Phase One Items Flashcards
(33 cards)
Evacuation
Fuel Condition Lever ……………………CUTOFF Propeller Control Lever ………………FEATHER Radio Call ……………………………. AS REQUIRED Cabin Lights ………………………………..AS REQUIRED Battery Switch …………………………………… OFF Evacuation …………………………………………… ORDER
Engine securing procedure
IF at night OR in IMC: Standby Vacuum System ………………………….ON Power Lever …………………………… FLIGHT IDLE Propeller Control Lever ………………FEATHER Fuel Condition Lever ………………………… CUTOFF
REJECTED TAKE-OFF / ENGINE FAILURE – DURING THE TAKE-OFF ROLL
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
REJECTED TAKE-OFF / ENGINE FAILURE – AIRBORNE BELOW TURNBACK ALTITUDE
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
ENGINE POWER LOSS DURING FLIGHT
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
AIR START WITH STARTER ASSIST
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
AIR START WITH NO STARTER ASSIST
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.
FORCED LANDING WITHOUT POWER
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.
PRECAUTIONARY LANDING WITH ENGINE POWER
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
DITCHING
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
ENGINE FIRE DURING GROUND OPERATIONS
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
ENGINE FIRE IN FLIGHT
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
ELECTRICAL FIRE
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
CABIN FIRE ON THE GROUND
Power Lever …………………………..IDLE Brakes ……………………………………… AS REQUIRED Propeller Control Lever ……………………….FEATHER Fuel Condition Lever …………………………CUTOFF Battery Switch ……………………………………………OFF Airplane ………………………………………….. EVACUATE Fire …………………………………………….. EXTINGUISH
CABIN FIRE IN THE AIR
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
WING FIRE
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
EXITING ICING CONDITIONS
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.
Yoke snatch
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.
PROPELLER ANTI-ICE SYSTEM MALFUNCTION
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.
SURFACE DE-ICE BOOT MALFUNCTIONS
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.
OIL PRESS LOW
Oil Pressure Gauge ……………………….CHECK IF Oil Pressure Gauge confirms annunciator: Engine Shutdown ……………………… CONSIDER Consistent with safety, continue engine operation and prepare for emergency landing.
FCU MALFUNCTION (engine falls to idle)
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
BETA ANNUNCIATOR
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.
CHIP DETECTOR ANNUNCIATOR
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.
