MSFS 2024 · Fighter

F/A-18E Super Hornet Startup Checklist

F/A-18E Super Hornet Startup Notes

The Rhino follows the same family logic as the legacy Hornet: battery on, APU on, crank the right engine first, then use crossbleed air to start the left. In MSFS the systems depth is far shallower than a study-level module - there is no full INS alignment to babysit and many switches are simplified - but flying the real flow still pays off, because the jet comes alive in the correct order and the habits transfer straight to the DCS Hornet.

The biggest mistake is leaning on auto-start (Ctrl+E) forever and never learning the flow - the Super Hornet is one of the easiest jets to start manually. Beyond that, pilots skip the APU step and wonder why nothing cranks, take off with the wrong flap setting (HALF is standard for the Hornet family), and forget takeoff trim. Run the console flow deliberately, watch the crank switch sequence, and set flaps and trim before the runway.

Common mistakes

Relying on Ctrl+E instead of learning the flow
Taking off with the wrong flap setting
Cranking engines before the APU is running

Related Aircraft

F/A-18C Hornet

DCS World checklist

Pilot Tools for This Flight

METAR DecoderDecode field weather Crosswind CalculatorRunway wind components Unit ConverterAll aviation units

U.S. Navy / Wikimedia CommonsPublic Domain

Fighter4th Gen

AIRCRAFT BRIEF

The Boeing F/A-18E Super Hornet is an enlarged, redesigned evolution of the classic Hornet that first flew on November 29, 1995 and entered U.S. Navy fleet service in 1999. It features a 20% larger airframe, 33% more internal fuel, and twin F414-GE-400 engines producing 35% more thrust than the F404 engines of the classic Hornet, dramatically improving range, payload, and carrier bringback capability. The Super Hornet replaced the F-14 Tomcat and A-6 Intruder and remains the backbone of carrier air wings today.

RANGE VISUALIZER

Startup Walkthrough

SPECIFICATIONS

manufacturer: Boeing (formerly McDonnell Douglas)
first Flight: 1995
role: Carrier-based multirole strike fighter
crew: 1 pilot
engines: 2x GE F414-GE-400 (22,000 lbf each with AB)
max Speed: 1,915 km/h (Mach 1.8)
range: 2,346 km (1,267 nmi) combat radius
ceiling: 50,000+ ft
weight: 29,937 kg (MTOW)

SOURCES

FLIGHT2.8.0Checklist

F/A-18E Super HornetMSFS 2024 · Startup Checklist · 225 steps · 15 phases

DATE PILOT TAIL

PHS 1 — Pre-Flight Planning10 steps

	01	Mission Planning / Fuel PlanningCOMPLETENOTE: NATOPS 6.1.1: planned minimum on deck fuel should not be less than 1,800 lb. Refer to A1-F18EA-NFM-200 Performance Data or approved fuel planning software for consumption and profile.
	02	NATOPS Admin Briefing GuideBRIEFEDNOTE: NATOPS 6.2.1.1 covers times, callsigns, loadout gross weight, max trap, comm plan, waypoint plan, takeoff data and recovery.
	03	Weather and NOTAMsREVIEWED
	04	Joker / Bingo / Fuel LadderSET
	05	Gross WeightWITHIN LIMITSNOTE: NATOPS figure 4-4: 66,000 lb field takeoff and in flight, 50,600 lb field landing / FCLP / touch-and-go, 66,000 lb catapult, 44,000 lb carrier landing.
	06	Lateral Weight AsymmetryWITHIN LIMITSNOTE: NATOPS figure 4-4: 29,000 ft-lb field takeoff and in flight, 33,000 ft-lb field landing, 30,800 ft-lb carrier landing.
	07	Center of Gravity16.8 TO 31.8 PERCENT MAC
	08	Takeoff DataCOMPUTEDNOTE: NATOPS 7.5.2: compute nosewheel liftoff speed, takeoff speed, takeoff distance and abort speed for the configuration and expected ambient conditions.
	09	A-Sheet / Aircraft Discrepancy BookREVIEWEDNOTE: NATOPS 7.1.1: check aircraft status, configuration, armament loading and servicing before manning the aircraft.
	10	Divert / Recovery PlanBRIEFED

