* Memory Items * Flashcards Preview

United 737 > * Memory Items * > Flashcards

Flashcards in * Memory Items * Deck (17)
Loading flashcards...
1
Q

Max operating pressure altitude

A

41,000 feet

2
Q

Max takeoff/landing tailwind component

A

15 kts

3
Q

Recommended Severe Turbulence Penetration Speed:

Cruise

A

Turb N1 setting from cruise page

4
Q

Recommended Severe Turbulence Penetration Speed:

Climb and Descent

A

280 kts/.76 Mach

5
Q

Takeoff Crosswind Component (knots) blended winglet/split scimitar winglet:

Dry rwy:

A

33/34

Assumes an engine failure RTO

6
Q

Takeoff Crosswind Component (knots) blended winglet/split scimitar winglet

Wet rwy:

A

25/25

Assumes an engine failure RTO

7
Q

Landing Crosswind Component (knots) blended winglet/split scimitar winglet:

Dry rwy:

A

40/37

Reduce landing crosswind guidelines by 5kts on wet or contaminated runways when asymmetric reverse thrust is used

8
Q

Landing Crosswind Component (knots) blended winglet/split scimitar winglet:

Wet rwy:

A

40/37

Reduce landing crosswind guidelines by 5kts on wet or contaminated runways when asymmetric reverse thrust is used

9
Q

Icing conditions exist on the ground and for takeoff when:

A

OAT 10°Cor below

And

  • visible moisture in any forms present (I.e. Clouds, fog with visibility of 1 mile or less, rain, snow, sleet, or ice crystals) OR
  • while operating on ramps,taxiways, or runways where snow, standing water or slush may be ingested by the engines or freeze on the engines, nacelles, or engine sensor probes.
10
Q

Icing conditions exist in flight when:

A

Total Air Temp is 10°C or below

AND

  • visible moisture in any form is present ( i e clouds, fog with visibility of 1 mile or less, rain, snow, sleet, or ice crystals)
11
Q

On takeoff or missed approach, do not engage autopilot below:

A

800 ft

12
Q

Auto land max headwind:

A

25 kts

13
Q

Auto land max crosswind:

A

15 kts

14
Q

Auto land max tailwind (flaps 30 and 40):

A

10 kts

-900[401-412] Flaps 30:

Field elevation 4000 ft or less: 10 kts

Field elevation 4001-6000 ft: 5 kts

Field elevation 6000 ft and above: 0 kts

15
Q

Minimum altitude for use of autopilot on approach

ILS/GPS coupled approach (no auto land):

A

50 ft AGL

16
Q

Minimum altitude for use of autopilot on approach

Non precision approaches:

A

50 feet below MDA

17
Q

Maximum flap extension altitude:

A

20,000 ft