Version 1.0, September 25th, 2008 Page 1 of 33

NORMAL PROCEDURES CHECKLIST

PA-28RT-201T, PIPER TURBO ARROW IV

(ICAO: P28T)

FOR REFERENCE ONLY NOT FOR FLIGHT

Introduction -1

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INSURANCE Countries European Union plus Norway and Switzerland EU = Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, United Kingdom. PIC requirements Approved by owner >300 hrs total Instrument Rated Uses Private and Private Business WEIGHT LIMITS Maximum Ramp Weight 2912 LB (1321 kg) Maximum Takeoff Weight (MTOW) 2900 LB (1315 kg) Maximum Landing Weight 2900 LB (1315 kg) Basic Empty Weight (dd 080919) 1942 LB (881 kg) Maximum Baggage 200 LB (91 kg)

FUEL LIMITATIONS Minimum Aviation Fuel Grade 100LL / 100 Total Capacity 77 U.S. GAL. ( 291 l) Unusable Fuel 5 U.S. GAL. ( 19 l) Usable Fuel 72 U.S. GAL. ( 272 l 196 kg) Usable Fuel to bottom of filler neck indicator 50 U.S. GAL. ( 189 l 136 kg) USEFUL LOADS Useful load, total 958 LB (434 kg) Useful load with full fuel 525 LB (238 kg) Useful load with fuel to filler neck indicator 657 LB (298 kg) OPERATING ALTITUDE LIMITATIONS Flight above 20,000 feet pressure altitude is not approved. Flight up to and including 20,000 feet is approved if equipped with oxygen in accordance with FAR 23.1441 and avionics in accordance with FAR 91 or FAR 135. REMARKS

� Checklist items indicated with a dot on the left side are additional items not mentioned in the POH. Checklist items indicated by a barber pole are additional items especially for IFR flights.

Introduction - 2

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AIRSPEEDS FOR SAFE OPERATIONS Best Angle of Climb Speed, gear down, flaps up 73 KIAS Best Angle of Climb Speed, gear up, flaps up 79 KIAS Best Rate of Climb Speed, gear down, flaps up 79 KIAS Best Rate of Climb Speed, gear up, flaps up 97 KIAS Turbulent Air Operating Speed 124 KIAS (2900 LBS) – 97 KIAS (1893 LBS) Maximum Flaps Extended Speed 108 KIAS Landing Final Approach Speed (Flaps 40°) 75 KIAS Maximum Demonstrated Crosswind Velocity 17 KTS Maximum tail wind for take-off and landing 5 KTS AIRSPEED LIMITATIONS Never Exceed Speed (VNE) 193 KIAS Do not exceed this speed in any operation. Maximum Structural Cruising Speed (VNO) 152 KIAS Do not exceed this speed except in smooth air and then only with caution. Design Maneuvering Speed (VA) Do not make full or abrupt control movements above this speed. At 2900 LBS. Gross Weight 124 KIAS At 1893 LBS. Gross Weight 97 KIAS

CAUTION Maneuvering speed decreases at lighter weight as the effects of aerodynamic forces become more pronounced. Linear interpolation may be used for intermediate gross weights. Maneuvering speed should not be exceeded while operating in rough air.

Maximum Flaps Extended Speed (VFE) 108 KIAS Do not exceed this speed with the flaps extended. Maximum Landing Gear Extension Speed (VLO) 133 KIAS Do not exceed this speed when extending the landing gear. Maximum Landing Gear Retraction Speed (VLO) 111 KIAS Do not exceed this speed when retracting the landing gear. Maximum Landing Gear Extended Speed (VLE) 133 KIAS Do not exceed this speed with the landing gear extended. POWER PLANT LIMITATIONS Engine: one Teledyne Continental Model No. TSIO-360-FB Engine Operating Limits Maximum Engine Speed 2575 RPM Maximum Oil Temperature 240 °F Maximum Manifold Pressure 41 inHg Propellers Hartzell (3 Blade) PHC-C3YF1( )F/F7663

Preflight - 1

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Preflight Checklists COCKPIT

CAUTION The flap position should be noted before boarding the airplane. The flaps must be placed in the UP position before they will lock and support weight on the step.

Control wheel release restraints Parking Brake SET All switches OFF

� Magnetos OFF � Radio Master Switch OFF � Gear Handle DOWN

Mixture IDLE CUT-OFF Master Switch ON ELT annunciator CHECK – OFF ; otherwise reset Fuel Gauges CHECK quantity Annunciator Panel CHECK Master Switch OFF Primary Flight Controls PROPER OPERATION Flaps PROPER OPERATION

� Flaps EXTEND Trim NEUTRAL Pitot and Static System DRAIN Windows CHECK clean Required Papers CHECK on board Tow bar baggage STOW PROPERLY – SECURE Baggage door CLOSE AND SECURE RIGHT WING

CAUTION When draining any amount of fuel, care should be taken to ensure that no fire hazard exists before starting engine.

