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62 

14 CFR Ch. I (1–1–14 Edition) 

Pt. 60, App. A 

T

ABLE

A2A—F

ULL

F

LIGHT

S

IMULATOR

(FFS) O

BJECTIVE

T

ESTS

—Continued 

QPS Requirements 

Information 

Test 

Tolerance 

Flight conditions 

Test details 

Simulator level 

Notes 

Entry No. 

Title 

A B 

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

The requirements of tests h(1) through (6) of this attachment are applicable to computer controlled aircraft 

only. Time history 

results are required for simulator response to control inputs during entry into envelope protection limits including both norma

and degraded control states if the function is different. Set thrust as required to reach the envelope protection function. 

2.h.1.

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

Overspeed

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

±

5 kt airspeed

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

Cruise

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

2.h.2.

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

Minimum Speed

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

±

3 kt airspeed

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

Takeoff, Cruise, and 

Approach or Landing.

X X X 

2.h.3.

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

Load Factor

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

±

0.1 g normal load factor

....

Takeoff, Cruise

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

2.h.4.

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

Pitch Angle

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

±

1.5

° 

pitch angle

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

Cruise, Approach

.........

2.h.5.

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

Bank Angle

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

±

2

° 

or 

±

10% bank angle

......

Approach

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

2.h.6.

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

Angle of Attack

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

±

1.5

° 

angle of attack

...........

Second Segment 

Climb, and Approach 

or Landing.

X X X 

3. Motion System. 

3.a.

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

Frequency response. 

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

Based on Simulator Capa-

bility.

N/A

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

Required as part of the MQTG. The test 

must demonstrate frequency response 

of the motion system.

X X X X 

3.b.

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

Leg balance. 

Based on Simulator Capa-

bility.

N/A

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

Required as part of the MQTG. The test 

must demonstrate motion system leg 

balance as specified by the applicant 

for flight simulator qualification.

X X X X 

3.c.

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

Turn-around check. 

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

Based on Simulator Capa-

bility.

N/A

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

Required as part of the MQTG. The test 

must demonstrate a smooth turn- 

around (shift to opposite direction of 

movement) of the motion system as 

specified by the applicant for flight 

simulator qualification.

X X X X 

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