#	Beechcraft Bonanza V35B — Normal Operating Procedures
#	NOT FOR FLIGHT — source fidelity: not_applicable | operational review: none | completeness: normal_only | 1 unresolved safety defect(s)
#	Source: authored — no source document
#	Rights: original_expression CC-BY-4.0
#	Checklist hash: a38856325b9b5f84fbe37314288b84566422cff91b9720f75a17adde41d8e48b
#	Verify against the aircraft's own approved documentation before use.
section_id	phase	criticality	section_title	item_index	item_id	type	tickable	memory_item	indent	text	response	condition	detail
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	0		action	yes	no	0	Aircraft documents (ARROW)	ON BOARD AND CURRENT		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	1		action	yes	no	0	Weight and balance	COMPUTED AND WITHIN LIMITS		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	2		action	yes	no	0	Fuel quantity — visually confirm both tanks; compare with gauges	VERIFIED, ADEQUATE FOR FLIGHT WITH REQUIRED RESERVES		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	3		action	yes	no	0	Fuel grade and appearance	CORRECT GRADE PER POH; CLEAR, CORRECT COLOR, NO CONTAMINATION		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	4		action	yes	no	0	Fuel caps — both wing tanks	SECURELY SEATED AND LOCKED		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	5		action	yes	no	0	Fuel sump drains — both wing tanks and gascolator	SAMPLED; CLEAR, NO WATER OR SEDIMENT		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	6		action	yes	no	0	Oil level	CHECKED; WITHIN OPERATING RANGE PER POH		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	7		action	yes	no	0	Oil filler cap and dipstick	SECURED		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	8		action	yes	no	0	Engine cowling — upper and lower panels	LATCHED SECURELY, NO DAMAGE OR OIL STREAKS		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	9		action	yes	no	0	Air induction filter and inlet	CLEAR AND UNOBSTRUCTED		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	10		action	yes	no	0	Exhaust stacks	SECURE, NO CRACKS OR CARBON DEPOSITS INDICATING LEAK		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	11		action	yes	no	0	Propeller blades — both	NO NICKS, CRACKS, OR DAMAGE; SPINNER SECURE		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	12		action	yes	no	0	Nose gear strut extension and tire condition	PROPER EXTENSION, NO CUTS OR FLAT SPOTS, VALVE STEM INTACT		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	13		action	yes	no	0	Nose gear steering linkage and shimmy damper	VISIBLE, NO OBVIOUS DAMAGE OR LEAKS		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	14		action	yes	no	0	Right main gear strut, tire, and wheel fairing	STRUT PROPERLY EXTENDED, TIRE INFLATED AND SERVICEABLE		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	15		action	yes	no	0	Right wing leading edge and upper/lower surfaces	NO DAMAGE, DEFORMATION, OR CONTAMINATION		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	16		action	yes	no	0	Right wing tip and nav light	UNDAMAGED, LENS CLEAR		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	17		action	yes	no	0	Right aileron — travel, hinges, and pushrod	FREE, FULL TRAVEL, NO PLAY IN HINGES		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	18		action	yes	no	0	Right flap — hinges and surface condition	SECURE, NO DEFORMATION OR MISSING FASTENERS		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	19		action	yes	no	0	Static port — right side (if installed)	CLEAR AND UNOBSTRUCTED		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	20		action	yes	no	0	Fuselage and cabin area — windows, antennas	NO DAMAGE; ANTENNAS