Tecnam P2008 TC, Flight Manual

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P2008 TC
Flight Manual
A52
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 7.1hrs + 0.5hr RESERVE)
Pressure altitude H
P
:
0
ft
OAT: +15°C
Power
setting
Engine Speed
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
55% 4300 100 3.3 7.1 663
65% 4800 112 4.6 5.0 505
75% 5000 118 5.3 4.3 461
100% 5500 129 6.9 3.2 380
115% 5800 134 8.6 2.4 308
Pressure altitude H
P
:
2000
ft
OAT: +11°C
Power
setting
Engine Speed
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
54% 4300 101 3.2 7.5 695
64% 4800 112 4.4 5.2 527
74% 5000 119 5.3 4.3 466
99% 5500 130 6.8 3.2 391
114% 5800 135 8.5 2.5 320
Pressure altitude H
P
:
4000
ft
OAT: +7°C
Power
setting
Engine Speed
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
52% 4300 102 2.8 8.4 782
62% 4800 113 4.2 5.5 561
72% 5000 119 5.1 4.4 480
97% 5500 130 6.7 3.3 404
112% 5800 135 8.2 2.6 336
Pressure altitude H
P
:
6000
ft OAT: +3°C
Power
setting
Engine Speed
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
(including 30’ reserve)
Range (N.m.)
51% 4300 102 2.7 9.0 837
61% 4800 113 4.1 5.6 578
71% 5000 120 5.1 4.5 492
96% 5500 131 6.6 3.3 412
111% 5800 136 8.0 2.6 346