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'
7 bs
PIPER AIRCRAFT CORPORATION
PA-28-181, ARCHER Il
SECTION 2.
LIMITATIONS
2.7 POWER PLANT LIMITATIONS
(a)
Number
of Engines
(b)
Engine Manufacturer
(c) Engine Model No.
(d) Engine Operating Limits
(1)
Takeoff Power - 5 Minute
limit (BHP)
(2) Takeoff Engine Speed - 5
Minute Limit (RPM)
(3)
Maximum Continuous Power
(BHP)
(4) Maximum Continuous Engine
Speed (RPM)
(5) Maximum Oi! Temperature
(6)
Oil Pressure
Minimum (red line)
Maximum (red linc)
(7)
Fuel Pressure
Minimum (red line)
Maximum (red line) .
(8)
Fuel (AVGAS ONLY)
(minimum grade)
(9)
Number of Propellers
(10) Propeller Manufacturer
(11) Propeller Model
(12) Propeller Diameter
Minimum
Maximum
(13) Propeller Tolerance (static RPM
at maximum permissible throttle
setting, sea level, ISA)
NOTE
(
t
Lycoming
Q-360-A4M or
0-360-A4A with
carburetor setling
10-3878
180
2700
178
2650
245°F
25 PSI
90 or 100 PSI
0.5 PSI
8 PSI
100 or LOOLL
Aviation Grade
l
Sensenich
T6EMB8S5-0-62
76 IN.
TO IN.
Not above 2340 k. uA
Not below 2240 RPM
Refer to the airplane maintenance manual for test
procedure to determine approved static rpm
under non-standard conditions.
ISSUED: JULY 2, 1979
REVISED: APRIL 2, 1998
REPORT: VB-1120
2-3
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