PILOT'S OPERATING HANDBOOK - Glass Cockpit Aviation
PILOT'SOPERATINGHANDBOOKPIPER CHEROKEE ARCHER IIFAA APPROVEDIN NORMAL AND UTILITYCATEGORIES BASED ON CAR 3 AND FAR PART 21,SUBPART J. THIS DOCUMENT INCLUDES THEMATERIAL REQUIRED TO BE FURNISHED TO THEPILOT BY CAR 3 AND FAR PART 21, SUBPART JAND MUST BE CARRIED IN THE AIRPLANE AT ALLTIMES.PA-28-181REPORT: VB-760FAA APPROVED BY:WARD EVANSD.O.A. NO. SO-1PIPER AIRCRAFT CORPORAT10NVERO BEACH, FLORIDAAIRPLANE SERIAL NO.AIRPLANE REGISTRATION NO.HANDBOOK PART NO. 761 619DATE OF APPROVAL: AUGUST 15, 1975
WARNINGEXTREME CARE MUST BE EXERCISED TO LIMIT THE USE OF THIS MANUAL TOAPPLICABLEAS INDICATEDBELOW ORAIRCRAFT. THIS MANUAL REVISEDSUBSEQUENTLY REVISED IS VALID FOR USE WITH THE AIRPLANE IDENTIFIED ON THEFACE OF THE TITLE PAGE WHEN OFFICIALLY APPROVED. SUBSEQUENT REVISIONSSUPPLIED BY PIPER AIRCRAFT CORPORATION MUST BE PROPERLY INSERTED.MODEL PA-28-18 1, CHEROKEE ARCHER IIPILOT'S OPERATING HANDBOOK, REPORT: VB-760 REVISIONPIPER AIRCRAFT CORPORATIONAPPROV AL SIGNATURE AND ST AMPPublished byPUBLICATIONS DEPARTMENTPiper Aircraft CorporationIssued: August 15, 1975REPORT: VB-760H
APPLICABILITYApplication of this handbook is limited to the specific Piper PA-28-181 model airplaneserial number and registration number on the face of the title page of this handbook.This handbookcannotbe used for operationalpurposesdesignated byunless kept in a current status.REVISIONSThe informationcompiled in the Pilot'sdistributed to the airplane owners.OperatingHandbookand/orRevision material will consist of information necessary to updateto add information to cover added airplane equipment.I.RevisionsRevisions will be distributed wheneverbe inserted into the handbook in accordance1.2.3.II.will be keptthe text of the presentnecessary as complete page replacementswith the instructions given below:or additionsRevision pages will replace only pages with the same page number.lnsert all additional pages in proper numerical order within each section.Page numbersfollowed by a small letter shall be inserted in direct sequencecommon numbered page.Identificationby -revisionscurrentwithhandbookand shallthe sameof Revised MaterialRevised text and illustrations shall be indicated by a black vertical line along the outside margin ofpage, opposite revised, added or deleted material. A line along the outside margin of the page oppositepage number will indicate that an entire page was added.thetheBlack lines will indicate only current revisions with changes and additions to or deletions of existingtext and illustrations. Changes in capitalization, spelling, punctuationor the physical location of materialon a page will not be identified by symbols.ORIGINAL PAGES ISSUEDThe original pages issued for this handbookprior to revision are given below:Title, ii through v, 1-1 through 1-14, 2-1 through 2-8, 3-1 through 3-12, 4-1 through 4-16, 5-1 through5-26, 6-1 through 6-52, 7-1 through 7-26, 8-1 through 8-16, 9-1 through 9-14, 10-1 through 10-2.REPORT: VB-760iii
PILOT'S OPERATING HANDBOOK LOG OF REVISIONSCurrent Revisions to the PA-28-181 Cherokeeissued August 15, 1975.RevisionNumber andCodeRev. 1 761 ORT:ivVB-760Archer ll Pilot's OperatingDescription of RevisionRevised wording of 6.9 (a).Removed Piper Dwg. No. from item 155.Added items 236 and 238.Revised item 263.Revised ELT pilot's remote switch info.Revised 8.7 (a), items (1), (2), and (3).Ilandbook,REPORT:VB-760FAA ApprovalSignature andDateWard EvansJan. 6, 1976
