Transcription
wArrior IIpa-28-161REFERENCE ONLYTHIS ELECTRONIC VERSIONOF THE POH ISNOT APPROVED TOREPLACE ANY OPERATINGINFORMATION REQUIREDBY THE REGULATIONS.pilot’soperatinghandbookandfaa approvedairplane flight manualairplane airplaneregist. no.serial no.pa-28-161report: vb-1180 faa approved by:ward evansd.o.a. no. so-1piper aircraft corporationdate of approval:augusT 13, 1982vero beach, floridafaa approved in normal and utility categories based on car 3. Thishandbook includes the material required to be furnished to the pilotby car 3 and constitutes the approved airplane flight manual and mustbe carried in the airplane at all times.
PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR IIwarningExtreme care must be exercised to limit the use ofthis handbook to applicable aircraft. This handbook is valid for use with the airplane identifiedon the face of the title page. Subsequent revisionssupplied by Piper Aircraft Corporation must beproperly inserted.Published byPUBLICATIONS DEPARTMENTIssued: August 13, 1982 1982-1985,1988,1990,2005, 2015Piper Aircraft CorporationAll Rights ReservedREPORT: VB-1180iiISSUED: AUGUST 13, 1982REVISED: July 17, 2015
APPLICABILITYAPPLICABILITYApplication of this handbook is limited to the specific Piper PA-28-161model airplane designated by serial number and registration number on the faceof the title page of this handbook.Application of this handbook is limited to the specific Piper PA-28-161model airplane designated by serial number and registration number on the faceof the title page of this handbook.This handbook cannot be used for operational purposes unless kept in acurrent status.This handbook cannot be used for operational purposes unless kept in acurrent status.WARNINGWARNINGINSPECTION, MAINTENANCE AND PARTS REQUIREMENTSFOR ALL NON-PIPER APPROVED STC INSTALLATIONS ARENOT INCLUDED IN THIS HANDBOOK. WHEN A NON-PIPERAPPROVED STC INSTALLATION IS INCORPORATED ON THEAIRPLANE, THOSE PORTIONS OF THE AIRPLANE AFFECTEDBY THE INSTALLATION MUST BE INSPECTED INACCORDANCE WITH THE INSPECTION PROGRAMPUBLISHED BY THE OWNER OF THE STC. SINCE NON-PIPERAPPROVED STC INSTALLATIONS MAY CHANGE SYSTEMSINTERFACE, OPERATING CHARACTERISTICS ANDCOMPONENT LOADS OR STRESSES ON ADJACENTSTRUCTURES, PIPER PROVIDED INSPECTION CRITERIA MAYNOT BE VALID FOR AIRPLANES WITH NON-PIPER APPROVEDSTC INSTALLATIONS.INSPECTION, MAINTENANCE AND PARTS REQUIREMENTSFOR ALL NON-PIPER APPROVED STC INSTALLATIONS ARENOT INCLUDED IN THIS HANDBOOK. WHEN A NON-PIPERAPPROVED STC INSTALLATION IS INCORPORATED ON THEAIRPLANE, THOSE PORTIONS OF THE AIRPLANE AFFECTEDBY THE INSTALLATION MUST BE INSPECTED INACCORDANCE WITH THE INSPECTION PROGRAMPUBLISHED BY THE OWNER OF THE STC. SINCE NON-PIPERAPPROVED STC INSTALLATIONS MAY CHANGE SYSTEMSINTERFACE, OPERATING CHARACTERISTICS ANDCOMPONENT LOADS OR STRESSES ON ADJACENTSTRUCTURES, PIPER PROVIDED INSPECTION CRITERIA MAYNOT BE VALID FOR AIRPLANES WITH NON-PIPER APPROVEDSTC INSTALLATIONS.REVISED: MARCH 1, 2005REPORT: VB-1180iiiREVISED: MARCH 1, 2005REPORT: VB-1180iii
REVISIONSREVISIONSThe information compiled in the Pilot’s Operating Handbook, with theexception of the equipment list, will be kept current by revisions distributedto the airplane owners. The equipment list was current at the time theairplane was licensed by the manufacturer and thereafter must be maintainedby the owner.Revision material will consist of information necessary to update the textof the present handbook and/or to add information to cover added airplaneequipment.The information compiled in the Pilot’s Operating Handbook, with theexception of the equipment list, will be kept current by revisions distributedto the airplane