PIPER AEROSTAR 602P — Pilot's Operating Handbook
1 pilot's operating handbook reference for the PIPER AEROSTAR 602P.
Overview
1983-1983 Piper Aerostar 602P · 1983
The document provides detailed specifications and performance information for the Piper Aerostar 602P aircraft. It includes data on engines, weights, dimensions, performance metrics, and standard equipment.
- The Aerostar 602P is powered by two Lycoming 290 hp engines.
- Maximum take-off weight is 6000 lbs.
- Cruise speed at best power is 247 knots.
- Usable fuel capacity is 165.5 gallons.
- The aircraft features hydraulic retractable landing gear.
- Standard empty weight is 4125 lbs.
- Service ceiling is 28,000 feet.
- The aircraft includes dual automatic turbo-chargers.
1 document
PIPER AEROSTAR 602P — Pilot's Operating Handbook FAQ
How many Pilot's Operating Handbook documents does Sprinkle have for the PIPER AEROSTAR 602P?
Sprinkle has 1 Pilot's Operating Handbook document on file for the PIPER AEROSTAR 602P.
What year is the PIPER AEROSTAR 602P Pilot's Operating Handbook?
The PIPER AEROSTAR 602P Pilot's Operating Handbook on file is dated 1983.
Where does Sprinkle's PIPER AEROSTAR 602P Pilot's Operating Handbook come from?
This PIPER AEROSTAR 602P Pilot's Operating Handbook was originally published by aeroresourcesinc.com and is hosted on Sprinkle with full text and specs.