meridian_pa46 Checklist

Piper Meridian PA-46-500TP Checklist

Wright Aviation Services LLC 2011 Page 1

BEFORE ENGINE START PSGR BRIEFING Complete DOORS Closed 4 green

WARNING Do not initiate any flight if all four door pin indicators are not green and/or the DOOR AJAR annunciatior is illuminated SEATS Adjust & Lock PARK BRAKE SET ELECT SWITCHES-ALL Verify OFF FUEL SHUTOFF Verify IN, Cvrd MIC SELECT SWITCH Verify BOOM BLEED AIR LEVER Verify OUT POWER LEVER IDLE CONDITON LEVER AFT/FEATHER MOR LEVER AFT, IN Detent ECS Switch to OFF CABIN COMFORT Verify OFF CB PANELS-Left/Right CHECKEDALL IN AVIONICS Verify OFF ENGINE START IF CART START - Connected, volts 28 BATTERY SWITCH ON VOLTAGE BATT - 24-26 VOLTS

CART - 24-29 VOLTS FIRE DETECT TEST ANNUN ON FUEL PUMP MANUALANNUN ON IGNITORS MANUALANNUN ON PROP AREA CLEAR AUTO START switch LIFT COVER & PUSH OIL PRESS CHECK RISING Ng 13%+ STABLIZED CONDITION LEVER RUN MONITOR ITT ROLL BACK



ENGINE RUN-UP PARK BRAKE SET PCL 1900 RPMS OVERSPEED GEN

NP RELEASE SWITCH

LIFT GUARD AND PRESS OBSERVE 60 RPM DROP RPM RETURNS TO 1900

ICE Equip check as required REVERSE LOCKOUT PRESS & HOLD: 5+Seconds PCL TO BETA LOCKED OUT verify RELEASE LOCKOUT VERIFY BETA PCL IDLE ELECTRICAL CHECK GENERATOR . ALTERNATOR .. GENERATOR .... ALTERNATOR

OFF - VERIFY ANNUN ON VERIFY LOAD PICKUP OFF - VERIFY ANNUN ON . VERIFY LOW VOLTS ON ON - ANNUN OFF .. VERIFY LOW VOLT OFF ON VERIFY ANNUN OFF

BEFORE TAKEOFF Friction Lock Set Seat Backs Verify Upright Armrests Verify Stowed Belts/Harnesses Check ON and Adjusted Generator/Alternator Verify ON/ON Bleed Air Lever In (ON) ECS Switch Normal Pressure System Verify Set Flight Instruments Verify Set Engine Instruments Verify All in GREEN Radios/Avionics/GPS Set/Programmed Trim Verify Set-Elev & Rudder Flaps Set for takeoff Flight Controls Free and CORRECT Fuel Pumps ON Ignitors ON Windshield Heat ON as required (LOW) Pitot Heat ON Nav & Strobe Lights Verify ON Landing Light Cleared for takeoff-ON Recognition Lights Cleared for takeoff-ON Annunciators Appropriate for conditions TAKEOFF Brakes APPLY Power Set (1275-1300 torque) Brakes RELEASE Rotate (Vr) 85 KIAS Initial Airspeed Pitch for 100 KIAS Positive Rate of Climb GEAR UP Flaps UP & Verify Landing Light OFF Fuel Pumps AUTO Ignitors AUTO

CLIMB Climb Power Set to MCP (1300 LBS Torque) Ice Protection As required Recognition lights OFF

Torque .. 1313 ft lbs max ITT .. 770C max

Monitor Engine Instruments

Ng 101.7% max To FL200 145 KIAS Airspeed Above FL200 .. 135 KIAS

Pressurization Set & Monitor 10,000 Climb Check Repeat Above Cabin Comfort Adjust as required for psgrs Windshield Defog On as required Through FL180 Set Altimeters 29.92 CRUISE Cruise Power Set per Tables Engine Instruments Monitor Fuel Instruments Monitor Pressurization Adjust as needed & Monitor Cabin Comfort As required for psgrs Flight Instruments CROSS CHECK Periodically DESCENT ALT pre-select SET to next Altitude Windshield Defrost Verify ON Windshield Heat Defog or DeIce as required Ice Protection AS REQUIRED Power Set (approx cruise torque) Cabin Altitude Set to dest altitude MSL Cabin Rate Set for Comfort

Set Altimeters per ATC Through FL180 SET Cabin-(Field +500 ft)

