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444 

14 CFR Ch. I (1–1–18 Edition) 

Pt. 60, App. D 

T

ABLE

D2A—F

LIGHT

T

RAINING

D

EVICE

(FTD) O

BJECTIVE

T

ESTS

—Continued 

QPS requirements 

Information 

Test 

Tolerances 

Flight conditions 

Test details 

FTD level 

Notes 

Entry No. 

Title 

5 6 7 

Performance and 

Trimmed Flight Con-
trol Positions.

Vertical Velocity—±100 fpm (61 

m/sec) or ±10% Pitch Atti-
tude—±1.5°  Sideslip Angle— 
±2°  Longitudinal Control Posi-
tion—±5% Lateral Control Posi-
tion—±5% Directional Control 
Position—±5% Collective Con-
trol Position—±5%.

All engines operating 
One engine inoper-

ative.

Augmentation Sys-

tem(s) On and Off.

Record results for two gross 

weight and CG combinations. 
The data presented must be for 
normal climb power conditions. 
May be a series of snapshot 
tests.

X X X 

1.h. ........................

Descent. 

1.h.1. .....................

Descent Performance 

and Trimmed Flight 
Control Positions.

Torque—±3% Pitch Attitude— 

±1.5°  Sideslip Angle—±2°  Lon-
gitudinal Control Position—±5% 
Lateral Control Position—±5% 
Directional Control Position— 
±5% Collective Control Posi-
tion—±5%.

At or near 1,000 fpm 

(5 m/sec) rate of 
descent (RoD) at 
normal approach 
speed.

Augmentation Sys-

tem(s) On and Off.

Record results for two gross 

weight and CG combinations. 
May be a series of snapshot 
tests.

X X X 

1.h.2. .....................

Autorotation Perform-

ance and Trimmed 
Flight Control Posi-
tions.

Pitch Attitude—±1.5° 

Sideslip 

Angle—±2°  Longitudinal Con-
trol Position—±5% Lateral Con-
trol Position—±5% Directional 
Control Position—±5% Collec-
tive Control Position—±5%.

Steady descents. 

Augmentation Sys-
tem(s) On and Off.

Record results for two gross 

weight conditions. Data must 
be recorded for normal oper-
ating RPM. (Rotor speed toler-
ance applies only if collective 
control position is full down.) 
Data must be recorded for 
speeds from 50 kts, ±5 kts 
through at least maximum glide 
distance airspeed. May be a 
series of snapshot tests.

X X X 

1.i. ..........................

Autorotation. 

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