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钻石20系列飞机维护手册 DA 20 SERIES AIRPLANE MAINTENANCE MANUAL(89)

时间:2011-10-28 13:51来源:蓝天飞行翻译 作者:admin
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6. WEIGHT AND BALANCE
The change in weight and balance is negligible with the installation of the Brazilian placards and markings.
7. DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS
The Brazilian placards and markings installed do not affect the description of the airplane and its systems.
8. HANDLING, PREVENTATIVE AND CORRECTIVE MAINTENANCE
The Brazilian placards and markings installed do not affect the handling, preventative and corrective maintenance.

DA20-C1 Flight Manual
CHAPTER 9
SUPPLEMENT 13
GARMIN G500 INTEGRATED DISPLAY SYSTEM

1.
GENERAL .....................................................................................................S13-2


2.
OPERATING LIMITATIONS..........................................................................S13-3


3.
EMERGENCY PROCEDURES .....................................................................S13-9


4.
NORMAL OPERATING PROCEDURES.....................................................S13-13


5.
PERFORMANCE.........................................................................................S13-17


6.
MASS AND BALANCE ................................................................................S13-17


7.
DESCRIPTION OF THE AIRPLANE AND ITS SYSTEMS ..........................S13-18


8.
AIRPLANE HANDLING, CARE AND MAINTENANCE................................S13-23

 


DA20-C1 Flight Manual
1. GENERAL
This supplement supplies the information necessary for the efficient operation of the DA20-C1 airplane when the Garmin G500, Integrated Display System, is installed as an optional system. The information contained within this supplement is to be used in conjunction with the complete manual.
This Supplement to the AFM is provided to acquaint the pilot with the limitations as well as normal, abnormal and emergency operating procedures of the Garmin G500.  The limitations presented are pertinent to the operation of the G500 System as installed in the DA20-C1 airplane. Garmin provides a detailed Pilot’s Guide Document Number 190-01102-02, Rev B. This reference material is not required to be on board the aircraft but does contain a more in depth description of all the G500 functions.
This supplement is a permanent part of this Manual and must remain in this Manual as long as the Garmin G500 is installed.

DA20-C1 Flight Manual
2. OPERATING LIMITATIONS
2.1 Cockpit Reference Guide
The Garmin G500 Cockpit Reference Guide, Document Number 190-01102-03, Rev B dated June 2009 or later appropriate revision must be immediately available to the flight crew.
2.2 System Software Requirements
The G500 must utilize the following or later TCCA/FAA approved software versions for safe operation:
Component  Identification  Software Version 
 
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