kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
QPS requirements

Information

Jkt 247047

Test

FTD level
Tolerances

Flight conditions

Test details

Notes
5

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

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

Pitch Rate - Section10% or Section2Section/sec.
Pitch Attitude Change - Section10%
or 1.5Section.

Hover. Augmentation
On and Off.

Record results for a step control
input. The Off-axis response
must show correct trend for unaugmented cases. This test
must be conducted in a hover,
in ground effect, without entering translational flight.

X

This is a  - short time -  test.

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

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

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

Hover Augmentation
On and Off.

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

X

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

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

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

Yaw Rate - Section10% or Section2Section/sec. Hover Augmentation
Heading Change - Section10% or Section2Section.
On and Off.

Record results for a step control
input. The Off-axis response
must show correct trend for unaugmented cases. This test
must be conducted in a hover,
in ground effect, without entering translational flight.

X

This is a  - short time -  test.

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

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

Normal Acceleration Section0.1g ...........

Hover Augmentation
On and Off.

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

X

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

Longitudinal Handling Qualities.

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

Control Response .........

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.

Frm 00458
Sfmt 8002

448

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

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

X

6

X

7

X

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

Title

PO 00000

Entry No.

Pt. 60, App. D

16:30 Jun 25, 2019

TABLE D2A - FLIGHT TRAINING DEVICE (FTD) OBJECTIVE TESTS - Continued