I-EUST
Wheels folding into wings
Redesigned engine air intakes and tail fins
Photo: © SIAI Marchetti Brochure
AIRCRAFT DATA |
Manufacturer: |
Nardi
S.A. Per Costruzioni Aeronautiche; Aeroporto Forlanini, Milano, Italy.
Built by FIAT Divisione Aviazione; Corso G. Agnelli 200, Turin, Italy. |
Model: |
FN-333 |
Type
Certificate No: |
A-91
(RAI 1958-12-09)
7A5 (FAA 1958-12-15 ) |
Serial
Number: |
3 |
Manufacturing
Date: |
1956-??-?? |
Engine: |
Continental
O-470-H six-cylinder, 240 hp @ 2600 RPM, w/ extension shaft.
|
Remarks: |
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|
Reg.
No. |
Date |
Remarks |
I-EUST |
1956-??-?? |
Manufacturing
date. Built by Fiat? |
1956-10-14 |
First
flight from Bergamo Airport, Milan, Italy, by Ing. G. Ferrari.
From FLIGHT Magazine, 11 January 1957, page 42:
Nardi FN.333. The first prototype,
which completed a series of test flights from Bergamo airfield last
month, is back in the factory so that advantage can be taken of bad
weather for inspections and modifications.
From FLIGHT Magazine, 25 January 1957, page 114:
Some time ago Fiat
concluded an agreement with the Nardi company for the construction of
four prototypes of the Nardi FN.333 single-engined, four-seat
amphibian. The first of these made its first flight on October 14,
piloted by Ing. G. Ferrari. Taking advantages of Fiat facilities,
these machines will be tested and developed as quickly as possible to
confirm wit American C.A.A. specifications. Interest both in Italy and
abroad so far suggests that series production of this aircraft may
well prove to be justified.
|
1957-05-24 |
Static
display at Paris Air Show, 22nd International Aeronautical Salon; Le
Bourget, France (I-EUST?).
From FLIGHT Magazine, 31 May 1957, page 736:
Nardi FN 333. Fiat
are building the first Nardi amphibians and test flying is continuing
with the second prototype. One machine, brought to Paris by surface
transport and displayed in the static park, has tiny bullet-shaped
retractable floats and a retractable nosewheel undercarriage. The
engine is a Lycoming 180 h.p. pusher. Of all-metal structure, the FN
333 has a small three-/four-seat cabin and slender twin booms. All
engine cooling air is drawn in through two intakes in the wing root
and dumped by the ejector exhausts. The long boat-shaped hull carries
a retractable water rudder at the back. Main characteristics are:
span, 33 ft ll in; length, 23 ft 11 in; empty weight, 1,962 lb; gross
weight, 2,970 lb; top speed, 180 m.p.h.; ceiling, 19,685 ft; maximum
range, 776 miles; and water take-off run, 1,385 ft.
|
1961-05-29 |
Static
display at Paris Air Show, 24th International Aeronautical Salon; Le
Bourget, France (I-EUST?).
From FLIGHT Magazine, 1 Juni 1961, page 740:
SIAI Marchetti FN.333 Riviera
During the two years since the last Salon this type has undergone many
trials and tribulations, but it is now established in production. The
example in the static park is highly polished and attractive.
|
1960/61? |
Remanufactured
by SIAI Marchetti; main wheel landing gear redesigned to fold into aft
fuselage, instead of wings. Wing roots redesign after removal of main
wheels wheel wells. Became s/n 101? |
|
|
|
Sources: |
FAA
Aircraft Registry
Hendrik van der Veen
FLIGHT Magazine On-line Archive |
I-EUST
Redesigned main wheels, installation of IO-470P engine, etc.
Photo: © SIAI Marchetti via Margherita Alesini
I-EUST
Redesigned engine air intakes and tail fins
Photo: © SIAI Marchetti Brochure
I-EUST
Redesigned engine air intakes and tail fins
Photo: © Nardi
I-EUST
Redesigned engine air intakes and tail fins
Photo: © Nardi
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Photo: © Nardi
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Photo: © Nardi
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Photo: © Nardi
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Updated
2019-12-07 |
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© 2019 Steinar Saevdal |
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