SECTION 2 CESSNA
OPERATING LIMITATIONS MODEL T182T NAV III
GFC 700 AFCS
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 (Serials T18208665 and T18208669 thru
T18208806 not incorporating SB08-34-01)
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.
(Continued Next Page)
T182TPHBUS-01
2-18
To Next Page
Loading...
Need help?
General
