Phase One Items

Question 1

Evacuation

Answer 1

Fuel Condition Lever ……………………CUTOFF Propeller Control Lever ………………FEATHER Radio Call ……………………………. AS REQUIRED Cabin Lights ………………………………..AS REQUIRED Battery Switch …………………………………… OFF Evacuation …………………………………………… ORDER

Question 2

Engine securing procedure

Answer 2

IF at night OR in IMC: Standby Vacuum System ………………………….ON Power Lever …………………………… FLIGHT IDLE Propeller Control Lever ………………FEATHER Fuel Condition Lever ………………………… CUTOFF

Question 3

REJECTED TAKE-OFF / ENGINE FAILURE – DURING THE TAKE-OFF ROLL

Answer 3

Power Lever …………………………..BETA Range Brakes ………………………………………………….APPLY Wing Flaps …………………………………………RETRACT IF the aircraft cannot be stopped on the remaining runway: Fuel Condition Lever ………………………….. CUTOFF Fuel Shutoff …………………………………. OFF Pull out. Fuel Tank Selectors …………………………………….OFF Warning horn will sound. Battery Switch ……………………………………………OFF Park Brake ………………………………….AS REQUIRED Phase One Drills ……………………………..COMPLETE R/T ………………………………………. AS REQUIRED Evacuate …………………………………… AS REQUIRED Phase Two Drills …………………………. AS REQUIRED

Question 4

REJECTED TAKE-OFF / ENGINE FAILURE – AIRBORNE BELOW TURNBACK ALTITUDE

Answer 4

IF at night OR in IMC: Standby Vacuum System ……………………………..ON Airspeed …..85 KIAS (20° Flap) 95 KIAS if Flap 10°. IF time permits (AND aircraft control assured): Power Lever ……………………………. FLIGHT IDLE Fuel Selectors ………………….CONFIRM BOTH ON Fuel Boost Switch ……………………………………….ON Ignition Switch …………………………………………….ON Propeller …………………………………………FEATHER Wing Flaps ………………………………….FULL DOWN Flap setting may be varied to ensure glide performance to selected landing area. Fuel Condition Lever ………………………….CUT OFF Fuel Shutoff ………………………………………….OFF Pull out. Fuel Tank Selectors ………………………………….OFF Warning horn will sound. Battery Switch ………………………….AS REQUIRED Park Brake ………………………………….AS REQUIRED Phase One Drills ……………………………..COMPLETE R/T ………………………………………. AS REQUIRED Evacuate …………………………………… AS REQUIRED Phase Two Drills …………………………. AS REQUIRED

Question 5

ENGINE POWER LOSS DURING FLIGHT

Answer 5

IF at night OR in IMC: Standby Vacuum System …………………………….ON Airspeed ………………………………………….. 95 KIAS Adjusted for weight once stabilised. Fuel Selectors …………………..CONFIRM BOTH ON Fuel Boost Switch …………………………………. ON Ignition Switch………………………………………. ON IF Ng > 50% (suspected flameout OR FCU pneumatic governor failure) Power Lever ……………………….. CHECK RESPONSE Decrease to Flight Idle and advance IF no response AND Ng remains > 50% (confirmed FCU governor failure) Power Lever …………………………… FLIGHT IDLE Emergency Power Lever …………….. AS REQUIRED Minimum 65% Ng in flight. IF Ng

