LNC2

LANCAIR Lancair 320

Aircraft
Name
Lancair 320
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufacturered as
PAI Lancair 320
NEICO Lancair 200
NEICO Lancair 235
NEICO Lancair 320
NEICO Lancair 360
LANCAIR Lancair 235
LANCAIR Lancair 360
LANCAIR Lancair 200
LANCAIR Lancair 320

LNC2

The Lancair 320 is a two-seat single-engined light aircraft marketed in kit form. It is based on the Lancair 235, but with a larger fuselage and more powerful engine, and like the 235, is a low-winged monoplane of composite construction with a retractable tricycle undercarriage, with side-by-side seating in an enclosed cockpit. The Lancair 360 is similar, but with a more powerful engine.

  • Lancair 200 2-seat kit powered by a Continental 0-200 engine, released in 1985
  • Lancair 235 2-seat kit powered by a Lycoming O-235 engine, released in 1986
  • Lancair 320 2-seat kit powered by a Lycoming O-320 engine, released in 1988
  • Lancair 360 2-seat kit powered by a Lycoming O-360 engine, released in 1988.
Technical Data
Wing span (metric)
7.16 m
Length (metric)
6.40 m
Height (metric)
2.13 m
Powerplant

1 x Textron Lycoming O-320 air-cooled flat four, 160 hp.

Engine Model(s)
Continental O-200
Lycoming O-290
Lycoming O-320
Lycoming O-360
Indicative Performance Data
Take-Off
V2
n/a
Distance
120 m
MTOW
764 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
2000 ft/min
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
240 kts
MACH
n/a
Ceiling
180
Range
1450 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
270 m

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