Piper ARCHER II - Page 24

PIPER AIRCRAFT CORPORATION |
PA-28-181, ARCHER II
SECTION I
GENERAL
- 1.3 ENGINES
1.5
1.7
(a)
(b)
(c)
(d)
(e)
(
(g)
1)
(i)
G)
(k)
(I)
Number of Engines
Engine Manufacturer
Engine Model Number
Takeoff Power - 5 Minute Limit (BHP)
Takeoff Engine Speed - 5 Minute
Limit (RPM)
Maximum Continuous Power (BHP)
Maximum Continuous Engine
Speed (RPM)
Bore (inches)
Stroke (inches)
Displacement (cubic inches)
Compression Ratio
Engine Type
PROPELLERS
(a)
(b)
(c)
(d)
(e)
(f)
Number of Propellers
Propelier Manufacturer
Model
Number of Blades
Propeller Diameter (inches)
(1) Maximum
(2) Minimum
Propeller Type
FUEL
AVGAS ONLY
(a)
(b)
(c)
Fuel Capacity (U.S. gal.) (total)
Usable Fuel (U.S. gal.) (total)
Fue}
(1) Minimum Octane
(2) Alternate Fuel’
|
Lycoming.
O-360-A4M or
0-360-A4A
180
2700
178
2650
5.125
4.375
361.0
8.5:1
Four Cylinder, Direct
Drive, Horizontally
Opposed, Air Cooled
j
Sensenich
76EM8S5-0-62
; 2
76
76
Fixed Pitch
50
48
100 Green or IOOLL Blue
Aviation Grade
Refer to latest issue of
Lycoming Instruction No. 1070.
ISSUED: JULY 2, 1979
REVISED: JUNE 29, 1984
REPORT: VB-1120
1-3