Surface Condition CLEAR OF ICE, FROST, SNOW Flap and Hinges CHECK Aileron and Hinges CHECK Wing Tip and Lights CHECK Fuel Tank CHECK supply; visually - SECURE CAP Fuel Tank Vent CLEAR Fuel Tank Sump DRAIN and CHECK for water, sediment and proper fuel Tie Down and Chock REMOVE Main Gear Strut PROPER INFLATION (2.5 +/- 0.25 in.) Tire CHECK Brake Block and Disc CHECK Fresh air inlet CLEAR NOSE SECTION General Condition CHECK Cowling SECURE Windshield CLEAN Propeller and Spinner CHECK Air Inlets CLEAR Alternator belt CHECK tension Chock REMOVE Nose Gear Strut PROPER INFLATION (2.75 ± 0.25 in.) Nose Wheel Tire CHECK Engine Baffle Seal CHECK Oil CHECK QUANTITY Dipstick PROPERLY SEATED Oil Filler Cap SECURE Fuel strainer DRAIN and CHECK for water, sediment and proper fuel

Preflight - 2

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LEFT WING Surface Condition CLEAR of ICE, FROST, SNOW Fresh air inlet CLEAR Tie Down and Chock REMOVE Main Gear Strut INFLATION (2.5 +/- 0.25 INCH) Tire CHECK Brake Block and Disc CHECK Fuel Tank CHECK supply; visually - SECURE CAP Fuel Tank Vent CLEAR Fuel Tank Sump DRAIN and CHECK for water, sediment and proper fuel Pitot/static Head REMOVE cover, HOLES CLEAR Wing Tip and Lights CHECK Aileron and Hinges CHECK Flap and Hinges CHECK FUSELAGE Antennas CHECK Empennage CLEAR OF ICE, FROST, SNOW Fresh air inlet CLEAR Stabilator and trim tab CHECK Tie Down REMOVE

� Rudder CHECK MISCELLANEOUS Oxygen System (if installed) CHECK MASKS and HOSES

� Flaps RETRACT Master Switch ON Cockpit Lighting CHECK (overhead, panel) Pitot Heat Switch ON Nav and strobe lights ON

� Landing Light ON Nav and strobe light right wing CHECK Landing Light CHECK Nav and strobe light left wing CHECK Stall Warning CHECK Pitot heat CHECK – WARM

� Taxi Light ON � Taxi Light CHECK

All Lighting Switches OFF Pitot Heat Switch OFF Master Switch OFF All Switches OFF Passengers BOARD Cabin Door CLOSE and LATCH Seats adjusted and locked in position Seat Belts and Harness FASTEN/ADJUST;CHECK inertia reel

� Seat Belts empty seats SECURED

Starting - 1

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Before Starting Engine Checklist BEFORE STARTING ENGINE

� Passengers BRIEFED Avionics switch OFF

� Trims CHECK – T/O position � Brakes CHECK pressure

Parking Brake SET Propeller Control FULL INCREASE rpm Alternate air OFF

� Circuit Breakers CHECK in � All Switches OFF (incl. A/P) � Audio panel CHECK & SET � COM/NAV/ADF volume SET (approx. half open) � Cockpit inspection COMPLETED � All instruments CHECK

Flashlight CHECK � Ignition key IN PACE and OFF � Master switch ON � Annunciator panel PRESS TO TEST � Fuel quantity CHECK SUFFICIENT

Fuel selector DESIRED TANK - LEAST FULL TANK � Avionics master switch ON � ATIS COPIED � Altimeter SET � Start-up clearance ("CPFIR') RECEIVED � "CPFIR" = Call Sign + type, Position + POB, Flight Rules, Information, Request � Avionics master switch OFF

Starting - 2

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Starting Engine Checklist ENGINE START - GENERAL

CAUTION If a positive oil pressure is not indicated within 30 seconds following an engine start, stop the engine and determine the trouble. In cold weather it will take a few seconds longer to get a positive oil pressure indication.

NOTE To prevent starter damage, limit starter cranking to 30 second periods. If the engine does not start within that time, allow a cooling period of several minutes before engaging starter again. Do not engage the starter immediately after releasing it. This practice may damage the starter mechanism.

