Limitations Flashcards
Maximum tailwind component for takeoff
15 kts
Maximum tailwind component for landing
10 kts (may be authorized up to 15 kts if specified in Ops Advisory page or by F4 message
Severe turbulent air penetration speed
280kts/.76M
Max altitude with flaps extended
20,000ft
Holding in icing condition with flaps extended
Prohibited
Minimum altitude for speed brake deployment
1,000ft RA
3RA-3VM: Speedbrakes cannot be deployed with flaps ____
40 degrees
Limitation on Rapid Flight Control Movements
Avoid rapid and large ALTERNATING control inputs especially in combination with changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA
Reverse Thrust is prohibited
In flight
Aileron trim is prohibited
With autopilot engaged
Minimum altitude for autopilot engagement after takeoff
400ft AGL
Minimum altitude for autopilot engagement during approach
50ft AGL
While autopilot engaged, do not select LVL CHG on final approach below
1000ft AFE
Maximum altitude for APU Bleed Air + Electrical (in flight)
10,000ft
Maximum altitude for APU Bleed Air
17,000ft
Maximum altitude for APU Electrical load
41,000ft
Weather Radar must not be used where?
In a hangar
When must HF Radio not be used?
During refueling operations
Vmo/Mmo
340kts/.82M
Maximum Operating Alititude
41,000ft
Maximum altitude for Takeoff and Landing
8,400ft
Max Crosswind for Takeoff and Land on Dry Runways
3AA-3PX: 33kts
3RA-3VM: 32kts
Anytime passengers are on board,
At least 1 floor level exit must be open or armed
All doors must be armed
On revenue flights
Packs must not be in HIGH when one or both engine bleed air switches ON, and
For takeoff, approach and landing
Maximum cabin differential pressure
9.1psi
Maximum altitude for unpressurized flight following an in flight depressurization
Maximum altitude when aircraft is dispatched for unpressurized flight
14,000ft
10,000ft
Icing Conditions Exist when
OAT on the ground and for takeoff, or TAT inflight is 10 degrees or below and
Visible moisture in any form is present such as clouds, fog with visibility of one mile or less, rain, snow, sleet and ice crystals
OR
When operating in ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze in the engines or nacelles.
Engine ignition must be ____ when operating in icing conditions
ON
Prior to descent in all icing conditions including temperatures below -40C SAT, engine anti-ice must be
ON
Engine ignition for operating in heavy rain
CONT
Minimum oil quantity prior to engine start
3AA-3PX: 12qts
3RA-3VM: 14qts
Maximum allowable on the ground difference between captain and first officer altitude displays for RVSM
50ft (sea level to 5,000ft)
60ft (5,001ft to 10,000ft)
Maximum fuel tank temperature
49 degrees C
Minimum Fuel Tank temperature
-43 degrees C, or 3 degrees above the fuel freezing point temperature limit, whichever is higher
Maximum fuel imbalance
1,000lbs
Main tanks must be full if center tank contains more than
1,000lbs