SECURE		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	21		action	yes	no	0	V-tail ruddervator surfaces — left and right	FREE MOVEMENT, SECURE HINGES, NO DAMAGE OR DEFORMATION		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	22		action	yes	no	0	V-tail ruddervator control rods and gust locks	CONTROL RODS ATTACHED; GUST LOCK REMOVED IF INSTALLED		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	23		action	yes	no	0	Left aileron and flap — travel and condition	FREE, FULL TRAVEL, SURFACES UNDAMAGED		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	24		action	yes	no	0	Left wing fuel cap and sump drain	CAP SECURED; SUMP SAMPLED, CLEAR		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	25		action	yes	no	0	Left main gear strut, tire, and brake assembly	STRUT PROPERLY EXTENDED, TIRE INFLATED, BRAKE LINES INTACT		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	26		action	yes	no	0	Pitot tube cover removed and tube clear	COVER REMOVED AND STOWED; TUBE CLEAR		
preflight-inspection	preflight_inspection	normal	Preflight Walk-Around	27		action	yes	no	0	Stall warning vane (if installed)	MOVES FREELY, UNOBSTRUCTED		
before-start	before_start	normal	Cockpit Preparation / Before Start	0		action	yes	no	0	Seats, seat belts, and shoulder harnesses	ADJUSTED AND LOCKED; OCCUPANTS BRIEFED		
before-start	before_start	normal	Cockpit Preparation / Before Start	1		action	yes	no	0	Rudder pedals	ADJUSTED FOR PILOT REACH		
before-start	before_start	normal	Cockpit Preparation / Before Start	2		action	yes	no	0	Flight controls — free and correct movement	FREE, FULL TRAVEL, CORRECT DIRECTION		
before-start	before_start	normal	Cockpit Preparation / Before Start	3		action	yes	no	0	Trim — elevator and rudder	SET FOR TAKEOFF PER POH		
before-start	before_start	normal	Cockpit Preparation / Before Start	4		action	yes	no	0	Fuel selector valve	FULLEST TANK OR BOTH PER POH		
before-start	before_start	normal	Cockpit Preparation / Before Start	5		action	yes	no	0	Mixture control	RICH (OR PER POH FOR FIELD ELEVATION)		
before-start	before_start	normal	Cockpit Preparation / Before Start	6		action	yes	no	0	Throttle	CLOSED; FRICTION SET		
before-start	before_start	normal	Cockpit Preparation / Before Start	7		action	yes	no	0	Propeller control	FULL FORWARD (HIGH RPM)		
before-start	before_start	normal	Cockpit Preparation / Before Start	8		action	yes	no	0	Parking brake	SET		
before-start	before_start	normal	Cockpit Preparation / Before Start	9		action	yes	no	0	Avionics master switch	OFF (BEFORE ENGINE START)		
before-start	before_start	normal	Cockpit Preparation / Before Start	10		action	yes	no	0	All electrical switches — lighting, pitot heat, etc.	OFF		
before-start	before_start	normal	Cockpit Preparation / Before Start	11		action	yes	no	0	Master switch (battery)	ON		
before-start	before_start	normal	Cockpit Preparation / Before Start	12		action	yes	no	0	Fuel quantity gauges	CHECKED AGAINST VISUAL INSPECTION; CONSISTENT		
before-start	before_start	normal	Cockpit Preparation / Before Start	13		action	yes	no	0	Gear selector and position indicator	GEAR DOWN INDICATED; THREE GREEN (IF POWER AVAILABLE)		
before-start	before_start	normal	Cockpit Preparation / Before Start	14		action	yes	no	0	Flaps	SET FOR TAKEOFF PER POH		
before-start	before_start	normal	Cockpit Preparation / Before Start	15		action	yes	no	0	Gyroscopic instruments — suction gauge or electric indicators	CHECKED, WITHIN LIMITS		
engine-start	engine_start	normal	Engine Start	0		caution	no	no	0	The IO-520 is fuel-injected; normal start uses no carburetor heat. Hot starts require a specific lean-mixture technique — refer to POH.			