owners. The equipment list was current at the time theairplane was licensed by the manufacturer and thereafter must be maintainedby the owner.Revision material will consist of information necessary to update the textof the present handbook and/or to add information to cover added airplaneequipment.I.RevisionsRevisions will be distributed whenever necessary as complete pagereplacements or additions and shall be inserted into the handbook in accordancewith the instructions given below:1. Revision pages will replace only pages with the same page number.2. Insert all additional pages in proper numerical order within eachsection.3. Page numbers followed by a small letter shall be inserted in directsequence with the same common numbered page.I.II. Identification of Revised MaterialRevised text and illustrations shall be indicated by a black vertical line alongthe outside margin of the page, opposite revised, added or deleted material. Aline along the outside margin of the page opposite the page number will indicatethat an entire page was added.Black lines will indicate only current revisions with changes and additionsto or deletions of existing text and illustrations. Changes in capitalization,spelling, punctuation or the physical location of material on a page will notbe identified by symbols.II. Identification of Revised MaterialRevised text and illustrations shall be indicated by a black vertical line alongthe outside margin of the page, opposite revised, added or deleted material. Aline along the outside margin of the page opposite the page number will indicatethat an entire page was added.Black lines will indicate only current revisions with changes and additionsto or deletions of existing text and illustrations. Changes in capitalization,spelling, punctuation or the physical location of material on a page will notbe identified by symbols.ORIGINAL PAGES ISSUEDThe original pages issued for this handbook prior to revision are givenbelow:ORIGINAL PAGES ISSUEDThe original pages issued for this handbook prior to revision are givenbelow:Title, ii through vii, 1-1 through 1-10, 2-1 through 2-9, 3-1 through3-16, 4-1 through 4-25, 5-1 through 5-29, 6-1 through 6-17, 7-1 through 7-26,8-1 through 8-18, 9-1 through 9-72 and 10-1 through 10-2.Title, ii through vii, 1-1 through 1-10, 2-1 through 2-9, 3-1 through3-16, 4-1 through 4-25, 5-1 through 5-29, 6-1 through 6-17, 7-1 through 7-26,8-1 through 8-18, 9-1 through 9-72 and 10-1 through 10-2.REPORT: VB-1180ivREPORT: VB-1180ivREVISED: MARCH 1, 2005RevisionsRevisions will be distributed whenever necessary as complete pagereplacements or additions and shall be inserted into the handbook in accordancewith the instructions given below:1. Revision pages will replace only pages with the same page number.2. Insert all additional pages in proper numerical order within eachsection.3. Page numbers followed by a small letter shall be inserted in directsequence with the same common numbered page.REVISED: MARCH 1, 2005
PILOT'S OPERATING HANDBOOK LOG OF REVISIONSCurrent Revisions to the PA- 28-161 Warrior II Pilot's Operating Handbook, REPORT: VB-1180 issued August 13, 1982.RevisionNumber 8)RevisedPages4-21,4-225-186-57-10Revised para. 4.27.Deleted MEA.Added GAMA placardRevised para. 6.7.Revised page top.Revised para. 7.33.Revised para. 8.3.Revised para. 8.5.1-31-6,1-72-22-63-1Revised para. 1.7.Revised para. 1.19 (b).4-44-64-134-144-15LJcuJ.Revised fig. 5-15.Revised fig. 6-3.Revised para. 7.15.1-82-96-116-167-238-28-3,8-44-5FAA ApprovalSignature andDateDescription of RevisionsOct. 15, 1982Ward Evansw July 15, 1983Ward EvansRevised para. 2.7.Revised para. 2.23.Revised para. 3.1.Revised procedures.Revised procedure; movedinfo. to pg. 4-6.Relocated info. from pg. 4-5.Revised para. 4.9.Revised para. 4.9; moved info.to pg. 4-15.Relocated info. from pg. 4-14.REPORT: VB-1180v
