DA 62 AFM
Emergency
Procedures
3.5.4 AIR DATA COMPUTER (ADC) FAILURE
NOTE
Complete loss of the Air Data Computer is indicated by a red
X and yellow text over the airspeed, altimeter, vertical speed,
TAS and OAT displays. Some FMS functions, such as true
airspeed and wind calculations, will also be lost.
1. Use standby airspeed indicator and altimeter, part of the Standby Attitude
Module.
END OF CHECKLIST
3.5.5 ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS
NOTE
Loss of an engine parameter is indicated by a red or yellow X
through the data field. Erroneous information may be
identified by indications which do not agree with other system
information. Erroneous indications may be determined by
comparing a display with other displays and other system
information.
1. Set power based on power lever position, engine noise and speed.
2. Monitor other indications to determine the health of the engine.
3. Use known power settings and Section 5.3.2 of the AFM for approximate fuel
flow values.
4. Use other system information, such as annunciator messages, GPS fuel
quantity and flow to safely complete the flight.
END OF CHECKLIST
Doc. No. 11.01.05-E
Rev. 0
11-Jan-2019
Page 3 - 21
Summary of Contents for DA 62
Page 2: ...DA 62 AFM Introduction Intentionally left blank Page 0 0a Rev 0 11 Jan 2019 Doc 11 01 05 E ...
Page 36: ...DA 62 AFM General 1 7 THREE VIEW DRAWING Doc No 11 01 05 E Rev 0 11 Jan 2019 Page 1 19 ...
Page 363: ...Performance DA 62 AFM Intentionally left blank Page 5 92 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 438: ...Airplane Description DA 62 AFM Page 7 46 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 496: ...Handling Care Maintenance DA 62 AFM Page 8 10 Rev 0 11 Jan 2019 Doc No 11 01 05 E 1 4 5 2 3 ...