kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
QPS requirements

Information

Jkt 247047

Test
Tolerance(s)

Flight condition

2.d.1.a ........

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

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

Cruise Augmentation On and
Off.

2.d.1.b. .......

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

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

2.d.2. ..........

Directional Static Stability.

Lateral Control Position - 
Section10% of change from trim
or Section0.25 in. (6.3 mm) or
Lateral Control Force - 
Section0.5 lb. (0.223 daN) or
10%, Roll Attitude - Section1.5,
Directional Control Position - Section10% of change from
trim or Section0.25 in. (6.3 mm)
or Directional Control
Force - Section1 lb. (0.448 daN)
or 10%, Longitudinal Control Position - Section10% of
change from trim or Section0.25
in. (6.3 mm), Vertical Velocity - Section100 fpm (0.50m/
sec) or 10%.

Test details

C

D

Record results for at least
two airspeeds, including
the speed at or near the
minimum power required
airspeed.
Record results for a step control input. The Off-axis response must show correct
trend for unaugmented
cases.

X

X

X

Cruise Augmentation On and
Off.

Record data for at least two
airspeeds, including the
speed at or near the minimum power required airspeed.
Record results for a step control input. The Off-axis response must show correct
trend for unaugmented
cases.

X

X

X

Cruise; or Climb (may use
Descent instead of Climb if
desired), Augmentation On
and Off.

Record results for at least
two sideslip angles on either side of the trim point.
The force may be shown
as a cross plot for irreversible systems. May be a series of snapshot tests.

X

X

X

Frm 00360

B

Notes

Sfmt 8002

350

Fmt 8010
Q:\14\14V2.TXT

This is a steady heading
sideslip test at a fixed collective position.

PC31

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

Title

PO 00000

Entry No.

Simulator
level

Pt. 60, App. C

16:30 Jun 25, 2019

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