PILOT'S OPERATING HANDBOOK LOG OF REVISIONSRevisionNumber andCodeRev. 3 ,8-29-iRev.6(PR900228)Description of RevisionsRevised para. 7.7.Revised para. 7.13.Revised para. 7.15.Revised para. 8.21.FAA ApprovalSignature andDateLJ Ward EvansJune 28, 1984Revised para. 7.15Revised para. 7.26Added Supplement 8(Aux. Vacuum System)Revised fig. 5.23example.Revised para. 8.1.Added Supplement 8toT.O.C.p, JD.H.TromplerSept. 23, 1985J wD.H.TromplerAugust 11, 1988viAdded Rev. 6 to Log ofRevisions.7-24a& Added pages. Revisedpara. 7.35. Added7-24bNarco ELT 910 info.Revised para. 8.3.8-2&8-38-11Revised para's. 8.19 & 8.21.8-12Revised Fuel Grade Chart.J .D. H:rromJerMar. 2!2. 1290DateRev. 7(PR900912)V11-32-32-3aREPORT: VB-1180viAdded Rev. 7 to Log ofRevisions.Revised para. 1.5 (c).Revised para. 2.7 G) and (1).Added para. 2.7 (m). Movedinfo. to page 2-3a.Page added. Info. relocatedfrom page 2-3.
PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR IIpilot’s operating handbook log of revisionsRevisionNumber andRevisedDescription of RevisionsCodePagesRev. 7 (cont)2-3bPage added.7-2Revised para. 7.5.8-3Revised para. 8.5.D. H. TromplerOct. 8, 1990DateRev. dded Warning and movedinfo. to page iv.Moved info. from page iii.Added Rev. 8 to L of R.Revised para. 3.3.Revised para. 3.23.Corrected Issued date.Revised para. 7.15.Moved info. to page 8-1b andrevised para. 8.1.Added page andrevised para. 8.1.Added page and moved info.from pages 8-1 and 8-2.Moved info. to page 8-1b andrevised para. 8.3.Linda J. DickenMarch 1, 2005Rev. 9(PR150717)Added copyright info.Added Rev. 9 to L of R.Revised Para. 2.25.Revised Para. 8.1.Eric A. WrightJuly 17, 2015iivi-a2-88-1bISSUED: AUGUST 13, 1982REVISED: July 17, 2015FAA ApprovalSignature andDateREPORT: VB-1180vi-a
PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR IITHIS PAGE INTENTIONALLY LEFT BLANKREPORT: VB-1180vi-bISSUED: AUGUST 13, 1982
TABLE OF CONTENTSSECTION 1GENERALSECTION 2LIMITATIONSSECTION 3EMERGENCY PROCEDURESSECTION 4NORMAL PROCEDURESSECTION 5PERFORMANCESECTION 6WEIGHT AND BALANCESECTION 7DESCRIPTION AND OPERATION OFTHE AIRPLANE AND ITS SYSTEMSSECTION 8AIRPLANE HANDLING, SERVICINGAND MAINTENANCESECTION 9SUPPLEMENTSSECTION 10OPERATING TIPSREPORT: VB-1180vii
TABLE OF CONTENTSSECTION 71.9l.l11.131.151.171.19Introduction . .Engines . .Propellers . .Fuel . .Oil . .Maximum Weights . .Standard Airplane Weight . .Baggage Space . .Specific Loadings . .Symbols. Abbreviations and Terminology . .1-41-41-41-41-41-5REPORT: VB-11801-i
PIPER AIRCRAFT CORPORATIONPA-l8-16l ·WARRIOR IISECTION 1GENERALSECTION 1GENERAL1.1 INTRODUCTIONThis Pilot's Operating Handbook is designed for maximum utilizationas an operating guide for the pilot. It includes the material required to befurnished to the pilot by C.A.R. 3 and FAR Part 21, Subpart J. It alsocontains supplemental data supplied by the airplane manufacturer.This handbook is not designed as a substitute for adequate andcompetent flight instruction, knowledge of current airworthiness directives,applicable federal air regulations or advisory circulars. It is not intended tobe a guide for basic flight instructwn or a training manual and should not beused for operational purposes unless kept in a current status.Assurance that the airplan\! is in an airworthy condition is theresponsibility of the owner. The pilot in command is responsible fordetermining that the airplane is safe for flight. The pilot is also responsiblefor remaining within the operating limitations as outlined by