Other Limitations Flashcards

1
Q

Takeoff/Landing Pressure Altitude

Maximum

A

10,000 feet

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2
Q

Runway Slope

Maximum

A

+/- 2%

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3
Q

Runway Width

Normal

Narrow

Minimum

A

148 feet wide or greater

Less than 148 feet but not less than minimum runway width

100 feet

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4
Q

Maximum Airspeed

VMO

MMO

A

Indicated by max airspeed pointer on airspeed indicated

.82 Mach

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5
Q

Maximum Airspeed

Maximum gear retraction speed

Maximum gear extension speed

Maximum gear operating/extended speed

A

235 knots

270 knots/.82 Mach

320 knots/.82 Mach

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6
Q

Flap Speeds

1
2
5
10
15
25
30
40
A
250
250
250
210 or 205 (9ER)
200 or 195 (700)
170, 190, 195
165-180
156-171
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7
Q

QFE Altimetry

A

Pilots are prohibited from operating with a QFE altimeter setting selected.

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8
Q

VA is defined as:

A

the speed above which maneuvers involving full application of rudder, ailerons, or elevator, or maneuvers involving angles of attack near stall, should be avoided

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9
Q

Minimum Ground Time After Landing

Steel brakes

Carbon brakes

A

67 minutes

48 minutes

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10
Q

Portable Oxygen Bottles

Minimum

A

At least one for each assigned flight attendant

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11
Q

Pressurization

Maximum cabin pressure differential

Maximum differential pressure for takeoff and landing

A

9.10 PSI

.125 PSI

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12
Q

Duct Pressure

Maximum cooling

A

20-25 PSI

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13
Q

When engine bleeds are on (either one or both), do not:

A

operate air conditioning packs in high for takeoff, approach, and landing

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14
Q

Duct Pressure For Two Pack Operation From One Bleed Source

Minimum

Do not operate more than _____ from one engine.

A

20-25 PSI

one pack (MAX, applies only on the ground)

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15
Q

Engine Anti-Ice

Must be ON during all ground operations, including after landing, when:

Must be ON during all flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below:

Must be ON prior to and during descent in:

Engine ignition must be selected to ____ prior to and during engine anti-ice operation.

A

icing conditions exist or are anticipated.

-40°C SAT

all icing conditions, including temperatures below -40°C SAT

CONT

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16
Q

Wing Anti-Ice

Use wing anti-ice during all operations between engine start and takeoff when:

Do not operate wing anti-ice on the ground when the OAT is above:

Do not use wing anti-ice as a substitute for:

Use of wing anti-ice above approximately ____ may cause ____ and possible loss of cabin pressure.

A

icing conditions exist or are anticipated, unless the aircraft is or will be protected by the application of Type II or Type IV fluid.

10°C/50°F

ground deicing/anti-icing

FL 350, bleed trip off

17
Q

Autolandings

Autoland capability may only be used to runways at or below:

The ILS autoland capability may only be used with flaps ____ and ____ with both ____ operative.

Maximum and minimum glideslope angles for autoland are :

The autoland system shall not be used for:

Autolands with the ____ as Pilot Flying are not authorized.

A

8400 feet pressure altitude.

30, 40, engines

3.25° and 2.5°

overweight landings.

First Officer

18
Q

Wi-Fi System

Do not operate the KA GND TX ENABLE switch in the OVERRIDE position or the WIFI COMM ENABLE/BROADBAND SYSTEM switch in the ON position during:

A

deicing, when maintenance is being performed in the vicinity of the WiFi radome, or in a hangar

19
Q

Battery Voltage For APU Start

Minimum

A

23 volts

20
Q

Engine Ignition

Ignition must be on for:

A

Takeoff, Landing, Engine anti-ice operation, Heavy rain

21
Q

Engine Oil Pressure

Oil pressure must be in the normal range for takeoff.

Minimum

A

13 PSI, 17.4 (MAX)

22
Q

Engine Oil Temperature

Minimum starting (MAX)

Minimum takeoff (MAX)

Maximum

A

-40°C

31°C

155°C