Extra EA 500 - Page 209

Pilot’s Operating Handbook Section 5
EXTRA 500 Performance
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
14000
FEET
Conditions
: Landing gear
and f
l
aps
UP
2030 RPM(
*)
-
BLEED 2
20
C
BELOW
ST
ANDA
RD
30
C
ABO
VE
ST
A
NDA
RD TEM
P
T
EM
PER
AT
URE ST
ANDA
RD TEM
P
-3
3
-13
17
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
225
220
225 126
33
90
223
218
221 124
33
228 224 221 124
33
85
218
213
211 118
31
223 218 211 118
31
80
213
208
200 112
30
218 212 200 112
30
75
207
202
189 105
28
212 206 189 105
28
219 213 189 105
28
70
201
196
177
99 26
206 200 177
99 26
213 206 177
99
26
65
195
189
166
93 24
200 193 166
93 24
206 199 166
93
24
60
189
182
155
87 23
193
186 155
87 23
199 191 155
87
23
55
181
174
145
81
21
185 178 145
81
21
191 183 145
81
21
50
174
166
135
75 20
177 170 135
75 20
182 174 135
75
20
45
165
158
125
70 19
169 161 125
70 19
173 165 125
70
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 8 of 14)
26. January 2011
5-31