Extra EA 400 - Page 207

Pilot’s Operating Handbook Section 5
EXTRA 500 Performance
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
10000
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 T
E
M
P
T
EM
PER
A
T
URE ST
ANDA
RD TEM
P
-2
5
-5
2
5
T
R
Q
F
UE
L FLOW
F
UE
L FLOW
F
UE
L FLOW
%
K
T
AS
K
T
AS
L
B/HR
L/HR
G
AL/HR
KTAS KTAS
LB/HR L/HR
GA
L/HR
KTA
S
KTAS
LB/HR
L/HR
G
AL/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
217
212
229 128
34
222 217 229 128
34
90
215
211
225 126
33
220 215 225 126
33
85
210
206
214 120
32
215 210 214 120
32
222 217 214 120
32
80
205
200
203 113
30
210 205 203 113
30
216 211 203 113
30
75
200
195
192
107
28
204 199 192 107
28
211 205 192 107
28
70
194
189
181 101
27
198 193 181 101
27
205 199 181 101
27
65
188
183
170
95 25
192 187
170
95 25
198 192
170
95
25
60
182
176
160
89 24
186 180 160
89 24
192 185 160
89
24
55
175
169
150
84 22
179 172 150
84 22
184 177 150
84
22
50
168
161
141
79 21
171 164 141
79 21
176 169 141
79
21
45
160
153
132
74
20
163 156 132
74
20
168 160 132
74
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
p
lay
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 6 of 14)
26. January 2011
5-29