Grega GN-1 Air Camper
Early in 1958, John W. Grega, EAA 3808,
embarked on the Pietenpol Project, the object of which was to
modernize the excellent 1933 Model A Ford powered version, to a
Continental A-65 powered two-seat "fun plane" with good small field
capabilities, using modern straight forward construction methods.
With engineering know-how available to him from his then EAA Chapter
5, located at the old Welcome Airport in Northfield Centre Township
in Ohio, John Grega enlisted the aid of a fellow member to run a
preliminary weight and balance on the 65 hp version of the Pietenpol
Aircamper. Armed with this data, John Grega, an experienced
woodworker, proceeded to design a new fuselage structure employing
Piper J-3 motor mount, landing gear, control assembly, and tail
wheel assembly. Using a GN modified clip wing off a J-3 Cub, for
which the original fuselage designed was intended.
Along with the use of a J-3 wing, an improved and modernized version
of the original Pietenpol Aircamper wing was initiated, lending
versatility to the design. The original airfoil was redesigned with
a more rounded leading edge for better stall characteristics, the
truss was improved for more strength, and spars were relocated for
greater depth and in keeping with modern designed parameters.
Construction of the GN-1 prototype was immediately started after the
original drawings were completed. This was to the be the J-3 wing
version. John Grega finished and was flying his GN-1 prototype,
N4705G, in 1963.
Selling plans on the GN-1 Aircamper was the furthest thing from John
Grega's mind, until a small article appeared in the June 1960 issue
of Sport Aviation, regarding the fact that the GN-1 was under
construction. From that time on, the amount of mail received by John
Grega was overwhelming, all letters expressing the desire to
purchase plans for the GN-1, if and when available. Most requested
parts were drawn up and sent out so construction could start. All
sketches, doodles, and bits and pieces of construction were
correlated into a set of drawings, first pencil tracings, and as
construction problems arose, they were resolved and incorporated
into a finished set of drawings. The finished set being officially
copyrighted in 1992, by John W. Grega.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
Cont. HP
Range65/65-90
x
18.1ft
6.8ft
29ft
145sq. ft
2
650lb
x
1100lb
12gal
400n.m |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
300ft
500fpm
115mph
87mph
300ft
12,000ft |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
x
25mph
x |
All specifications are based on manufacturer's
calculations
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