CESSNA
SECTION 2
MODEL 172S NAV III
OPERATING LIMITATIONS
KAP 140 AUTOPILOT
U.S.
FAA APPROVED
G1000 LIMITATIONS
(Continued)
The COM 1/2 (split COM) function of the Audio Panel is not approved
for use. During COM 1/2 operation, transmission by one crew member
inhibits reception by the other crew member.
The fuel quantity, fuel used and fuel remaining functions of the G1000
are supplemental information only and must be verified by the pilot.
GPS - WAAS (Airplanes 172S9810 thru 172S10431
incorporating MK206-34-08 and not incorporating SB09-
34-06 and Airplanes 172S10432 thru 172S10467 and
172S10469 thru 172S10506 and 172S10508 thru
172S10639 and 172S10641 thru 172S10655 not
incorporating SB09-34-06)
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
than 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 Audio
Panel is inoperative (since the aural warning will not be provided when
Autopilot is disengaged).
(Continued Next Page)
172SPHAUS-05
2-21
For
Training
Purposes
Only
Summary of Contents for Cessna 172S NAV III Skyhawk SP
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