Pt. 60, App. A

14 CFR Ch. I (1-1-19 Edition)

TABLE A2E - ALTERNATIVE DATA SOURCES, PROCEDURES, AND INSTRUMENTATION - 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.
Table of objective tests

kpayne on VMOFRWIN702 with $$_JOB

Test entry number and title

Sim level

Information

Notes
Alternative data sources, procedures, and
instrumentation

A

B

1.b.7. Performance. Takeoff.
Rejected Takeoff.

X

X

Data may be acquired with a synchronized video of calibrated airplane
instruments, thrust lever position, engine parameters, and distance (e.g.,
runway markers). A stop watch is required..

1.c. 1. Performance. Climb. Normal Climb all engines operating..

X

X

Data may be acquired with a synchronized video of calibrated airplane
instruments and engine power throughout the climb range.

1.c.2. Performance. Climb. One
engine Inoperative Climb.

X

X

Data may be acquired with a synchronized video of calibrated airplane
instruments and engine power throughout 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 synchronized video of calibrated airplane
instruments and engine power throughout the climb range.

1.d.1. Cruise/Descent. Level
flight acceleration..

X

X

Data may be acquired with a synchronized video of calibrated airplane
instruments, thrust lever position, engine parameters, and elapsed time.

1.d.2. Cruise/Descent. Level
flight deceleration..

X

X

1.d.4. Cruise/Descent. Idle descent.

X

X

Data may be acquired with a synchronized video of calibrated airplane
instruments, thrust lever position, engine parameters, and elapsed time.
Data may be acquired with a synchronized video of calibrated airplane
instruments, thrust lever position, engine parameters, and elapsed time.

1.d.5. Cruise/Descent. Emergency Descent.

X

X

Data may be acquired with a synchronized video of calibrated airplane
instruments, thrust lever position, engine parameters, and elapsed time.

1.e.1. Performance. Stopping.
Deceleration time and distance, using manual application of wheel brakes and no
reverse thrust on a dry runway.

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 position and the pertinent parameters of engine power.

1.e.2. Performance. Ground.
Deceleration Time and Distance, 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 position and pertinent parameters of engine
power.

1.f.1. Performance. Engines.
Acceleration.

X

X

Data may be acquired with a synchronized video recording of engine instruments and throttle position.

1.f.2. Performance. Engines.
Deceleration.

X

X

Data may be acquired with a synchronized video recording of engine instruments and throttle position.

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