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BEECHCRAFT MODEL 17

Beechcraft 99 Airliner · Wiring Diagram

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Overview

This document is a wiring diagram for the Beechcraft Model 17. It provides detailed instructions and specifications for the electrical systems, rigging, and adjustments necessary for the aircraft's operation and maintenance. The manual is intended for use by technicians and pilots who require a comprehensive understanding of the aircraft's wiring and systems. It includes sections on rigging, major assemblies, electrical systems, specifications, and performance data, ensuring that users have access to all necessary information for safe and effective operation.

  • The Beechcraft Model 17 requires precise rigging of flaps and ailerons for safe operation.
  • Electrical systems are detailed with wiring diagrams for troubleshooting.
  • Performance data includes critical metrics like speed and fuel consumption for flight planning.
  • Regular maintenance and adjustments are necessary to ensure aircraft safety and performance.
  • The manual includes exploded views of major assemblies for reference during repairs.

Document

Source

Originally published by mcr01.ch. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Wiring Diagram
Pages
108
File size
5.9 MB
Publisher
mcr01.ch
Documentation completeness
3/7

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In this document

Rigging and Adjusting

This section covers the rigging of various components such as flaps, ailerons, wings, elevator, rudder, and landing gear. It includes detailed procedures for adjusting these components to ensure proper functionality and safety during flight.

Major Assemblies

This section provides an overview of the major assemblies of the Beechcraft Model 17, including the wing assembly, landing gear, and tailwheel assembly. It includes exploded views and part numbers for reference.

Electrical Systems

This section details the electrical systems of the aircraft, including wiring diagrams and specifications for various components. It is crucial for troubleshooting and maintenance of the aircraft's electrical systems.

Specifications, Repair, and Basic Maintenance

This section outlines the specifications for the Beechcraft Model 17, including dimensions, weight, and performance data. It also provides guidelines for basic maintenance and repair procedures.

Performance Data

This section includes performance data for the Beechcraft Model 17, such as speed, range, and fuel consumption. It is essential for pilots to understand these metrics for effective flight planning.

Safety notes

  • Ensure all rigging is performed according to specifications to avoid flight issues.
  • Electrical systems should be checked regularly for faults to prevent failures during flight.

