______________________________________________________________________________
____________________________________________________________________________
LMM for the Kodiak 100
Page 7-19
190-02102-00 Rev.4
3. Follow the checklist items displayed on the PFD and press the ENTER key as
each one is completed or confirmed. When the CALIBRATE field is flashing press
the ENTER key to begin the procedure.
4. The PFD display advises the operator when to turn the aircraft to a cardinal
heading, when to stop, and when to turn to another heading. During the
procedure, the operator turns to magnetic headings of 360, 090, 180, and 270
degrees, within a tolerance of ±0.25°.
NOTE
A tolerance of ±0.5° can be used if ±0.25° is not achievable.
5. Maneuver the aircraft with the longitudinal axis aligned with the desired heading
line of the compass rose.
6. The operator must confirm each aircraft heading. Press the ENTER key to
confirm. The CONFIRM HEADING field stops flashing.
7. The PFD informs the operator of the calibration results. Press the ENTER key on
the PFD to conclude this procedure.
7.6.5 Calibration Procedure D: Engine Run-Up Vibration Test
Calibration Procedure D is required for all installations to validate the vibration
characteristics of the installation. Calibration Procedures A-1 through C are not required
before this procedure.
1. If the PFD is not displaying the GRS/GMU CALIBRATION configuration page,
follow steps from calibration procedure A-1 listed previously.
2. The FMS small knob can now be used to select which calibration/validation
procedure to run. Select ENGINE RUN-UP TEST and press the ENTER key. If
the ENGINE RUN-UP TEST selection is still flashing, press the ENTER key
again.
3. Follow the checklist items displayed on the PFD and press the ENTER key as
each one is completed or confirmed. When the CALIBRATE field is flashing,
press the ENTER key to begin the procedure.
4. The PFD display instructs the operator to gradually increase power from idle to
full throttle and back to idle over the course of a couple of minutes.
5. When the operator has completed the engine run-up and the engine is back to an
idle setting, press the ENTER key to indicate the process is complete. When this
is done, the TEST COMPLETE field stops flashing.
6. The PFD informs the operator if the installation has passed or failed the vibration
test. If the test fails, the specific measurements causing the failure are identified
Uncontrolled if Printed
Summary of Contents for Cessna Caravan G1000
Page 2: ...BLANK PAGE Uncontrolled if Printed...
Page 288: ...Uncontrolled if Printed...
