PILOT'S OPERATING HANDBOOK
PILOT'S OPERATING HANDBOOK Cessna.SKY LANE1977 MODEL 182QSerial No ./G'Z.t,. 5 3 50Registration No . ) /7350VTHIS HANDBOOK INCLUDES THE MATERIALREQUIRED TO BE FURNISHED TO THE PILOTBY CAR PART 3COPYRIGHT 1976CESSNA AIRCRAFT COMPANYWICHITA , KANSAS , USA01087 - 13-RPC-300-2/92
CESSNAMODEL 182QLIST OF EFFECTIVE PAGESLIST OF EFFECTIVE PAGESNOTE:INSERT LATEST CHANGEDPAGES: DISPOSE OFSUPERSEDED PAGES.This handbook will be kept current by Service Letters published by-Cessna AircraftCompany. These are distributed t9 Cessna Dealers and to those who subscribethrough the Owner Follow-Up System. If you are not receiving subscription service,you will want to keep in touch with your Cessna Dealer for information concerningthe change status of the handbook. Subsequent changes should be examined immediately after receipt;. the handbook should not be used for operational purposesuntil it has been updated to a current status. On a changed page, the portion of thetext or illustration affected by the change is indicated by a vertical line in the outermargin of the page. Dates of issue for original and changed pages are:Original . . . 0 . . . 24 August 1976THE TOTAL NUMBER OF PAGES IN THIS HANDBOOK IS 262, CONSISTING OF THEFOLLOWING. THIS TOTAL INCLUDES THE SUPPLEMENTS PROVIDED IN SECTION9 WHICH COVER OPTIONAL SYSTEMS AVAILABLE IN THE AIRPLANE.,PageNo.Title.A.i thru iiiiv Blank1-1 thru 1-82-12-2 Blank2-3 thru 2-112-12 Blank .3-1 thru 3-153-16 Blank .4-1 thru 4-225-15-2 Blank5-3 thru 5-27#ChangeNo.0000000000-000 \00PageNo.5-28 Blank6-16-2 Blank6-3 thru 6-136-14 Blank .6-15 thru 6-247-1 thru 7-397-40 Blank8-18-2 Blank&-3 thru 8-149-1 thru 9-2Supplements (90 Pages)(Refer to Section 9 Table ofContents for Optional SystemsSupplements)# Zero in this column indicates an original page.A#ChangeNo.0000000000000!J. .-.,,--')
CESSNAMODEL 182QrCONGRATULATIONSCONGRATULATIONS .Welcome to the ranks of Cessna owners! Your Cessna has been designed and constructedto give you the most in performance, economy, and comfort. It is our desire that you will findflying it, either for business or pleasure, a ·pleasant and profitable experience.This Pilot's Operating Handbook has been prepared as a guide to help you get the mostpleasure and utility from your airplane. It contains information about your Cessna's equipment, operating procedures, and performance; and suggestions for its.servicing and care. Weurge you to read it from cover ·to cover, and to refer to it frequently.Our interest in your flying pleasure has not ceased with your purchase of a Cessna. Worldwide, the Cessna Dealer Organization backed by the Cessna Customer Services Departmentstands ready to serve you. The following services are offered by most Cessna Dealers: THE CESSNA WARRANTY, which provides coverage for parts and labor, is availableat Cessna Dealers worldwide. Specific benefits and provisions of warranty, plus otherimportant benefits for you, are contained in your Customer Care Program book, supplied with your airplane. Warranty service is available to you at authorized CessnaDealers throughout the world upon presentation of your Customer Care Card whichestablishes your eligibility under the warranty. FACTORY TRAINED PERSONNEL to provide you with courteous expert service .(" :-r · FACTORY APPROVED SERVICE EQUIPMENT to provide you efficient and accurateworkmanship.A STOCK OF GENUINE CESSNA SERVICE PARTS on hand when you need them .THE LATEST AUTHORITATIVE INFORMATION FOR SERVICING CESSNAAIRPLANES, since Cessna Dealers have all of the Service Manuals and PartsCatalogs, kept current by Service Letters and Service News Letters, published byCessna Aircraft Company.We urge all Cessna owners to use the Cessna Dealer Organization to the fullest.A current Cessna Dealer Directory accompanies your new airplane. The Directory isrevised frequently, and a current copy can be obtained from your Cessna Dealer. Makeyour Directory one of your cross-country flight planning aids; a warm welcome awaits youat every Cessna Dealer.·i