TABLE OF EMERGENCYSECTION4NORMAL 7DESCRIPTIONAIRPLANESECTION8AIRPLANE HANDLING, SERVICING ANDMAINTENANCESECTION9SUPPLEMENTSSECTION10SAFETY TIPSPROCEDURESAND BALANCEAND OPERATION OF THEAND ITS SYSTEMSREPORT: VB-760Y
TABLE OF CONTENTSSECTION eSpace.SpecificLoadingsSymbols, Abbreviations and 1-41-41-51-11REPORT: VB-7601-i
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IISECTION 1GENERALSECTION 1GENERAL1.1 INTRODUCTIONThis Pilot's Operating Handbook is designed for maximum utilization as an operating guide for thepilot. It includes the material required to be furnished to the pilot by C.A.R. 3 and FAR Part 21, Subpart J.It also contains supplemental data supplied by the airplane manufacturer.This handbook is not designed as a substitute for adequate and competent flight instruction,knowledge of current airworthiness directives, applicable federal air regulations or advisory circulars. It isnot intended to be a guide for basic flight instruction or a training manual and should not be used foroperational purposes unless kept in a current status.Assurance that the airplane is in an airworthy condition is the responsibility of the owner. The pilot incommandris responsible for determining that the airplane is safe for flight. The pilot is also responsible formarkings, placards, and thisremaining within the operating limitations as outlined by instrumenthandbook.Although the arrangement of this handbook is intended to increase its in-flight capabilities, it shouldnot be used solely as an occasional operating reference. The pilot should study the entire handbook tofamiliarize himself with the limitations, performance, procedures and operational handling characteristics ofthe airplane before flight.The handbook has been divided into numbered (arabic)sections, each provided with a "finger-tip" tabdivider for quick reference. The limitations and emergency procedures have been placed ahead of thenormal procedures, performanceand other sections to provide easier access to information that may berequired in flight. The "Emergency Procedures"Section has been furnished with a red tab divider topresent an instant reference to the section. Provisions for expansion of the handbook have been made bythe deliberate omission of certain paragraph numbers, figure numbers, item numbers and pages noted asbeing left blank intentionally.ISSUED: AUGUST 15, 1975REPORT: VB-7601-1
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER HSECTION 1GENERAL12' 10.48"2' 6.00"Wing Area (sq. ft.)Min. Turning Radius (ft.)(from pivot point to wingtip)170.030.05' 3.00" 35' 0.00"10' 0.08"23' 5.80"T 3.60"UNEgigtC GROUND6' 6.91"THREE VIEWFigure 1-1REPORT: VB-7601-2ISSUED: AUGUST 15, 1975
SECTION 1PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IIGENERAL1.3 ENGINES(a) Number of Engines(b) Engine Manufacturer(c) Engine Model Number(d) Rated Horsepower(e) Rated Speed (rpm)(f) Bore (inches)(g) Stroke (inches)(h) Displacement (cubicinches)(i) Compression Ratio(j) Engine :1Four Cylinder, Direct Drive,Horizontally Opposed, Air CooledPROPELLERS(a)(b)(c)(d)(e)(f)Number of PropellersPropeller ManufacturerModelNumber of BladesPropeller Diameter (inches)(1) Maximum(2) MinimumPropeller Type1Sensenich76EM8SS-0-6027676Fixed Pitch1.7 FUEL(a) Fuel Capacity (U.S. gal) (total)(b) Usable Fuel (U.S. gal) (total)(c) Fuel Grade, Aviation (min.octane)100/130-5048Green1.9 OIL(a)(b)Oil Capacity (U.S. quarts)Oil Specification(c)Oil Viscosity per Average Ambient Temp. for Starting8Referto latest issue ofLycoming Service Instruction(1)(2)(3)(4)Above 60 F30 F to 90 F0 F to 70 FBelow 10 FISSUED: AUGUST 15, 1975SINGLES.A.E. 50S.A.E. 40S.A.E. 30S.A.E. 201014.MULTIS.A.E. 40 or 50S.A.E. 40S.A.E. 40 or 20W-30S.A.E. 20W-30REPORT: VB-7601-3
