Piper PA-28R-201 Arrow — Normal Operating Procedures (independently worded)

Preflight Walk-Around preflight_inspection

Aircraft documents (ARROW)ON BOARD AND CURRENT
Fuel quantity — visually inspect both tanks; verify adequate fuel for flight with legal reservesCONFIRMED, ADEQUATE
Fuel grade and appearance — sample from all sump drainsCORRECT GRADE PER POH; CLEAR, NO WATER OR SEDIMENT
Fuel filler caps — both tanksPROPERLY SEATED AND SECURED AFTER SAMPLING
Fuel vent linesUNOBSTRUCTED
Engine oil levelWITHIN OPERATING RANGE PER POH; DIPSTICK SECURE
Engine compartment — fuel lines, oil hoses, wiringNO LEAKS; ALL CONNECTIONS SECURE
Induction air inletCLEAR AND UNOBSTRUCTED
IO-360 is fuel-injected — no carburetor heat. Alternate air control bypasses the induction filter.
Exhaust stacks — visible portionsNO CRACKS OR LOOSE HARDWARE
Cowling latchesCLOSED AND SECURE
Propeller blades — nicks, cracks, erosionSERVICEABLE
Spinner and prop hubSECURE; NO CRACKS
Nose gear — strut, tire, and steering linkageSTRUT EXTENDED NORMALLY; TIRE INFLATED; LINKAGE INTACT; GEAR DOOR CLEAR
Pitot tube — cover removed, inlet unobstructedCOVER OFF; CLEAR
Static portsCLEAR
Left main gear — strut, tire, brake, gear door, hydraulic linesSTRUT NORMAL; TIRE INFLATED; BRAKE PAD VISIBLE; HYDRAULIC LINES UNDAMAGED; UPLOCK MECHANISM CLEAR
Left wing leading edge and fuel ventNO DEFORMATION OR FUEL STAINING; VENT CLEAR
Left aileron and flap — travel and attachmentHINGES SECURE; FULL FREE MOVEMENT; NO DAMAGE
Left wingtip and navigation lightUNDAMAGED; LENS INTACT
Stall warning vane — left wing leading edgeMOVES FREELY; ACTIVATES TONE WHEN LIFTED
Horizontal stabilizer, elevator, and trim tabUNDAMAGED; HINGES SECURE; NO EXCESSIVE PLAY
Vertical stabilizer and rudderUNDAMAGED; FULL FREE MOVEMENT
ELT — armed switch and antennaARMED; ANTENNA CONNECTED
Right main gear — strut, tire, brake, gear door, hydraulic linesSTRUT NORMAL; TIRE INFLATED; BRAKE PAD VISIBLE; HYDRAULIC LINES UNDAMAGED; UPLOCK MECHANISM CLEAR
Right wing — aileron, flap, wingtip, and navigation lightSECURE; FULL FREE MOVEMENT; UNDAMAGED; LENS INTACT
All tiedowns, chocks, and control locksREMOVED

Cockpit Preparation / Before Start before_start

POH and weight-and-balance dataON BOARD
Seats — adjusted and locked; seatbelts and shoulder harnesses for all occupantsADJUSTED, LOCKED, AND FASTENED
Rudder pedalsADJUSTED FOR FULL RUDDER AND BRAKE TRAVEL
Control lockREMOVED; AILERON, ELEVATOR, AND RUDDER FREE AND CORRECT
Trim — elevatorSET TO TAKEOFF POSITION PER POH
Avionics master switchOFF — before start to protect avionics from start transient
All non-essential electrical switchesOFF
Circuit breakersALL IN; CHECK FOR ANY TRIPPED
Fuel selectorFULLEST TANK — DETENT CONFIRMED ENGAGED
MixtureRICH — FULL FORWARD
Propeller controlFULL FORWARD — HIGH RPM
ThrottleCRACKED PER POH STARTING GUIDANCE
Primer — use as required for engine temperaturePUMPED PER POH; LOCKED AFTER USE
Gear handle positionDOWN — GEAR-DOWN INDICATOR LIGHTS CONFIRMED
Parking brakeSET

Engine Start engine_start

Area around aircraft — announce CLEAR PROPCLEAR
Master switch (battery)ON
Beacon / anti-collision lightON — before cranking
Throttle — set per POH for start conditionSET
Ignition switchSTART — crank until engine fires; release immediately
Throttle — after startREDUCE TO IDLE RPM PER POH
Oil pressureRISING WITHIN 30 SECONDS — if not, shut down immediately
Avionics masterON — after engine stabilized at idle
Engine instrumentsALL IN GREEN; OIL TEMPERATURE RISING NORMALLY
Alternator / ammeterCHARGING — positive indication confirmed