Question 6

AIR START WITH STARTER ASSIST

Answer 6

Electrical Load ……………………………REDUCE Standby Power Switch …………………………………OFF Avionics Power Switches ……………………………..OFF Ignition Switch …………………………………….NORM Airconditioner ……………………………………………..OFF Bleed Air Switch ………………………………………OFF Emergency Power Lever ………………………NORMAL Power Lever ………………………………..FLIGHT IDLE Propeller Control Lever ……………………… MIN RPM Fuel Condition Lever …………………………..CUT OFF Fuel Shutoff ……………………………………………….ON Push In. Fuel Tank Selectors ………………………… BOTH ON Battery Switch …………………………………………….. ON Fuel Boost Switch ………………………………………. ON Check annunciators - AUX FUEL PUMP ON illuminated, FUEL PRESS LOW extinguished. Altitude ……………………………….. 20,000’ MAXIMUM Starter Switch ……………………………………….START IGNITION ON annunciator …………….ILLUMINATED Engine Oil Pressure ………………………………CHECK Ng ……………………………………………………..12% MIN Fuel Condition Lever ………………………….. LOW IDLE Monitor ITT (1090° MAX) Starter Switch …………………………………………… OFF Ng ≥52% Ignition Switch …………………………… AS REQUIRED Fuel Boost Switch ………………………………………………………………………… NORM Leave ON if pump is observed to cycle on & off. Fuel Condition Lever ………………………….HIGH IDLE Propeller Control Lever ………………..AS REQUIRED Power Lever …………………………………AS REQUIRED Electrical Equipment / Avionics ……..AS REQUIRED

Question 7

AIR START WITH NO STARTER ASSIST

Answer 7

Generator Switch ……….. TRIP and RELEASE Standby Power Switch ………………………………..OFF Avionics Power Switches …………………………..OFF Airconditioner …………………………………………….OFF Bleed Air Switch …………………………………………OFF Emergency Power Lever ………………………NORMAL Power Lever …………………………………FLIGHT IDLE Propeller Control Lever ………………………MIN RPM Fuel Condition Lever ……………………………CUT OFF Fuel Shutoff ………………………………..ON Push In. Fuel Tank Selectors ……………………………BOTH ON Battery Switch …………………………………………….ON Fuel Boost Switch ……………………………………ON Check annunciators - AUX FUEL PUMP ON illuminated, FUEL PRESS LOW extinguished. Ignition Switch ……………………………………………..ON Check IGNITION ON annunciator illuminated. Airspeed ………………………………………………………………….. 100 KIAS MINIMUM 140 KIAS minimum if propeller feathered. Altitude ……………………………… 20,000’ MAXIMUM 15,000’ if propeller feathered. Ng Indicator……………………………… CHECK STABLE Fuel Condition Lever …………………………LOW IDLE Monitor ITT (1090° MAX) Ignition Switch ………………………………………..NORM Ng ≥52% WARNING: If conditions exist such as HEAVY PRECIPITATION or NEARLY EMPTY FUEL TANKS, leave ignition switch ON. Fuel Boost Switch ……………………………………NORM Leave ON if pump is observed to cycle on & off. Fuel Condition Lever ………………………..HIGH IDLE Propeller Control Lever …………………AS REQUIRED Power Lever ………………………………..AS REQUIRED Generator Switch ……………….RESET and RELEASE Electrical Equipment / Avionics ……..AS REQUIRED CAUTION: If a rise in Ng and ITT are not indicated within 10 seconds, place Fuel Condition Lever to CUT OFF and ABORT START. Refer to Engine Power Loss During Flight and Emergency Landing Without Power checklists. CAUTION: Emergency airstarts may be attempted below 10% Ng and outside the normal airspeed envelope, BUT ITT MUST BE CLOSELY MONITORED. The Fuel Condition Lever may be moved alternatively to CUT OFF and then back to LOW IDLE if overtemperature tendencies are encountered. CAUTION: Do not attempt a restart without starter assist if Ng tachometer indicates zero RPM. This procedure is likely to require a significant amount of height to attempt. The pilot should ensure that at all times the aircraft remains within gliding distance of a suitable landing area if the airstart attempt is not successful. Consideration should be given to the merits of attempting an airstart without starter assist when operating below 10,000’ AGL.

