kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
Jkt 247047
PO 00000

1.g. .............

Torque - Section3%, Pitch Attitude - Section1.5Section, Sideslip
Angle - Section2Section, Longitudinal
Control Position - Section5%,
Lateral Control Position - 
Section5%, Directional Control
Position - Section5%, Collective
Control Position - Section5%.

Cruise (Augmentation On and
Off).

Record results for two gross
weight and CG combinations with varying trim
speeds throughout the airspeed envelope. May be a
series of snapshot tests.

X

X

X

Vertical Velocity - Section100 fpm
(6.1m/sec) or Section10%, Pitch
Attitude - Section1.5Section, Sideslip
Angle - Section2Section, Longitudinal
Control Position - Section5%,
Lateral Control Position - 
Section5%, Directional Control
Position - Section5%, Collective
Control Position - Section5%.

All engines operating; One
engine inoperative; Augmentation System(s) On
and Off.

Record results for two gross
weight and CG combinations. The data presented
must be for normal climb
power conditions. May be a
series of snapshot tests.

X

X

X

Climb
Performance and Trimmed
Flight Control Positions.

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Descent Performance and
Trimmed Flight Control Positions.

Torque - Section3%, Pitch Attitude - Section1.5Section, Sideslip
Angle - Section2Section, Longitudinal
Control Position - Section5%,
Lateral Control Position - 
Section5%, Directional Control
Position - Section5%, Collective
Control Position - Section5%.

At or near 1,000 fpm (5 m/
sec) rate of descent (RoD)
at normal approach speed.
Augmentation System(s)
On and Off.

Results must be recorded for
two gross weight and CG
combinations. May be a
series of snapshot tests.

X

X

X

1.h.2. ..........

Autorotation Performance
and Trimmed Flight Control
Positions.

Pitch Attitude - Section1.5Section, Sideslip
Angle - Section2Section, Longitudinal
Control Position - Section5%,
Lateral Control Position - 
Section5%, Directional Control
Position - Section5%, Collective
Control Position - Section5%,
Vertical Velocity - Section100 fpm
or 10%, Rotor Speed - 
Section1.5%.

Steady descents. Augmentation System(s) On and Off.

Record results for two gross
weight conditions. Data
must be recorded for normal operating RPM. (Rotor
speed tolerance applies
only if collective control position is full down.) Data
must be recorded for
speeds from 50 kts, Section5 kts,
through at least maximum
glide distance airspeed, or
maximum allowable autorotation airspeed, whichever is slower. May be a
series of snapshot tests.

X

X

X

1.i. ...............

Autorotation

Pt. 60, App. C

Descent

1.h.1. ..........

PC31

1.h. .............

This test validates performance at speeds above
maximum endurance airspeed.

Federal Aviation Administration, DOT

16:30 Jun 25, 2019

Performance and Trimmed
Flight Control Positions.