aircraft

Our Aircraft

We are going to fly a Cessna 210 Centurion, which Ed bought new in 1977. It is a 6 seat single engine airplane, powered by a 300 HP Continental IO‑520‑L engine. It has a cruising speed of 160 KTS (185 MPH). The normal fuel quantity is 90 gallons, but this aircraft is equipped with long-range wing-tip tanks providing an extra 32 gallons, for a range of 1350 miles. The certified take off weight is 3800 lbs.

Since some of the legs of our trip are more than 2500 miles, additional fuel is required. We will be carrying an additional 162 gallons of fuel in three tanks located behind us in the cabin, where passenger seats are normally located, requiring a special ferry permit from the FAA. With this additional fuel we will be able to fly our longest legs with a reserve of 500 miles or about three hours.

The instrument panel includes a Bendix/King KLN 90B GPS (Global Positioning System). ILS and VOR navigation and VHF radio communication. An Argus 5000/CE moving map for navigation. A solid state transponder, a Stomscope for thunderstorm detection and a high frequency radio transceiver.


Photo Courtesy of Mark Seeman
N2160S and her jockey
Photo Courtesy of Mark Seeman
In flight
Photo Courtesy of Mark Seeman
In flight
Long range communication HF Antenna streches from tail to left wing tip
Photo Courtesy of Ed Galkin
All seats removed, this is where the cabin fuel tanks are going to be
Photo Courtesy of Ed Galkin
Pilots seats removed to allow for fuel tanks insertion
Photo Courtesy of Ed Galkin
Marty Balk working on HF radio installation
Photo Courtesy of Ed Galkin
120 Gallon tank with pumps and meter provided by John Coale
Photo Courtesy of Ed Galkin
22 Gallon tank
Photo Courtesy of Ed Galkin
Myron Olsen from O & N after installing 20 Gallon tank at bottom of baggage compartment

performance - specifications

speed
maximum at sea level 175 knots
cruise, 75% power at 6500 ft 171 knots
cruise
75% power at 6500 ft, 534 pounds usable fuel
range 855 nm
time 5.1 hours
maximum range at 10,000 ft, 534 pounds usable fuel
range 1060 nm
time 7.8 hours
rate of climb at sea level 860 fpm
service ceiling 15,500 ft
takeoff performance
ground roll 1250 ft
total distance over 50-Ft obstacle 2030 ft
landing performance
ground roll 755 ft
total distance over 50-Ft obstacle 1500 ft
stall speed (cas)
flaps up, power off 65 knots
flaps down, power off 56 knots
maximum weight 3800 lbs
standard empty weight
centurion 2170 lbs
centurion II 2244 lbs
maximum useful load
centurion 1630 lbs
centurion II 1556 lbs
baggage allowance 240 lbs
wing loading 21.7 pounds/sq ft
power loading 12.7 pounds/hp
fuel capacity 90 gal
oil capacity 10 qts
engine IO‑520‑L
at 2850 RPM (5 minute takeoff rating) 300 hp
at 2700 RPM (maximum continuous rating) 285 hp
propeller 80 in

Instrument Panel


© 2004 Pascal Landi