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VerDate Sep<11>2014
Jkt 247047

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D71
D71
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D71
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R = Rationale included in the data package
Appendix.

D73
D73

Q:\14\14V2.TXT

(d71)
D71
(d73)
(d73)
D71

X

PC31

D73
D73

Eng sim data wl modified EEC accel rate in VDR.
Eng sim data wl modified EEC accel rate in VDR.
No flight test data available; see rationale.

D73

X
X
(x)

X
X

D73

(d71)
D7l

Primary data contained in IPOM.
See engineering rationale for test data in VDR.
Primary data contained in IPOM.
Alternative engine thrust rating flight test data in
VDR.
Alternative engine thrust rating flight test data in
VDR.
Test procedure anomaly; see rationale.
No flight test data available; see rationale.
Primary data contained in IPOM.
Alternative engine thrust rating flight test data in
VDR.
AFM data available (73K).

D73

R
D73

X

D71
D73

X

D71

(d73)

(x)

D71

(d73)

X

(x)

D71

(d73)

X

(x)

D71

(d73)

X

(d71)

D73

No flight test data available; see rationale.

Pt. 60, App. C

X

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Lower case, within parentheses = alternative
validation source.

0

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D73

(d71)
(d71)

Bold upper case =primary validation source.

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(d71)

X
X

(x)

Legend:
D71 =Engine Type (Thrust Rating of71.5K)
D73 =Engine Type (Thrust Rating of73K)

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X
X
X

X

l.e.2.b.

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Rejected Takeoff.
Dynamic Engine Failure After Takeoff.
Normal Climb -All Engines.
Climb - Engine-out, Second Segment.

l.e.l.c.

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l.b.7.
l.b.8.
l.c.l.
l.c.2.

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Comments

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Climb - Engine-out, Enroute.
Engine-out, Approach Climb.
Level Flight Acceleration.
Level Flight Deceleration.
Cruise Performance.
Stopping Time Section Distance
(Wheel brakes I Light weight).
Stopping Time Section Distance
(Wheel brakes/ Med. weight).
Stopping Time Section Distance
(Wheel brakes I Heavy weight).
Stopping Time Section Distance
(Reverse thrust I Light weight).
Stopping Time Section Distance
(Reverse thrust I ~Jed.
Weight).

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Crosswind Takeoff.

l.c.3.
l.c.4.
l.c.5.a.
l.c.5.b.
l.d.l.
l.e.l.a.

Validation Document

d..

l.b.6.

l.e.2.a.

ER09MY08.036</GPH>

Validation
Source

Federal Aviation Administration, DOT

16:30 Jun 25, 2019

ICAO
or
Test Description
lATA#
Notes:
1. Only one page is shown; and some test conditions were
deleted for brevity.
2. Relevant regulatory material should be consulted and
all applicable tests addressed.
3. Validation source, document and comments provided
herein are for reference only and do not constitute
approval for use.
4. CCA mode must be described for each test
condition.
5. If more than one aircraft type (e.g., derivative and
baseline) are used as validation data more columns
may be necessary.
l.a.l.
Minimum Radius Tum.
l.a.2.
Rate of Tum vs. Nosewheel Angle (2 speeds).
l.b.l.
Ground Acceleration Time and Distance.
l.b.2.
Minimum Control Speed, Ground (Vmcg).
l.b.3.
Minimum Unstick Speed (Vmu).
l.b.4.
Normal Takeoff.
l.b.5.
Critical Engine Failure on Takeoff.