kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
Jkt 247047
PO 00000
Frm 00363

3.e.1. ..........

Takeoff (all engines).

As specified by the sponsor
for flight simulator qualification.

Ground ...................................

3.e.2. ..........

Hover performance (IGE and
OGE).

As specified by the sponsor
for flight simulator qualification.

3.e.3. ..........

Autorotation (entry).

3.e.4. ..........

Pitch attitude due to initial
climb must dominate over
cab tilt due to longitudinal
acceleration.

See paragraph 6.d., of this
attachment, Motion cueing
performance signature.

X

Sfmt 8002
Q:\14\14V2.TXT
PC31

Associated to test number
1.c.1.

Ground ...................................

X

X

Associated to test number
1.d.

As specified by the sponsor
for flight simulator qualification.

Flight ......................................

X

X

Associated to test number 1.i.

Landing (all engines).

As specified by the sponsor
for flight simulator qualification.

Flight ......................................

X

X

Associated to test number
1.j.1.

3.e.5. ..........

Autorotation (landing).

As specified by the sponsor
for flight simulator qualification.

Flight ......................................

X

X

Associated to test number
1.j.4.

3.e.6. ..........

Control Response

3.e.6.a. .......

Longitudinal ...........................

As specified by the sponsor
for flight simulator qualification.

Flight ......................................

X

X

X

Associated to test number
2.c.1.

3.e.6.b. .......

Lateral. ...................................

As specified by the sponsor
for flight simulator qualification.

Ground ...................................

X

X

X

Associated to test number
2.d.1.a.

3.e.6.c. ........

Directional ..............................

As specified by the sponsor
for flight simulator qualification.

X

X

X

Associated to test number
2.d.1.c.

3.f. ..............

Characteristic Motion (Vibration) Cues - For all of the following tests, the simulator test results must exhibit the overall appearance and trends of the helicopter data, with at least three (3) of the predominant frequency  - spikes -  being present within Section2
Hz.

....

....

....

Characteristic motion cues
may be separate from the
 - main -  motion system.

X

Pt. 60, App. C

X

353

Fmt 8010

X

Federal Aviation Administration, DOT

16:30 Jun 25, 2019

Required as part of MQTG.
These tests must be run
with the motion buffet
mode disabled.