Width/Span
33.5 ft
(10.20 m)
Empty Wgt
2,116 lb
(960 kg)
Wgt Diff
+1,190 lb
(+540 kg)
(Showcased structural values pertain to the Grob G120A production variant)
Installed:
1 x Lycoming AEIO-540-D4D5 air-cooled flat-six piston engine developing 260 horsepower driving five-bladed propeller at the nose.
Max Speed
199 mph
(320 kph | 173 kts)
Ceiling
18,045 ft
(5,500 m | 3 mi)
Range
957 mi
(1,540 km | 2,852 nm)
Rate-of-Climb
1,280 ft/min
(390 m/min)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the Grob G120A production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
None.
(Not all ordnance types may be represented in the showcase above)
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