Extra EA 500 - Page 206

Section 5 Pilot’s Operating Handbook
Performance EXTRA 500
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
8000
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
A
T
URE ST
ANDA
RD TEM
P
-2
1
-1
2
9
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
214
209
230 129
34
218 213 230 129
34
90
212
207
226
126
33
216 211 226 126
33
223 218 226 126
33
85
206
202
215 120
32
211 207 215 120
32
217 213 215 120
32
80
201
197
204 114
30
206 201 204 114
30
212 207 204 114
30
75
196
192
194 108
29
200 196 194
108
29
207 202 194 108
29
70
191
186
183 102
27
195 190 183 102
27
201 195 183 102
27
65
185
180
173
97 26
189 184 173
97 26
195 189 173
97
26
60
179
173
163
91 24
183 177 163
91 24
188 182
163
91
24
55
172
166
154
86 23
176 170 154
86 23
181 174 154
86
23
50
165
159
145
81 21
169 162 145
81
21
173 166 145
81
21
45
157
151
136
76 20
160
153
136
76 20
165
157
136
76
20
(*
) 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 5 of 14)
5-28 26. January 2011