Grob spn  
Initial Operational Capability (IOC): April 2008
Maiden Flight: 20 June 2006
Total Production: 76
Origin: Switzerland
Corporations: Grob Aerospace
Parent System: spn
Initial Operational Capability (IOC): April 2008
Maiden Flight: 19 June 2006
Total Production: 76
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Description: The spn is a twin-engine light business jet designed by Grob Aerospace combining short and unimproved runway performance of turboprop aircraft with comfort cabin and cruise speed of luxury jets. The spn offers a seating capacity for up to nine passengers and the cabin can be easily and quickly converted for cargo transport or air ambulance roles. The aircraft's maximum range varies from 3,121 to 3,334 kilometers carrying eight or six passengers plus a single pilot. First deliveries and EASA certification for single pilot operation are expected in April 2008 with FAA certification following in the second quarter of 2008.

The Grob spn light jet is equipped with all-glass cockpit, state-of-the-art Primus Apex avionics from Honeywell and two FJ44-3A engines from Williams International developing 2,800-lb of thrust each and fitted with Full Authority Digital Engine Control (FADEC) system. The aircraft's cabin can be configured following Executive layout with six passengers or Business layout for eight passengers. Besides, its durable carbon fiber airframe has been designed for low maintenance and long service life.

Grob spn Specifications

Crew: 2
Number of Engines: 2
Passengers: 8
Service Life Flight Hours: 28,000
Cabin Height: 1.64 meter (65 inch)
Cabin Length: 5.10 meter (201 inch)
Cabin Width: 1.52 meter (60 inch)
Height: 5.12 meter (202 inch)
Length: 14.8 meter (583 inch)
Wingspan: 14.9 meter (49 foot)
Max Maneuvering Load Factor: 3.10 g
Min Maneuvering Load Factor: -1 g
Landing Run Distance: 814 meter (2,671 foot)
Max Range: 3,334 kilometer (1,800 nautical mile)
Operational Altitude: 12,497 meter (41,001 foot)
Take Off Run Distance: 914 meter (2,999 foot)
Climb Rate: 22 mps (4,314 fpm)
Cruise Speed: 769 kph (415 KTAS)
Top Speed at High Altitude: 0.70 mach (452 KTAS)
Baggage Capacity: 57 cu ft (1.62 metric ton)
Cabin Volume: 405 cu ft (11.5 metric ton)
Fuel Tank Capacity: 660 galon (2,508 liter)
Fuel Load: 2,000 kilogram (4,409 pound)
Max Takeoff Thrust: 5,600 pound
Max Takeoff Weight: 6,300 kilogram (13,889 pound)
Payload: 1,130 kilogram (2,491 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Grob spn News

There are 2 news between
19 May 2008 and 19 May 2008
Monday, May 19, 2008Grob Aerospace Teams up with FedEx to Offer Fastest Parts Distribution for spn Customers
Grob Aerospace Announces Flight Training Program for spn Jet

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