engine-start	engine_start	normal	Engine Start	1		action	yes	no	0	Area clear of personnel and obstructions	CHECKED; CALL CLEAR		
engine-start	engine_start	normal	Engine Start	2		action	yes	no	0	Throttle	OPEN APPROXIMATELY PER POH FOR START		
engine-start	engine_start	normal	Engine Start	3		action	yes	no	0	Mixture — cold start fuel prime via mixture or primer per POH	PRIMED PER POH PROCEDURE		
engine-start	engine_start	normal	Engine Start	4		action	yes	no	0	Mixture control — after prime	IDLE CUTOFF (COLD START) OR RICH (HOT START PER POH)		
engine-start	engine_start	normal	Engine Start	5		action	yes	no	0	Ignition switch	START		
engine-start	engine_start	normal	Engine Start	6		action	yes	no	0	Mixture — advance to rich as engine fires	ADVANCED TO RICH; ENGINE RUNNING SMOOTHLY		
engine-start	engine_start	normal	Engine Start	7		action	yes	no	0	Throttle — reduce to idle RPM after start	IDLE PER POH; ENGINE STABLE		
engine-start	engine_start	normal	Engine Start	8		action	yes	no	0	Oil pressure	RISING WITHIN LIMITS; CHECK WITHIN TIME LIMIT PER POH		
engine-start	engine_start	normal	Engine Start	9		action	yes	no	0	Avionics master switch	ON		
engine-start	engine_start	normal	Engine Start	10		action	yes	no	0	Engine instruments — oil temp, oil pressure, fuel flow	MONITORING; ALL IN RANGE FOR IDLE		
engine-start	engine_start	normal	Engine Start	11		action	yes	no	0	Alternator output — ammeter or loadmeter	CHARGING INDICATED		
after-start	after_start	normal	Before Taxi / After Start	0		action	yes	no	0	Brakes	TESTED; FIRM PEDAL PRESSURE, BOTH SIDES EQUAL		
after-start	after_start	normal	Before Taxi / After Start	1		action	yes	no	0	Taxi lights	ON AS REQUIRED		
after-start	after_start	normal	Before Taxi / After Start	2		action	yes	no	0	ATIS or weather information	OBTAINED AND NOTED		
after-start	after_start	normal	Before Taxi / After Start	3		action	yes	no	0	Altimeter	SET TO CURRENT ALTIMETER SETTING; FIELD ELEVATION CONFIRMED		
after-start	after_start	normal	Before Taxi / After Start	4		action	yes	no	0	Heading indicator / directional gyro	ALIGNED WITH MAGNETIC COMPASS		
after-start	after_start	normal	Before Taxi / After Start	5		action	yes	no	0	Engine warm-up — oil temperature reaching operating range	OIL TEMPERATURE APPROACHING GREEN ARC BEFORE FULL POWER		
after-start	after_start	normal	Before Taxi / After Start	6		action	yes	no	0	Clearance — ASOS/ATIS code, departure, transponder code	RECEIVED AND READBACK CORRECT		
after-start	after_start	normal	Before Taxi / After Start	7		action	yes	no	0	Transponder	ALT MODE; CODE SET		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	0		action	yes	no	0	Parking brake	SET		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	1		action	yes	no	0	Flight controls — final check, free and correct	FREE, FULL TRAVEL, CORRECT DIRECTION		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	2		action	yes	no	0	Elevator trim	SET FOR TAKEOFF PER POH		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	3		action	yes	no	0	Fuel selector valve	FULLEST TANK OR CORRECT TANK PER POH		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	4		action	yes	no	0	Mixture	RICH (OR ADJUSTED FOR FIELD ELEVATION PER POH)		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	5		action	yes	no	0	Throttle — advance to run-up power per POH	RUN-UP POWER SET PER POH		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	6		action	yes	no	0	Magneto check — both, left, right, back to both	DROP WITHIN LIMITS PER POH; NO EXCESSIVE ROUGHNESS		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	7		action	yes	no	0	Propeller cycle — full forward, reduce RPM, observe drop, advance back to full forward	RPM DROP NOTED; OIL PRESSURE STABLE; PROP RETURNED FULL FORWARD		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	8		action	yes	no	0	Engine instruments at run-up power	OIL TEMP AND PRESSURE IN GREEN; FUEL FLOW NORMAL		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	9		action	yes	no	0	Throttle — reduce to idle and check idle RPM	IDLE STABLE PER POH; NO ROUGHNESS		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	10		action	yes	no	0	Throttle friction	SET TO PREVENT CREEP		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	11		action	yes	no	0	Gyroscopic instruments — attitude indicator erect, heading indicator set	ATTITUDE INDICATOR STABLE; HEADING ALIGNED		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	12		action	yes	no	0	Flaps	SET FOR TAKEOFF PER POH		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	13		action	yes	no	0	Gear — position indicator and manual override	DOWN AND LOCKED — THREE GREEN; OVERRIDE HANDLE STOWED		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	14		action	yes	no	0	Landing light and strobes	ON		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	15		action	yes	no	0	Doors and windows	CLOSED AND LATCHED		
before-takeoff	before_takeoff	normal	Run-Up / Before Takeoff	16		action	yes	no	0	Departure briefing — engine failure plan, abort point	BRIEFED		
takeoff	takeoff	normal	Takeoff	0		action	yes	no	0	Runway heading — align and hold brakes	ALIGNED; INSTRUMENTS CROSS-CHECKED FOR HEADING		
takeoff	takeoff	normal	Takeoff	1		action	yes	no	0	Throttle — advance smoothly to full power	FULL POWER; INSTRUMENTS CHECKED — OIL PRESSURE, FUEL FLOW, RPM NORMAL		
takeoff	takeoff	normal	Takeoff	2		action	yes	no	0	Directional control during roll — rudder as needed	TRACKING CENTERLINE		
takeoff	takeoff	normal	Takeoff	3		note	no	no	0	The IO-520 is a direct-drive engine; torque and P-factor require right rudder during takeoff roll.			
