Limit Flashcards
Flight Maneuvering load acceleration
Flaps up………………. +2.5 to -1
Flaps down………….. +2 to 0
Maximum takeoff and landing tailwind component
15 knots
Max Operating Alt
41,000
Maximum Takeoff and Landing Alt
8400
Minimum Takeoff and landing temp
-54 C
Maximum Operating Limit Speed
Observe Vmo/Mmo and gear/flap placards
Severe turbulence penetration speed
280/.76 (whichever is lower)
When BLEED air switches are on…
Don’t operate packs in HIGH for takeoff, approach or landing
When icing conditions exist on ground or flight…
Engine Anti-Ice must be on. Except during climb and cruise if it is below -40C SAT. Prior to descent engine anti-ice must be on in icing conditions including temps below -40C SAT.
Do not engage the autopilot below ________ AGL on takeoff
1000 ft
For single channel operation during approach, the autopilot shall not remain engaged below ______ AGL.
50 ft
For manually flown HGS AIII approaches, the autopilot shall not remain engaged below _____ AGL.
500 ft.
Use of _______ ______ with autopilot engaged is prohibited.
Aileron trim
Maximum time limit for takeoff thrust
5 minutes (10 mins if single engine during takeoff)
ENGINE START switches must be in the CONT position for
Takeoff, Landing, Anti-Ice operation, hail, sleet or moderate to heavy rain
ENGINE START switches must be in the FLT position for
Severe turbulence
Minimum oil temp before setting takeoff thrust on the MAX?
31C
Intentional selection of reverse thrust in flight is _________.
Prohibited.
The APU can supply bleed and Electrics up to _________ ft.
10,000
The APU can provide bleed only up to _______.
17,000
The APU can provide electric only up to _______.
41,000
Max operating altitude for the APU?
41,000
Ensure that APU BLEED switch is closed for ___ minutes after start and ___ minute prior to shutdown.
Note: When the APU switch is moved to OFF, this time delay is met mechanically. APU bleed valve may be open during engine start, but avoid engine power above idle. Except for engine start, the APU bleed valve must be closed when another source is pressurizing the left bleed air duct.
2, 1
Maximum flap extension altitude
20,000
Holding in icing conditions with flaps extended is
Prohibited
Do not deploy speed brakes in flight below _____ AGL.
1,000 ft
In flight, do not extend the speed brake lever beyond the _____ detent.
Flight
Do not deploy speed brakes with more than flaps ____ extended.
10
Can you override the LOAD ALLEVIATION SYSTEM?
No
Minimum fuel temperature
-37C (unless fuel freeze point is known)
To operate electric hydraulic pumps on the ground you must have _____ lbs in respective fuel tank.
1675
Center tank fuel pumps must not be on unless…
personnel in flight deck monitor LOW PRESSURE lights.
On ground, center tank FUEL PUMP switches can’t be turned on unless center tank exceeds ______ lbs.
1000 (except when defueling or transferring fuel)
When LOW PRESSURE light illuminates
Center tank fuel pumps must be off. If center tank is empty, position both center tank fuel pump switches to OFF.
Allowable lateral imbalance from Main Tank 1 and 2 must be scheduled to be____.
Zero
Transient fuel imbalance must not exceed ______ lbs for taxi, takeoff, flight, or landing
1000
Main Wing Tanks must be scheduled to be full if ____________.
Center Tank contains more than 1000 lbs.
