Limitations Flashcards
FUEL
Release
4,000 pounds
FUEL
Hot Spare
8,500 pounds
FUEL
Emergency
1,500 pounds
Runway for Release
Dry 5000 FT
Width 75 FT
Slope +-2%
Runway
Ops Review Required if
Dry Less than 5500 FT
Wet/Contaminated
Less than 6300 FT
Exception to Runway Requirements Airport
Anguilla
4472 FT
CP approval
Baggage Compartment
Weight Limit
900 pounds
Spoilers min altitude
300 FT
FUEL
45 minute IFR Reserve
2500 pounds
Minimum Takeoff Temp Limit
-40•C
Maximum Takeoff/Landing
Temp Limit
ISA + 35
Max # of pax
14 including lap babies because of # O2 masks
AC Generator Load Limits
Altitude
Altitude
0 to 35,000 FT……30 kVA
Above 35,000 FT…..25 kVA
DC TRU Load Limit
Max continuous: 100 A
FUEL JETTISON
Flap setting 0•
Do not jettison fuel in known lighting conditions
Auxiliary Tank Fuel Load Restrictions
If Aux tank has 500 pounds or less, Takeoff is permitted if each wing tank has at least 1,500 pounds and
Tail tank is empty
If Aux tank has more than 500 pounds refer to chart on Pg 9-7 on AOM
Fuel Transfer
Must be off for takeoff
During normal operations, do not use tail transfer to control CG, selector must remain on Auto mode
Do not manually transfer tail tank with more than 7,000 pounds in the aux tank
Engine Limitations
Above 40,000 FT select one air-conditioning unit or cowl anti-ice for each engine
Left and right engine N2 must be within 2% at ground idle power
Cold-soaked -30•C or colder for more than 8 hours
Motor engine for 60 seconds n verify fan rotation before engine start
Test TR until deploy n stow cycles are less than 5 seconds
Engine starter limitations
3 consecutive engine starts cycles with 5 minutes cooling between additional cycles
Auto throttle limitations
Do not use ATS
During OEI
Go arounds Manually set thrust to override ATS
If RA is unavailable or invalid disengage ATS prior to 100 FT AGL
If Flaps are selected to less than 45 disengage ATS prior to 100 ft AGL
Auto throttle limitations
Do not use ATS
During OEI
Go arounds Manually set thrust to override ATS
If RA is unavailable or invalid disengage ATS prior to 100 FT AGL
If Flaps are selected to less than 45 disengage ATS prior to 100 ft AGL
Dry motor
Ignition off and Thrust Lever shutoff.
90 secs on. 5 off
30secs on. 5 off
30 secs on 5 off
LnR engine N2 must not differ by more than 2% at ground idle
2%
Cold soaked ac in -30 degrees Celsius or lower for more than 8 hours
Motor for 60 seconds n very fan rotation before engine start
Thrust reverser check cycle less than 5 seconds