APPROACH Altimeters Set to field Flight Instruments Crosscheck & Verify Pressure Check Fuel Pumps Manual/on Ignitors Manual/on Fuel Quantity Check Seats & Armrests Upright and Stowed Seatbelts Verify ON & Snug FLAPS SET - 10 168 kias GEAR DOWN 168 kias LANDING CHECK GEAR THREE (3) GREEN BRAKES VERIFY PRESSURE FLAPS AS REQUIRED (135/118) AUTOPILOT OFF POWER AS REQUIRED FINAL AIRSPEED 85 KIAS over threshold



GO AROUND/MISSED APPROACH Initiate PRESS GA button

Positive Pitch Attitude Pitch & Power Set Power - 1300 ft lbs

Climb Pitch for 85 KIAS FLAPS Set 10 GEAR Positive rate of climb - Gear Up Navigation Initial Climb as instructed Autopilot Engage as appropriate GPS Guidance Unsuspend for MA guidance

Once stabilized Refer to CLIMB CHECKLIST

AFTER LANDING (clear of active runway) FLAPS UP Transponder Verify GRD or SBY DeIce Equipment OFF Pitot Heat OFF Landing Lights OFF Recognition Lights TO TAXI Radar OFF ECS Switch OFF Bleed Air PULL OUT (OFF) Cabin Comfort AS REQUIRED Fuel Pump AUTO Ignitor OFF Traffic System OFF Standby Altimeter OFF

SHUTDOWN WARNING: If there is any evidence of fire within the engine during shutdown, proceed IMMEDIATELY with DRY MOTORING Procedures CAUTION: When the Condition Lever is moved aft to the CUTOFF/FEATHER position, the prop should go into the FEATHER position and quickly (20 to 30 seconds) come to a stop. If the prop continues to windmill (failed to feather) a feathering failure has occurred. Investigate and correct the problem prior to the next flight. Parking Brake Set ECS Switch Verify OFF Cabin Controls OFF ALL Exterior Lights OFF Avionics Master OFF Fuel Pump OFF Ignitor Verify OFF Generator OFF Alternator OFF Autopilot Master OFF Condition Lever CUTOFF/FEATHER Feather Annunciator Verify ON Battery Master OFF Oxygen System OFF Parking Brake when chalked - Release HOBBS Note READING

DRY MOTORING PROCEDURE

Allow a minimum of 30 seconds of fuel draining before proceeding to this procedure

PCL IDLE Condition Lever Cutoff/Feather Fuel Pump OFF Ignitors OFF Battery Master ON Start Mode MANUAL Manual Starter PUSH and HOLD 15 seconds Manual Starter Release

NOTE Observe Starter Motor Cooling Limits

(POH Section 2.9) FLIGHT INTO KNOWN ICING

NOTE: Flight into known icing conditions is approved only if the required ice protection systems are installed and functioning properly. That equipment includes:

Surface De-Ice System Propeller Heat Anti-Ice System

Windshield Heat Anti-Ice System Pitot Anti-Ice System

Stall Warning Anti-Ice System Wing Ice Inspection Light

WARNING: Flight into known icing conditions is prohibited if there is known failure of any of the ice protection equipment OR if the Generator or Alternator are failed or are inoperative. WARNING: MAXIMUM FLAP extension with ANY accumulation of ice is 20. PRIOR to entering known icing conditions the following ice protection equipment MUST be activated. Surface De-Ice ON

Stall Heat ON

Prop Heat ON

Pitot Heat verify ON

Windshield Heat As requiredDefog/Anti-Ice

Ignition Manual

Windshield Defog ON

ECS HIGH

Wing Leading Edges Monitor for continual shedding of ice

Annunciator Panel Monitor for correct function of ice protection systems

WARNING: If any aircraft ice protection system fails during flight in icing conditions, exit icing immediately and avoid any further known icing conditions. Departing Icing conditions with residual and intercycle airframe ice, leave all Ice Protection Systems ON Ignition Auto

After removal of residual and intercycle airframe ice

Surface De-Ice OFF

Stall & Prop Heat OFF

Windshield Heat As requiredDefog/Anti-Ice



AIRSPEEDS FOR SAFE OPERATIONS

Vx (Best Angle) 95 Vy (Best Rate) 125

SL to FL200 145 VCruise Climb-Normal FL200 to FL300 135 Vo Max Operating Maneuvering 127 Vno Structural Cruise 168 Vne Never Exceed 188 Vg Best Glide 100

