Beechcraft Musketeer Sport III A23-19 Pilot Operating Handbook Download

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Summary of Contents for Musketeer Sport III A23-19

Page 1: ...e granted by Raytheon Company Prior to March 26 2007 Beechcraft Corporation was owned by Raytheon Company but is no longer affiliated with Raytheon Company Beechcraft Corporation was formerly named Hawker Beechcraft Corporation from March 26 2007 until March 1 2013 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 2: ...U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 3: ... reach of the pilot during all flight operations This handbook includes the material required to be furnished to the pilot by CAR 3 Airplane Serial Number This handbook supersedes all BEECH published owner s manuals flight manuals and check lists issued for this airplane with the exception of FAA Approved Airplane Flight Manual Supplements COPYRIGHT BEECH 1994 PIN 169 590002 7 lssued October 1979 ...

Page 4: ... Publications BEECH AIRCRAFT CORPORATION Wichita Kansas 67201 i eechcraft Allllvlll Company U S A Member of GAMA Generał Aviation Manufacturera Aaaociation U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 5: ... al fllght operatlons Part Number SubJect Date 169 590002 7TC1 Fuel Selector Placard 8 26 97 lnetalistlon Note Thla page ahould be filed In the front of the Pllot s Operating Hsndbook snd FAA Approved A rp ans Fllght Manua lmmedlately fol lowlng the T7t e page Thla page raplacea any Log of Tamporary Changes page dated prlor to the data In the lower rlght carner of thla page 1 or 1 August 28 1997 U...

Page 6: ...U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 7: ...TING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL A2 Revision July 1994 LOG OF REVISIONS Paga Dascrlptlon Title Page Updated Page A A2 New 10 1 thru Revised Section X Safety 10 48 lnfonnation May 1994 rA2 PAGE A U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 8: ...U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 9: ...NG HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL A 1 Revision October 1990 LOG OF REVISIONS Page Description Title Page Updated Page A A1 New 10 1 thru Revised Section X 10 48 Safety lnformation October 1990 PAGE A U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 10: ...U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 11: ...iginal Page A Original a and b Original 1 1 thru 1 18 Original 2 1 thru 2 30 Original 3 1 thru 3 12 Original 4 1 thru 4 14 Original 5 1 thru 5 20 Original 6 1 thru 6 20 Original 7 1 thru7 28 Original 8 1 thru 8 46 Original Section 9 See Log of Supplements 10 1 thru 10 30 Original l A Page A U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 12: ...U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 13: ...s In recent years BEECHCRAFT handbooks contained most ot the data now provided however the new handbooks contain mote detailed data and some entirely new data For example attention is called to Section X SAFETY IN FORMATION While little ot the information is new and every pilot has been exposed to the basie fundamentals BEECHCRAFT feels it is highly important to have SAFETY INFORMATION in a conden...

Page 14: ...tions SECTION 3 Emergency Procedures SECTION 4 Normai Procedures SECTION 5 Performance SECTION 6 Weight and Balance Equipment List SECTION 7 Systems Description SECTION 8 Handling Servicing and Maintenance SECTION 9 Supplements SECTION 1O Safety lnformation b October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 15: ...1 8 Descriptive Data Engine 1 9 Propeller 1 9 Fuel 1 9 Oil Capacity 1 1 O Approved Oil Types 1 1 O Maximum Certificated Weights 1 1 O Cabin and Entry Dimensions 1 11 Baggage Space 1 11 Specific Loadings 1 11 Symbols Abbreviations and Terminology Genera l Airspeed 1 12 Meteorological 1 14 Power 1 15 Engine Controls and lnstruments 1 15 Airplane Performance and Flight Planning 1 16 Weight and Balanc...

Page 16: ...6L61 Jaqopo IN VlB l ł31 A 11VNOI1N31NI VGL 61 EZVJaalallsnw llllJOdS l łVł I JH l338 z L II Jaua 1 uo loas U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 17: ...ed Airplane Flight Manual andjor placards which are located in the airplane As a further reminder the owner and operator of this airplane should also be familiar with the Federal Aviation Regulations applicable to the operation and maintenance of the airplane and FAR Part 91 General Operating and Flight Rules Further the airplane must be operated and maintained in accordance with FAA Airworthiness...

Page 18: ...ssary documents may be maintained for the safe and efficient operation of the airplane The handbook has been prepared in loose leaf form for ease in maintenance and in a convenient size for storage The handbook has been arranged with quick reference tabs imprinted with the title of each section and contains ten basie divisions Section 1 General Section 2 Limitations Section 3 Emergency Procedures ...

Page 19: ... Revision Service applicable to this handbook eonsuit any BEECHCRAFT Aero or Aviation Center or International Distributor or Dealer or refer to the latest revision of BEECH CRAFT Service lnstructions No 0250 01 O BEECH AIRCRAFT CORPORATION EX PRESSLY RESERVES THE RIGHT TO SUPER SEDE CANCEL AND OR DECLARE 08 SOLETE ANY PART PART NUMBERS KITS OR PUBLICATION THAT MAY BE REFERENCED IN THIS HANDBOOK WI...

Page 20: ...able for installation on the BEECH CRAFT airplane Upon receipt of a new or revised supplement compare the Log page just received with the existing Log page in the manual Retain the Log page with the Jatest dateon the bott m of the page this log will usually have the greater number of entries and discard the other Jog VENDOR ISSUED STC SUPPLEMENTS When a new airplane is delivered from the factory t...

Page 21: ...BEECHCRAFT Sport III Musketeer A23 19 19A Section l General l8 0 1 32 9 j 6 2 DIAMETER AIRPLANE THREE VIEW October 1979 1 7 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 22: ...us for Wing Tip 23 ft 11 in Radiusfor Nose Wheel 9ft 10 in Radius for lnside Gear 2 ft O in Radius for Outside Gear 13 ft O in TURNING RADli ARE CALCULATED USING FULL STEER ING ONE BRAKE AND PARTlAL POWER 1 8 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 23: ...M6 0 58 fixed pitch twa blade propeller Static rpm at maximum permissible throttle settings Not over 2400 rpm and not under 2300 rpm No additional tolerance permitted Diameter 74 inches no cutoff permitted FUEL Aviation Gasoline 80 87 red minimum grade or 100LL blue or 100 green 59 8 gallon system 29 9 gallans each tank 58 8 gallans usable Each tank has provisions for partial filling to 20 gallans...

Page 24: ...ion Number 301 E approves for use lubricating oils which eonform to both MIL L 60828 straight minera type and MIL L 22851 ashless dispersant lubricants for airplane engines Refer to the Approved Engine Oils table in the HANDLING SERVICING AND MAINTENANCE section for a list of approved products MAXIMUM CERTIFICATED WEIGHTS NORMAL CATEGORY A23 19 Maximum Ramp Weight 2205 lbs Maximum Take Off Weight ...

Page 25: ...aximum Weight in Baggage Compartment 340 lbs CABIN AND ENTRY DIMENSIONS Length maximum 7 ft 11 in Height maximum 4ft O in Width maximum 3 ft 5 in Cabin Door 36 in wide by 38 in high BAGGAGE SPACE Compartment Volume 28 5 cu ft SPECIFIC LOADINGS 2200 lbs Wing Loading 15 07 lbsjsq ft Power Loading 14 67 lbsjhp SPECIFIC LOADINGS 2250 lbs Wing Loading 15 41 lbsjsq ft Power Loading 15 00 lbsjhp October ...

Page 26: ...rror Calibrated airspeed is equal to true airspeed in standard atmosphere at sea level GS Ground Speed is the speed ot an airplane relative to the ground lAS lndicated Airspeed is the speed of an airplane as shown on the airspeed indicator lAS values published in this handbook assume zero instrument error KCAS Calibrated Airspeed expressed in knots KlAS lndicated Airspeed expressed in knots TAS Tr...

Page 27: ...should not be exeeeded exeept in smooth air and then only with caution Stalling Speed or the minimum steady flight speed at which the airplane is controllable Stalling Speed or the minimum steady flight speed at whieh the airplane is eontroilabie in the Ianding eonfiguration Best Angle of Ciimb Speed is the airspeed whieh delivers the greatest gain of altitude in the shortest possible horizontal d...

Page 28: ... Temperatura is the free air static temperatura obtained either from inflight temperatura indica tions adjusted for instrument error and compressibility effects or ground meteorological sources The number actually read from an altimeter when the barometric sub scale has been set to 29 92 in Hg 1 013 2 millibars Altitude measured from standard sea level pressure 29 92 in Hg by a pressure or baromet...

Page 29: ...limited by time ENGINE CONTROLS AND INSTRUMENTS Throttle Control Mixture eontroi EGT Exhaust Gas Temperatura lndicator Tachorneter October 1979 Used to eontroi power by intro ducing fuel air mixture into the intake passages of the engine This eontroi is used to set fuel flow in all modes of operation and cuts off fuel completely for engine shut down This indicator is used to identify the lean and ...

Page 30: ... during take off and Iand ing was actually demonstrated during certification tests Minimum enroute IFR altitude A part of a route Each end of that part is identified by 1 a geograph ical location or 2 a point at which a definite radio fix can be established U S Gallans per hour Pounds per hour WEIGHT AND BALANCE TERMINOLOGY Reference Daturn Station 1 16 An imaginary vertical piane from which all h...

Page 31: ... would balance if suspended lts distance from the reference daturn is found by dividing the total moment by the total weight of the airplane The arm obtained by adding the air plane s individual moments and dividing the sum by the total weight The extreme center of gravity loca tions within which the airplane must be operated at a given weight Fuel available for flight planning Fuel remaining afte...

Page 32: ...euvering lt includes weight of start taxi and run up fuel Maximum weight approved for the start ot the take off run Maximum weight approved for the Ianding touchdown Weight exclusive of usable fuel The weight of chocks blocks stands etc used on the scales when weighing an airplane Those points which are used during the weighing process to level the airplane Points on the airplane identified by the...

Page 33: ... o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o 2 7 Center ot Gravity Limits o o o o o o o o o o o o o o o o o o o o o o o o o 2 7 Reference Daturn o o o o o o o o o o o o o o o o o o o o o o o o o o o 2 8 Maneuver Limits o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o 2 8 Flight Load Factors o o o o o o o o o o o o o o o o o o o o o o o o o o o o o o 2 9 Minimum Fligh...

Page 34: ... INY lB l ł31 A11 NOI N3 NI 6 L 6 L El J88 9 1SOII I III od s l ł H lH033B z z SU0 8 W 1 11 U0 09S U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 35: ...S Never Exceed 152 175 152 175 Do not exceed VNE this speed in any operation Maximum 133 153 134 154 Do not exceed Structural this speed Cruising except in smooth VNO or Vc air and then only with caution Maneuvering 116 133 115 132 Do not make fuli VA or abrupt eontroi movements above this speed Maximum 96 110 97 111 Do not extend Flap flaps or operate Extension with flaps ex Extended tended above...

Page 36: ...75 134 152 154 175 Operate With Arc Caution Only in Smooth Air Red 152 175 152 175 Maximum Line Speed For Ali Operations The limits of the arcs on the airspeed indicator are marked in CAS values POWER PLANT UMITATIONS ENGINE One Avco lycoming engine model 0 320 E28 0 320 E2C or 0 320 E3D engine rated at 150 hp Take aft and Maximum Continuous Power Fuli Throttle or 2700 rpm whichever occurs first 2...

Page 37: ...y Alcor Inc O L SPECIFICA T ONS Avco Lycoming Specification Number 301 E approves for use lubricating oils which eonform to both MIL L 60828 straight minera type and MIL L 22851 ashless dispersant lubricants for airplane engines Refer to the Approved Engine Oils table in the HANDLING SERVICING AND MAINTENANCE section for a list ot approved products PROPELLER SPECIFICATIONS Sensenich M74DM 0 58 or ...

Page 38: ...to 90 psi Maximum Pressure Red Line 100 psi FUEL PRESSURE Operating Range Green Arc 0 5 to 6 0 psi TACHOMETER Engine Warm up 800 to 1200 rpm Normai Operating Range Green Arc 2200 to 2700 rpm Maximum RPM Red Radial 2700 rpm MISCELLANEOUS INSTRUMENT MARKINGS INSTRUMENT AIR Operating Range Green Arc 4 3 to 5 9 in Hg FUEL GUANTITY After compliance with BEECHCRAFT S l No 0624 281 Yellow Band E to 3 8 f...

