124 

14 CFR Ch. I (1–1–19 Edition) 

Pt. 60, App. A 

T

ABLE

A2E—A

LTERNATIVE

D

ATA

S

OURCES

, P

ROCEDURES

, 

AND

I

NSTRUMENTATION

—Continued 

QPS REQUIREMENTS 

The standards in this table are required if the data gathering methods described in paragraph 

9 of 

Appendix A are not used. 

Information 

Table of objective tests 

Sim level 

Alternative data sources, procedures, and 

instrumentation 

Notes 

Test entry number and title 

A 

B 

1.b.7. Performance. Takeoff. 

Rejected Takeoff.

X 

X 

Data may be acquired with a syn-

chronized video of calibrated airplane 
instruments, thrust lever position, en-
gine parameters, and distance (e.g., 
runway markers). A stop watch is re-
quired..

1.c. 1. Performance. Climb. Nor-

mal Climb all engines oper-
ating..

X 

X 

Data may be acquired with a syn-

chronized video of calibrated airplane 
instruments and engine power through-
out the climb range.

1.c.2. Performance. Climb. One 

engine Inoperative Climb.

X 

X 

Data may be acquired with a syn-

chronized video of calibrated airplane 
instruments and engine power through-
out the climb range.

1.c.4. Performance. Climb. One 

Engine Inoperative Approach 
Climb (if operations in icing 
conditions are authorized).

X 

X 

Data may be acquired with a syn-

chronized video of calibrated airplane 
instruments and engine power through-
out the climb range.

1.d.1. Cruise/Descent. Level 

flight acceleration..

X 

X 

Data may be acquired with a syn-

chronized video of calibrated airplane 
instruments, thrust lever position, en-
gine parameters, and elapsed time.

1.d.2. Cruise/Descent. Level 

flight deceleration..

X 

X 

Data may be acquired with a syn-

chronized video of calibrated airplane 
instruments, thrust lever position, en-
gine parameters, and elapsed time.

1.d.4. Cruise/Descent. Idle de-

scent.

X 

X 

Data may be acquired with a syn-

chronized video of calibrated airplane 
instruments, thrust lever position, en-
gine parameters, and elapsed time.

1.d.5. Cruise/Descent. Emer-

gency Descent.

X 

X 

Data may be acquired with a syn-

chronized video of calibrated airplane 
instruments, thrust lever position, en-
gine parameters, and elapsed time.

1.e.1. Performance. Stopping. 

Deceleration time and dis-
tance, using manual applica-
tion of wheel brakes and no 
reverse thrust on a dry run-
way.

X 

X 

Data may be acquired during landing tests 

using a stop watch, runway markers, 
and a synchronized video of calibrated 
airplane instruments, thrust lever posi-
tion and the pertinent parameters of en-
gine power.

1.e.2. Performance. Ground. 

Deceleration Time and Dis-
tance, using reverse thrust 
and no wheel brakes.

X 

X 

Data may be acquired during landing tests 

using a stop watch, runway markers, 
and a synchronized video of calibrated 
airplane instruments, thrust lever posi-
tion and pertinent parameters of engine 
power.

1.f.1. Performance. Engines. 

Acceleration.

X 

X 

Data may be acquired with a syn-

chronized video recording of engine in-
struments and throttle position.

1.f.2. Performance. Engines. 

Deceleration.

X 

X 

Data may be acquired with a syn-

chronized video recording of engine in-
struments and throttle position.

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