SECTION 1GENERALPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER II1.11 MAXIMUM WEIGHTS25502550UTILITY195019502000NORMAL(a) Maximum Takeoff Weight (lbs)(b) Maximum Landing Weight (lbs)(c) Maximum Weights in Baggage Compartment1.13 STANDARD AIRPLANE WEIGHTSEmpty Weight (lbs): Weight of astandard airplane including unusable fuel,full operating fluids and full oil.Maximum Useful Load (lbs)*:The differencebetween the Maximum Takeoff Weight andthe Standard Empty Weight.(a) Standard(b)139011601.15 BAGGAGE SPACE242220(a) Compartment Volume (cubicfeet)(b) Entry Width (inches)(c) Entry Height (inches)1.17 SPECIFIC LOADINGS15.014.2(a) Wing Loading (lbsper sq ft)(b) Power Loading (lbsper hp)*This value is for a standard airplane without optional equipment.value to be used for C.G. calculations for the airplane specified.REPORT: VB-7601-4Refer to Figure 6-5 forthe useful loadISSUED: AUGUST 15, 1975
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IISECTION 1GENERAL1.19 SYMBOLS, ABBREVIATIONS AND TERMINOLOGYThehandbook(a)following definitions are of symbols, abbreviations andand those which may be of added operational significance toterminology used throughout thethe pilot.General Airspeed Terminologyand SymbolsCASCalibrated Airspeed means the indicated speed of an aircraft,corrected for position and instrument error. Calibrated airspeed isequal to true airspeed in standard atmosphere at sea level.KCASCalibrated Airspeed expressed in "Knots."GSGround Speed is the speed of an airplane relativeIASIndicated Airspeed is the speed of an aircraft as shown on theairspeed indicator when corrected for instrument error. IAS valuespublished in this handbook assume zero instrument error.KIASIndicated Airspeed expressed in "Knots."MMach Number is the ratio of true airspeed toTASTrue Airspeed is the airspeed of an airplane relative to undisturbedair which is the CAS corrected for altitude, temperature andcompressability.VAManeuvering Speed is the maximum speed at which application offull available aerodynamic control will not overstress the airplane.VFEMaximum Flap Extended Speed is the highest speed permissiblewith wing flaps in a prescribed extended position.VNE/MNENever Exceed Speed or Mach Number is the speed limitnot be exceeded at any time.VNOMaximum Structural Cruising Speed is the speed that should notbe exceeded except in smooth air and then only with caution.VSStalling Speed or the minimumairplane is controllable.VSOStalling Speed or the minimumairplane is controllableVXinto the ground.the speed of sound.that maysteady flight speed at which thesteady flight speed at which thethe landing configuration.Best Angle-of-Climb Speed is the airspeed which delivers thegreatest gain of altitude in the shortest possible horizontaldistance.VYISSUED: AUGUST 15, 1975Speed is the airspeed which deliversBest Rate-of-Climbgainaltitudeinin the shortest possible time.greatesttheREPORT: VB-7601-5
SECTION 1GENERAL(b)PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IIMeterological TerminologyISAInternational Standard Atmosphere in which:The air is a dry perfect gas;The temperature at sea level is 15 Celcius (59 Fahrenheit);The pressure at sea level is 29.92 inches hg. (1013 mb);The temperature gradient from sea level to the altitude at which(-69.7 F)is -56.5 Cis -0.00198 Cthetemperature(-0.003566 F) per foot and zero above that altitude.OATOutside Air Temperature is the free air static temperature,obtained either from inflight