PHS 2 — Preflight Checks15 steps

	01	Exterior inspectionCOMPLETENOTE: NATOPS 7.1.3: the exterior inspection is divided into 20 areas.
	02	All doors forward of the intakesSECURED
	03	Boarding ladderSECURE (2 POINTS)
	04	Spoilers and upper blade antennaCHECK CONDITION
	05	ECS auxiliary duct doorsCHECK DOWN/CONDITION
	06	Maintenance handleCHECK STOWED
	07	EMI shields (covers over bay behind ejection seat)CLOSED/SECUREDCAUTION: Ensure the EMI shields are properly closed and secured prior to closing the canopy to prevent damage to the shields and the canopy actuation link.
	08	Ejection seat SAFE/ARMED handleSAFE
	09	Ejection seat manual override handleFULL DOWN AND LOCKED
	10	Top latch plunger locking indicatorFLUSH WITH END OF PLUNGERCAUTION: If the top latch plunger locking indicator is not flush, the seat could come loose on the mounting rails.
	11	Electronic sequencer and thermal batteriesNOT ACTIVATEDNOTE: Sequencer indicator should be BLACK. Thermal battery indicator should be WHITE or PINK. Black or purple is unsatisfactory.
	12	Emergency oxygen gaugeIN THE BLACK
	13	Leg restraint linesCHECK ROUTINGWARNING: Failure to route the restraint lines properly through the garters could cause serious injury during ejection or emergency egress.
	14	Lap beltsSECURE
	15	Parachute risers and SEAWARSCHECK

PHS 3 — Interior Checks - Pilot53 steps

	01	Leads, leg restraints and harnessSECURE/ADJUSTWARNING: The leg restraint lines must be buckled at all times during flight to ensure that the legs will be pulled back upon ejection.
	02	Ejection control handleCLEAR
	03	Ejection control handle pinVERIFY REMOVED
	04	Circuit breakers (left and right consoles)IN
	05	Manual canopy handleSTOWED
	06	MC and HYD ISOL switchesNORM
	07	OBOGS control switchOFF
	08	OXY FLOW knobOFF
	09	COMM 1 / IFF ANT SEL switchesAUTO/BOTH
	10	COMM panelSETNOTE: RLY and GXMT switches OFF. ILS CHANNEL/ILS switch SET/UFCD. CRYPTO, MODE 4 and IFF MASTER switches NORM/OFF/NORM.
	11	FCS GAIN switchNORM/GUARD DOWN
	12	APU switchOFF
	13	PROBE switchRETRACT
	14	EXT TANKS switchesNORM
	15	DUMP switchOFF
	16	INTR WING switchNORM
	17	GEN TIE CONTROL switchNORM/GUARD DOWN
	18	EXT LT panelSET
	19	ThrottlesOFF
	20	BRK PRESS switchCHECK (2,600 PSI MINIMUM)
	21	PARK BRK handleSET
	22	LDG/TAXI LIGHT switchOFF
	23	ANTI SKID switchON
	24	SELECT JETT knobSAFE
	25	FLAP switchFULL
	26	LAUNCH BAR switchRETRACT
	27	LDG GEAR handleDN
	28	Landing gear handle mechanical stopFULLY ENGAGED
	29	CANOPY JETT handleFORWARD
	30	MASTER ARM switchSAFE
	31	EMERG JETT buttonNOT PRESSED IN
	32	FIRE and APU FIRE warning lightsNOT PRESSED INNOTE: If a FIRE light is depressed, approximately 1/8 inch of yellow and black stripes will be visible around the outer edges of the light.
	33	L(R) DDI, HUD and MPCD knobsOFF
	34	COMM 1 and 2 knobsOFF
	35	CVRS mode switchOFF
	36	ALT switchBARO OR RDR
	37	ATT switchAUTO
	38	Standby attitude reference indicatorCAGED
	39	IR COOL switchOFF
	40	SPIN switchNORM/GUARD DOWN
	41	HOOK handleUP
	42	WINGFOLD switchSAME AS WING POSITION
	43	AV COOL switchNORM
	44	ECM JETT button and JAMMER / RWR / DISPENSER switchesNOT PUSHED IN / OFF
	45	AUX REL switchNORM
	46	RUD PED ADJ leverSET AS DESIRED FOR FLIGHTCAUTION: Ensure the rudder pedals are locked in position after adjustment. Failure to lock the rudder pedals may result in uncommanded forward rudder pedal movement inflight.
	47	GEN switchesNORM
	48	BATT switchOFF
	49	ECS panelSETWARNING: Selection of MAN with the ECS mode switch is prohibited. Selecting MAN while the aft cooling fan shutoff valve is open may cause the fan to overspeed.NOTE: MODE switch AUTO, CABIN TEMP as desired, CABIN PRESS NORM, BLEED AIR knob OFF, ENG ANTI ICE OFF, PITOT ANTI ICE AUTO.
	50	DEFOG handleMID RANGE
	51	WINDSHIELD switchOFF
	52	INTR LT panelSET
	53	Sensor control panelSETNOTE: FLIR, LTD/R and LST/NFLR switches OFF/SAFE/OFF. INS and RADAR knobs OFF.