CESSNAMODEL 182QPERFORMANCESPECIFICATIONSPERFORMANCE- SPECIFICATIONS·)SPEED:Maximum at Sea Level . . . . . . . . .Cruise, 75% Power at 8000 Ft . . . . . .CRUISE: Recommended Lean Mixture with fuelengine start, taxi, takeoff, climb andreserve at 45% power.7 5% Power at 8000 Ft . .56 Gallons Usable Fuel75% Power· at 8000 Ft . . . .75 Gallons Usable FuelMaximum Range at 10,000 Ft56 Gallons Usable FuelMaximum Range at 10, 000 Ft75 Gallons Usable FuelRATE OF CLIMB AT SEA LEVELSERVICE CEILING . . . . .TAKEOFF PERFORMANCE:Ground Roll . . . . . .Total Distance Over 50-Ft ObstacleLANDING PERFORMANCE:Ground Roll . . . . . . . . . . .Total Distance Over 50-Ft ObstacleSTALL SPEED (CAS):Flaps Up, Power Off . .Flaps Down, Power Off .MAXIMUM WEIGHT . . . .STANDARD EMPTYWEIGHT:Skylane . . . . . . .Skylane II . . . . . .MAXIMUM USEFUL LOAD:Skylane . . . . . . .· Skylane II . . . . . .BAGGAGE ALLOWANCE . . .WING LOADING: Pounds/Sq FtPOWER LOADING: Pounds/HPFUEL CAPACITY: TotalStandard TanksLong Range Tanks .OIL CAPACITY . . . .ENGINE: Teledyne Continental230 BHP at 2400 RPMPROPELLER: Constant Speed, Diameter .ii. . . . . . 148 KNOTS. . . . . . 144 KNOTSallowance for45 minutesRangeTimeRangeTimeRangeTimeRangeTime520 NM3. 7 HRS735 NM5. 2 HRS640 NM5. 7 HRS910 NM8.1 HRS1010 FPM16,500 FT705FT1350 FT0'),)590FT1350 FT56 KNOTS50 KNOTS2950 LBS1717 LBS1781 LBS1233. LBS1169 LBS200 LBS16. 912. 861 GAL.80 GAL.12 QTS0-470-U82 IN.·)
CESSNAMODEL 182QTABLE OF CONTENTSTABLE OF CONTENTSSECTIONGENERAL .1LIMITATIONS2EMERGENCY PROCEDURES·,3NORMAL PROCEDURES .4PERFORMANCE . . . .5WEIGHT & BALANCE/EQUIPMENT LIST . . . . . . . . . . . . . 6AIRPLANE & SYSTEMSDESCRIPTIONS . . .AIRPLANE HANDLING,SERVICE & MAINTENANCE . . 7. . . . . . . 8SUPPLEMENTS(Optional Systems Description& Operating Procedures) . . . . . . . . . . 9iii/(iv blank)
CESSNAMODEL 182QSECTION 1GENERALSECTION ·1GENERALTABLE OF CONTENTSPageThree View·IntroductionDescriptive DataEngine·PropellerFuel . . .OilMaximum Certificated WeightsStandard Airplane Weights . .Cabin and Entry DimensionsBaggage Space and Entry DimensionsSpecific Loadings . . . . . . . . .Symbols, Abbreviations and TerminologyGeneral Airspeed Terminology and SymbolsMeteorological Terminology . . . . . . .Engine Power Terminology . . . . . . . .Airplane Performance and Flight Planning TerminologyWeight and Balance Terminology . . . . . . . . . . 1-71-7
CESSNAMODEL 182QSECTION 1GENERALMAX.11'-8" NOTES:1.Wing span shown with strobelights installed.2.Maxiinum height shown withnose gear depressed, all tiresand nose strut properly. inflatedand flashing beacon installed.3.Wheel base length is 66 1/2".4.Propeller ground clearanceis 10 7/8".5.Wing area is 174 square feet.6.Minimu'm .turning radius!*pivot point to outboardwing tip) is 27'.1-------------,----36'-0"-------------lFigure 1-1. Three View1-2;.,,-,· )