Question 8

FORCED LANDING WITHOUT POWER

Answer 8

ELT …………………………………………ACTIVATE Seats, Seatbelts, Harnesses …………..SECURE Airspeed ……………………………………..AS REQUIRED Optimum glide Power Lever ……………………………………………..IDLE Propeller Control Lever …………………….. FEATHER Fuel Condition Lever …………………………..CUTOFF Fuel Boost Switch ………………………………………..OFF Ignition Switch ……………………………………… NORM Standby Power Switch …………………………………OFF Non-Essential Equipment ……………………………OFF Fuel Shutoff ………………………………………………OFF Pull out. Fuel Tank Selectors …………………………………… OFF Warning horn will sound. Wing Flaps ………………………… AS REQUIRED Recommend FULL DOWN prior to touchdown. Crew Doors …………………………………. UNLATCH Prior to touchdown Battery Switch ……………………………………………. OFF Once landing assured with flap selected. Touchdown ………………………..SLIGHTLY TAIL LOW Brakes ………………………………………..AS REQUIRED WARNING: Passengers should be instructed to adopt a brace position prior to landing.

Question 9

PRECAUTIONARY LANDING WITH ENGINE POWER

Answer 9

ELT ………………………………………..ACTIVATE Seats, Seatbelts, Harnesses ……………. SECURE Wing Flaps ………………………………. 10° Airspeed ………………………….. 90 KIAS Selected Field ……………………………………. INSPECT Note obstructions and terrain. Electrical Switches ……………………………………. OFF Except BATTERY and GENERATOR Wing Flaps ………………………………… FULL DOWN On final approach. Airspeed …………………………………………… 80 KIAS Crew Doors ……………………………………… UNLATCH Prior to touchdown. Generator Switch …………………. TRIP and RELEASE Battery Switch …………………………………………….OFF Touchdown………………………..SLIGHTLY TAIL LOW Consider attempting to keep the nosewheel off the ground until speed has reduced. Fuel Condition Lever ……………………….. CUT OFF Brakes ………………………………………… AS REQUIRED

Question 10

DITCHING

Answer 10

Radio, Transponder, ELT……….AS REQUIRED Cabin ……………………………………. SECURE Stow loose objects in Zone 6 or jettison. Use passenger to assist. Seats, Seatbelts …….. SECURE Wing Flaps …………………………………….FULL DOWN Power ………………………………………… AS REQUIRED Establish 300 FPM descent at 80 KIAS Attitude ………………………………………..MAINTAIN NO FLARE for touchdown. Airplane ………………………………………….EVACUATE

Question 11

ENGINE FIRE DURING GROUND OPERATIONS

Answer 11

Fuel Condition Lever …………………………….CUTOFF Fuel Boost Switch ………………………………………… OFF Starter Switch ………………………………………..MOTOR IF fire persists: Fuel Shutoff ……………………………………………OFF Starter Switch …………………………………..MOTOR CAUTION: Do not exceed starting cycle limitations. Should the fire persist, as indicated by sustained ITT, immediately close the fuel shutoff and continue motoring. IF the fire cannot be controlled OR once the fire is extinguished: Starter Switch ………………………………………….. OFF Fuel Shutoff ……………………………………………..OFF Pull out. Battery Switch ………………………………………….. OFF Airplane ………………………………………… EVACUATE Fire ……………………………………………. EXTINGUISH

Question 12

ENGINE FIRE IN FLIGHT

Answer 12

Engine Fire ……………………………………CONFIRM Check for smoke, flames and/or abnormal engine indications (ie ITT) IF engine fire IS NOT confirmed: LAND AS SOON AS PRACTICAL IF engine fire IS confirmed: Power Lever ……………………………………………….IDLE Propeller Control Lever ………………………. FEATHER Fuel Condition Lever …………………………..CUT OFF Fuel Shutoff ………………………………………… OFF Cabin Heat Firewall Shutoff Control ……. PULL OFF IF at night or in IMC: Standby Vacuum System …………………………… ON Forward Side Vents …………………………….. CLOSE Overhead Vents …………………………………… OPEN Ventilation Fans …………………………………………. ON Wing Flaps …………………………………………..20°-30° Airspeed ………………………………………..80-85 KIAS Seats, Seatbelts, Harnesses ………………..SECURE Fuel Boost Switch ………………………………………. OFF Ignition Switch ……………………………………..NORM Standby Power Switch ……………………………… OFF Non-Essential Equipment ……………………….. OFF Fuel Tank Selectors ……………………………………. OFF Warning horn will sound. Wing Flaps ………………………… AS REQUIRED Recommend FULL DOWN prior to touchdown. Crew Doors …………………………………….. UNLATCH Prior to touchdown Battery Switch ………………………………………….. OFF Once landing assured with flap selected. Touchdown …………………….. SLIGHTLY TAIL LOW Brakes ………………………………………. AS REQUIRED

