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Quick Reference Guide - aste.usu.edu

SOP Quick ReferenceGuide 3 USU SOP Quick ReferencePrivate and Commercial QRGG round Reference ManeuversTurns Around a Point, Rectangular Course, S-Turns, and Eights on PylonsDA40 FAltitude 800 AGLP ower ~ 2350 RPMA irspeed 95 KIASP itch +4 Flaps UP Fuel Pump ONArrow PA28r-200 Altitude 800 AGLP ower ~ 17 MP, 2550 RPMA irspeed 100 MPHP itch +2 Flaps UP Fuel Pump ONPivotal Altitude CalculationsThe formula is as follows: ground speed squared divided by for knots and ground speed squared divided by 15 for miles per these are figured in Groundspeed and rounded AGL8710067091105735961108101041209601091 2510501131301130 Performance ManueversMinimum Altitude +2000 AGLSteeP turnSDA40F 95 KIASPA28R-200 100 MPHChAnDelleSDA40F VABelow 2161 lbs.

Quick Reference Guide . 3 USU SOP uick Reference Private and Commercial QRG Ground Reference Maneuvers Turns Around a Point, Rectangular Course, S-Turns, and Eights on Pylons ... USU SOP uick Reference Compass Deviation - caused by an aircraft’s structure and the electrical accessories in the aircraft. See deviation card on the magnetic

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1 SOP Quick ReferenceGuide 3 USU SOP Quick ReferencePrivate and Commercial QRGG round Reference ManeuversTurns Around a Point, Rectangular Course, S-Turns, and Eights on PylonsDA40 FAltitude 800 AGLP ower ~ 2350 RPMA irspeed 95 KIASP itch +4 Flaps UP Fuel Pump ONArrow PA28r-200 Altitude 800 AGLP ower ~ 17 MP, 2550 RPMA irspeed 100 MPHP itch +2 Flaps UP Fuel Pump ONPivotal Altitude CalculationsThe formula is as follows: ground speed squared divided by for knots and ground speed squared divided by 15 for miles per these are figured in Groundspeed and rounded AGL8710067091105735961108101041209601091 2510501131301130 Performance ManueversMinimum Altitude +2000 AGLSteeP turnSDA40F 95 KIASPA28R-200 100 MPHChAnDelleSDA40F VABelow 2161 lbs.

2 94 KIASUpto 2535 lbs. 108 KIASPA28R-200 <131 MPHlAzy eightSDA40F Below 2161 lbs. 84 KIASUpto 2535 lbs. 95 KIASPA28R-200 110 MPHSteeP SPirAlDA40F Vg 73 KIASPA28R-200 Vg 95-105 MPH4 USU SOP Quick ReferenceStalls & Slow FlightMinimum Altitude +2000 AGLSlow FlightDA40F 2200 RPMB elow 2161 lbs. 45-47 KIASUpto 2535 lbs. 52-54 KIASPA28R-200 19 MP 2700 RPMB ottom of White Arc 55-63 MPHP ower on StAllSDA40F 65 KIAS Takeoff Config. 73 KIAS Cruise Climb 75 MPH Takeoff Config. 100-110 MPH Cruise Climb oFF StAllSDA40F 75 KIAS Landing 75 MPH Landing and Flaps Extended5 USU SOP Quick ReferenceInstrument QRGPitCh/Power tAble (DA40)PhASeAirSPeeDConFigrPMPitChInitial Climb <1000 AGL** See ChartFlaps T/O, Carb heat coldFull - 2600+8 Cruise Climb >1000 AGL** See ChartFlaps UP, Carb heat coldFull - 2600+7 Normal Cruise110 Clean, Carb heat cold2500-1 Holding, Transition100 Clean, Carb heat cold2400+1 Cruise Descent (smooth air only)130 Clean, Carb heat ON2500-8 Normal Descent120 Clean, Carb heat ON2350-2 Vectors (within 90 of inbound course)

3 90 Clean, Carb heat cold2300+2 Vtgt*CalculatedFlaps T/O, Carb heat ON2000-4 Standard Vref85 Flaps T/O, Carb heat cold1950-4 Final Approach Landing Assured** See Chart**See Chart, Carb Heat Cold1500-3*Vtgt = Vref + 5 + 1/2 the steady state wind + gust factor (never to exceed Vref + 25)**ChartAirSPeeDS1874 lbS2205 lbS2535 lbSInitial Climb54 KIAS 60 KIAS66 KIASC ruise Climb60 KIAS68 KIAS73 KIASA pproach in Cruise settings (Flaps UP or T/O)60 KIAS68 KIAS73 KIASA pproach for normal landing (Flaps LDG)58 KIAS63 KIAS71 KIAS6 USU SOP Quick ReferenceTurnsStAnDArD rAte turnStandard Rate Turn 3 per secondBank Estimate (TAS/10) +6 or 15% TAStiMeD turnSA standard-rate turn of 3 per second equates to 10 seconds required to turn 30.