STARTING ENGINE Fuel selector ON (LEAST FULL TANK) Mixture full RICH Throttle full FORWARD Propeller full FORWARD Master Switch ON Auxiliary fuel pump OFF

� Strobe Lights ON � Propeller CLEAR

Primer ON see tables:

OAT Priming Time (s) OAT Priming Time (s) °C Min Max °C Min Max

-29 29 34 0 9 11 -27 27 32 2 8 10

-24 25 30 4 7 9

-22 24 28 7 6 8 -20 22 26 9 6 7

-18 20 24 11 5 7

-16 18 22 13 4 6 -13 16 20 16 4 5

-11 15 19 18 4 5

-9 14 17 20 - 38 3 4 -7 12 15

-4 11 14

-2 10 13 Primer HOLD ON WHEN OAT below 20 °F = - 6 °C Primer RELEASE WHEN OAT above 20 °F = - 6 °C Throttle CLOSE Starter ENGAGE IMMEDIATELY When engine starts firing: Throtltle OPEN slowly At 500 RPM: Starter RELEASE Throttle CONTINUE OPEN SLOWLY 1000 RPM Primer RELEASE Auxiliary fuel pump ON – LOW as necessary to obtain smooth engine operation (1 – 3 min when OAT < 20 °F = - 6 °C)

� Starter warning light CHECK - OUT Oil Pressure CHECK Alternator CHECK Gyro Suction CHECK (4.8 – 5.1 inHg) WARM-UP

� Engine start time NOTED Throttle 900 to 1200 RPM

Avionics, Briefing, Autopilot and Trim

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Briefing and Avionics Checklist

� Autopilot Master Switch ON � Start-up clearance ("CPFIR') RECEIVED � "CPFIR" = Call Sign + type, Position + POB, Flight Rules, Information, Request

Avionics CHECK: Marker lights, COM 1/2, ILS 1/2, NAV 1/2, DME, ADF, Transponder. Crew briefing COMPLETED: I will do the flying, you monitor all instruments and report malfunctions loud and clear On my command you read the checklist, do the RT, set the transponder, tune and identify beacons. When VMC you check outside for safety. Any questions?

� ANWB briefing = Aircaft, Notams, Weather, Departure Briefing, Taxi route � Avionics SET

Autopilot and Trim Checklist NOTE This a short preflight test, the official preflight test can be found in the ‘External Normal Procedures Checklist’ further down in this booklet.

� Autopilot Master Switch CHECK - ON � AP Annunciator CHECK – RDY on (within 3 minutes after switching AP on) � Autopilot Master Switch TEST � AP Annunciators CHECK - ALL on � Autopilot Master Switch ON � AP Annunciators CHECK - RDY on � HDG bug SET to lubber line � HDG and ALT mode SELECT � AP Annunciators CHECK – HDG and ALT annunciators on � HDG bug left and right CHECK control wheel moving correctly � UP button PRESS - CHECK control wheel moves aft,

and keeps moving when button released � DOWN button PRESS - CHECK control wheel slows down and

moves forward and keeps moving when button released � AP disconnect button PRESS

CHECK AP disconnects to RDY annunciator CHECK control wheel freedom

� Trim Master Switch ON � Both electrical trim buttons CHECK trim wheel moves in correct direction (both)

Either electrical trim button CHECK trim wheel does not move � Trim Master Switch OFF � Both electrical trim button CHECK trim wheel does not move � Trim Master Switch ON � HDG mode SELECT � AP Annunciators CHECK – HDG annunciator on � Both electrical trim buttons CHECK trim wheel moves in correct direction (both)

CHECK AP disconnects to RDY annunciator CHECK control wheel freedom

� Trim SET for take-off

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Taxi and ground - 1

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Before Taxiing Checklist � Alternator & Alt load CHECK � Pitot heat CHECK (ON – OFF) � Engine instruments CHECK � HSI CHECK � Slaving OFF � CW/CWW CHECK � Slaving ON � HSI CHECK heading � RMI rose CHECK heading � Backup Directional Gyro SET � Lights (Taxi) AS REQUIRED � Strobe Lights AS REQUIRED

Taxiing Checklist � Request taxi APPROVED

Chocks REMOVED Taxi Area CLEAR Parking Brake RELEASED Prop FULL INCREASE Throttle APPLY SLOWLY Brakes CHECK Steering CHECK

� Flight Instruments / Gyro’s CHECK (Attitude Indicators (2x), HSI, DG, RMI, Turn ind.) Route clearance ("CRAX") COPIED/RECEIVED "CRAX" = Cleared to, Route, Altitude/FL, Transponder

� Transponder SET

Ground Check Checklist Parking Brake SET Radios & Nav equipm. if recleared: SET, briefed

� Fuel selector SWITCH TANK - FULLEST TANK Propeller FULL INCREASE Throttle 1800 to 2000 RPM

� Horizon SET � Horizon second AI SET

Magnetos (max 10 sec) max. drop 150 RPM max. diff. 50 RPM Vacuum CHECK (4.8 inHg to 5.1 inHg) Oil Temperature CHECK Oil Pressure CHECK Annunciator Panel PRESS-TO-TEST Propeller Control EXERCISE – then FULL INCREASE Limit to max drop of 200 – 300 RPM Cold weather: 3 times Alternate Air CHECK

NOTE Engine is warm for takeoff when oil temperature is at least 100 °F

Auxiliary Fuel Pump OFF Fuel Pressure CHECK Throttle RETARD 1200 RPM Manifold Pressure Line DRAIN (5 sec at < 25 inHg)

