N206BW Bell Jet Ranger Checklist Rev 6

LANDING LIGHT GLASS CONDITION ANTENNAS CHECK SECURE BEFORE BOARDING MAIN ROTOR BLADES UNTIED AND TURNED AIRWORTHINESS ON BOARD REGISTRATION ON BOARD OPERATING LIMITATIONS ON BOARD WEIGHT AND BALANCE ON BOARD FIRE EXTINGUISHER CHARGED / CURRENT COPILOT CONTROLS AS DESIRED COPILOT / PASSENGER SEAT BELTS SECURE ALL REQUIRED INSPECTIONS COMPLETE N206BW Bell Jet Ranger Checklist Rev 6 11.17.11 EMERGENCY CHECKLIST - WARNING / NOTE ENGINE FIRE DURING STARTING OR SHUTDOWN: PRESS OR CONTINUE TO HOLD THE STARTER BUTTON THROTTLE CLOSED FUEL VALVE OFF ING ENG CIRCUIT BREAKER OUT COMPLETE SHUTDOWN ENGINE FIRE DURING FLIGHT THROTTLE CLOSED IMMEDIATE AUTOROTATION FUEL VALVE OFF BATTERY OFF VENTILATE CABIN ENGINE FAILURE IN FLIGHT (POWER OFF LANDING) LOWER COLLECTIVE ROTOR RPM AT THE HIGH END OF THE OPERATING RANGE WILL PROVIDE MAXIMUM ROTOR ENERGY TO ACCOMPLISH THE LANDING; BUT WILL CAUSE AN INCREASED RATE OF DESCENT REDUCE FORWARD AIRSPEED TO DESIRED AUTOROTATIVE AIRSPEED FOR EXISTING CONDITIONS. MINIMUM DESCENT 52 KNOTS MAXIMUM GLIDE DISTANCE 69 KNOTS IAS SPEED BETWEEN 52 – 69 KNOTS (MAX 115) WITH CYCLIC COLLECTIVE, MAINTAIN 90-107% ROTOR RPM AT LOW ALTITUDE, CLOSE THROTTLE AND FLARE COLLECTIVE PITCH MAY BE NECESSARY LEVEL HELICOPTER AND USE COLLECTIVE TO CUSHION EXCESSIVE GROUND RUN WITH THE COLLECTIVE UP, OR ANY TENDENCY TO FLOAT FOR LONG DISTANCE PRIOR TO GROUND CONTACT SHALL BE AVOIDED ENGINE AIR START WHEN THE CAUSE OF THE ENGINE FAILURE IS BELIEVED TO BE MECHANICAL, DO NOT ATTEMPT A RESTART. LOWER COLLECTIVE SPEED BETWEEN 52 – 69 KNOTS (MAX 115) COLLECTIVE, MAINTAIN 90-107% ROTOR RPM DO NOT ATTEMPT AIR START ABOVE 12,000 FEET (TOT RISES TOO FAST TO CONTROL) FUEL CONTROL AND/OR GOVERNOR FAILURE ENGINE FUEL CONTROL AND/OR GOVERNOR FAILURE IS EVIDENCED BY A CHANGE OF POWER OR RPM. THERE IS NO MANUAL FUEL CONTROL ON THE ENGINE. CONTROL POWER WITH THROTTLE IF ENGINE OVER SPEEDS. MAINTAIN RPM WITH COLLECTIVE PITCH IF ENGINE UNDER SPEEDS. ESTABLISH AUTOROTATIVE GLIDE IF POWER IS VERY LOW OR IF ENGINE MUST BE SHUT DOWN. PREPARE FOR POWER-OFF LANDING. HYDRAULIC SYSTEM FAILURE REDUCE AIRSPEED TO 61-69 KNOTS HYD BOOST CIRCUIT BREAKER OUT, IF NOT RESTORED, IN HYDRAULIC SWITCH ON, IF NOT RESTORED, OFF LAND AS SOON AS PRACTICAL AND INVESTIGATE A RUN-ON LANDING AT 10-15 KNOTS IS RECOMMENDED EMERGENCY CHECKLIST - WARNING / NOTE DRIVESHAFT FAILURE FAILURE OF MAIN DRIVESHAFT TO TRANSMISSION WILL RESULT IN COMPLETE LOSS OF POWER TO MAIN ROTOR. ALTHOUGH COCKPIT INDICATIONS FOR A DRIVESHAFT FAILURE ARE SIMILAR TO AN ENGINE OVERSPEED, IT IS IMPERATIVE THAT AUTOROTATIVE FLIGHT PROCEDURES BE ESTABLISHED IMMEDIATELY. FAILURE TO REACT IMMEDIATELY TO ROTOR LOW RPM LIGHT, AND AUDIO AND DUAL TACHOMETER CAN RESULT IN LOSS OF CONTROL. COLLECTIVE, MAINTAIN 90-107% ROTOR RPM SPEED BETWEEN 52 – 69 KNOTS (MAX 115) WITH CYCLIC THROTTLE OPEN (ENGINE IS POWERING TAIL ROTOR) COMPLETE AUTOROTATION LANDING AND SHUTDOWN TAIL ROTOR CONTROL FAILURE COMPLETE LOSS OF THRUST THROTTLE IDLE ENTER AUTOROTATION FIXED PITCH FAILURE DEPENDING ON THE PITCH POWER - ADJUST AS REQUIRED TO MINIMIZE EXCESSIVE YAWING AIRSPEED – ADJUST TO DETERMINE BEST VELOCITY TO MINIMIZE EXCESSIVE YAWING ELECTRICAL POWER FAILURE GENERATOR FAIL LIGHT ON GENERATOR SWITCH RESET THEN ON IF POWER NOT RESTORED GENERATOR SWITCH OFF ALL NON-ESSENTIAL ELECTRICAL EQUIPMENT OFF REDUCE ALTITUDE TO BELOW 6000 FEET PRESSURE ALTITUDE IF FLIGHT PERMITS BECAUSE OF POSSIBLE LOSS OF FUEL BOOST PUMPS. LAND AS SOON AS PRACTICAL ENGINE ICING ANTI-ICE SWITCH ON TOT – MAINTAIN WITHIN LIMITS ENGINE OIL PRESSURE LOW, HIGH, OR FLUCTUATING LAND AS SOON AS POSSIBLE HIGH ENGINE OIL TEMPERATURE LAND AS SOON AS PRACTICAL CAUTION LIGHTS LOW ROTOR RPM REDUCE COLLECTIVE TRANS OIL PRESS LAND AS SOON AS POSSIBLE TRANS OIL TEMP LAND AS SOON AS POSSIBLE BATTERY TEMP TURN BATTERY OFF ENGINE CHIP LAND AS SOON AS POSSIBLE TRANS CHIP LAND AS SOON AS POSSIBLE T/R CHIP LAND AS SOON AS POSSIBLE GEN FAIL RESET, LAND AS SOON AS PRACTICAL BAGGAGE DOOR LAND AS SOON AS PRACTICAL A/F FUEL FILTER LAND AS SOON AS PRACTICAL FUEL PUMP < 6000 LAND AS SOON AS PRACTICAL FUEL LOW 19 GALLONS REMAIN, PLAN LANDING