PHS 4 — Engine Start21 steps

	01	BATT switchONNOTE: A self-contained battery/APU start is the primary method for starting the engines.
	02	Battery gaugeCHECKNOTE: Nominal voltage for a good battery is 23 to 24 vdc. EFD blanking and/or uncommanded APU shutdown should be anticipated at or below approximately 18 vdc.
	03	Caution lights panelCHECK
	04	ICSCHECK
	05	FIRE warning testPERFORMNOTE: FIRE test switch TEST A until all lights and aural warnings pass, NORM for at least 7 seconds, then TEST B. Failure to pause in NORM for at least 3 seconds results in a false BALD failure MSP code.
	06	Forward MPCD and UFCD knobsON
	07	APU ACC caution lightVERIFY OFF
	08	APU switchON (READY LIGHT WITHIN 30 SECONDS)CAUTION: To prevent an APU running engagement and APU exhaust torching, a minimum of 2 minutes must elapse between APU shutdown and another APU start.
	09	ENG CRANK switchRNOTE: The right engine is normally started first in order to provide normal hydraulics to the brakes.
	10	Right throttleIDLE (10 PERCENT N2 MINIMUM)CAUTION: Do not allow N2 rpm to dwell between 26 and 29 percent during engine motoring, to prevent vibration and damage to compressor blades.NOTE: Oil pressure should be a minimum of 10 psi within 30 seconds. Maximum transient EGT during start is 871 degC. During ground starts the FADEC automatically cuts back fuel flow to prevent EGT exceeding 815 degC.
	11	CFIT voice warningsCHECK
	12	Battery gaugeVERIFY 28 VDC
	13	L(R) DDI, HUD and MPCD knobsONCAUTION: During a battery start of the right engine, recognition of an R ATS caution is delayed until the displays are turned on. Once powered, verify the R ATS caution is not set.
	14	HMD switch (if applicable)ON
	15	EFDCHECK GROUND IDLENOTE: Ground idle: RPM 61 percent minimum, TEMP 250 to 590 degC, FF 600 to 900 pph, OIL 35 to 90 psi (warm oil), NOZ 77 to 83 percent.
	16	BLEED AIR knobNORMNOTE: The bleed air shutoff valves close during the fire warning test, so the knob must be rotated from OFF to NORM with ac power applied to reset the valves.
	17	LT TEST switchTEST
	18	ENG CRANK switchL
	19	Left throttleIDLE (10 PERCENT N2 MINIMUM)
	20	ENG CRANK switchCHECK OFFNOTE: The crank switch returns to OFF when the corresponding generator comes online at approximately 60 percent N2. After both generators are online the APU runs for 1 minute and then shuts down automatically.
	21	EFDCHECK GROUND IDLE

