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Pilot’s Operating Handbook Section 5
EXTRA 500 Performance
CRUISE PERFORMA
NCE
PRESSURE ALTITUDE
22000
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
-4
9
-2
9
1
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
70
217
210
176
98 26
65
210
202
165
92 24
215 207 165
92 24
60
203
195
152
85 23
207 199 152
85 23
214 204 152
85
23
55
195
186
140
78 21
199 190 140
78 21
205 195 140
78
21
50
186
177
128
72 19
190 181 128
72 19
196 186 128
72
19
45
176
168
117
65 17
180 171 117
65 17
185 176 117
65
17
40
166
158
107
60
16
170 161 107
60 16
175 166 107
60
16
(*
)
Pr
opeller 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 12 of 14)
26. January 2011
5-35

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