takeoff	takeoff	normal	Takeoff	4		action	yes	no	0	Rotate at Vr per POH	SMOOTH ROTATION; POSITIVE RATE OF CLIMB ESTABLISHED		
takeoff	takeoff	normal	Takeoff	5		action	yes	no	0	Gear — retract after positive climb rate confirmed	GEAR UP; GEAR-IN-TRANSIT LIGHT EXTINGUISHES; GEAR UNSAFE LIGHT OUT		
takeoff	takeoff	normal	Takeoff	6		action	yes	no	0	Climb attitude and airspeed — Vy per POH	PITCH ATTITUDE SET; AIRSPEED CONFIRMED AT Vy		
takeoff	takeoff	normal	Takeoff	7		action	yes	no	0	Flaps — retract per POH schedule	FLAPS RETRACTED; AIRSPEED IN NORMAL RANGE		
climb	climb	normal	Climb	0		action	yes	no	0	Airspeed — establish Vy or cruise climb speed per POH	AIRSPEED CONFIRMED		
climb	climb	normal	Climb	1		action	yes	no	0	Power — set climb power per POH (manifold pressure and RPM)	POWER SET PER POH		
climb	climb	normal	Climb	2		action	yes	no	0	Propeller — set climb RPM per POH	PROP SET		
climb	climb	normal	Climb	3		action	yes	no	0	Mixture — enrich or lean per altitude and POH guidance	MIXTURE ADJUSTED PER POH FOR ALTITUDE		
climb	climb	normal	Climb	4		action	yes	no	0	Engine instruments — oil temp, oil pressure, CHT, fuel flow	ALL IN GREEN; CHT RISING BUT WITHIN LIMITS		
climb	climb	normal	Climb	5		action	yes	no	0	Fuel selector — verify correct tank selected	CORRECT TANK SELECTED		
climb	climb	normal	Climb	6		action	yes	no	0	Altimeter and transponder	ALTIMETER SET; TRANSPONDER IN ALT MODE		
climb	climb	normal	Climb	7		action	yes	no	0	Landing gear position indicator	THREE GREEN LIGHTS OUT (GEAR UP CONFIRMED) OR INDICATOR SHOWS RETRACTED		
cruise	cruise	normal	Cruise	0		action	yes	no	0	Power — set cruise power per POH for altitude and desired performance	MANIFOLD PRESSURE AND RPM SET PER POH		
cruise	cruise	normal	Cruise	1		action	yes	no	0	Propeller — set cruise RPM per POH	PROP SET		
cruise	cruise	normal	Cruise	2		action	yes	no	0	Mixture — lean for altitude and power setting per POH EGT procedure	MIXTURE LEANED PER POH; EGT NOTED		
cruise	cruise	normal	Cruise	3		action	yes	no	0	Fuel selector — select tank per POH fuel management schedule	CORRECT TANK; FUEL REMAINING NOTED		
cruise	cruise	normal	Cruise	4		action	yes	no	0	Fuel quantity — check both tanks against time flown	FUEL BURN CONSISTENT WITH POH ESTIMATE		
cruise	cruise	normal	Cruise	5		action	yes	no	0	Engine instruments — oil temp, CHT, oil pressure, fuel flow	ALL WITHIN NORMAL RANGE		
cruise	cruise	normal	Cruise	6		action	yes	no	0	Altimeter — reset to current setting	ALTIMETER RESET; ALTITUDE CONFIRMED		
cruise	cruise	normal	Cruise	7		action	yes	no	0	Trim — pitch and rudder adjusted for cruise	AIRCRAFT IN TRIM; CONTROL PRESSURES ZERO		
descent	descent	normal	Descent	0		action	yes	no	0	ATIS or current weather at destination	OBTAINED; RUNWAY IN USE AND WINDS NOTED		
descent	descent	normal	Descent	1		action	yes	no	0	Altimeter — reset to destination or current station altimeter setting	ALTIMETER SET		
descent	descent	normal	Descent	2		action	yes	no	0	Mixture — enrichen progressively as altitude decreases per POH	MIXTURE ADJUSTED FOR ALTITUDE AND POWER		
descent	descent	normal	Descent	3		action	yes	no	0	Power — reduce for descent; monitor CHT for shock cooling	POWER REDUCED GRADUALLY PER POH; CHT WITHIN LIMITS		
descent	descent	normal	Descent	4		caution	no	no	0	Rapid power reduction with cold OAT can cause cylinder shock cooling on the IO-520. Reduce throttle gradually and monitor CHT throughout descent.			
