kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
QPS requirements

Information

Jkt 247047

Test
Tolerance(s)
Entry No.
4.g.2. ..........

PO 00000

4.h. .............

Flight condition

Test details

Title

Simulator
level
B

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360

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N/A .........................................

An SOC is required and must
include the relevant calculations.

The visible segment in the
simulator must be Section20% of
the segment computed to
be visible from the helicopter flight deck. This tolerance may be applied at
the far end 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.

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

The QTG must contain appropriate calculations and a
drawing showing the data
used to establish the helicopter location and the
segment of the ground that
is visible considering design eye point, the 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:

D

X

X

X

X

Notes

Visual ground segment
X

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

PC31

14 CFR Ch. I (1-1-19 Edition)

Q:\14\14V2.TXT

Not less than 25:1 .................

C

Pt. 60, App. C

16:30 Jun 25, 2019

TABLE C2A - FULL FLIGHT SIMULATOR (FFS) OBJECTIVE TESTS - Continued