Full document text

-l-l-l-l-l BEE[HIRAFT -l-l -l-l r-l r-lttt.l MODEL 17 I EilOIIIEERIIIG FIETD SERVICE DI'lISIOI{. . BEECll IIRCRAIT CORPORATIOl{. O IIICIlITA, I(Ail$AS t_i t____. L t-r_r t_-l; l- BEE[HCRAFT 17 SECTION I-RIGGING AND ADJUSTING Farcs I to 15 ìneløívc SECTION II-MAJOR ASSEMBLIES Fafct tó te 26 ínclutíve SECTION III-ELECTRICAL SYSTEMS Fa,rct 27 to 34 ïneluüvc SECTION IV_SPECIFICATIONS, REPAIR AND BASIC MAINTENANCE Fa,f! 35 to 4l ínclutìve SECTION V-PERFORMANCE DATA Faîet ln to 47 ínclutívc MODEL D SERVICE AND OPERATION DATA PullÍtl'el ly t/'c ENGINEERING SERVICE DEPARTMENT BEECH AIRCRAFT CORPORATION WICHIT^ã., KÃNSJ{''S Ptìce $2.5O sEcTtoN I RIGGING AND ADJUSTING RIGGING FLAPS RIGGING AILERONS HANGING ITINGS RIGGING WINGS RIGGING ELEVATOR RIGGING ELEVATOR TABS RIGGING RUDDERS RIGGING RUDDER TABS RIGGING LANDING GEAR RETRACT CHAINS RIGGING LANDING GEAR AND ADJUSTING RETRACT CHAINS RIGGING MAIN LANDING GEAR FAIRING RIGGING TAIL \IHEEL AND TAILIIHEEL DOORS RIGGING THROTTLE STOPS ADJUSTING BRAKES BRAKE BLEEDING PROCEDURE I i I l I I 1 I I 1 I I L tI ! 'f ì ( r ! BEECHCRAFT MODEL T7 t43"o INCREASE "UP'' TRAVEL INCREASE TRAVEL DECREASE'UP'' IRAVEL f ot*t^tt t*^,rt. 3.DISCONNECÍ LEFÍ fLAP SHAFÍ HOUS. ING AT LEFT SIDE OF FLAP MOÏOR AND REPEAT OPERATIONS f OLLOVED IN ADJUSTING RIGHI FLAP. ,1. TO ADJUÍ LlMlf SVIICH RUN FLAP rO FULL 'UP" POSITION ELECTRICALLY. TO INCREASE "UP" IRAVEL;TURN FOR- VARD JAM NUTS IOVARD ÍORVARD END OF BOLT. TO DÉCREASE'UP'' TRAVÊI, TURN FORVARD .lAM NUTS IN DIRECIION OT CEN'ÍER OF BOLI. 5. OPER,\TÊ FLAP TO ruLL'DO\VN" POSI- ÍON. CORRECT 'DOVN'ÌRAVEL IS 43'1l". TO INCREASE rRAvEL, TURN REAR JAM NI.'Ts TOVARD AFf END OF BOLÍ. TO DECREASE TRAVEL TURN JAM NI'TS IN DIRECNON Of CENTER OF BOLT 9. S€f RIGHI TLAP IN NEUTRAL POSITION BY ROÍAÍING SI{ATT COUNTER CLOCK. VISE TO RAISE TRAILING EDGE OF fLAP Oß CLOCKVISE TO LOVER TRAILING EDGE OI FLAP. VITH RIGHÍ FLAP IN NÊUTRAL 'UP" POSIIION CONNECT sI{AFT AND HOUSING AT RIGHÎ OI FLAP MOTOR. ó. VfiU FLAP ADJT,SIED IO PROPER ELEC. TRICAL IRAVEL, SEf SCREV LO(ATED IN BLOCI( AT RIGHT OF fLAP SCREV SHOUT.D BE SEI SNUG AGAINSÍ (EN. IER FLAP HINGÊ ERACI(EI. sEf scREw br ÍtG. 7 SHOULD 8f TOOSfNED SEFORI /N fÎavEL ot flGGTNG FI,APS SHOUID JAM WHILE ADJUSI'NG. IEMOYE 8O¿TS ÁT e, SC¡EW TNÞ ffD IUIN sWIÌCH OPPOSIÎE OF JÂA'I AND IAP SC¡EW END WfrH iAAUN C,ARÉ SHOUT"D 8Ê TAKSN TO AYOID C¡OSS IH¡EÂD'ITG WflEN coNNÊc1,NG s¡tafr NUts ro ^10fo¡ 1. DISCONNÉCI FLAP SHAff HOUSING '\T RIGHÍ SIDE OT FLAP MOTOR. Aff6R fIAPS ANE RIGGED. SHAF' NT,'S AT MOTON 5'íOU1O 8E SAFfl'fD RIGGING FLAPS 7. TIGHIEN JAM NUÍS ON SEf SCREV SIOP. I Í I I I I i J I L { I I I l ¡ L- ç i f I I i I i ( I I f I I I I f I BEECHCRAFT MODEL IZ 3(r 1 9. UP. e5'1 r" DovN. MAKE UP AILERON CAELES LEAVING ¡Þpnoxru¡tetv rHREE fHREADS SHOVING ON EACH END OF'I}IE IOUß IURNBUCI(LES LOCAIf,D JUsf OT'TBOARD TROM TI.ISEIAGÉ IN VING. TURNBUCKLES ARE ACCESgBLE THROUGH INSPECTION DOORS. 9"t*y €tl Tazn["cll¿t '. SET AILERONS AND CONIROL I{/HEEL IN NEUTRAL. ON PILOI'S SIDE ONLY S€T CONIßOL VHEEL IN NEUTRAL. AIIIRON SHO{'lI' BE IN NEUTRAL. IF NECESSAR¿ MAKE 5UGHT AD- JUÍMENTS ON ALENON CABTES AND RECHECI( IENSION. 3. ÍIGHTEN IURNEUCKLES EVENLY, KEEP. ING AILERONS AND CONTROL VHEÊL IN NEUIRAL, UNIIL CORRECÍ CABLE ÍENION IS OBTAINED. 4. AILERON CAELEIÊNSTONTS 45 È5 POUNDS õENSION SFIOULD BE sET AÌ 55. IEMPERATURE.) AILERON RIGGING BEECHCRAFT MODEL TZ PREPARATION 1, REMOVE OUTBOARD INSPECÍION PL,\ÍE ON UPPER VING IOP OUTBO,{RD SUR. FACE. 5. REMOVE OUTBOARD INSPECTION PLAIE ON LOVER SURFACÉ OF LOWER VING 9. INSERT L. H. THREADED END OF *,i" FLY. ING WIRES THROUGH HOLES IN UPPER WING OUÍBOARD SPAR TRUNNION. ó. INSERT R. H. IHREADED END OF r6e' LANDING WIRES THROUGH HOLES IN OUIBOARD SPAR TRUNNION. 3. INSIALL BALL SEAT V/ASHER, STAI IO TRUNNION, AND ADJUSÍ JAM NUIS IO ALLOW TVO. THREADS SHOIIING TROM END OF VIRE TO FIRSÍ JAM NUT, ,I. INSIALL "I" SfRUI ON UPPER VING, IIING UPSIDE DOIIN. 8E SURE ADJUSIMENÍ NUÍS AND EALL SET WASHERS ARÊ INIALLED CORRECTLY. 7. INIALL BALL SEAT WASHER, SEAI TO IRUNNION, AND ADJUST JAM NUIS TO ALLOW C,ú" OF ÍHRÉAÞ5 SHOVING FROM END OF VIRE IO FIRST JAM NUT, rT. INSTALL ''t" STRUT BOLIs, FORVARD BOLI FIRsI, IN LOVÊR VING, I3. INÍALL UPPER ÊNDS OT I'LANDING WIRES IN UPPER FUSELAGE TRUNNION. ASSEMBLY 8. CONNÊCT PITO¡ LINES AND GAS LINE AT WPER LEFT fRONI HINGE FTNNG. OF C) f 9. ¡NSTALL UPPER VING HINGE 8OLI5- TT. INÍALL LOVER VING HINGE BOLTS E HEADS OT EOLTS AT TRONT SHOULÐ FACE REAR. HEAm iDF 8OLT5 AT REAR SHOULD FACË FOftVARD. 14. INÍALL LOVER ENDS OF %' tLvlNG VIRES lN LOVER Ft SEL,\GE ÍRUNNION' rs.ADJUSÍ'I"SIRUTADJUSTMENTBOLÍTOALLOVI'OFfHREADSSHOVINGFßOMENDOf BOLT TO FIRÍ ,lAM NI'T. HANGING WINGS BEECHCRAFT MODEL Iz MEASURE FROM ÍRAILING EDGÊ OF g vtNG ÌP foRv^RD 3o%' AND AS SHOWN IN ILLUSIRATION. SIRETCH OIHEDRAL CHECK SIRING FROM VING TIP IO VING IIP. SIRING MUST CROSS DIRECILY OVÊR POINTSMA¡KED 30%'FROM VING TIP TRAILING EDGES. ø o P g ô ó. VR,\P LANDING VIRES VfIH THNEE IURNS OF tRKllON IAPE ¿\ND Y/RAP rLvrNG vtREs vfm rvo runNs ot TAPE, rHÉN INSTALL FLYING VIRE SPREADER AT VIRE INÍERSECTION. LANDING VIRES trlus¡RliloN srows ß,Glll H ND WüitG f¡OÁ{ ¡€ÁR 5. L,\NDING VIRES VlLl AUTOMATI- CALLY HAVE APPNOXIMATILY T'95 LBS. OF IENS¡ON. CHECK EOTH VIRES FOR EOUAL IENgON. 7. CHECK ALL VIRES FOR CLEATANCE THROUGH VING SXIN ^ND INSTALL FLYING VIRE VING TAIRINGS. 3. TIGHIEN 5 .Ió" LANDING VIRES EVCNLY UNTIL SIRING CLEARS TUSELAGE ? 8- AT A POINÌ I " INEOARD Of TUSELAGÊ LEN ¡. flGHlEN 3^' ÍLYING v4REs lO 1150 LBS. Of TEN$ON. IHIS VILL REDUCE THE AND RIGT{Í EXTREMIIIES. (SIRING MUST STREICHED TIGHT.) É06É CLE,\RANCE OT IHE sfRrNG FROM /8" TO APPROXIMA¡ELY AS t/t GIVEN IN SIEP 3 \ ¡sÉ eO'6É 116tl1Éì¡Éo NorÊ, rr rs pe¡urssrglÈ to DIHEDRAL ON UPPER VINGS IF NECESSARY IO CLEAR THE CABIN DOOR. INCREASE ?/8' D|M€NS|ON-tN SIEP 3. RIGGING WINGS { a I f i r 1 I I r BEECHCRAFT MODEL Tz , I r. CORRECT TRAVEL OF ELEVATO 15 MAINTAINED BY ELEVATOR CONIROL COLUMN CHECK CABLES.

