Federal Aviation Administration, DOT

Pt. 60, App. A

least two (2) levels so that upon encountering the windshear the pilot may identify
its presence and apply the recommended procedures for escape from such a windshear.
(1) If the intensity is lesser, the performance capability of the simulated airplane in
the windshear permits the pilot to maintain
a satisfactory flightpath; and
(2) If the intensity is greater, the performance capability of the simulated airplane in
the windshear does not permit the pilot to
maintain a satisfactory flightpath (crash).
Note: The means used to accomplish the
 - nonsurvivable -  scenario of paragraph 3.b.(2)
of this attachment, that involve operational
elements of the simulated airplane, must reflect the dispatch limitations of the airplane.
c. Be available for use in the FAA-approved
windshear flight training program.
4. DEMONSTRATIONS
a. The sponsor must identify one survivable takeoff windshear training model and
one survivable approach windshear training
model. The wind components of the survivable models must be presented in graphical
format so that all components of the
windshear are shown, including initiation
point, variance in magnitude, and time or
distance correlations. The simulator must be
operated at the same gross weight, airplane
configuration, and initial airspeed during the
takeoff demonstration (through calm air and
through
the
first
selected
survivable
windshear), and at the same gross weight,
airplane configuration, and initial airspeed
during the approach demonstration (through
calm air and through the second selected
survivable windshear).
b. In each of these four situations, at an
 - initiation point -  (i.e., where windshear
onset is or should be recognized), the recommended procedures for windshear recovery are applied and the results are recorded
as specified in paragraph 5 of this attachment.
c. These recordings are made without inserting programmed random turbulence.
Turbulence that results from the windshear
model is to be expected, and no attempt may
be made to neutralize turbulence from this
source.
d. The definition of the models and the results of the demonstrations of all four?(4)
cases described in paragraph 4.a of this attachment, must be made a part of the
MQTG.

kpayne on VMOFRWIN702 with $$_JOB

5. RECORDING PARAMETERS
a. In each of the four MQTG cases, an electronic recording (time history) must be made
of the following parameters:
(1) Indicated or calibrated airspeed.
(2) Indicated vertical speed.
(3) Pitch attitude.

(4) Indicated or radio altitude.
(5) Angle of attack.
(6) Elevator position.
(7) Engine data (thrust, N1, or throttle position).
(8) Wind magnitudes (simple windshear
model assumed).
b. These recordings must be initiated at
least 10 seconds prior to the initiation point,
and continued until recovery is complete or
ground contact is made.
6. EQUIPMENT INSTALLATION AND OPERATION
All windshear warning, caution, or guidance hardware installed in the simulator
must operate as it operates in the airplane.
For example, if a rapidly changing wind
speed and/or direction would have caused a
windshear warning in the airplane, the simulator must respond equivalently without instructor/evaluator intervention.
7. QUALIFICATION TEST GUIDE
a. All QTG material must be forwarded to
the NSPM.
b. A simulator windshear evaluation will
be scheduled in accordance with normal procedures. Continuing qualification evaluation
schedules will be used to the maximum extent possible.
c. During the on-site evaluation, the evaluator will ask the operator to run the performance tests and record the results. The
results of these on-site tests will be compared to those results previously approved
and placed in the QTG or MQTG, as appropriate.
d. QTGs for new (or MQTGs for upgraded)
simulators must contain or reference the information described in paragraphs 2, 3, 4, and
5 of this attachment.
END QPS REQUIREMENTS
lllllllllllllllllllllll
BEGIN INFORMATION
8. SUBJECTIVE EVALUATION
The NSPM will fly the simulator in at
least two of the available windshear scenarios to subjectively evaluate simulator
performance as it encounters the programmed windshear conditions.
a. One scenario will include parameters
that enable the pilot to maintain a satisfactory flightpath.
b. One scenario will include parameters
that will not enable the pilot to maintain a
satisfactory flightpath (crash).
c. Other scenarios may be examined at the
NSPM-s discretion.
9. QUALIFICATION BASIS
The addition of windshear programming to
a simulator in order to comply with the
qualification for required windshear training

175

VerDate Sep<11>2014

16:30 Jun 25, 2019

Jkt 247047

PO 00000

Frm 00185

Fmt 8010

Sfmt 8002

Q:\14\14V2.TXT

PC31