Page 39: ...Landing Weight 2250 lbs Zero Fuel Weight No Structural Limitation Maximum Baggage Compartment Load 340 lbs UliLITY CATEGORY A23 19 UTILITY ACROBATIC CATEGORY 19A Maximum Ramp Weight 2035 lbs Maximum Take off and Landing Weight 2030 lbs Zero Fuel Weight No Structural Limitation Maximum Baggage Compartment Load Utility Category Only 340 lbs CENTER OF GRAVITY LIMITS NORMAL CATEGORY A23 19 Forward 107...

Page 40: ...ft ot daturn at 2030 lbs Aft 114 0 inches aft ot daturn at all weights REFERENCE DATUM Daturn is 103 inches forward ot wing leading edge MAC length is 52 7 inches MANEUVER LIMITS The A23 19 and 19A airplane is approved for 4 place in the Normai Category and for 2 place in the Utility Category The 19A is also approved for 2 place in the Acrobatic Category Maximum slip duration is 30 seconds NORMAL ...

Page 41: ...Operating Handbook and FAA Approved Airplane Flight Manuał Supplement FLIGHT LOAD FACTORS NORMAL CATEGORY 2250 POUNDS 2200 POUNDS Flight maneuvering load tactors Flaps Up 3 8 1 9 Flaps Down 1 9 UTILITY CATEGORY 2030 POUNDS Flight maneuvering load tactors Flaps Up 4 4 2 2 Flaps Down 2 2 ACROBATIC CATEGORY 19A 2030 POUNDS Flight maneuvering load tactors Flaps Up 6 0 3 0 Flaps Down 2 0 MINIMUM FLIGHT...

Page 42: ...ure continued airworthiness lf deviations from the installed equipment were not permitted or if the operating rules did not provide for various flight conditions the airplane could not be flown unless all equipment was operable With appropriate limitations the operation of every system or component installed in the airplane is not necessary when the remaining operative instruments and equipment pr...

Page 43: ...lowing equipment requirements and exceptions are presented lt is the fina l responsibility of the pilot to determine whether the lack of or inoperative status of a piece of equipment on his airplane willlimit the conditions under which he may operate the airplane WARNING FLIGHT IN KNOWN ICING CONDITIONS PROHIBITED LEGEND Numbers refer to quantities required to be operative for a specified conditio...

Page 44: ...munications system ELECTRlCAL POWER Battery OC alternator VFR Day VFR Night IFR Day IFR Night Remarks andl or Exceptions Per FAR 91 33 Per FAR 91 33 1 1 1 1 1 1 1 1 l c 3 l o s o s Cli S a c m Cli m n I a l m CD c o l CD_ U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 45: ...ncy locator trans mitter FIRE PROTECTION Portable fire extinguisher Per Person or Per FAR 91 33 As required for acrobatic flight Per FAR 91 52 Optional S aJ c m en m 11 t CD JI ł en c Do l tD r 3 en CD g o l l 1 l U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 46: ...xceptions 1 1 1 1 May be inoperative for ferry flight provided tabs are visually checked in the neutral position prior to takeoff and checked for fuli range ot operation 1 1 1 1 May be inoperative provided flap travel is visually inspected prior to takeoff 1 1 1 1 l l c 3 o III O s o s en 3 a c m en m I l o 0 N n W t en CD C o t CD_ U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U...

Page 47: ...ve pro en vided other side is operational co o l and amount of fuel on board can co be established to be adequate l for the intended flight l l l l l Fuel pressure indicator ICE AND RAIN PROTECTION Emergency static Optional J r air source 3 en Pitot heater 1 1 Optional D o III o N l o o o s _ s J1 1 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 48: ... light Rotating beacon Position light VFR Day VFR Night IFR Day IFR Night Remarks andlor Exceptions Lights must be operative Per FAR 91 33 1 1 Optional 3 3 c 3 n l o t J o l III s tD c m III m I 0 N TI w ł Cfj ID C o l ID_ U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 49: ...tic compass 1 1 1 1 l Attitude indicator 1 1 Turn coordinator Directional gyro Clock Transpander l l l l l Per FAR 91 24 91 90 91 97 Navigation equipment Per FAR 91 33 VACUUM r Voouum sy em fo 1 1 l m n 1 Instrument a1r t o Vacuum gage 1 1 g 1 III U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 50: ... temperature indicator ENGINE OIL INSTRUMENTS Oil pressure indicator Oil temperature indicator VFR Day VFR Night IFR Day IFR Night Remarks andl or Exceptions 1 1 1 1 Optional 1 1 1 1 1 1 1 1 c 3 n III 0 e o III S o c m III m n t l n D l CD O o co_ U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 51: ...tanks in wings with a total of 52 2 gallons usable Value given is nominal Tank capacity will vary with temperatura and manufacturing tolerances FUEL MANAGEMiiNT Do not take off when the Fuel Ouantity Gages indicate in the Yellow Bandor with less than 11 gallonsin each main tank Maximum slip duration 30 seconds Yellow band was installed by BEECHCRAFT S l No 0624 281 October 1979 2 19 U N C O T R O ...

Page 52: ... WHIP STAllS I MAXIMUM ENTAY SPEEO 133 MPH 133 MPH 133 MPH SLOW OECElEAATION On Left Cabin Door ar Left Side Panel CAS MB 253 thru MB 288 2 20 THIS AIAPLANE MUST BE OPERATED IN COMPUANCE WITH THE OPERATING UMITATIONS STATEO IN THE FORM OF PLACAROS MAR ING S ANO MANUALS NORMAL CATEGORY MAXIMUM DESIGN WEIGHT RHER TO WEIGHT ANO BAtANCE DATA fOR LOAO NG INSTRUCTIONS FLIGHT MANEUVERtNG LOAD FACTDR MAXI...

Page 53: ... H NO A CROBATIC MANEUVERS IN GLUDING SPINS APPROVEO UliLITY CATEGOR Y MAXIMUM OESIGN Wf IGHT REFER TO WEIGHT ANO BALANCE DATA fO R LOAOING INSTRUCTIQNS FLIG I łf MANEUVERING LOAO FACTOR 2030 LBS FLAPS UP 4 4 2 2 DOWN 2 2 NO ACROBATIC MANEUVERS APPAOVED EXCEPT THOSE USTED BELOW MANEUve R M A xtMUM ENT Rv SPEEO CHANOHlES 133 MPH LAlY EIGI ITS 133 MPH STEEP TURNS 133 MPH STALLS IEXC EPT WI I IP STAl...

Page 54: ...ANCE DATA FOl LOAOING INSTIUCTIONS 2250 LBS li l ł 19 132 MPH 2030 LIS FLIGHT MANEUVUING lOAO FACTOit fLAPS UP 6 O 3 O DOWN 2 0 NO ACROBATIC MANEUVERS APPROVED EXCEPT THOSE LISlED BELOW MANEUVU MAXIMUM ENTU SPEED CHANDELlfS 133 MPH LAlY EIGHTS 133 MPH STEEP TUINS 133 MPH STALLS IEXCEPT WHIP STALLSI SLOW DECHEU TION NOTE MAXIMUM Al TITUDł LOSS DURING STAll 300 FT SPINS lfOI OPEIATIONAL LIMITATIONS ...

Page 55: ...RRYING OF BAGGAGE OR REAR SEAT PASSENGERS AND USE OF FLAPS PROHIBITED DURING ACROBATIC MANEUVERS On Left Cabin Door Model 19A MB 322 thru MB 454 ACROBATIC EMERGENCY EXIT TURN HANDLE CLOCKWISE KICK OUT TO JETIISON DOOR On Right Cabin Door Model 19A MB 322 thru MB 454 ACROBATIC EMERGENCY EXIT TURN HANDLE COUNTER CLOCKWISE KICK OUT TO JETIISON DOOR October 1979 2 23 U N C O T R O L L E D C O P Y N O ...

Page 56: ...tate towards the appłied rudder When the wings are 90 to the horizon apply fuli aileron against i e against t he intended direction oł spin The airplane will go slightly inverted and enter a normai spin Ił aileron againsi is not applied or applied too late the airplane will enter a rapid spiral dive and recovery musi be initi ated by the second turo lf the fuli back stick is not applied and held t...

Page 57: ... Fuel Selector Panel MB 1 thru MB 288 L TANK R TANK 29 GAL 29 GAL OFF Section 11 Limitations On Fue Selector Panel after compliance with BEECHCRAFT S No 0838 October 1979 2 25 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 58: ... 0624 281 DO N01 TAKE OH WHfN UH OUANTITT GAUGE tNOICATES IN YEUOW OR WITH USS THAN 11 G AllONSIN EACH MA IN TANK MAXIMUM SliP DURAllON IS 30 SECONOS On Upper Right Instrument Panel RAISE FLAPS To INCREASE BRAKE EFFECTIVENESS On Flap Extension Handle CAS FLAPS PULL TO EXTEND MAX SPEED 11O MPH RETRACTED oo FIRST NOTCH 15 SECOND NOTCH 25 THIRD NOTCH 35 2 26 October 1979 U N C O T R O L L E D C O P Y...

Page 59: ... 1 thru MB 460 Numbera Affected Descrlptlon of The addltlon of a placard to the fuel Chenge selector to warn of the no flow condltlon that exlsts between the fuel selector detents Filing lnetructlona lnsert thls ternporary change lnto the A23 19 and 19A Pllot s Operating Handbook and FAA Approved Alrplane Fllght Manual lmmedlately followlng page 2 26 Sectlon li LIMITATIONS and retaln untll resclnd...

Page 60: ...ve For Those Airplanes In Compliance With S B 2670 WARNING POSITION SELECTOR IN DETENTS ONLY NO FUEL FLOW TO ENGINE BETWEEN DETENTS Approved 2 of 2 tttŁLe A C Jackson Raytheon Aircraft Company DOA CE 2 P N 169 590002 7TC1 August 26 1997 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 61: ...AIRCRAFT LEVEL BAGGAGE COMPARTMENT FLOOR On Aft Cabin Bulkhead IEf BAGGAGE COMPARTMENT 340 POUNDS MAXIMUM CAPACITY l l l On Aft Cabin Bulkhead Optional with famiły seat installed HAT SHELF NO HEAVY OBJECTS October 1979 2 27 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 62: ...ALTIMETER EB EMERGENCY EB or o WAR N ING o EMERGENCY AIRSPEED STATIC SOURCE ON EMERGENCY SEE PILOTS CHECK LIST OR FLIGHT MANUAL c EMERGENCY PROCEDURES FOR AIRSPEED ALTIMETER CALIBRATlON ERROR 0 N0 AL O or EB WARNING EB EMERGENCY AIRSPEED STATIC SOURCE EMERGENCY ON SEE PILOTS CHECK liST i OR FLIGHT MANUAL OFF EMERGENCY PROCEDURES FOR AIRSPEED ALTIMETER NORMAL CALIBRATlON ERROR EB EB October 1979 _ ...

Page 63: ...rt III Musketeer A23 19 19A On Pedestal Between Front Seats October 1979 lo l g l N Oi N o s E l l l l u l p i L L ___ Section 11 Limitations 2 29 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 64: ...Section 11 Limitations 2 30 BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 65: ...ngine Power 3 5 Airstart Procedure 3 6 Engine Fire In Flight 3 6 On The Ground 3 7 Emergency Descent 3 7 Maximum Glide Configuration 3 7 Landing Emergencies Landing Without Power 3 8 Systems Emergencies Alternator Out Procedure 3 8 Unscheduled Electric Stabilator Trim 3 9 Emergency Static Air Source System 3 9 Unlatched Door In Flight 3 1 O Spins 3 10 Entry 3 1 O Spin Recovery 3 11 October 1979 3 ...

Page 66: ...Section III Emergency Procedures BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK 3 2 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 67: ...mation is presented to enable the pilot to form in advance a definite plan ot action for coping with the most probabie emergency situations which could occur in the operation ot the airplane Where practicable the emergencies requiring immediate corrective action are treated in check list form for easy reference and familiari zation Other situations in which more time is usually per mitted to decid...

Page 68: ...OOST switehes OFF 5 Magneto Start Switeh OFF AFTER LIFTOFF AND IN FLIGHT Landing straight ahead is usually advisable f sufficient a titude is available for maneuvering accomplish the fol owing 1 Mixture FULL RICH then LEAN as required 2 Fuel Boost Pump ON 3 Fuel Selector Valve SELECT OTHER TANK Check to feel detent and check visually 4 Magnetos CHECK LEFT and RIGHT then BOTH 3 4 NOTE The most prob...

Page 69: ...hen certain ot reaching the selected Ianding site 7 Airspeed 65 kts 75 mph 8 Flaps AS REQUIRED ENGINE DISCREPANCY CHEGKS CONDITION ROUGH RUNNING ENGINE 1 Mixture FULL RICH then LEAN as required 2 Magneto Start Switch CHECK LEFT and RIGHT then BOTH COND TION LOSS OF ENGINE POWER 1 Fuel Pressure Gage CHECK f fuel flow is abnormally low a Mixture FULL RICH b Fuet Boost Pump ON Lean as required c Fuel...