instrumentmarkings, placards, and this handbook.Although the arrangement of this handbook is intended to increase itsin-flight capabilities, it should not be used solely as an occasional operatingreference. The pilot should study the entire handbook to familiarize himselfwith the liltlitations, performance, procedures and operational handling·characteristics of the airplane before flight.The handbook has been divided into numbered (arabic) sections, eachprovided with a "finger-tip" tab divider for quick reference. The limitationsand emergency procedures have been placed ahead of the normalprocedures, performance and other sections to provide easier access toinformation that may be required in ilight. The "t:.mergency Procedures"Section has been furnished with a red tab divider to present an instantreference to the section. Provisions for expansion of the handbook havebeen made by the deliberate omission of certain paragraph numbers, figurenumbers, item numbers and pages noted as being intentionally left blank.ISSUED: AUGUST 13, 1982REPORT: VB-11801-1
SECTION IGENERALPIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR II1-------------35'-------------jTHREE VIEWFigure l-lREPORT: VB-11801-2ISSUED: AUGUST 13, 1982
PIPER AIRCRAFT CORPORATIONPA·28·lfil, WARRIOR U1.3ENGINES(a)(b)(c)(d)(e)(t)(g)(b)(i)(J)1.5Number of EnginesEngine ManufacturerEngine Model NumberRated HorsepowerRated Speed (rpm)Bore (inches)Stroke (inches)Displacement (cubic inches)Compression RatioEngine Type1Lycoming0-320-D2A or 0-320-D3G16027005.1253.875319.88.5:1Four Cylinder, Direct Drive,Horizontally Opposed,Air CooledPROPELLERS(a) Number of Propellers(b) Propeller Manufacturer(c) Model(d) Number of Blades(e) Propeller Diameter (inches)(1) Maximum(2) Minimum(f) Propeller Type1.7SECTION 1GENERALSensenich74DM6-0-60 or74DM6-0-5827472Fixed PitchFUELAVGASONLY(a) Fuel Capacity (U.S. gal) (total)(b) Usable Fuel (U.S. gal) (total)(c) Fuel(1) Minimum Octane(2) Alternate FuelISSUED: AUGUST 13,1982REVISED: SEPTEMBER 12, 19905048100 Green or 1OOLL BlueAviation GradeRefer to Fuel Requirements,Section 8 - Handling, Servicingand Maintenance.REPORT: VB-11801-3I
SECTION 1GENERAL1.9PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR llOIL(a) Oil Capacity (U.S. quarts)(b) Oil Specification8Refer to latest issueof Lycoming ServiceInstruction 1014.(c) Oil Viscosity per Average AmbientTemp. for Starting(1) Above 60 F(2) 30 F to 90 F(3) 0 F to 70 FSingleS.A.E. 50S.A.E. 40S.A.E. 30(4) Below 10 FS.A.E. 20MultiS.A.E. 40 or 50S.A.E. 40S.A.E. 40 or20W-30S.A.E. 20W-301.11 MAXIMUM WEIGHTS(a)(b)(c)(d)Maximum Takeoff Weight (lbs)Maximum Ramp Weight (lbs)Maximum Landing Weight (lbs)Maximum Weight in BaggageCompartment (lbs)Normal244024472440200Utility20202027202001.13 STANDARD AIRPLANE WEIGHTSRefer to Figure 6-5 for the Standard Empty Weight and the UsefulLoad.1.15 BAGGAGE SPACE(a) Compartment Volume (cubic feet(b) Maximum Ramp Weight (lbs)(c) Maximum Landing Weight (lbs)2422201.17 SPECIFIC LOADINGS(a) Wing Loading (lbs per sq ft)(b) Power Loading (lbs per hp)REPORT: VB-11801-414.415.3ISSUED: AUGUST 13, 1982
PIPER AIRCRAFT CORPORATIONPA-28·161, WARRIOR IISECTION 1GENERAL1.19 SYMBOLS, ABBREVIATIONS AND TERMINOLOGYThe following definitions are of symbols, abbreviations and terminology used throughout the handbook and those which may be of addedoperational significance to the pilot.