Garmin G1000 Pilot's Training Guide (Instructor's Reference -04) - Page 11

Ground Lesson 2

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GROUND LESSONS Ground Lesson 2 TRANSITION TO THE PRIMARY FLIGHT DISPLAY (PFD) Objectives Upon completion of this lesson, the pilot should be able to read, understand and interpret the primary six (6) instruments that are displayed on the PFD and that indicate airspeed, attitude, altitude, vertical speed, turn rate/coordination and heading. Resources • G1000 Pilot's Guide • G1000 Cockpit Poster Exercise 2.1: Instrumentation Layout In the space provided below, sketch the primary six (6) instruments as displayed on the PFD. Slip/Skid Indicator Altitude Reference Window Airspeed Indicator Altitude Reference Bug Attitude Indicator Vertical Speed Indicator Altimeter Turn Coordinator True Airspeed Window Horizontal Situation Indicator Altimeter Setting Window Exercise 2.2: Instrumentation Depiction Assume that the aircraft is flying with the following indications and fill in the appropriate fields on the sketch with this data: • Airspeed = 120 KIAS • True Airspeed = 120 KTAS • Altitude = 6760 ft. • Vertical Speed = 0 fpm • Heading = 95° • Altimeter Setting = 30.15" Hg 190-00368-04 Rev. A Garmin G1000 Pilot's Training Guide - Instructor's Reference 5

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Garmin G1000
Pilot’s Training Guide –
Instructor’s Reference
190-00368-04
Rev. A
5
GROUND LESSONS
Ground Lesson 2
TRANSITION TO THE PRIMARY FLIGHT DISPLAY (PFD)
Objectives
Upon completion of this lesson, the pilot should be able to read, understand and interpret the primary six (6) instruments that
are displayed on the PFD and that indicate airspeed, attitude, altitude, vertical speed, turn rate/coordination and heading.
Resources
G1000 Pilot’s Guide
G1000 Cockpit Poster
Exercise 2.1:
Instrumentation Layout
In the space provided below, sketch the primary six (6) instruments as displayed on the PFD.
Airspeed Indicator
Turn Coordinator
Horizontal
Situation
Indicator
Slip/Skid
Indicator
Vertical Speed
Indicator
Altimeter
Attitude Indicator
Altitude
Reference
Window
Altitude
Reference Bug
Altimeter
Setting
Window
True Airspeed
Window
Exercise 2.2:
Instrumentation Depiction
Assume that the aircraft is flying with the following indications and fill in the appropriate fields on the sketch with this data:
Airspeed = 120 KIAS
True Airspeed = 120 KTAS
Altitude = 6760 ft.
Vertical Speed = 0 fpm
Heading = 95°
Altimeter Setting = 30.15” Hg