Page 70: ...ixture FULL RICH 4 Fuel Boost Pump ON until power is regained then OFF Leave on if engine driven fuel pump is inoperative 5 Throttle ADJUST to desired power 6 Mixture LEAN as required ENGINE FIRE IN FLIGHT The ventilation controls must be closed to shut off ali heat ing system outlets so that smoke and fumes will not enter the cabin The eontroi labeled CABIN AIR must be pulled out to close The con...

Page 71: ...uel Selector Valve Or F 2 Throttle CLOSED 3 Mixture IDLE CUT OFF 4 BATIERY ALT and Magneto Start Switches OFF 5 Extinguish with Fire Extinguisher EMERGENCY DESCENT 1 Throttle IDLE 2 Airspeed ESTABLISH 132 kts 153 mph MAXIMUM GLIDE CONFIGURATION 1 Flaps UP 2 Air speed 78 kt sj SO mph Glide distance Zero Wind Condition is approximately 1 7 nautical miles 2 statute miles per 1000 feet of altitude abo...

Page 72: ...RNATOR OUT PROCEDURE A failure of the alternator will place the entire electrical operation of the airplane on the battery Alternator failure will be indicated by a discharging or fluctuating ammeter lf this condition develops turn the AlT switch to OFF Turn off all nonessential electrical load to conserve the battery life 3 8 WARNING Deactivation of the battery alternator switch alternator switch...

Page 73: ...ty of obstructed static ports should be considered Partia obstructions will result in the rate of climb indication being sluggish during a climb or descent Verification of suspected obstruction is possible by switching to the emergency system and noting a sudden sustained change in rate of climb This may be accompanied by abnormal indicated airspeed and altitude changes beyond normai calibration d...

Page 74: ...ns are also prohibited in the Utility Category unless the airplane is approved for operation in the Acrobatic Category and has complied with BEECHCRAFT S l No 0871 090 The airplane will not spin if orthodox entry is used but will enter a spiral dive Speed builds rapidly in a spiral dive requiring high pullout loads Therefore if a spiral is inadvertently entered recovery from the spiral is to be in...

Page 75: ...i back stick is not applied and held the airplane may spiral Again recovery must be initiated not later than the second turn lf aileron is applied too early the airplane will not rotate and merely remain in a straight stalled condition SPIN RECOVERY From spins entered intentionally or inadvertently lmmediately move the eontroi column fuli forward and si multaneously apply fuli rudder opposite to t...

Page 76: ...Section III Emergency Procedures BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK 3 12 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 77: ...ore Taxi 4 8 Before Takeoff 4 8 Takeoff 4 9 Climb 4 10 Cruise 4 1 O Leaning Using the Exhaust Gas Temperature lndicator 4 1 O Descent 4 11 Before Landing 4 11 Balked Landing 4 12 After Landing 4 1 2 Shutdown 4 1 2 Environmental Systems 4 12 Heating and Ventilation 4 12 Cold Weather Operation 4 13 Preflight lnspection 4 1 3 Engine 4 1 3 lcing Conditions 4 14 Engine Break In lnformation 4 14 October...

Page 78: ...6L6 L Jaqoł Q z tr IN B 1 131 A 11VNOI 1N3 1NI 6 L 6 L E z J99ł llsnw III łJOdS 1 1Vkł0H033B saJnpa OJd teWJON Al UO ł l9S U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 79: ...aximum Climb Best Rate Vyl Best Angle Vxl Cruise Climb Maximum Turbulent Air Penetration Balked Landing Landing Approach Maximum Demonstrated Crosswind October 1979 65 Knots 75 mph 72 Knots 83 mph 72 Knots 83 mph 65 Knots 75 mph 89 Knots 100 mph 114 Knots 131 mph 58 Knots 67 mph 65 Knots 75 mph 13 Knots 15 mph 4 3 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 80: ...HECK b Tie Down REMOVE c Position Light CHECK 4 LEFT FUSELAGE a Static Pressure Button UNOBSTRUCTED b Ali Antennas CHECK 5 LEFT WING TRAJUNG EDGE a Flap CHECK b Fuel Vent Line UNOBSTRUCTED c Aileron CHECK d Wing Tip CHECK e Position Light CHECK 6 LEFT WING LEADING EDGE 4 4 a Pitot Tube CHECK Remove Cover b Landing Light CHECK c Tie Down and Chaeks REMOVE d Stall Warning CHECK for movement ot vane ...

Page 81: ...r CHECK e Engine Oil CHECK See Servicing Section 8 Cap and Dipstick SECURE f Right Cowl SECURE g Fuel Strainer DRAIN h Chaeks REMOVE 9 RIGHT LANDING GEAR a Fuel Sump DRAIN b Tire and Brake CHECK 1O RIGHT WING LEADING EDGE a Fuel Tank CHECK QUANTITY Filier Cap SECURE b Tie Down and Chaeks REMOVE c Wing Tip CHECK d Position Light CHECK 11 RIGHT WING TRAILING EDGE a Aileron CHECK b Flap CHECK c Fuel ...

Page 82: ...ARNIN G Do not take off if gages indicate in yellow arc on either gage airplanes after compliance with BEECHCRAFT S l No 0624 281 EXTER NAL POWER The following precautions shall be observed while using external power 1 The Battery Switch shall be ON and all avionics and electrical switches OFF This protects the voltage rag ulators and associated electrical equipment from volt age transients power ...

Page 83: ...ator Switch ON STARTING CAUTION Vernier type engine centrols should not be rotated clockwise after being advanced to the fuli forward position 1 Mixture FULL RICH 2 Throttle FAST IDLE position 3 Fuel Boost Pump ON coId weather starts use one to six strokes of engine prime as required CAUTION Starter cranking period should be limited to a maximum of 30 seconds with at least 2 minutes between cranki...

Page 84: ...mmeter CHECK CAUTION Charge indication should begin to decrease within 2 minutes after engine start and should be within 1 4 scale of zero prior to takeoff lf not an electrical difficulty is indicated and the airplane should be shut down 12 Throttle IDLE 13 Fuel Boost Pump OFF for test of engine driven pump then ON AFTER STARTING AND BEFORE TAXI 1 Parking Brakes RELEASE 2 Brakes RELEASE AND CHECK ...

Page 85: ... 11 Throttle FAST IDLE 12 Stabilator Trim TAKE OFF RANGE Green Band 13 Flaps CHECK and SET 14 Controls CHECK FREE and for proper direction of travel 15 Fuel Boost Pump CHECK ON 16 Mixture FULL RICH or as required by field elevation tighten friction on push pull type control 17 Doors and Window SECURE 18 Parking Brake RELEASE 19 lnstruments CHECK engine instruments in green range at the start of th...

Page 86: ...ower or less the EGT unit should be used in the following manner 1 Lean the mixture and note the point on the indicator that the temperature peaks and starts to fali a CRUISE LEAN MIXTURE Enrich mixture until the EGT shows a drop of 25 F below peak on the rich side of peak b BEST POWER MIXTURE Enrich mixture until the EGT shows a drop of 75 F below peak on the rich side of peak CAUT ON Do not cont...

Page 87: ...tor Valve SELECT TANK MORE NEARLY FULL feel for detent and check visually 3 Mixture FULL RICH or as required by field elevation tighten friction on push pull type eontroll 4 Landing Light AS REQUIRED 5 Flaps DOWN maximum extension speed 97 kts 111 mph NOTE The Flaps Up Ianding procedure will increase the Flaps Down Ianding distances total over 50 foot obstacle by 50 6 Airspeed ESTABLISH LANDING AP...

Page 88: ... Pump OFF 3 Electrical and Avionics Equipment OFF 4 Throttle CLOSE 5 Mixture IDLE CUT OFF 6 Magneto Start Switch OFF after engine stops 7 BATTERY ALT Switch OFF 8 ALT Switch OFF 9 Control Lock INSTALL if conditions warrant 10 lnstall wheel chocks and release brakes if the airplane is to be leh unattended ENVIRONMENTAL SYSTEMS HEATING AND VENTILATION Refer to the SYSTEMS DESCRIPTION Section for op ...

Page 89: ... properties of the airfoils The normai preflight procedures should then be com pleted with particular attention given to check of flight controls for complete freedom of movement ENGINE Use engine oil in accordance with Consumable Materials in the HANDLING SERVICING AND MAINTENANCE Section WARNING Ascertain that magneto switch and battery master switch are off before moving propeller by hand Alway...

Page 90: ... in a warm area until the next flight lf there is no oil pressure within the first 30 seconds of running or if oil pressure drops after a few minutes of ground operation shut down and check for broken oil lines oil cooler leaks or the possibility of congealed oil NOTE lt is advisable to use external power for start ing in cold weather During warm up monitor engine temperatures closely since it is ...

Page 91: ...libration Normai System 5 8 Airspeed Calibration Alternate System 5 9 Altimeter Correction Normai System 5 1 O Altimeter Correction Alternate System 5 11 Power Off Stall Speeds 5 12 Wind Components 5 13 Take Off Distance 2200 5 14 Take Off Distance 2250 5 15 Rate of Ciimb 5 16 Cruise Performance 5 17 5 18 Landing Distance 5 19 October 1979 5 1 U N C O T R O L L E D C O P Y N O T F O R O P E R A T ...

Page 92: ...SectionV Perlormance BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK 5 2 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 93: ...r a sample VFR trip from Denver to Wichita are detailed below Ali examples and calculations assume the following conditions CONDITIONS At Denver Outside Air Temperatu re 15 C 59 F Field Elevation 5330 ft Altimeter Setting 29 60 in Hg Wind 270 at 10 kts Runway 26L length 10 010 ft Route of Trip DEN V4 GLD V132 HUT V73 ICT For VFR Cruise at 9 500 feet WIND OAT 9500 9500 ALT ROUTE MAGNETIC DIST FEET ...

Page 94: ... 92 and subtract 100 feet from field elevation for each 1 in Hg above 29 92 Pressure Altitude at DEN 29 92 29 60 32 in Hg The pressure altitude at DEN is 320 feet above the field elevation 5330 320 5650 ft Pressure Altitude at ICT 29 92 29 56 36 in Hg The pressure altitude at ICT is 360 feet above the field elevation 5 4 1332 360 1692 ft NOTE For flight planning the difference between cruise altit...

Page 95: ... Time and fuel used were calculated as follows Time Distance Ground Speed Fuel Used Time Fuel Flow Results are FUEL EST TIME AT USED GROUNO CRUISE FOR ROUTE D1STANCE SPEED ALTITUDE CRUISE SEGMENT NM KNOTS HRS MIN GAL DEN TXC 72 108 0 40 5 5 TXC GLD 73 108 0 41 5 6 GLO HUT 194 116 1 40 13 9 HUT ICT 28 113 0 15 2 1 October 1979 5 5 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S ...

Page 96: ... RPM 9500 feet Enter the CRUISE PERFORMANCE table for 9500 feet and obtain fuel flow at 2300 RPM The fuel flow is 6 2 gallans per hour Reserve fuel 45 min 6 2 GPH 4 7 gallans Total Fuel 28 0 4 7 32 7 gallans The estimated Ianding weight is determined by subtracting the fuel required for the trip from the ramp weight 5 6 Assumed ramp weight 2205 lbs Estimated fuel from DEN to ICT 28 0 gal 6 lbs gal...

Page 97: ...EED CALIBRATlON NORMAL SYSTEM Chart 3 The associated conditions define the specific conditions from which performance parameters have been determined They are not intended to be used as instructions however performance values de termined from charts can only be achieved if specified conditions exist 4 The fuli amount of usable fuel is available for all approved flight conditions 5 Engine and compo...

Page 98: ...4 60 69 62 71 61 70 65 75 66 76 65 75 70 81 70 81 69 79 75 86 75 86 73 84 80 92 80 92 78 90 85 98 85 98 83 95 90 104 90 104 88 101 95 109 95 109 93 107 100 115 100 115 105 121 106 122 110 127 111 128 115 132 116 133 120 138 120 138 125 144 124 143 130 150 128 147 823 KCI 9 O Ul o e o 3 J l J s D c m III m i n J a l Ul Ul C o Ul_ l U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S...

