Limitations Flashcards
Maximum landing tailwind component is _____ kts.
15
Maximum takeoff tailwind component is _____ kts.
15
Maximum operating altitude is _____.
41,000’
Maximum takeoff and landing altitude is _____ ft.
8400
Maximum Turbulence Penetration airspeed is
280 KIAS/ .76 M
With engine bleed air switches _____ do not operate the air conditioning packs in _____ for takeoff, approach or landing.
ON/ HIGH
Engine TAI must be ON when icing conditions exist or anticipated except during climb or cruise below _____.
-40 degrees SAT
Do not engage the autopilot below _____ AGL on takeoff.
1000’
For single channel ILS operation during approach the autopilot shall not remain engaged below _____ feet AGL.
50’
For manually flown HGS AIII approach, the autopilot shall not remain engaged below _____ AGL.
500’
Use of aileron trim with autopilot engaged is _____.
prohibited.
Operated the engines for a minimum of _____ minutes prior to takeoff.
3
Operate engines at or near idle (taxi thrust acceptable) for a minimum of _____ minutes prior to shutdown.
3
Maximum time limit for Takeoff Thrust assuming normal takeoff with both engines operating is _____ minutes.
5
Maximum time limit for Takeoff Thrust in the event of loss of engine thrust during takeoff is _____ minutes.
10
ENGINE START Switches must be in the CONT position for _____. (3 answers)
takeoff, landing, anti-ice operation
Maximum start EGT is _____ degrees.
725
ENGINE START Switches must be in the FLT position for _____.
operation in severe turbulence.
Minimum engine start pressure at sea level is _____ psi.
30
Engine Starter Duty Cycle (normal starts) - limit each start attempt to a maximum of _____.
2 minutes.
Intentional use of reverse thrust in flight is _____.
prohibited.
Maximum altitude for APU operation with electrical loads is _____ feet.
41,000
Maximum altitude for APU operation with bleed loads only is _____feet.
17,000
Maximum operating altitude for the APU is _____ feet.
41,000
Maximum altitude for APU operation with both bleed and electrical loads is _____ feet.
10,000
Close the APU bleed valve when _____. (3)
Ground air connected and isolation valve open
Engine No 1 Bleed Valve open with No 1 engine running
Isolation Valve and Engine No 2 Bleed Valve open with Engine No 2 running
Maximum flap extension altitude if _____ feet.
20,000
Do not deploy speed brakes in flight at radio altitudes less than _____ feet.
1000
Random fuel imbalance must not exceed _____ lbs for taxi, takeoff, flight, or landing.
1000
Minimum fuel temperature is ______ unless actual fuel freeze point is known.
-37 degrees C
(Ground Operation) DO NOT turn Center Tank Fuel pumps ON unless center tank fuel quantity exceeds _____ lbs except when refueling or transferring fuel.
1000
Operating Electric Hydraulic Pumps on the ground requires a minimum of _____ lbs of fuel in the respective tank.
1675
