SECTION 9
SUPPLEMENT 20 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-114, 4 of 30 REVISED: JANUARY 9, 2006
SECTION 2 - LIMITATIONS
A. PFD Limitations
1. IFR flight is prohibited when the PFD or any standby instrument is
inoperative (altimeter, airspeed indicator, artificial horizon, or whiskey
compass).
2. IFR flight is prohibited upon aircraft total loss of essential engine
parameter display (manifold pressure, tachometer, fuel flow).
3. The Avidyne FlightMax Entegra series Primary Flight Display Pilot’s
Guide, p/n 600-00104-000 revision 00 or appropriate later revision, or
p/n 600-00143-000 revision 01 (EXP 5000 R6) or appropriate later
revision, must be available to the pilot during all flight operations.
4. If a VOR or Localizer (VLOC) navigation source is displayed on the
HSI and GPSS mode is engaged on the autopilot, the autopilot will
track the active flight plan in the GPS corresponding to the selected
VLOC source selected for display on the HSI (i.e. GPS1 for VLOC1 or
GPS2 for VLOC2). This configuration is potentially confusing and
must be avoided.
5. GPSS mode must not be used on the final approach segment of a VLOC
approach (ILS, LOC or non-GPS-overlay VOR). GPSS mode must be
deselected (i.e., NAV mode selected) prior to the turn onto the final
approach course.
NOTE
The PFD integrates with separately approved sensor and
flight control installations. Adherence to limitations in
appropriate installation AFM supplements is mandatory.
B. MFD Limitations
1. The Avidyne moving map display provides visual advisory of the
airplane’s GPS position against a moving map. This information
supplements CDI course deviation and information presented on
the GPS navigator. The moving map display must not be used as
the primary navigation instrument.
2. Use of Map page during IFR flight requires an IFR approved GPS
receiver and installation, operated in accordance with its applicable
limitations.
3. The Avidyne FlightMax EX-series Pilot’s Guide, p/n 600-00105-
000 revision 00 or appropriate later revision, must be available to
the pilot during all flight operations.
SECTION 9
SUPPLEMENT 20 PA-28-181, ARCHER III
REPORT: VB-1611 ISSUED: JULY 12, 1995
9-114, 4 of 30 REVISED: JANUARY 9, 2006
SECTION 2 - LIMITATIONS
A. PFD Limitations
1. IFR flight is prohibited when the PFD or any standby instrument is
inoperative (altimeter, airspeed indicator, artificial horizon, or whiskey
compass).
2. IFR flight is prohibited upon aircraft total loss of essential engine
parameter display (manifold pressure, tachometer, fuel flow).
3. The Avidyne FlightMax Entegra series Primary Flight Display Pilot’s
Guide, p/n 600-00104-000 revision 00 or appropriate later revision, or
p/n 600-00143-000 revision 01 (EXP 5000 R6) or appropriate later
revision, must be available to the pilot during all flight operations.
4. If a VOR or Localizer (VLOC) navigation source is displayed on the
HSI and GPSS mode is engaged on the autopilot, the autopilot will
track the active flight plan in the GPS corresponding to the selected
VLOC source selected for display on the HSI (i.e. GPS1 for VLOC1 or
GPS2 for VLOC2). This configuration is potentially confusing and
must be avoided.
5. GPSS mode must not be used on the final approach segment of a VLOC
approach (ILS, LOC or non-GPS-overlay VOR). GPSS mode must be
deselected (i.e., NAV mode selected) prior to the turn onto the final
approach course.
NOTE
The PFD integrates with separately approved sensor and
flight control installations. Adherence to limitations in
appropriate installation AFM supplements is mandatory.
B. MFD Limitations
1. The Avidyne moving map display provides visual advisory of the
airplane’s GPS position against a moving map. This information
supplements CDI course deviation and information presented on
the GPS navigator. The moving map display must not be used as
the primary navigation instrument.
2. Use of Map page during IFR flight requires an IFR approved GPS
receiver and installation, operated in accordance with its applicable
limitations.
3. The Avidyne FlightMax EX-series Pilot’s Guide, p/n 600-00105-
000 revision 00 or appropriate later revision, must be available to
the pilot during all flight operations.
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