Cockpit Reference Guide

Garmin G1000 Cockpit Reference Guide for the Cessna Nav III

190-00384-12 Rev. A

WARNINGS,

CAUTIONS, & NOTES

CAUTION: The PFD and MFD displays use a lens coated with a special anti-reﬂective coating that is very sensitive

to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE

COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is

speciﬁed as safe for anti-reﬂective coatings.

CAUTION: The Garmin G1000 does not contain any user-serviceable parts. Repairs should only be made by an

authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and the

pilot’s authority to operate this device under FAA/FCC regulations.

NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms

that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge

points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has

been cleared.

NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and

displays, are subject to change and may not reﬂect the most current G1000 system and aviation databases.

Depictions of equipment may differ slightly from the actual equipment.

NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions:

(1) this device may not cause harmful interference, and (2) this device must accept any interference received,

including interference that may cause undesired operation.

NOTE: The GDU 1040 and GDU 1044B PFD/MFD may require a warm-up time of up to 30 minutes when exposed

to -40˚C for an extended period. A warm-up time of up to 15 minutes may be required when exposed to -30˚C

for an extended period.

NOTE: This product, its packaging, and its components contain chemicals known to the State of California to

cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s

Proposition 65. If you have any questions or would like additional information, please refer to our web site at

www.garmin.com/prop65.

NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude

and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the

source of the interference should alleviate the condition.

NOTE: The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to ﬁnd operating

instructions on the major features of the G1000 system more easily. It is not intended to be a comprehensive operat-

ing guide. Complete operating procedures for the system are found in the G1000 Pilot’s Guide for this aircraft.

NOTE: Use of polarized eyewear may cause the ﬂight displays to appear dim or blank.