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Entegra PFD:
• ALT (Altitude Hold) Mode
• VS (Vertical Speed) Mode
• Altitude Capture Mode
• HDG (Heading Capture/Hold Mode)
Revision A7
P/N 13772-001 7-91
Cirrus Design Section 7
SR22 Airplane Description
• NAV Mode
• GPSS (GPS Steering) Mode
The following three modes of the System 55SR are supported by the
Entegra PFD:
• ALT (Altitude Hold) Mode
• HDG (Heading Capture/Hold Mode)
• NAV Mode
28 VDC for autopilot and altitude selector/alerter is supplied through
the 5-amp AUTOPILOT circuit breaker on the Essential Bus.
Refer to S-Tec System Fifty-Five X Autopilot Pilot's Operating
Handbook, P/N 87109 dated 8 November 2000 or later, and the
applicable POH supplement for a more complete description of the
autopilot, its operating modes, and additional detailed operating
procedures.
GPS Navigation
The Jeppesen Navigation Database provides access to data on
Airports, Approaches, Standard Instrument Departures (SIDs),
Standard Terminal Arrivals (STARs), VORs, NDBs, Intersections,
Minimum Safe Altitudes, Controlled Airspace Advisories and
Frequencies. North American and International databases are
available. Database information is provided on a card that can be
inserted into the card slot on the GPS unit. Subscription information is
provided in a subscription packet provided with each system.
Serials with Avionics Configuration A - 0002 through 1601, 1603
through 1643 and 1645 through 1662 without PFD:
The airplane is equipped with two GPS navigators. The Garmin GNS
430 is designated GPS 1 and the Garmin GNS 420 is designated GPS
2. Both Garmin GPS navigators are IFR certified. The primary unit,
designated GPS 1, is coupled to the airplane’s HSI, Autopilot, and
multifunction display. The secondary unit, designated GPS 2, is
coupled to the airplane’s HSI.
The GPS navigators are capable of providing IFR enroute, terminal,
and approach navigation with position accuracies better than 15
meters. Each GPS navigator utilizes the Global Positioning System
(GPS) satellite network to derive the airplane’s position (latitude,
Revision A7
7-92 P/N 13772-001
Section 7 Cirrus Design
Airplane Description SR22
longitude, and altitude) and the altitude encoder to enhance the
altitude calculation.
The GPS1 antenna is located above the headliner along the airplane
centerline. The GPS2 antenna is located below the glareshield and
behind the MFD. All GPS navigator controls and functions are
accessible through the GPS receiver units’ front control panels located
in the center console. The panels include function keys, power
switches, MSG and NAV status annunciators, a color LCD display
(GNS 430), two concentric selector knobs on each panel, and a
Jeppesen NavData card slot in each panel. The displays are daylight
readable and automatically dimmed for low-light operation. The
primary GPS navigator is powered by 28 VDC through the 5-amp GPS
1 and 7.5-amp COM 1 circuit breakers on the Avionics Essential Bus.
The secondary GPS navigator is powered by 28 VDC through the 5-
amp GPS 2 and the 7.5-amp COM 2 circuit breaker on the Avionics
Non-Essential Bus.
Avionics Configuration B and PFD:
The airplane is equipped with two GPS navigators. Dual Garmin GNS
430s are designated GPS 1 and GPS 2. Both Garmin GPS navigators
are IFR certified. The primary unit, designated GPS 1, is coupled to
the airplane’s HSI or PFD, Autopilot, and MFD. The secondary unit,
designated GPS 2, is coupled to the airplane’s HSI or PFD, and MFD.
The GPS navigators are capable of providing IFR enroute, terminal,
and approach navigation with position accuracies better than 15
meters. Each GPS navigator utilizes the Global Positioning System
(GPS) satellite network to derive the airplane’s position (latitude,
longitude, and altitude) and the altitude encoder to enhance the
altitude calculation.
The GPS1 antenna is located above the headliner along the airplane
centerline. The GPS2 antenna is located below the glareshield and
behind the MFD. All GPS navigator controls and functions are
accessible through the GPS receiver units’ front control panels located
in the center console. The panels include function keys, power
switches, MSG and NAV status annunciators, a color LCD display
(GNS 430), two concentric selector knobs on each panel, and a
Jeppesen NavData card slot in each panel. The displays are daylight
readable and automatically dimmed for low-light operation. The
primary GPS navigator is powered by 28 VDC through the 5-amp GPS
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CIRRUS DESIGN SR22西锐22飞行员操作手册和飞机飞行手册(87)