After Start after_start

ATIS / weather informationOBTAINED; ALTIMETER SETTING NOTED
AltimeterSET TO CURRENT ALTIMETER SETTING; FIELD ELEVATION CROSS-CHECKED
Radios and navigation — departure frequenciesLOADED AND SET
TransponderCODE SET; MODE SELECTED PER ATC REQUIREMENTS
Heading indicatorALIGNED WITH MAGNETIC COMPASS ON KNOWN HEADING
Gyroscopic instruments — suction gaugeIN GREEN ARC
Gear indicator lightsTHREE GREEN — ALL GEAR DOWN-AND-LOCKED CONFIRMED

Run-Up / Before Takeoff before_takeoff

Parking brakeSET
Flight controls — free and correct for wind directionVERIFIED
Fuel selectorFULLEST TANK — DETENT CONFIRMED
Mixture — adjust for field elevationSET PER POH
Propeller controlFULL FORWARD
Engine warm-up — oil temperatureIN GREEN ARC BEFORE RUN-UP
Throttle — advance to run-up RPM per POHSET
Magneto check — LEFT, then RIGHT, return to BOTHDROP ON EACH MAG WITHIN LIMITS PER POH; BOTH DROPS WITHIN DIFFERENTIAL LIMIT
Maximum single-magneto drop and maximum differential between magnetos per POH. Return selector to BOTH after check.
Propeller cycle — move slowly to low RPM; note drop; advance back to full forwardRPM DROP OBSERVED; RPM RETURNED TO FULL HIGH; REPEAT 2–3 TIMES; FINAL POSITION FULL FORWARD
Cycling warms governor oil and confirms constant-speed mechanism responds. Do not slam the control forward — cycle smoothly.
Throttle — return to idle; confirm smooth idleIDLE SMOOTH; RPM WITHIN LIMITS
Suction gaugeIN GREEN ARC
Engine instrumentsALL IN GREEN; NO ANOMALIES
Heading indicator — aligned with compassSET
AltimeterSET TO CURRENT ALTIMETER SETTING
FlapsSET TO TAKEOFF POSITION PER POH
Doors and windowsLATCHED AND SECURED
TransponderALT MODE
Takeoff briefing — abort criteria, initial climb airspeeds, departure routeREVIEWED

Takeoff takeoff

Runway clear — traffic and obstaclesCONFIRMED CLEAR
MixtureSET PER POH FOR FIELD ELEVATION
Propeller controlFULL FORWARD — HIGH RPM
Throttle — advance smoothly to full power; check engine instrumentsFULL POWER; INSTRUMENTS IN GREEN
Directional control during rollMAINTAINED WITH RUDDER
Rotate — at rotation airspeed per POHSMOOTH BACK PRESSURE APPLIED
Gear retraction — after positive rate of climb and no runway remaining for landingGEAR HANDLE UP; CONFIRM GEAR RETRACTS AND LIGHTS EXTINGUISH

Climb climb

Airspeed — establish best-rate or cruise-climb speedESTABLISHED PER POH
Engine instruments — oil pressure, oil temp, CHTWITHIN NORMAL RANGE
Power — throttle and RPMADJUSTED PER POH CLIMB POWER SCHEDULE
MixtureLEANED PER POH IF ABOVE DENSITY ALTITUDE THRESHOLD; RICH OTHERWISE
Fuel selectorAPPROPRIATE TANK; MONITOR BALANCE
Gear indicatorUP — NO GREEN LIGHTS; GEAR-UNSAFE HORN SILENT
FlapsRETRACTED PER POH SPEED SCHEDULE AFTER POSITIVE CLIMB ESTABLISHED
Heading and altitudeON ASSIGNED DEPARTURE CLEARANCE OR VFR COURSE

Cruise cruise

Power — throttle and propeller RPMSET TO CRUISE POWER PER POH
Set manifold pressure and RPM per POH power table for desired percent power and altitude.
Mixture — lean to peak EGT then enrich per POH cruise guidanceSET PER POH FOR SELECTED POWER SETTING
TrimADJUSTED FOR HANDS-OFF LEVEL FLIGHT
Engine instruments — oil pressure, oil temp, CHT, EGTALL WITHIN NORMAL RANGES; MONITORED CONTINUOUSLY
Fuel quantity — switch tanks per POH interval guidanceMONITORED; TANKS BALANCED
Gear indicator — confirm UPNO GREEN LIGHTS ILLUMINATED
Altimeter and heading indicator — cross-check compassSET AND TRACKING
Traffic and airspace — see-and-avoid; altitude and clearanceMAINTAINED