Taxi and Ground - 2

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Before Takeoff Checklist Master Switch ON Flight Instruments CHECK Fuel Selector PROPER TANK - FULLEST Auxiliary Fuel Pump OFF Engine Gauges CHECK Alternate Air CLOSED Seat Backs ERECT

� Seats ADJUSTED& LOCKED IN POSITION Mixture SET Prop SET Belts/Harness FASTENED/ADJUSTED Flaps CHECK - SET Trim tab SET Controls FREE Doors LATCHED

� Magnetos verify BOTH � Autopilot NOT ACTIVE � HSI CHECK heading � RMI rose CHECK heading � Backup Directional Gyro CHECK - SET � T/O briefing Cockpit silence during T/O

If you observe any malfunctioning below Vr= 70-77 KIAS / 53-64 KIAS call "STOP" loud and clear and state the reason. In case of engine failure when airborne and not enough runway to land straight ahead, I will make shallow turns to avoid obstacles and select a suitable field.

� Departure Clearance RECEIVED � Window CLOSED � Landing Light ON � Nav lights & Panel lights AS REQUIRED � Strobe Lights AS REQUIRED � Pitot Heat ON

Clearance limit KNOWN � Departure time NOTED � Transponder CORRECT CODE & ALT

Parking Brake RELEASE

Take off

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Takeoff Checklist TAKEOFF - GENERAL

NOTE At altitudes below 12,000 feet, normal take offs are made with less than full throttle setting. Use the throttle as required to obtain 4l In. Hg. manifold pressure DO NOT EXCEED 4l inHg MANIFOLD PRESSURE. The overboost warning light will illuminate when manifold pressure approaches the maximum limit.

1) NORMAL TECHNIQUE Flaps SET Trim Tab SET

� Heading CHECKED � Power Max 41 inHg

Accelerate to 70-77 KIAS Control wheel BACK PRESSURE to rotate to climb attitude

� Best Angle of Climb Speed, gear down, flaps up 73 KIAS

� Best Rate of Climb Speed, gear down, flaps up 79 KIAS � When straight ahead landing on runway not possible: � Positive climb CHECK � Gear BRAKES, UP � Best Angle of Climb Speed, gear up, flaps up 79 KIAS � Best Rate of Climb Speed, gear up, flaps up 97 KIAS

� 200 ft AGL: Flaps RETRACT � 200 ft AGL: Transponder CHECK - ALT

FOR CLIMB SEE NEXT PAGE

2) SHORT FIELD, OBSTACLE CLEARANCE

Flaps 25°, second notch � Trim Tab SET � Heading CHECKED � Power Max 41 inHg

Accelerate to 53 - 64 KIAS depending on aircraft weight Control wheel BACK PRESSURE to rotate to climb attitude After breaking ground: Accelerate to 59 – 68 KIAS depending on aircraft weight Gear BRAKES, UP Accelerate to Best flaps up Angle of Climb speed 79 KIAS Flaps RETRACT slowly, climb past obstacle Accelerate to Best flaps up Rate of Climb Speed 97 KIAS

� 200 ft AGL: Transponder CHECK - ALT

FOR CLIMB SEE NEXT PAGE

3) SOFT FIELD

Flaps 25°, second notch � Trim Tab SET � Heading CHECKED � Power Max 41 inHg

Accelerate to 53 - 64 KIAS depending on aircraft weight Control wheel BACK PRESSURE to rotate to climb attitude After breaking ground: Accelerate to 59 – 68 KIAS depending on aircraft weight Gear BRAKES, UP Accelerate to Best Rate of Climb Speed 97 KIAS Flaps RETRACT slowly

� 200 ft AGL: Transponder CHECK - ALT

FOR CLIMB SEE NEXT PAGE

Climb

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Climb Checklist TAKEOFF CLIMB Mixture FULL RICH Propeller Speed 2575 RPM Manifold Pressure DO NOT EXCEED 41 inHg Climb Speed Best Angle 79 KIAS Best Rate 97 KIAS Auxiliary Fuel Pump LO – if required: hot weather, vapor suppression (fluctuating fuel flow) CRUISE CLIMB

� (after takeoff: set when adequate terrain clearance obtained (e.g. 500 feet AGL)) Mixture FULL RICH Manifold Pressure 33 inHg Propeller Speed 2450 RPM

� Best Rate of Climb Speed 97 KIAS, only to be used in exceptional cases, � when really required; Otherwise

Climb Speed (improved cooling etc.) 104 KIAS

� Cylinder Head Temp CHECK - MAX 460 °F

Auxiliary Fuel Pump LO – if required: hot weather, high altitude, vapor suppression (fluctuating fuel flow)

� At transition altitude or outside CTR: � Landing Light OFF � Altimeter QNE (1013 hPa) at Transition Alt � Fuel CHECK and SET � Auxiliary Fuel pump OFF at desired altitude

Cruise

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Cruise Checklist

NOTE The maximum permissible cylinder head temperature for all operations is 460°F. To obtain maximum service life of engine components, cylinder head temperature should not exceed 440 °F during cruise operation. Adjust cylinderhead temperatures by reducing power, adjusting the mixture, or any combination of these methods.

