240 

14 CFR Ch. I (1–1–14 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. 

VerDate Mar<15>2010 

20:48 Jan 30, 2014

Jkt 232047

PO 00000

Frm 00250

Fmt 8010

Sfmt 8002

Q:\14\14V2.TXT

ofr150

PsN: PC150