Question 13

ELECTRICAL FIRE

Answer 13

Battery Switch ………………………. OFF Generator Switch …………………… TRIP & RELEASE Standby Power Switch …………………………………………. OFF Vents ……………………………………………..CLOSED Bleed Air Heat Switch ………………………………. OFF Fire Extinguisher ……………………………….ACTIVATE WARNING: Occupants should use oxygen masks, if installed, until smoke clears. After discharging an extinguisher within a closed cabin, ventilate the cabin. Avionics Power Switches ………………………….. OFF All Other Electrical Switches ……………………… OFF WARNING: Without electrical power, all electrically operated gyros & engine instruments, fuel boost pump, annunciator lights, wing flaps and all avionics will be inoperative. Vacuum driven gyros will still be operative. KFC-150 autopilot vacuum gyros: Pilot AI / Co-Pilot DI KFC-250 autopilot vacuum gyros: Co-Pilot AI and DI IF fire appears to be extinguished AND electrical power is necessary for further flight: Battery Switch ……………………………….. ON Standby Power Switch ………………………………… ON Generator Switch ………………….. RESET & RELEASE Circuit Breakers……………………………………… CHECK Identify faulty circuit, DO NOT reset. Radio Switches …………………………………………..OFF Avionics Power Switches ………………………………ON Radio & Electrical Switches …………………………. ON Only for required systems, one at a time with delay after each to identify fault. Smoke Clearance Procedure …………….COMPLETE Only once the fire is confirmed to be completely extinguished. Bleed Air Heat ……………………….. AS REQUIRED

Question 14

CABIN FIRE ON THE GROUND

Answer 14

Power Lever …………………………..IDLE Brakes ……………………………………… AS REQUIRED Propeller Control Lever ……………………….FEATHER Fuel Condition Lever …………………………CUTOFF Battery Switch ……………………………………………OFF Airplane ………………………………………….. EVACUATE Fire …………………………………………….. EXTINGUISH

Question 15

CABIN FIRE IN THE AIR

Answer 15

Battery Switch …………………………. OFF Generator Switch ……………………..TRIP & RELEASE Standby Power Switch ………………………………. OFF Vents ……………………………………………..CLOSED Bleed Air Heat Switch ………………………………… OFF Fire Extinguisher …………………………….ACTIVATE Smoke Clearance Procedure …………….COMPLETE LAND AS SOON AS POSSIBLE

Question 16

WING FIRE

Answer 16

Pitot / Static Heat Switch ………………….OFF Stall Heat Switch ……………………………………….OFF Strobe Lights Switch ………………………………….OFF Navigation Lights Switch …………………………OFF Landing & Taxi Light Switches ……………………OFF Radar ……………………………………………………….. OFF Ventilation Fans …………………………………………OFF

