kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
QPS requirements

Information

Jkt 247047

Test
Tolerance(s)
Entry No.

Flight condition

Test details

Title

Simulator
level
B

C

Notes

D

+ 3db to Section6db or Section10% of
nominal vibration level in
flight cruise and correct
trend (see comment).

(a) On ground (idle);
(b) In flight

Characteristic vibrations include those that result from
operation of the helicopter
(for example, high airspeed, retreating blade
stall, extended landing
gear, vortex ring or settling
with power) in so far as vibration marks an event or
helicopter state, which can
be sensed in the flight
deck.
[See Table C1A, table entries
5.e. and 5.f.]

X

Correct trend refers to a comparison of vibration amplitudes between different
maneuvers; e.g., if the 1/
rev vibration amplitude in
the helicopter is higher during steady state turns than
in level flight this increasing
trend should be demonstrated in the simulator.
Additional examples of vibrations may include:
(a) Low Section High speed transition to and from hover;
(b) Level flight;
(c) Climb and descent (including vertical climb;
(d) Auto-rotation;
(e) Steady Turns.

3.f.2. ...........

Buffet - Test against recorded
results for characteristic
buffet motion that can be
sensed in the flight deck.

+ 3db to Section6db or Section10% of
nominal vibration level in
flight cruise and correct
trend (see comment).

On ground and in flight.

Characteristic buffets include
those that result from operation of the helicopter (for
example, high airspeed, retreating blade stall, extended landing gear, vortex
ring or settling with power)
in so far as a buffet marks
an event or helicopter
state, which can be sensed
in the flight deck.
[See Table C1A, table entries
5.e. and 5.f.]

X

The recorded test results for
characteristic buffets
should allow the checking
of relative amplitude for different frequencies.
For atmospheric disturbance,
general purpose models
are acceptable which approximate demonstrable
flight test data.

Frm 00364
Sfmt 8002

354

Fmt 8010
Q:\14\14V2.TXT
PC31

4. Visual System
4.a. .............

Visual System Response Time: (Choose either test 4.a.1. or 4.a.2. to satisfy test 4.a., Visual System Response Time Test. This test is also sufficient for motion system response timing and flight deck instrument response timing.)

4.a.1. ..........

Latency

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

Vibrations - to include 1/Rev
and n/Rev vibrations
(where  - n -  is the number
of main rotor blades).

PO 00000

3.f.1. ...........

Pt. 60, App. C

16:30 Jun 25, 2019

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