PARTENAVIA P-68 B — Weight & Balance
1 weight & balance reference for the PARTENAVIA P-68 B.
Overview
P68 & P68B VICTOR FLIGHT MANUAL · 1979
This document is an appendix to the R.A.I. Approved Flight Manual for the Partenavia P-68 B aircraft, detailing maximum take-off and landing weight increases. It includes weight limits, center of gravity limits, and airspeed limitations relevant to the aircraft's operation.
- Maximum Take-off Weight: 4387 Pounds (1990 Kilograms)
- Maximum Landing Weight: 4167 Pounds (1890 Kilograms)
- Aft Center of Gravity Limit: 20.7 Inches
- Forward Center of Gravity Limit: 13.03 Inches at maximum weight
- Maneuvering Speed (VA): 130 KIAS
- Performance data may be obtained from the basic Flight Manual
- Stall speeds vary with angle of bank and flap settings
- Best rate of climb speed is 90 KIAS
1 document
PARTENAVIA P-68 B — Weight & Balance FAQ
How many Weight & Balance documents does Sprinkle have for the PARTENAVIA P-68 B?
Sprinkle has 1 Weight & Balance document on file for the PARTENAVIA P-68 B.
What year is the PARTENAVIA P-68 B Weight & Balance?
The PARTENAVIA P-68 B Weight & Balance on file is dated 1979.
Where does Sprinkle's PARTENAVIA P-68 B Weight & Balance come from?
This PARTENAVIA P-68 B Weight & Balance was originally published by alfako.be and is hosted on Sprinkle with full text and specs.