temperature indications or groundmeteorologicaladjustedfor instrument error andsources,compressibilityeffects.Indicated PressureAltitudeThe number actually read from an altimeter when the barometricsubscale has been set to 29.92 inches of mercury (1013 millibars).Pressure AltitudeAltitude measured from standard sea-level pressure (29.92in. Hg)by a pressure or barometric altimeter. It is the indicated pressurealtitude corrected for position and instrumenterror. In thishandbook, altimeter instrument errors are assumed to be zero.Station PressureActual atmosphericWindThe wind velocities recorded as variables on the charts of thishandbookare to be understoodas the headwind or tailwindcomponents of the reported winds.REPORT: VB-7601-6pressure at field elevation.ISSUED: AUGUST 15, 1975
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IISECTION 1GENERAL(c) Power Terminology (Specific)Takeoff PowerMaximum Rated Power(180 HP @ 2700 RPM)Maximum ContinuousPowerMaximum Rated Power(180 HP @ 2700 RPM)Maximum Climb PowerMaximum Rated Power(180 HP @ 2700 RPM)Maximum Cruise PowerMaximum Rated Power(180 HP @ 2700 RPM)Flight Idle PowerThrottleClosedGround Idle PowerThrottleClosed(d) Engine InstrumentsEGT GaugeExhaust Gas TemperatureGauge(e) Airplane Performance and Flight Planning TerminologyClimb GradientDemonstratedVelocityThe demonstrated ratio of the change in height during a portion ofa climb, to the horizontal distance traversed in the same timeinterval.CrosswindThe demonstratedcrosswind velocity is the velocity of thecrosswind component for which adequate control of the airplaneduring takeoff and landing was actually demonstrated duringcertification tests.Accelerate-Stop DistanceThe distance required to accelerate an airplane to a specified speedand, assuming failure of an engine at the instant that speed isattained, to bring the airplane to a stop.MEAMinimum en route IFR altitude.Route SegmentA part of a route. Each end of that part is identified by: (1) ageographical location; or (2) a point at which a definite radio fixcan be established.ISSUED: AUGUST 15, 1975REPORT: VB-7601-7
SECTION 1GENERAL(f)PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IIWeight and Balance TerminologyReference DatumAn imaginary vertical plane from which all horizontalmeasured for balance purposes.StationA location along the airplane fuselage usually given in terms ofdistance from the reference datum.ArmThe horizontal distance fromgravity (C.G.).of an item.MomentThe product of the weight of an item multiplied by its arm.(Moment divided by a constant is used to simplify balancecalculations by reducing the number of digits.)Center of Gravity(C.G.)The pointdistances arethe reference datum to the center ofat which an airplanewould balance if suspended.Itsdistance from the reference datum is found by dividing the totalmoment by the total weight of the airplane.C.G. ArmThe arm obtained by adding the airplane's individual moments anddividing the sum by the total weight.C.G. LimitsThe extreme center of gravity locations within which the airplanemust be operated at a given weight.Usable FuelFuel available for flight planning.Unusable FuelFuel remaining after a runout test has beenaccordance with governmental regulations.Standard Empty WeightWeight of a standardBasic Empty WeightStandard empty weight plus optional equipment.PayloadWeight of occupants, cargo and baggage.Useful LoadDifference between takeoff weight, or ramp weight if applicable,and basic empty weight.Maximum Ramp WeightMaximum weight approved for groundweight of start, taxi and run up fuel.)Maximum TakeoffMaximum weight approved for the start of the takeoff run.airplaneoperating fluids and full (It includesWeightMaximum LandingWeightMaximum weight approved for the landing touchdown.Maximum Zero FuelMaximum weight exclusive of usable fuel.WeightREPORT: VB-7601-8ISSUED: AUGUST 15, 1975