NOTE In order to keep the airplane in best lateral trim during cruise flight, the fuel should be used alternately from each tank at one hour intervals.

Normal max power 75 % Power SET per power table Mixture ADJUST Auxiliary Fuel Pump LO – if required: hot weather, high altitude, vapor suppression (fluctuating fuel flow) Alternate Air SET (ON when induction icing expected)

� Fuel balance MONITOR & TIME � Engine instruments MONITOR � Electronics MONITOR � Location MONITOR

POWER SETTING TABLE

Arrival, Approach and Landing

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Arrival, Approach And Landing Checklist

� ARRIVAL � ATIS COPIED

STAR/Approach plates SELECT Heading/distance to IAF/P Holding inbound track KNOWN/SET Holding entry KNOWN TYPE KNOWN COURSE Radio's and nav equip. SET Crew briefing Route, Approach plate Crew briefing Weather APPROACH AND LANDING

� Landing Light ON � Brakes CHECK / OFF � Magnetos CHECK - BOTH � Loose items SECURE � Annunciators CHECK

Terrain clearance/MSA KNOWN � Descent/Approach/Entry CLEARANCE RECEIVED � Altimeter SET

Fuel Selector PROPER TANK – FULLEST Seat Backs ERECT

� Seats ADJUSTED & LOCKED IN POSITION Belts/Harness FASTEN/ADJUST FAF/FAP CHECK: DME and/or NDB SELECTED Missed approach point KNOWN Pos. Fix Alt. KNOWN MDA/DA KNOWN Briefing PNF YOU CALL: OM ALT, 500' HAT(resh), 100' MIN, CONTACT Cockpit silence REQUEST Mixture SET full RICH Gear DOWN - 133 KIAS max. Flaps SET – 108 KIAS max. Propeller @ 800 ft AGL SET full INCREASE Trim to 75 KIAS

� FINAL � Prop FULL FORWARD � Undercarriage THREE GREENS � Flaps SET

After landing

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After Landing Checklist � Landing time NOTED � Stopwatch START for engine shutdown time

Flaps RETRACT � Strobe Lights AS REQUIRED � Landing, Taxi Lights AS REQUIRED � Pitot Heat OFF � Transponder CHECK - GND

Stopping Engine Checklist � Strobe Lights ON

ELT annunciator CHECK – OFF ; otherwise reset and notify ATC At least 5 minutes after landing: Avionics Master Switch OFF Propeller FULL INCREASE Throttle FULL AFT (IDLE) Mixture IDLE CUT-OFF Magnetos OFF

� Switch off time NOTED Master Switch OFF

Parking Checklist Parking Brake SET Control Wheel SECURED with belts Flaps FULL UP Wheel Chocks IN PLACE Tie Downs SECURE

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INFORMATION

PA-28RT-201T, PIPER TURBO ARROW IV

FOR REFERENCE ONLY NOT FOR FLIGHT

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Information

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Information

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2100 lbs 953 kg 1000 ft 305 m

2200 lbs 998 kg 1100 ft 335 m

Surface condition

Takeoff corrections

Landing corrections

2300 lbs 1043 kg 1200 ft 366 m 1° up +10 % - 5 % 2400 lbs 1089 kg 1300 ft 396 m 1° down - 5 % + 10 %

2500 lbs 1134 kg 1400 ft 427 m Wet + 15% + 15 %

2600 lbs 1179 kg 1500 ft 457 m Dry grass + 15 % + 45 % 2700 lbs 1225 kg 1600 ft 488 m Wet grass + 40 % + 70 %

2800 lbs 1270 kg 1700 ft 518 m

2900 lbs 1315 kg 1800 ft 549 m 1900 ft 579 m

2000 ft 610 m

2250 ft 686 m 2500 ft 762 m

2750 ft 838 m

3000 ft 914 m 3250 ft 991 m

3500 ft 1067 m

3750 ft 1143 m 4000 ft 1219 m

Information

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Information

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EXTENDED NORMAL PROCEDURES CHECKLIST

PA-28RT-201T, PIPER TURBO ARROW IV

FOR REFERENCE ONLY NOT FOR FLIGHT

Extended Normal - Starting

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ENGINE START WHEN FLOODED Mixture IDLE CUT-OFF Throttle full FORWARD Propeller full FORWARD Master Switch ON Auxiliary Fuel Pump OFF

� Strobe Lights ON Propeller CLEAR Starter ENGAGE When engine fires: Throttle RETARD Mixture ADVANCE SLOWLY

� Starter warning light CHECK - OUT � Oil Pressure CHECK � Alternator CHECK � Gyro Suction CHECK (4.8 – 5.1 inHg)

ENGINE START WITH EXTERNAL POWER SOURCE Master Switch OFF All Electrical Equipment OFF External Power Plug INSERT in receptacle Proceed with normal start.

