Limitations Flashcards
(29 cards)
Takeoff and landing wind limits
Max takeoff tailwind component (AFM) - 15 knots
Max landing tailwind component (AFM) - 15 knots
Max altitudes (AFM)
Maximum operating altitude (ft) - 41,000 ft
Maximum takeoff and landing altitude - 8400 ft
Minimum takeoff and landing temperature =
-54°C.
Operating speeds
Maximum operating limit (AFM) -
Severe turbulence penetration target speed -
observe Vmo/Mmo and gear/flap placard speeds
280 KIAS/.76M (whichever is lower)
With either one or both engine bleed air switches on, do not operate air conditioning packs at 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 _________.
Engine anti-ice must be on prior to and during descent in _________________, including ______.
are anticipated except during climb and cruise below -40°C SAT.
In all icing conditions, temperatures below -40°C SAT.
Do not engage the auto pilot below _____.
For single channel operations during approach, the autopilot ____________.
For manually flown HGS AIII Approach, the autopilot shall not remain engaged _________.
Use of aileron trim with autopilot engaged _________.
1000 feet AGL on takeoff (AFM/ASA)
shall not remain engaged below 50 ft AGL.
below 500 ft AGL.
is prohibited (AFM)
Maximum time limit for takeoff thrust -
5 minutes (10 minutes is allowed in the event of a lost thrust on one engine during takeoff.
Engine ignition (AFM/ASA)
Engine start switches must be in the CONT position for:
-Takeoff
-Landing
-Anti-ice operation
-Operations 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
NG - none
Max - 31°C
Intentional selection of reverse thrust in flight:
Is Prohibited
APU load limits (AFM)
Bleed and electrical load – 10,000 ft
Bleed only – 17,000 ft
Electric only - 41,000 ft
Max operating altitude – 41,000 ft
Ensure APU bleed air switch is closed for _____ minutes after start and for ___ minute prior to shut down
2 minutes after start, 1 minute prior to shutdown.
Note: when the APU switch is moved to off, this time delay is met automatically
APU bleed valve may be _____ during engine start, but avoid engine power above _____
Open during engine start, avoid power above idle.
Except for ________, the APU bleed valve must be closed when another source is pressurizing the ______ bleed air duct
Engine start, LEFT
Maximum flap extension altitude is:
20,000 ft (AFM)
Holding in icing conditions with the flaps extend is:
Prohibited (AFM)
Do not deploy speed breaks in flight below_______
In-flight, do not extend speed brake lever beyond__________
Do not do not deploy speed breaks with more than _________
1000 Ft AGL
The flight detect
Flaps 10 Extended
Load alleviation system 700W/900ER
Manually overriding the load alleviation system is not authorized.
Minimum fuel temperature is _________
-37°C unless actual freeze point is known.
Allowable imbalance between main tanks 1 and 2 must be scheduled to be __
0.
Fuel imbalance must not exceed ______ pounds for taxi, takeoff, flight or landing.
1000 lbs
Main and Wing tanks must be scheduled to be _____ if the center tank contains more than ______
Full, 1000 lbs
