kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
1.c.2. through 1.c.3

Reserved.

1.d. ........................

Hover.

Jkt 247047

All Engines ....................

PO 00000
Frm 00453

Performance ..................

Sfmt 8002

443

Fmt 8010

1.e. ........................

Q:\14\14V2.TXT

Record results of takeoff flight
path (running takeoff and takeoff from a hover). The criteria
apply only to those segments
at airspeeds above effective
translational lift. Results must
be recorded from the initiation
of the takeoff to at least 200 ft
(61 m) AGL.

X

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

In Ground Effect
(IGE); and Out of
Ground Effect
(OGE).

Record results for light and heavy
gross weights. May be a series
of snapshot tests.

X

Vertical Velocity - Section100 fpm (0.50
m/sec) or Section10%, Directional
Control Position - Section5%, Collective Control Position - Section5%.

From OGE Hover .....

Record results for light and heavy
gross weights. May be a series
of snapshot tests.

X

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.

Level Flight.
Performance and
Trimmed Flight Control Positions.

PC31
Climb.

X

X

X

This test validates performance at speeds above
maximum endurance airspeed.

Pt. 60, App. D

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

Ground/Takeoff and
Initial Segment of
Climb.

Vertical Climb.
Performance ..................

1.f. .........................

Airspeed - Section3 kt, Altitude - Section20 ft
(6.1 m) Torque - Section3%, Rotor
Speed - Section1.5%, Vertical Velocity - Section100 fpm (0.50 m/sec) or
10%, Pitch Attitude - Section1.5Section,
Bank Attitude - Section2Section, Heading - 
Section2Section, Longitudinal Control Position - Section10%, Lateral Control Position - Section10%, Directional Control Position - Section10%, Collective
Control Position - Section10%.

Federal Aviation Administration, DOT

16:30 Jun 25, 2019

1.c.1. ......................