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9. SELECI BOLT HOLE IN IORVARD CHECX C^BLE ERACI(FT IO OBIAIN CLE^R- ANCE OF AT LEAST %" BETVEEN CON. TROL COLUMN AND INSTRUMENT PANEL VHEN CONTROL COLUMN IS IN FULL FORVARD POSITION. 3. HOLD CONIROL COLUMN IN fULL FOR. VARD POSITION, AND AD.,UsI ELE. VATOR CAELES TO OETAIN CORRECÍ DOVN IRAVEL(98'19) ON ELÊVATOR. 4.n¡ut ELrv¡roR coNTRoL coLUMN BACK UNTIL ELEVATOR HAS CORRECT "uP" TRAVEL (30"i t) AND ADJUSÍ CONÎROL COLUMN CHECK C,\81E. OBÎAIN TÊNS¡ON BY ADJUSÍM€NT OF EACH TURNBUCKLE. ó. ó5Ì 5 POUNDS ON LOVER CABLES SAFETY IURNBTJCKLËs. 5. ADJUÍ ELEVATOR CONIROL CABLES UN¡IL CORRECI TENSION IS OSIAINED. 7. VORK ELEVATOQ SEVERAL TIM€S AND RECHECK ELEVATOR FOR CORRÊCÌ IRAVEL ^ND CABLE IEN9ON. USÊ 18 GAUGE SAFEÌY VNE S"t"ty €ll l"znl,"câlot 3o"t ?' UP r'.+?. DOVN ELEVATOR RIGGING BEECHCRAFT MODEL 17 I. REMOVE Dl ELEVAIOR 7777 TAPEI, PINS THROUGH TÂ8 SHAFT AND SLIDE TO ONÊ SIDE fAR ENOUCH TA8 CABLE. COUPLING TO ADMIT 5. INSÎALL S7I BOWDEN HOUSING CAR- RIER SPRINC. CHECK FOR CLEA¡,ANCE OF SPR¡NG AND BOVDÊN HOUSING ¡N REAR ÍUSELAGE, OPERATING ELEVATOR TO FULL UP AND DOWN EXTREMES. t. 2. AD'UST SPLICE ON RUDDER TA8 CABLE TO OETAIN CLEARANCE OF APPROXI. I,t t MAIELY TV/O INCHES BEIWEEN CAELE SPLICE AND FORWARD END OF BOV- DEN HOUSING. OPERATE TAB TO BOTH EXTREMES AND RECHECK CLEARANCC 8ET\¡r'EEN SPLICE AND IND OF BOV- DEN HOUSINC. 14t4' 1 4Y2" e'uP. e" DOWN. 6. CONNECÎ lAB POSITION INDICÀÌOR \À/IRES AT 1A¡ INDICATOR RHEOSTAT IERMINALS. ADJUST CLEVIS ON IAB CONNECTING ROD TO OBÍAIN CORRECT ÍRAVEL. 3. INSTALL ¡LEVAIOR TA8 BOVDEN IIOUSINC IIIROUGH 8OVDEN HOUS- rNc Mot NTrNc StacKEls. CAUTIONI TIGHÍEN BOVDEN ING NUTS ONLY TILL SNUG. HOUS- 7. WITH TABS SET IN NEUTRAL POSITION, .ADIUST INDTCATOR RHEOSTAT TO SHOV NEUTRAL ON ÞIAL. THIS AD- IUSTMENT IS OBÎAINED BY ROTATINC VORM CEAR ON RHEOsTAT W¡TH RHEOSTAT LOWIRED IN MOUNTING 8R,ACKET. AñÎER NEUTRAL POSITION Õ t 't. 4. ROUTE TAB CÂ8LC TH*'OUGH TA8 PULLEY AND ADIUST TO PROPER TEN- SION. CASLE TENSION IS OBTAINED BY ADIUSTING BOWDEN HOUSING AT MouNÍtNc BRACKETS. Rlc caBLEs ro FREE BUf POSIIIVE TENSION. CI{ECK fO SEE THAT DIRECNON Of TNAVEL TAB VILL CORRESPOND VITH IHAT OF INDICATOR. t I 8. V¡TH TABS AND RHEOSTAT IN NEU. TRÂL FOSITION. ANCHOR VOTM GEAR oN lAB SHAFT EY DRILLINC l,/16 INCH HOLE ÎHROUCH SHAFT ÂND CON. NËCTING COLLAR AND INSTALLING ¡02809-062-016 PlN. rose\. DOWN Nost \)P /' É. L Ê I o R I B s f--o \\1 RIGGING ELEVATOR TABS fI L_ { I ; f i f ì r, I f l I I I L I I { { { I L { I i II I tr t BEECHCRAFT MODEL TZ t8' t 9' r. RIG RUDD€R STOP CA8LEs TO OEIAIN CORRECÍ RUDDER NAVEL, 'A LEFÎ AND RIGHT. NOIE. RUODER HORN MUsf CLEAR TIN SPAR VHEN FULL'ÍRAVEL IS OETAINED- ', MANÊ UP RUDDER CAELE ÍURNEUCXLES LEAVING APPROXIMAÏELY THREE I}IREADS SHOVING ON BOTH ÉNDS OF THE IURNBUCI(LÊ- S"f.ty Qll î"¿"tacltct 'S GAreE SAFEÎY VIRE ON RUDDER CA8LE9 S GAUGE SAFÊÍY VRE ON NUDæI SÍOP CABLE a VfTH RUDDÉR IN NEUIRAL, ÏIGHT€N CABLES UNTIL PILOT'S AND CO.PILOÍ'S PED^LS ARE CENIERED TOßE AND AFf IN IHE RUDDER PÉDAL SLOIS. 5. NlG BRAKÊ BALANCE CABLE VTTH JUST ENOIJGH IENSION TO REMOVE ALL SLACI( FROM CABLE, X=Y RTGGING RUDDERS BEECHCRAFT MODEL IT I, OPERATINC RUDD¡R TAB IO ¡OTH EXTREME5, ADIUST SPLICE IN CAELE TO CLEAR FOiV/ARD END OF BOWDEN HOUSINC A'PNOXIMATELY 1}IREE INCHES. 5. txsTAtL 755-12 CLÂMP A,ND 755-4 CLAMP. CHECI( FOR CLIARANCT Of SOVDTN HOUSING IN IEAT ¡USELAGE, OPÊR,ÀÍ INC RUDOET FULL EXTREMES. AND TA8 TO 2. ¡NSTALL EOVDEN HOUSING IN CAR. RI¡T ERACKETS. .