SECTION 1GENERALPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IITHIS PAGE INTENTIONALLYISSUED: AUGUST 15, 1975LEFT BLANKREPORT: VB-7601-9
SECTION 1GENERALPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IITHIS PAGE INTENTIONALLY LEFT BLANKREPORT: VB-7601-10ISSUED: AUGUST 15, 1975
SECTION 1GENERALPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER II1.21 CONVERSION FACTORSTO OBTAINMULTIPLYBYTO .033cm Hg at 0 Cin. Hg at 0 Clb/sq in.lb/sq ftkg/sq .28 lx 10in.1.136 x 101.829 x 105.080 x 101.934 x 1027.85135.95lb/sq in.lb/sq ftkg/sq m3.281 x 102.237 x 10mphft/lb1.383 x 10m-kg106.102 xl 02.642 x 10-4literscu in.U.S. galft-lb/min3.030 x 10hpft-lb/sec1.818 x 10hp2.832 x 1041,7283.704 x 107.48 128.32cu cmcu in.cu yardsU.S. galfluid oz829.6dramcu cm277.41.2014.546U.S. galliterscm Hgem/secondcu centimeterscu ftcu ft/mincu in.4.719 x 10-1*2.832 x 1016.39*1.639 x 10 '4.329 x 10 21.732 x km/hrcm/secknots1.09730.48.5925ft/secgal, Imperialliterscu in.liters/seccu m/mingal, U.S. drycu cmlitersU.S. galquartsgal, U.S. liquid268.81.556 x 101.1644.405cu in.cu ftU.S. gal liquidliterscu in.cu ft231.01.337 x 10cu meters1.30835.31264.2cu yards27.07.646 x 102.022 x 102cu ftcu metersU.S. gal-2deg(arc)1.745 x 10ISSUED: AUGUST 15, 19753.7858.327 x 101.280 x 10"litersgrams/cm0.126.721 x 105.601 x 10"kg/mlb/ftlb/in.grams/cu cm1,00062.43kg/cu mcu in.cu yardscu ftU.S. gal61,023metersyardsmilesnautical milesradiansImperial galfluid ozlb/cu ftREPORT: VB-7601-11
SECTION 1GENERALPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IIMULTIPLYBYTO 014m-kg/secmetric hphorsepower, metric75.09.863 x 10m-kg/sechpinches2.540'83.33 x 10ftin. Hg at 0 Ckilogramskg-calorieskg/cu mkg/sq cmkilometers"knotscu cm-2cu ftU.S. galImperial galquarts39.373.28 11.0946.214 x 10yardsmilesmeter-kilogram7.233ft-lbmeter/sec3.28 12.2373.600miles/hrkm/hrcmin.ftatmosphereslb/sq in.lb/sq ftkg/sq mft/secozgramsmicrons3.937 x 10in.308724.269 x 10ft-lbmilesm-kg52801.6098.690 x 10kmnautical miles62.43 x 1010 'lb/cu ftgrams/cu m1.4674.470 x 101.6098.690 x 10m/seckm/hrknotsmiles/hr sq2.151ft/sec sqmilibars2.953 x 102in. Hg at 0 Cnautical miles6076.11.1511852ftmilesmounces, fluid29.571.805cu cmcu in.lb/cu ft16.02kg/cu mlb/cu in.172827.68lb/cu ftgrams/cu cm14.222.048 x 1028.963.28 lx 106.214 x 105.400 x 48 x 101-1210'1031.853REPORT: VB-760TO OBTAINBY61.033.532 x 102.642 x 102.200 x 101.057lb10"km/hrlitersmeters3.342 x 10 '4.912 x l070.73,3.453 x 102.20535.27MULTIPLYlb/cu ftlb/sq ftin. Hg at 0 Cftmilesnautical milescentimetersft/secknotsmphm/secnautical mphft/secmphkm/hrm/secmphftft/secISSUED: AUGUST 15, 1975
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IIMULTIPLYSECTION 1GENERALTO OBTAINBYlb/sq in.2.0366.805 x 107.031 x 102in. Hg at 0 Catmosphereskg/sq mradians57.30deg (arc)radians/sec57.3015.92 x n1.047 x 10radians/secrod16.55.5ydslug32.174lbsq cm1.550 x 101.076 x 10sq in.sq ftsq ft929.0144.01.111 x 102.296 x 10deg/secft-1sq cmsq in.sq yardsacressq in.6.452sq cmsq kilometers3.861 x 10sq miles10.761.196sq ftsq yardssq miles2.590640sq kmacressq rods30.25sq ydsq yards8.361 x 109sq msq ftyards9.144 x 103.036.0meterssq metersISSUED: AUGUST 15, 1975ftin.REPORT: VB-7601-13
