Extra EA 500 - Page 203

Pilot’s Operating Handbook Section 5
EXTRA 500 Performance
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
2000
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
-9
11 41
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
204
198
238 133
35
208 202 238 133
35
213 208 238 133
35
90
202
196
234
131
35
206 200 234 131
35
211 206 234 131
35
85
196
192
224 125
33
200 196 224 125
33
206 202 224 125
33
80
191
187
214 120
32
195 191 214 120
32
201 197 214 120
32
75
186
182
204 114
30
190
186 204
114
30
196
191 204 114
30
70
181
177
194 108
29
185 180 194 108
29
190 186 194 108
29
65
175
171
184 103
27
179 175 184 103
27
185 180 184 103
27
60
170
165
175
98 26
173 168 175
98 26
179 173 175
98
26
55
164
159
167
93 25
167 162 167
93 25
172 166 167
93
25
50
157
152
158
88 23
160 155 158
88 23
165 159 158
88
23
45
150
144
150
84 22
153 147
150
84 22
157 150
150
84
22
(*
) 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).
Figure 5-8
Cruise Performance (Sheet 2 of 14)
26. January 2011
5-25