PIPER PA31-350 Navajo Chieftain — Pilot's Operating Handbook
1 pilot's operating handbook reference for the PIPER PA31-350 Navajo Chieftain.
Overview
Piper Aircraft Corporation Chieftain PA31-350 Specifications/Performance · 1983
The Piper PA31-350 Navajo Chieftain Pilot's Operating Handbook provides detailed specifications, performance data, and standard equipment information for the aircraft. It serves as a comprehensive guide for pilots to understand the operational capabilities and limitations of the Navajo Chieftain.
- The aircraft is powered by two Lycoming TI0-540-J2BD engines.
- Maximum take-off weight is 7000 lbs.
- Cruise speed can reach up to 230 knots.
- Standard fuel capacity is 192 gallons, with 182 gallons usable.
- The cabin can accommodate up to eight passengers.
- The aircraft features a retractable hydraulic landing gear.
- Service ceiling is 24,000 feet.
- The recommended TBO for the engines is 1600 hours.
1 document
PIPER PA31-350 Navajo Chieftain — Pilot's Operating Handbook FAQ
How many Pilot's Operating Handbook documents does Sprinkle have for the PIPER PA31-350 Navajo Chieftain?
Sprinkle has 1 Pilot's Operating Handbook document on file for the PIPER PA31-350 Navajo Chieftain.
What year is the PIPER PA31-350 Navajo Chieftain Pilot's Operating Handbook?
The PIPER PA31-350 Navajo Chieftain Pilot's Operating Handbook on file is dated 1983.
Where does Sprinkle's PIPER PA31-350 Navajo Chieftain Pilot's Operating Handbook come from?
This PIPER PA31-350 Navajo Chieftain Pilot's Operating Handbook was originally published by aeroresourcesinc.com and is hosted on Sprinkle with full text and specs.