CESSNAMODEL 182QSECTION 1GENERALINTRODUCTIONThis handbook contains 9 sections, and includes the materia!"required to be furnished to the pilot. by CAR Part 3. It also contains supplemental data supplied by Cessna Aircraft Company.Section 1 provides basic data and information of general interest. Italso contains definitions or explanations of symbols, abbreviations, andterminology commonly used.DESCRIPTIVE DATAENGINE-- \! - 'Number of Engines: 1.Engine Manufacturer: Teledyne Continental.Engine Model Number: 0-470-U.Engine Type: Normally-a-spirated, direct-drive, air-cooled, horizontally-opposed, carburetor-equipped, six-cylind r engine with 470 cu.in. displacement.·Horsepower Rating and Engine Speed: 230 rated BHP at 2400 RPM.PROPELLERPropeller Manufacturer: McCauley Accessory Division.Propeller Model Number: C2A34C204/90DCB-8.Number of Blades: 2.·Propeller Diameter, Maximum: 82 inches.Minimum: 80.5 inches.Propeller Type: Constant speed and hydraulically actuated, with a lowpitch setting of 15.0 and a high pitch setting of 29.4 (30 inchstation).FUELApproved Fuel Grades (and Colors):100LL Grade Aviation Fuel (Blue).100 (Formerly 100/ 130) Grade Aviation Fuel (Green).1-3
CESSNAMODEL 182QSECTION 1GENERALFUel Capacity:Standard Tanks:Total Capacity: 61 gallons.Total Capacity Each Tank: 30. 5 gallons.Total Usable: 56 gallons.Long Range Tanks:Total Capacity: 80 gallons.Total Capacity Each Tank: 40 gallons.Total Usable: 75 gallons.NOTETo ensure maximum fuel capacity when refueling, placethe fuel selector valve in either LEFT or RIGHT position to prevent cross-feeding.OILOil Grade (Specification):MIL-L-6082 Aviation Grade Straight Mineral Oil: Use to replenishsupply during first 25 hours and at the first 25-hour oil change.Continue to use until a total of 50 hours has accumulated or oilconsumption has stabilized.NOTEThe airplane was delivered from the factory with a corrosion preventive aircraft engine oil. This oil should bedrained after the first 25 hours of operation.Continental Motors Specification MHS-24A, Ashless Dispersant Oil:This oil must be used after first 50 hours or oil consumption hasstabilized.Recommended Viscosity For Temperature Range:SAE 50 above 4 C (40 F).SAE 10W30 or SAE 30 below 4 C (40 F).NOTEMulti-viscosity oil with a range of SAE 10W30 is recommended for improved starting in cold weather.Oil Capacity:Sump: 12 Quarts.Total: 13 Quarts (if oil filter installed).1-4
CESSNAMODEL 182QSECTION 1GENERALMAXIMUM CERTIFICATED WEIGHTSTakeoff: 2950 lbs.Landing: 2950 lbs.Weight in Baggage CQmpartment:Baggage Area "A II (or passenger on child's seat)-Station 82 to 108:120 lbs. · See note below.Baggage Area "B" and Hatshelf-Station 108 to 136: , 80 lbs. Seenote below.NOTEThe max mum combined weight capacity -for baggageareas A and. B, including the hatshe1f, is 200 lbs. Themaximum hatshelf load is 25 lbs.STANDARD AIRPLANE WEIGHTSStandard Empty Weight, Skylane:Skylane II:Maximum Useful Load, Skylane:Skylane II:1717 Ibs.1781 lbs.1233 lbs.1169 lbs.CABIN AND ENTRY DIMENSIONSDetailed dimensions of the cabin interior and entry door openings areillustrated in Section 6.BAGGAGE SPACE AND ENTRY DIMENSIONSDimensions of the baggage area and baggage door opening are illustrated in detail in Section 6. .LI.SPECIFIC LOADINGSWing Loading:16. 9 lbs./ sq. ft Power Loading: 12. 8 lbs./hp.1-5
CESSNAMODEL 182QSECTION 1GENERALSYMBOLS, ABBREVIATIONS AND TERMINOLOGYGENERAL AIRSPEED TERMINOLOGY AND SYMBOLSKCASKnots Calibrated Airspeed is indicated airspeed correctedfor position and instrument error and expressed in knots.Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea level.KIASKnots Indicated Airspeed is the speed shown on the airspeedindicator and expressed in knots.KTASKnots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitudeand temperature.Maneuvering Speed is the maximum speed at which you may .use abrupt control travel.·Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position.VNOMaximum Structural Cruising Speed is the speed that shouldnot be exceeded except in smooth air, then only with caution.VNENever Exceed Speed is the speed limit that may not be exceeded at any time.Stalling Speed or the minimum steady flight speed at whichthe airplane is controllable . Stalling Speed or the minimum steady flight speed at whichthe airplane is controllable in the landing configuration atthe most forward center of gravity.Best Angle-of-Climb Speed is the speed which results in thegreatest gain of altitude in a given horizontal distance.VyBest Rate-of-Climb Speed is the speed which results in thegreatest gain in altitude in a given time.METEOROLOGICAL TERMINOLOGYOATOutside Air Temperature is the free air static temperature.It is expressed in either degrees Celsius (formerly Centi-grade) or degrees Fahrenheit.1-6
CESSNAMODEL 182QSECTION 1GENERALStandardTemperatureStandard Temperature is 15 C at sea level pressure altitudeand decreases by 2 C for each 1000 feet of altitude.PressureAltitudePressure. Altitude is the altitude read. from an altimeterwhen the altimeter's barometric scale has been set to 29.92inches of mercury (1013mb).ENGINE POWER TERMINOLOGYBHPBrake Horsepower is the power developed by the engine.RPMRevolutions Per Minute is engine speed.MPManifold Pressure is a pressure measured in the engine'sinduction system and is expressed in inches of mercury (Hg).AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGYDemonstratedCrosswindVelocityr Demonstrated Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplaneduring takeoff artd landing was actually demonstrated duringcertification tests. The value shown is not considere.d to belimiting.Usable Fuel Usable Fuel is the fuel available for flight planning.UnusableFuelUnusable Fuel is the quantity of fuel that can not be safelyused in flight.GPHGallons Per Hour is the· amount of fuel (in gallons) consumedper hour.NMPGNautical Miles Per Gallon is the distance (in nautical miles)which can be expected per gallon of fuel consumed at a specific engine power setting and/or flight configuration.g[is acceleration due to gravity.\.WEIGHT AND BALANCE TERMINOLOGYReferenceDatumReference Datum is an imaginary vertical plane from whichall horizontal distances are measured for balance purposes.StationStation is a location along the irplane fuselage given interms of the distance from the reference datum.1-7
SECTION 1GENERALCESSNAMODEL 182QArmArm is the horizontal distance from the reference datum tothe center of gravity (C. G.) of an item.MomentMoment is the product of the weight of an item multiplied byits arm. (Moment divided by the constant 1000 is used inthis handbook to simplify balance calculations by reducingthe number of digits. )Center ofGravity(C. G.)Center of Gravity is the point at which an airplane, or equipment, would balance if suspended. Its distance from thereference datum is found by dividing the total moment by thetotal weight of the airplane.e.G.Center of Gravity Arm is the arm obtained by adding theairplane's individual moments and dividing the sum by thetotal weight.Arme.G.LimitsCenter of Gravity Limits are the extreme center of gravitylocations within which the airplane must be operated at agiven weight.StandardEmptyWeightStandard Empty Weight is the weight of a standard airplane,including unusable fuel, full operating fluids and full engineoil.Basic Empty Basic Empty Weight is the standard empty weight plus theWeightweight of optional equipment.UsefulLoadUseful Load is the difference between takeoff weight and thebasic empty weight.Gross(Loaded)WeightGross (Loaded) Weight is the loaded weight of the airplane.·MaximumTakeoffWeightMaximum Takeoff Weight is the maximum weight approvedfor the start of the takeoff run.MaximumLandingWeightMaximum Landing Weight is the maximum weight approvedfor the landing touchdown.TareTare is the weight of chocks, blocks, stands, etc. used whenweighing an airplane, and is included in the scale readings.Tare is deducted from the scale reading to obtain the actual(net) airplane we ght.1-8-.11