Page 99: ...CLOSED STORM WINDOW OPEN FLAPS UP FLAPS DOWN FLAPS UP FLAPS DOWN lAS lAS lAS lAS MPH MPH MPH MPH 75 74 80 79 86 84 90 89 96 94 111 99 107 105 121 109 117 115 132 119 127 142 138 152 148 162 158 IXJ c m 111m 1t C E CD C D l m C o l co lm O CD n 3 III O l l g U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 100: ...10000 FT SL 10000 FT 40 46 9 11 45 52 7 9 50 58 5 6 55 63 4 5 60 69 10 14 3 4 65 75 8 12 1 2 70 81 6 9 6 3 75 86 2 6 17 11 80 92 4 3 23 17 85 98 5 4 26 20 90 104 4 3 95 109 2 o 100 115 1 3 105 121 4 6 11 o 127 7 9 823 KCI 11 C 1 1 o o e o 3 j o 1 s tD c m m n I n 1 l en co o co_ U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 101: ...M WINDOW CLOSED STORM WINDOW OPEN FLAPS UP FLAPSDOWN FLAPS UP FLAPS DOWN FEET FEET FEET FEET 20 20 45 40 30 25 60 50 40 30 70 60 50 35 85 70 60 40 95 BO 70 110 75 120 85 135 150 aJ c m e11 m n I CD 1 1 l 1 en Do _ 1 CD l C CD lm O CD n 3 e III 0 l l g U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 102: ...8 kts 63 kts 70 kts 86 kts FLAPS DOWN 35 55 mph 60 mph 67 mph 82 mph 48 kts 53 kts 58 kts 71 kts WEIGHT 2250 LBS Maximum attitude loss during a normat stall recovery is approximately 300 ft ANGLE OF BANK LEVEL 30 45 60 FLAPS UP l 68 mph 74 mph 83 mph 101 mph 59 kts 64 kts 72 kts 88 kts FLAPS DOWN 35 56 mph 62 mph 68 mph 84 mph 49 kts 54 kts 59 kts 73 kts L _ 5 12 October 1979 U N C O T R O L L E D...

Page 103: ...3KTS 15MPH o z l z z o 0 E o V c c X EXAMPLEo WIND SPEED ANGLE BETWEEN WIND OIRECTION AND FLIGHT PATH HEADWIND COMPONENT CROSSWIND COMPONENT 20 10 o 10 o 10 20 CROSSWIND COMPONENT 3CY KNOT S October 1979 15 KTS 50 10 K TS 11 K TS 40 5 13 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 104: ... indicates tailwind 4000 Ft To Clear Grnd 50 Run Obst Ft Ft 1499 2553 1864 3142 2317 3784 1052 1857 1344 2323 1672 2843 959 1696 1227 2139 1298 2609 770 1372 993 1769 1206 2147 EXAMPLE OAT PRESSURE ALTITUDE HEADWIND GROUNO ROLL TOTAL D 1STANCE 15 F 4000 FEET 10 KNOTS 959 FEET 1696 FEET 6000 Ft 8000 Ft To To Clear Clear Grnd 50 Grnd 50 Oat Run Obst Oat Run Obst f O Ft Ft f O Ft Ft_ 10 1713 3004 o 2...

Page 105: ... 75 1767 3005 836 1547 15 1014 1792 1105 1939 45 1297 2261 1377 2366 75 1614 2760 680 1250 15 815 1450 890 1590 45 1050 1870 1120 1940 75 1275 2270 NOTE Minus sign indicates tailwind EXAMPLE OAT PRESSURE ALTITUDE HEADWIND GROUNO ROLL TOTAL D1STANCE 15 F 4000 FEET 10 KNOTS 1014 FEET 1792 FEET 6000 Ft 8000 Ft To To Clear Clear Grnd 50 Grnd 50 Oat Run Obst Oat Run Obst f O Ft Ft f O Ft Ft 10 1810 317...

Page 106: ... 2200 4000 8000 12000 SL 2000 4000 8000 12000 SL 1800 4000 8000 12000 5 16 FULL THROTTLE UP FULL RICH 2000 LBS 4000 FT 70 81 KTS MPH 708FT MIN RATE OF CLIMB SPEED CLIMB KNOTS MPH FT MIN 74 85 700 73 84 485 70 81 270 69 80 55 74 85 740 73 84 525 70 81 310 69 80 95 72 83 935 70 81 708 69 79 482 68 78 258 69 80 1167 70 81 925 69 79 685 66 76 448 19A KCI 2 October 1979 U N C O T R O L L E D C O P Y N ...

Page 107: ...6 7 97 112 75 9 0 113 130 63 7 6 104 120 54 6 6 97 111 73 8 8 112 129 62 7 4 103 119 53 6 5 97 111 71 8 5 111 128 60 7 2 102 117 52 6 4 96 110 69 8 3 111 127 59 7 1 107 117 51 6 2 95 109 63 7 6 106 122 57 6 9 101 116 50 6 1 94 108 SectionV Performance EN DUR ANCE RANG E HOURS S MILES 3 7 469 4 4 513 5 2 559 3 7 470 4 3 507 5 0 546 3 7 472 4 4 515 5 2 564 3 7 468 4 3 512 5 0 551 3 7 475 4 4 519 5 1...

Page 108: ...5 7 8 105 121 55 6 7 97 112 75 9 0 113 130 63 7 6 104 120 54 6 6 97 111 73 8 8 112 129 62 7 4 103 119 53 6 5 97 111 71 8 5 111 128 60 7 2 102 117 52 6 4 96 110 69 8 3 111 127 59 7 1 107 117 51 6 2 95 109 63 7 6 106 122 57 6 9 101 116 50 6 1 94 108 ENDUR ANCE RANG E HOURS S MILES 6 0 749 7 1 818 8 4 894 6 0 751 6 9 813 8 0 874 6 0 756 7 0 827 9 3 905 5 8 752 6 8 823 8 0 887 5 9 763 54 836 8 1 897 6...

Page 109: ...TAL KNOTS KNOTS ALT GROUNO TO CLEAR GROUNO TO CLEAR GROUNO TOCLEAR GROUNO TO CLEAR MPH MPH FEET ROLL 50 FTOBS ROLL 50FT OBS ROLL 50FT OBS ROLL 50FT OBS SL 543 1793 578 1892 613 1988 650 2088 2000 616 1995 656 2102 697 2213 741 2328 65 75 54 62 4000 701 2224 748 2348 796 2477 846 2610 6000 815 2493 856 2636 914 2786 972 2940 8000 922 2809 986 2976 1053 3148 1121 3327 10000 1066 3183 1141 3377 1219 ...

Page 110: ...SectionV Performance BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK 5 20 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 111: ... 6 7 Weight and Balance Record 6 9 Weight and Balance RespoQsibilities 6 11 Gross Weight Moment Limits 6 12 6 14 Computing Procedura 6 1 5 Sample Weight and Balance Loading Form 6 16 Weight and Balance Loadi ng Form 6 1 7 Useful Load Weights and Moments 6 18 Occupants 6 18 Oil 6 19 Usable Fuel 6 19 Baggage 6 20 Equipment List Provided for Each Airplane October 1979 6 1 U N C O T R O L L E D C O P ...

Page 112: ...SectionVI Wt and Bai Equip List BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK 6 2 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 113: ...ht and Balance When the air plane is delivered from the tactory it will first be weighed and the data recorded on this form Provision has been made on the form for Iisting additions of items to be installed before the delivery or subtractions of items to be removed before delivery from the as weighed condition This then represents the empty weight of the airplane When the airplane is first fueled ...

Page 114: ... weighing two on the wing front spar at Fuselage Station 129 4 and one on the ah fuselage at Fuselage Station 285 9 tail tie down ring 2 Fuel should be drained preparatary to weighing Tanks are drained from the regular drain ports with the airplane in static ground attitude The unusable fuel to be added to a Basic Empty Weight is 6 lbs at Fuselage Station 125 0 45 6 lbs airplanes aher compliance w...

Page 115: ...o be taken with thetapelevel with the hangar floor and parailel to the fuselage centerline The locations of the wheel reactions will be approximately at Fuselage Station 129 5 for main wheels and Fuselage Station 57 6 for the nose wheel 7 Jack point weighings are accomplished by placing scales at the jack points specified in step 1 above Since the center of gravity of the airplane is forward of Fu...

Page 116: ...T BAGGAGE FLOOR JACK POINT F S 129 4 A NOSE TO PLUMB BOB B DATUM TO PLUMB BOB F S 126 438 C DATUM TO MAIN GEAR e en ID l e c O Dl l l c c c r iii S m c m III m X Co D N W t en C0 tl o co_ U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 117: ...IGHT MAIN NOSE OA TAIL TOTAL AS WEIGHED Space below provided for additions and subtractions to as weighed condition EMPTY WEIGHT DRY ENGINE OIL 15 0 48 0 720 UNUSABLE FUEL MB 1 thru MB 460 6 0 125 0 750 Airplanes after compliance with S l No 0624 281 45 6 125 0 5700 BASIC EMPTY WEIGHT OJ c m en m 71 l t al D J l UJ o co Dol l Q OJ Dol UJ c al c g g c l Cli U N C O T R O L L E D C O P Y N O T F O R...

Page 118: ...ans for meeting both requirements The current equipment list and empty weight and c g information must be retained with the airplane when it changes ownership Beech Aircraft Corporation cannot maintain this information the current status is known only to the owner lf these papers become lost the FAA will require that the airplane be re weighed to establish t he empty weight and c g and that an inv...

Page 119: ...ATION NO PAGE NO 1 WEIGHT CHANGE RUNNING BASIC DESCRIPTION OF ARTICLE ADDED OR REMOVED EMPTY WEIGHT OR CHANGE WT l ARM l MOM WT l MOM LBS IN 100 LBS r50 s m c m en m J l o C c o _ J co E l l Q Dl l C Q c o a 5 r 1 u U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 120: ...NO PAGE NO 2 WEIGHT CHANGE RUNNING BASIC DESCRIPTION OF ARTICLE ADDED OR REMOVED EMPTY WEIGHT OR CHANGE WT _lARM l MOM WT lMOM _ILB IN 1 00 LB 100 III O l c O al l III D C c al c m III m C S t CD t J J N T1 W t m CD C o CD_ l U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 121: ...ad Weights and Moments tables The minimum and maxi murn moments are shown on the Moment Limits vs Weight table and can also be plotted on the Moment Limits vs Weight graph as visual indication that the limit is within the operational envelope These moments correspond to the forward and aft center of gravity flight limits for a particular weight The airplane must be loaded in such a manner to keep ...

Page 122: ...sketeer A23 19 19A GROSS WEIGHT MOMENT LIMITS SGNilOd HDI3 M łVH lHIV G3GVO I A23 19 o o o a N o 111 1 l l Ie Z Q l 1 9A A23 19 w hen Beechcraft Kit 23 5003 is installed 6 12 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 123: ...1 2532 1630 1757 1928 1890 2054 2236 2150 2395 2543 1640 1768 1940 1900 2067 2248 2160 2409 2555 1650 1779 1952 1910 2080 2260 2170 2423 2567 1660 1789 1964 1920 2092 2271 2180 2436 2579 1670 1800 1976 1930 2106 2283 2190 2450 2591 1680 1811 1987 1940 2118 2295 2200 2463 2603 1690 1822 1999 1950 2133 2307 2210 2477 2614 1700 1833 2011 1960 2144 2319 2220 2490 2626 1710 1843 2023 1970 2157 2331 223...

Page 124: ...703 1801 1760 1897 2006 1940 2120 1714 1813 1770 1908 2018 1950 2133 1725 1824 1780 1919 2029 1960 2145 1736 1835 1790 1930 2041 1970 2158 1746 1847 1800 1940 2052 1980 2172 1757 1858 1810 1953 2063 1990 2185 1768 1870 1820 1966 2075 2000 2198 1779 1881 1830 1978 2086 2010 2211 1789 1892 1840 1991 2098 2020 2224 1800 1904 1850 2004 2109 2030 2237 Max Mom 100 2120 2132 2143 2155 2166 2177 2189 2200...

Page 125: ...he Fuel to Zero Fuel Condition to obtain the SUS TOTAL Ramp Condition 5 Subtract the fuel to be used for start taxi and take off to arrive at the SUS TOTAL Take off Condition 6 Subtract the weight and moment of the fuel in the incremental sequence in which it is to be used from the take off weight and r 1oment The Zero Fuel Condi tion the Take Off Condition and the Landing Condi tion moment must b...

Page 126: ...MPTY CONDITION 1437 1594 2 FRONT SEAT OCCUPANTS 340 374 3 3rd 4th SEAT OCCUPANTS 140 199 4 BAGGAGE OR CARGO 45 64 5 SUB TOTAL ZERO FUEL CONDITION 1962 2231 6 FUEL LOADING 192 225 7 SUB TOTAL RAMP CONDn s 2154 2456 8 LESS FUEL FO TART TAXI AND TAKE OFF 5 6 9 SUB TOTAL TAKE OFF CONDITION 2149 2450 1O LESS FUEL TO DESTINATION 25 GAL 150 176 11 LANDING CONDITION 1999 2284 Fuel for start taxi and take ...

