Quantcast AFTER LANDING - TM-1-1510-223-MTF0093

 

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GO-AROUND
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TM-1-1510-223-MTF Maintenance Test Flight Manual Army Model RC-12
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ENGINE SHUTDOWN - TM-1-1510-223-MTF0094
TM 1-1510-223-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
AFTER LANDING
Complete the following procedures after the aircraft has
cleared the runway:
1. CONDITION levers - HIGH IDLE.
2. PROP levers - Retard to FEATHER detent.
3. ICE VANE CONTROL switches - ON.
4. Engine AUTO IGNITION switches -Off.
5. ICE & RAIN switches - Off.
6. Flaps - UP.
7. Radar/transponder - As required.
* 8. Lightning sensor system (LSS) - Test as follows:
a.
Lightning sensor system mode selector
switch (weather radar/LSS control panel) -
CLR/TST.
Display  should  show  a
simulated lightning strike at a bearing of
045 degrees at 25 nautical miles.
NOTE
The lightning sensor system antenna is used in
this test, and as a result, any real lightning activity
that occurs while the test is in operation may also
be displayed.
9. Lights - As required.
10. Mission control panel - Set as follows:
a. ELINT power switch (mission status panel,
in rack behind pilot) -OFF.
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