PHS 5 — Before Taxi Checks32 steps

	01	WYPT 0 and MVARCHECK/SET
	02	GPWS/TAWSCHECK BOXED
	03	INS knobGND (PARK BRK SET)
	04	RADAR knobOPR
	05	FLIR and LST/NFLR switchesAS DESIRED
	06	UFCD avionicsTURN ONNOTE: RALT ON/SET, TCN ON, T/R and channel set, IFF ON with modes unboxed.
	07	WINGFOLD switchSPREAD
	08	FCS RESET buttonPUSH (VERIFY RSET ADVISORY)
	09	FLAP switchAUTO
	10	FCS IBITPERFORMWARNING: Flight with BLIN codes could result in a FCS failure and aircraft loss.NOTE: Hold the FCS BIT consent switch up for at least 2 seconds then press the FCS option. Verify the AOA warning tone at completion, FCS A and FCS B BIT status GO and no BLIN codes.
	11	TrimCHECK PITCH, ROLL AND YAW
	12	T/O TRIM buttonPRESS UNTIL TRIM ADVISORY DISPLAYEDNOTE: Sets stabilators 4 deg nose up. A CHECK TRIM caution is displayed when both throttles are advanced beyond 27 deg THA if the stabilators are trimmed less than 3.5 deg TEU with the launch bar up.
	13	Control stickCYCLENOTE: Full aft: 24 deg NU stabilator. Full forward: 20 deg ND stabilator. Full left/right: 30 deg differential stabilator (21 deg with tanks or A/G stores on any wing station). Tolerance plus or minus 1 deg.
	14	FLAP switchHALF
	15	Rudder pedalsCYCLE RUDDERS 40 DEG L/R
	16	PROBE, speedbrake, LAUNCH BAR switches and HOOK handleCYCLENOTE: Ensure the HOOK handle is fully up to minimize the probability of inadvertent hook drops.
	17	Pitot and AOA heat checkPERFORMWARNING: Failure of both AOA probe heaters in icing conditions may cause a sharp uncommanded nose down attitude, uncontrollable by normal stick forces or paddle switch actuation.
	18	AV COOL switch emergency checkPERFORM (IF GROUND PERSONNEL PRESENT)
	19	APUVERIFY OFF
	20	FLBIT optionSELECT
	21	BINGOCHECK/SET
	22	CVRSAS DESIRED
	23	Standby attitude reference indicatorUNCAGE AND ERECT
	24	Altimeter settingSETNOTE: HUD altitude displayed within 30 feet of parking spot elevation. Standby altimeter within 60 feet of parking spot elevation.
	25	INSCHECKNOTE: Alignment status COMPLETE, GPS HERR/VERR within limits, INS knob NAV or IFA. Verify HUD airspeed indicates less than 50 kts.
	26	MUMI/IDSELECT/ENTER DATE AND FLT
	27	Stores pageVERIFY INVENTORY AND STATION STATUS
	28	Weapons/sensorsON/BIT CHECK AS REQUIRED
	29	BIT pageNOTE DEGD/FAIL INDICATIONS
	30	HMDALIGNNOTE: Canopy must be down and locked to align the HMD/AHMD.
	31	Standby attitude dataCHECKNOTE: ATT switch STBY, verify standby data replaces INS data on the HUD and agrees, then ATT switch AUTO.
	32	OBOGS systemCHECKWARNING: Continued operation and use of the OBOGS system with an OBOGS DEGD caution may result in hypoxia.NOTE: OBOGS control switch ON, OXY FLOW ON with mask on, check flow, press the OBOGS monitor electronic BIT pushbutton and verify the OBOGS DEGD caution sets and clears within 15 seconds.

