Need help?Do you have a question about the Piper PA-39 Twin Comanche C/R and is the answer not in the manual?
General| Manufacturer | Piper Aircraft |
|---|---|
| Model | PA-39 Twin Comanche C/R |
| Type | Light twin-engine aircraft |
| Engines | 2 |
| Crew | 1 |
| Seating Capacity | 4 |
| Max Takeoff Weight | 3, 600 lb (1, 633 kg) |
| Powerplant Output | 160 hp each |
| Capacity | 4 |
| Wingspan | 36 ft 0 in (10.97 m) |
| Service Ceiling | 20, 000 ft (6, 100 m) |
| Fuel Capacity | 100 US gal (379 L) |
Specifies critical operating limits for engines, fuel, propellers, and instruments.
Details standard, systems operation, and emergency procedures for the aircraft.
Presents performance data charts for takeoff, climb, and landing.
Provides detailed performance figures for normally aspirated and turbocharged engines.
Lists gross, empty, and useful load weights for the aircraft.
Details engine specifications, including bore, stroke, and displacement.
Outlines the essential preflight inspection procedures and checks.
Details the step-by-step procedure for starting the aircraft engines.
Covers taxi procedures, brake checks, and pre-takeoff operations.
Guides pilots through takeoff procedures, climb speeds, and related checks.
To Next Page