Kazan Helicopters Mi-17-1V Flight Manual page 146

M",-17-1B. Flight manual
Table of contents
6.
EMERGENCY PROCEDURES
3
6.1. Failure of one engine 3
6.2. Failure of two engines. Autorotation landing 8
6.3. Fire 10
6.4. Troubles in gearboxes 12
6.5. In-flight troubles in engine automatic control system 12
6.6. Abnormal vibration of engine 15
6.7 Low engine oil pressure. Illumination of the L ENG (R ENG) LOW OIL
PRESSURE annunciator 15
6.7A. Illumination of the CHIPS IN L ENG or CHIPS IN R ENG (for helicopters
the engine oil system of which is equipped with CC-78 chip detector) 15
6.8. Unstable operation of engine 16
6.9. Failure of turbine gas temperature (TGT) control 16
6.10. Failure offuel system (fuel booster and transfer pumps) 16
6.10.1. Failure of Fuel Booster Pump 16
6.10.2. Failure of Fuel Transfer Pumps 17
6.11. 270-L1TER FUEL RSV (OCTAnOCb 270
ru
annunciator illumination 17
6.11A. Illumination of the L ENG FUEL FILTER CLOG or R ENG FUEL FILTER
CLOG annunciator 18
6.12. Failure of directional control system 18
6.13. Failure of hydraulic system 19
6.14. Ground resonance 20
6.15. Inadvertent overspeeding above maximum limit speed 20
6.16. Inadvertent slowing down below minimum limit speed 20
6.17. Low frequency oscillation in flight 21
6.18. Failure of AC generators and rectifiers 21
6.18.1. Failure of One AC Generator 21
6.18.2. Failure of Two AC Generators 22
6.18.3. Failure of One Rectifier 23
6.18.4. Failure of Two Rectifiers 23
6.18.5. Failure of ,QMP-200,Q equipment... 24
6.19. Failure of autopilot.. 24
6.20. Failure of gyro horizon 25
6.21. Failure of compass system 25
6.22. Failure of pressure altimeter 26
6.23. Failure of left YC-450Kairspeed indicator 26
6.24. of VHF radio set with two control panels 26
6.25. Failure of APK-15 ADF 27
6.26. Abandonment of helicopter 27
6.27. Emergency evacuation on the. ground 30
6.28. Loss of radio communication 30
6.29. Failure of tail rotor pitch limit system 30
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