CESSNA
SECTION 2
MODEL 172S NAV III
OPERATING LIMITATIONS
G1000 LIMITATIONS
(Continued)
GPS-WAAS (Airplanes 172S10432 and On)
Use of the Garmin G1000 system for GPS or WAAS navigation
under Instrument Flight Rules (IFR) requires that:
1. The airplane must be equipped with an approved and
operational alternate means of navigation appropriate to the
route being flown (NAV receiver, DME or ADF).
2. For flight planning purposes, if an alternate airport is
required, it must have an approved instrument approach
procedure, other then GPS or RNAV, that is anticipated to
be operational and available at the estimated time of arrival.
All equipment required for this procedure must be installed
and operational.
3. For procedures requiring a prediction of GPS Receiver
Autonomous Integrity Monitoring (RAIM) capability for TSO-
C129a (non-WAAS) equipment (e.g. oceanic operations,
U.S. RNAV routes, European BRNAV and PRNAV, etc.),
the Garmin WAAS Fault Detection/Exclusion Prediction
program (006-A0154-01 or later approved version) should
be used to confirm the availability of RAIM for the intended
route and time of flight. Generic prediction tools do not
provide an accurate indication of RAIM availability for the
Garmin G1000 system.
4. When flight planning an LNAV/VNAV or LPV approach, the
Garmin WAAS Fault Detection/Exclusion Prediction
program (006-A0154-01 or later approved version) should
be used in addition to any NOTAMs issued from the
approach.
BENDIX/KING KAP 140 2 AXIS AUTOPILOT (if installed)
Use of the Bendix/King KAP 140 Autopilot is prohibited when the
GMA 1347 Audio Panel is inoperative (since the aural warning will
not be provided when Autopilot is disengaged).
FAA APPROVED
I
172SPHAUS-04
U.S. 2-19