Uh 1h Huey Ii Systems Knowledge Jeopardy Template

Cool Engine Stuff	N2 Knowledge	Emergency Procedures	More Emergency Procedures	I want some more EPs!
100 approximately 2/3 How much total power that the engine produces does the N1 Turbine extract	100 Reduction Gearbox on front of the engine, the transmission and the overspeed governor and tachometer drive gearbox on the left side of the engine The N2 turns the following three systems	100 1. COLLECTIVE ADJUST as required to maintain rotor 2. PEDALS ADJUST as required 3. THROTTLE ADJUST as required 4. AIRSPEED ADJUST as required AUTOROTATE	100 transmit May Day call, set the transponder to emergency, jettison external stores and lock the shoulder harness During an emergency autorotational landing, if time permits the crew should	100 1. Collective - Reduce 2. DE-ICE and BLEED AIR switches - off 3. Land as soon as possible Engine Compressor Stall
200 approximately 1/3 How much of the total power from the engine does the N2 Turbine extract	200 21090 RPM to 6600 RPM The reduction gearbox reduces the N2 RPM from what to what	200 1. THROTTLE - OFF 2. FUEL switches - OFF 3. BATT switch - OFF EMERGENCY SHUTDOWN	200 Autorotate Engine malfunction in a hover	200 Accomplish an approach and landing to the ground with torque not to exceed the maximum available. If possible, a running landing is recommended Inlet Guide Vane Actuator Failure - Closed
300 Anti-Ice system, Start Fuel System, Oil Cooler Fan, Heater, Bleed Band Which systems use Bleed Air	300 N2 tachometer generator, the power turbine governor and the torquemeter boost pump The overspeed governor and tachometer drive gearbox drives these N2 accessories	300 1. GOV - switch - EMER 2. Throttle - adjust as necessary to control RPM 3. Land as soon as POSSIBLE EMER GOV OPNS	300 1. AUTOROTATE 2. EMER GOV OPNS Engine malfunction at low altitude/low airspeed or in cruise flight	300 due to increasingly lower N1 settings accelration times will correspondingly increase Inlet Guide Vane Actuator Failure - Open: What happens to the power application of the helicopter
400 The Bleed Band What regulates the air passing through the N1 section to ensure proper operation during various engine RPM settings and helps with avoiding a compressor stall	400 Senses the actual N2 RPM, senses the reference RPM selected by the GOV RPM INC/DECR switch and sends the signal to the fuel control thru a rod to maintain reference RPM What does the Power Turbine Governor do	400 Land as soon as POSSIBLE ENGINE OIL TEMPERATURE HIGH	400 1. Throttle - off 2. Starter Gen Switch - START 3. FUEL switches - ON 4. GOV switch - EMER 5. Attempt Start 6. Land as soon as possible Engine Restart During Flight	400 1. Collective - Increase to load the rotor in an attempt to maintain rpm bellow the max operating limit 2. Throttle - reduce until normal operating rpm is attained. Continue with manual throttle control 3. EMER GOV OPNS if reduction of throttle does not reduce rpm as required Engine Overspeed
500 N1 Tachometer Generator, Fuel Control, Engine Driven Fuel Pump, Oil Pump Assembly, Starter Generator What accessories are driven by the Accessory Gearbox	500 Throttle Quadrant position, N2 demand from the Power Turbine Governor Rod, N1 RPM from the geartrain, Outside Air Temperature from the OAT sensor and Pressure Altitude from the Pressure Altitude Bellows The Automatic Fuel Control Unit schedules fuel flow to the combustor based on data from these 5 systems	500 GOV switch may be moved to the EMER position and throttle adjusted in an attempt to correct the surging condition. If flight is not possible close the throttle completely and complete an autorotational landing. Partial Power Condition with engine surges	500 EMER GOV OPNS Droop Compensator Failure	500 1. Land as soon as POSSIBLE 2. EMER SHUTDOWN - After Landing Transmission oil hot or low pressure

UH-1H Huey II Systems Knowledge

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