(a) General Airspeed Terminology and SymbolsCASCalibrated Airspeed means the indicatedspeed of an aircraft, corrected for positionand instrument error. Calibrated airspeedis. equal to true airspeed in standardatmosphere at sea level.KCASCalibrated Airspeed expressed in Knots.GSGround Speed is the speed of an airplanerelative to the ground.lASIndicated Airspeed is the speed of an aircraft as shown on the airspeed indicatorwhen corrected for instrument error. lASvalues published in this handbook assumezero instrument error.KIASIndicated Airspeed expressed in Knots.MMach Number is the ratio of true airspeedto the speed of sound.T ASTrue Airspeed is the airspeed of an airplanerelative to undisturbed air which is theCAS corrected for altitude, temperatureand compressibility.VAManeuvering Speed is the maximum speedat which application of full availableaerodynamic control will not overstress theairplane.VFEMaximum Flap Extended Speed is thehighest speed permissible with wing flapsin a prescribed extended position.ISSUED: AUGUST 13, 1982REPORT: VB-11801-5
SECTION 1GENERALV'\E/ M NEPIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR IINever Exceed Speed or MachNumber is the speed limit that shouldnot be exceeded at any time.Maximum Structural Cruising Speed is thespeed that should not be exceeded exceptin smooth air and then only with caution.VsStalling Speed or the minimum steadyflight ;;peed at which the airplane iscontrollable.VsoStalling Speed or the minimum steadyflight speed at which the airplane iscontrollable in the landing configuration.VxBest Angle-of-Climb Speed is the airspeedwhich delivers the greatest gain of altitudein the shortest possible horizontal distance.VYBest Rate-of-Climb Speed is the airspeedwhich delivers the greatest gain in altitudein the shortest possible time.(b) Meteorological Terminology!SAInternational Standard Atmosphere inwhich: The air is a dry perfect gas; Thetemperature at sea level is !5 Celsius (59 Fahrenheit); The pressure at sea level is29.92 inches Hg ( 1013.2 mb): The temperature gradient from sea level to the altitudeat which the temperature is -56.5 C(-69.7 f.') is -0.00198 C (-0.003564 F) perfoot and zero above that altitude.OATOutside Air Temperature is the free. airstatic temperature obtained either !rominflight temperature indications or groundmeteorological source . adjusted for instrument error and compressibility effects.REPORT: VB-11801-6ISSUED: AUGUST 13, 1982REVISED: JUNE 28, 1984
PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR II(C)SECTION 1GENERALIndicated PressureAltitudeThe number actually read rrom analtimeter when the barometric subscale hasbeen set to 29.92 inches of mercury { (Q 13.2 ·millibars).Pressure AltitudeAltitude measured from standard sea levelpressure {29.92 in. Hg) by a pressure orbarometric altimeter. It is the indicatedpressure altitude corrected for position: a.nctinstrument error. In this handbook.altimeter instrument errors are assumedto be zero.Station PressureActual atmosphericelevation.WindThe wind velocities recorded as variableson the charts of this handbook are to beunderstood as the headwind or tailwindcomponents of the reported winds.pressureatfield·Power TL·rminologyTakeoff PowerMaximum power permissible for takeoff.Maximum Continuous PowerMaximum power permissible continuouslyduring flight.Maximum ClimbPowerMaximumclimb.power permissible duringMaximum CruisePowerMaximumcruise.power permissible during{d) Engine I1HrumentsEGT l aug.:ISSUED: Al'Gl'S'f 13. 1982REVISED: Jl ;q: 28. 1984Exhaust Gas Temperature liaugeREPORT: VB-11801-7