NOTE For all normal operations using an external power source, the battery master switch should be OFF, but it is possible to use the ship’s battery in parallel by turning the battery master switch ON. This will give longer cranking capabilities, but will not increase amperage.

CAUTION Care should be exercised because if the ship’s battery has been depleted, the external power supply can be reduced to the level of the ship’s battery. This can be tested by turning the battery master switch ON momentarily while the starter is engaged. If cranking speed increases, the ship’s battery is at a higher level than the external power supply.

Throttle LOWEST POSSIBLE RPM External Power Plug DISCONNECT from receptacle Master Switch ON – CHECK alternator ampere meter

� Strobe Lights ON � Oil Pressure CHECK

� Alternator CHECK Gyro Suction CHECK (4.8 – 5.1 inHg) Priming graph

-20 °F = -29 °C /// 0°F = -18 °C /// 20 °F = -6°C /// 40 °F = 4°C /// 60°F = 16 °C /// 80°F = 27 °C /// 100 °F = 38 °C

Extended Normal - Autopilot

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AMS = Autopilot Master Switch, CW = Control Wheel, TW= Trim Wheel, ANN = Annunciators Mode set Action Reaction

El. Trim OFF AMS ON ANN: RDY (within 3 min)

AMS TEST ANN: All ON

Heading bug to lubber line CW freedom left/right HDG mode CW REDUCED freedom left/right

CW OVERRIDE left/right

CW freedom forward/aft ALT mode CW REDUCED freedom forward/aft

CW OVERRIDE forward/aft

UP switch PRESS/HOLD, while maintaining a grasp on CW

Servo disengages after ½ second, as sensed by the increased freedom of CW forward/aft

UP switch RELEASE Servo immediately re-engages, as sensed by the reduced freedom of CW forward/aft

DOWN switch PRESS/HOLD, while maintaining a grasp on CW

Servo disengages after ½ second, as sensed by the increased freedom of CW forward/aft

DOWN switch RELEASE Servo immediately re-engages, as sensed by the reduced freedom of CW forward/aft

AMS ON ANN: All off except RDY on

HDG mode ANN: HDG Heading Bug TURN to the

left and right side of Lubber Line CW turns respectively left and right

Heading bug on lubber line CW stops VOR SELECT

CDI CENTERED

AIRCRAFT TURN course pointer under lubber line

NAV mode ANN: NAV, SOFT

Course pointer TURN to left and right CDI needle 2 dots from center

CW turns right and left respectively

Course pointer TURN to left CDI needle centered

CW stops

HDG mode ANN: HDG

ALT mode ANN: HDG, ALT CW MOVE to elevator neutral

UP switch PRESS/HOLD CW moves aft

UP switch RELEASE CW still moves aft DOWN switch PRESS/HOLD CW slows aft, moves forward

DOWN switch RELEASE CW still moves forward

VS mode ANN: HDG, VS; CW stops UP switch PRESS/HOLD CW moves aft

UP switch RELEASE CW still moves aft

DOWN switch PRESS/HOLD CW slows aft, moves forward DOWN switch RELEASE CW still moves forward

El. Trim ON Move CW full forward After 3 seconds TW run nose up at increasing speed

Move CW aft until TW stops Move CW full aft After 3 seconds TW run nose down at increasing speed

Move CW forward until TW stops

Press manual trim both ANN: RDY 5 sec flashing, RDY steady Press manual trim single (each) TW does not run

Press manual trim both forward ANN: TRIM, TW runs nose down

Press AP DISC / TRIM INTR TW stops RELEASE AP DISC / TRIM INTR TW resumes running nose down

RELEASE manual trim ANN: TRIM off, TW stops

Press manual trim both aft ANN: TRIM, TW runs nose up Press AP DISC / TRIM INTR TW stops

RELEASE AP DISC / TRIM INTR TW resumes running nose up

RELEASE manual trim ANN: TRIM off, TW stops TRIM for T/O

Extended Normal – Stall Exercise

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Before Stall Checklist Trim ADJUST Mixture RICH Primer LOCKED Auxiliary Fuel Pump ON - LO Fuel quantity CHECK Flaps UP Engine instruments CHECK Seat belts FASTENED Loose equipment STOWED Altitude CHECK Position KNOWN Orientation BUG SET Sky clear IF VFR region: CHECK

After Stall Checklist Mixture RICH Engine instruments CHECK Flaps UP Auxiliary Fuel Pump AS REQUIRED Gyro instruments CHECK & SET Orientation CHECK

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EMERGENCY PROCEDURES CHECKLIST

