FCOM General Flashcards
Do not hold in icing conditions with …
… flaps extended
When side window icing is observed …
suspect SLD icing. Wing and engine A/I must be on. Leave icing conditions asap
Engine A/I on the ground when …
OAT <= 10C and (visible moisture visible in any form (vis <=1sm, rain, snow, sleet, ice crystals)) or (when operating on ramps, taxiways, runways where surface snow, ice, standing water or slush is present)
Icing conditions in flight exist when …
TAT <= 10C to SAT>= -40C and visible moisture in any form is present.
In flight the engine A/I must be on when …
… flying in icing conditions or when ICE DETECTED CAS message is on.
The wing A/I system must be ON for ground operations (including T/O) when …
… OAT<=5C and (visible moisture in any form is present (fog <=1 sm vis, rain, snow, sleet or ice crystals)) or (when operating on ramps, taxiways or runways where surface snow, ice, standing water or slush is present.
The wing A/I system must be on in flight when …
…flying in icing conditions (and < 210KIAS) or ICE DETECTED CAS message is on.
Operations with a glide path angle of ? degrees or greater are prohibted?
GPA > 4.5 degrees prohibited for AP elevations below 3,000’ - for higher AP elevations max GPA decreases down to 4.2 at 10,000’
Min flight crew
pilot and copilot
Max ramp weight
39,000 lbs
Max TOW
38,850 lbs
Max ZFW
27,200 lbs
MLW - Max certified landing weight
33,750 lbs
Min Flight Weight
23,100 lbs
V(MO) up to 8,000’
300 KIAS
V(MO) for 8,001’ to 29,475’
320 KIAS
M(MO) above 29,745’
.83 MI
V(RA) Rough air penetration
265 KIAS / .75 MI
V(LO, RET)
200 KIAS
V(LO, EXT)
250 KIAS
V(LE)
250 KIAS
V(FE) Max flap extended speeds
Flaps 10 …… 210 KIAS
Flaps 20 …… 210 KIAS
Flaps 30 …… 175 KIAS
Max tire speed (GS)
182 kts
Max T/O and landing pressure altitude
10,000’
Max tailwind component
10kts
T/O and Landings are limited to … rwys
paved
Max runway slopes
2% uphill and -2% downhill
T/O is prohibited with xxx adhering to yyy
Takeoff is prohibited with frost, ice, snow, or slush adhering to any critical
surface (wings, horizontal stabilizer, vertical stabilizer, control surfaces or
engine inlets).
Frost adhering to underside of the wing caused by cold soaked fuel or upper surface of the fuselage.
Max Pressure Altitude
45,000’
Maneuvering Load Factors
Flaps up 2.6g < load < -1.0g
Flaps extended 2.0g < load < 0.0g
Operation with Type II, III or IV anti-icing fluid on the ground, …
The wing A/I must only be selected ON (if required), just before thrust increase for takeoff
Max temp for T/O?
ISA + 35C
Min temp for T/O?
-40C
