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VEMD and Flight Instruments: Vehicle and Engine Multi-function Display

Learn about the Vehicle and Engine Multi-function Display (VEMD) and flight instruments, including engine parameters, test patterns, parameter monitoring, caution messages, and more.

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VEMD and Flight Instruments: Vehicle and Engine Multi-function Display

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  1. EC 130 B4 Initial Pilot Ground School Chapter 11 VEMD and Flight Instruments

  2. Chapter 11 - VEMD and Flight Instruments Vehicle and Engine Multi-function Display - Description …...……….. 11.3 Engine / Vehicle Page ………………………………………………….. 11.4 “Start-Up” Mode ………………………………………………………… 11.5 “Flight” Operational Mode …………………………………………….. 11.6 Test Pattern ………………………………………………………………. 11.7 Engine Power Check ……………………………………………………. 11.9 Parameter Monitoring ………………………………………………….. 11.11 Flight Report …………………………………………………...………… 11.12 Single Screen Failure …………………………………………………… 11.13 Double Screen Failure ………………………………………………….. 11.14 Caution Messages on the VEMD ……………………………………… 11.17 Caution Messages on the VEMD - continued ………………………. 11.22 Flight Instruments - General Description ……………………………… 11.24 Pitot - Static System ……………………………………………………. 11.25 Pitot Heat Switch ………………………………………………………… 11.27 Pitot Caution Light ………………………………………………………. 11.33 Review Questions ………………………………………………………….. 11.34 11.2

  3. Indicating and Control Panels VEMD Description (Vehicle and Engine Multifunction Display) Module No. 2 Module No. 1 Upper Screen Lower Screen Control Buttons 11.3

  4. Engine Page • P2 Bleed Air Indication (with sand filter) • T4 in Degrees C • Torque in Percent • NG and NG in Percent • Fuel in Percent • Fuel Quantity in Pounds, Gallons, • Kilos, or Liters • Outside Air Temperature • Vehicle Page • Engine Oil Temperature and Pressure • Voltage and Current of the Electrical • Power Source (Battery, APU, or Generator) • Fuel Flow in Pounds, Gallons, Kilos, or • Liters / Hour • Messages • Fuel Endurance Remaining 11.4

  5. VEMD In “Start-Up” Mode T4, NG, and Torque: digital value and analog scale The VEMD switches automatically to the First Limitation Indicator at ~ 60% NG. Bleed Valve Flag Fuel Quantity: digital value and analog scale Outside Air Temperature Error Message Area Engine Oil Pressure and Temperature: digital value and analog scale START Digital value of volts on electrical busbar Digital value of starting current - 200 Error Message Area 11.5

  6. VEMD In “Flight” Operational Mode FLI analog scale, plus digital values of NG, T4, & Torque parameters. The upper screen shows all the engine limitation data on the First Limitation Indicator. During start-up, the FLI is automatically displayed at ~ 60% NG. “SCROLL” pushbutton for selecting display - FLI or 3-Scale display. Note: Collective Lever also has a “SCROLL” button. The three primary engine parameters (NG, T4, & TRQ) are displayed in an easy-to-use synthetic form for monitoring engine power: 0 = zero power 9.6 = Max Continuous Power 9.6 to 10 = Take-Off Power 10 = Max Take-Off Rating 10.4 = Max Transient Power (5 s) FADEC = Full Authority Digital Engine Control Digital value of generator current. 11.6

  7. Test Pattern • The test pattern helps to • check both screens. • A target number is • displayed on the screen. • Pressing the “Light Test” • button activates the screen. • This page is displayed on • both screens. • The alpha-numeric code • shown indicates the • software version installed • in your VEMD. 11.7

  8. Pressing “SCROLL” twice displays the “Performance” page; the pilot then uses the “+”, “-” and “ENTER” keys to record the payload carried. The VEMD computes the AUW (All-Up Weight [Gross Weight]), and the maximum takeoff weights in IGE or OGE conditions. Performance Not yet available. 2866 lb lb 0160 0441 1212 lb 470 lb 480 +16 IGE 4960 lb lb 5000 OGE 6173 lb 11.8

  9. In compliance with the Flight Manual, the pilot can check engine power by selecting “Engine Power Check”. The VEMD indicates the conditions that need to be observed to initiate an Engine Power Check. Every condition requires a pilot action. Once every condition has been met, the VEMD proceeds automatically. Engine Power Check 11.9

  10. Engine Power Check The test runs in three phases denoted by rectangles on the VEMD screen. If the flight parameters are not updated, the test repeats the previous phase. On completion of the test, which lasts about 30 seconds, the results are shown on the screen. 11.10

  11. 5 T4 820 0C 7 3 9 x100 -4 -8 -12 TQ 4 FLI FAILED Parameter Monitoring The NG parameter is invalid. The FLI symbology is replaced by the 3-scale display, however the NG value is not shown. Error Message Different values have been detected between processors 1 and 2. The display is inhibited. LANE 1 PARAM FAILED Error Message 11.11