*tt'tJ3$$ol{t' $oÙ5' ADJUST CLEVIS ON IAB CONNECIING ROD TO OSIAIN CORRECT IRAVEL 3. ROUTE IA8 CAELE THROUGH TA3 IREMÊ RICHI OR LEFT SPOND WITH SPLICÊ ON so SPLICE u/¡LL CLTAR END OI TOVDEN HOUSINC USINC FULL IRÂVEL.) "o*o"* iI. ADIUSf CAIL¡ TO PROPET TENS¡ON IAPPN,OXIMATELY 40 L¡S.). THIS AD- IUSTMENI IS MAD¡ ãY ADIUSTINC BOWDEN HOUSING AT MOUNTINC ERACI(TTS. ICAALE MUST HAVE SUFFI. CIENÌ TENSION TO PiEVENf CAELE SLIPPING AI TXTIEMT ENDS OF TRAVEL.) RIGHT 90 ù 9 LEn!Oa? ¡ËfER- to cÂ3r€ DIaGRA^i FOR ENrnE SYSÍE { RIGGING RUDDER TABS 6. ADIUST CAELE IN PULLEY ÌO SHOV coiREcT Tn,AVEL RIGHT AND L¡FT COT,RESPONDINC VIIH PLACARD AT coNtnol tN ca8lN. I I J I I I¡ r I I f i I I i f I I L- ( I j ! f I Í I L. BEECHCRAFT MODEL Iz I r. HOIST OR JÀCK AIRPLANE AND SLOCK LOWER VINGS AT STRIJT POINTS SETORE CHECKING LANÞING GEAR. GEAR CAN BE OPERATED MANUAILY !ÛIITH MASIER SV/ITCH OFF OR ELECÌRICALLY VIIH MASÍER svtlcH oN. '. ROLL LANDING GEAR UP UNNL LANDING GEAR SLIDE CLEARS THROTfLE STOP APPROXIMAIELY ONE INCH. 3. TIGHÏEN LANDING GEAR CHAIN EYE BOIT UNÏIL CHAIN DOES NOI DRAG ON SLID€ TUBE, YEI OPERAIES FREÊLY. q 5. IF ONE SLIDE IS I{IGHER. INBOARD ÊYEBOLT AND LOOSTN THE IreH¡EN THE 4. CHÊCK SYNCHßONIZATION OF IHE RIGHT AND LEFf SLIDES. Ot'ÍBOARD BOLT AN ÊVEN NUMDÊR Of ruRNs UNNL SIJO€S ARE SYN- CHRONIZED A1 EXIENDGD POS¡TION. 6. RUN LANDING GEAR SEVERAL TIMES THEN RECHECX SìI/NCHRONZANON OF SLIDES RIGGING Lr\NDING GEAR RETRACT CHAINS BEECHCRAFT MODEL Iz I. AIRPLANE SHOULD BE IN HOISTED POSTTTON OR ON WrñG J^CKS. 3 2- ÂDrusT lov¡r. LIMIT svlrcH 8Y AD.DING OR ßEMOVINC SHIMS TO RAISE OR LOVER. BOLT }iEAD IN LIMIÎ S\VITCH ACTUATOR MOUNTINC ERACKET AT RIGHT SIDË OF SLIDE ON SLIDE TUBE. 3. ADIUST LOWER SWITCH TO EREAK c¡iculr oN ltlE THIRD To LÂsr NOÎCH OF TRAVEL OF RÀTCHET DOGS ON RATCHÊT cOG \¡¡lHlEL. 4. RUN CEAR TRICALLY EXTENDED ALL THE WAY DO\IN ELEC. AND VITH CEAR IN FULLY POSITION, CHECK RATCHET SUN.E DOCS ARE FULLY EN- COG VHIEL ON RATCHET. 5. POSITION OF RAÍCHET COC WHEEL MAY BE CHANCED 8Y ADIUSTING IAM NUTS AN EVEN NUMSÊT, Of TURNS ON lOP AND LOVER LANDINC CEAR 6. AOIUSTMENTOF UPPER LrMrT SV/ITCH IS MADE 8Y MOVINC ENTIR€ SVITCH 8OX UP OR DOVN IN SLOTÌEÞ HOLIS IN MOUNTING 8N,ACKET. TO MAI(E CAGED IN CHAINS. LA6T NOTCH NEXT TO LAST 7. UPPEN, LIMIT SVITCH SHOULD 8E AD- IUSÎEO TO EREAK CIN,CUIT HALF VAY .EEIWEEN THE LAST AND NEXÎ TO LAST NOÌCH OF TRAVEL OF RATC¡IËT DOGS ON RATCHET COC WHEIL. 8. TRAVEL OF LEFT LANDINC CEAR CHAIN SHOULD 8E SYNCHRONIZED VITH RIGHI. RIGGING MAIN LANDING GEAR AND ADJUSTING LIMIT SWITCHES 9. OPERATE GEAR SEVÊRAL TIMES ÊLEC- TRICALLY AND CHÊCK TO 8E SURE SL¡DE IS USING FULL TRAVET ON SLIDE TU8E, AND fHAT R,AICHTI DOGS ATE FULLY ENGÂGID ON RAÍCHEf COG VHIEL. BEECHCRAFT MODEL IT .a r. HOIST AIRPLANE- '. REÎRACI LANDING GEAR TO FULL"UP'' POS|TTON Al.tD CHECK CABLE TENS|ON ON HINGED DOOR. 3. ADJIJST DOOR BY TIGHTENING IURN. BUCKLE TO TNCREASE 'ENgON ON DOOR OR BY LOOSENING TI¡RIÈ BUCKLE IO RELIEVE TENSION. o o fr rl ó. PLACE VASHER AND FERRULE Sh¡UG AGAINÍ INBOARD CABLE FAIRLEAD AND SOLDER ¡N PLACE. ¡1. EXIEND GEAR tO FULL DOVN pOSÛtON. PLACE DOOR AT A 9O ANGLE VJÍH MAIN VHTEL fAIRING. 5, HOLDING DOOR AT 90" ANGLE VITH â'ålâ,ñ'¿f,¡f,ftikP,Eârdft L?,e MAIN VHEEL FAIRING, PULL CABLE TIGHT AT INBOARD END. RIGGING MAIN LANDING GEAR FAIRING r I ! i BEECHCRAFT MODEL Iz I. HCIsT AIRPLANE. 