CESSNAMODEL 182QSECTION 2LIMITATIONSSECTION 2LIMITATIONSTABLE OF CONTENTSPage\,.,.,.,'-'Introduction . . . . . . . .Airspeed Limitations . . . .Airspeed Indicator MarkingsPower Plant Limitations . .Power Plant Instrument MarkingsWeight Limits . . . . . .Center of Gravity Limits .Maneuver Limits . . . . .Flight Load Factor LimitsKinds of Operation LimitsFuel LimitationsPlacards . . . . . . . .2-3.2-42-42-52-62-62-72-72-72-72-82-92-1/(2-2 blank)
CESSNA·MODEL 182QSECTION 2LIMITATIONSINTRODUCTIONSection 2 includes operating limitations, instrument markings, andbasic placards necessary for the safe operation of the airplane, its engine, standard systems and standard equipment. The limitations includedin this section have been approved by the Federal Aviation Administration.When applicable, limitations associated with optional systems or equip-'ment are included tn Section 9.NQTEThe ai:rspeeds listed in the Airspeed Limitations chart(figure 2-1) and the Airspeed Indicator Markings chart(figure 2-2) are based on Airspeed Calibrationdatashown in Section '5 with the normal·static source. If thealternate static source is being used, ample marginsshould be observed to allow for the airspeed calibration·var1ations between the normal and alternate staticsources as shown·iri Section 5.·Your Cessna is certificated under FAA Type Certificate No. 3A13 asCessna Model No. 182Q.2-3
CESSNAMODEL 182QSECTION 2LIMITATIONSAIRSPEED LIMITATIONSAirspeed limitations and their operational significance are shown infigure 2-1.SPEEDKCASKIASREMARKSVNENever Exceed Speed172179Do not exceed this speed inany operation.VNOMaximum StructuralCruising Speed139143Do not exceed this speedexcept in smooth air, andthen only with caution.VAManeuvering Speed:2950 Pounds2450 Pounds1950 Pounds109998911110089Do not make full or abruptconi:rol movements abovethis speed.Maximum Flap ExtendedSpeed:To 10 Flaps10 - 40 Flaps1379514095Do not exceed these speedswith the given flap settings.172179Do not exceed this speed withwindows open.VFEMaximum Window OpenSpeedFigure 2-1. Airspeed LimitationsAIRSPEED INDICATOR MARKINGSAirspeed indicator .markings and their color code significance areshown in figure 2-2.2-4
CESSNAMODEL 182QSECTION 2LIMITATIONSMARKINGKIAS VALUEOR RANGEWhite Arc45-95Green 'Arc48- 143Yellow ArcRed LineSIGNIFICANCEFull Flap Operating Range. Lowerlimit is maximum weight v5 inlanding configuration. Uppe limitis maximum speed permissible with- flaps extended.Normal Operating Range. Lower limitis maximum weight v5 at most forwardC.G. with flaps retracted. Upper limitis maximum structural cruisin J speed.143- 179Operations must be conducted withcaution and only in smooth air.179Maximum speed for all operatipns.Figure 2-2. Airspeed Indicator MarkingsPOWER PLANT LIMITATIONSEngine Manufacturer: Teledyne Continental.Engine Model Number: 0 470-U.Engine Operating Limits for Takeoff and Continuous Operations: Maximum Power: 230 BHPMaximum Engine Speed: 2400 RPM.Maximum Cylinder Head Temperature: 238 C (460 F).Maximum Oil Temperature: 116 C (240 F).Oil Pressure, Minimum: 10 psi.Maximum: 100 psi.Propeller Manufacturer: McCauley Accessory·DivisionPropeller Model Number: C2A34C204/90DCB-8.Propeller Diameter, Maximum: 82 inches.Minimum: 80.5 ·inches.Propeller Blade Angle at 30 Inch Station, Low: 15.0 ;. High: 29.4 .2-5
