Piper Cherokee Archer II Pilot Operating Handbook page 76

SECTION 5
PERFORMANCE
PIPER AIRCRAFT CORPORATION
PA·28-1 81. CHEROKEE ARCHER II
PA-28-181
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Example:
Cruise pressure altitude: 5500 ft.
Cruise OAT: 40° F
Percent power: 65%
Engine RPM: 2450 RPM
,
2000
2200 2400
ENGINE SPEED RPM
1600
ENGINE PERFORMANCE (SERIAL NOS. 28-7890001 AND UP)
Figure 5-18
REPORT: VB·790
5-20
ISSUED: JUNE 18, 1976
REVISED: JULY 12, 1977