Limitations Flashcards
Maximum Takeoff Tailwind Component (AFM)
15 kts
Maximum Landing Tailwind Component (AFM)
15 kts
Maximum Operating Altitude (ft)
41,000
Maximum Takeoff and Landing Altitude (ft)
8,400
Minimum Takeoff and Landing Temperature
-54°C
Maximum operating limit (speed)?
Observe Vmo/Mmo and Gear/Flap Placards
Severe Turbulence Penetration Target Speed
280 kts/.76M (whichever is lower)
With either one or both engine BLEED air switches ON, do not operate air condition in HIGH for ______.
Takeoff, approach, or landing
The engine anti-ice system must be ON during all ground and flight operations when icing conditions exist or are anticipated, except ___.
Engine anti-ice must be ON prior to and during descent _______.
Except during climb and cruise below -40C SAT.
In all icing conditions, including temperatures below -40C SAT
(MAX) Engine anti-ice must be turned ______ when not in actual or anticipated icing conditions
OFF
Do not engage autopilot below _______ on takeoff
1,000 ft AGL (AFM/ASA)
For single channel operation during approach, the autopilot shall not remain engaged below _______.
50 ft AGL (AFM)
For manually flown HGS AIII approach, the autopilot shall not remain engaged below ______
500 ft AGL
Use of aileron trim with autopilot engaged is ________
Prohibited (AFM)
Warm-up:
Engines must be operated for a minimum of _______ prior to takeoff.
3 minutes (ASA)
Cool-down:
Engines must be operated at or near idle (taxi thrust acceptable) for a minimum of ________ prior to shutdown.
3 minutes (ASA)
Maximum Time Limit for Takeoff Thrust
5 Minutes
(10 minutes allowed in the event of the loss of thrust on one engine during takeoff)
ENGINE START switches must be in the CONT position for:
Takeoff
Landing
Anti-ice operation
Operation in hail, sleet or moderate to heavy rain
ENGINE START switches must be in the FLT position for:
Operation in severe turbulence
Minimum Oil Temperature before setting takeoff thrust
31C (MAX)
Intentional selection of reverse thrust in flight is
Prohibited
APU LOAD
Bleed and Electric Load
10,000 ft
APU LOAD
Bleed Only
17,000 ft
APU LOAD
Electric Only
41,000 ft
APU LOAD
Maximum Operating Altitude
41,000 ft
Ensure APU BLEED air switch is closed for _______ after start and for ______ prior to shutdown
2 minutes
1 minute
NOTE: When the APU switch is moved to OFF, the time delay is met automatically.
Maximum Flap Extension Altitude
20,000 ft (AFM)
Holding in icing conditions with flaps extended is
Prohibited (AFM)
Do no deploy speed brakes in flight below
1,000 ft AGL
In flight, do not extend the SPEED BRAKE lever beyond
the FLIGHT DETENT (AFM)
Do no deploy speed brakes with more than
Flaps 10 Extended
(Although not prohibited, the use of speed brakes with Flaps 1-10 extended should be avoided as much as possible. The use of speed brakes with flaps extended increases loads on the trailing edge flaps, resulting in increased wear and tear)
Manually overriding the Load Alleviation System is
Not authorized
Minimum fuel temperature
-37c unless actual fuel freeze point is known.
Allowable lateral imbalance between main tanks 1 and 2 must be scheduled to be ______. Fuel imbalance must not exceed ________ for _____, _____, ______ or _______
Zero
1,000 lbs
Taxi, takeoff, flight or landing
Main Wing Tanks must be scheduled to be ______ if the Center Tank contains more than ______
Full
1,000 lbs
For ground operations, Center Tank FUEL PUMP switches must not be positioned to ON unless ____, except when defueling or transferring fuel.
Center Tank Fuel Pumps must not be on unless ____.
Center Tank fuel quantity exceeds 1,000 lbs
Personnel are available in the flight deck to monitor LOW PRESSURE lights.
Center Tank Fuel Pumps must not be ______ unless personnel are available in the ________ to monitor __________
ON
Flight Deck
FLOW PRESSURE lights
For ground and flight operations, the corresponding Center Tank Fuel Pump switch must be positioned OFF when _____. If the Center Tank is empty, position both Center Tank FUEL PUMP switches to ___.
The LOW PRESSURE light illuminates
OFF
Ground operation of electric hydraulic pump requires minimum _________ in the respective fuel tank.
1,675 lbs
Except for engine start, the APU bleed valve must be closed when another source is pressurizing ____.
Left blead air duct
The APU bleed valve may be open during engine start, but avoid engine power _____.
Above idle
