Extra EA 400 - Page 210

Section 5 Pilot’s Operating Handbook
Performance EXTRA 500
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
16000
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
-3
7
-17
13
T
R
Q
F
UE
L FLOW
FUE
L
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
KTA
S
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
90
227
222
221 123
33
85
222
217
211 118
31
227 222 211
118
31
80
217
211
200 112
30
222 216 200 112
30
75
211
205
188 105
28
216
210 188 105
28
70
205
199
176
99 26
210 203 176
99 26
217 209 176
99
26
65
199
192
165
92 24
203 196 165
92
24
210 202 165
92
24
60
192
185
153
86 23
196 189 153
86 23
202 194 153
86
23
55
185
177
142
80 21
189 181 142
80 21
194 186 142
80
21
50
177
169
132
74 20
180 172 132
74 20
186 177 132
74
20
45
168
160
123
69 18
171 163 123
69 18
176 168 123
69
18
(*
) 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 9 of 14)
5-32 26. January 2011