Engine/Cruise Perform A Nce (55%) - Piper ARCHER III Pilot Operating Handbook

PA-28-181, ARCHER ill
•
Pressure
Altitude
Feet
Sea Level
2000
•
4000
6000
8000
9000
•
10000
NOTE:
**
ISSUED: December 22, 2017
Engine / Cruise Performance for Non-ISA OAT*
RPM for Constant 55 % Power
Fuel Flow: Best Economy Mixture, 8.2 GPH
Indicated Outside Air Temperature
oc
ISA-15
ISA
ISA I IO
ISA +20
ISA +30
ISA -15
ISA
ISA +10
ISA +20
ISA +30
ISA -15
ISA
ISA +10
ISA +20
ISA +30
ISA -15
ISA
ISA +10
ISA +20
ISA +30
ISA -15
ISA
ISA +10
ISA +17.5 16.5
ISA -15
ISA
ISA +8.5
ISA - 15
ISA
*
Aircraft weight 2550 Lbs., Wheel pants and strut fairings installed
Subtract 3 KTAS if wheel pants are removed.

ENGINE/CRUISE PERFORM A NCE (55%)

oc
Of
0 32
15 59
25
77
35 95
113
45
-4
25
I I
52
21 70
31 88
41 106
-8 18
7 45
17 63
27
81
37 99
-12 10
3 37
13 55
23
73
91
33
-16 3
- I 30
9 48
62
-18 0
-3
27
5.5 42
-4
-20
-5 23
Figure 5-2 l
SECTION 5
PERFORMANCE
Engine True Air
Speed Speed
RPM
Knots**
2245 105
2265
2275
2285
2295
106
2265 106
2280
2295
2305
2315 107
2285 106
2300
2315
2325
2335 108
2305
107
2320
2330
2345
2355 108
2320 107
2340
2350
2360 108
2330
107
2350
2360 108
2340 107
2360 108
REPORT: VB-2749
5-21