  12. Flight Report • At the end of the flight when N1 < 10% and NR < 70 rpm, the VEMD switches automatically to the “SHUTDOWN” mode. The VEMD then displays the Flight Report: • flight number (automatically incremented) • flight time • generator & turbine cycles (computed by the FADEC) [NG < 60% until NG > 50%] • overlimits or failures detected during the flight. 11.12

  13. VEMD Screen Failure - failure of one screen • Select the failed screen to OFF • Read the information on the other • screen. • All the information is available using the SCROLL push-button either on the VEMD or on the collective pitch lever. • If the top screen has failed, with the lower screen in 3-parameter mode ( NG, T4, Torque), only T4 and NG will be available. • (Refer to the procedure provided in the Flight Manual, paragraph 3.5.4, ‘Loss of Ng, Torque, or T4 parameters’ for compliance with limitations.) Flight Manual - Emergency Procedures - Page 3 - 7 11.13

  14. VEMD Screen Failure - failure of both screens [ First, insure that the Day / Night switch is in the appropriate position. ] • [ Real failure is highly improbable ] • Can be a single failure when battery and DC generator are in “OFF” position (fire and smoke detection procedure). • In this case, to avoid any power overlimit, the maximum authorized power will be the power needed to establish level flight with the following law: • IAS kt = 100 kt at sea level minus (2 kt / 1000 ft Hp) • Landing procedure: carry out a no hover landing. LAND AS SOON AS PRACTICABLE Flight Manual - Emergency Procedures - Page 3 - 7 11.14

  15. Caution Messages on VEMD • When a parameter is off line, the parameter value is not displayed on the VEMD upper screen and the parameter scale symbology is displayed in yellow. Caution messages are self explanatory and the pilot shall comply with the action requested. If no light is lit on the caution and warning panel, no other action is required from the pilot. • LANE 1 (or LANE 2) FAILED • PRESS OFF 1 (or OFF 2) : Self-explanatory Flight Manual - Emergency Procedures - Page 3 - 7 11.15

  16. Caution Messages on VEMD • When a parameter is off line, the parameter value is not displayed on the VEMD upper screen and the parameter scale symbology is displayed in yellow. Caution messages are self explanatory and the pilot shall comply with the action requested. If no light is lit on the caution and warning panel, no other action is required from the pilot. • LANE 1 (or LANE 2) FAILED • PRESS OFF 1 (or OFF 2) : Self-explanatory • VEH PARAM OVER LIMIT : Vehicule Parameter overlimit Flight Manual - Emergency Procedures - Page 3 - 7 11.16

  17. (Continued • Caution Messages on VEMD • When a parameter is off line, the parameter value is not displayed on the VEMD upper screen and the parameter scale symbology is displayed in yellow. Caution messages are self explanatory and the pilot shall comply with the action requested. If no light is lit on the caution and warning panel, no other action is required from the pilot. • LANE 1 (or LANE 2) FAILED • PRESS OFF 1 (or OFF 2) : Self-explanatory • VEH PARAM OVER LIMIT : Vehicule Parameter overlimit • ENG PARAM OVER LIMIT : Engine Parameter overlimit • These messages appear when a parameter usually displayed on this page reaches a limitation, as the relevant (vehicle or engine) pages are not displayed. • - SCROLL ………. DEPRESS to reach the relevant pages and check the • parameter. Flight Manual - Emergency Procedures - Page 3 - 7 11.17

  18. Caution Messages on the VEMD(continued) • CROSS TALK FAILED • PRESS OFF 1 (or OFF 2) : Self-explanatory Flight Manual - Emergency Procedures - Page 3 - 8 11.18

  19. Caution Messages on the VEMD(continued) • CROSS TALK FAILED • PRESS OFF 1 (or OFF 2) : Self-explanatory • BRT CNTRL FAILED : Brightness has failed Flight Manual - Emergency Procedures - Page 3 - 8 11.19

  20. Caution Messages on the VEMD(continued) • CROSS TALK FAILED • PRESS OFF 1 (or OFF 2) : Self-explanatory • BRT CNTRL FAILED : Brightness has failed • FLI FAILED : One power parameter (Ng, T4, TQ) is • CHECK PARAM not consistent. • - Parameters consistancy …………………. : CHECKED • - Relevant procedures in ABNORMAL ENGINE PARAMETER INDICATION • (SECTION 3) ………….. : APPLY Flight Manual - Emergency Procedures - Page 3 - 8 11.20

  21. Caution Messages on the VEMD(continued) • CROSS TALK FAILED • PRESS OFF 1 (or OFF 2) : Self-explanatory • BRT CNTRL FAILED : Brightness has failed • FLI FAILED : One power parameter (Ng, T4, TQ) is • CHECK PARAM not consistent. • - Parameters consistancy …………………. : CHECKED • - Relevant procedures in ABNORMAL ENGINE PARAMETER INDICATION • (SECTION 3) ………….. : APPLY • GEN PARAM OVERLIMIT : Generator parameter overlimit Flight Manual - Emergency Procedures - Page 3 - 8 11.21

