kpayne on VMOFRWIN702 with $$_JOB

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Reserved

The QTG must contain relevant
calculations and a drawing
showing the data used to establish the helicopter location
and the segment of the ground
that is visible considering design eyepoint, helicopter attitude, flight deck cut-off angle,
and a visibility of 1200 ft (350
m) RVR. Simulator performance must be measured
against the QTG calculations.
The data submitted must include at least the following: (1)
Static helicopter dimensions as
follows: (i) Horizontal and
vertical distance from main
landing
gear
(MLG)
to
glideslope reception antenna.
(ii) Horizontal and vertical distance from MLG to pilot-s
eyepoint. (iii) Static flight deck
cutoff angle. (2) Approach data
as follows: (i) Identification of
runway. (ii) Horizontal distance
from runway threshold to
glideslope intercept with runway. (iii) Glideslope angle. (iv)
Helicopter pitch angle on approach. (3) Helicopter data for
manual testing: (i) Gross
weight. (ii) Helicopter configuration. (iii) Approach airspeed. If
non-homogenous fog is used to
obscure visibility, the vertical
variation in horizontal visibility
must be described and be included in the slant range visibility calculation used in the
computations.

X

Pre-position for this test is
encouraged, but may be
achieved via manual or
autopilot control to the
desired position.

Pt. 60, App. D

5.

Landing configuration, trimmed for
appropriate airspeed, at 100 ft
(30m) above the
touchdown zone,
on glide slope with
an RVR value set
at 1,200 ft (350m).

Federal Aviation Administration, DOT

16:30 Jun 25, 2019

The visible segment in the simulator must be within 20% of the
segment computed to be visible
from the helicopter flight deck.
The tolerance(s) may be applied at either end or at both
ends of the displayed segment.
However, lights and ground objects computed to be visible
from the helicopter flight deck
at the near end of the visible
segment must be visible in the
simulator.