Maximum pressure differential during ground maneuvering

A

0.1 psi

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18
Q

Maximum differential pressure during initial landing (at touchdown):

A

1.0 psi

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19
Q

Maximum altitude for single pack operation

A

31,000 ft.

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20
Q

Aircraft doors limitation for low pressure air or pressurized Cabin

A

Low pressure air must be off prior to the main cabin door being closed and secure, and the airplane must be completely D pressurized prior to opening any of the airplane doors

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21
Q

To preclude possible crew, and/or passenger ear damage, use of the__________ switch off of 15,000 feet is prohibited.

A

EMER DEPRESS

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22
Q

Maximum severe turbulence penetration speed

A

280 KIAS/.75M, whichever is lower.

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23
Q

Maximum gear extension speed

A

220 KIAS

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24
Q

Maxximum gear extended speed

A

220 KIAS

25
Q

Maximum gear retraction speed

A

200 KIAS

26
Q

Maximum airspeed for windshield wiper operation

A

250 KIAS

27
Q

Maximum airspeed for windshield wiper operation failed in the non-parked position

A

250 KIAS

28
Q

Maxximum cruise MACH in RVSM airspace

A

0.82 M

29
Q

Tire limit ground speed, <CR7></CR7>

A

182 KIAS

30
Q

Tire limit groundspeed, <CR9></CR9>

A

195 KIAS

31
Q

Flaps 1 Vfe

A

230 KIAS

32
Q

Flaps 8 Vfe

A

230 KIAS

33
Q

Flaps 20 Vfe

A

220 KIAS

34
Q

Flaps 30 Vfe

A

185 KIAS

35
Q

Flaps 45 Vfe

A

170 KIAS

36
Q

Minimum temperature for cold-soaked APU starting on the ground:

A

-40°C

37
Q

APU starter motor duty cycle limitation

A

No more than three (3) starts/start attempts in one (1) hour with a two (2) minute delay between cranking attempts.

38
Q

Maximum APU RPM

A

106%

39
Q

Maximum APU starting altitude

A

37,000 feet

40
Q

Maximum APU Operating Altitude

A

41,000 feet

41
Q

Max APU temperature for Ground, Flight, and All Conditions

A

Ground 789°C
Flight 806°C
All Conditions 1038°C

42
Q

Maximum bleed air extraction from the APU is not permitted above__________ for Air-Conditioning.

A

25,000 ft.

43
Q

APU Bleed Air for engine start during ground operations allowed?

A

Each engine may be started using the APU as a bleed air source

44
Q

Maximum altitude for APU Bleed air for engine start during flight

A

21,000 feet or below.

In-flight (MES) Main engine start altitude limitation. Not an APU Bleed limitation.

45
Q

APU Display markings on the EICAS

RED

GREEN

A

RED = maximum and minimum limitations

GREEN = normal operating range

46
Q

APU EGT °C GREEN (normal) vs. RED (maximum)

A

GREEN = 0 to 806

RED = greater than or equal to 807

47
Q

APU RPM % GREEN vs. RED

A

GREEN = 0 to 106

RED = greater than or equal to 107

48
Q

APU Door Open Limitation

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

49
Q

APU generator loading altitude limit?
APU altitude starting altitude limit?
APU bleed altitude limit?
APU ground starting altitude limit?

A

APU generator loading limit: 41,000
APU altitude starting limit: 37,000
APU bleed altitude limit: 25,000
APU ground starting altitude limit: 15,000

50
Q

Maximum individual AC generator and loading must not exceed the following values:

A

40kVA

0 to 41,000 feet main generator (each), APU generator

51
Q

Maximum continuous load on each TRU?

(DC electrical system load) (in-flight)

A

120 amps

52
Q

Maximum permissible time for ground operations with DC power only is__________. To protect the Flight compartment CRT displays.

A

5 minutes

53
Q

AMBER engine limit display marking on EICAS

A

Caution range

54
Q

During all starts, do not exceed 75% N1 until….

A

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

55
Q

Operate engines at or near idle for______________ prior to shutdown.

A

2 minutes

56
Q

Taxi time at a stabilize_____________ or below may be credited towards the two-minute cool down period.

A

80% N2

57
Q

RED N1 % rpm

RED N2 % rpm

A

N1 99.5

N2 99.4

58
Q

Oil pressure psi RED

A

0 to 24

LCA (1 decks)

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