2-21-18
Yaw Damper
Above FL155 (15,500 ft), when the yaw damper is not operating, the aircraft must be flown
only in balanced flight (slip-skid ind/- 1 trapezoid).
2-21-19
Primus Apex - Electrionic Checklist
The Electronic Checklist functionality allows implementation of a user defined Electronic
Checklist database. With respect to airworthiness approval the AFM remains the primary
reference for checklists.
Implementation of an Electronic Checklist Database is the responsibility of the aircraft owner/
operator, use and operational approval is dependent on the rules of operation.
Implementation of Electronic Checklist functionality does not constitute operational approval.
2-21-20
Primus Apex - Electrionic Charts
The APEX Electronic Charts provide supplemental situational awareness only and do not allow
“blind taxi” procedures or flight navigation by use of these charts. At any time the pilot shall
remain responsible for taxiing by external visual references and for flying by airborne
navigation by the use of primary navigation instruments.
The position accuracy of the aircraft symbol on the charts can decrease in the case of
insufficient GPS signal reception or GPS sensor failure. The aircraft symbol is not in-scale with
the APEX Electronic Charts.
The APEX Electronic Charts do not replace approved published paper or approved electronic
systems for aeronautical charts, which must remain available as a backup reference for chart
data.
Note
It is the responsibility of the operator to apply for specific operational approval at the local
authority for the use of external electronic charts (e.g. Electronic Flight Bags Class 1 and
Class 2) instead of paper charts. Class 3 EFBs require a Supplemental Type Certificate
(STC) or certification design approval as part of the aircraft equipment.
2-21-21
Primus Apex - Video Input
It is the responsibility of the operator to make sure that no interference with the installed
avionics systems results from the connection of a camera device to the Video Input Module.
2-21-22
Primus Apex - XM Sat Weather
The XM Weather System does not work in PDC mode (STBY bus). Even though the layers
can be selected, no data will be transmitted until the aircraft is powered by the batteries (or
external power or the engine) and re-selection of the required XM layers is performed.
Section 2 - Limitations (EASA Approved)
Yaw Damper
Pilot's Operating Handbook
Report No: 02406
Issue date: Dec 18, 2020
Page 2-21-8
12-C-A15-10-0221-00A-043A-A
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GENERAL
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