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Grob Aerospace's new SPn Utility Jet completed its maiden flight on July 20, 2005.
Grob Aerospace's new SPn Utility Jet completed its maiden flight on July 20, 2005.
Grob
G180 SPn
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Grob launched its first business
jet project in complete secrecy in January 2004.
Prototype assembly took place between October
2004 and January 2005.
Rumors that Grob was working on a business jet
began to circulate in the spring of 2005,
pointing to a very light jet. Surprise was
therefore great when Grob presented its SPn
Utility Jet at the Paris Air Show on 13 June
2005, not only showing a cabin mock up but the
real prototype.
Grob Aerospace's new SPn
Utility Jet completed its maiden flight on July
20, 2005. It departed Allgäu Airport (EDJA) near
Memmingen in southern Germany at 11:14 am. The
aircraft was commanded by Capt. Gerard
Guillaumaud and co-test pilot Tore Reimers. It
landed 66 minutes later after performing initial
handling tests and system checks. Previously, a
test airframe had successfully passed a program
of full strength testing on the fuselage and
wing required for certification.
As the largest private jet to be
certified for single-pilot operations, the Grob
SPn is equipped with the state of the
art and newly improved Honeywell APEX integrated
all glass cockpit which sets new standards for
simplicity, reliability and technology.
Propulsion consists of two rear mounted FADEC
controlled Williams J44-3A engines with 1.270 kg
of thrust, and a proven track record from use in
many of today's leading light jets.
A fully-equipped pre-production
aircraft will enter service at the beginning of
2007 and will be used to complete final
certification and reliability testing. It will
be fitted with a full interior and major
avionics options. |
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Developing nation: |
Germany |
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Manufacturer/designer: |
Grob Aerospace. |
| Production line: |
Tussenhausen-Mattsies, Germany. |
| Type aircraft: |
Business jet. |
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First flight: |
July 20, 2005, D-ISPN. |
| First delivery: |
end of 2007. |
| |
Grob G180 SPn |
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Cockpit crew: |
1- 2. |
| Passengers one
class: |
8 -9. |
| Cabin length: |
5,10 m. |
| Cabin diameter: |
1,52 m. |
| Cabin height: |
1,64 m. |
| Cabin volume: |
11,5 m³. |
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Wing span: |
14,86 m over winglets. |
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Fuselage length: |
14,81 m. |
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Fuselage diameter: |
1,60 m. |
| Height: |
5,12 m. |
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Engines: |
Two Williams FJ44-3A turbofans
Thrust: 2 x 2800 lbs at sea level, ISA. |
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Weight: |
- fuel: 200 kg.
- max. payload: 1.130 Kg. |
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Max. take off weight: |
6.300 Kg. |
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Cruise speed: |
504 km/h. |
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Max. speed: |
754 km/h. |
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Stall speed: |
143 km/h. |
| Rate of climb: |
22 m/sec. |
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Service ceiling: |
12.500 m. |
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Max. range: |
3.335 km. |
| Performance: |
- take-off run 914 m at max.
take-off weight.
- landing run 899 m at max.
landing weight. |
1 Grob G180 SPn
written-off by accidents:
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29-11-2006 |
D-CGSP |
90002 |
Grob Aerospace, second prototype crashed
shortly after take-off from
Tussenhaussen-Mattsies airport, Germany,
Test-pilot killed. |
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