Question 17

EXITING ICING CONDITIONS

Answer 17

Ignition Switch ……………………. ON Inertial Separator ……………………………….BYPASS Pitot / Static Heat Switch ………………………………ON Stall Warning Heat Switch …………………………… ON Propeller Anti-Ice Switch ………………………….. AUTO If installed. Icing Conditions ………………………………………. EXIT Descend or change course to facilitate. Ignition Switch ………………………………………….. OFF After 5 minutes of Inertial Separator in BYPASS Bleed Air Heat Switch / Temperature Control ………………………… ON & ADJUST Cabin Heat / Defrost Controls ………AS REQUIRED Cabin Heat FULL IN and Defrost FULL OUT for maximum windshield defrosting. Propeller ……………………………………1900 RPM Minimises ice build-up. If the propeller ammeter indicates unusually high or low amperage during the 90 second cycle of operation, a malfunction has occurred (refer section 3.3.8.3). CAUTION: If excessive vibration is noted, momentarily reduce propeller RPM to 1600 RPM, then rapidly move the propeller control lever full forward. Cycling the RPM flexes the propeller blades and the higher RPM increases centrifugal effect – causing ice to shed more readily. IF icing conditions are unavoidable: Landing …………………. AS SOON AS PRACTICAL Consider off airport landing if icing build up is extremely rapid. NOTE: If BYPASS is used at any point during flight or aircraft operation due to suspected or actual icing conditions, do not return it to NORMAL until the separator has been visually inspected and verified that the separator and its door are free of ice and water.

Question 18

Yoke snatch

Answer 18

It is important to minimise flap extension if icing is suspected on the horizontal stabiliser. A tail stall will be characterised by “yoke snatch” and the correct response is to retract flap, reduce power and apply back pressure to the control column. Increasing power will exacerbate the problem. Maintain extra airspeed consistent with field length available.

Question 19

PROPELLER ANTI-ICE SYSTEM MALFUNCTION

Answer 19

IF uneven anti-icing of the propeller blades is indicated by excessive vibration: Propeller Control Lever …….EXERCISE, then MAX Prop Anti-Ice / Prop Anti-Ice Control Circuit Breakers ……………………………. IN Prop Anti-Ice Ammeter ……………………CHECK Ammeter should indicate 20-24 Amps for 90 seconds, then 0 Amps for 90 seconds. IF ammeter continuously indicates 0 Amps: Prop Anti-Ice Switch ……………………CHECK AUTO IF 0 Amps indications persist: Prop Anti-Ice Switch ………………………….. MANUAL Hold for 90 seconds. Repeat procedure at 90 sec intervals. WARNING: When operating Propeller Anti-Ice in MANUAL (requiring the switch to be held in the lower position), it is important to cycle the switch at intervals of 90 secs ON / 90 secs OFF. If the switch is held in MANUAL without being cycled OFF every 90 secs, runback ice may build up on the propeller blades causing a loss in propeller efficiency, reducing aircraft performance. This characteristic may be more pronounced with Hartzell propellers. IF 0 Amps indications STILL persist: Icing Conditions ……………………………………….. EXIT Descend or change course to facilitate IF ammeter reading is below the green arc (possible non-uniform de-icing): Prop Anti-Ice Switch …………………………………… OFF Propeller Control Lever ………………………….. CYCLE At frequent intervals to aid in ice shedding. Icing Conditions …………………. EXIT Descend or change course to facilitate NOTE: A slight propeller vibration at the start of the de-ice cycle lasting for 20-30 seconds is due to propeller ice shedding characteristics and is normal. This may be more pronounced with the Hartzell propeller. NOTE: To check the heating elements and anti-ice timer for one complete cycle, the system must be left on for approximately three minutes. NOTE: Propeller anti-ice is inoperative in the AUTO mode whenever the OIL PRESS LOW annunciator is illuminated. CAUTION: If, after leaving icing conditions, engine roughness or vibration develops / persists that is not traceable to icing or another cause, reduce propeller RPM to smoothest condition plan a landing at the nearest suitable airfield and check the security of the anti-ice boots and leads as a possible cause.

