| |
|
| PIPER PA-28-236 DAKOTA |
| SPECIFICATIONS |
|
| ENGINE |
|
Lycoming |
|
O-540-J3A5D |
|
235/2400 |
|
6 |
|
2000 |
|
| PROPELLER |
|
Hartzell |
|
2 |
|
Constant Speed |
|
80/205 |
|
| WEIGHTS |
|
3011/1366 |
|
3000/1361 |
|
1610/730 |
(Includes unusable fuel, full oil and full operating fluids)
|
|
1401/635 |
|
|
WING AREA AND LOADINGS |
|
170/15.8 |
|
17.6/86.1 |
|
12.8/5.8 |
|
| DIMENSIONS |
|
35.4/10.8 |
|
24.7/7.5 |
|
7.2/2.2 |
|
98/248.9 |
|
41.75/106.0 |
|
44.75/113.7 |
|
|
38/96.5 |
|
35/88.9 |
|
22/55.9 x 20/50.8 |
|
36/91.4 x 35/88.9 |
|
6.5/1.98 |
|
10/3.05 |
|
| FUEL CAPACITY |
|
77/291 |
|
72/273 |
|
| OIL CAPACITY (qts/L) |
12/11.36 |
|
| BAGGAGE |
|
26/0.74 |
|
|
|
200/91 |
|
|

|
| PERFORMANCE |
|
| MAXIMUM SPEED (kts/kmh) |
|
|
148/274 |
|
| CRUISING SPEEDS |
Best Power |
Best Economy |
|
|
|
144/267 |
139/257 |
|
139/258 |
134/248 |
|
130/240 |
126/233 |
|
| CRUISE RANGE |
(Cruising range includes 45-minute fuel reserve at maximum range
power plus allowance for fuel used during taxi, take-off, climb at MCP,
cruise at optimum altitude and stated mixture and descent)
|
| |
Best Power |
Best Economy |
|
650/1204 |
720/1334 |
|
710/1315 |
770/1426 |
|
750/1390 |
810/1500 |
|
| FUEL CONSUMPTION |
Best Power |
Best Economy |
|
13.6/51.5 |
12.7/47.9 |
|
11.8/44.7 |
10.9/41.3 |
|
10.1/38.2 |
9.3/35.2 |
|
| RATE OF CLIMB (At Sea Level and Gross Wt) |
|
|
1110/338 |
|
| STALL SPEED |
IAS |
CAS |
|
56/104 |
58/107 |
|
65/120 |
65/120 |
|
| SERVICE CEILING (100 fpm) (ft/m) |
|
17,500/5334 |
|
| TAKE-OFF DISTANCE |
|
|
(Sea Level, Zero Wind, Standard
|
|
|
|
886/270 |
|
|
1216/371 |
|
| LANDING DISTANCE |
Std. Brakes |
H.D. Brakes |
(Sea Level, Zero Wind, Standard Temperature)
|
|
825/251 |
640/195 |
|
1725/526 |
1530/466 |
|
|
Reference: Piper Aircraft Corporation Brochure, Vero Beach, FL, 1 Nov. 1988 |
|
Given data is only for information. Please refer to the manufacturer for current
data. |
|
|