4. CHÊCK AUTOMAIICÂLLY i ÊRLY ROUTINC SHOCX CORD.} tr SAFffY ruRNEUCKLES ONLY ON ÎAIL VH€EL SIDÊ OF BARREL. aDrusl TÁILWHEEL SLtO€ ON SLTDE TUEE TO ALLOV APPROXIMATELY l/32 |NCH OF CLEAIANCI SETWEEN AFT END OF SLIDE AND SLIDÊ TUEE MOUNÎ AT AFl END OF SLIOË IU8T. 5. TAILVHEEL DOORS SHOULD 8Ë N,IGGED TO FIT SNUG IO CONTOUR OF REAR FUSELÂGE. ADIUSTMENI IS MADÊ BY USE OF THE TVO IURNSUCI(LES LO- CATED IN TII¡ CENTER OF THE DOON, ACTUATOR ARMs. 2. ADIUST TRAVTL OF SL¡DC ON SLIDE TUBE 8Y TURNINC TURNBUCI(LE, LO- CATED IUST Afl OF EAGCAGE COM" PARTMENT, TO RICHÎ OR LÈfT. RIGGING TAIL \ÙIHEEL AND TAIL WHEEL DOORS l8- BEECHCRAFT MODEL 17 I úI. INSTAIL PLUNCER ENÞ OF CONÎROL IN MOUNTINC BRACKTT AT RICHT REAR OT CARBUREIOR. 6. OPERATE LANDING GEAR UP AND DOVN SEVERAL TIMES ELECTRICALLY- WITH GEAR FULLY EXIENDED. PLUNCER AT THROÍTLE Aß,M SHOULD IO CHECK IHÂOΡIÊ slOP IO¿t GEAÎ 7¿ " ÊRO^l PTUNGEN [OCÅ'€D A' TOW€N fND OF TEFÍ HAND 5¿'D! lUBf IRfFÊR fO FIGUIE 5 PAGE 9). oP€N THRO]TIE Â80Uf ItA¿t-7HEN CTOSE- ROIT G€Á¡ CTEAN DOWN_IHROIT¿É SHOUIO CTOSE ÂNOTHER 7¡". 2, CUT PLUNGEß OFF AT END OF CON. TR,OL IUST LONG ÊNOU6I{ TO CLEAR THR,OTÍLE ARM A?PROXIMATELY ¡ 8 INCH. I 000 5. }IOLDING WIRE IN THIS POSITION, B¡ND WIRE AROUND EOLT LOCATED IN lHC END OF ACTUATING PLUNCÊR AT fHE INBOAßD ÉND OF LETT DIAG- ONAL LIFI LEG AND IIG¡ITIN DOVN NUT. SINO UP OR DO\YN 4. VITH GEAN. FULLY EXTËNED, PULL VIRE THRU BOWDEN HOUS]NG IUSI IIGIIÎ ENOUGH TO RÊÎRACT PI.UNGER + AI IH¡OITLÊ ÂRM. 3. VIIH PLUNCER FULLY EXI¡NDED, AND ÎHROTTLE ARM SNUC AGAINSÏ ?LUNG¡R, ADIUST CONTROL MOUNT- ING IRACXET UP ON, DOVN UNTIL CLE nANcË oF 9o/lo0o ls OBfalN:D EITVEIN ADIUSTINC SCnEV AND sToPs. RIGGING TH ROTTLE STOPS BEECHCRAFT MODEL .T 2. DISCONNECT BRAKE LINE AT VHEEL 4. Ì,EMOVE AXLE ASSEMELY. ÁND ENTITE VHEEL DT,UM. I. HOIST AIRPLANE. 3. REMOVE INSPECTION PLATE ON Y/'HEEL FAIRING, ALVAYS DETLATE TIR,Es BEFORE DOING ANY VORK ON VHEELS- 7. VASH ALL PARÎS OF BRAI(E UNIT VIÎH INDUSTRIAL OR DENATUR€D ALCOHOL. DO NOT USE WOOD ALCO- IIOL, OIL OR GASOLINC ON BRAKÊ UNIT OR PARTS. .a €,' o '4 e, 8. REASSEMBI.E PARÎS OF ERAKE UNIT IN THE ORDER SHOVN IN ILLUSTRA. TION, CARTFULLY INSPÊCTING EACH PAR,T FOR DEFECTS. CHECK PISTON SEAL FOR CRACKS. CHECK ALL DISCS FOR IIEAR AND ALIGNMENT. VANPED DISCS MUSÍ BE REPLACÊD. SAFETY EACH OF THf THREE RETUIN SPRINGS. ,9 ,Ð 6, DISASSËM8LE BRAKE UNIT 1. BIEEDER PLUG AND CAP. t. PtsroN SEAL. 3. P|STON. 4. ASSEMSLÊD ERAI(E UNTT. 5- ROTATING ERONZE DISC. ó. SATIONARY 9ÍEEL DISC. 7. RflAINING AND ADJUÍMEN] 8. RETAINING Nt,T LOCK S<NEV" 9. ASSESTOS INSULAÍOR Þlsc. r0. RgluiN *¡lNGs. 1t- tcvs foR sfE¡L Dlscs. IT. SAL EXP.^NSION SPRING. tr- ANCHOR 8n^CKEI (Aslþao, 14- tNLEl. NtJI 1år*-.\ 5. REMOVE ASSEMBLCD FROM VHCEL. BNAKE UNIT è) .:!tç rh "t.{ q¡t PLACE STEEL DÍSC FIRSI, SECOND. DISC IS ERONZE, THIRD,-ÍEEL, EIC. 9. USING FOUN, IO. ROIATÊ TO LEÍT fOR RE. II. INSTALL ASSEMBLED BRAI(Ë UNIT IN VHE¡L. 12. INSTALL VHEEL ON AIRPLAN€. SAFETY LOCK NUÌ ON ÂXLE. I3. FLUSH SRAXE HYDRAULIC LINE FßOM TOP TO BOTTOM VITH CLIAN BR.AKE FLUID OF SAME SPECIÍICAIION USED IN SYSTCM. IiI. CONNECT HYDRAULIC LINE AT FLUID INLET ON SRAI(€ DßUM. sRAKE TO HAVE TO FIRST IAINING NUT LOCK SCREV AND SETVTEN ADIUSTMENI NUT FACTNC ST!