PA-28RT-201T, PIPER TURBO ARROW IV

FOR REFERENCE ONLY NOT FOR FLIGHT

AIRSPEEDS FOR SAFE OPERATIONS Best Angle of Climb Speed 79 KIAS Best Rate of Climb Speed 97 KIAS Turbulent Air Operating Speed 124 KIAS (2900 LBS) – 97 KIAS (1893 LBS) Landing Final Approach Speed (Flaps 40°) 75 KIAS Maximum Demonstrated Crosswind Velocity 17 KTS Maximum Flaps Extended Speed 108 KIAS Best power off glide speed, prop full decrease 97 KIAS

Emergencies - FIRE

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ENGINE FIRE DURING START Starter (crank engine). CRANCK ENGINE Mixture IDLE CUT-OFF Throttle OPEN Primer OFF Fuel Selector OFF Abandon if fire continues FIRE IN FLIGHT Source of Fire CHECK a) Electrical Fire (smoke in cabin): Master Switch OFF Vents OPEN Cabin heat OFF Land as soon as possible.

WARNING If oxygen is installed, use ONLY if flames and heat are not present.

b) Engine fire: Fuel Selector OFF Throttle CLOSED Mixture IDLE CUT-OFF Auxiliary Fuel Pump CHECK OFF Heater and defroster OFF Master switch OFF (if no radio communication needed) Proceed with power off landing procedure.

NOTE The possibility of an engine fire in flight is extremely remote. The procedure given is general and pilot judgment should be the determining factor for action in such an emergency.

Emergencies – ENGINE - 1

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ENGINE POWER LOSS DURING TAKEOFF a) If sufficient runway remains for a normal landing, leave gear down and land straight ahead. b) If area ahead is rough, or if it is necessary to clear obstructions: Gear Selector Switch UP

� Auxiliary Fuel Pump OFF � Fuel Selector OFF � Mixture IDLE CUT-OFF

c) If sufficient altitude has been gained to attempt a restart: Maintain Safe Airspeed Fuel Selector SWITCH to tank containing fuel Auxiliary fuel pump UNLATCH, HI Mixture RICH Alternate Air ALTERNATE Emergency Gear lever as required If power is not regained: Prepare for power off landing.

NOTE If engine failure was caused by fuel exhaustion, power will not be regained after switching fuel tanks until the empty fuel lines are filled. This may require up to ten seconds.

ENGINE POWER LOSS IN FLIGHT Trim for 97 KIAS (Power off glide speed) Fuel selector SWITCH to tank containing fuel Auxiliary Fuel Pump UNLATCH, HI Mixture RICH Alternate Air OPEN Engine Gauges CHECK for indication of cause of power loss If no fuel pressure is indicated, check tank selector position to be sure it is on a tank containing fuel. a) If power is restored: Alternate Air CLOSED Auxiliary Fuel Pump OFF Land as soon as practical and investigate cause of power loss. b) If power is not restored: Trim for 97 KIAS (Power off glide speed) Prepare for power off landing. If time permits: Ignition L then R then BOTH Throttle MOVE Mixture MOVE Fuel tank SWITCH

Emergencies - ENGINE - 2

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POWER OFF LANDING Propeller Control FULL DECREASE Best gliding angle 97 KIAS Suitable field LOCATE Spiral pattern ESTABLISH 1000 ft.above field at downwind position for normal landing approach. When field can easily be reached SLOW to 75 KIAS for shortest landing. Gear down emergency landing Touchdowns should normally be made at lowest possible airspeed with full flaps. When committed to landing: Landing Gear Selector DOWN Throttle CLOSED Mixture IDLE CUT-OFF Master Switch OFF Ignition OFF Fuel Selector OFF Seat belt and harness TIGHT Gear up emergency landing In case of very soft or very wet ground In the event a gear up landing is required proceed as follows: Flaps AS DESIRED Throttle CLOSED Mixture IDLE CUT-OFF Flaps AS REQUIRED Master Switch OFF Ignition OFF Fuel Selector OFF Seat belt and harness TIGHT Contact surface at minimum possible airspeed.

NOTE If the master switch is OFF, the gear cannot be retracted.

ENGINE ROUGHNESS Mixture ADJUST FOR MAXIMUM SMOOTHNESS Alternate Air OPEN

� Auxiliary Fuel Pump LO Fuel Selector SELECT ANOTHER TANK Magnetos L then R then BOTH Magnetos SELECT best setting If roughness persists, prepare for a precautionary landing at pilot’s discretion PROPELLER OVERSPEED Throttle RETARD Oil Pressure CHECK Propeller Control FULL DECREASE rpm, then set if any control available Airspeed REDUCE Throttle AS REQUIRED to remain below 2575 rpm

Emergencies - OIL, FUEL

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LOSS OF OIL PRESSURE Land as soon as possible and investigate cause. Prepare for power off landing. Maintain altitude until such time as a dead stick landing can be accomplished. Don't change power settings unnecessarily, as this may hasten complete power loss. HIGH OIL TEMPERATURE Land at nearest airport and investigate the problem. Prepare for power off landing. LOSS OF FUEL PRESSURE Auxiliary Fuel Pump UNLATCH, HI Fuel selector CHECK on full tank If fuel pressure recovers: Auxiliary Fuel Pump OFF

CAUTION If normal engine operation and fuel flow are not reestablished auxiliary fuel pump should be turned OFF. The lack of a fuel flow indication, while in the HI auxiliary fuel pump position, could indicate a leak in the fuel system or fuel exhaustion.