PHS 6 — Taxi Checks3 steps

	01	CanopyEITHER FULL UP OR FULL DOWN FOR TAXICAUTION: Taxiing with the canopy at an intermediate position can result in canopy attach point damage and failure.
	02	Normal brakesCHECK
	03	Nosewheel steeringCHECK IN HIGH MODE L/RNOTE: Apply firm, steady brake pedal pressure. Use nosewheel steering whenever possible, minimizing differential braking. Wet brakes can degrade brake effectiveness by as much as 50 percent.

PHS 7 — Before Takeoff Checks9 steps

	01	CHKLST page FUEL TYPEVERIFY
	02	T.O. checklistCOMPLETE
	03	WINGFOLD switchLEVER-LOCKED IN SPREADWARNING: If the wings are commanded to unlock or fold during a catapult shot, the wings will unlock, the ailerons will fair, the wings may fold partially, and the aircraft will settle.
	04	CanopyCHECK CLEAR/CLOSEDCAUTION: Prior to operating the canopy switch, confirm aircrew are clear to reduce the potential for injury.
	05	OXY FLOW knobON/MASK ONCAUTION: It is possible to place the OXY FLOW knob in an intermediate position between the ON and OFF detents, which may result in a reduced flow of oxygen.
	06	IFF sublevelBOX REQUIRED MODES
	07	PARK BRK handleFULLY STOWED
	08	ENG pageCHECK ENGINES AT MIL (IF DESIRED)NOTE: MIL: N1 86 to 98 percent, N2 88 to 100 percent, EGT 720 to 932 degC, FF 11,000 pph maximum, NOZ 0 to 45 percent open, oil pressure 80 to 150 psi.
	09	FLAP switchHALF (FIELD TAKEOFF)NOTE: NATOPS 7.3.13 leaves the FLAP switch in HALF after the control check and selects FULL only for carrier-based operations. The After Takeoff check returns the switch to AUTO.

PHS 8 — Normal Takeoff9 steps

	01	Both enginesSTABILIZE AT 80 PERCENT N2
	02	BrakesRELEASE
	03	ThrottlesMIL (MAX IF DESIRED)
	04	EGT and RPMCHECK
	05	Afterburner light-off (if MAX selected)VERIFY BOTH NOZZLES OPENING
	06	Runway centerlineTRACK WITH SMALL RUDDER PEDAL INPUTSNOTE: Nosewheel steering is the most effective means of directional control during takeoff. Differential braking is much less effective and should be avoided.
	07	Rotation1/3 TO 1/2 AFT STICK AT PREDICTED NOSEWHEEL LIFTOFF SPEEDCAUTION: Pitch attitude shall not exceed 10 deg on takeoff. Above 10 deg the trailing edge of the stabilators can impact the ground during an over-rotation check; above 14 deg the engine exhaust nozzles may contact the ground.
	08	Velocity vectorCAPTURE 3 TO 5 DEG
	09	Standing water on the runwayCONSIDERCAUTION: Takeoff with significant standing water (greater than 1/4 inch) on the runway may cause water ingestion, which in extreme cases can cause engine stalls, flameouts, AB blowouts and/or engine FOD.

