| |
|
| PIPER PA-28-181 ARCHER II |
|
|
|
| SPECIFICATIONS |
|
| ENGINES |
|
|
|
|
Manufacturer |
Lycoming |
|
|
Model |
O-360-A4M |
|
|
Rating (hp @ rpm) (Take-off) |
180 @ 2700 |
|
|
Rating (hp @ rpm) (Continuous) |
178 @ 2650 |
|
|
Number of Cylinders |
4 |
|
|
Recommended TBO (hrs) |
2000 |
|
|
| PROPELLERS |
|
|
|
Manufacturer |
Sensenich |
|
|
Number of Blades |
2 |
|
|
Type |
Fixed Pitch |
|
|
Diameter (in/cm) |
76/193 |
|
|
| WEIGHTS |
|
|
|
|
Ramp Weight (lbs/kg) |
2558/1160 |
|
|
Gross Weight (lbs/kg) |
2550/1156 |
|
|
Standard Empty Weight (lbs/kg) |
1413/641 |
|
|
(Includes unusable fuel, full operating fluids and full oil) |
|
|
Standard Useful Load (lbs/kg) |
1145/519 |
|
|
| WING AREA AND LOADINGS |
|
|
|
Wing Area (ft.2/m2) |
170/15.8 |
|
|
Wing Loading (lbs/ft.2) (kg/m2) |
15.0/73.2 |
|
|
Power Loading (lbs/hp)/(kg/hp) |
14.2/6.4 |
|
|
| DIMENSIONS |
|
|
|
Wing Span (ft/m) |
|
35.0/10.7 |
|
Length (ft/m) |
|
23.8/7.3 |
|
Height (ft/m) |
|
7.3/2.2 |
|
Cabin Length (Instrument Panel to Rear Bulkhead) (in/cm) |
98/248.9 |
|
Cabin Width (in/cm) |
|
41.75/106.0 |
|
Cabin Height (in/cm) |
|
45/114.3 |
|
Headroom (Seat to Ceiling) |
|
|
|
Front Seat (in/cm) |
|
38/96.5 |
|
Rear Seat (in/cm) |
|
34.5/87.6 |
|
Baggage Door Size (in/cm) |
|
22/55.9 x 20/50.8 |
|
Cabin Door Size (in/cm) |
|
36/91.4 x 35/88.9 |
|
Wheel Base (ft/m) |
|
6.58/2.01 |
|
Wheel Tread (ft/m) |
|
10/3.05 |
|
| FUEL CAPACITY |
|
|
|
Two 25 gal. tanks (gal/L) |
50/189 |
|
|
Usable Fuel (gal/L) |
48/182 |
|
|
| OIL CAPACITY (qts/L) |
8/7.57 |
|
|
| BAGGAGE |
|
|
|
Volume (ft3/m3) |
26/.74 |
|
|
Capacity (lbs/kg) |
200/91 |
|
|
|
|
|
| PERFORMANCE |
|
| MAXIMUM SPEED (kts/kmh) |
|
(TAS at Gross Weight) |
129/239 |
|
| CRUISING SPEEDS |
Best Power |
Best Economy |
|
(TAS at Gross Weight) |
|
|
|
75% at 8,000 ft (kts/kmh) |
129/239 |
126/233 |
|
65% at 12,000 ft (kts/kmh) |
125/232 |
121/224 |
|
55% at 12,500 ft (kts/kmh) |
111/206 |
106/196 |
|
| CRUISE RANGE |
|
(Cruising range includes 45-minute fuel reserve at max. range power plus
allowance for fuel used during taxi, take-off, climb at MCP, cruise at stated
mixture and descent) |
|
|
Best Power |
Best Economy |
|
75% at 8,000 ft (nm/km) |
520/963 |
600/1111 |
|
65% at 12,000 ft (nm/km) |
565/1047 |
645/1195 |
|
55% at 12,500 ft (nm/km) |
580/1075 |
670/1241 |
|
| FUEL CONSUMPTION |
Best Power |
Best Economy |
|
75% power (gph/lph) |
10.5/39.7 |
8.8/33.3 |
|
65% power (gph/lph) |
9.0/34.1 |
7.6/28.8 |
|
55% power (gph/lph) |
7.8/29.5 |
6.3/23.8 |
|
| RATE OF CLIMB (At Sea Level and Gross Wt) |
|
Full Throttle (fpm/mpm) |
735/224 |
|
| STALL SPEED |
IAS |
CAS |
|
Flaps Down Full 40o (kts/kmh) |
47/87 |
53/98 |
|
Flaps Up (kts/kmh) |
53/98 |
59/109 |
|
| SERVICE CEILING (100 fpm) (ft/m) |
13,650/4161 |
|
| TAKE-OFF DISTANCE |
|
|
(Sea Level, Zero Wind, Standard Temperature, 25o flaps) |
|
Ground Run (ft/m) |
|
870/265 |
|
Total over 50 ft obstacle (ft/m) |
|
1660/502 |
|
| LANDING DISTANCE |
|
|
|
(Sea Level, Zero Wind, Standard Temperature) |
|
Ground Roll (ft/m) |
|
925/282 |
|
Total over 50 ft obstacle (ft/m) |
|
1390/424 |
|
|
Reference: Piper Aircraft Corporation Brochure, Vero Beach, FL, 1 Sep. 1987 |
|
Given data is only for information. Please refer to the manufacturer for current
data. |
|
|