  22. Caution Messages on the VEMD(continued) • CROSS TALK FAILED • PRESS OFF 1 (or OFF 2) : Self-explanatory • BRT CNTRL FAILED : Brightness has failed • FLI FAILED : One power parameter (Ng, T4, TQ) is • CHECK PARAM not consistent. • - Parameters consistancy …………………. : CHECKED • - Relevant procedures in ABNORMAL ENGINE PARAMETER INDICATION • (SECTION 3) ………….. : APPLY • GEN PARAM OVERLIMIT : Generator parameter overlimit • BAT PARAM OVER LIMIT : Battery parameter overlimit • These messages appear when the relevant parameter is not displayed on • the vehicle page and when an electrical limitation is reached. Flight Manual - Emergency Procedures - Page 3 - 8 11.22

  23. Configuration Page Maintenance Page VEMD Introduction Flight Mode VEMD Tool Book VEMD Videos 1. Select the Video you desire by clicking on the button below. 2. For the Full Screen View: Hold down ALT key & press ENTER. 3. After the video is full screen and playing, move your mouse pointer to the very bottom of the page and leave it there. 4. Upon completion: Press the ESC key, and with your mouse pointer still at the bottom of the page, click once. VEMD Tool Book Insert Tool Book Disc into CD ROM Drive and Click on the button below. 11.23

  24. Flight Instruments 11.24

  25. Pitot Static System Vertical Speed Indicator Air Speed Indicator Altimeter Temperature Probe Ram Air partialvacuum Pitot Head OAT VEMD Drain Valve Static Port Static Port 11.25

  26. Pitot Tube 11.26

  27. Pitot Heat Switch DIRECT BATT Aircraft is flown with the Pitot Heat ON all the time. 11.27

  28. OAT and Static Sensing OAT Probes Static Ports 11.28

  29. PITOT WARNING PANEL CORRECTIVE ACTIONS Pitot heating not operative Flight Manual - Emergency Procedures - Page 3-20 11.29

  30. PITOT WARNING PANEL CORRECTIVE ACTIONS PITOT …………………….….. CHECK ON Yes Pitot heating not operative Flight Manual - Emergency Procedures - Page 3-20 11.30

  31. PITOT WARNING PANEL CORRECTIVE ACTIONS PITOT …………………….….. CHECK ON Yes Pitot heating not operative Monitor airspeed indicator CONTINUE FLIGHT Flight Manual - Emergency Procedures - Page 3-20 11.31

  32. PITOT WARNING PANEL CORRECTIVE ACTIONS PITOT …………………….….. CHECK ON Yes No Pitot heating not operative Monitor airspeed indicator CONTINUE FLIGHT Flight Manual - Emergency Procedures - Page 3-20 11.32

  33. PITOT WARNING PANEL CORRECTIVE ACTIONS PITOT …………………….….. CHECK ON Yes No Pitot heating not operative Monitor airspeed indicator PITOT …..…….. ON CONTINUE FLIGHT Flight Manual - Emergency Procedures - Page 3-20 11.33

  34. Review Questions 11.34

  35. 94. What will occur on the VEMD when it loses a required FLI parameter? A. The triple indication page will appear with the lost parameter displaying an amber arc.

  36. 95. On the VEMD, the upper screen can display three engine values simultaneously. What three values are displayed? C. T4, Torque, and NG

  37. 96. Does the VEMD display both digital and analog values simultaneously? C. Yes

  38. 97. During start-up, at what percent NG does the VEMD automatically switch from the triple display to the First Limitation Indicator (FLI)? D. ~ 60% NG

  39. 98. Are the FLI values listed below correct? Maximum Continuous Rating = 9.6 Takeoff Rating Range= 9.6 to 10 Maximum Takeoff Rating = 10 Maximum Transient Rating = 10.4 (5 s) A. Yes

  40. 99. Can the fuel quantity, which is displayed in both digital & analog readouts, be shown in either pounds, gallons, kilos, or liters? B. Yes

  41. 100. What does the alpha-numeric code on the TEST PATTERN page tell you? D. The software version installed on that particular VEMD.

  42. 101. With a single screen failure, can the data from both screens be viewed? A. Yes.

  43. 102. With a single screen failure, how does the pilot view the data from both screens? D. By SCROLLING between the two displays.

  44. 103. Where are the SCROLL switches located? C. On the VEMD and on both collective control heads.

  45. 104. After a night flight, and during start-up the next morning, you appear to have a double screen failure. What is the most likely cause of this apparent failure? B. The “Day / Night” switch is still on “Night”.

  46. 105. How is the Pitot Heat activated? D. Push on the pushbutton switch located on the center console.

  47. PITOT 106. What does illumination of the light indicate? D. Pitot heating is not operative.

  48. 107. Where are the static ports located? C. Underneath the helicopter on the belly panel.

  49. EC 130 B4 Initial Pilot Ground School End of Chapter 11 VEMD and Flight Instruments

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