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General| Manufacturer | Piper Aircraft |
|---|---|
| Type | Light aircraft |
| Crew | 1 |
| Capacity | 1 passenger |
| Max Takeoff Weight | 1, 220 lb (553 kg) |
| Horsepower | 65 hp (48 kW) |
| Maximum Speed | 87 mph (140 km/h, 76 kn) |
| Cruise Speed | 75 mph (121 km/h, 65 kn) |
| Stall Speed | 38 mph (61 km/h, 33 kn) |
| Service Ceiling | 11, 500 ft (3, 500 m) |
| Rate of Climb | 450 ft/min (2.3 m/s) |
| Powerplant | 1 × Continental A-65-8 air-cooled flat-four engine |
| Range | 190 nmi |
Procedure for leveling the airplane laterally and longitudinally.
Method for checking and adjusting the dihedral angle of the wings.
Procedure for adjusting the wash out in the wings.
Description of hydraulic brakes, pedals, and bleeding procedure.
Construction of the fuselage frame and member replacement.
Structure, maintenance, and lubrication of ailerons.
Transmission of elevator control stick motion via linkage.
Lateral control stick motion and rigging procedure for ailerons.
Operation of the stabilizer by crank and indicator system.
Inspection and cleaning of the gascolator/fuel strainer.
Checklist for line inspection of aircraft components.
Items to check during a 20-hour inspection.
Checklist for 100-hour periodic maintenance inspection.
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