kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
Jkt 247047

Ground Takeoff .....................

If brakes are used, brake
pedal position and brake
system pressure must be
matched to the helicopter
flight test value.

X

X

X

1.b.3. ..........

Taxi ........................................

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

Ground ...................................

Record results for control position and pitch attitude
during ground taxi for a
specific ground speed,
wind speed and direction,
and density altitude.

X

X

X

1.b.4. ..........

Brake Effectiveness ...............

Section10% of time and distance.

Ground ...................................

X

X

X

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

Takeoff
When the speed range for the following tests is less than 40 knots, the applicable airspeed tolerance may be applied to either airspeed or ground speed, as appropriate.

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

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

Airspeed - Section3 kt, Altitude - 
Section20 ft (6.1m), Torque - 
Section3%, Rotor Speed - Section1.5%,
Vertical Velocity - Section100 fpm
(0.50m/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%.

Ground/Takeoff and Initial
Segment of Climb.

Record results of takeoff
flight path as appropriate to
helicopter model simulated
(running takeoff for Level
B, takeoff from a hover for
Level C and D). For Level
B, 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 (61m) AGL.

X

X

X

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

One Engine Inoperative continued takeoff.

Airspeed - Section3 kt, Altitude - 
Section20 ft (6.1m), Torque - 
Section3%, Rotor Speed - Section1.5%,
Vertical Velocity - Section100 fpm
(0.50m/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%.

Ground/Takeoff; and Initial
Segment of Climb.

Record takeoff flight path as
appropriate to helicopter
model simulated. Results
must be recorded from the
initiation of the takeoff to at
least 200 ft (61m) AGL.

X

X

X

Frm 00351
Sfmt 8002

341

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

Because several kinds of
takeoff procedures can be
performed, the specific
type of takeoff profile
should be recorded to ensure the proper takeoff profile comparison test is
used.

Pt. 60, App. C

Section10% or Section2Section/sec. Turn Rate.

PO 00000

Rate of Turn vs. Pedal Deflection, Brake Application,
or Nosewheel Angle, as
applicable.

Federal Aviation Administration, DOT

16:30 Jun 25, 2019

1.b.2. ..........