Piper ARCHER III Pilot Operating Handbook page 155
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PA-28-181,
ARCHER
III
SECTION
5
PERFORMANCE
Engine
/
Cruise Performance
for Non-ISA OAT*
RPM
for
Constant
557o
Power
Fuel
Flow:
Best
Economy
Mixturer
S.2
GPH
Pressure
Alritude
Feet
Indicated Outside
Air
Temperature
OC
OC
OF
Engine
Speed
RPM
True
Air
Speed
Knots
**
Sea
Level
ISA-I5
ISA
ISA
+10
ISA
+20
ISA
+30
0
15
25
35
45
32
59
77
95
113
2245
2265
2275
2285
2295
105
106
2000
ISA
-I5
ISA
ISA
+IO
ISA
+20
ISA
+30
-4
il
2t
3l
4t
25
52
70
88
106
2265
2280
2295
2305
2315
106
101
4(XX)
ISA
-I5
ISA
ISA
+10
ISA
+20
ISA
+30
-8
7
17
21
JI
18
45
63
8l
99
2285
2300
2315
2325
2335
106
108
6000
ISA
-15
ISA
ISA
+10
ISA
+20
ISA
+30
-12
3
13
23
-t-t
10
37
55
IJ
9t
2305
2320
2330
2345
2355
107
108
8000
ISA
-15
ISA
ISA
+10
ISA
+17.5
-16
-1
9
r6.5
.,
30
48
62
2320
2340
2350
2360
107
108
9000
ISA
-I5
ISA
ISA
+8.5
-18
--t
5.5
0
27
42
2330
2350
2360
107
108
10000
ISA
-
15
ISA
20
-5
-4
23
2340
2360
101
108
NOTE:
*
Aircraft
weight
2550
Lbs., Wheel
pants and strut
fairings installed
**
Subtract
3
KTAS
if
wheel
pants
are
removed.
ENGINE/CRUISE PERFORMANCE
(55
Vo)
Figure
5-21
REPORT:
VB-2749
5-21
ISSUED:
December 22,
2017
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