rollin59
11-19-2020, 10:21 AM
Plan-Built Aircraft Partially Assembled, located Xenia Ohio
The C.P. 750 Piel Beryl is a tandem two seat, low wing aircraft designed by Claude Piel (France). Fixed gear, tail dragger. Aerobatic as a single seater. Type first flown 1965. Only 6 known to be completed in USA.
Must sell, Asking $4900 or reasonable offer. Photos of airframe available on request.
For questions or more details, or to schedule viewing, contact Tom at boicetw@gmail.com
History: Project first planned in 1968 by EAA member in Colorado Springs. Much completed work dates to early 1980s. Current owner has FAA signed-off records for three previous builders. Much of the big work is done. Current owner lost interest. In dry storage. Needs to be gone soon.
Parts included/work completed: 1960 Lycoming O-320-G engine, complete, believed never run, with mounting hardware installed, turns over by hand. Have original Lycoming order document. Engine is a non-certified “ground use” variant with CCW rotation.
F-86 fighter jet canopy. Custom fabricated welded steel fuselage frame, control pulleys and cables, dashboard, tailwheel and some instruments installed.
Dihedryl Wing Ribs, Vertical and Horizontal Stabilizer spars, Rudder, Elevator and Flap Spars (L and R), Vertical and Horizontal Stabilizers, Rudder, Elevator, and Flaps (L&R), assembled but not covered.
Custom fabricated landing gear, aluminum fuel tanks and exhaust system. Propeller spinner (no prop). No wing spar. Several boxes of loose parts including carburetors, hardware, gauges, etc., too many to list.
Documentation: Large file with blueprints, correspondence and photographs. Previous FAA Aircraft registration cards by builders. Construction Logbook with inspection approval of flap assy. Etc.
Work to be completed: Fuselage skin, main wing spar, assembly, go through engine, electrical, etc.
Seller prefers new owner who will complete and fly this rare aerobatic aircraft.
(boicetw@gmail.com)
Characteristics
Span
26.5 ft
Length
22.75 ft
Height
6.9 ft
Area
117 sq ft
Fuel
220 lbs
Max Baggage
80 lbs
Max Takeoff Weight
1700 lbs (N)
Max Takeoff Weight
1400 lbs (A)
U/C Track
7.8 ft
Dihedral
5° 40'
Incidence
4° 10'
Performance
Max Speed
185 mph
Cruise 75% 5,000 ft
167 mph
Cruise 65% 5,000 ft
155 mph
Rate Of Climb (ft/min)
1200 ft/min
T/O distance (ft)
620 ft
Landing Distance
900 ft
Vne
212 mph
Approach Speed Flaps Down
80 mph
Stall Flaps Up
65 mph
Stall Flaps Down
56 mph
Range
680 miles
Optimum Climb Speed
75 mph
EAA Experimenter December 2014 magazine feature article shows finished example of this type, built by Randy Weselmann, Indiana, Reg. No. N42WX. (Photo below show appearance of finished plane, not one advertised)
8747
The C.P. 750 Piel Beryl is a tandem two seat, low wing aircraft designed by Claude Piel (France). Fixed gear, tail dragger. Aerobatic as a single seater. Type first flown 1965. Only 6 known to be completed in USA.
Must sell, Asking $4900 or reasonable offer. Photos of airframe available on request.
For questions or more details, or to schedule viewing, contact Tom at boicetw@gmail.com
History: Project first planned in 1968 by EAA member in Colorado Springs. Much completed work dates to early 1980s. Current owner has FAA signed-off records for three previous builders. Much of the big work is done. Current owner lost interest. In dry storage. Needs to be gone soon.
Parts included/work completed: 1960 Lycoming O-320-G engine, complete, believed never run, with mounting hardware installed, turns over by hand. Have original Lycoming order document. Engine is a non-certified “ground use” variant with CCW rotation.
F-86 fighter jet canopy. Custom fabricated welded steel fuselage frame, control pulleys and cables, dashboard, tailwheel and some instruments installed.
Dihedryl Wing Ribs, Vertical and Horizontal Stabilizer spars, Rudder, Elevator and Flap Spars (L and R), Vertical and Horizontal Stabilizers, Rudder, Elevator, and Flaps (L&R), assembled but not covered.
Custom fabricated landing gear, aluminum fuel tanks and exhaust system. Propeller spinner (no prop). No wing spar. Several boxes of loose parts including carburetors, hardware, gauges, etc., too many to list.
Documentation: Large file with blueprints, correspondence and photographs. Previous FAA Aircraft registration cards by builders. Construction Logbook with inspection approval of flap assy. Etc.
Work to be completed: Fuselage skin, main wing spar, assembly, go through engine, electrical, etc.
Seller prefers new owner who will complete and fly this rare aerobatic aircraft.
(boicetw@gmail.com)
Characteristics
Span
26.5 ft
Length
22.75 ft
Height
6.9 ft
Area
117 sq ft
Fuel
220 lbs
Max Baggage
80 lbs
Max Takeoff Weight
1700 lbs (N)
Max Takeoff Weight
1400 lbs (A)
U/C Track
7.8 ft
Dihedral
5° 40'
Incidence
4° 10'
Performance
Max Speed
185 mph
Cruise 75% 5,000 ft
167 mph
Cruise 65% 5,000 ft
155 mph
Rate Of Climb (ft/min)
1200 ft/min
T/O distance (ft)
620 ft
Landing Distance
900 ft
Vne
212 mph
Approach Speed Flaps Down
80 mph
Stall Flaps Up
65 mph
Stall Flaps Down
56 mph
Range
680 miles
Optimum Climb Speed
75 mph
EAA Experimenter December 2014 magazine feature article shows finished example of this type, built by Randy Weselmann, Indiana, Reg. No. N42WX. (Photo below show appearance of finished plane, not one advertised)
8747