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Malfunction Analysis Examination

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Malfunction Analysis Examination

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  1. Instructions: You will be shown CDU, PDU, Caution Advisory and Master Caution panel indications. Additionally, significant aircraft sounds e.g. engine out or low rotor audio will be depicted by the symbol followed by a written description of the sound. All indications appear as if the pilot made NO corrective action. You will have 20 seconds from the time the last indication appears to identify the malfunction. The exact operator's manual description of the malfunction is not required although your answer must clearly identify the correct malfunction. Malfunction Analysis Examination

  2. STEADY TONE LOW ROTOR RPM 102 0 54 55 1840 745 946 710 955 1 LOUD BANG RIGHT SIDE 102 0 105 0 1840 850 846 625 955

  3. MASTER CAUTION #1 PRI #1 HYD #1 TAIL RTR PRESS TO RESET SERVO PRESS PUMP SERVO 2

  4. #1 ENG #2 ENG OUT OUT STEADY TONE LOW ROTOR RPM 102 0 54 55 1840 750 946 725 955 MASTER CAUTION #2 ENGINE #1 ENGINE PRESS TO RESET OIL PRESS OIL PRESS #1 ENG #2 ENG ANTI-ICE ON ANTI-ICE ON 3 102 0 0 0 1840 200 206 150 305

  5. 102 0 54 55 1840 750 946 725 955 4 102 0 95 40 1840 830 855 640 980

  6. STEADY TONE LOW ROTOR RPM 102 0 54 55 1840 750 946 725 955 #2 ENG ANTI-ICE ON 5 102 0 105 29 1840 850 876 670 985

  7. MASTER CAUTION #2 RSVR #2 HYD BACK-UP BOOST SERVO #2 PRI BACK-UP FLT PATH LOW PRESS TO RESET PUMP OFF SERVO PRESS STAB RSVR LOW PUMP ON 6 TRIM FAIL SAS OFF

  8. #2 ENG OUT STEADY TONE LOW ROTOR RPM 102 102 0 0 105 54 0 55 1840 1840 850 730 206 946 150 710 995 955 MASTER CAUTION #2 ENGINE PRESS TO RESET OIL PRESS #2 ENG ANTI-ICE ON 7

  9. MASTER CAUTION #2 HYD BOOST SERVO FLT PATH #2 PRI PRESS TO RESET PUMP OFF STAB SERVO PRESS 8 SAS OFF TRIM FAIL

  10. 102 0 54 55 1840 750 946 725 955 #2 ENG ANTI-ICE ON 9 102 0 75 25 1840 780 876 670 985

  11. MASTER CAUTION BACK-UP #1 PRI #1 HYD #1 TAIL RTR #2 TAIL RTR #1 RSVR BACK-UP PRESS TO RESET PUMP ON SERVO PRESS PUMP SERVO SERVO ON LOW RSVR LOW

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