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1966 Piper Cherokee 140
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| Used price: | $26,000 | |
| Engine make/model: | Lycoming O-320 |
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| TBO (hrs.): | 2000 | |
| Horsepower@altitude: | 150@SL | |
| Horsepower on takeoff: | 150 | |
| Fuel type: | 100LL | |
| Propeller type: | Fixed pitch | |
| Landing gear type: | Tri./Fixed | |
| Max ramp weight (lbs.): | 2150 | |
| Gross weight (lbs.): | 2150 | |
| Landing weight (lbs.): | 2150 | |
| Empty weight, std. (lbs.): | 1128 | |
| Useful load, std. (lbs.): | 900 | |
| Useful fuel, std. (gals.): | 50 | |
| Payload, full std. fuel (lbs.): | 600 | |
| Wingspan: | 30 ft. | |
| Overall length: | 23 ft. 6 in. | |
| Height: | 7 ft. 3.5 in. | |
| Wing area (sq. ft.): | 160 | |
| Wing loading (lbs./sq. ft.): |
13.4 | |
| Power loading (lbs./bp): | 14.3 | |
| Wheel size (in.): | 6.00 x 6 | |
| Seating capacity: | 4 | |
| Cabin doors: | 1 | |
| Cabin width: | 40 in. | |
| Cabin height: | 44 in. | |
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PERFORMANCE
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| CRUISE SPEED (kts.): | ||
| 75% power: | 117 | |
| 65% power: | 109* | |
| 55% power: | 101* | |
| FUEL CONSUMPTION (gph): | ||
| 75% power: | 8.1 | |
| 65% power: | 7.0 | |
| 55% power: | 5.9 | |
| RANGE, 50 GAL. (nm): | ||
| 75% power: | 540* | |
| 65% power: | 588* | |
| 55% power: | 707* | |
| *Estimated | ||
| Vso (kts.): | 47 | |
| Best rate of climb (fpm): | 690 | |
| Service ceiling (ft.): | 14,900 | |
| Takeoff ground roll (ft.): | 800 | |
| Takeoff over 50-ft. obstacle (ft.): |
1220 | |
| Landing ground roll (ft.): | 535 | |
| Landing over 50-ft. obstacle (ft.): | 870 | |
| Source: Jane’s All The World’s Aircraft and Intertec’s Aircraft Bluebook Price Digest | ||
1966 Piper Cherokee 140
Key Takeaways:
- The article provides detailed specifications for the 1966 Piper Cherokee 140, noting it as a strong value on the used market with a price of $26,000.
- It is powered by a 150 HP Lycoming O-320 engine, has a fixed pitch propeller, fixed tricycle landing gear, and a seating capacity for 4 people.
- Key performance figures include a 75% power cruise speed of 117 knots, a useful load of 900 lbs, a service ceiling of 14,900 feet, and a maximum estimated range of 707 nautical miles.
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