ÊL DISC. INSTALL LOCK SC¡,E\y. ADJUSTING BRAKES I l ,| i i I f I f I I I I r I I f I I I i ( I Í { f I I BEECHCRAFT MODEL IT F F ø wV,r¿ \\ 5. DISCONNECT SIEEDER POI AT SUP. PLY TANK CONNECTION. AÏ COM. PLETION OF ELEEDER PROCËDURE SUPPLY TANK MUST 8É ßETVEÊN I/2 AND '/4 FULL. 3, DEPRESS ERAXE PEDAL SEVENAL TIMES DURING SLÊÉDINC PROCESS TO BÊ SUR.E NO AIR FOCKEÍS AC. CUMULATE IN MASTTR CYLINDER. * 4. VHEN LONGER CLOSE PLUG5. HOSTS AT \THEEL ¡EPLACE CAP CH¡CI( VENT TO BE SUTE 11 IS OPEN AND FR,EE IN,OM D]RÎ 2. AITACH HOSE FROM BLEEDER POI TO SUPPLY LINE. USING A MAXIMUM OF 15 LBS, OF AIR PRESSURE IN BLEEDER POT. sfARl FLOV OF ERAKE FLUID IHROUGH SYSTEM. BR,{KES MAY BE BLED 8Y SAME PROCESS WIIHOUT USE OF AIR. SUPPLY IANK 15 KEPT FILLED VITH OIL VHILE PUMPING BRAKE PEDALS. AFTER BRAKES ARE BLED, LINES CAN BE CHECKED FOR LEAKS BY SETTING HAND BRAKE. I. RÊMOVË CAP SCREV FROM PLUC AND INSÊNT IN ITS PLACE A sLEEDER HOSE. PLACE LOOSE INDS OF SLEEDER HOSES IN CLEAN GLA55 JUGs, SO IHAT ÎHEY ARE SUBMERGTD IN OIL ]¿ INCH. BRAKE BLEEDING PROCEDURE I I t- II I L_ I t I t ( i L t I I L ( I t (- f I I L_ rI L i_ íI L (I L ( I I i_ tI L sEciloN il MAJOR ASSEMBLIES EXPLODED AIRPLANE WING ASSEMBLY UPPER WING ASSEMBLY LOWER LANDING GEAR AND TAILWHEEL LOCK ASSEMBLY TAILWHEEL ASSEMBLY RUDDER AND ELEVATOR ASSEMBLIES FLAP SCREV AND LIMIT SWITCH COLUMN CONTROL ASSEMBLY ENGINE CONTROL SYSTEM NSTALLATION-R'EL SYSTEM INSTALLATION - OIL SYSTEM EXPLODED VIEW I. DI753O STRUT ASSEMBLY_ I r. MN?OC LOOP_ANIENNAE 3. R985 AN-f OR AN.g ENGINE 4. D171OOó V¡NG ASSEMBLY_UPPER LEFT 5. Df 70890 MAT.-LEFT VING Vr\LK ó- Dl?o8el Mi\T.-RIGHT VING VAIJ( 7. 6167A.15 BLADE _ PROPELLER S. TCL3O HUB-PROPELLÊR 9. DI7O9ó SPREADER-INTERPLANE VIRE 10. D17IOO1 VING ASSEMBLY_UPPER RIGHT 11. DI71OO4 L.H. WNG ASSEMBLY_LOVER LEFT f 9. DI71OO4 R.H. WNG ASSEMBLY_LOVER RrcHT f 3. D175'95 FAIRING-I STRUT LOVER R€AR t4. DrTSel50 SCOOP ASSEMBLv-CAREUnrron An 15. DI753O9 FAIRING ASSEMELY_I SIRUÍ UPPER tó. Dl753ro FAIRING ASSEMBLy- I S[Rttf LOTVER 11. D17543+1 & .2 FILLET_LOVER VING REAR 18. DI71711 PLATE-BELLY INSPECÍION 19. D171749 TUBE ASSEMELY_HEATED PÍTOT '0. D17175.1 PLATE-EXTERNAL TIE ROD UPPER ROOT et. Dl7393r covER-cABlN VENÏ 99. DI75O47 BULKHEAD ASEMBLY_FRONT 93. D175950 DOOR ASSEMBLY-BAGGAGE 14, DITÍ óO L.H. FLAP ASSEMBLY_L.H- i5. DITIóO R.H. FLAP ASSEMELY_R.H. 2ó. DI7I3O L.H, AILERON '\SSEMBLY_L.H. '7. D17130 R.H, AILERON ASSEMBLY-R.H. 28. D17544t STRIP_VING WALK TAIRING L.H. 19. D1r545o SHEET-SIDE 30. Df 75597 STRIP_VING ROOT FAIRING UPPER L.H' 31. DI7559?.I SÍRIP-VING ROOT TAIRING UPPER R.H. 3'. D175óO DOOR ASSEMBLY_CABIN 33. D175710 COVLING ASSEMBLy-TAIL 3¡1. Dt75?90 DOOR ASSEMBLV-TA]L VllËEL 35. Dl7578o FAIRING ASSEMBLv-S}|oC( AESoRSER 3ó. D175793 FAIRING ASSEMBLY_REAR SIDE EELLY 37. D1?5794 COVLING ASSEMBLY_REAR EELLY SID€ 38. D17579ó FAIRING ASSEMBLY_REAR LEG ?g. D175797 DOOR ASSEMBLY_BELLY FAIR¡NG BULI(HEAD 40. Dr?57e9 CO\VL ASSEMBLy-RE,\R CENIER EELLv ¡lf. D175800 4t. Dr758ó4 ¡t3. Dl758ó8 11. D175869 45. Dr75870 L,H. ,ló. D175870 R.H' 47. D175880 -? L.H. 43. Dr75880 -? R.H. 49. Dr75904 50. D175905 5f. Dl759fl 5r. Df759f1 53. D175950 5,f. Dt7óO50 55. Dr7ó10 5ó, Dr7ó111 L.H. 57. Dr7órfl R.H. 58. Dl7ó20 59. Dr7ótr0 60. Dr7ó3@ ór. D17ó400 ót. D17ó40ó ó3. D17800 ó,1. Df 7S9100 ó5. Dr7S990 6. Dt792t 67. D179515 ó8. ¡89r93 69. 't89194 ?o- Dr7543r L.H. 7f. D17543r R.H. 7r. Dr7543l L.H. 7!. Dl75,l3t R.H. 7¡t. Dí75433 L.H. 7s. I 1754ó9 7ó. Dr7175-r L.H. 77. Dr7175-9 R.H. 78. D17175-3 L.H. 79. Dl7175-4 L.H. 80. Dl7175.