CESSNAMODEL 182QSECTION 2LIMITATIONSPOWER PLANT INSTRUMENT MARKINGSPower plant instrument markings and their color code significanceare shown in figure 2-3.·RED LINEGREEN ARCYELLOW ARCRED LIMITTachometer- - -21002400 RPM- --2400 RPMManifold Pressure-- -15-23in. Hg-- ----Oil Temperature- - -100 - 240 F- - -240 FCylinder HeadTemperature- - -200 - 460 F-- -460 F10 psi30-60 psi-- -100 psi- - --- --15 to 5 C-- -INSTRUMENTOil PressureCarburetor AirTemperatureFigure 2-3.Power Plant Instrument MarkingsWEIGHT LIMITSMaximum Takeoff Weight: 2950 lbs.Maximum Landing Weight: 2950 lbs.Maximum Weight in Baggage Compartment:Baggage Area "A" (or passenger on child's seat) Station 82 to 108: 120 lbs. See note below.Baggage Area "B" and Hatshelf Station.108 to 136: 80 lbs. See note below.NOTEThe maximum combined weight capacity for baggageareas A and B, including the hatshelf, is 200 lbs. Themaximum hatshelf load is 25 lbs.2-6
CESSNAMODEL 182QSECTION 2LIMITATIONSCENTER OF GRAVITY LIMITS Center of Gravity Range:Forward: 33. 0 inches aft of datum at 2250 lbs. or less, with straightline variation to 39. 5 inches aft of datum at 2950 lbs.Aft: 48. 5 inches aft of datum at all weights. ·Reference Datum: Front face of firewall.·MANEUVER LIMITSThis airplane is certificated in the normal category. The normalcategory is applicable to aircraft intended for non-aerobatic operations.These include any maneuvers incidenta
AIRPLANES, since Cessna Dealers have all of the Service Manuals and Parts Catalogs, kept current by Service Letters and Service News Letters, published by Cessna Aircraft Company. We urge all Cessna owners to use the Cessna Dealer Organization to the fullest. A current Cessna Dealer Directory accompanies your new airplane.
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 .
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
Jabiru Aircraft Pilot's Operating Handbook Model J120-C JP-FM-10 Revision: 0 1 2 28 Oct 2014 Page 5 of 72 0. INTRODUCTION 0.1 PILOT'S OPERATING HANDBOOK The POH handbook consists of the following: Basic POH The basic POH provides all the information, procedures and limitations required to operate the aircraft as a Light Sport Aircraft.
POH Pilot's Operating Handbook Pilot Information Manual These terms are inter-changeable and refer to the approved manufacturers handbook. Cessna most often uses the term Pilot's Operating Handbook, early manuals were called Owners Manual and legal texts often use the term AFM. A Pilot Information Manual is a new term, coined to
POH Pilot's Operating Handbook Pilot Information Manual These terms are inter-changeable and refer to the approved manufacturers handbook. Cessna most often uses the term Pilot's Operating Handbook, early manuals were called Owners Manual and legal texts often use the term AFM. A Pilot Information Manual is a new term, coined to
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
This checklist is a guide to coordinate Pilot Operating Handbook and STC data applicable to this particular aircraft only. The applicable Pilot Operating Handbook and STC installations remain the official documentation for this aircraft. The pilot in command is responsible for complying with all items in the Pilot Operating
This checklist is a guide to coordinate Pilot Operating Handbook and STC data applicable to this particular aircraft only. The applicable Pilot Operating Handbook and STC installations remain the official documentation for this aircraft. The pilot in command is responsible for complying with all items in the Pilot Operating
