kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
Jkt 247047
PO 00000

Landing.

1.j.1. .......................

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

1.j.2. through 1.j.3

Reserved.

Frm 00455

1.j. ..........................

Sfmt 8002

445

Fmt 8010

Rotor Speed - Section3% Pitch Attitude
Section2Section Roll Attitude - Section3Section Yaw Attitude - Section5Section Airspeed - Section5 kts.
Vertical Velocity - Section200 fpm
(1.00 m/sec) or 10%.

Cruise; or Climb .......

Record results of a rapid throttle
reduction to idle. If accomplished in cruise, results must
be for the maximum range airspeed. If accomplished in
climb, results must be for the
maximum rate of climb airspeed at or near maximum
continuous power.

Airspeed - Section3 kts, Altitude - Section20 ft
(6.1 m) Torque - Section3%, Rotor
Speed - Section1.5%, Pitch Attitude - 
Section1.5Section, Bank Attitude - Section1.5Section,
Heading - Section2Section,
Longitudinal
Control Position - Section10%, Lateral Control Position - Section10%,
Directional Control Position - 
Section10%, Collective Control Position - Section10%.

Approach ..................

Record results of the approach
and landing profile (running
landing or approach to a
hover). The criteria apply only
to those segments at airspeeds
above effective translational lift.
Record the results from 200 ft
AGL (61 m) to the landing or to
where the hover is established
prior to landing.

X

X

X

Federal Aviation Administration, DOT

16:30 Jun 25, 2019

Entry ..............................

Q:\14\14V2.TXT
PC31

Pt. 60, App. D