kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
QPS requirements

Information

Jkt 247047

Test
Tolerance(s)

Flight condition

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

Cyclic .....................................

Breakout - Section0.25 lbs. (0.112
daN) or 25%; Force - Section1.0
lb. (0.224 daN) or 10%.

Ground; Static conditions with
the hydraulic system (if applicable) pressurized; supplemental hydraulic pressurization system may be
used. Trim On and Off.
Friction Off Augmentation
(if applicable) On and Off.

2.a.2. ..........

Collective/Pedals ...................

Breakout - Section0.5 lb. (0.224
daN) or 25%; Force - Section1.0
lb. (0.224 daN) or 10%.

Ground; Static conditions with
the hydraulic system (if applicable) pressurized; supplemental hydraulic pressurization system may be
used. Trim On and Off.
Friction Off. Augmentation
(if applicable) On and Off.

2.a.3. ..........

Brake Pedal Force vs. Position.

Section5 lbs. (2.224 daN) or 10%.

Ground; Static conditions.

2.a.4. ..........

Trim System Rate (all applicable systems).

Rate - Section10%.

Ground; Static conditions.
Trim On, Friction Off.

Test details

Notes

Frm 00356
Sfmt 8002

346

Fmt 8010
Q:\14\14V2.TXT

B

C

D

Record results for an uninterrupted control sweep to the
stops. (This test does not
apply if aircraft hardware
modular controllers are
used.)

X

X

X

Flight Test Data for this test
does not require the rotor
to be engaged/turning. The
phrase  - if applicable -  regarding stability augmentation systems means if an
augmentation system is
available and if this system
may be operational on the
ground under static conditions as described here.

Record results for an uninterrupted control sweep to the
stops.

X

X

X

Flight Test Data for this test
does not require the rotor
to be engaged/turning. The
phrase  - if applicable -  regarding stability augmentation system means if a stability augmentation system
is available and if this system may be operational on
the ground under static
conditions as described
here.

X

X

X

X

X

X

PC31

The tolerance applies to the
recorded value of the trim
rate.

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