Tecnam P2008 - Cruise; Balked Landing

45
4.9 Cruise
Maximum takeoff weight = 600 kg (1320 lbs)
Fuel tanks 2x52 liters (13.7 gal) (less the unusable fuel = 1.1gal)
ALL ENDURANCE DATA (HOURS AND n.m.) ARE GIVEN WITH A RESERVE OF 30’
(FOR EXAMPLE: THE FIRST ROW INDICATES A RANGE OF 5.8hrs + 0.5hr RESERVE)
Pressure altitude H
P
: 0 ft OAT: +15°C
Engine
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
55%
4600
96
4
5.8
552
65%
5000
102
4.8
4.8
490
75%
5200
108
5.3
4.3
470
Pressure altitude H
P
: 2000ft OAT: +11°C
Engine
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
55%
4600
98
4
5.8
4.8
4.4
564
508
482
65%
5000
106
4.8
73%
5200
109
5.2
Pressure altitude H
P
: 4000 ft OAT: +7°C
Engine
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
55%
4600
101
4
5.8
581
60%
5000
105
4.5
5.1
537
70%
5200
110
4.9
4.7
516
Pressure altitude H
P
: 6000 ft OAT: +3°C
Propeller
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
55%
5000
104
4
5.8
598
60%
5200
108
4.5
5.1
552
Pressure altitude H
P
: 8000 ft OAT: -0.8°C
Propeller
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
55%
5150
99
4
5.8
569
58%
5200
102
4.3
5.3
546
Pressure altitude H
P
: 10000 ft OAT: -5°C
Propeller
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
55%
5200
100
4
5.8
575
Pressure altitude H
P
: 12000 ft OAT: -9°C
Propeller
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
50%
5200
98
3.7
6.2
609
4.10 Balked Landing
RATE OF CLIMB: BALKED LANDING