Question 20

SURFACE DE-ICE BOOT MALFUNCTIONS

Answer 20

IF ice remains on leading edges AND DE-ICE PRESS annunciator does not illuminate during all three sequences of inflation cycle: Annunciator ………………………………………CHECK Push to Test. De-Ice Boot Circuit Breaker ……………………. IN Suction Gauge ……………………………… CHECK IF vacuum is below normal AND / OR there is an audible leak in the forward cabin or left wing root area: Broken Engine Bleed Air Line …………….. SUSPECT Icing Conditions ……………………………………EXIT Descend or change course to facilitate. USE NON-VACUUM INSTRUMENTS. IF instrument vacuum is normal: Boot Press Switch ……………. MANUAL & HOLD Hold for approx. 9 seconds. LEADING EDGES ………………………………… CHECK Visually observe for simultaneous inflation of all boots. DE-ICE PRESS Annunciator ………………….. CHECK Should illuminate within 6 seconds of MANUAL selection. IF DE-ICE PRESS annunciator does not illuminate OR any boots do not inflate: Icing Conditions ……………………………………….. EXIT Descend or change course to facilitate. Airspeed ……………………………. 105 KIAS MINIMUM If there is unshed ice accumulation along any leading edge surface during the approach to land, refer to the considerations for approach and landing under the severe icing environment. WARNING: With inoperative de-ice boots, increase engine power to MCP and leaving icing conditions ASAP. In severe icing conditions, it may not be possible to maintain altitude or proper glide path on approach. In this case, it is imperative that a safe airspeed be maintained. The aural stall warning horn may not function and there may be little or no pre-stall buffet with heavy ice loads on the wing leading edges.

Question 21

OIL PRESS LOW

Answer 21

Oil Pressure Gauge ……………………….CHECK IF Oil Pressure Gauge confirms annunciator: Engine Shutdown ……………………… CONSIDER Consistent with safety, continue engine operation and prepare for emergency landing.

Question 22

FCU MALFUNCTION (engine falls to idle)

Answer 22

Evidenced by engine power decreasing to minimum flow idle – ITT 500-600°C, NG approx. 48% (higher with altitude) and no engine response to power lever movement. Power Lever …………………………………….IDLE Emergency Power Lever ……………… AS REQUIRED Maintain 65% NG minimum during flight. CAUTION: The EPL overrides normal fuel control functions and results in the direct operation of the fuel metering valve. Utilise slow and smooth movement of the EPL to avoid engine surges and/or exceeding ITT, NG and Torque limits. NOTE: When using the EPL, monitor gas generator RPM when reducing power near idle in order to prevent it from decreasing below 65% in flight. Operation below 65% Ng will result in longer than usual engine spool up times, a higher than normal stall speed and increased risk of engine flame out. NOTE: The EPL may have a “dead band” – such that no engine response is observed during the initial forward travel from the IDLE position. NOTE: Rapid movement of the EPL can cause engine flame out

Question 23

BETA ANNUNCIATOR

Answer 23

The BETA annunciator is connected to an oil pressure switch which indicates when the propeller is in beta mode (ie capable of reversing). If the BETA annunciator does not extinguish with power application during take-off, the departure should be aborted and the source of the malfunction rectified before further flight. If the beta annunciator illuminates in flight, the most appropriate action should be to advance the power lever, however the power may need to be adjusted otherwise in order to control (ie minimise) propeller drag.

Question 24

CHIP DETECTOR ANNUNCIATOR

Answer 24

The optional Engine Chip Detection System as fitted to Company aircraft consists of two magnetic chip detectors and a split indicator. The LH half of the indicator is for the accessory gearbox and the RH half is for the detector in the propeller reduction gearbox. In the event of the amber CHIP DETECTOR annunciator illuminating in flight, the procedure is: Engine Gauges ……………………………………. CHECK IF indications are normal: Flight ………………………………………… CONTINUE IF indications confirm annunciation: Engine Shutdown ……………………………. CONSIDER Consistent with safety, continue engine operation and prepare for emergency landing. In the majority of cases, continued flight to a chosen destination will be possible. However, if there are any indications of impending engine seizure, the Engine Shutdown / Securing Procedure should be completed. During continued engine operation with a confirmed indication, the considerations for operating the engine as described in section 3.3.9.1 (Loss of Oil Pressure) may be applied. In no case shall a subsequent departure be considered without determining and rectifying the cause of the annunciation.

