cessna-172-training-supplement

Recommendations

Info

Calculate the Following1. Zero Fuel Weight2. Zero Fuel CG3. Takeoff Weight4. Takeoff CG5. From comparing the Takeoff CG and Zero Fuel CG, which direction doesthe CG move as fuel is burned off?Plot Zero Fuel CG and Takeoff CG on the CG Envelope Graph Below.Answers: (1) 2226.3 lbs. (2) 44.07" (3) 2536.3 lbs. (4) 44.55" (5) ForwardFormulas• Weight × Arm = Moment• Total Moment ÷ Total Weight = CG• Max Ramp Weight – Zero Fuel Weight = Usable Fuel Weight• Fuel Weight ÷ 6 = Fuel Gallons• 100LL fuel weighs 6 lbs./gal.; oil weighs 7.5 lbs./gal.• 3 Gallons of unusable fuel and oil at full capacity are included in BasicEmpty WeightCG Envelope Graph260025002400230022002100200019001800170016001500UtilityCategoryNormalCategory34 35 36 37 38 39 40 41 42 43 44 45 46 47 48CG Location22 • Performance / Weight & BalanceNOTE: Graph shown is for S-model and upgraded R-model 172s.For early-model 172s, consult the aircraft manual for weight andbalance graphs and envelopes.
SECTION 4Departure ProceduresEngine Failure Immediate Action and Off-Airport LandingsWhile a complete loss of engine power is a rare occurrence, it can happen.ATP pilots must know the emergency procedures from the POH and have acontingency plan in mind for the worst-case scenario.General Guidelines:• Know immediate action items• Best glide speed & altitude = time• Gliding distance from 1000 ft. AGL = Approx. 1.5 miles and 1 ½minutesThe following chart comes from extracted POH data and shows theglide distance and time expected after an engine failure with no windand at max gross weight. Aircraft performance may vary considerablybased on wind conditions, airplane weight and bank angle.C-172SBest Glide Speed 68 KIASAltitude (ft. AGL) Distance (NM) Time700 0.75 1 min1000 1.7 1 min 15 sec2000 3.0 2 min 30 sec3000 4.5 3 min 45 secDeparture Procedures • 23
Page 1 and 2: Cessna 172Training SupplementATPFli
Page 3: Revised 2021-10-08ContentsEarly & L
Page 6 and 7: NOTE: R-model 172s were originally
Page 8 and 9: Landing GearThe landing gear is a f
Page 10 and 11: Exterior LightingExterior lighting
Page 12 and 13: maximum smoothness. Carburetor heat
Page 14 and 15: G1000 Flight InstrumentsPrimary Fli
Page 16 and 17: Right Side - Top to BottomBottom Ed
Page 18 and 19: AHRS FailureADC FailureAHRS ModesTh
Page 20 and 21: Standard Avionics ConfigurationsGar
Page 22 and 23: Single Garmin GNS430VFR & Traffic P
Page 24 and 25: SECTION 3Performance / Weight & Bal
Page 28 and 29: General Guidelines (continued):Engi
Page 30 and 31: Below 800 Feet AGLIf the engine qui
Page 32 and 33: 800 to 1500 Feet AGLIf an engine fa
Page 34 and 35: Engine Failure over WaterAlthough A
Page 36 and 37: Short-Field Takeoff1. Flaps 10°2.
Page 38 and 39: SECTION 5Arrival ProceduresSummary
Page 40 and 41: TIP: Do not allow briefing the appr
Page 42 and 43: the windshield, increase the pitch
Page 44 and 45: Seat PositionCorrectly positioning
Page 46 and 47: Normal Approach & Landing1. Complet
Page 48 and 49: No-Flap Approach & LandingSteps 1-4
Page 50 and 51: Soft-Field Approach & LandingSteps
Page 52 and 53: Power-Off 180° Accuracy Approach &
Page 54 and 55: Crosswind Approach & LandingCareful
Page 56 and 57: TIP: Develop the habit of applying
Page 58 and 59: Rejected or Balked LandingA rejecte
Page 60 and 61: Non-Precision Approach (VOR, LOC Ap
Page 62 and 63: SECTION 6In-Flight ManeuversNOTE: C
Page 64 and 65: GROUND USE ONLYPVT COM Power-Off St
Page 66 and 67: GROUND USE ONLYPVT Rectangular Cour
Page 68 and 69: GROUND USE ONLYPVT Turns Around A P
Page 70 and 71: GROUND USE ONLYCOM Lazy EightsLazy
Page 72 and 73: GROUND USE ONLYCOM Steep SpiralsSte
Page 74 and 75: GROUND USE ONLYCFI Elevator Trim St
Page 76 and 77:
11. Will the engine continue to run
Page 78 and 79:
47. Are the power settings listed o
Page 80:
53 (Usable Fuel) 4810 GPHFlaps 10Ce
show all

cessna-172-training-supplement

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?