kpayne on VMOFRWIN702 with $$_JOB

VerDate Sep<11>2014
QPS requirements

Information

Jkt 247047

Test
Tolerance(s)
Entry No.

Flight condition

Test details

Title
Entry ......................................

Simulator
level
B

PO 00000

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 .....................

Frm 00354

Record results of a rapid
throttle reduction to idle. If
the cruise condition is selected, comparison must be
made for the maximum
range airspeed. If the climb
condition is selected, comparison must be made for
the maximum rate of climb
airspeed at or near maximum continuous power.

C

D

X

X

Notes

Sfmt 8002

344

Fmt 8010
PC31

Landing
When the speed range for tests 1.j.1., 1.j.2., or 1.j.3. is less than 40 knots, the applicable airspeed tolerance may be applied to either airspeed or ground speed, as appropriate.

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

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

Airspeed - Section3 kts., Altitude - 
Section20 ft. (6.1m), 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
as appropriate to the helicopter model simulated
(running landing for Level
B, or approach to a hover
for Level C and D). For
Level B, the criteria apply
only to those segments at
airspeeds above effective
translational lift.

X

X

X

1.j.2. ............

One Engine Inoperative.

Airspeed - Section3 kts., Altitude - 
Section20 ft. (6.1m), 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 for both Category A and Category B
approaches and landing as
appropriate to helicopter
model simulated. For Level
B, the criteria apply only to
those segments at airspeeds above effective
translational lift.

X

X

X

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

Q:\14\14V2.TXT

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

Pt. 60, App. C

16:30 Jun 25, 2019

TABLE C2A - FULL FLIGHT SIMULATOR (FFS) OBJECTIVE TESTS - Continued