Introduction to T-45C Configuration
T-45C TS, ADV & IUT ENG-01
B. Airborne data recording system 1.4.19.5
Sg 11, fr 9
Air Data Recorder
1.
Description: The airborne data recording system
Push Button
consists of an airborne data recorder (ADR);
Fig 23: Cockpit
incident record push button in each cockpit, an
Armament Controls/
ADR BIT panel, and aircraft system sensors
Indications
2.
Function: The system provides the combined
functions of a flight incident recorder, engine usage
monitoring, and structural fatigue monitoring
IV. Centralized warning system (CWS) 1.4.4.3.1.2
Sg 2, fr 2
Lesson Organization
T-45C CONFIGURATION
LESSON NOTES
* Overview
* Major aircraft systems
overview
The CWS will not be taught in this curriculum as a separate,
* Other T-45C aircraft systems
* Centralized warning
major aircraft system. Each of its indications and the conditions
system (CWS)
that cause the indication will be taught in conjunction with the
associated aircraft system--for example, GTS FIRE, WHEELS,
and L BAR lights. However, because the warning and caution
annunciations cross multiple system boundaries and are critical
to flight safety, they will be presented here.
Use the cockpit wall chart to identify the location of cockpit
Wall Chart: T-45C
Cockpit
components throughout this lesson.
A.
MASTER ALERT switch/light
?
The MASTER ALERT light provides what indication?
ANSWER: It alerts the aircrew to a warning or caution
indication on the warning and caution advisory panels. It also
flashes in conjunction with the illumination of the FIRE or L
BAR warning lights.
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