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Clockwise aircraft propeller B 1650/1950-A-3B (B 04)
60 - 65in100 - 150hp2000 - 2500rpm

Clockwise aircraft propeller - B 1650/1950-A-3B (B 04) - Peszke - 60 - 65in / 100 - 150hp / 2000 - 2500rpm
Clockwise aircraft propeller - B 1650/1950-A-3B (B 04) - Peszke - 60 - 65in / 100 - 150hp / 2000 - 2500rpm
Clockwise aircraft propeller - B 1650/1950-A-3B (B 04) - Peszke - 60 - 65in / 100 - 150hp / 2000 - 2500rpm - image - 2
Clockwise aircraft propeller - B 1650/1950-A-3B (B 04) - Peszke - 60 - 65in / 100 - 150hp / 2000 - 2500rpm - image - 3
Clockwise aircraft propeller - B 1650/1950-A-3B (B 04) - Peszke - 60 - 65in / 100 - 150hp / 2000 - 2500rpm - image - 4
Clockwise aircraft propeller - B 1650/1950-A-3B (B 04) - Peszke - 60 - 65in / 100 - 150hp / 2000 - 2500rpm - image - 5
Clockwise aircraft propeller - B 1650/1950-A-3B (B 04) - Peszke - 60 - 65in / 100 - 150hp / 2000 - 2500rpm - image - 6
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Characteristics

Configuration
clockwise
Diameter
60 - 65in
Power capacity
100 - 150hp
Maximum rotation speed
2500 - 3000rpm, 2000 - 2500rpm
Number of blades
3 teeth
Technology
adjustable pitch
Material
composite
Applications
for light aircraft

Description

Full-carbon fibre composite blade construction, 3-blade configuration, right rotation, aeroelastic properties, ground adjustable pitch, steel mat paint finish with red tips, blade leading edge protection tape. HUB PS2 3B Billet CNC machined duraluminium 7075 material, anti-corrosive protection (anodizing). Installation pattern dimensions: centre hole ø47 mm, mounting holes 6xø8/ø75 mm. PARAMETERS Weight: 3230 g Inertia momentum: 3400 kG.cm² EXEMPLARY APPLICATION PULLER Aircrafts with engines ROTAX 912 UL; V max 180-250 km/h. Aircrafts with engines ROTAX 912 ULS; V max 220-300 km/h.
*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.