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HIGHLIGHTS from bookGENERAL AIRCRAFTELECTRICALPOWER PLANT AND SYSPROPELLERFUEL SYSFLIGHT CONTROLSLANDING GEARENVIRONMENTALFLIGHT INSTRUMENTSAVIONICSLENGTH35 FT 6.0 INHEIGHT14 FT 2.6 INWING SPAN50 FT 2.9 INMAX RAMP WEIGHT9710 LBSMAX LAND WEIGHT9168 LBSVMO and (changes ___KIAS per ___ ft above ___MSL227 KIAS, 4 KIAS/1000’ ABOVE 15,500 ft MSLVyse110 KIASLanding Limitations? (3)flared landings onlymax sink rate = 600 fpmmax xwind = 20 ktsMin crew with passengers?AC COMMANDER +2nd pilot, IUT, PIU, SNAELT has _____ battery. Transmit for ___ hoursSelf-contained battery48 hrsRubber door seal pressure provided by____Pnuematic air (bleed air? Pg 1-10 workbook)DO NOT OPEN _____ WHILE AIRCRAFT PRESSURIZEDEmergency Exit Hatch4 sources of DC POWERBattery – 24 V / 42 amp-hrAux Bat – 24 V / 5 amp-hrL/R Starter Gen – 28 V/ 250 ampEach Generator Control box provides (5)Voltage regulation (28.25 +/- 0.8 Vdc)Auto parallelingOVERvoltage protection (31 Vdc)UNDERvoltage protection (18 Vdc)REVERSE current protectionAPU must NOT exceed ____ Vdc and must be capable of delivering CONTINUOUS load of ____ amps and SURGE loads up to ______ amps for _____ second if required28 vdc300 amps1000 amps0.1 secondAPU START requires20 VHOT BAT BUS single powered?L/R fire extingThreshold lightsHOT BAT BUS Dual powered?XFEED VALVEL/R BOOST PUMPL/R FIREWALL SHUTOFF[no more AC power __ 20170220][no more AC power __ 20170220]GEN malfunction: first indications?L/R GEN OUT light andFlashing FAULT WARNSingle Gen failure: steps?Turn gen off, attempt resetUnsuccessful? Turn gen off and perform current limiter check –see page 2-12Dual Gen failure: If both lights on and gen do not reset you are running on ____ power exclusively.Last for ____ amp hours, as few as ____ minutesBATTERY POWER42 amp hours for 10 minutesDual Current Limiter Fail: All equipment still powered?Volt meter will read ____ V.Yes as long as gens good24 V, battery no longer chargingGen fail with OPPOSITE side current limiter: equipment lost?Battery is ______.Not initially Discharging –see page 2-13Gen fail with SAME side current limiter: buses and equipment on fail side working?Battery is ______.Results in loss of _____, and main _____ and _____ busses.NO, INOPNot being dischargedfuel and avionics buses[no more AC power __ 20170220]DO NOT RESET THESE CIRCUIT BREAKERSSubpanel feeder circuit breakerNon-essential circuit breakerCOMPRESSOR PROGRESSIVE BLEED VALVE: Full closed at ____%Fully open at ____% and below75%62% and belowCompression ratio = 7:1When N1 reads 100%, Gas gen/comp speed=When N1 reads 101.5%, Gas gen/comp speed=37,500 rpm38,000 rpmApprox. ____% intake air mixed with fuel25%_____ fuel nozzles (___primary and ____ secondary)____ igniter plugs14, 10 primary, 4 secondary2 igniter plugsRGB directly connected to _____Power turbinePower turbine at 33,000 rpm, prop spd:Power turbine at 28,500 rpm, prop spd:2200 rpm1900 rpmOIL fuel heater: begins to bypass at _____, full bypass at ____.70 DEGREES F90 DEGREES FSTUDY diagram power quadrant fig 3-3 controls pg 3-9Power Lever connected to Cam boxFCU and beta linkagesCondition Lever connected to SCU (starter control unit)Power Lever ranges: What power lever cntrlsA = B =REVERSE = A = N1 ONLYB = BLADE ANGLEREVERSE = BOTHStudy chart on 3-12Max allowable: AKA _____Oil temp rangeOil P rangeOn takeoff initially ____ limited as you climb you are ____ limitedHi/Lo idle for N1 ___/____ITT exceed ____ discontinue startGen load 0.5 to 0.75 min N1? Chart on 3-12Takeoff = max allowable10-99 C85-100 psiTorque, ITT (normal day)70-73 / 51-54925(see chart)COLD TEMP LOW ALT = Torque or ITT limited?HOT and HIGH = Torque or ITT limited?TORQUEITTITT LIMITS (normal range, max continuous, max starting?)400-790, 790, 1090 CelsiusBlade angles:FeatherLow pitchZero thrustReverseApprox. cruise8715-5-1125-35Normal prop op range1800-2200Primary gov fail? If overspeed N2 ____2288 +/- 40Prop Gov test switch tests ______, resets to maintain b/w ____ to ____ rpmOVERSPEED GOV1900-2100Fuel topping gov prevents rpm exceeding ____2332 rpmAuto feather occurs if engine dies if (2)System armedBOTH power leverS above 90% N1With auto feather in armed, retarding 1 or both power levers will disengage auto feather system. T or FTRUEBelow 410 +/- 50 ft lbs= Below 260 +/- 50 ft-lbs=Turns off auto feather sys for opposite engine, denergizes opposite auto feather lightAuto feather system ACTIVATELEFT prop _____, right prop = _____MASTER – slaveIf synchrophaser in use and right landing gear extended, this light will illuminatePROP SYNC – pg 4-10Plus or Minus ____ RPM is the limit of actuator authority30 RPM, pg 4-11Prop link fail, either result in (2)Prop remain at current settingOr increase to 2200 rpm5 fuels approved2 alternatesAVGAS on for _____ use.JET: A1, B, 4 / JP 5,8JET A1 and F4280/87/100LL through 115/145TRANSFER SWITCHESPump on at ____ galPump off at ___ gal or ___ if other fails42 on51 off or 59If fuel transfer fails with fuel in wing tanks, up to ___ gal can be trappedOVERRIDE mode bypasses _____ switches and it runs Continuously/Set amount of time?28 gallonBypass float switchesRuns CONTINUOUSLYR/L NO FUEL TRANSFER LIGHT can mean 3 things1) Total fuel = Nacelle? – no fuel in wing tanks2) Total fuel > Nacelle? –depends, you need those 28 lbs?Yes? Try switch to OVERIDENFT light off = pump goodNFT light still on = pump fail, plan for 28 lbs unusableNo? don’t use override, turn pump off, gravity flow starts once nacelle drop to 3/8 full3) Fuel in wings but Nacelle = YELLOW ARC, with no light?Transfer switch off?Transfer pump CB out?42 gal float switch inop- override itTransfer light warning IF (2)Pressure switch detect <3 psiPUMP TOLD TO RUNBoost pump fail, indications?FUEL P Light FLICKERXFEED LIGHT ON (if in auto)Crew close xfeed valve to determine which boost pump has failedXfeed or suction decisionXfeed if range not factor, if it is suck itXFEED goes from TANK on one side to ____ Generally used for ____ failsWhy do we not fly with xfeed valve open normally?ENGINE on the other sideBoost pump failsThe strongest boostpump will feed both engines and imbalance will occurSteering range with NWS and brakes?48 either sideDO NOT tow with ____ control lockRUDDERElevator trim tab = ______ actionAnti servoTrim disconnect switch, 2 levels1st = disconnect auto pilot and YD2nd = disconnect ELECTRIC TRIMLanding gear, what holds gear in the UP position?What prevents coasting and overtravel?Jackscrew and dynamic braking (pg 7-3)Dynamic braking and limit switchesWHEELS UP WARNING = 3 signalsWarning Horn, WHEELS UP light, 2 red handleGet the warnings if gears not down and locked and: (2)Both power levers retarded below 79% N1 rpmFLAPS beyond apprchSee figure 7-1 pg 7-5workbook for how to silenceR SQUAT SWITCHES“FLRSTOTS”F-light hour meterL-anding gear circuitR- ight eng inlet lip boot heatS- tall warnT- ransponderO- peration of some stuff in (AHRS/DCU/GPS)T- AS/RADAR S- tall warn heatGROUPSFLR = INOPSTO = DEACTIVATE/INHIBITT = STDBYS = GOES TO 14 VL SQUAT SWITCHESL- eft engine inlet lip heat = INOPE-lectric heater = GND MAXA-mbient air solenoid = CLOSEP-ressurization controls = INOP LIMIT SWITCHES: locationOn landing gear drive train assembly underneath floor of cabinParking brakes CAN/CANNOT be set using copilot brake pedalsCANNOTRetraction of landing gear automatically centers nose wheel and disengages OR can you move it in flight?Disengage, no move in flightOUTFLOW VALVE: diff p not exceed ___ PSIDDoes it have negative P relief?4.7YesSAFETY VALVE: diff p not exceed ___ PSIDDoes it have negative P relief?4.9Yes“Our friend MANUAL” COOL controlled through INCR/DECR or knob thingyINCR/DECR, manual = no knobELECTRIC HEATER LOCKOUT, if these ON (3)Windshield HeatProp De-iceEngine Lip boot heatOxygen Supply gives _____ cubic ftPressure = ____ psiTemperature491850 psi +/- 5070Operate windshield on dry glass?NoICE VANES EXTENDED, what results? (3)Engine torque DECREASE – around 40-60 ft lbsITT may INCREASERange REDUCED – around 10-12%On deck electrical power to heating elements goes from 28 Vdc to ____ Vdc14Except during TO roll, pitot heat SHOULD/SHOULD NOT be used while aircraft on groundSHOULD NOTOverheat possible, lack of cooling airflowSTDBY COMPASS can give error if these are activated (5)Windshield ANTI ICEWindshield WIPERSACElectric HeatVent blowerAlternate static located in ______, info goes to _____ instruments and _____ if normal static air source fail. Rear pressure bulkheadPilot instruments and ESISPg 9-6ESIS powered by ______ bus, that bus in emergencies can be powered by ____ Gets info from AHRS 1 OR 2?Has its own ADC?Gets other stuff from ____ 1. See page 9-7ESSENTIAL AV BUS, AUX BATTAHRS 1YESNAV 1AV ESSENTIAL BUS POWERS: CRANEC-OM 1R-TUA-UDIO (PILOT)N-AV 1E-SISFMS consisted of ____ and _____ computer. System blends input from ____, _____, and____ to compute present positionCDU and FMSVOR, DME, GPSCDU- TUN button allows tune and select for:COM1NAV1 AND NAV2 (receive VOR/LOC freqs only)DMEHOLDATCADFFLIGH DIRECTOR (FD) provides ___ and ____ guidance based on crew inputs on the ____Pitch and rollFGP (Flight Guidance System)Autopilot may be engaged at ____ on dep, ____ at cruise, disengaged by ____ on aprch400 AGL dep1000 AGL cruise180 AGL aprchTAS provides/does not provide resolutionDOES NOT Weather radar antenna located on _____Detect Precip (WX mode) up to ____ NMDetect Turb (WX + T) up to ____ NMTo display RADAR PFD must be in ____ or ____ and RDR ____ selectedNose of aircraft30050120, 120 map mode, overlay ................
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