BCSX Limitations
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Cartes-fiches
Engine Near Idle is defined as ____ % N1
40
According to Operational Guidance 8.01.01 Aircraft is considered to be "COLD SOAKED" when it has been at an ambient temperate of ___°C or below for more than ___ consecutive hours, without having performed the recommended procedures for preventing cold soak.
-7 8
Ice Shedding procedure: Advance Thrust Levers to a minimum of ___ % N___
60 N1
ICE SHEDDING heavy Snow conditions exist whe. visibility is ____ m or less
400
Takeoff from ____ runways must be with ____ Thrust
contaminated TO
after Landing on contaminated Runway, do not ____ ____ .
retract flaps
in wich icing conditions is operation prohibited?
supercooled large droplet icing
The maximum airport pressure altitude for autoland is (feet)
8466
Maximum wind for passenger and cargo door operation
Do not operate the passenger and cargo doors with winds at the door of more than ___ kts. Do not keep doors open when wind gusts are more than ___ kts.
40 65
Maximum altitude loss during a go‐around from an autoland approach with two engines is approximately __ feet. On aver- age, a __ feet-altitude loss is expected.
50 25
Maximum altitude loss during a go‐around from an autoland approach with one engine is approximately __ feet. On aver- age, a __ feet-altitude loss is expected.
100 30
APPR 2 (no autoland) Approach glideslope angle: ____ to ____
2.5 3.5
LAND 2 (autoland) Approach glideslope angle: ____ to ____
2.5 3.25
APPR 2 (no autoland) Runway Slope ___% upslope, ___% downslope
2.0 2.0
LAND 2 (autoland) Runway Slope ___% upslope, ___% downslope
0.8 1.0
APPR 2 (no autoland) min Runway width
30
Land 2 (autoland) min Runway width
45
ASA displays highest capability between ____(ft) and ____(ft)
1500 800
Retard armed (ft)
400
ALIGN arm, FLARE arm from ____ ft to ____ ft
350 250
ALIGN active from ____ to _____
200 150
FLARE active, Rollout arm at ____ ft
65
RETARD active at ft
20
ROLLOUT active WW + ___ seconds
2
Rollout is removed at ___ kts
30
Thrust Limitation at Low Speed (TLLS) limits the thrust of the engines to approximately ___% of the takeoff power. As the aircraft accelerates in the takeoff run, thrust increases with airspeed and reaches full power at ____ kt.
60 80
APPROACH IDLE is avtive when:
aircraft descends below _____ ft RA
or
when F___ is selected
or
when the_____ is down
400 4 gear
Minimum oxygen dispatch pressure with 2 crew members in cockpit (whilst flying over mountainous terrain)
950
Minimum oxygen dispatch pressure with 3 crew members in cockpit (whilst flying over mountainous terrain)
1300
Minimum height with flight spoilers manually extended is ____ft AGL.
300
Minimum speed with flight spoilers manually extended is VREF + ____ KIAS.
10
BTMS range green? format: XX-XX
00-06
BTMS range white? format: XX-XX
07-14
BTMS range red? format: XX-XX
15-20
Takeoff allowed with BTMS in _____ ranging from which values?
format: (colour) XX-XX
white 07-09
