曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
approach information.
Section 4 - Normal Procedures
• Note •
Back-up approach charts for CMax are not required. However,
back-up approach data for departure, destination, and
alternate field is recommended. Reference CMax Description
in this supplement.
Section 7 - System Description
The CMax installation is entirely software dependant. No additional
hardware is required.
• Note •
Back-up approach charts for CMax are not required. However,
back-up approach data for departure, destination, and
alternate field is recommended. Back-up approach data could
be printed copies of published approach charts, a laptop
containing the JeppView software and data, or notes providing
the approach vertical data (the Garmin 430 can display lateral
approach information).
Revision 1: 12-15-07
4 of 4 P/N 13772-125
Section 9 Cirrus Design
Supplements SR22
Refer to Avidyne FlightMax EX5000C Pilot’s Guide, for a more
complete description of CMax Approach Charts, its operating modes,
and additional detailed operating procedures.
Revision 1: 12-15-07
P/N 13772-132 1 of 10
Cirrus Design Section 9
SR22 Supplements
Pilots Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
For
Garmin 400W-Series GPS Navigator
When a Garmin 400W-Series GPS Navigator is installed in the Cirrus
Design SR22, this Supplement is applicable and must be inserted in
the Supplements Section (Section 9) of the Cirrus Design SR22 Pilot's
Operating Handbook. This document must be carried in the airplane at
all times. Information in this supplement either adds to, supersedes, or
deletes information in the basic SR22 Pilot's Operating Handbook.
• Note •
This POH Supplement Change, dated Revision 01: 11-11-07,
supersedes and replaces the original release of this POH
Supplement dated 08-15-07.
Revision 01: 11-11-07
2 of 10 P/N 13772-132
Section 9 Cirrus Design
Supplements SR22
Section 1 - General
The WAAS-enabled, Garmin 400W-Series GPS Navigator is capable
of providing primary navigation information for enroute, terminal, nonprecision,
and precision approaches with typical position accuracies of
1 meter horizontally and 2 meters vertically.
The Wide Area Augmentation System (WAAS) consists of ground
reference stations positioned across the United States that monitor
GPS satellite data. Two master stations, located on either coast,
collect data from the reference stations and create a GPS correction
message. This correction accounts for GPS satellite orbit and clock
drift plus signal delays caused by the atmosphere and ionosphere.
The corrected data is then broadcast through geostationary satellites.
WAAS also provides the capability of quickly determining when signals
from a given satellite are wrong and removing that satellite from the
navigation solution using Receiver Autonomous Integrity Monitoring
(RAIM), a technology developed to assess the integrity of GPS
signals.
• Note •
WAAS satellite coverage is only available in North America.
User in other parts of the world can receive WAAS data,
however, the signal has not been corrected and thus does not
improve the accuracy of your receiver.
Models Covered
Two Garmin 400W-Series GPS Navigators are covered in this
publication; the GNC 420W and GNS 430W. Generally, both models
will be referred to as the Navigator, except where there are physical or
operational differences.
• Note •
For detailed descriptions and full operation instructions for the
GNC 420W or GNS 430W Navigators, refer to the Garmin
400W-Series GPS Navigator Pilot's Guide and Reference, P/N
190-00356-00, Revision A or later revision.
Revision 01: 11-11-07
P/N 13772-132 3 of 10
Cirrus Design Section 9
SR22 Supplements
SR22_FM09_1109
SR22_FM09_1285
Figure - 1
GNC 420W and GNS 430W 400W-Series Navigators
Revision 01: 11-11-07
4 of 10 P/N 13772-132
Section 9 Cirrus Design
Supplements SR22
Section 2 – Limitations
1. The Garmin 400W-Series GPS Navigator Pilot's Guide and
Reference, P/N 190-00356-00, Revision A or later must be
immediately available to the pilot during flight. The software status
stated in the pilot's guide must match that displayed on the
equipment.
2. IFR enroute and terminal navigation is prohibited unless the pilot
verifies the currency of the database or verifies each selected
waypoint for accuracy by reference to current approved data.
3. The Garmin 400W-Series GPS Navigator meets RNP5 (BRNAV)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Cirrus Design SR20西锐20飞行员操作手册和飞机飞行手册附录(74)
