Extra EA 500 - Page 208

Section 5 Pilot’s Operating Handbook
Performance EXTRA 500
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
12000
FEET
Conditions
: Landing gear
and f
l
aps
UP
2030 RPM(
*)
-
BLEED 2
20
C
BELOW
ST
ANDA
RD
30
C
ABO
VE
ST
ANDA
RD TEM
P
T
EM
PER
AT
URE ST
ANDA
RD TEM
P
-2
9
-9
2
1
T
R
Q
F
UE
L FLOW
FUEL
FLOW
FUEL
FLOW
%
K
T
AS
K
T
AS
L
B/HR
L/HR
GA
L/HR
KTAS KTAS
LB/HR L/HR
GA
L/HR
KTAS KTAS
LB/HR
L/HR
GA
L/HR
WEI
G
H
T
3900
4696
LB
S
3900 4696
LB
S
3900 4696
LB
S
1769
2130
KG
1769 2130
KG
1769 2130
KG
92
221
216
227 127
34
226 221 227 127
34
90
219
214
223 125
33
224 219 223 125
33
85
214
209
213 119
31
219 214
213 119
31
80
209
204
201 113
30
214 209 201 113
30
220 215 201 113
30
75
203
198
190 106
28
208 203 190 106
28
215 209 190 106
28
70
198
192
179 100
26
202 197 179
100
26
209 202 179 100
26
65
192
186
168
94 25
196 190 168
94 25
202 195 168
94
25
60
185
179
157
88 23
189 183 157
88 23
195 188 157
88
23
55
178
172
147
82 22
182 175 147
82 22
188 180 147
82
22
50
171
164
138
77
20
174 167 138
77 20
179 171 138
77
20
45
162
155
129
72 19
166 158 129
72 19
170 162 129
72
19
(*
) Propeller RPM utilz
ation betw
een 1900 and 2030 RPM is
pos
s
i
ble wi
thout changing
per
f
o
rm
anc
e. Dis
play
the T
R
Q
indicated in table w
i
th N2 = 2030 RPM, then reduc
e N2
w
i
thout r
e
s
e
tting pow
er
lever
(
w
ithin lim
its per
m
i
tted by
tor
que).
Indic
ates
per
f
o
rm
anc
e outs
ide the engine lim
itations
.
Data is
pr
ovided f
o
r extr
apolation pur
pos
es
.
Figure 5-8
Cruise Performance (Sheet 7 of 14)
5-30 26. January 2011