SECTION 1GENERALPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER HTHIS PAGE INTENTIONALLY LEFT BLANKREPORT: VB-7601-14ISSUED: AUGUST 15, 1975
TABLE OF CONTENTSSECTION -32-42-42-42-52-52-7REPORT: VB-7602-i
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IISECTION 2LIMITATIONSSECTION 2LIMITATIONS2.1GENERALThis section provides the "FAA Approved" operating limitations, instrumentand basic placards necessary for the safe operation of the airplane and its systems.Limitationsassociatedwith those optional systemssupplements can be found in Section 9 (Supplements).2.3andequipmentmarkings, color codingwhichrequirehandbookAIRSPEED LIMITATIONSSPEEDNever Exceed Speedany operation.CAS(VNE)-this speed inDo not exceed171 MPH(148 KTS)140 MPH(121 KTS)Design Maneuvering Speed (Vg) Do not make full orabrupt control movements above this speed.124 MPH(108 KTS)Maximum Flaps Extended Speed (VFE)this speed with the flaps extended.115 MPH(100 KTS)Maximum Structural Cruising Speed (VNo)exceed this speed except in smooth air andwith caution.Do notthen only--ISSUED: AUGUST 15, 1975-Do not exceedREPORT: VB-7602-1
CORPORATÎÒNPA-28-181, CHEROKEE ARCHER IIPIPER AIRCRAFTSECTION 2LIMITATIONS2.5AIRSPEED INDICATOR MARKINGSMARKINGCASRed Radial Line (Never Exceed)Yellow Arc (Caution Range Smooth Air Only)-171 MPH140 MPH(148 KTS)to 171 MPH(121 KTS to 148 KTS)2.7Green Arc (Normal Operating Range)68 MPH to 140 MPH(59 KTS to 121 KTS)White Arc (Flap Down)61 MPH to 115 MPH(53 KTS to 100 KTS)POWER PLANT LIMITATIONS(a) Number of Engines(b) Engine Manufacturer(c) Engine Model No.(d)(e)(f)(g)(h)(i)(j)(k)(1)Engine Operating Limits(1) Maximum Horsepower(2) Maximum Rotation Speed (RPM)(3) Maximum Oil TemperatureOil PressureMinimum (red line)Maximum (red line)Fuel PressureMinimum (red line)Maximum (red line)Fuel Grade (minimumoctane)Number of PropellersPropeller ManufacturerPropeller ModelPropeller DiameterMinimumMaximumPropeller Tolerance (static RPM at maximumpermissible throttle setting)1LycomingO-360-A4M withcarburetor setting 10-38781802700245 F25 PSI90 PSI.5PSI8 PSI100/130-Green1Sensenich76EM8S5-0-6076 IN.76 IN.Not above 2425 RPMNot below 2325 RPMNo additional tolerance permitted.REPORT:2-2VB-760ISSUED: AUGUST 15, 1975
SECTION 2LIMITATIONSPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER II2.9 POWER PLANT INSTRUMENT MARKINGS(a)(b)TachometerGreen Arc (Normal Operating Range)Red Line (Maximum Continuous Power)Oil TemperatureGreen Arc (Normal Operating Range)Red Line (Maximum)500 to 2700 RPM2700 RPM75 to 245 F245 F(c) Oil Pressure(d)60 PSI to 90 PSI25 PSI to 60 PSI25 PSI90 PSIGreen Arc (Normal Operating Range)Yellow Arc (Caution Range) (Idle)Red Line (Minimum)Red Line (Maximum)Fuel PressureGreen Arc (Normal Operating Range)Red Line (Minimum)Red Line (Maximum).5PSI to 8 PSIPSI8 PSI.52.11 WEIGHT LIMITS(a)(b)NORMAL2550 LBS200 LBSMaximum WeightMaximum BaggageUTILITY1950 LBS0 LBSNOTERefer to Section 5 (Performance)by performance.ISSUED: AUGUST 15, 1975for maximumweight as limitedREPORT: VB-7602-3
SECTION 2LIMITATIONSPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER H2.13 CENTER OF GRAVITY LIMITS(a) NormalCategoryWeightPoundsForward LimitRearward LimitInches Aft of DatumInches Aft of Datum25502050 (and less)88.682.093.093.0(b) UtilityCategoryWeightPounds1950(and less)Forward LimitRearward LimitInches Aft of DatumInches Aft of Datum82.086.5NOTESStraight line variation between points given.The datum used is 78.4 inches ahead of the wing leading edge atthe inboard intersection of the straight and tapered section.the responsibility of the airplane owner and the pilot to insurethat the airplane is properly loaded. See Section 6 (Weight andIt isBalance) for proper loading instructions.2.15 MANEUVER LIMITS(a) Normal Category All acrobatic maneuvers including spins prohibited.(b) Utility Category Approved maneuvers for bank angles exceeding 60 .--Steep TurnsLazy EightsChandellesEntry Speed124 MPH124 MPH124 MPH2.17 FLIGHT LOAD FACTORS(a) Positive Load Factor (Maximum)(b) Negative Load Factor (Maximum)REPORT: VB-7602-4NORMALUTILITY3.8 G4.4 GNo inverted maneuvers approvedISSUED: AUGUST 15, 1975
