CP80

PIEL CP-80 Zephir

Aircraft
Name
CP-80 Zephir
Manufacturer
Body
Narrow
Wing
Fixed Wing
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Manufacturered as
PIEL CP-801 Zephir
PIEL CP-802 Zephir
PIEL Zephir
PIEL CP-80 Zephir

CP80

The Piel CP.80 Zephir and Piel CP.801 are racing aircraft developed in France in the 1970s and marketed for homebuilding. They are compact, single-seat, single-engine monoplanes with low, cantilever wings.

Technical Data
Wing span (metric)
5.30 m
Length (metric)
6.00 m
Height (metric)
1.70 m
Powerplant

1 x Continental C90-8F, 67 kW (90 hp)

Engine Model(s)
Continental O-200
Indicative Performance Data
Take-Off
V2
n/a
Distance
400 m
MTOW
400 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
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
80 kts
MACH
n/a
Ceiling
100
Range
240 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
360 m

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