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General| Manufacturer | Piper Aircraft |
|---|---|
| Model | PA-32-300 |
| Engine | Lycoming IO-540-K1A5 |
| Horsepower | 300 hp |
| Seating Capacity | 6 |
| Propeller | Constant speed, 2-blade |
| Wingspan | 32 ft 10 in |
| Length | 27 ft 8 in |
| Maximum Takeoff Weight | 3, 400 lbs |
| Fuel Capacity | 84 gallons |
| Stall Speed | 61 mph |
| Rate of Climb | 1, 050 ft/min |
| Cruise Speed | 172 mph |
Published performance figures for standard airplanes at gross weight.
Details on standard empty weight and maximum useful load.
Information on engine, propeller, and related specifications.
Describes the semi-monocoque structure and wing airfoil section.
Details the Lycoming engine and propeller specifications.
Explains the induction air system and fuel injection system.
Describes the steerable nose gear, oleo struts, and brakes.
General guidance on recommended emergency procedures.
Procedures for engine power loss during takeoff.
Actions to take for engine power loss during flight.
Procedure for landing the aircraft with no engine power.
Steps to take in case of propeller overspeed.
Recovery techniques for an inadvertently entered spin.
Actions to take in case of electrical or engine fire.
Procedure for indication of loss of oil pressure.
Actions to take for loss of fuel pressure.
Procedure for high oil temperature indication.
Steps to take in case of alternator failure.
Covers preflight walk-around inspection and engine start procedures.
Details engine warm-up, ground checks, and takeoff techniques.
Graphs for takeoff distance based on weight and flaps.
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