Limits Flashcards
Max Tailwind Component -Takeoff
15 Knots
Max Tailwind Component - Landing
15 Knots
Max Operating Altitude
41,000
Max T/O and Landing Altitude
8,400
Min. T/O and Landing Temperature
-54C
Severe Turbulence Penetration Speed
Lesser of 280 Knots or .76M
Autopilot must be disengaged:
Below 1000’ AGL on T/O
Below 50’ AGL single channel appr.
Below 500’ AGL manual Cat3a HGS
Engine warm-up/cool-down:
3 minutes
Max time using T/O thrust
2 engines: 5 min
1 engine: 10 min
Engine Start switches must be in Cont:
Take-off
Landing
Anti-ice operations
Hail, sleet, moderate to heavy rain
Engine Start switches must be in FLT:
Sever Turbulence
Minimum oil temp for T/O thrust:
NG - none
Max - 31C
Reverse thrust prohibited:
In flight
APU Bleed and Electric load limit:
10,000 ft
APU bleed only load limit
17,000 ft
APU electric load limit:
41,000 ft
APU max Operating altitude
41,000’
APU bleed switch must be closed for _ min after start
2 min
APU bleed switch must be closed for _ min. before shutdown
1 min
Avoid power above _ with the APU bleed air valve open
Idle power
When another source is pressurizing the L Duct, the APU bleed switch must be _
Closed
Max Flap extension Altitude:
20’000 ft
Minimum Altitude for speed brake:
1000 ft
Max Flap setting for use of the speed brake:
10 degrees
Minimum Fuel temperature:
-37C
Max fuel imbalance for taxi, take-off and Landing:
1000 lbs
Unless main tanks are _ , center tanks limited to _
Full
1000 lbs
Center tanks pumps must be off unless:
Pilot on flight deck
<1000 lbs in tank(unless fueling or tx)
No low press light
Min fuel quantity in respective tank for electric hydraulic pump operation:
1675