descent	descent	normal	Descent	5		action	yes	no	0	Fuel selector — switch to fullest tank or per POH approach fuel plan	CORRECT TANK SELECTED; QUANTITY ADEQUATE		
descent	descent	normal	Descent	6		action	yes	no	0	Cabin heat and defrost — adjust as needed for visibility	SET AS REQUIRED		
before-landing	before_landing	normal	Before Landing	0		action	yes	no	0	Fuel selector valve	FULLEST TANK OR BOTH PER POH		
before-landing	before_landing	normal	Before Landing	1		action	yes	no	0	Mixture	RICH		
before-landing	before_landing	normal	Before Landing	2		action	yes	no	0	Propeller	FULL FORWARD (HIGH RPM) — READY FOR GO-AROUND POWER		
before-landing	before_landing	normal	Before Landing	3		action	yes	no	0	Landing gear — select DOWN on downwind abeam touchdown point	GEAR DOWN SELECTED		
before-landing	before_landing	normal	Before Landing	4		action	yes	no	0	Gear position indicator — confirm three green	THREE GREEN — GEAR DOWN AND LOCKED		
before-landing	before_landing	normal	Before Landing	5		action	yes	no	0	Gear-unsafe light	EXTINGUISHED		
before-landing	before_landing	normal	Before Landing	6		action	yes	no	0	Flaps — extend per POH for pattern position and speed	FLAPS EXTENDED PER POH; AIRSPEED WITHIN FLAP LIMIT		
before-landing	before_landing	normal	Before Landing	7		action	yes	no	0	Airspeed — establish approach speed per POH	APPROACH SPEED CONFIRMED PER POH		
before-landing	before_landing	normal	Before Landing	8		action	yes	no	0	Seat belts and shoulder harnesses	FASTENED AND SNUG		
before-landing	before_landing	normal	Before Landing	9		action	yes	no	0	Landing light	ON		
gear-check	Gear Check	normal	Gear Check — Final Approach	0		warning	no	no	0	GEAR CHECK IS MANDATORY ON EVERY APPROACH. A gear-up landing will cause serious aircraft damage.			
gear-check	Gear Check	normal	Gear Check — Final Approach	1		action	yes	no	0	Landing gear selector — confirm in DOWN position	SELECTOR DOWN		
gear-check	Gear Check	normal	Gear Check — Final Approach	2		action	yes	no	0	Gear position indicator — three green lights	THREE GREEN LIGHTS ILLUMINATED		
gear-check	Gear Check	normal	Gear Check — Final Approach	3		action	yes	no	0	Gear-unsafe light	EXTINGUISHED		
gear-check	Gear Check	normal	Gear Check — Final Approach	4		action	yes	no	0	Gear horn — if equipped, verify no horn with gear extended at low power	NO HORN WITH GEAR DOWN		
landing	landing	normal	Landing	0		action	yes	no	0	Airspeed — maintain Vref or approach speed per POH on final	AIRSPEED STABILIZED PER POH		
landing	landing	normal	Landing	1		action	yes	no	0	Wind correction applied	CRAB OR SLIP AS APPROPRIATE		
landing	landing	normal	Landing	2		note	no	no	0	The V-tail ruddervators provide less crosswind control authority than a conventional tail. Plan landing technique accordingly; consult POH crosswind limits.			