{ R.H. FAIRING ASSEMELY_ WHEEL SHEEI_TOP WRAPPER COVL ASSEMBLY _ BULKHEAD POINÏ TAIRING ASSEMBLY_FRONT SIDE EELLY GILL_ ENGINE COMPARTMENI L.H. GILL _ ENGINE COMPARTMENT R.H. DOOR ASSEMBLY_ENGINE COMPARTMENT LOUVRE L.H. DOOR ASS€M8LY_ENGINE COMPARTMENT LOUVRE R.H. VRAPPER ASSEMBLY _ SIDE COVL LEFÍ VRAPPER ASSEMBLY _ SIDE COWL RIGHT COVLING ASSEMBLY-ENGINE UPPER COVLING ASSEMBLY-ENGINE LOVER COVLING ASSEMBLY _ ENGINE INNER SÍABILIZÊR ¿\SSEMBLY ELEVATOR ASS€MBLY IAB ASSEMBLY - ELEV/qÏOR LH. TAB ASSEMBLY_ELEVATOR R.H. RUDDER ASS€M8LY TAB ASSEMBLY-RUDDER rIN ASSEMBLY FAIRING ASSEMELY_ FIN AND SÍABILIZER DOOR ASSEMBLY_IAIL FAIRING GEAR ¿\SSEMBLY - LANDING MOUNT ASSEMELY _ ENGINE SÍACX,\SSEMBLY _ EXHAUST HEATÊR - Cr{BlN AND CARBURETOR COVLING ASSEMBLY _ REAR FIREVALL DUCÍ ,\SSEMBLy-CARB. AIR FILIER L.H. DUCT ASSEMBLY_CARB, A¡R FILÏER R,H, TILLET_UPPER VING NOSE L.H. TILLET_UPPER VING NOSE R.H. TILLET _ UPPER wlNG REAR FILLET_UPPER V¡NG REAR FILLET_ LOVER VING FRONT RADIO ACCESS DOOR PL,\IE - EXTERNAL nE ROD UPPER SIRUT L.H. PLATE_EXTERNAL IIE ROD UPPER STRUT R.H. PLAIE_EXIERNAL NE ROD LOWER ROOT L.H. PLATE _ EXTERNAL IIE ROD LOVER SÍRUT L.H. PLATE _ EXIERNAL TIE ROD LOVER STRUT R.H. BEECHCRAFT MODEL Iz ro l 27 -58 "i 20 ¿ 7 ft T r9 f8 4t 52 EXPLODED V¡EW WING ASSEMBLY.-UPPER l REF. I z 3 4 5 6 7 8 8 t to ll l2 t3 t{ l4 t5 t5 t6 l6 t7 t7 t8 t8 t9 20 2l 22 zt 24 24 25 26 27 27 za z9 29 30 3l 32 t2 3¡ 33 l,l 35 36 31 38 38 39 ,lo 4t 42 {3 ,14 t:!. xo. 15 a6 ,t6 47 17 ¡t8 {8 49 50 50 5l 52 53 51 55 56 76 77 7S 79 80 8t 82 57 t7 58 59 59 60 6l 62 6¡ a 65 66 6' 68 69 70 7t 72 73 71 75 t3 84 85 r6 a7 E8 NO. ?alÎ to. Dt7t00t-3 Dr7090-3 Dt 7090-4 Dr 7090-6 Dt7t021 Dr7t03t Dr 7t 0{3 Dl7lO,+5 LH Dt7t045 RH D¡7tofl Dt7t076 Dt7to80 DtTto0t-7 Dt 71o89 Dt7¡to5 LH Dt7no5 tH Dt7¡tt5 LH DrTtttS nH DtTtat-t LH DtTlat-t tH Dt72tO-t LH Dt72to-t RH Dt7r4r-r5 LH Dt?t4¡-¡5 RH Dr7t697 ot7t698 DI7t704 Dt7t7!5 Dt7r80,6 DtTtSto LH DtTrSro ¡H Dt7r8r4 D¡7! 8r 5 Dr718¡6 LH Dt7¡8t6 RH Dr?18r7 DI7I8I8 LH Þr7r8t8 nH Dt7t8t9 DtTt 820 Dt7t82t LH D¡7I82I RH Dr7t822 LH Dt7r822 RH Dt7t823 Dr 7r 82¡t Dt7t83t DtTt 84 DlTtSiro LH Dl7l8,lo RH Dr7t84r DtTtE{Z Dr 7l8it3 Dt72t¿l Dl7Zl22 Dt72¡24 t^tT xo. Dr7260-t f,17260-2 L8 Dt726{r-2 RH Dttz60-3 Llt ot7260-3 tH Dt7735 LH Dt7t35 RH Dt7965 DrTrür6-f, DtTt(x}6-t2 Dt7090-3 Dt7t022 Dt?to29 Dt7t695 Dl7t832 Dl7¡l¡16 DrTr@6-4 DtTt(X¡t-t I D¡7tdt6-8 aN5-22 aN3¡0-5 aN380-2-2 AN960-5t6 Dr7r30-l Llr Dttt3o-t r.H Dr7t30-2 Dt7t30-6 LH Dt7t30-6 Rfi D¡7r 30-¡2 DrTt t0-¡ 3 Dl7¡30- l ¡t Þr7r:to-t 5 D¡7t30-t6 D¡7r30-t9 D¡7t30-24 D¡7r30-46 D¡7t30-48 D¡7t30-{9 Dr7¡ 30-52 DtTtto-96 Dt 7¡30-14 Dr 7r 30-35 Dr 7r 30-36 Dt7tt2-5 AN,l-! ¡ aN3lO-it AN960-4t6 aN3-r2 AN3rO-3 4N960-3t6 PA¡I XME PANEL_VÍNG TI' T,EINTORCINC UPPER ROD ASSCMSLY_UPPER \vINC TIE ROD ASSEMELY_UPPTR WINC TIE ROD ASSÉM8LY_U??ER WINC TIT BOTTOM ASSËMBLY-UPPIR VINC ÎANK COMPAß,TMENT EDGE ASSEMSLY_UPPER RIGHT VINC LEADING SRACKET ASSEMBLY-VINC IANK COV€R SRACKEI ASSEMBLY_METAL WING TANK COVER LH BI,ÂCKET ASSEMILY_METAL VING TAN( COVÊR RH MÊM8ER ASSTMBLY_UPPER VING COMPRESSION SIRIP ASSEM8LY_UPPER RIGHT WING RT¡ STTAIGHTENIR EDGE - UPPER VINC TN,AILING SÍII P_ UPPCI VING TRAILINC BRACE_ROOT AND TAIL RIB DIAGONÂL ST¡IP ASSEMBLY_VING YIP FORMER LH SÌTIP ASStMSLY_VINC TIP FORMER RH COVER ASSEMBLY_VING T¡P LH covEn assEMsLY-wrNc ïrP nH gPAR ASSEMBLY_UPPER U/INC FRONT I-H SPAR ASSEMBLY_UPPER WING FRONT RH FITTING ASSEMILY_VINC ROOY LH F¡TTINC