Garmin Software Version 0719.12 Guide de l'utilisateur Page 10

  • Télécharger
  • Ajouter à mon manuel
  • Imprimer
  • Page
    / 174
  • Table des matières
  • MARQUE LIVRES
  • Noté. / 5. Basé sur avis des utilisateurs
Vue de la page 9
Garmin G1000 Cockpit Reference Guide for the Socata TBM 850/900
190-00708-05 Rev. A
Warnings, Cautions & Notes
CAUTION: The system 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: All visual depictions contained within this document, including screen
images of the panel and displays, are subject to change and may not reflect
the most current system and 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 harm-
ful interference, and (2) this device must accept any interference received,
including interference that may cause undesired operation.
NOTE: The data contained in the terrain and obstacle databases comes from
government agencies. Garmin accurately processes and cross-validates the
data, but cannot guarantee the accuracy and completeness of the data.
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: Operating the system in the vicinity of metal buildings, metal
structures, or electromagnetic fields can cause sensor differences that may
result in nuisance miscompare annunciations during start up, shut down, or
while taxiing. If one or both of the sensed values are unavailable, it will be
annunciated as a ‘NO COMP’ (no compare).
NOTE: Use of polarized eyewear may cause the flight displays to appear dim
or blank.
Vue de la page 9
1 2 ... 5 6 7 8 9 10 11 12 13 14 15 ... 173 174

Commentaires sur ces manuels

Pas de commentaire