SECfiON lGENERALPIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR II(e) Airplane Performance and Flight Planning TerminologyClimb GradientThe demonstrated ratio of the change inheight during a portion of a climb. to thehorizontal distance traversed in the sametime interval.DemonstratedCrosswindVelocityThe demonstrated crosswind velocity i thevelocity of the crosswind component forwhich adequate control of the airplaneduring takeoff and landing was actuallydemonstrated during certification tests.Accelerate-StopDistanceThe distance required to accelerate an airplane to a specified speed and, assumingfailure of an engine at the instant that speedis attained. to bring the airplane to a stop.Route SegmentA part of a route. Each end of that part isidentified by (I) a geographical locationor (2) a point at which a definite radio fixcan be established.(f) Weight and Balance TerminologyReference DatumAn imaginary vertical plane from which allhorizontal distances are measured forbalance purposes.StationA location along the airplane fuselageusually given in terms of distance from thereference datum.ArmThe horizontal distance from the referencedatum to the center of gravity (C.G.) of anitem.REPORT: VB-11801-8ISSUED: AUGUST 13, 1982REVISED: JULY 15, 1983
PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR IISECTION 1GENERALMomentThe product of the weight of an itemmultiplied by its arm. (Moment divided bya constant is used to simplify balancecalculations by reducing the number ofdigits.)Center of Gravity(C.G.)The point at which an airplane wouldbalance if suspended. Its distance from thereference datum is found by dividing thetotal moment by the total weight of theairplane.C.G. ArmThe arm obtained by adding the airplane'sindividual moments and dividing the sumby the total weight.C.G. LimitsThe extreme center of gravity locationswithin which the airplane must be operatedat a given weight.Usable FuelFuel available for flight planning.Unusable FuelFuel remaining after a runout test has beencompleted in accordance with governmental regulations.Standard EmptyWeightWeight of a standard airplane includingunusable fuel, full operating fluids and fulloil.Basic Empty.WeightStandard empty weight plus optionalequipment.PayloadWeight of occupants, cargo and baggage.Useful LoadDifference between takeoff weight, orramp weight if applicable, and basic emptyweight.Maximum RampWeightMaximum weight approved for groundmaneuver. (It includes weight of start, taxiand run up fuel.)ISSUED: AUGUST 13, 1982REPORT: VB-11801-9
SECTION 1GENERALMaximumTakeoff WeightMaximum weight approved for the startof the takeoff run.MaximumLanding WeightMaximum weight approved for the landingtouchdown.Maximum ZeroFuel WeightMaximum weight exclusive of usable fuelREPORT: VB-11801-10PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR IIISSUED: AUGUST 13, 1982
TABLE OF CONTENTSSECTION 2LIMITATIONSParagraphNo.PageNo.2.12.32.52. 72. 92.112.132.152. 62-62-7General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Airspeed Limitations.Airspeed Indicator Markings . , . . . . . . . . .Power Plant Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . .Power Plant Instrument Markings . . . . . . . . . . . . . . . . . .Weight Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Center of Gravity Limits.Maneuver Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Flight Load Factors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Kinds of Operation E4uipment List .·.Fuel Limitations . . . . . . . . . .Noise Levels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Placards . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .REPORT: VB-11802-i
PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR IISECTION 2LIMITATIONSSECTION 2LIMITATIONS2.1 GENERALThis section provides the "FAA Approved" operating limitations,instrument markings, color coding and basic placards necessary for·operation of the airplane and its systems.This airplane must be operated as a normal or utility category airplanein compliance with the operating limitations stated in the form of placardsand markings and those given in this section and handbook.·Limitations associated with those optional systems and equipmentwhich require handbook supplements can be found in Section 9 (Supplements).2.3 AIRSPEED LIMITATIONSSPEEDNever Exceed Speed (VNE) - Do notexceed this speed in any operation.KIASKCAS160153126122103100Maximum Structural Cruising Speed(VNo) - Do not exceed this speedexcept in smooth air and then onlywith caution.Maximum Flaps Extended Speed(VFE) - Do not exceed this speedw1th the tlaps extended.ISSUED: AUGUST 13, 1982REPORT: VB-11802-1
SECTION 2LIMITATIONSPIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR IISPEEDKIASDesign Maneuvering Speed (VA} Do not make full or abrupt controlmovements above this speed.At 2440 LBS. G.W.At 1531 LBS. G.W.Ill88KCAS10889CAUTIONManeuvering speed decreases at lighter weightas the effects of aerodynamic forces becomemore pronounced. Linear interpolation may beused for intermediate gross weights. Maneuvering speed should not be exceeded whileoperating in rough air.2.5 AIRSPEED INDICATOR MARKINGSKIASMARKINGRed Radial Lint: (Never Exceed)Yellow Arc (Caution Range -Smooth A;r Only)Green Arc (Normal Operating Range)White Arc (Flap Down)160126 lu 16050 to I2644 to 1032.7 POWER PLANT LIMITATIONSNumber of EnginesEngine ManufacturerLycoming0-320-D2A or 0-320-DJGEngine Model No.Engine Operating Limits(I) Maximum Horsepower160(2) Maximum Rotation Speed (RPM)2700(3) Maximum Oil Temperature24SO F(e) Oil PressureMinimum (n:d line)25 PSIMaximum (red line)100 PSI(f) Fuel Pres urcMinimum (n:d line).5 PSIMaximum (red line)g PSI(g) Fuel (AVGAS ONLY)(minimum rade}100 or IOOLL Aviation Grade(a)(b)(c)(d)REPORT: VB-ll802-2ISSUED: AUGUST 13, 1982REVISED: JUNE 28, 1984
PIPER AIRCRAFf CORPORATIONPA-28-161, WARRIOR II(h) Number of Propellers(i) Propeller ManufacturerG) Propeller ModelSECTION 2LIMITATIONS1Sensenich74DM6-0-60 or74DM6-0-58(k) Propeller DiameterMinimumMaximum(1) 74DM6-0-60 Propeller Tolerance(static rpm at maximum permissiblethrottle setting, Sea Level, ISA)72IN.74 IN.Not above 2430 RPMNot below 2330 RPMN01ERefer to the airplane maintenance manual for testprocedure to determine approved static rpmunder non standard conditions.(m) 74DM6-0-58 Propeller Tolerance(static RPM at maximum permissiblethrottle setting, Sea Level, ISA)Not above 2465 RPMNot below 2365 RPMN01ERefer to the airplane maintenance manual for testprocedure to determine approved static rpmunder non standard conditions.2.9POWER PLANT INSTRUMENT MARKINGS(a) TachometerGreen Arc (Normal Operating Range)Red Line (Maximum Continuous Power)(b) Oil TemperatureGreen Arc (Normal Operating Range)Red Line (Maximum)ISSUED: AUGUST 13, 1982REVISED: SEYfEMBER 12, 1990500 to 2700 RPM2700RPMREPORT: VB-11802-3I
SECTION2UMITATIONS2.9PIPERAIRCRAFf CORPORATIONPA-28-161, WARRIOR llPOWER PLANT INSTRUMENT MARKINGS (Continued)(c) Oil PressureGreen Arc (Nonnal Operating Range)Yellow Arc (Caution Range) (Idle)Yellow Arc (Ground Warm-Up)Red Line (Minimum)Red Line (Maximum)(d) Fuel PressureGreen Arc (Normal Operating Range)Red Line (Minimum)Red Line (Maximum)60 to90PSI25 to 60PSI90 to lOOPSI25PSI100 PSI.5 to 8 PSI.5PSI8PSI2.11 WEIGHT LIMITSNormal(a) Maximum Weight(b) Maximum Ramp Weight(c) Maximum Baggage2440LBS2447LBS200LBSUtility2020LBS2027 LBSOLBSNOTERefer to Section 5 (Performance) for maximumweight as limited by performance.REPORT: VB-11802-3aIISSUED: SEPTEMBER 12, 1990
PIPER AIRCRAFT CORPORATIONPA-28-161, WARRIORllSECTION 2LIMITATIONSTHIS PAGE INTENTIONALLY LEFT BLANKISSUED: SEPTEMBER 12, 1990REPORT: VB-11802-3bI
