Extra EA 400 - Page 204

Section 5 Pilot’s Operating Handbook
Performance EXTRA 500
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
4000
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
3
7
3
7
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
207
201
234 131
35
211 206 234 131
35
217 212 234 131
35
90
205
200
230 129
34
209 204 230 129
34
215 210 230 129
34
85
199
195
220 123
33
204 199 220 123
33
210 205 220 123
33
80
194
190
210
117
31
198 194 210 117
31
204 200 210 117
31
75
189
185
200 112
30
193
189 200
112
30
199
195 200 112
30
70
184
180
190 106
28
188 184 190 106
28
194 189 190 106
28
65
178
174
180 101
27
182 178 180 101
27
188 183 180 101
27
60
173
168
171
96 25
176 171 171
96 25
182 176 171
96
25
55
166
161
162
91 24
170 164 162
91
24
175 169 162
91
24
50
160
154
154
86 23
163 157 154
86 23
168 161 154
86
23
45
152
146
145
81 21
155
149 145
81 21
160
153 145
81
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)
.
Figure 5-8
Cruise Performance (Sheet 3 of 14)
5-26 26. January 2011