Page 127: ...EAT OCCUPANTS 3 3rd 4th SEAT OCCUPANTS 4 BAGGAGE OR CARGO 5 SUB TOTAL ZERO FUEL CONDITION 6 FUEL LOADING GAL 7 SUB TOTAL RAMP CONDITION 8 LESS FUEL FOR START TAXI AND TAKE OFF 9 SUB TOTAL TAKE OFF CONDITION 10 LESS FUEL TO DESTINATION GAL 11 LANDING CONDITION Fuel for start taxi and take off is normally 5 lbs at an average mom 100 of 6 Octoł er 1979 6 17 U N C O T R O L L E D C O P Y N O T F O R O...

Page 128: ...0 120 132 170 130 143 185 140 154 199 150 165 213 160 176 227 170 187 241 180 198 256 190 209 270 200 220 284 Reclining seat with back in full up position Values computed from a C G criterion based on a 170 pound male Differences in physical characteristics can cause variation in center of gravity location 6 18 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 129: ...TS WEIGHT MOMENT 100 8 15 7 USABLE FUEL ARM 117 GALLONS WEIGHT MOMENT 100 5 30 35 10 60 70 15 90 105 20 120 140 22 132 154 25 150 176 27 162 189 30 180 211 32 192 225 35 210 246 37 222 259 40 240 281 45 270 316 50 300 351 52 312 365 55 330 386 57 342 400 58 348 407 October 1979 6 19 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 130: ... A23 19 19A USEFUL LOAD WEIGHTS AND MOMENTS BAGGAGE ARM 142 MOMENT WEIGHT 100 10 14 20 28 30 43 l 40 57 50 71 60 85 70 99 80 114 90 128 100 142 11 o 156 120 170 130 185 140 199 6 20 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 131: ... System Manual Trim 7 6 Electric Trim 7 6 Instrument Panel 7 6 lllustration 7 7 Switches 7 8 Circuit Breakers 7 8 Flight lnstruments 7 8 Ground Control 7 8 Wing Flaps Manual 7 9 Electric 7 9 Landing Gear 7 10 Brakes 7 1O Baggage Compartmant Seats Seat Belts and Shoulder Harnesses Seat Adjustment Seat Belts Shoulder Harnesses October 1979 7 11 7 11 7 12 7 12 7 1 U N C O T R O L L E D C O P Y N O T ...

Page 132: ... Fuel System 7 1 6 Fuel Tanks 7 16 Fuel Drains 7 17 Fuel Quantity lndicators 7 17 Fuel Boost Pump 7 17 EnginePrimer 7 18 Fuel Tank Selection 7 18 Fuel Required for Flight 7 18 Fuel System Schematic 7 19 Electrical System 7 20 Battery 7 20 Alternator 7 20 External Power Receptacle 7 22 Lighting Systems Interior Lighting 7 22 Exterior Lighting 7 23 Environmental Systems 7 2 Cabin Heating 7 23 Enviro...

Page 133: ...Continued SUBJECT PAGE Pitot and Static Systems Pitot System 7 25 Pitot Heat Optional 7 25 Normai Static Air System 7 25 Emergency Static Air System Optional 7 26 Vacuum System 7 26 Stall Warning System 7 26 October 1979 7 3 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 134: ...Section VII Systems Description BEECHCRAFT Sport III MusketeerA23 19 19A INTENTIONAllY lEFT BlANK 7 4 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 135: ...ase knob below the left forward seat carner pull to the right then up and slide the seat forward or aft as desired Make certain the seat is locked securely in place after adjustment The backs of both individual seats can be placed in any of three posi tions Outboard armrests for the front seats are provided FLIGHT CONTROLS CONTROL SURFACES The eontroi surfaces are operated with conventional cable ...

Page 136: ...rim system is controlled by the ON OFF switch located on the instrument panel a thumb switch on the eontroi wheel and a circuit breaker on the right subpanel The ON OFF switeh must be on the ON position to operate the system The thumb switch is moved forward for nose down aft for nose up and when re leased returns to the center OFF position When the sys tem is not being eleetrically actuated the m...

Page 137: ...BEECHCRAFT Sport III Musketeer A23 19 19A J w z t o l z w E l a l CI z October 1979 SectionVII Systems Description 7 7 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 138: ...agnetic compass is located above the instrument panel Ram air pressure for the airspeed indieator enters through the pitot tube under the left wing statie air pressure for the altimeter vertical speed and airspeed indieator is supplied by a statie port oneach side of the fuselage justaft of the eabin Instrument lights are turned on and dimmed by a rheostat switch loeated on the left subpanel GROUN...

Page 139: ...pressed nor should it be to lower the flaps ELECTRIC MB 452 thru MB 460 The electric wing flaps are controlled by a three position switch UP OFF and DOWN located to the right of the power quadrant The switch must be pulled out of detent before it can be repositioned A dial type indicator has markingsfor UP 1ODEGREES 20 DEGREES and DOWN The indicator is located adjacent to the power quadrant Limit ...

Page 140: ...ing toe pressure to the rudder pedals The parking brake push pull eontroi is located on the right side of the lower left subpanel To set the parking brakes depress the pilot s toe pedals umil firm and pull out on the parking brake knob then release the toe pressure Release the parking brake by depressing the pilot s toe pedals then push in the parking brake knob Check both wheels for free roll bef...

Page 141: ...ce for light miscellaneous arti cles Both the baggage compartment and hat shelf are ac cessible in flight WARNING Do not carry hazardous material anywhere in the airplane Do not carry children in the baggage compart ment SEATS SEAT BELTS AND SHOULDER HARNESSES SEAT ADJUSTMENTS To adjust either of the front seats pull up on the release knob below the left hand seat corner and slide the seat for war...

Page 142: ... buckle The har ness should be used with the seatsin the upright position The spring loading at the inertia reel keeps the harness snug but will allow normai movement required during flight operations The inertia reel is designed with a locking device that will secure the harness in the event of sudden forward movement or an impact action DOORS AND EXITS FORWARD CABIN DOORS The airplane has a conv...

Page 143: ...ck is provided with the loose tools to prevent movement ot the eontroi eolumn and impairs aeeess to the magnetQStart switeh To install the Control Loek 1 Level the eontroi wheel and move eontroi eolumn so the holes in t he eontroi eolumn hanger and eontroi eol umn will align to aecept the pin 2 Push the eontroi eolurnn loek pin through the hole pro videdin the eontroi eolurnn hanger and into the h...

Page 144: ...of the knob ENGINE INSTRUMENTS The engine instrument eluster is loeated on the lower left subpanel and indudes the left fuel quantity indieator an ammeter oil temperatura oil pressure and the right fuel quantity indicator The tachorneter is located on the upper left ot the instrument panel The fuel pressure indiestor is located on the left subpanel ENGINE BREAK IN INFORMATION New engines have been...

Page 145: ...f it should become blocked CARBURETOR HEAT There is a possibility of ice forming in the induction sys tem under certain moist atmospheric conditions Gen erally ice mayform in the vicinity of the carburetor butter fly and may build up enough that a drop in power output could result The induction installation is equipped with a system for preheating the incoming air to the carburetor The air preheat...

Page 146: ...itch tvvo blade propeller Static rpm at maximum permissible throttle settings Not over 2400 rpm and not under 2300 rpm No additional tolerance permitted Diameter 74 inches no cutoff permitted FUEL SYSTEM The airplane is designed for operation on 80 87 Red grade aviation gasoline In the event this gradeis not avail able 1OOLL Biue or 100 Green grade aviation gasolines may be used CAUTION See Avco L...

Page 147: ...he fuselage aft of the nose wheel Sump drains provide a means to visually inspect the fuel for water or con taminants Refer to HANDLING SERVICING AND MAINTENANCE Section for procedures describing how and when to use fuel tank sump drains FUEL GUANTITY INDICATORS Fuel quantity is measured by a float operated sensor lo cated in each wing tank system These transmit electrical signals that indicate fu...

Page 148: ...L REGUIRED FOR FLIGHT lt is the pilot s responsibility to ascertain that the fuel quantity indicators are functioning and maintaining a reasonable degree of accuracy and to be certa in of ample fuel for a flight Takeoff is prohibited if the fuel quantity indicators do not indicate above the yellow arc or with less t han 11 gallans in each main tank The caps should be removed and fuel quantity chec...

Page 149: ...FT Sport III Musketeer A23 19 19A LEFT FUEL TANK Section VII Systems Description FUEL SELECTOR VALVE FUEL SYSTEM SCHEMATIC October 1979 7 19 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 150: ...ft fuselage Battery servicing procedures are described in the HANDLING SERVICING AND MAINTENANCE Section ALTERNATOR The alternator maintains its full rated output at cruise engine rpm and uses a voltage regulator to adjust alternator output Dual switches are required to activate the alternator circuit The switch placarded BADERY ALT when placed in the ON position will only activate the battery cir...

Page 151: ...o reading which is nor mai in cruising flight indicates that the battery is fully charged and that the alternator output has been adjusted by the voltage regulator to balance the load of the electri cal equipment in use Should an alternator or regulator become inoperative in dicated by a heavy discharging or widely fluctuating am meter indication turn the ALT switch to OFF and mini mize the electr...

Page 152: ...s switches must be OFF when connecting the ground power plug Care should be taken to assure correct polarity negative ground prior to connecting and energizing the ground power unit The battery switch must be turned ON to connect the ground power unit to the airplane bus Alter nator switch must be OFF while using external power LIGHTING SYSTEMS INTERIOR LIGHTING Lighting for the instrument panel i...

Page 153: ...ts when installed should be turned off before entering an overcast their use may not be advisable under instrument or limited VFR conditions ENVIRONMENTAL SYSTEMS CABIN HEATING Air for warming the cabin and defrosting the windshield enters through an intake on the lower cowl forward bulk head and passes through the heater and into a mixer box where it is blended with cold air to obtain the desired...

Page 154: ...IR fYr ip FB FRESH AIR EXHAUST HEATER MUFFLER DEFROST AIR AIR FIREWALL FRESH AIR INLET COCKPIT FRESHt AIR OUTLETS 121 l COCKPIT HEATER III OUTLETS 121 REAR SEAT FRESH AIR OUTLETS 2 19A EXHAUST OUTLET AFT CABIN BULKHEAD 7 24 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 155: ... on the leading edge of the left wing PITOT HEA T OPTIONAL The pitot mast is provided with an electric heating ele ment which is turned on and off with a switch on the instrument panel The switch should be ON when flying in visible moisture lt is not advisable to operate the pitot heating element on the ground except for testing or for shor intervals of time to remove ice or snow NORMAL STAliC AIR...

Page 156: ... equipment is supplied by an engine driven vacuum pump An adjustable relief valve centrols suction by bleeding outside air into the vacuum pump A suction gage indicates system vacuum in inches ot mer cury This instrument is located on the pilot s side ot the instrument panel The vacuum should be maintained within the green arc for proper operation of the air driven instruments STALL WARNING SYSTEM...

Page 157: ...RY ALT switch in the OFF position the stall warning horn is inoperative Airplane certification requires the stall warning system to be on during flight except in emergency conditions as stated in Section III October 1979 7 27 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 158: ...SectionVII Systems Description BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK 7 28 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 159: ... to Airplane 8 5 Ground Handling 8 6 Towing 8 6 Parking 8 7 eontroi eolumn Lock Pin 8 7 Tie Down 8 8 Jacking 8 8 Flyable Storage 7 to 30 Days Mooring 8 9 Fuel eells 8 9 Flight eontroi Surfaces 8 9 Grounding 8 9 Pitot Tube 8 9 Windshield and Windows 8 9 During Flyable Storage 8 9 Preparation for Service 8 1 O Prolonged Out of Service eare 8 1 O External Power 8 11 ehecking Electrical Equipment 8 11...

Page 160: ...7 Minor Maintenance Rubber Seals 8 18 Alternator 8 18 Magnetos 8 19 Cleaning Exterior Pai nted Surfaces 8 19 Windshields and Windows 8 20 Interior 8 21 Engine 8 22 Lubrication 8 22 Lubrication Points 8 23 Recommended Servicing Schedule 8 29 Consumable Materials 8 34 Approved Engine Oils 8 36 Bulb Replacement Guide 8 38 Overhaul or Replacement Schedule 8 39 8 43 lnspections 8 43 8 2 Operational lns...