PHS 9 — After Takeoff Checks2 steps

	01	LDG GEAR handleUPNOTE: If required, reduce power to MIL or below to ensure the landing gear is up and locked before passing 250 KCAS.
	02	FLAP switchAUTO

PHS 10 — Airborne Checks9 steps

	01	Climb speedUP TO 350 KCAS AS REQUIRED BELOW 10,000 FEETNOTE: For optimum climb performance refer to A1-F18EA-NFM-200.
	02	Cabin altimeter (10,000 foot checks)VERIFY 8,000 FEET
	03	Fuel transferCHECK INTERNAL AND EXTERNAL
	04	RALTCHECK/SET TO 5,000 FEET
	05	Maximum range cruise3.0 DEG AOANOTE: Maximum range cruise is approximated by establishing 3.0 deg AOA, but no faster than Mach 0.85.
	06	Maximum endurance cruise3.7 DEG AOA
	07	Cabin altimeterMONITORCAUTION: A slowly increasing cabin pressure altimeter may be the first or only warning of a gradual loss of cabin pressurization.NOTE: Below 8,000 feet aircraft altitude the cabin is ambient. From 8,000 to 24,500 feet the cabin holds 8,000 feet. Above 24,500 feet the cabin is approximately altitude x 0.4.
	08	RVSM AOA crosscheckCOMPARE L AND R AOANOTE: If L and R AOA values on the FCS page differ by more than 2 deg, notify ATC that the aircraft is no longer RVSM compliant.
	09	RVSM altitude crosscheckCOMPARE STANDBY AND HUD ALTITUDENOTE: If altitudes differ by more than 250 feet, notify ATC that the aircraft is no longer RVSM compliant.

PHS 11 — Descent / Penetration Checks15 steps

	01	HOOK handle / HOOK BYPASS switchAS REQUIRED/DESIRED
	02	Exterior lightsSET FOR LANDING
	03	Visual ID IDENT knobNORM
	04	ENG ANTI ICE switchAS REQUIRED
	05	PITOT ANTI ICE switchAUTO
	06	DEFOG handleHIGH (IF REQUIRED)NOTE: The windshield may fog rapidly under conditions of very high descent rates and high humidity.
	07	WINDSHIELD switchAS REQUIRED
	08	Altimeter settingCHECK
	09	RALTCHECK/SET
	10	NAV master modeSELECTNOTE: Compare the HUD with the standby flight instruments and standby compass.
	11	Navaids / MAG VARCROSSCHECK
	12	ILSON/CHANNEL SET (IF REQUIRED)
	13	IFFAS DIRECTED
	14	Weapons / sensorsOFF AS REQUIRED
	15	Penetration250 KCAS / 4,000 TO 6,000 FPMNOTE: Up to 350 KCAS may be required below 10,000 feet for safe maneuverability.

PHS 12 — Landing Checks14 steps

	01	BreakTHROTTLES IDLE / SPEEDBRAKE AS REQUIREDNOTE: The desired abeam distance is 1.0 to 1.3 nm.
	02	LDG GEAR handleDOWN (BELOW 250 KCAS)
	03	FLAP switchFULL
	04	On-speed AOA8.1 DEGNOTE: On-speed is approximately 136 KCAS at 44,000 lb gross weight (max trap). Subtract 1.5 KCAS for each 1,000 lb decrease and add 1.5 KCAS for each 1,000 lb increase in gross weight.
	05	Landing checklistCOMPLETENOTE: WHEELS, FLAPS, HOOK, ANTI SKID, HARNESS, DISPENSER, EJECT SEL, AOA.
	06	Report3 DOWN AND LOCKED, FLAPS FULL (HALF), AOA CROSSCHECKED
	07	Pattern altitude600 FEET AGL (LOW PATTERN)
	08	180 position27 TO 30 DEG AOB / 300 TO 400 FPM
	09	90 position450 FEET AGL / 400 TO 500 FPM
	10	The start220 TO 250 FEET AGL / 650 TO 750 FPM ON-SPEED
	11	Final approachCENTERED BALL TO TOUCHDOWN, ON CENTERLINE, ON-SPEED
	12	TouchdownPLACE VELOCITY VECTOR AT LEAST 500 FEET PAST THRESHOLD
	13	ThrottlesIDLENOTE: The engines will not select ground idle until the aircraft has decelerated below 80 KCAS.
	14	BrakingMODERATE TO HEAVY, ONE SMOOTH APPLICATIONCAUTION: Any landing above 46,000 lb gross weight is a heavy gross weight landing. Delay initial brake application to 115 KCAS or lower if possible to avoid melted fuse plugs and deflated tires.NOTE: Anti-skid is effective down to approximately 40 KGS. Below 40 KGS relax heavy brake pedal pressure to prevent tire skid. Selecting aft stick below 100 KCAS increases stabilator down force and aids deceleration.

