Airbus Helicopters BK 117B2 – Operating Costs, Specifications, and Performance Data

Compare the fixed costs, variable cost, and performance of Airbus Helicopters BK 117B2 to over 500 jets, turboprops, helicopters and piston aircraft, with accurate data from Conklin & de Decker.

Summary

FULL AIRCRAFT NAME
Airbus Helicopters BK 117B2
AIRCRAFT NAME
BK 117B2
AIRCRAFT MANUFACTURER
Airbus Helicopters
MAX RANGE (30 MIN RESERVE)
238 nm
SPEED
133 kts
PASSENGERS
9 people
ACQUISITION COST
$1500000
ENGINES
Honeywell Engines LTS-101-750 2
WINGSPAN
8.2 ft
IFR CERTIFIED
Yes

Aircraft History

Design of the BK 117 medium twin-engine helicopters was started in 1977 as a joint effort between MBB GMBH in Germany and Kawasaki Heavy Industries in Japan. MBB (now Eurocopter) has responsibility for design and manufacturing of the dynamic system, the tail boom, landing gear, and various systems integration. Kawasaki has responsibility for the fuselage, transmission and various systems. Final assembly takes place at two locations, one at Donauworth, Germany, and one at Gifu, Japan.
 
It is an 8- to 11-place medium twin-engine turbine helicopter that is characterized by a large combined passenger cabin and luggage compartment that extends the full length of the fuselage. Clamshell doors at the back of the fuselage allow access to this combined passenger and luggage compartment that has an unobstructed length of over 9 feet. The standard seating configuration has a pilot and one passenger seat up front and two or three rows of three seats in the back. Alternatively, two litters can be loaded through the clamshell doors and placed side by side on the flat floor. In this configuration, there is also room for two or three medical attendants.
 
The drivetrain uses two Honeywell (Lycoming at the time) LTS 101-750B1 engines and a rigid, hingeless, four-bladed rotor based on the Bo 105 design. The main rotor blades are made of composite construction, as are the two tail rotor blades. The tail rotor is mounted at the top of the vertical fin, which provides unobstructed access to the rear clamshell doors. The primary fuselage structure is constructed of aluminum alloy. Secondary fuselage structures are made of Kevlar and other composites.
 
The first flight of the BK 117 took place in 1979 and certification to the standards of FAR 29 was obtained in 1983. Certification for Category A operations and single-pilot IFR operations was also obtained. First deliveries were made in 1983 and the helicopter has been in production since that time. To date, over 400 BK 117 models have been delivered. Aircraft that are assembled in Japan have serial numbers that start with 1001, whereas aircraft that are assembled in Germany have serial numbers that start with 7001. The BK 117 B2 was certificated in 1992 and was in production from 1992 to 1998.