Page 161: ...i limits procedures safety practices time limits servicing and maintenance requirements contained in this handbook are considered mandatory Authorized BEECHCRAFT Aero or Aviation Centers and International Distributors or Dealers will have recommended modification service and Operating procedures issued by both FAA and Beech Aircraft Corporation designed to get maximum utility and safety from the a...

Page 162: ... of this handbook For information on how to obtain Revision Service applicable to this handbook eonsuit any BEECHCRAFT Aero or Aviation Center or International Distributor or Dealer or refer to the latest revision of BEECH CRAFT Service lnstructions No 0250 010 AIRPLANE INSPECTION PERlODS 1 FAA Required Annual lnspections 2 BEECHCRAFT Recommended lnspection Guide 3 Continuing Care lnspection Guide...

Page 163: ...ntenance must be performed by licensed personnel NOTE Pilots operating airplanes of other than U S registry should refer to the regulations of the registering authority for information con cerning preventative maintenance that may be performed by pilots ALTERATIONS OR REPAIRS TO AIRPLANE The FAA should be contacted prior to any alterations on the airplane to ensure the airworthiness of the airplan...

Page 164: ...r linkage may be damaged One person can move the airplane on a smooth and level surface using the hand tow bar furnished with the loose equipment Attach the tow bar to the tow lugs on the nose gear lower torque knee Where movement is restricted two people can pivot the airplane on the main wheels One person should push on the wing leading edge or hold the wing tip while the other operates the tow ...

Page 165: ...ntroi is located on the right side of the pilot s lower subpanel To set the parking brakes pull out on the parking brake eontroi and depress the pilot s toe pedals until firm Release the parking brake by pushing the parking brake eontroi forward Check both wheels for free roll before applying take off power NOTE The parking brake should be left off and wheel chaeks installed if the airplane is to ...

Page 166: ... wheels fore and aft 3 Using nylon line or ehain of suffieient strength seeure the airplane at the three points provided DO NOT OVER TIGHTEN if the line at the rear ot the fuselage is exeessively tight the nose may rise and produee lift due to the angle of attaek ot the wings 4 Release the parking brake lf high winds are antieipated a vertieal tail post may be in stalled at the rear tie down lug a...

Page 167: ...SURFACES Lock with interna locks GROUNOING Static ground airplane securely and effectively PITOT TUBE lnstall cover WINDSHIELD AND WINDOWS Close window vent DURING FLYABLE STORAGE In a favorable atmospheric environment the engine of an aircraft that is flown intermittently can be adequately pro tected from corrosion by turning the engine over five revolutions by means ot the propeller This will di...

Page 168: ...ld be made long enough to produce an oil temperature within the lower green arc range Ex cessive ground runup should be avoided PREPARA T ON FOR SERVICE Remove all covers clean the airplane and give it a thorough inspection particularly flaps and eontroi openings Preflight the airplane PROLONGED OUT OF SERVICE CARE The storage procedures listed are intended to protect the airplane from deteriorati...

Page 169: ...e certai n no power is being sup plied when the connection is made 3 Make certain that the BATI ALT switch is ON the ALT switch and all avionics and electrical switches OFF and a battery is in the system before connecting an external power unit This protects the voltage re gulators and associated electrical equipment from transients power fluctuations CHECKING ELECTRlCAL EQUIPMENT Connect an auxil...

Page 170: ...of 15 gallans when the fuel reaches the bottom of the tab or 20 gallans when the fuel reaches the top of the slot This partial filling of the fuel tanks allows an increase in the payload The fuel indicators on the instrument panel will indicate fuli tanks even though each tank contains only 20 gallans of fuel 8 12 CAUTION Connect a grounding cable from the fuel ser vice unit to the airframe and co...

Page 171: ...ere is an excessive amount of sand or dirt the strainers should be inspected at more frequent intervals The screen in the fuel strainer at the system low spot on the bottom of the fuselage should be removed and washed in fresh cleaning solvent at each 100 hour inspection of the airplane Ordinarily the finger strainers in the fuel tank outlets should not require cleaning unless there is a definite ...

Page 172: ...ed under adverse operating conditions Use engine oil as indicated in Consumable Materials in this section The engine oil sump capacity is eight quarts The normai operating range is six to eight quarts RECOMMENDED 0 L GRADES FOR ENGINES Average MIL L 22851 l Ambient Air MIL L 6082 Ashless Dispersant Temperature Grades Grades i Above 60 F SAE 50 SAE 40 or SAE 50 30 F to 90 F SAE 40 SAE 40 0 F to 70 ...

Page 173: ...ion will minimize tread wear and aid in preventing tire failure caused from running over sharp stones When inflating tires visually inspect them for eraeks and breaks NOTE Beech Aircraft Corporation cannot recom mend the use of recapped tires Recapped tires have a tendency to swell as a result of the in creased temperature generated during takeoff lncreased tire size can jeopardize proper func tio...

Page 174: ...ustment Complete information on brake wheel and tire maintenance is contained in the ap propriate manual included in the loose tools and acces sories kit INDUCTION AIR FILTER This filter should be inspected for foreign matter at least once during each 50 hour operating period In adverse climatic conditions or if the airplane is stored preflight inspection is recommended To remove and clean the fil...

Page 175: ...etui examination of the propeller blades for nicks and scratches Each blade leading edge should receive particular attention lt is very important that all nicks and scratches be smoothed out and polished The BEECHCRAFT Aero or Aviation Center and International Distributors or Dealers will beglad to answarany questions concerning propeller blade repair WARNING When servicing a propeller always make...

Page 176: ...ke certain that the ground polarity of the battery and the ground polarity of the alternator are the same 2 When connecting a boaster battery be sure to connect the negative battery terminais together and the positive battery terminais together 3 When using a battery charger connect the positive lead of the charger to the positive battery terminal and the negative Iead of the charger to the negati...

Page 177: ...ng the switch lead at the noise filter capacitor with a wire which is grounded to the engine case Otherwise all spark plug Ieads should be disconnected orthe cable outlet plate on the rear of the magneto should be removed CLEANING EXTERIOR PAINTED SURFACES CAUTION Do not apply wax or polish for a paint cure period of 90 days after delivery Waxes and polishes seal the paint from the air and prevent...

Page 178: ...corrosion or scratches To remove stubborn oil and grease use a cloth dampened with aliphatic naphtha see Consumable Materials After being cleaned with naphtha the surface should be re waxed and polished To prevent scratches use soft cleaning cloths or a chamcis when cleaning and polishing Any good grade ot automotive wax or polish can be used on painted surfaces WINDSHIELD AND WINDOWS The windshie...

Page 179: ... upholstery head liner and carpet clean the interior regularly with a vacuum cleaner Blot up any spilled liquid promptly with cleansing tissue or rags Do not pat the spot press the blotting material firmly and hold it for several seconds Continue blotting until no more liquid is taken up Scrape off sticky materials with a duli knife then spot clean the area Oily spots may be cleaned with household...

Page 180: ...tic should not be used LUBRICATION Proper lubrication is essential in keeping the airplane components in top condition lf this operation is per formed thoroughly generał maintenance will be reduced and the service life of the airplane will be greatly increased The grease fittings or parts must be wiped clean to make sure that no dirt is carried into the part when lubricated Apply lubricant sparing...

Page 181: ...FT Sport III MusketeerA23 19 19A Section VIII Handling Serv Maint LUBRICATION POINTS D C F E A DETAIL A NOSE GEAR STEERING October 1979 8 23 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 182: ...ng Serv Maint BEECHCRAFT Sport III MusketeerA23 19 19A DETAIL B FG FLAP MECANISM DETAIL C 0 RUDDER BELLCRANK DETAIL D 0 RUDDER HINGE 8 24 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 183: ...9 19A DETAIL E 8 Section VIII Handling Serv Maint ELEVATOR HINGE DETAIL F STABILATOR HINGE BRACKET DETAIL H DETAIL G AILERON BELLCRANK RUDDER PEDALS October 1979 8 25 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 184: ... Maint BEECHCRAFT Sport III Musketeer A23 19 19A DETAILI DETAIL J l DETAIL K 8 26 0 0 l LANDING GEAR CONTROL COLUMN UNKAGE 1 8 TRIM TAB ACTUATOR October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 185: ... LUBRICATE CONE WITH VERY THIN COAT ING OF LUBRICANT NOTE Airplanes having complied with BEECHCRAFT S No 0622 289 or S No 0838 need no ubrication NOTE DO NOT OVER LUBRICATE VALVE CONE APPLY MINIMUM AMOUNT OF LUBRICANT FOR COATING FUEL SELECTOR VALVE DETAIL M AILERON HINGE AND ROD ENDS October 1979 8 27 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 186: ...efer to items in the consumabie materiais chart Lubri cate all piain bearing bushings as required or every 500 hours with SAE No 30 oil Appiy SAE No 20 o1 i to push pull eontroi housings as required Lubricate flight eontroi pully bushtngs with SAE No 30 oii every 1000 hours SAE 1Ow 30 oii is an acceptabie repiacement for SAE 20 or SAE 30 oil 8 28 October 1979 U N C O T R O L L E D C O P Y N O T F ...

Page 187: ...tanks Top ot wings Check battery electrolyte Behind aft cabin bulkhead Clean induction air filter In lower forward cowl Lubricate Ianding gear On Ianding gear l knee pins Change engine oil Lower side ot engine Clean oil screens Aft right side of accessory case and bottom of sump LUBRICANT Number refers to item on Consumable Materials 1 3 See Shop Manual 5 1 2 l l m c m 0 m l t Cli 9l u l l IIJ TI ...

Page 188: ...ear l On top ot nose gear A On aft side of nose gear A Under floorboards B lnboard end ot flaps B Bottom of rudder C On rudder leading edge D On trailing edge of p stabilator E LUBRICANT Number refers to item on Consumable Materials 2 8 11 5 14 11 11 11 4 10 t m III l l o Q o l l P m l o 3 l 3 1XJ c m en m I a l l l m CD C o t CD_ l U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U...

Page 189: ...tral filter MB 289 thru MB460 Lubricate eontroi column pivot points Lubricate trim tab actuator In aft tail section F 11 In wing forward of aileron 11 G Outboard trailing edge ot 11 wings M In front nose cowl Forward cabin floor H 11 Forward cabin floor H 11 Behind instrument panel Behind instrument panel J 11 In aft tail section K 9 l l S CXI c m en m 11 1 t Cli C1 IJ 1 Tl w ł en o co X l s g s t...

Page 190: ...fluid reservoir MB 1 thru MB 264 On individual rudder pedal linkage N MB 265 thru MB 460 On firewall N Clean spark plugs In engine compartment Replace Emergency Locator Transmitter Battery LUBRICANT Number refers to item on Consumable Materials 15 7 l 7 r cn III CD g_ o l l p cnE ID III a al r m III m r t 0 w 4 en CD g o CD_ l U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 191: ...9 19A Section VIII Handling Serv Maint NOTE Anytime the eontroi surfaces are altered repaired or repainted they must be rebalanced per the Shop Manual October 1979 8 33 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 192: ...era ture 6 Corrosion Preven MIL C 6529 tive Engine 7 Hydraulic Fluid MIL H 5606 tt8 Grease General MIL G 81322 Purpose Wide Temperaturej tt9 Grease High MIL G 23827 Law Tempera ture 1O Lubricating Oil MIL L 7870 Low Tempera ture 11 Lubricating Oil SAE No 20 or 1OW 30 12 Lubricating Oil SAE No 30 or 1OW 30 ttt13 Lubricant Rubber Oakite 6 Compound Seal tttt 14 Lubricant Silicone Krylon No 1329 Spray...

Page 193: ...0 87 red fuel is not available use 1OOLL blue or 100 green Mix with quick evaporating liquid naphtha and apply with a brush t Produet of BRC Bearing Company Wichita Kansas tt In extremely cold climates MIL G 23827 grease should be used in place of MIL G 81322 grease Care should be exercised when using either MIL G 81322 or MIL G 23827 grease as they contain a rust pre venting additive which is har...

Page 194: ...il and Supply Co Chevron Oil Company Humble Oil and Refining Co Standard Oil Company ot California 8 36 60068 Aeroshell W120 Aeroshell W80 TX 6309 Aircraft Engine Oil Premium AD120 Aircraft Engine Oil Premium AD80 PQ Aviation Lubricant 753 Chevron Aero Oil Grade 120 Esso Aviation Oil E 120 Enco Aviation Oil E 120 Esso Aviation Oil A 1 00 Enco Aviation Oil A 1 00 Esso Aviation Oil E 80 Enco Aviatio...

