曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

groundspeed from GPS1. Flight time starts when the groundspeed
reaches 35 knots on takeoff and pauses when the groundspeed
descends below 35 knots on landing.
ALT MONITOR - Controlled by START / STOP key. Activates a voice
alarm when altitude limit is exceeded
COUNT UP TIMER - The count up timer is controlled by the START /
STOP key. Pressing the CLR key zeros the display.
COUNT DOWN TIMER - The count down timer is controlled by the
START / STOP key. The CRSR and “0 - 9” keys are used to set the
initial time. Pressing the CLR key resets the timer to the initial value.
CONTRAST - Allows adjustment of display contrast in Configuration
Mode. When CONTRAST is selected, pressing the “8” key reduces
contrast and pressing “9” increases contrast.
DISPLAY - The display function is not available in this installation.
Display brightness is automatically controlled through a photocell in
the front panel.
Original: 07-03-04
P/N 11934-S31 1 of 4
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Avidyne EMax™ Engine
Instrumentation
When the Avidyne EMax™ Engine Instrumentation system is installed
in the Cirrus Design SR20, this POH Supplement is applicable and
must be inserted in the Supplements Section (Section 9) of the Cirrus
Design SR20 Pilot’s Operating Handbook. This document must be
carried in the airplane at all times. Information in this supplement adds
to, supersedes, or deletes information in the basic SR20 Pilot’s
Operating Handbook.
• Note •
This POH Supplement Revision dated Revision 1: 12-15-07
supersedes and replaces the original release of this supplement dated
Original: 10-12-05.
Revision 1: 12-15-07
2 of 4 P/N 11934-S31
Section 9 Cirrus Design
Supplements SR20
Figure - 1
Section 1 - General
EMax™ Engine Instrumentation provides the pilot with engine
parameters depicted on simulated gauges and electrical system
parameters located in a dedicated region within in the EX5000C MFD
display.
Avidyne EMax™ Engine Instrumentation
Revision 1: 12-15-07
P/N 11934-S31 3 of 4
Cirrus Design Section 9
SR20 Supplements
Section 2 - Limitations
No Change.
Section 3 - Emergency Procedures
No Change.
Section 4 - Normal Procedures
No Change.
Section 5 - Performance
No Change.
Section 6 - Weight & Balance
Installation of the Avidyne Engine Instruments adds the following
optional (Sym = O) equipment at the weight and arm shown in the
following table.
Section 7 - System Description
An Engine Sensor Unit interfaces (SIU) with engine-mounted sensors,
some of which are shared with the standard airplane gauges, and
provide data to the MFD for display.
Airplanes equipped with EMax™ Engine Instrumentation display all
engine settings and parameters on a dedicated MFD engine monitor
page. The MFD also displays engine and fuel data in data blocks on
the full-screen moving map display. In the event of an exceedence,
each out-of-limit parameter is highlighted on the screen for immediate
attention. The engine monitor also includes data capture capability,
ATA /
Item
Description Sym Qty Part Number
Unit
Wt
Arm
34-03 Engine Sensors O 11 - 1.0 75.0
34-04 Engine Sensor Unit O 1 14843-001 1.1 118.0
34-05 Engine Sensor Harness O 1 15030-001 0.9 92.0
34-06 Engine Sensor Cabin Harness O 1 15032-001 2.1 108.0
Revision 1: 12-15-07
4 of 4 P/N 11934-S31
Section 9 Cirrus Design
Supplements SR20
providing full-time recording of critical engine performance
parameters.
The Engine Instruments system is powered by 28 VDC supplied
through the 5-amp Engine Instruments breaker on the Main Bus 1.
Refer to Avidyne FlightMax EX5000C Pilot’s Guide for a more
complete description of EMax Engine Instruments, its operating
modes, and additional detailed operating procedures.
Revision 1: 12-15-07
P/N 11934-S33 1 of 4
Cirrus Design Section 9
SR20 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
XM Satellite Weather System
When the XM Satellite Weather System system is installed in the
Cirrus Design SR20, this POH Supplement is applicable and must be
inserted in the Supplements Section (Section 9) of the Cirrus Design
SR20 Pilot’s Operating Handbook. This document must be carried in
the airplane at all times. Information in this supplement adds to,
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Cirrus Design SR20西銳20飛行員操作手冊(cè)和飛機(jī)飛行手冊(cè)附錄(37)