landing	landing	normal	Landing	3		action	yes	no	0	Threshold crossing — begin flare at appropriate height	FLARE INITIATED; THROTTLE RETARDING TO IDLE		
landing	landing	normal	Landing	4		action	yes	no	0	Touchdown — main gear first for normal landing	SMOOTH TOUCHDOWN ON MAINS; NOSE HELD OFF BRIEFLY		
landing	landing	normal	Landing	5		action	yes	no	0	Directional control after touchdown — rudder pedals	TRACKING CENTERLINE; NOSE LOWERED SMOOTHLY		
landing	landing	normal	Landing	6		action	yes	no	0	Brakes — apply smoothly after nose gear is on ground	BRAKES APPLIED AS NEEDED; NO SKIDDING		
landing	landing	normal	Landing	7		action	yes	no	0	Flaps	RETRACT AFTER CLEAR OF RUNWAY (OPTIONAL DURING ROLLOUT FOR BRAKING EFFICIENCY PER POH)		
go-around	go_around	normal	Go-Around	0		action	yes	no	0	Throttle — advance to full power immediately	FULL POWER; CONFIRM ENGINE RESPONDING		
go-around	go_around	normal	Go-Around	1		action	yes	no	0	Propeller — confirm full forward if not already	FULL FORWARD		
go-around	go_around	normal	Go-Around	2		action	yes	no	0	Mixture	RICH		
go-around	go_around	normal	Go-Around	3		action	yes	no	0	Pitch — establish positive climb attitude	PITCH ATTITUDE INCREASING; POSITIVE RATE OF CLIMB		
go-around	go_around	normal	Go-Around	4		action	yes	no	0	Flaps — retract incrementally per POH; do not retract all at once at low speed	FLAPS RETRACTING PER POH; AIRSPEED INCREASING		
go-around	go_around	normal	Go-Around	5		action	yes	no	0	Landing gear — retract after positive rate of climb confirmed	GEAR UP; THREE GREEN OUT		
go-around	go_around	normal	Go-Around	6		action	yes	no	0	Airspeed — accelerate to Vy or climb speed per POH	AIRSPEED AT Vy PER POH		
go-around	go_around	normal	Go-Around	7		action	yes	no	0	ATC — advise of go-around	ATC NOTIFIED		
after-landing	after_landing	normal	After Landing	0		action	yes	no	0	Flaps — retract after runway is clear	FLAPS UP		
after-landing	after_landing	normal	After Landing	1		action	yes	no	0	Landing light	OFF OR AS APPROPRIATE FOR TAXI		
after-landing	after_landing	normal	After Landing	2		action	yes	no	0	Strobes	OFF AFTER CLEARING ACTIVE RUNWAY		
after-landing	after_landing	normal	After Landing	3		action	yes	no	0	Transponder	STDBY OR GROUND MODE		
after-landing	after_landing	normal	After Landing	4		action	yes	no	0	Mixture — lean for taxi if field elevation requires	LEANED PER POH FOR GROUND OPERATION		
shutdown	shutdown	normal	Shutdown and Securing	0		action	yes	no	0	Parking brake	SET		
shutdown	shutdown	normal	Shutdown and Securing	1		action	yes	no	0	Throttle — idle for engine cool-down per POH before shutdown	IDLING AT SPECIFIED TIME PER POH		
shutdown	shutdown	normal	Shutdown and Securing	2		action	yes	no	0	Avionics master switch	OFF		
shutdown	shutdown	normal	Shutdown and Securing	3		action	yes	no	0	Electrical loads — all non-essential switches	OFF		
shutdown	shutdown	normal	Shutdown and Securing	4		action	yes	no	0	Mixture — pull to idle cutoff; engine stops	IDLE CUTOFF; ENGINE STOPS CLEANLY		
shutdown	shutdown	normal	Shutdown and Securing	5		action	yes	no	0	Ignition switch	OFF AFTER ENGINE STOPS		
shutdown	shutdown	normal	Shutdown and Securing	6		action	yes	no	0	Master switch	OFF		
shutdown	shutdown	normal	Shutdown and Securing	7		action	yes	no	0	Fuel selector valve	OFF (IF PLACARDED; OTHERWISE PER POH)		
shutdown	shutdown	normal	Shutdown and Securing	8		action	yes	no	0	Control lock / gust lock	INSTALLED TO PROTECT RUDDERVATOR SURFACES		
shutdown	shutdown	normal	Shutdown and Securing	9		action	yes	no	0	Wheel chocks	INSTALLED		
shutdown	shutdown	normal	Shutdown and Securing	10		action	yes	no	0	Pitot tube cover	INSTALLED		
shutdown	shutdown	normal	Shutdown and Securing	11		action	yes	no	0	Aircraft secured — tie-downs and cover as appropriate	SECURED PER LOCAL CONDITIONS		
shutdown	shutdown	normal	Shutdown and Securing	12		action	yes	no	0	Flight log and Hobbs/tach time recorded	RECORDED