History of theTwin Navion Different Types ofNavions The History of Each IndividualTwin Navion
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Different Types of Twin Navions
TEMCO-Riley D-16A Riley '55


The D-16A was a continued development of the D-16, introduced two years prior. With important items such as constant speed, fully feathering propellers now developed, the goal was set for the D-16A, or Riley '55 to meet the performance numbers originally quoted for its older brother.

Lycoming was asked to develop a higher horsepower engine, resulting in the 170hp O-340-A1A. Fuel tanks were increased from two to five, which removed the under seat fuel tank and improved safety. Access to the rear cargo compartment was now made through a separate door on the rear left hand fuselage - a major improvement over other Navion models. The cockpit was equipped with the latest in avionics, heavily padded leather seats and plush appointments. Externally all D-16As left TEMCO's Greenville Texas plant with a standard paint scheme - a first for any Twin Navion.

As new designs from Cessna, Piper and Beech arrived on the market, sales of the Twin Navion panned out, production ceased in 1957 at serial number TTN-90.

Several D-16s in both the TN and TTN serial number ranges returned to TEMCO, before and after production ceased, for upgrades to D-16A standard.

Type Certificate
2A1
Certified
April 8, 1955

Wingspan
34' 3"
Length
27' 3/4"
Height
10' 4"

Engines
Lycoming O-340A1A
Power rating
170 hp at 2,700 rpm

Maximum takeoff weight
3,600 lbs
Number of seats
4
Maximum baggage weight
134 lbs (forward) 180 lbs (rear)
Fuel capacity
39.5 US-gallons plus 65 US-gallons in nacelle tanks (40 US-gallon tip tanks optional)
Oil capacity
4 US-gallons

Never exceed speed
190 mph (165 knots)
Maximum structural cruise
153 mph (133 knots)
Maneuvering speed
149 mph (129 knots)
Flap and gear extension
116 mph (101 knots)

Maximum range
Greater than 1,200 miles

Rate of climb (gross weight, sea level)
1,400 fpm
Service ceiling
20,000 feet
Single engine service ceiling
6,000 feet
Single engine absolute ceiling
8,000 feet

Take-off distance (over 50 foot obstacle)
1,150 feet
Landing roll (over 50 foot obstacle)
1,050 feet