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IISECTION 2LIMITATIONS2.19 TYPES OF OPERATIONThe airplane is approved for the following operationsFAR 135.(a)(b)(c)(d)(e)when equippedin accordancewith FAR 91 orDay V.F.R.Night V.F.R.Day I.F.R.Night I.F.R.Non Icing2.21 FUEL LIMITATIONS(a) Total Capacity(b) Unusable Fuel50 U.S. GAL2 U.S. GAL(c)48 U.S. GALThe unusable fuel for this airplane has been determinedas 1.0 gallon in each wing in critical flight attitudes.Usable FuelThe usable fuel in this airplane has been determined as24.0 gallons in each wing.ISSUED: AUGUST 15, 1975REPORT: VB-7602-5
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IISECTION 2LIMITATIONSTHIS PAGE INTENTIONALLYREPORT: VB-7602-6LEFT BLANKISSUED: AUGUST 15, 1975
PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IISECTION 2LIMITATIONS2.23 PLACARDSIn full view of the pilot:"THIS AIRPLANE MUST BE OPERATED AS A NORMAL ORUTILITY CATEGORY AIRPLANE IN COMPLIANCE WITHTHE OPERATING LIMITATIONS STATED IN THE FORM OFPLACARDS, MARKINGS AND MANUALS.ALL MARKINGS AND PLACARDSAPPLY TO ITS OPERATIONAS AAIRPLANE.FOR NORMAL ANDOPERATIONS, REFER TO THEHANDBOOK.ON THIS TINGNO ACROBATICMANEUVERS ARE APPROVED FORNORMALCATEGORYOPERATIONS.SPINS AREPROHIBITEDFORBOTH NORMAL AND UTILITYCATEGORIES."In full view of the pilot, the following takeoff and landing check lists will be installed:TAKEOFFFuel on proper tankElectric fuel pump onEngine gauges checkedFlaps setCarb heat offCHECK LISTMixture setSeat backs erectFasten belts/harnessTrim tab set-Controls freeDoor latchedAir Conditioner----offLANDING CHECK LISTFuel on proper tankMixture richElectric fuel pump onThe "AIR COND OFF"conditioned aircraft only.ISSUED: AUGUST 15, 1975Flaps set (ll 5 mph)Fasten belts/harnessAir Conditioneroff-Seat back erect-item in the above takeoff and landingcheck lists is mandatoryfor airREPORT: VB-7602-7
SECTION 2PIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IILIMITATIONSIn full view ofinstalled:the pilot, in the area of the air conditionercontrol panel whenthe air conditionerisAIR CONDITIONER MUST BE OFF TO INSURE"WARNINGNORMAL TAKEOFF CLIMB PERFORMANCE."-Adjacent to upper door latch:"ENGAGE LATCH BEFORE FLIGHT."On inside of the baggage compartmentdoor:"BAGGAGE MAXIMUM 200 LBS"CATEGORY OPERATION NO BAGGAGE OR AFTPASSENGERS ALLOWED. NORMAL CATEGORY OPERATIONSEE PILOT'S OPERATING HANDBOOK WEIGHT ANDBALANCE SECTION FOR BAGGAGE AND AFT PASSENGERLIMITATIONS.""UTILITY--In full view of the pilot:"ROUGH AIR OR MANEUVERING SPEED"UTILITY CATEGORYALLOWED.""DEMONSTRATEDOn the instrumentOPERATION--124 MPH."NO AFT PASSENGERSCROSS WIND COMPONENT 20 MPH."-panel in full view of the pilot whenthe oil cooler winterizationkit is installed:"OIL COOLER WINTERIZATION PLATE TO BE REMOVEDWHEN AMBIENT TEMPERATURE EXCEEDS 50 F."In full view ofthe pilot:"UTILITY CATEGORY ONLY."ACROBATIC MANEUVERS ARE LIMITED TO THE FOLLOWING:ENTRY SPEED124 MPH124 MPH124 MPHSTEEP TURNSLAZY EIGHTSCHANDELLESOn the instrumentpanel in full view ofthe pilot:TURN OFF STROBE LIGHTS WHEN TAXIING"WARNINGIN VICINITY OF OTHER AIRCRAFT, OR DURING FLIGHTTHROUGH CLOUD, FOG OR HAZE."--REPORT: VB-72-8ISSUED: AUGUST 15, 1975
