Limitations Flashcards
Max tailwind component:
Takeoff/Landing: 15 kts
Max operating altitude:
41,000ft
Max takeoff and landing altitude:
8400ft
Minimum takeoff and landing temperature:
-54c
Maximum Operating speed Limit:
Observe Vmo/Mmo and Gear/Flap placards
Severe turbulence penetration speed:
280 kts or .76M (whichever is lower)
Do NOT operate air conditioning packs in HIGH with either or both engine bleed air switches
ON for takeoff, approach, or landing
When must Engine anti-ice be on??
Engine Anti-Ice must be ON when icing conditions exist or are anticipated (on the ground or in flight)
EXCEPT during climb or cruise below -40°C SAT and prior to and during descent in ALL icing conditions,
including below -40°C SAT.
A/P must be disengaged:
a. Below 1000ft AGL on takeoff
b. Below 50ft AGL on single channel approach
c. Below 500ft AGL on manually flown HGS AIII approach NO AILERON TRIM with autopilot
engaged.
Warm up/ Cool time (near idle):
3 Min
Max time limit for takeoff thrust:
5 minutes* *10 minutes if single engine after takeoff
ENGINE START switches must be in CONT position for:
a. Takeoff
b. Landing
c. Anti-ice operation
d. Hail, sleet,
e. Or moderate to heavy rain
ENGINE START switches must be in FLT position for:
severe turbulence.
Minimum oil temperature before setting takeoff thrust:
a. MAX only +31°C,
b. No limit for NG
c. Reverse thrust is prohibited inadvertently in flight.
. APU is limited in the following load configurations:
APU is limited in the following load configurations:
a. Bleed & Electric: 10,000ft
Bleed Only: 17,000ft
Electric Only: 41,000ft
16. Max Operating Altitude:
a. FL410
The APU BLEED AIR switch must be CLOSED
a. 2 minutes after start and
b. 1 minute before shutdown (although turning the switch off meets this time limit automatically)
Avoid power above idle with the APU bleed valve open.
APU bleed valve must be CLOSED when another source is pressurizing L bleed air duct.
Max altitude for flap extension:
20,000ft
HOLDING w/ flaps in icing
PROHIBITED
Speed Brakes:
a. No speed brakes below 1,000ft AGL
b. Do NOT move lever past FLT detent in flight (shouldn’t allow you to anyways)
c. No speed brakes with flaps beyond flaps 10
Manually override the Load Alleviation System.
Dont do it
Minimum fuel temperature:
-37°C (unless actual fuel freeze point is known).
Fuel imbalance
must be scheduled to be zero
No more than 1,000lbs imbalance for taxi, takeoff, flight, or landing
Main tanks must be FULL with more than
1,000lbs in center tank.
Center tank fuel pumps must be OFF
with less than 1,000lbs in tank (except for defueling or
transferring fuel).
unless someone is in the flight deck to monitor fuel
when low pressure light illuminates (under 1000lbs)
or the tank is empty.
Ground operation of electric hydraulic pump requires
minimum 1675 in respective fuel tank
