(f)
SIGMET’s
and AIRMET’s.
(7)
Use of the DUAT
(a)
Location identifiers.
(b)
Filing flight plans.
(c)
Notices to Airmen (NOTAM’s).
B. Completion Standards. The lesson will be completed when, by oral examination and demonstration, the student displays the ability to interpret and use aviation weather reports and forecasts and can obtain a weather briefing directly from an AFSS or through the use of DUAT.
5. LESSON NO. 3 2:00 HOURS.
A. Objective. This lesson will consist of a review of the previous two lessons and instruction in the use of Coordinated Universal Time (UK),
in-flight weather advisories and weather recognition.
CONTENT:
(1)
Review Lessons No. 1 and 2.
(2)
UTC.
(3)
In-flight weather advisories.
(4)
Weather recognition
from
the ground and inflight.
B. Completion Standards. This lesson will be completed when, by oral examination, the student displays a working knowledge of UTC and in-flight aviation weather advisories.
AC 141~1A
2/18/93
Appendix 2
6. STAGE THREE FINAL WRITTEN EXAMINATION
:30
MINUTES. (A copy of the Stage Three final written examination should be included with the training syllabus when submitted to the FAA FSDO for review. The examination should be comprehensive and contain questions on information covered during this stage.)
STAGE
FOUR
FLIGHT FUNDAMENTALS AND AIRPLANE SYSTEMS: 1390
HOURS
1.
STAGE FOUR OBJECTIVE. To develop the student’s knowledge to operate an airplane safely in high density airport operations, using collision avoidance precautions and radio communication procedures.
2.
STAGE FOUR COMPLETION STANDARDS. This stage will be successfully completed when the student passes the Stage Four final written examination with a grade of 80 percent.
3.
LESSON NO. 1
2:30
HOURS.
A. Objective. During this lesson, the student will be instructed in the fundamentals of flight basic aerodynamics, including load factors.
CONTENT:
(1)
Forces action on an airplane in flight.
(a)
Lift.
(b)
Weight
(c)
Thrust.
(d)
Drag.
(2)
Airfoils.
(a)
Angle of incidence.
(b)
Angle of attack.
(c)
Bernoulli’s Principle.
(3)
Factors affecting lift and drag.
(a)
Wing area,
(b)
Airfoil shape.
(c)
Angle of attack.
(d)
Airspeed.
(e)
Air density.
(4)
Functions of the controls.
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