The
Schweizer 330
and
S333
are turbine-powered developments of the
Schweizer 300
light piston-powered helicopter. As of 2007, only the Schweizer 333 remains in production.
[1]
In February 2009, the 333 was rebranded as the
Sikorsky S-333
.
[2]
In 2018 the Schweizer R.S.G. bought the
Schweizer Aircraft
from
Sikorsky Aircraft
and it was rebranded as Schweizer S333 again.
[3]
Development
[
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]
Schweizer 330
[
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]
In 1987, Schweizer announced development of the Schweizer 330 using the dynamic components, rotors, controls and systems of the 300C; however, it was redesigned with an all-new fuselage.
[4]
The first 330, converted from a 300C and powered by an
Allison 250
-C10A, flew on June 14, 1988. The FAA certified the aircraft in September 1992.
The improved 330SP was introduced in May 1997 and featured an improved rotor and raised skids, which could be retrofitted to previous 330 models. An Allison (later Rolls-Royce) 250-C20W turboshaft was derated to 165 kW (220 hp), giving the 330SP excellent hot and high performance, maintaining power output to 18,000 feet.
[
citation needed
]
Schweizer 333
[
edit
]
Schweizer 333
Shortly after the release of the 330, Schweizer began work on upgrading the dynamic components of the Schweizer 330SP. Over two years later, Schweizer released a new variant, the Schweizer 333. Featuring the newly developed dynamic systems components and new-technology rotor blades with a cambered airfoil and a larger diameter rotor, the upgraded helicopter benefited from a greater max gross weight, more useful load, more speed and more hover performance; nearly a 30% increase in performance over the 330SP. Schweizer created a kit to upgrade Model 330 and 330SP aircraft.
[5]
In February 2008, an improved version of the series, the
S-434
was released.
[6]
[7]
Design
[
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]
The 330 used the 300C's dynamic components, a Rolls-Royce 250 turboshaft engine, and a new four-seat cockpit/cabin and body and new instrumentation.
Operational history
[
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]
Schweizer was purchased on August 26, 2004, by
Sikorsky Aircraft
. The Schweizer 300/333 models fill a gap in the Sikorsky helicopter line, which is known for its medium and heavy utility and cargo helicopters. Sikorsky has since taken advantage of Schweizer's rapid prototyping technology, originally used during development of the 333 dynamic components and the RQ-8 prototype, to develop the
X-2 Technology Demonstrator
.
[8]
Variants
[
edit
]
A RQ-8A Fire Scout helicopter preparing to land on the
USS
Nashville
- 330
- Using the 300C dynamic components, Schweizer mounted a Rolls-Royce 250-C10A engine to the airframe and developed a new four-seat cockpit/cabin and body.
- 330SP
- improved rotor and raised skids, Rolls-Royce 250-C20W engine.
- 333
- Featuring new dynamic system components, new rotor blades, and high skids as standard equipment, the 333 has a 30% greater useful load than the 330SP.
- RQ-8/MQ-8 Fire Scout
- The
Northrop Grumman MQ-8B Fire Scout
is an
unmanned
derivative of the Schweizer 330SP/333 helicopter, with a new fuselage, new fuel system, and UAV electronics and sensors. It also utilizes a new four-bladed rotor system based on that of the Schweizer 333. The Fire Scout is currently in development for the
United States Navy
's VTUAV program with cooperation from
Northrop Grumman
. The original RQ-8A was based on the 330SP.
- Sikorsky S-434
- Based on improvements developed for the MQ-8B, this is a new version of the 333, having a four-bladed main rotor.
[9]
Operators
[
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]
Dominican Republic
Saudi Arabia
Non-state operators
[
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]
Specifications (333)
[
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]
Data from
International Directory of Civil Aircraft
[4]
and Technical specifications
[17]
General characteristics
- Crew:
1-2
- Capacity:
1-3 pax
- Length:
31 ft 2 in (9.50 m) overall
- Height:
11 ft 0 in (3.35 m)
- Empty weight:
1,210 lb (549 kg)
- Gross weight:
2,460 lb (1,116 kg)
- Max takeoff weight:
2,550 lb (1,157 kg)
- Powerplant:
1 ×
Rolls-Royce M250-C20W
turboshaft
engine, 235 shp (175 kW)
- Main rotor diameter:
27 ft 6 in (8.38 m)
- Main rotor area:
594 sq ft (55.2 m
2
) *
Blade section:
-
NACA 0015 modified
[18]
Performance
- Cruise speed:
105 kn (121 mph, 194 km/h)
- Range:
319 nmi (367 mi, 591 km)
- Rate of climb:
1,380 ft/min (7.0 m/s)
See also
[
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]
Related development
Aircraft of comparable role, configuration, and era
References
[
edit
]
- ^
Schweizer Aircraft 333 page
Archived
2007-05-31 at the
Wayback Machine
- ^
"Sikorsky Press Release February 23, 2009"
. Archived from
the original
on July 25, 2011
. Retrieved
February 25,
2009
.
- ^
"HOME - Schweizer"
. Schweizerrsg.com
. Retrieved
2022-05-02
.
- ^
a
b
Frawley, Gerard:
The International Directiory of Civil Aircraft, 2003-2004
, page 190. Aerospace Publications Pty Ltd, 2003.
ISBN
1-875671-58-7
- ^
Flug Revue article on the 333
Archived
2007-06-15 at the
Wayback Machine
- ^
Sikorsky announces launch of Schweizer S-434 Commercial Helicopter at Heli-Expo
- ^
Heli-Expo 2008: Sikorsky launches Schweizer 434
- ^
"Rotor & Wing Magazine :: Big Plans"
.
www.aviationtoday.com
. Archived from
the original
on 2007-03-25.
- ^
Rotorcraft Report: New Schweizer Model? The Turbine 434
Archived
2008-12-01 at the
Wayback Machine
- ^
"Escuela de Helicopteros"
. aeroflight.co.uk
. Retrieved
15 February
2013
.
- ^
"Dominican Republic Schweizer-333"
. Demand media
. Retrieved
17 February
2013
.
- ^
Philippe Chapleau
(29 November 2015).
"DynCorp signe pour cinq nouvelles annees de soutien au profit de l'Alat saoudienne"
(in French).
Ouest-France
. Retrieved
2 December
2015
.
- ^
"Royal Saudi Land Forces"
.
http://www.scramble.nl
. 2015. Archived from
the original
on 25 September 2017
. Retrieved
2 November
2015
.
- ^
"Turkish News - Latest News from Turkey"
.
Hurriyet Daily News
. Retrieved
2023-12-18
.
- ^
"Contract to Buy 16 Helicopters Signed by Kurdistan R. Govt. - Media monitor"
.
www.ekurd.net
. Retrieved
2023-12-18
.
- ^
http://iwpr.net/report-news/contract-buy-16-helicopters-signed
- ^
Technical Data Summary, Model 333
(PDF)
, archived from
the original
(PDF)
on 2007-07-26
- ^
Lednicer, David.
"The Incomplete Guide to Airfoil Usage"
.
m-selig.ae.illinois.edu
. Retrieved
16 April
2019
.
External links
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]
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