TABLE OF CONTENTSSECTION 3EMERGENCY .93.113.133.153.173.19Emergency Procedures Check ListAmplified Emergency Procedures 3-73-73-83-83-93-93-103-103-103-103-113-11REPORT: VB-7603-i
SECTION 3EMERGENCY PROCEDURESPIPER AIRCRAFT CORPORATIONPA-28-181, CHEROKEE ARCHER IISECTION 3EMERGENCY PROCEDURES3.1GENERALThe recommended procedures for coping with various types of emergencies and critical situations areprovided by this section. All of required (FAA regulations) emergency procedures and those necessary forthe safe operation of the airplane as determined by the operating and design features of the airplane arepresented.Emergency procedures associated with those optional systems and equipmentsupplements are provided by Section 9 (Supplements).which require handbookThe first portion of this section consists of an abbreviated emergency check list which supplies anaction sequence for critical situations with little emphasis on the operation of systems.The remainder of the section is devoted to amplified emergency procedures containinginformation to provide the pilot with a more complete understanding of the procedures.additionalThese procedures are suggested as the best course of action for coping with the particular conditiondescribed, but are not a substitute for sound judgment and common sense. Since emergencies rarely happenin modern aircraft, their occurrrence is usually unexpected and the best corrective action may not alwaysbe obvious. Pilots should familiarize themselveswith the procedures given in this section and be prepared totake appropriate action should an emergency arise.Most basic emergency procedures, such as power off landings, are a normal part of pilot training.Although these emergencies are discussed here, this information is not intended to replace such training,but only to provide a source of reference and review, and to provide information on procedures which arenot the same for all aircraft. It is suggested tha
PIPER AIRCRAFT CORPORATION SECTION 1 PA-28-181, CHEROKEE ARCHER II GENERAL SECTION 1 GENERAL 1.1 INTRODUCTION This Pilot's Operating Handbook is designed for maximum utilization as an operating guide for the pilot. It includes the material required to be furnished to the pilot by C.A.R. 3 and FAR Part 21, Subpart J. It a
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Pilot’s Operating Handbook And FAA Approved Airplane Flight Manual (abridged for KCN Aero Club) N49696 For complete information, consult Pilot’s operating Manual This abbreviated pilot’s handbook contains excerpts of the Cessna 152 Pilot’s Operating Handbook. Standard Temperature Chart added January 2, 2003 Performance - Specifications .
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Forecast Pilot Supply & Demand. 26 UND U.S. Airline Pilot Supply Forecast (2016) predicts cumulative pilot shortage of 14,000 by 2026. Boeing Pilot Outlook (2017) projects worldwide growth in pilot demand, with 117,000 pilots needed in North America by 2036. CAE Airline Pilot Demand Outlook (2017) indicates 85,000 new
Here are a few suggested references for this course, [12,15,1]. The latter two references are downloadable if you are logging into MathSci net through your UCSD account. For a proof that all p{ variation paths have some extension to a rough path see, [14] and also see [6, Theorem 9.12 and Remark 9.13]. For other perspectives on the the theory, see [3] and also see Gubinelli [7,8] Also see, [9 .
