Extra EA 500 - Page 205

Pilot’s Operating Handbook Section 5
EXTRA 500 Performance
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
6000
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
-1
7
3
3
3
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
210
205
232 130
34
214 210 232 130
34
221 216 232 130
34
90
208
203
228 127
34
212 208 228 127
34
219 214 228 127
34
85
203
198
217 121
32
207
203
217 121
32
213
209
217
121
32
80
198
193
207
116
31
202 198 207 116
31
208 204 207 116
31
75
192
188
196 110
29
197 192 196 110
29
203 198 196 110
29
70
187
183
186 104
28
191 187 186 104
28
197 192 186 104
28
65
182
177
176
99 26
186 181 176
99 26
191 186 176
99
26
60
176
171
167
93 25
180
174 167
93 25
185 179 167
93
25
55
169
164
158
88 23
173 167 158
88 23
178 171 158
88
23
50
162
156
149
84 22
166 159 149
84 22
170 163 149
84
22
45
155
148
141
79 21
158 151 141
79 21
162 155 141
79
21
(*
) 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 4 of 14)
26. January 2011
5-27