Sennheiser SI 234 - ANNEXE 802 Operations Instructions Page 54

  • Download
  • Add to my manuals
  • Print
  • Page
    / 440
  • Table of contents
  • BOOKMARKS
  • Rated. / 5. Based on customer reviews
Page view 53
Operating Limitations DA 42 NG AFM
Page 2 - 14 Rev. 3 01-Apr-2014
EASA
approved
Doc. No. 7.01.16-E
Color and Significance of the Caution Alerts on the G1000
Caution alerts
(amber)
Meaning / Cause
L/R ECU A FAIL
A fault has occurred in the left/right engine ECU A (one reset
of minor faults is possible)
or
ECU A is being tested during FADEC-test procedure during
the 'Before Take-Off Check'.
L/R ECU B FAIL
A fault has occurred in the left/right engine ECU B (one reset
of minor faults is possible)
or
ECU B is being tested during FADEC-test procedure during
the 'Before Take-Off Check'.
L/R FUEL LOW Left / Right main tank fuel quantity is low.
L/R ALTN FAIL Left / Right engine alternator has failed.
L/R VOLTS LOW Left / Right engine bus voltage is too low (< 25 Volts).
L/R COOL LVL Left / Right engine coolant level is low.
PITOT FAIL Pitot heat has failed.
PITOT HT OFF Pitot heat is OFF.
STAL HT FAIL Stall warning heat has failed.
STAL HT OFF Stall warning heat is OFF.
STICK LIMIT Control stick limiting system (variable elevator stop) has
failed.
LOI GPS integrity is insufficient for the current phase of flight.
AHRS ALIGN:
Keep Wings Level
The AHRS (Attitude and Heading Reference System) is
aligning.
L/R AUX FUEL E Left / Right auxiliary fuel tank empty (if installed).
Page view 53
1 2 ... 49 50 51 52 53 54 55 56 57 58 59 ... 439 440

Comments to this Manuals

No comments