PHS 13 — After Landing Checks8 steps

	01	Ejection seat SAFE/ARMED handleSAFEWARNING: Make sure the handle is locked in the SAFE detent and the word SAFE is completely visible. If unable to properly safe the ejection seat, instruct line personnel to remain clear of the cockpit.
	02	EJECTION MODE handleNORM
	03	Landing gear handle mechanical stopCHECK FULLY ENGAGEDCAUTION: If the DOWNLOCK ORIDE button is pressed or the mechanical stop is not fully engaged, the LDG GEAR handle can be raised on the ground and the main landing gear will retract.
	04	FLAP switchAUTO
	05	T/O TRIM buttonPRESS UNTIL TRIM ADVISORY DISPLAYED
	06	MaskOFF
	07	OBOGS systemSECURENOTE: OXY FLOW knob OFF, then OBOGS control switch OFF.
	08	CanopyEITHER FULL UP OR FULL DOWN FOR TAXI

PHS 14 — Before Engine Shutdown Checks14 steps

	01	PARK BRK handleSET
	02	BIT displayRECORD DEGD/FAIL INDICATIONS
	03	Radar maintenance (BOA) codesRECORD IF PRESENT
	04	RADAR knobOFF
	05	FCS displayRECORD BLIN CODES
	06	EFDRECORD MSP CODES
	07	INS knobOFF
	08	Standby attitude reference indicatorCAGE
	09	HMD switchOFF
	10	CRYPTO switchAS REQUIRED
	11	Sensors, avionics and CVRSOFFNOTE: The aircraft incorporates an avionics auto-shutdown feature which powers down all UFCD controlled avionics when both throttles are secured.
	12	EXT and INTR LT knobsOFF
	13	CanopyCHECK CLEAR/OPENWARNING: A high voltage static electrical charge may build up inflight and be stored in the windscreen and canopy. Avoid direct contact with the outside of the windscreen and canopy to prevent electrical shock.
	14	QDCDISCONNECTED AND STOWED

PHS 15 — Engine Shutdown Checks11 steps

	01	Brake accumulator gaugeCONFIRM 3,000 PSI
	02	Paddle switchPRESS (DISENGAGE NWS)
	03	Engine cool downCONFIRM 5 MINUTESNOTE: Both engines should be operated at ground idle (75 percent N2 or less) for 5 minutes before shutdown to allow temperatures to stabilize and prevent engine seizure and rotor damage.
	04	BLEED AIR knobOFFNOTE: If an engine is shut down before placing the BLEED AIR knob to OFF, the corresponding primary bleed air shutoff valve may not fully close, resulting in residual engine fumes in the cockpit on subsequent start.
	05	ThrottleOFF (ALTERNATE SIDES)
	06	FLAP switchFULLNOTE: Performed after hydraulic pressure decays through 500 psi to verify proper switching valve operation.
	07	FCS pageVERIFY NO CHANNEL FULLY CROSSED OUT
	08	COMM 1 and 2 knobsOFF
	09	L(R) DDI, HUD and MPCD knobsOFF
	10	Other throttleOFF
	11	BATT switchOFF (WHEN AMBER FLAPS LIGHT ILLUMINATES)CAUTION: Due to FCS keep alive circuitry, uncommanded flight control movement may occur for up to 10 seconds after the BATT switch is placed to OFF if residual hydraulic pressure is still present.