Question 25

ENGINE ATM ANNUNCIATOR

Answer 25

If an exceedance has occurred then land as soon as practicable

Question 26

FUEL PRESS LOW

Answer 26

Fuel Boost Switch …………………………….. ON IF FUEL PRESS LOW annunciator extinguishes: Fuel Qty & Cabin Odour ……………………MONITOR Monitor for evidence of a fuel leak. Land ………………………..AS SOON AS PRACTICAL Determine cause of motive flow failure prior to next flight. IF FUEL PRESS LOW and AUX FUEL PUMP ON annunciators illuminated: Engine Gauges …………………………….. MONITOR Monitor for sign of fuel starvation. Land ………………….. AS SOON AS POSSIBLE

Question 27

RESERVOIR FUEL LOW

Answer 27

This annunciation will be caused by the fuel quantity in the reservoir tank reducing to approx. ½ capacity. WARNING: There is only enough fuel in the reservoir for approximately 1-1½ minutes of engine operation at MCP after illumination of the RESERVOIR FUEL LOW annunciator. Fuel Tank Selectors …….. LEFT ON / RIGHT ON Fuel Boost Switch …………………………………… ON Ignition Switch ……………………………………….. ON IF RESERVOIR FUEL LOW annunciator remains illuminated & there is useable fuel in the wing tanks: Engine Gauges / FUEL PRESS LOW Annunciator …………………………… MONITOR Monitor carefully for signs of fuel starvation. Land …………………………. AS SOON AS POSSIBLE Determine cause of RESERVOIR FUEL LOW annunciation. WARNING: If there are signs of fuel starvation, prepare for a forced landing. If the fuel selectors had been turned off, selecting them on will quickly refill the reservoir tank. Once the cause of the original annunciation has been determined and rectified, the ignition and fuel boost switches may be returned to their NORM positions.

Question 28

STARTER CONTACTOR DOES NOT DISENGAGE AFTER ENGINE START

Answer 28

Battery Switch ………………………………… OFF Auxiliary Power Unit ………..OFF, then DISENGAGE Fuel Condition Lever …………………………….CUTOFF Engine Shutdown ……………………………..COMPLETE A possible cause is a disconnected speed sensor – located on the left side of the engine, the connection is a cannon type plug.

Question 29

STANDBY ALTERNATOR OVERHEAT ANNUNCIATOR ILLUMINATION

Answer 29

Standby Power Switch ……………………………………………………………………. OFF STBY ELECT PWR INOP Annunciator ………………………………………… CHECK ON IF primary generator electrical system is not available: Electrical Load …………………………………………………………………….. REDUCE Avionics Bus 2 Switch ……………………………………………………………. OFF Avionics Bus Tie Switch …………………………………………………………. OFF Avionics Standby Power Switch ………………………………………………. OFF Flashing Beacon ……………………………………………………………………. OFF Strobe Lights ……………………………………………………………………….. OFF All De-icing Equipment ………………………………………………………….. OFF IF pitot heat is required: RIGHT PITOT HEAT circuit breaker ………………………………. PULL OFF Pitot Switch ………………………………………………………………………. ON Vent Fans …………………………………………………………………………….. OFF Air Conditioner (if Installed) …………………………………………………… OFF