Page 195: ...on Oil 65 Grade 1100 Conoco Aero Oil 1065 Conoco Aero Oil 1100 Avrex 101 1065 101 1100 Phillips 66 Aviation Engine Oil Grade 1065 Phillips 66 Aviation Engine Oil Grade 1100 Aeroshell Oil 65 Aeroshell Oil 100 Ashless Dispersant Oils Complying with MIL L 22851 NOTE Ashless dispersant oil complying with MIL L 22851 is recommended after the oil consump tion has stabilized or after the first 50 hours o...

Page 196: ...erenee only and are not specifi eally reeommended by Beeeh Aireraft Corporation Any produet eonforming to the specifieation may be used LOCATION BULB REPLACEMENT GUIDE NUMBER Compass light Dome light eabin Instrument flood light overhead Landing light wing Navigation light tail eone Navigation light wing Rotating beaeon Engine instrument eluster Landing gear position indieators lf simulated retrae...

Page 197: ...erage usage and average environmental conditions SPECIAL CONDITIONS CAUTIONARY NOTICE Airplanes operated for Air Taxi or other than normai operation and airplanes operated in humid tropics or cold and damp climates etc may need more frequent inspections for wear corrosion andj or lack of lubrication In these areas periodic inspections should be performed until the operator can set his own inspecti...

Page 198: ...ANT NOTE When an engine has been overhauled or a new engine installed it is recommended that low power settings NOT be used until oil con sumption has stabilized The average time for piston ring seating is approximately 50 hours Refer to Lycoming Engine Operator s Manual Engine 0 320 E2B 0 320 E2C 0 320 E2D Engine Controls Engine Vibration lsolator Mounts 8 40 2000 hours 2000 hours 2000 hours On C...

Page 199: ...nated On Condition or 1000 hours At Engine Overhaul or On Condition lnspect every 100 hours At engine overhaul or every 5 years Ali other hoses on condition Every 300 Hours On Condition At engine overhaul or on condition FUEL SYSTEM Fuel Boost Pump Ali Hose carryi ng flammable liquid Ali Hose not carrying flammable liquid Fuel Selector Valve Fuel System Check Valves Fuel Celi Drain Valve Wing Fuel...

Page 200: ...onths per FAA Directive lnspect and calibrate On Condition On Condition On Condition On Condition On Condition On Condition On Condition On Condition On Condition On Condition ELECTRlCAL SYSTEM Battery Master Relay Ali other Relays Voltage Regulator Starter Relay On Condition On Condition On Condition On Condition FLAPS AND FLIGHT CONTROLS Flight Centrols Stabilator Tab Actuator Flap Motor and Act...

Page 201: ...g practice requires that the airplane be pre flighted prior to takeoff ltems found during preflight and engine run up should be corrected on the basisof their im portance to the safe operation of the airplane however in any event early correction of items found is good pre ventative maintenance Although it is not a requirement that FAA qualified per sonnel change the oil and inspect the airplane e...

Page 202: ...s 14 Power cheek 2300 to 2400 rpm statie Power Plant 1 Oil screens cleaned 2 lnduetion air filter cleaned 3 Check engine eontrols wiring harness and plumbing for elearanee and seeurity 4 Check propeller for rock damage and spinner and spinner bulkheads for eraeks and seeurity engine for oil leaks 5 Cheek engine baffles and eowling for eraeks and seeurity 6 Cheek exhaust system and air duets for co...

Page 203: ... door operation 3 Check interior furnishings and seat belts 4 Check battery water level Exterior 1 Check flight eontroi suńaces for condition and security 2 Check tires brake pucks and discs 3 Check static ports pitot mast and fuel vent lines for obstructions 4 Check generał condition of fuselage and wings October 1979 8 45 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 204: ...Section VIII Handling Serv Maint BEECHCRAFT Sport III Musketeer A23 19 19A l NTENTIONALLY LEFT BLANK B 46 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 205: ... equipment for which the vendor obtained a Supplemental Type Certificate were included as loose equipment with the airplane at the time of delivery These and other Supplements for other equipment that was installed after the airplane was delivered new from the tactory should be placed in this SUPPLEMENTS Section of this Pilot s Operating Handbook and FAA Approved Airplane Flight Manual October 197...

Page 206: ...SectioniX Supplements BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK 9 2 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 207: ...upplemenrs musr be in rhe airplane for flighr operarion when subject equipmenr is installed Supp Pan Rev Date No Number Subject No 1 169 590004 5 Aeroba tic 10 79 2 169 590002 9 Two Ooor Wai Around 10 79 3 169 590002 11 Aeroplanes Regisłered in 1 1182 The Uniłed Kingdom January 1982 9 3 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 208: ...Section IX Supplements BEECHCRAFT Sport III Musketeer A23 19 19A INTENTIONALLY LEFT BLANK 9 4 October 1979 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 209: ...tered at 140 MPH 122 KTS lAS at 2700 RPM A 3 0 to 3 5 G pull up is recommended The airspeed at the top of the loop will be 50 to 60 MPH 43 to 52 KTS lAS which is fast enough to retain positive ac celeration and prevent a stall Completion of the loop is ac complished by keeping the G level just below that where a buffet occurs The altitude lass is 50 to 100 feet IMMELMANN The maneuver is entered at...

Page 210: ...ottle is to be retarded as the nose drops past the horizon in the inverted position WARNING Do not use abrupt or fuli eontroi travel at speeds greater than the maximum design maneuvering speed Spins are approved Spins have not been demonstrated in excess ot 6 turns For sp in entry and recovery see pages 3 1O and 3 11 ot this Pilot s Operating Handbook and FAA Approved Flight Manual Continuous inve...

Page 211: ...oors which have been installed in accordance with BEECH CRAFT FAA approved data This document supersedes or adds to the Pilot s Operating Handbook and FAA Approved Airplane Flight Manual only where covered in the items eontainad herein LIMITATIONS No change EMERGENCY PROCEDURES No change NORMALPROCEDURES PREFUGHT INSPECTION Emergency Locator Transmitter ARMED location may vary with individual airp...

Page 212: ...on CHECK d Wing Tip CHECK e Position Light CHECK 3 LEFT WING LEADING EDGE a Pitot Tube CHECK Remove Cover b Landing Light CHECK c Tie Down and Chocks REMOVE d Stall Warning CHECK for movement of vane e Fuel Tank CHECK QUANTITY Filier Cap SECURE 2 of 4 FAA Approved October 1979 P N 169 590002 9 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 213: ...trainer DRAIN h Chocks REMOVE 6 RIGHT LANDING GEAR a Fuel Sump DRAIN b Tire and Brake CHECK 7 RIGHT WING LEADING EDGE a Fuel Tank CHECK QUANTITY Filier Cap SECURE b Tie Down and Chocks REMOVE c Wing Tip CHECK d Position Light CHECK 8 RIGHT W NG TRAIL NG EDGE a Aileron CHECK b Flap CHECK c Fuel Tank Vent Line UNOBSTRUCTED 9 RIGHT FUSELAGE a Static Pressure Button UNOBSTRUCTED FAA Approved October 1...

Page 214: ...K 11 LEFT FUSELAGE a Static Pressure Button UNOBSTRUCTED b Ali Antennas CHECK PERFORMANCE No change 4 of 4 Approved Jl W H Schultz Beech Aircraft Corporation DOA CE 2 FAA Approved October 1979 P N 169 590002 9 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 215: ...book and in any relevant supplement This supplement overrides the handbook should there be disagreement between the two doeuments 1 For the purpose of the first schedule of the Air Naviga tion Order this aeroplane is classified as an Aeroplane landplane 2 The BEECHCRAFT models A23 19 and 19A are eligible for eertifieation in the United Kingdom in the Transport Category Passenger This aeroplane may...

Page 216: ...e perform ed children under the age ot three years may be camed in the arms ot passengers and left out ot the total number count 7 The aeroplane may be operated on short dry grass surfaces When so operating he take off and Ianding distances given in Section V ot the Pilot s Operating Handbook must be increased by 10 8 When Iłying for public transport the effect of tempera ture on the rate ot climb...

Page 217: ...he Pilot s Operat ing Handbook shall be decreased 60 ftimin for every 1O degrees Cenligrade above standard WEIGHT AND BALANCE No change SYSTEMS DESCRIPTION No change HANDLING SERVICING AND MAINTENANCE No change APPROVED W H Schultz Beech Aircraft Corporation DOA CE 2 FAA Approved Revised January 1982 P N 169 590002 11 3 of 3 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 218: ...U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 219: ...viation News 10 15 FAA Accident Prevention Program 10 15 Additional lnformation 10 16 General lnformation on Specific Topies 10 17 Maintenance 10 17 Hazards of Unapproved Modifications 10 19 Flight Planning 10 20 Passenger lnformation Cards 10 20 Stowage of Articles 10 21 Flight Operations 10 21 General 10 21 Preflight lnspection 10 21 Weight and Balance 10 22 Autopilots and Electric Trim Systems ...

Page 220: ...ces Wake Turbulance 10 39 Takeoff and Landing Conditions 10 40 Medical Facts for Pilots 10 40 General 10 40 Fatigue 10 41 Hypoxia 10 41 Hyperventilation 10 43 Alcohol 10 43 Drugs 10 45 Scuba Diving 10 45 Carbon Monoxide and Night Vision 10 45 Decompression Sickness 10 46 A Finał Word 10 47 10 2 May 1994 U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 221: ...e Know its limitations and your own Maintain your currency or fly with a qualified instructor until you are current and proficient Praclice emer gency procedures at safe altiludes and airspeeds prefer ably with a qualified instructor pilot until the required action can be accomplished without reference to the manuał Peri odically review this safety information as part of your recur rency training ...

Page 222: ...nce manu als which accompany the airplane that FAA requirements for ratings certifications and review be scrupulously com plied with and that you allow only persens who are properly licensed and rated and thoroughly familiar with the contents of the Pilot s Operating Handbook and FAA Approved Air piane Flight Manual to operate the airplane IMPROPER OPERATION OR MAINTENANCE OF AN AIR PLANE NO MATIE...

Page 223: ...ice until you are proficient Preplan all aspects of your flight including a proper weather briefing and adequate fuel reserves Use services available weather briefing inflight weather and Flight Service Station Carefully preflight your airplane Use the approved checklist Have more than enough fuel for takeoff plus the trip and an adequate reserve Be sure your weight and C G are within limits Use s...

Page 224: ...erence to the manual Keep your airplane in good mechanical condition Stay informed and alert fly in a sensible manner DON TS Don t take off with frost ice or snow on the airplane Don t take off with less than minimum recommended fuel plus adequate reserves and don t run the tank dry before switching Don t fly in a reckless show off or careless manner Don t fly into thunderstorms or severe weather ...

Page 225: ...plane was manufac tured it was equipped with one or more of the following placards Owner s Manual FAA Approved Airplane Flight Manual FAA Approved Airplane Flight Manual Supple ments Pilot s Operating Handbook and FAA Approved Air plane Flight Manual Beech has revised and reissued many of the early manuals for certain models of airplanes in GAMA Standard Format as Pilot s Operating Handbooks and F...

Page 226: ...s to BEECH CRAFT Owner addresses as Iisied by the FAA Aircraft Reg istration Branch List and the BEECHCRAFT International Owner Notification Service List While this information is dis tributed by Beech Aircraft Corporation Beech can not make changes in the name or address furnished by the FAA The owner must eontael the FAA regarding any changes to name or address Their address is FAA Aircraft Regi...

Page 227: ...otification request card furnished with the loose equipment of each airplane at the time of delivery or by a letter requesting this service referencing the specific airplane serial number owned Write to Supervisor Speclal Servlces Dept 52 Beech Aircraft Corporation P O Box 85 Wichita Kansas 67201 0085 From time to time Beech Aircraft Corporation issues BEECHCRAFT Safety Communiques dealing with th...

Page 228: ...igned for your protection and the protection of your passengers and the public Com pliance is mandatory AIRWORTHINESS DIRECTIVES FAR Part 39 specifies that no person may operate a produet to which an Airworthiness Directive issued by the FAA applies except in accordance with the requirements of that Airworthiness Direetive AIRMAN S INFORMATION MANUAL The Airman s lnformation Manuał AIM is designed...

Page 229: ... Mountain Flying Airport Operalians Wake Turbulance Vortices Clearances and Separations Medical Facts for Pilots Preflight Bird Hazards Departures IFR Good Operating Practices En route IFR Airport Location Directory Arrival IFR Ali pilols must be thoroughly familiar with and use the infor mation in the AIM ADVISORY INFORMATION NOTAMS Notices to Airmen are documents that have information of a time ...

Page 230: ...ese documents are subject to periodic revision Be certain the Advisory Circular you are using is the latest revision available Some of the Advisory Circulars of interest to pilots are 00 6 Aviation Weather 00 24 00 30 OD 45 00 46 20 5 20 32 2D 35 2D 43 20 105 20 113 2D 125 1D 12 Thunderstorms Rules of Thumb for Avoiding or Minimizing Encounters with Clear Air Turbulance Aviation Weather Services A...