SECTION2LIMITATIONSPIPER AIRCRAFf CORPORATIONPA-28-161, WARRIOR II2.13 CENTER OF GRAVITY LIMITS(a) Nonnal CategoryWeightPoundsForward LimitInches Aft of DatumRearward LimitInches Aft of Datum88.383n93.093nForward LimitInches Aft of DatumRearward LimitInches Aft of Datum83.083.893.093.024401950 (and less)(b) Utility CategoryWeightPounds1950 (and less)2020NOTESStraight line variation between points given.The datum used is 78.4 inches ahead of the wingleading edge at the inboard intersection of thestraight and tapered section.It is the responsibility of the airplane owner andthe pilot to insure that the airplane is properlyloaded. See Section 6 (Weight and Balance) forproper loading instructions.2.15 MANEUVER LIMITS(a) Normal Category - All acrobatic maneuvers including spinsprohibited.(b) Utility Category- Approved Maneuvers for bank angles exceeding6()0:Steep TurnsLazy EightsChandellesREPORT: VB-11802-4Entry Speed111 KIAS111 KIAS111 KIASISSUED: AUGUST 13, 1982
SECTION 2LIMITATIONSPIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR II2.17 FLIGHT LOAD FACTORS(a) Positive Load Factor (Maximum)(b) Negative Load Factor (Maximum)UtilityNormal3.8 G4.4 GNo inverted maneuversapproved2.19 KINDS OF OPERATION EQUIPMENT LISTThis airplane may be operated in day or night VFR, day or night IFRwhen the appropriate equipment is installed and operable.The following equipment list identifies the systems and equipment uponwhich type certification for each kind of operation was predicated and mustbe installed and operable for the particular kind of operation indicated.However, certain operations may be authorized with certain listed equipment and/ or systems inoperative under certain conditions and underprovisions defined by a current Minimum Equipment List (MEL) approvedby the FAA which is dated concurrently with or after this Pilot's OperatingHandbook and FAA Approved Airplane Flight Manual and authorizedunder an operating regulation which provides for use of an MEL.(a) Day VFR(l) Airspeed indicator(2) Altimeter(3) Magnetic compass(4) Tachometer(5) Oil pressure indicator(6) Oil temperature indicator(7) Fuel pressure indicator(8) Fuel quantity indicator - each tank(9) Volt-ammeter(10) Elevator/ rudder trim indicator(11) Alternator( 12) Safety restraint - each occupant(b) Night VFR(I) All equipment required for Day VFR(2) Position lights(3) Instrument lights(4) Anti-collision (strobe) lightsISSUED: AUGUST 13, 1982REPORT: VB-11802-5
SECTION 2LIMITATIONSPIPER AIRCRAFT CORPORATIONPA-28-161, WARRIOR II(c) Day IFRAll equipment required for Day VFRVacuum pump(3) Gyro suction indicator( 1)(2)(d) Night IFR( 1) All equipment required for Day and Night VFR(2) All equipment required for Day IFRNOTEThe above system and equipment list does notinclude specific flight instruments and commu. nication/ navigation equipment required by theFAR Part 91 and 135 operating requirements.2.21 FUEL LIMITATIONS(a) Total Capacity(b) Unusable FuelThe unusable fuel for this airplane hasbeen determined as 1.0 gallon in eachwing in critical flight attitude-:.(c) Usable FuelThe usable fuel in this airplane has beendetermined as 24.0 gallons in each wing.50 U.S. GAL2 U.S. GAL48 U.S. GAL2.23 NOISE LEVELThe noise level of this aircraft is 72.9 dB(A).No determination has been made by the Federal Aviation Admini tration that the noise levels of this airplane are or should be acceptable orunacceptable for operation at. into, or out of, any airport.Th
pilot's operAting hAndbook And fAA Approved AirplAne flight mAnuAl faa approved in normal and utility categories based on car 3. this handbook includes the material required to be furnished to the pilot by car 3 and constitutes the approved airplane flight manual and must be carried in the airplane at all times. AirplAne AirplAne