Question 30

GENERATOR OVERHEAT ANNUNCIATOR ILLUMINATION

Answer 30

Generator Switch ……………………………………………………….. TRIP and release GENERATOR OFF Annunciator ………………………………….. CHECK ILLUMINATED Electrical Load ………………………………………………………….. REDUCE as follows: Avionics Bus 2 Switch ………………………………………………………………… OFF Flashing Beacon ……………………………………………………………………….. OFF Strobe Lights ……………………………………………………………………………. OFF All De-icing Equipment ………………………………………………………………. OFF IF pitot heat is required: RIGHT PITOT HEAT circuit breaker ………………………………….. PULL OFF Pitot Switch ………………………………………………………………………….. ON Vent Fans ………………………………………………………………………………… OFF Air Conditioner (if Installed) ………………………………………………………. OFF GEN CONT and GEN FIELD Circuit Breakers …………………………………. PULL Top row, last two breakers on forward end. With KFC-150 or KFC-225 Automatic Control System Installed: A/P CONT Circuit Breaker …………………………………………………………. PULL Third row from bottom, first breaker from forward end. To reactivate the avionics fan and the disabled section of the audio amplifier, if desired: AVIONICS BUS 2 Circuit Breakers …………………………………………. PULL ALL Except AVIONICS FAN and AUDIO AMP breakers (Last two breakers on forward end) Avionics Bus 2 Switch ………………………………………………………………….. ON STBY PWR Circuit Breakers (2) …………………. CHECK IN or RESET as required First and second rows, first breaker on aft end, each row. Standby Power Switch …………………………………………………………………….. ON Avionics Standby Power Switch ……………………………… LIFT GUARD, TURN ON Avionics Bus Tie Switch ………………………………………… LIFT GUARD, TURN ON Electrical Load …………………………….. REINSTATE essential electrical systems Exercise caution not to exceed capacity of standby electrical system (approximately 75 amps). LAND AS SOON AS PRACTICAL

Question 31

EMERGENCY DECENT

Answer 31

Seats, Seat Belts, Shoulder Harnesses ………………………………………….. SECURE Power Lever …………………………………………………………………………………..IDLE Propeller Control Lever …………………………………………………… FULL FORWARD Wing Flaps …………………………………………………………………………………….. 10° Airspeed ………………………………………………………………………………… 175 KIAS A moderate angle of bank may be used to turn the aircraft off the current airway and to ensure positive airframe loading until the descent is established. If in turbulent conditions Wing Flaps ………………………………………………………………………………………. UP Airspeed ………………………………………………………………………………………….. VA

Question 32

State the meaning behind each annunciator

Answer 32

VOLTAGE LOW

Indicates electrical system bus voltage is low and power is being supplied from the battery.

ENGINE FIRE

Indicates an excessive temperature condition and/or possible fire has occurred in the engine compartment.

VACUUM LOW

Indicates the vacuum system suction is less than approximately 3.0 in. Hg.

OIL PRESSURE LOW

Indicates engine oil pressure is less than 38 psi.

RESERVOIR FUEL LOW

Indicates the fuel level in the reservoir tank is approximately half full or less.

GENERATOR OFF

Indicates the generator is not connected to the airplane bus.

EMERGENCY POWER LEVER

Indicates the emergency power lever is advanced out of the NORMAL position.

BATTERY OVERHEAT

Indicates the electrolyte temperature in the optional Ni Cad battery is critically high.

DOOR WARNING

Indicates the upper cargo door and/or upper aft passenger doors (Passenger Version only) are not latched.

FUEL SELECT OFF

Indicates one or both fuel tank selectors are off.

LEFT FUEL LOW

Indicates fuel quantity in the left fuel tank is 25 gallons or less.

RIGHT FUEL LOW

Indicates fuel quantity in the right fuel tank is 25 gallons or less.

AUXILIARY FUEL PUMP ON

Indicates the auxiliary fuel pump is operating.

STANDBY ELECTRICAL POWER ON

Indicates the standby alternator is supplying electrical power to the bus.

FUEL PRESSURE LOW

Indicates fuel pressure in the fuel manifold assembly is below 4.75 psi.

INVERTER INOP

Indicates the selected inverter is not operating (Airplanes with KFC-250 Autopilot).

STANDBY ELECTRICAL POWER INOPERATIVE

Indicates electrical power is not available from the standby alternator.

CHIP DETECTOR

Indicates that metal chips have been detected in either the reduction gearbox case or accessory gearbox case.

BATTERY HOT

Indicates the electrolyte temperature in the optional Ni Cad battery is excessively high.

STARTER ENERGIZED

Indicates the starter-generator is operating in the starter mode.

IGNITION ON

Indicates electrical power is being supplied to the engine ignition system.

DE-ICE PRESSURE

Indicates pressure in the de-ice boot system has reached approximately 15 psi.

WINDSHIELD ANTI-ICE

Indicates electrical power is being supplied to the windshield anti-ice power relay.