737 Memory Limitations (and a couple more) Flashcards
Operating Pressure Altitude
Maximum
41,000 feet
Maximum Takeoff/Landing Tailwind Component
Maximum
15 Knots
Recommend Severe Turbulence Penetration Speed
Cruise
TURB N1 setting from cruise page
Recommend Severe Turbulence Penetration Speed
Climb and Descent
280 Knots / .76 Mach
Takeoff Crosswind Component
Blended/Scimitar
Runway Condition Code 6
34/33
Landing Crosswind Component
Blended/Scimitar
Runway Condition Code 6
40/37
Takeoff Crosswind Component
Blended/Scimitar
Runway Condition Code 5
25/25
Landing Crosswind Component
Blended/Scimitar
Runway Condition Code 5
40/37
Icing Conditions Exist On The Ground And For Takeoff When:
Outside Air Temperature is
10 degrees C or below
Icing Conditions Exist In Flight When:
Total Air Temperature is
10 degrees C or below
Autopilot Minimum Engagement Height
On takeoff or missed approach, do not engage the autopilot below:
400 feet AGL
Autoland - Maximum Winds
Headwind
25 Knots
Autoland - Maximum Winds
Crosswind
15 Knots
Autoland - Maximum Winds
Tailwind (flaps 30 and 40)
10 Knots
Autoland - Maximum Winds
Flaps 30 (-900[401-412])
Field elevation 4000 ft or less - 10 knots
Field elevation 4001-6000 ft - 5 knots
Field elevation 6001 ft and above - 0 knots
Minimum Altitude for Use of Autopilot on Approach
ILS/GLS coupled approaches (no autoland)
50 ft AGL
Minimum Altitude for Use of Autopilot on Approach
Non-precision approaches
50 ft below MDA/DA
Autoflight Parameters
LVL CHG on Approach
Do not use LVL CHG on final approach below 1000 ft AFE
Battery voltage for APU start
Minimum
23 Volts
Minimum oil pressure for takeoff
NG
MAX
13 PSI NG
17.4 PSI MAX
Start attempt limited to __ minutes NG and __ minutes MAX
2
3
APU Maximum Altitude
APU bleed and electrical
APU bleed
APU electric load
10,000 ft
17,000 ft
41,000 ft
Engine oil quantity
Minimum prior to engine start
70%
APU warmup
Operate APU for __ minute(s) before using APU bleed air
1 minute
APU shutdown
Wait a minimum of __ seconds for APU shutdown cycle to complete, then turn battery switch to OFF.
120 seconds
Maximum flap extension altitude
20,000 ft
Maximum allowable in-flight difference between CA and FO altitude displays for RVSM operation is __ ft.
200 ft
Fuel imbalance
Must not exceed 1000 lbs
Hydraulic Quantity
Maximum
Minimum for dispatch
105%
Above RF
Tire Groundspeed maximum
NG
MAX
195 knots
204 knots
4 No Go Lights
EEC
PSEU
ELEC
Display Failure
When do you put the Eng Start Switch to Flight
Severe Turbulence
Tiller gives you how much turning
Rudder give you how much
Which has priority
78
7
Tiller
Speed Window
A
8
A = Under speed
8 = Over speed
LNAV and VNAV engage at what altitudes
LNAV 50 ft
VNAV 400 ft
Bingo fuel
Current Fuel - burn to destination - ALT fuel - FAR reserve
Holding fuel in lbs / burn per hour x 60 = holding time available
Flaps 1&2 United limit speed
240kts
Flaps 5 United limit speed
230kts