GEAR AND FLAP SPEEDS

Vlo Landing Gear Retract Max 129 Vle Landing Fear Extend Max 168 Vfe - 10 Flaps 10 Degree Max 168 Vfe - 20 Flaps 20 Degree Max 135 Vfe - 36 Flaps 36 Degree Max 118

Critical Air Speeds

Vs Stall Speed Gear & Flaps UP 79 Vso Stall Speed Gear Down, Full Flaps 69 Vi - Minimum Ice Penetration Speed 140 Vbi - Max Boot Inflation Speed 178

WEIGHT AND BALANCE CALCULATIONS

FORMULA is Wgt X ARM = Moment Description Wgt Arm Moment

Aircraft Empty Wgt

Flight Deck Wgt

135.50

Storage Cabinets

156.25

Aft Facing Seats Wgt

177.00

Rear Seats Wgt

218.75

Bag Stowage Wgt (100 lbs max)

248.23

Oil Storage Compart. 286.5 Zero Fuel Weight (4850 lbs maximum)

Fuel (*use chart-page 6)

Ramp Weight (5134 lbs max)

Minus Fuel for Start, Taxi, Run-up

Gross Takeoff Wgt (5092 lbs Max)



PREFLIGHT INSPECTION

COCKPIT ALL SWITCHES OFF GEAR HANDLE DOWN ALL CIRCUIT BREAKERS IN FLIGHT CONTROL LOCKS REMOVED BATTERY MASTER ON FLAPS DOWN FUEL TANKS NOTE QTY HOBBS METER NOTE READING EXTERNAL LIGHTS VERIFY ALL LANDING GEAR LIGHTS THREE GREEN BATTERY MASTER OFF EMPENNAGE STATIC PORTS LEFT & RIGHT

CLEAR

STOWAGE COMPARTMENT DOOR SECURE GPU PORT DOOR SECURE ANTENNAS (TOP & BOTTOM) CHECK SURFACE CONDITION UNCONTAMINATED DEICE BOOTS CHECK ELEVATOR & TRIM TAB CHECK VORTEX GENERATORS CHECK Note: if more than 5 vortex generators are damaged or missing, aircraft is not airworthy. EMPENNAGE (continued) RUDDER & RUDDER TRIM CHECK STATIC WICKS (11) CHECK TIE DOWN REMOVED RIGHT WING SURFACE CONDITION UNCONTAMINATED FLAPS & HINGES CHECK AILERON & HINGES CHECK STATIC WICKS (3) CHECK WING TIP & LIGHTS CHECK FUEL TANK VENT CHECK DEICE BOOT CHECK STALL STRIPS CHECK VORTEX GENERATORS CHECK Note: if more than 5 vortex generators are damaged or missing, aircraft is not airworthy. RADAR POD & STOWAGE CHECK & SECURE PITOT HEAD REMOVE COVER & CK TIE DOWNS & CHOCK REMOVE GEAR DOOR CHECK TIRE CHECK BRAKE BLOCK & DISC CHECK

NOSE SECTION GENERAL CONDITION CHECK RIGHT COWL OPENCHECK-SECURE INLET PLUGS REMOVE & STOW EXHAUST STACKS REMOVE COVER-CHECK AIR INLETS CLEAR RIGHT FUEL SUMPS DRAIN AND CHECK PROP SPINNER CHECK PROPELLER CHECK & ROTATE LANDING LIGHT CHECK NLG STRUT CHECK NLG TIRE CHECK NLG GEAR DOORS CHECK LEFT FUEL SUMPS CHECK FWD UPPER COWL CHECK & SECURE LEFT COWL DOOR OPEN CHECK OIL LEVEL OIL FILLER CAP VERIFY FULLY CLOSED ALT & AC COMP BELT CHECK TENSION & WEAR BRAKE FLUID CAP VERIFY CLOSED LEFT COWL DOOR CLOSE & SECURE LEFT WING SURFACE CONDITION UNCONTAMINATED DEICE BOOTS CHECK STALL WARNING VANE CHECK PITOT HEAD REMOVE COVER & CK TIE DOWNS & CHOCK REMOVE GEAR DOOR CHECK TIRE CHECK BRAKE BLOCK & DISC CHECK VORTEX GENERATORS CHECK Note: if more than 5 vortex generators are damaged or missing, aircraft is not airworthy STALL STRIPS CHECK FUEL TANK VENT CHECK WING TIP & LIGHTS CHECK STATIC WICKS (3) CHECK AILERON & HINGES CHECK FLAPS & HINGES CHECK ENTRY DOOR SEAL CHECK

meridian_pa46 Checklist

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