Models

560F

The 560F is the same as the 680F except for gross weight was reduced to 7500 pounds and Lycoming engine IGO540-B1A installed. The 560F was Certified on February 8, 1961.

Note: All Specifications & Performances Data provided below are for Reference Only. See Piston Commander 560F TCDS, POH/AFM, & ICA's for Model & S/N specific Specification & Performance Data.

Specification Performance Kit Finder
560F

Specifications

Dimensions

Wing span

49.04'

14.94m
Length35.10′10.69m
Height14.50′4.41m
Tread12.91′3.93m
Cabin Door Height3.58' 1.09m
Cabin Door Width2.33' 0.71m
Cabin Height (Inside Interior)4.41′ `.34m
Cabin Length10.62′3.23m
Cabin Width (Inside Interior)4.33′1.31m
Cabin Volume177 ft³53.94m³
Baggage compartment height3.41′x.xxm
Baggage compartment width3.91′ 1.03m
Baggage compartment length2.58′ 0.78m
Baggage compartment volume32 ft³  9.75m³
Baggage door height1.91′0.58m
Baggage door width1.58′0.48m
Baggage compartment load limit350 lbs158 kg
560F

Propellers

HC-B3Z-30-2B (15)/9349 / HC-B3Z-30-2B-9349-6.5 (3 blade)

Power Plant

Lycoming IGO-540-B1A/-B1C

Weights - Aircraft

Max Ramp Weight:7500 lbs / 3402 kg
Take-off Weight:7500 lbs / 3402 kg
Landing Weight:7500 lbs / 3402 kg
Dry Empty Weight:4650 lbs / 2109 kg
Useful Load:2800 lbs / 1293 kg
560F
560F

Performance

Operating Speed

Cruise Speed (@ 70% power @ 10,000 Ft)232 mph / 201 kts
Normal Cruise Speed

(70% NRP @ 10,000 ft)

208 mph/ 180 kts
Twin Engine Best Rate of Climb Speed (CAS):120 mph / 104 kts
Stall Speed, Clean (CAS):83 mph / 72 kts
Minimum Control Speed (CAS):90 mph / 78 kts
Stall Speed, Gear and Flaps Down (CAS):73 mph / 63 kts
Stall Speed (Dirty)73.5 mph / 63.8 kts
Range (@ 50% power, 30 Min Reserve)1705 SM / 1481 NM

Cruising Ranges

All Models