Limits

Question 1

Max operating altitude

Answer 1

41,000’

Question 2

Max T/O and landing Pressure altitude

Answer 2

10,000’

Question 3

Min runway width

Answer 3

100’

Question 4

Max T/O and landing tailwind component

Answer 4

15 kts

Question 5

Recommended severe turbulence penetration speed

Answer 5

Cruise - TURB N1 setting from the cruise page
Climb and Descent - 280 kts / .76 Mach

Question 6

Recommended crosswind component guidelines

Answer 6

Runway code 6 (dry) blended winglet/Split Scimitar
- Takeoff 34/33
- Landing 40/37

Runway code 5 (Good) blended/split
-Takeoff 25/25
- Landing 40/37

Question 7

Icing conditions exist on ground and for Takeoff when:

Answer 7

OAT is 10° C and below and:
-visible moisture in any form is present (rain, sleet, snow, ice crystals, or vis less than 1 sm)
- While operating on ramps, taxiways, or runways where snow, standing water, or slush may be ingested by the engines

Question 8

Icing conditions exist when:

Answer 8

TAT is 10°C or below and:
- visible moisture is present

Question 9

Autopilot min engagement height

Answer 9

400’ AGL

Question 10

Autoland max winds

Answer 10

Headwind 25kts
Crosswind 15 kts
Tailwind 10 kts

Question 11

Min altitude for use of autopilot on approach

Answer 11

ILS/GLS coupled approaches (no autoland) - 50’ AGL
Non-precision approaches - 50’ below MDA/DA

Question 12

Autoland limitations

Answer 12

•Max pressure altitude - 8400’
•ILS autoland may only be used with flaps 30 and 40 with both engines operative
• Max glide slope angle 3.25°, min glide slope angle 2.5°
• Shall not be used for overweight landings

Question 13

Do not use LVL CHG below:

Answer 13

1000’ AFE

Question 14

In all cases other than autoland the autothrottle must be disconnected no lower than:

Answer 14

50’AGL

Question 15

Max flaps extension altitude

Answer 15

20,000’

Question 16

MMO

Answer 16

.82 Mach

Question 17

Max gear retraction speed
Max gear extension speed
Max gear extended speed

Answer 17

235 knots
270 kts / .82 mach
320 kts / .76 mach

Question 18

Max cabin pressure differential

Answer 18

9.1 PSI

Question 19

Max differential pressure for T/O and landing

Answer 19

.125 PSI

Question 20

Window heat must be on for how many minutes before T/O

Answer 20

10

Question 21

Min battery voltage for APU start

Answer 21

23 volts

Question 22

Engine starter duty cycle

Answer 22

Multiple consecutive starts are permitted.
Each start attempt is limited to 2 min
A min of 10 sec is required between starts

Question 23

APU max altitude

Answer 23

Bleed and electrical 10,000’
Bleed 17,000’
Electrical 41,000’

Question 24

Min engine oil quantity prior to engine start

Answer 24

70%

Question 25

APU starter duty cycle

Answer 25

for both ground and air 15 min cooling is required after 3rd attempt

Question 26

APU warmup required for use of APU bleed air

Answer 26

NG - 1 min
Max - 2 min

Question 27

APU shutdown

Answer 27

wait a min of 2 min for APU shutdown cycle to complete, then turn battery switch OFF

Question 28

Speed Brake operation limits

Answer 28

• In flight do not extend speed brakes past the FLIGHT DETENT
• In flight do not extend speed brakes beyond ARMED detent with flaps 40 selected
• Do not deploy speed brakes at less than 1000’ RA

Question 29

Do not operate weather radar when:

Answer 29

Within 50 of a fuel spill or within 15 feet of people except in test mode

Question 30

Random fuel imbalance must not exceed

Answer 30

1000 lbs

Question 31

Max tire ground speed
NG
Max

Answer 31

NG 195 kts
Max 204 its