Descent descent

ATIS / destination weatherOBTAINED; RUNWAY AND APPROACH IN USE NOTED
Altimeter — update to destination settingSET TO CURRENT ALTIMETER SETTING
Fuel selector — switch to fullest or appropriate tank for approachSELECTED; DETENT ENGAGED
Mixture — gradually enrichen as altitude decreases; rich by pattern altitudeENRICHENING WITH DESCENT
Power — reduce gradually to avoid shock coolingREDUCED IN INCREMENTS PER POH
Heading indicator — cross-check and re-align with compass if neededALIGNED
Radios — approach and tower frequencies; ATC contact establishedSET AND ACTIVE

Before Landing before_landing

Fuel selector — fullest tank; detent confirmed engagedFULLEST TANK SELECTED
MixtureRICH — FULL FORWARD FOR GO-AROUND CAPABILITY
Propeller controlFULL FORWARD — HIGH RPM FOR GO-AROUND AVAILABILITY
Gear — place handle DOWN; confirm three green lights; gear-unsafe horn silentTHREE GREEN — NOSE, LEFT MAIN, RIGHT MAIN ALL DOWN-AND-LOCKED
Verbalize THREE GREEN to confirm positive indication. The gear-unsafe horn should be silent with throttle at approach power setting.
Flaps — extend to approach settingSET PER POH
Airspeed — stabilize at approach speedESTABLISHED PER POH
Seatbelts — all occupantsSECURED

Landing landing

Gear — final verification before crossing thresholdTHREE GREEN CONFIRMED
Approach — stable on glidepath, centerline, and airspeedSTABILIZED
Flaps — landing setting as requiredSET PER POH
Flare — initiate at appropriate height; reduce power smoothly to idleSMOOTH FLARE; POWER TO IDLE
Touchdown — main wheels first; nose lowered gently after speed decaysDIRECTIONAL CONTROL MAINTAINED WITH RUDDER
Braking — smooth and progressive; avoid wheel lockupAPPLIED AS NEEDED; AERODYNAMIC BRAKING USED DURING ROLLOUT

Go-Around go_around

ThrottleFULL POWER — advance smoothly and promptly
Pitch — establish positive climb attitude; arrest descentPOSITIVE CLIMB ATTITUDE ESTABLISHED
Flaps — retract to first notch or takeoff setting; full retraction in stages at safe airspeed per POHRETRACTING IN STAGES
Airspeed — accelerate to climb speed before further flap retractionCLIMBING AIRSPEED ESTABLISHED
Gear — UP after positive rate of climb established and no landing option remainsGEAR HANDLE UP; LIGHTS EXTINGUISHING
TrimADJUSTED TO REDUCE CONTROL FORCES DURING CLIMB
ATC — advise of go-around; comply with missed approach or traffic pattern instructionsADVISED

After Landing after_landing

Flaps — retract after clear of active runwayRETRACTED
TransponderSTBY OR GROUND MODE
Taxi speed — brakes tested gently; maintain awareness of gear-unsafe horn sensitivityCONTROLLED

Shutdown and Securing shutdown

Parking brakeSET
Mixture — idle cutoff to shut down engineIDLE CUTOFF — ENGINE STOPPED
Ignition switchOFF — after engine stops
Avionics masterOFF
All electrical switchesOFF
Master switchOFF
Fuel selectorLEFT OR RIGHT PER OPERATOR PRACTICE; AVOID LEAVING ON BOTH UNATTENDED
Flight controls — gust lock or control lockINSTALLED PER OPERATOR PRACTICE
Pitot cover and tiedownsCOVER INSTALLED; AIRCRAFT TIED DOWN AND CHOCKED IF OUTSIDE

Piper PA-28R-201 Arrow — Normal Operating Procedures (independently worded)

Ratings & reviews

Preflight Walk-Around preflight_inspection

Cockpit Preparation / Before Start before_start

Engine Start engine_start

After Start after_start

Run-Up / Before Takeoff before_takeoff

Takeoff takeoff

Climb climb

Cruise cruise

Descent descent

Before Landing before_landing

Landing landing

Go-Around go_around

After Landing after_landing

Shutdown and Securing shutdown

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