Bo-208B Specs and Performance
Technical Data
Aircraft Type: BOELKOW JUNIOR
Manufacturer: BOELKOW - APPARATEBAU GmbH
Nabern/Teck Wuerttemberg
Germany
First Year of Manufacture: 1963
Type of Construction: Shoulder Wing, Struts, Enclosed Cabin
Building Material: Aluminium and Composite
Airworthiness Category: CAR Part 3, Standart and Utility
No. of Seats: Two, side by side
Engine: 4 Cylinder, opposite opposed, aircooled,
CONTINENTAL O-200
Engine Performance: 100 hp at 2750 rpm
Propeller: McCauley 1 A 100 MCM 6758 or
6950,
fixed pitch
Landing Gear: fixed trycycle, steerable nosewheel
Weights
Empty Weight: 790 lbs
Fuel and Oil: 134 lbs
Baggage: 44 lbs
Max Takeoff Weight
Standart: 1325 lbs
Utility/Acrobatic: 1270 lbs
Wing loading: 14 lbs/sqft
Power loading: 13.22 lbs/ hp
Dimensions
Wingspan: 16.36 feet
17.68 feet with extended wingtips
Length: 19.17 feet
Height: 4.37 feet
Wing area: 94.20 sqft
102.15 sqft with extended wingtips
Width of Landing Gear: 6.41 feet
Tire Size (all Tires): 5.00 x 5
Fuel Capacity: 21.0 US Gal or
26.4 US Gal optional
Performance
at 1325 lbs MTOW
Max Operating: 153 KCAS
Max Level: 124 KTAS
Max Cruise 75%: 112 KTAS
Touchdown: 51 KCAS
Takeoff Run, Grass, MSL, ISA: 900 feet
Takeoff Run 50 feet, Grass, MSL, ISA: 1720 feet
Landing Roll: 770 feet
Landing Distance: 1480 feet
ROC at Cruise Climb 76 KCAS: 690 feet/min
Service Ceiling: 13.000 feet
Range at 67% at 6.000 feet: 366 NM
Fuel Consumption at 67%: 6.1 US Gal/ hour