BCSX Limitations
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Flashcards
BCS3 maximum usable fuel load (kg) left/right main
3050
BCS1 maximum usable fuel load (kg) center tank
11480
BCS3 maximum usable fuel load (kg) center tank
11300
BCS1 maximum usable fuel load (kg) total
17640
BCS3 maximum usable fuel load (kg) total
17400
minimum fuel quantity for go-around is ___ kg per wing, maximum bank angle ___° and maximum aircraft climb attitude of ____ degrees nose up
442 0 10
maximum bulk fuel temperature for starting and operating (°C)
52.5
take off perhibited with bulk fuel temperature below (°C)
-37
UNATTENDED APU Operation is prohibited, if either wind tank quantity is greater than _____ kg
2830
When operating on ground, the left engine must be started first, if any wing tank fuel quantity indication is greater than ____ kg
2830
ON GROUND: Manual fuel transfer must be done, if either wing tank fuel quantity is greater that ____ kg and center tank fuel quantity is less than _____ kg
2830 10670
BTMS digits green range from __ to __
0 6
BTMS digits white range from __ to __
7 14
landing gear maximum BTMS temperature for gear retraction: BTMS digit __ and decreasing
10
VSD Vertical Situation Display is for _______ only
advisory
DO not select ____ from the naviagtion databas
TACAN
Individual flight plan leg or between aircraft position and the TO waypoiunt must not exceed
RNAV-1, RNP-1 (NM)
200
Individual flight plan leg or between aircraft position and the TO waypoiunt must not exceed
RNAV-2, RNP-2 (NM)
400
Individual flight plan leg or between aircraft position and the TO waypoiunt must not exceed
RNP-4 (NM)
500
Individual flight plan leg or between aircraft position and the TO waypoiunt must not exceed
RNP-10 (NM)
500
FMS navigation of latitudes north of ___°N and south of ___°S is prohibited
73 60
To avoid giving unwanted alertsm the TAWSm TERR switch must be selected to INHIB for takoff or landing within ___1 NM of an airport not containied in the TAWS databse
15
When proceeding onto the departure runway do not exceed ___ knots ground speed or ____% N1 until within ____ degreees on the runway heading
35 55 10
Engine Type: Pure Power _______
PW1524G
Engine Start prohibited, if Engine Oil temperature below ___°C
-40
Engine Maximum N1 Setting: Idle, if temperate < ___°C and >= ___°C
-40 -6
Engine Maximum N1 Setting: 30% N1, if temperate < ___°C and >= ___°C
-6 21
Engine Maximum N1 Setting: 50% N1, if temperate < ___°C and >= ___°C
21 49
Engine Maximum N1 Setting: no limit if temperate >= ___°C
49
Engine max EGT all power settings except max continuous (°C)
1054
Engine max EGT max continuous (°C)
1016
Engine max continous oil temperate all thrust settings °C
163
Maximum time for thrust setting max takeoff (min) AEO
5
Maximum time for thrust setting max takeoff (min) OEI
10
Minimum Engine oil temperature for takeoff
49
Engine max peak oil temperate all thrust settings is ____ °C for ____ max minutes
174 20
thrust reversers mmust be cycled a minimum of ___ times before takoff on wet or contaminated runways, if the airplane is cold-soaked at an ambuent temperature of ____ °C or below for more than _____ hours
2 -20 8
Engine Start, after ____ start attempts, or after ____ minutes of continous cranking, a ___ minute cooling period is required
3 4 30
Do not engage the starter on ground if indicated N2 RPM Exceeds ____%
20
Engines must be operated at or near idle for at least ____ minutes (cumulative) before shutdown (recommend ____ minutes)
3 5
