Maximum Take-off Mass: 62 800 kg,
Maximum Zero Fuel Mass: 51 250 kg;
Maximum Landing Mass: 54 900 kg,
Maximum Taxi Mass: 63 050 kg,
Assume the following preplanning results:
Trip fuel: 1 800 kg,
Alternate fuel: 1 400 kg,
Holding fuel (final reserve): 1 225 kg,
Dry Operating Mass: 34 000 kg,
Traffic Load: 13 000 kg,
Catering: 750 kg,
Baggage: 3 500 kg.
Find the Take-off Mass (TOM):
A: 52 265 kg.
B: 55 765 kg.
C: 51 425 kg.
D: 51 515 kg.
A: the minimum enroute altitude (MEA) is 3500 ft
B: the minimum obstruction clearance altitude (MOCA) is 3500 ft
C: the airway base is 3500 ft MSL
D: the airway is a low level link route 2100 ft – 3500 ft MSL
B: VFR followed by IFR
C: IFR followed by VFR
A: 30 minutes holding 1,500 feet above aerodrome B
B: 30 minutes holding 2,000 feet above aerodrome B
C: 15 minutes holding 2,000 feet above aerodrome A
D: 30 minutes holding 1,500 feet above aerodrome A
A: the trip fuel to the destination aerodrome is to be calculated via the suitable enroute alternate.
B: the trip fuel to the destination aerodrome is to be calculated via the decision point.
C: a destination alternate is not required.
D: the fuel calculation is based on a contingency fuel from departure aerodrome to the decision point.
A: 700 kg
B: 1000 kg
C: 800 kg
D: 500 kg
A: N4135 E00415
B: 41(degrees)35′ N 04(degrees) 15’E
Distance from departure to destination:260 NM
Safe Endurance:4,1 h True Track:150
W/V: 100/30 TAS: 110 kt
What is the distance of the PSR from the departure point?
A: 213 NM
B: 154 NM
C: 107 NM
D: 47 NM
A: X = (D/2) + GSr / (GSo + GSr)
B: X = D x GSo / (GSo + GSr)
C: X = (D/2) x GSo / (GSo + GSr)
D: X = D x GSr / (GSo + GSr)