______________________________________________________________________________
____________________________________________________________________________
LMM for the Kodiak 100
Page 7-39
190-02102-00 Rev.4
6. Release the CWS switch and press the AP/YD DISC TRIM INTRPT switch on the
pilots control wheel. Verify the autopilot disengages with a flashing amber 'AP'
and YD annunciation on PFD1 and PFD2, accompanied by an aural alert. Verify
the control wheel is free in pitch and roll and the rudder pedals also move freely.
7. Engage the autopilot again by pressing the AP key on the AFCS mode controller.
Open AUTO PILOT circuit breaker. Verify the autopilot disconnects and the
abnormal disconnect is provided, consisting of a continuous aural alert and a
flashing red/white AP annunciation. Verify no AFCS annunciations (e.g. AFCS,
PFT, Mistrim) remain on PFD1 or PFD2. Close the AUTO PILOT circuit breaker
to restore power to the system and then press the AP/YD DISC TRIM INTRPT
switch to cancel the abnormal alert. Wait for completion of the pre-flight test
sequence.
8. Engage the autopilot again by pressing the AP key on the AFCS mode controller.
Ensure the autopilot is coupled to GIA1 by verifying the arrowhead next to the
XFR key on the AFCS mode controller is pointing to the pilot's side. If the
arrowhead points to the copilot's side, press the XFR key. Open NO 1 GPS NAV
circuit breaker. Verify the autopilot disconnects with a continuous aural alert and
a flashing red/white AP annunciation. Press the AP/YD DISC TRIM INTRPT
switch to cancel the alert and annunciation. Close the NO 1 GPS NAV circuit
breakers and wait for completion of the pre-flight test sequence. Repeat this test
with the NO 2 GPS NAV circuit breaker.
9. Press the XFR key on the AFCS mode controller and engage the autopilot by
pressing the AP key on the AFCS Mode Controller. Press the AP/YD DISC TRIM
INTRPT switch on the pilot side to disconnect the autopilot; verify the flashing
amber AP and YD alerts are displayed on PFD1 & 2.
10. Press the GO AROUND button on the left throttle. Verify 'TO' is annunciated on
PFD1 and PFD2 for both PITCH and ROLL modes and the FD command bars
show 9 ±1° degrees nose up and wings-level.
11. Press the Flight Director (FD) key on the AFCS mode controller to deactivate the
GA mode. Press the AP key to engage the autopilot. Press the CWS button for a
minimum of 5 seconds and release; verifying there is no residual force on the
control wheel.
12. Disengage the autopilot by pressing the AP/YD DISC TRIM INTRPT switch.
Engage VS mode by pressing the VS key on the AFCS mode controller. Verify
PFD1 and PFD2 display 'VS' in green and indicates a vertical speed reference of
'0 FPM'.
13. Press the ALT key on the AFCS mode controller and verify the ALT annunciation
is displayed in green on PFD1 and PFD2 with an altitude reference equal to the
aircraft altitude (within the nearest 20 feet).
Uncontrolled if Printed
Summary of Contents for Cessna Caravan G1000
Page 2: ...BLANK PAGE Uncontrolled if Printed...
Page 288: ...Uncontrolled if Printed...
