360 

14 CFR Ch. I (1–1–19 Edition) 

Pt. 60, App. C 

T

ABLE

C2A—F

ULL

F

LIGHT

S

IMULATOR

(FFS) O

BJECTIVE

T

ESTS

—Continued 

QPS requirements 

Information 

Test 

Tolerance(s) 

Flight condition 

Test details 

Simulator 

level 

Notes 

Entry No. 

Title 

B C D 

4.g.2. ..........

Not less than 25:1 .................

N/A .........................................

An SOC is required and must 

include the relevant cal-
culations. 

X X 

4.h. .............

Visual ground segment 

The visible segment in the 

simulator must be 

±

20% of 

the segment computed to 
be visible from the heli-
copter flight deck. This tol-
erance may be applied at 
the far end of the displayed 
segment. However, lights 
and ground objects com-
puted to be visible from the 
helicopter flight deck at the 
near end of the visible seg-
ment must be visible in the 
simulator. 

Landing configuration, with 

the aircraft trimmed for the 
appropriate airspeed, 
where the MLG are at 100 
ft (30 m) above the plane 
of the touchdown zone, on 
the electronic glide slope 
with an RVR value set at 
1,200 ft (350 m). 

The QTG must contain ap-

propriate calculations and a 
drawing showing the data 
used to establish the heli-
copter location and the 
segment of the ground that 
is visible considering de-
sign eye point, the heli-
copter attitude, flight deck 
cut-off angle, and a visi-
bility of 1200 ft (350 m) 
RVR. Simulator perform-
ance must be measured 
against the QTG calcula-
tions. The data submitted 
must include at least the 
following: 

X 

X 

X  Pre-positioning for this test is 

encouraged, and may be 
achieved via manual or 
autopilot control to the de-
sired position. 

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