Pt. 60, App. C

14 CFR Ch. I (1-1-19 Edition)
TABLE C1A - MINIMUM SIMULATOR REQUIREMENTS - Continued
QPS requirements

Simulator levels

Information

Entry No.

kpayne on VMOFRWIN702 with $$_JOB

General simulator requirements

B

5.c. ...........

The simulator must have a motion (force cueing) system that produces cues at least
equivalent to those of a six-degrees-of-freedom, synergistic platform motion system
(i.e., pitch, roll, yaw, heave, sway, and
surge).
An SOC is required.

5.d. ...........

The simulator must provide for the recording
of the motion system response time.
An SOC is required.

5.e. ...........

The simulator must provide motion effects programming to include the following:.
(1) Runway rumble, oleo deflections, effects of
ground speed, uneven runway, characteristics.
(2) Buffets due to transverse flow effects.
(3) Buffet during extension and retraction of
landing gear.
(4) Buffet due to retreating blade stall.
(5) Buffet due to vortex ring (settling with
power).
(6) Representative cues resulting from touchdown.
(7) High speed rotor vibrations.
(8) Tire failure dynamics ...................................
(9) Engine malfunction and engine damage
(10) Airframe ground strike
(11) Motion vibrations that result from atmospheric disturbances.

C

D

X

X

X

X

X

X

X

X

X

X

5.f. ............

The simulator must provide characteristic motion vibrations that result from operation of
the helicopter (for example, retreating blade
stall, extended landing gear, settling with
power) in so far as vibration marks an event
or helicopter state, which can be sensed in
the flight deck.

6. ..............

Visual System ..................................................

6.a. ...........

The simulator must have a visual system providing an out-of-the-flight deck view.

X

6.b. ...........

The simulator must provide a continuous fieldof-view of at least 75Section horizontally and 30Section
vertically per pilot seat. Both pilot seat visual
systems must be operable simultaneously.
The minimum horizontal field-of-view coverage must be plus and minus one-half (1-2)
of the minimum continuous field-of-view requirement, centered on the zero degree azimuth line relative to the aircraft fuselage. An
SOC must explain the geometry of the installation.
An SOC is required.

X

Notes

X

For air turbulence, general purpose disturbance models are acceptable if, when used,
they produce test results that approximate
demonstrable flight test data.

X

The simulator should be programmed and instrumented in such a manner that the characteristic buffet modes can be measured
and compared to helicopter data.

Additional horizontal field-of-view capability
may be added at the sponsor-s discretion
provided the minimum field-of-view is retained.
X

X

330

VerDate Sep<11>2014

16:30 Jun 25, 2019

Jkt 247047

PO 00000

Frm 00340

Fmt 8010

Sfmt 8002

Q:\14\14V2.TXT

PC31