Page 231: ...ility of lndustry Developed Guide linas for the Conduct of the Biennial Flight Review The Accident Prevention Counselor Pro gram Pilot Transition Courses for Complex Single Engine and Light Twin Engine Air planes Flight Training Handbook Pilot s Handbook of Aeronautical Knowl edge Instrument Flying Handbook Hazards Associated with Spins in Airplanes Prohibited from lntentional Spinning Role of Pre...

Page 232: ...ng of Air Driven Gyroscopic lnstruments Use of Alternate Grades of Aviation Gaso line for Grade 80 87 and Use of Automotive Gasoline Noise Hearing Damage and Fatigue in Generał Aviation Pilots Unreliable Airspeed lndications Operational and Maintenance Practices for Emergency Locator Transmitters and Receivers Gyroscopic lnstruments Good Operating Practices Importance of Transpander Operations and...

Page 233: ...ards and General Aviation District Office to organize accident prevention program activities In addition there are over 3 000 volunteer airmen serving as accident prevention counselors sharing their technical expertise and professionar knowledge with the general aviation commu nity The FAA conducts seminars and workshops and dis tributes invaluable safety information under this program Usually the...

Page 234: ...ogram These can be obtained at FAA Offices Weather Stations Flight Service Stations or Airport Facilities Some of these are titled 12 Golden Rules for Pilots Weather or Not Disariantalion Plane Sense Weather lnfo Guide for Pilots Wake Turbulance Don t Trust to Luck Trust to Safety Rain Fog Snow Thunderstorm TRW lcing Pilot s Weather Briefing Guide Thunderstorms Don t Flirt Skirt em IFR VFR Either ...

Page 235: ...r maintenance regularly and have your air plane serviced by a repulabie organization Be suspicious of bargain prices for maintenance repair and inspections Ił is the responsibility of the owner and the operator to assure that the airplane is maintainad in an airworthy condi tion and that proper maintenance records are kepi Use only genuine BEECHCRAFT or BEECHCRAFT approved parts obtained from BEEC...

Page 236: ...y for malfunctions failures damaga or injury caused by use of non BEECHCRAFT parts Airplanes operated for Air Taxi or other than normai opera tion and airplanes operated in humid tropics or cold and damp climates etc may need mora frequent inspections for wear corrosion andlor lack of lubrication In these areas periodic inspections should be performed until the operator can set his own inspection ...

Page 237: ...s Before installing an STC on your airplane check to make sure that the STC does not conflict with other STC s that have already been installed Because approval of an STC is obtained by the individual STC holder based upon modification of the original type design it is possible for STC s to interfere with each other when both are installed Never install an unapproved modi fication of any type howe...

Page 238: ...t for quick reference lt is strongly recommended a flight plan be filed with Flight Service Sta tions even though the flight may be VFR Also advise Flight Service Stations of changes or delays of one hour or more and remember to close the flight plan at destination The pilot musi be completely familiar with the pertormance of the airplane and perlormance data in the Pilot s Operat ing Handbook and...

Page 239: ... displacement Ił hard solid objects are stored beneath seats the energy absorbing feature is lost and severe spinal injuries can occur to occupants Prior to flight pilots should insure that articles are not stowad beneath seats that would restrict seat pan energy absorption or penetrate the seat in event of a high vertical velocity accident FLIGHT OPERATIONS GENERAL The pilot MUST be thoroughly fa...

Page 240: ...mb the cruising speed and the ranga ot the airplane at any level of tuel will all be lower than shown in the Performance section lt an airplane is loaded so that the C G is forward of the tor ward limit it will require additional eontroi movements for maneuvering the airplane with correspondingly higher eon troi forces The pilot may have difficufty during takeoff and Ianding because ot the elevato...

Page 241: ...pplements Ensure a fuli understanding of the methods of engagement and disengagement of the autopi lot and trim systems Compare the descriptions and procedures eontainad in the Supplements to the actual installation in the airplane to ensure that the supplement accurately describes your instal lation Test that all buttons switches and circuit breakers function as described in the Supplements lf th...

Page 242: ...ystem malfunction The safest course is to deactivate both Do not re engage either system until after you have safely landed Then have the systems checked by a qualified service łacility prior to furthar flight Depending upon the installation on your airplane the follow ing additional methods may be available to disengage the autopilot or electric trim in the event that the autopilot or electric tr...

Page 243: ...ntrol ler if installed NOTE After the autopilot is positively disengaged it may be necessary to restore other electrlcal functions Be sure when the master switches are turnad on that the autopilot does not re engage The above ways may or may not be available on your auto pilot Ił is essential that you read your airplane s AFM SUPPLEMENT for your autopilot system and check each function and operatl...

Page 244: ...d so that fiutter will not occur in the normai operating envelope of the airplane as long as the airplane is properły maintained In the case ot any airplane decreasing the damping and stiffness ot the structure or increasing the trailing edge weight of eontroi surfaces will tend to cause flutter lf a combination of those tactors is suf ficient fiutter can occur within the normai operating enve lop...

Page 245: ...d trailing edge heavy eontroi surface and flutter Ił an excessive vibration particularly in the eontroi column and rudder pedals is encountered in flight this may be the onset of fiutter and the procedura to follow is 1 IMMEDIATELLY REDUCE AIRSPEED lower the Iand ing gear if necessary 2 RESTRAIN THE CONTROLS OF THE AIRPLANE UNTIL THE VISRATlON CEASES 3 FLY AT THE REDUCED AIRSPEED AND LAND AT THE N...

Page 246: ...control Occupants are thrown violently against the belts and back into the seat Unsecured objects are tossed about Occupants require seat belts and occasion ally are thrown against the belt Unsecured objects move about Occupants may be required to use seat belts but objects in the airplane remain at rest Thunderstorms squall lines and vialent turhulance should be regarded as extremely dangerous an...

Page 247: ...of struciurai damage or failure on the other hand if your air speed is too low you may stall lf turbulence is encountered reduce speed to the turbuleni air penetration speed if given or to the maneuvering speed which is listed in the Limitations section of the Pilot s Oper ating Handbook and FAA Approved Airplane Flight Manual These speeds give the best assurance of avoiding exces sive stress load...

Page 248: ...shears is far trom an exact science Monitor your airspeed carefully when flying near storms particularly on approach Be mentally prepared to add power and go around at the first indication that a wind shear is being encountered WEATHER RADAR Airborne weather avoidance radar is as its name implies for avoiding severe weather not for penetrating it Whether to tly into an area of radar echoes depends...

Page 249: ...least 40 miles before you fly between them With weaker echoes you can reduce the dislance by which you avoid them Above all remember this never regard any thunderstorm lightly Even when radar observers report the echoes are of light intensity avoiding thunderstorms is the best policy The following are some do s and don ts of thunderstorm avoid ance 1 Don t land or take off in the face of an approa...

Page 250: ...oose objects 10 Plan and hold your course to take you through the storm in minimum time 11 To avoid the most critical icing establish a penetration altitude below the freezing level or above the level of 15 C 12 Verify that pilot heat is on and turn on carburetor heat or engine anti ice lcing can be rapid at any altitude and causa almost instantaneous power failura andlor loss of airspeed indicati...

Page 251: ... mountain wave turbulence will not be encountered A mountain wave downdraft may exceed the climb capabiliły of your airplane Avoid mountain wave downdrafts VFR LOW CEILINGS lf you are not instrument rated do not attempt VFR on Top or Special VFR flight or clearances Being caught above a solid cloud layer when an emergency descent is required or at destination is an extremely hazardous position for...

Page 252: ...nd may confuse the pilot s conception of the attitude and position of his air plane Under VFR conditions the visual sense using the horizon as a reference can override the illusions Under low visibil ity conditions night fog clouds haze etc the illusions pre dominate Only through awareness of these illusions and proficiency in instrument flight procedures can an airplane be operated safely in a lo...

Page 253: ... discontinued as soon as possible The result of vertigo is loss of eontroi of the airplane lf the loss of eontroi is sustained it will result in an excessive speed accident Exeessive speed aeeidents occur in one of two manners either as an inflight airframe separalian or as a high speed ground impact and they are fatal accidents in either case Ali airplanes are subject to his form of accident For ...

Page 254: ...ts circuit breakers or fuses Compliance with this requirement is especially important in all high performance single engine airplanes during simulated angine out praclice or stall dem onstrations because the stall speed is critical in all low speed operation of airplanes Training should be accomplished under the supervision ot a qualified instructor pilot with caretui reference to the appli cable ...

Page 255: ...ib erately inducing a yawing moment with the controls as the airplane is stalled lnadvertent spins result from the same combination stall plus yaw That is why it is important to use coordinated controls and to recover at the first indication of a stall when practicing stalls Always remember that extra alertness and pilot techniques are required for slow flight maneuvers including the practice or d...

Page 256: ...n againsi an inadvertent spin MAINTAIN YOUR AIRSPEED In airplanes not certificated for aerobatics spins are prohib ited lf a spin is antered inadvertently lmmediately move the eontroi column fuli forward and simul taneously apply fuli rudder opposite to the direction of he spin continua to hold this position until rotation stops and hen neutralize all controls and execute a smooth pullout Ailerons...

Page 257: ...lane the more pronounced and turbulant the wakes will be Wing tip vortices from large heavy airplanes are very severe at close range degenerating with time wind and distance These are rolling in nature from each wing tip In tests vor tex velocities of 133 knots have been recorded Encounter ing the rolling effect of wing tip vortices within two minutes after passage of large airpfanes is most hazar...

Page 258: ...ys are also hazardous The pilot should also be alert to the possibility of the brakes freezing Use caution when Iaking off or Ianding during gusty wind conditions Also be aware of the special wind conditions caused by buildings or other obstructions located near the runway MEDICAL FACTS FOR PILOTS GENERAL When the pilot enters the airplane he becomes an integral part of the man machine system He i...

Page 259: ...not getting enough oxygen lt is impossible to predict when or where hypoxia will occur during a given flight or how it will manifest itself Some of he common symptoms of hypoxia are increased breathing rate a light headed or dizzy sensation tingling or warm sensation sweating reduced visual field sleepiness blue coloring of skin fingernails and lips and behavior changes A particu larly dangerous f...

Page 260: ...pplemental oxygen should be thoroughly tamiliar with the operation ot the airplane oxygen systems A preflight inspection ot the system should be peńormed including proper tit ot the mask The passengers should be brieted on the proper use ot their oxygen system betore flight Pilots who wear beards should be careful to ensure that their beard is caretully trimmed so that it will not interfere with p...

Page 261: ...toms elear and then resume nor mai breathing rate Normai breathing can be aided by taik ing aloud ALGOHOL Common sense and scientific evidence dietale that you must not fly as a crew member while under the influence of alcohol Alcohol even in smali amounts produces among other things A dulling of critical judgement A decreased sense of responsibility Diminished skill reactions and coordination Dec...

Page 262: ...r Even after the body completely destroys a moderate amount of alcohol a pilot can still be severely impaired for many hours by hangover The effects ot alcehol on the body are magnified at altitudes as 2 oz of alcehol at 18 000 feet produce the same adverse effects as 6 oz at sea level Federal Aviation Regulations have been amended to reflect the FAA s growing concern with the effects of alcehol i...

Page 263: ...r remedies and drugs such as aspirin anti histamines cold tablets cough mixtures laxatives tranquil izers and appetite suppressors may seriously impair the judgment and coordination needed while flying The safest rule is to take no medicine before or while flying except after eonsuitalion with your Aviation Medical Examiner SCUBA DtVING Flying shortly after any prolongad scuba diving could be dang...

Page 264: ...ient air pressure is reduced by climbing to higher alti tudes The symptoms are pain in the joints abdominal cramps burning sensations in the skin visual impairment and numbness Some of these symptoms are similar to hyp oxia The only known remedy for decompression sickness is recompression which can only be accomplished in an unpressurized airplane by descending The pilot should immediately descend...

Page 265: ...r RNAV LORAN sophisticated autopilols and other devices which just a few years ago were too large and pro hibitively expensive for generał aviation size airplanes are becoming increasingly commonplace in even the smallest airplanes l lt is thus that this Safety lnformation is directed to the pilOt for it is in the area of the skill and proficiency of you the pirot that the graatest gains in safe f...

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Page 267: ... U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

Page 268: ...U N C O T R O L L E D C O P Y N O T F O R O P E R A T I O N A L U S E ...

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Beechcraft Musketeer Sport III A23-19, Pilot Operating Handbook

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Summary of Contents for Musketeer Sport III A23-19

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