4 To execute a timed turn:Timer StartBank Establish Standard RateEstimate/calculate Time for turnTime limit Roll outroll-out leADbAnk AngleleADUp to 15 5 15 -30 10 Above 30 15 Magnetic CompassCoMPASS errorSMagnetic DipUNOS - Undershoot North, Overshoot South Roll wings level prior to a desired northerly heading and after a desired southerly heading. The amount of lead or lag when turning directly north or south varies with and is a function of the current local latitude ( , 42 at KLGU). The undershoot or overshoot diminishes incrementally to zero at direct easterly and westerly of lead = function of current latitude + normal leadWhere.

5 Function of Current Latitude = (100- current latitude (## )% * current latitude)+Normal Lead = based on bank angle (see Roll-out Lead ) for KLGU Function of Current Latitude ((100-42) = 58%) *42 = Normal Lead = + 5 lead = ~29 Acceleration compass ErrorsANDS Accelerate North, Decelerate South The magnetic compass will indicate a temporary turn to the north anytime an aircraft is accelerated abruptly on a direct easterly or westerly heading and it will indicate a temporary turn to the south anytime an aircraft is decelerated abruptly on a direct easterly or westerly heading. 7 USU SOP Quick ReferenceCompass Deviation - caused by an aircraft s structure and the electrical accessories in the aircraft.

6 See deviation card on the magnetic compass in each specific Variation - Difference between true north and magnetic north. This varies according to location around the BugsAltimeter Bug - should always be set on assigned altitude or a target altitude for climb or Bug - should always be set on assigned heading, course intercept heading, heading required to maintain course, runway heading for takeoff, or outbound heading for inCreASe AirSPeeDPower Increase to TargetPitch Nose Down to TargetTrim Re-trim to AirspeedDeCreASe AirSPeeDPower Decrease to TargetPitch Nose Up to TargetTrim Re-trim to AirspeedClimbs/DescentsCAll-outS 1,000 FEET TO GO (1,000 FEET BELOW A HIGHER TARGET ALTITUDE OR 1,000 FEET ABOVE A LOWER TARGET ALTITUDE)

7 200 FEET TO GO (200 feet below a higher target altitude and 200 feet above a lower target altitude) These call-outs apply anytime an altitude change is made; this includes descending to the minimums on instrument approach procedures. Level-off from climbs and descents should be started at 10% of the VSI SloPeRate of descent is controlled by pitch! When high on the glide slope, pitch down. When low on the glide slope, pitch is controlled by power! When airspeed is slow, increase power. When airspeed is high, decrease Attitude RecoverynoSe-low reCoveryPower Bank Pitch (increasing airspeed)Throttle IdleWings *LevelElevator Pull to the Horizon * In a nose-low recovery level the wings before pulling the nose up.

8 This will avoid increased load factors imposed on the aircraft structure by the bank angle of the aircraft. The intent of this is to avoid structural damage which may occur to the aircraft during a poorly executed, nose-low unusual attitude SOP Quick ReferencenoSe-high reCoveryPower Pitch Bank (decreasing airspeed)Throttle FullWings Push to HorizonElevator LevelHoldsholD SetuPNav Source Set/IdentifiedEntry DetermineAirspeed 100 KIASRPM 2350 GPS (if using)

9 SUSP prior to FixTimer Start at FixCruise Checklist PerformDirection of TurnsStandard - right turns (used unless specified of depicted otherwise)Non-standard left turns (only used when depicted or specified)DireCtInitial turn will be in the same direction as the turns of the assigned Fix Turn to outbound headingTimer Start at Wings LevelTurn inbound At Desired TimeInbound Course InterceptteArDroPInitial turn will be in the same direction as the turns of the assigned Fix Turn to heading +/-30 of inbound courseTimer StartTurn inbound At Desired TimeInbound Course InterceptPArAllelInitial two turns will be in the opposite direction as the turns of the assigned Fix Turn to heading opposite of inbound courseTimer

10 StartTurn inbound *At Desired Time* a. For VOR stations and GPS waypoints- fly direct back to the holding fix. Continue normal hold procedures. b. For Localizer or Intersection Holds- turn to an intercept heading for the inbound course. When the course needle comes alive, intercept and track the inbound course to the fix. Continue normal hold SOP Quick ReferenceholD tiMing/DiStAnCeRegardless of whether you have completed the outbound turn or not, start the outbound timer upon crossing the perpendicular course. There are a few ways to identify the perpendicular course:1. Set the HSI to the perpendicular course and wait until the needle centers2.


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