H160 configuration frozen, but first delivery may slip
28 JULY, 2016 - BY: DOMINIC PERRY - LONDON
Airbus Helicopters has frozen the aeromechanical configuration of its
developmental H160 medium twin, but admits that certification and service entry
may need to slip into early 2019.
Since its first flight in June
last year, the H160 has accumulated about 250h, says programme chief Bernard
Fujarski.
Although it is still working
towards EASA certification at the end of 2018, he says “it may require that we
take some additional months and deliver the first aircraft in 2019” to ensure
the maturity of the helicopter and its production and support processes.
Discussions are continuing with
the H160’s launch customer about a “compromise” on the delivery schedule, he
adds.
Changes to the configuration of
the initial prototype include reshaped cowlings and air intakes, and a settled
design of the rotor mast.
The latter has been particularly
key to reducing vibration levels in the new helicopter, says Fujarksi; three
different mast lengths were tested, with the airframer eventually settling on
an intermediate design, he says.
Airbus
Helicopters
Overall vibration is at an
“unprecedented” low level, he says, even without the use of any damping system.
“We consider the H155 as a benchmark in our range, but the H160 is exceeding
its performance in vibration. What’s amazing is that the vibration level is
good whatever the flight profile.”
High temperature trials will be
largely wrapped up in the coming weeks in the south of France using aircraft
PT1, although certain tests will be repeated during 2017 using the production
conforming design introduced early next year with PT3.
So far the helicopter has been
exposed to temperatures above 38°C (100°F) and “as predicted we were within our
margins for those parameters”, Fujarski says.
Both current prototypes are
flying with the Turbomeca Arrano engine, but tests using fully calibrated
engines should begin by September, he says, allowing the manufacturer to set
the performance specification – including the crucial maximum take-off weight –
towards the end of the year
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