kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
QPS requirements

Information

Jkt 247047

Test
Tolerance(s)

Flight condition

Title

2.b.3.b. .......

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

Roll Rate - Section10% or Section3Section/sec.,
Roll Attitude Change - 
Section10% or Section3Section.

Hover Augmentation On and
Off.

2.b.3.c. ........

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

Yaw Rate - Section10% or Section2Section/sec.,
Heading Change - Section10% or
Section2Section.

2.b.3.d. .......

Vertical ...................................

PO 00000

Entry No.

Test details

Simulator
level
B

Notes

Frm 00358
Sfmt 8002

348

Fmt 8010

C

D

Record results for a step control input. The Off-axis response must show correct
trend for unaugmented
cases.

X

X

This is a  - short time -  test
conducted in a hover, in
ground effect, without entering translational flight, to
provide better visual reference.

Hover Augmentation On and
Off.

Record results for a step control input. The Off-axis response must show correct
trend for unaugmented
cases.

X

X

This is a  - short time -  test
conducted in a hover, in
ground effect, without entering translational flight, to
provide better visual reference.

Normal Acceleration - Section0.1 g.

Hover Augmentation On and
Off.

Record results for a step control input. The Off-axis response must show correct
trend for unaugmented
cases.

X

X

PC31

Longitudinal Handling Qualities

2.c.1. ...........

Control Response ..................

Pitch Rate - Section10% or Section2Section/
sec., Pitch Attitude
Change - Section10% or Section1.5Section.

Cruise Augmentation On and
Off.

Results must be recorded for
two cruise airspeeds to include minimum power required speed. Record data
for a step control input.
The Off-axis response
must show correct trend for
unaugmented cases.

X

X

X

2.c.2. ...........

Static Stability ........................

Longitudinal Control Position:
Section10% of change from trim
or Section0.25 in. (6.3 mm) or
Longitudinal Control Force
: Section0.5 lb. (0.223 daN) or
Section10%.

Cruise or Climb. Autorotation.
Augmentation On and Off.

Record results for a minimum
of two speeds on each side
of the trim speed. May be
a series of snapshot tests.

X

X

X

2.c.3. ...........

Dynamic Stability

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

Q:\14\14V2.TXT

2.c. ..............

Pt. 60, App. C

16:30 Jun 25, 2019

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