GROB RANGER 160         Grob Aerospace

 

Grob Aerospace - Impression

Grob Aerospace - Impression

Grob Aerospace - Impression

G160_GROB_RANGER_03_en.pdfPDF
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Technical Data
 

Engine Type: Prat & Whitney PT6A-42A

Power SHP: 850 flat rated to 41 C

Propeller: 4-blade Hartzell

Wingspan: 13.0 m / 42.7 ft

Length: 11.5 m / 37.7 ft

Height: 3.4 m / 11.2 ft

Wing area: 20.5 m2 / 220.4 ft2

Aspect ratio: 8.25

Max. take-off mass: 3300 kg / 7275 lb

Max. landing mass: 3300 kg / 7275 lb

Max. payload: 720 kg / 1587 lb

Useable fuel: 1375 ltr. / 363 USGal

Max. cruise speed at 25000 ft / ISA: 270 kts / 500 km/h TAS

Rate of climb at SL / ISA, max. mass ft/min 2360
 
Stalling speed: 61 kcas / 113 km/h

Take off distance to 15 m / 50 ft at SL / ISA, max. mass: 650 m / 2130 ft

Landing distance from 15 m / 50 ft at SL / ISA, max. mass, no reverse: 650 m / 2130 ft

Range with 6 persons at 25000 ft / ISA, 30 min. reserve:

Max range with full tanks at 25000 ft / ISA, 30 min. reserve:

Grob Aerospace - Impression