CAUTION DO NOT actuate the auxiliary fuel pump unless vapor suppression is required (LO position) or the engine-driven fuel pump fails (HI position). The auxiliary pump has no standby function. Actuation of the HI switch position when the engine is operating normal may cause engine roughness and/or power loss.

ENGINE DRIVEN FUEL PUMP FAILURE Throttle RETARD Auxiliary Fuel Pump UNLATCH, HI Throttle RESET (75% power or below)

CAUTION If normal engine operation and fuel flow are not reestablished auxiliary fuel pump should be turned OFF. The lack of a fuel flow indication, while in the HI auxiliary fuel pump position, could indicate a leak in the fuel system or fuel exhaustion.

CAUTION DO NOT actuate the auxiliary fuel pump unless vapor suppression is required (LO position) or the engine-driven fuel pump fails (HI position). The auxiliary pump has no standby function. Actuation of the HI switch position when the engine is operating normal may cause engine roughness and/or power loss.

CAUTION If the auxiliary fuel pump switch or primer switch fails causing the auxiliary fuel pump to be activated in the HI mode while the engine driven fuel pump is operating normally, engine roughness and/or power loss could occur. Should this condition exist, pull out the fuel pump pull-type circuit breaker, if so equipped, or shut off the master switch.

If power is not restored, proceed with power off landing procedure.

Emergencies - ELECTRICAL

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ELECTRICAL FAILURES ALT ANNUNCIATOR LIGHT ILLUMINATED AMMETER CHECK to verify alternator failure If ammeter show zero: ALT switch OFF Reduce electrical loads to minimum ALT circuit breaker CHECK and RESET as required ALT switch ON If power not restored: ALT Switch OFF If alternator output cannot be restored, reduce electrical loads and land as soon as practical. The battery is the only remaining source of electrical power. ELECTRICAL OVERLOAD ALT switch ON BAT switch OFF a) If alternator loads are reduced: Electrical load REDUCE to minimum Land as soon as practical

CAUTION Due to increased system voltage and radio frequency noise, operation with ALT switch ON and BAT switch OFF should be made only when required by an electrical system failure.

b) If If alternator loads are not reduced: ALT switch OFF BAT switch as required Land as soon as practical. Anticipate complete electrical failure

NOTE If the battery is depleted, the landing gear must be lowered using the emergency extension procedure. The gear position lights will be inoperative.

Emergencies - GENERAL

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EMERGENCY LANDING GEAR EXTENSION EXTRA IN CASE OF TRAINING ONLY: PULL “LANDING GEAR PUMP” circuit breaker Prior to emergency extension procedure: Master Switch CHECK ON Circuit Breakers CHECK Panel lights OFF (in daytime) Gear indicator bulbs CHECK If landing gear does not check down and locked: Airspeed BELOW 88 KIAS Landing Gear Selector DOWN If gear has still failed to lock down: Emergency lever MOVE to “EMERGENCY DOWN” If gear has still failed to lock down: Yaw airplane abruptly from side to side with the rudder. If the nose gear will not lock down using above procedure Speed SLOW to lowest safe speed attainable using Lowest power setting required for safe operation and accomplish the following: Landing gear selector switch gear DOWN position If gear does not check down: Gear Selector Switch CYCLE UP then DOWN IN CASE OF TRAINING ONLY: RESET “LANDING GEAR PUMP” circuit breaker EMERGENCY DESCENT

NOTE A malfunction of the oxygen system requires an immediate descent to an altitude at or below 12.500 ft.

NOTE Time of useful consciousness at 20,000ft is approximately 10 minutes

A malfunction of the oxygen system requires an immediate descent to an altitude at or below 12.500 ft. Throttle CLOSED Propeller Control FULL INCREASE Mixture AS REQUIRED to maintain smooth operation Landing Gear DOWN (103 KIAS maximum) SPIN RECOVERY Rudder FULL OPPOSITE to DIRECTION of ROTATION Control Wheel FULL FORWARD while NEUTRALIZING AILERONS Throttle IDLE Rudder (when rotation stops) NEUTRAL Control Wheel AS REQUIRED to smoothly regain level flight attitude OPEN DOOR If both upper and side latches are open, the door will trail slightly open and airspeeds will be reduced slightly To close door in flight: Speed SLOW to 87 KIAS Cabin vents CLOSE Storm window OPEN If upper latch is open LATCH If side latch is open PULL on armrest while moving latch handle to latched position If both latches are open Latch side latch Then top latch