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81 

Federal Aviation Administration, DOT 

Pt. 60, App. A 

data that will be available early in the flight 
test program will depend on the airplane 
manufacturer’s flight test program design 
and may not be the same in each case. The 
flight test program of the airplane manufac-
turer should include provisions for genera-
tion of very early flight test results for 
flight simulator validation. 

f. The use of preliminary data is not indefi-

nite. The airplane manufacturer’s final data 
should be available within 12 months after 
the airplane’s first entry into service or as 
agreed by the NSPM, the simulator sponsor, 
and the airplane manufacturer. When apply-
ing for interim qualification using prelimi-
nary data, the simulator sponsor and the 
NSPM should agree on the update program. 
This includes specifying that the final data 
update will be installed in the flight simu-
lator within a period of 12 months following 
the final data release, unless special condi-
tions exist and a different schedule is accept-
able. The flight simulator performance and 
handling validation would then be based on 
data derived from flight tests or from other 
approved sources. Initial airplane systems 
data should be updated after engineering 
tests. Final airplane systems data should 
also be used for flight simulator program-
ming and validation. 

g. Flight simulator avionics should stay 

essentially in step with airplane avionics 
(hardware and software) updates. The per-
mitted time lapse between airplane and 
flight simulator updates should be minimal. 
It may depend on the magnitude of the up-
date and whether the QTG and pilot training 
and certification are affected. Differences in 
airplane and flight simulator avionics 
versions and the resulting effects on flight 
simulator qualification should be agreed be-
tween the simulator sponsor and the NSPM. 
Consultation with the flight simulator man-
ufacturer is desirable throughout the quali-
fication process. 

h. The following describes an example of 

the design data and sources that might be 
used in the development of an interim quali-
fication plan. 

(1) The plan should consist of the develop-

ment of a QTG based upon a mix of flight 
test and engineering simulation data. For 
data collected from specific airplane flight 
tests or other flights, the required design 
model or data changes necessary to support 
an acceptable Proof of Match (POM) should 
be generated by the airplane manufacturer. 

(2) For proper validation of the two sets of 

data, the airplane manufacturer should com-
pare their simulation model responses 
against the flight test data, when driven by 
the same control inputs and subjected to the 
same atmospheric conditions as recorded in 
the flight test. The model responses should 
result from a simulation where the following 
systems are run in an integrated fashion and 

are consistent with the design data released 
to the flight simulator manufacturer: 

(a) Propulsion; 
(b) Aerodynamics; 
(c) Mass properties; 
(d) Flight controls; 
(e) Stability augmentation; and 
(f) Brakes/landing gear. 
i. A qualified test pilot should be used to 

assess handling qualities and performance 
evaluations for the qualification of flight 
simulators of new airplane types. 

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a. When a fully validated simulation (i.e., 

validated with flight test results) is modified 
due to changes to the simulated airplane 
configuration, the airplane manufacturer or 
other acceptable data supplier must coordi-
nate with the NSPM if they propose to sup-
ply validation data from an ‘‘audited’’ engi-
neering simulator/simulation to selectively 
supplement flight test data. The NSPM must 
be provided an opportunity to audit the engi-
neering simulation or the engineering simu-
lator used to generate the validation data. 
Validation data from an audited engineering 
simulation may be used for changes that are 
incremental in nature. Manufacturers or 
other data suppliers must be able to dem-
onstrate that the predicted changes in air-
craft performance are based on acceptable 
aeronautical principles with proven success 
history and valid outcomes. This must in-
clude comparisons of predicted and flight 
test validated data. 

b. Airplane manufacturers or other accept-

able data suppliers seeking to use an engi-
neering simulator for simulation validation 
data as an alternative to flight-test derived 
validation data, must contact the NSPM and 
provide the following: 

(1) A description of the proposed aircraft 

changes, a description of the proposed sim-
ulation model changes, and the use of an in-
tegral configuration management process, 
including a description of the actual simula-
tion model modifications that includes a 
step-by-step description leading from the 
original model(s) to the current model(s). 

(2) A schedule for review by the NSPM of 

the proposed plan and the subsequent valida-
tion data to establish acceptability of the 
proposal. 

(3) Validation data from an audited engi-

neering simulator/simulation to supplement 
specific segments of the flight test data. 

c. To be qualified to supply engineering 

simulator validation data, for aerodynamic, 
engine, flight control, or ground handling 

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