ASS¡MILY_VING ROOT RH SPAN ASSEMBLY-UPPER \TING REAR LH SPAR ASSEMBLY_UPPËR VINC REAR RH MÊMBER ASSEMBLY_UPPER VING IÑSPECTION fTAMT MEMSER ASSEMBLY-U?PEß, WINC INS?ECTION FRAME FRAME ASSEMSLY- UPPER VING INSPECÍION FRAME ASSEMELY-UPPER VING INSPECTION f,tB aSSEMBLY-NO.6, 7,8,9, r2, 13, UPtEn RI8 ÂSSIM¡LY_NO. IO, I¡. UPPEN, WING LH RIB ASSEMBLY-NO. IO. II. UPPER VING RH RIB ÂSSEMBLY-NO. I¡I UPPER ìyING R,I8 ASSEMBLY_NO. I' UP?ER, VINC RI3 ASSEMBLY_NO. 16 UPPER VING LH RIB ASSEMBLY_NO. Ió UP?ER VING T.H TI' ASSEMBLY-NO. 17 UPP¡ß, VING RIB ASSEMSLY_NO. 18 UPPER VINC LH RI8 ASSEMBLY-NO. ¡8 U'PER WING N,H RIB ASSEMELY-NO. 19 UPPER VING TIB ASSEMBLY_NO. 20 UPPER WING RIB ASSEMBLY-NO. 2I UPPER VING LH RIB ÄSSEMSLY-NO, ¿I UPPER VING RH R,IE ASSEMELY_NO. 22 UPPE¡ V/ING LH RIB ASSEMSLY_NO, 22 UPPIR WINC RH RIB ASSEMSLY_NO. 23 UPPER, RIB ASSEMBLY-NO. 24 UPPER RIB ASSEMBLY_UPPER RI6Hf NO. I,2,3,4, 5, NOSE RIB ASSTMELY_UPPER WING RIGHT R.OOT RIB ASSEMBLY_SOLID ÎAIL LH r,IB ASSEMBLY_SOLID TAIL RH N,IB ASSEMELY_UPPER NO. I TAIL RIB ASSEMSLY_UP?ER NO. 2 TAIL RIB ÂSSEMELY_NO.3, 4. 5, UPPER RIGHT TAIL MEMBER ASSEMBLY_UPPER VINC TIP COMPREs'ION M¡M8ER ASSEM¡LY- UPPER VINC COMPRESSION MEMBER ÂSSEMELY- UPPER VINC COMPRESSION PANT NA¡I H'NGE ASSÊMELY_AILERON HINCE ASSEMBLY_AILEN.OÑ LH HINCE ASSEMBLY_Á,ILERON T,H HINGE ASSGMSLY_AILÊN,ON LH HINCE AsSËMILY_AILERON RH CONTROL ASSEMSLY-AILINON LH CONIROL ASSEMBLY _AILERON R.H 5TRAP ASSEMSLY_VINC FUEL TANK PÁ.NEL_WING IIP R,EINFORC¡NG UPPER PANEL_WING TIP REINFORCINC LOVER r.OD ASSEMBLY_UPPEI VING TIE SOTÍOM ASSEMELY _ U??EN, IVI NG EDCE ÀSSEMBLY_UPPER LEFT \vING LEAD¡NG FRAME ASSEMELY-UPPER LEFT VING INSPECTION TI8 ASSEMELY_UP?¡R LEÍI VINC TOOT Ì,Iß ASSEMSLY_UPPEI LIÍI WINC COMPRESSION STR'P_ UPPER V/ING TRAITINC SÌRIP_ UPPER VING TR.AILINC STTIP_ UPPEN, V¡NG TRAILING BOLI NUT PIN VASHET AfLETON SPAR ASSEMBLY _AIL¡tO}¡ RII Å,SSEMBLY_Á,ILERON TI¡ ASSEMBLY_AILETON CENTER RI8 ASSEMBLY-AILERON CENÎER I,IB ASSEMBLY_AILEI,ON R(X)T RI8 A55EM8LY-AILERON N,I8 ASSEMBLY_ÂILETON RI8 ASSEMELY_AILERON f,IB ASSTM8LY_ATLERON CUSS¡T ASSEMsLY _ AILER,ON H I NCE OUf sOARD REI NFON,CI NG GUSSET ASSEMsLY_AILERON H¡NGE CENTER REINFORCING sRACE_AILERON OUTBOARD DIAGONAL BRACE_AILERON IN8O,AR,D DIAGONAL SRACE_AILET.ON INBOARD DIAGONAL ÉDCE_AILERON TRAILING R,¡8 ASSI MELY _ AILERON OUTBOARD SIR]P_ SPAR REINFON,CEMENT SIRIP_S?ÂN, R€INFORCEMENT STRIP_SPAN, N,EINFORCEMCNl TU¡E _A¡LERON IRAILING EÞCE EOLT NUT VASHER ¡oLÎ NUT VASHET, BEECHCRAFT MODEL T7 I Pep ÞEm@@DI A WING ASSEMBLY_UPPER rlf. xo, I I 2 3 4 5 6 7 8 9 t0 lt t2 t3 t{ r5 r6 t7 t8 t9 20 2l 22 23 24 2' 26 27 2a 29 30 3r 32 3t 34 35 36 37 3E 39 PARI NO. DtTtoo4-3 Dt7t004-3! Dt7090-2 Þr7090-,1 DrTto¡z Dt 7t032-4 Dl7¡032-3 Dr 7ro43 DtTto/t5 LH Dt7t077 DttloTS Dr7r42"t LH & RH Dl7142-t5 LH tr RH D¡7I444 LH & R,H DlTl 105 LH fr RH D!7III'LH&RH Dt7t7t8 Llt & RH Dl72l0-l LH (r Rll D17l72l -2 Dr7185 LH &rH Dì7t857 LH & ¡,H Dt 7t 858 Drtr36t LH It RH Dr 7t 862 Dr7t863 LH & tH Dr7l864 Dl7l865 LH ¿r RH Dt7t865 Dt 7t867 Dt7¡864 LH & LH Dl7l869 LH Ir Rtl Dt 7r 882 Dt7t89r DtTr 823 Dr7t82/t Dl71896 LH ¿r ß,H Dt7Zt33 D¡72¡34 Ltl ft tH Þ¡721/tl, LH fr Ì,H P tl XO. Dt726{-I Dt7264-2 D1726¡tl o1726É'0 D172668 DtTtü)4-3C Dttt00¡t-32 aN5-2t Dt7965 Dt72¡0-8 DtTZ¡O-4 Dt?t60-t Dt7¡6{r-9 D¡716,0-l I Dt7¡60-t2 Dt7t60-13 Dl7l60-t4 Dr7r60-¡5 Dr7t6{r-t8 DtT16¡'27 DtTtæ-24 Dt7',t60-34 Dt7t60-4t DtTlæ-47 Dt7t60-8 Dt7t60-7t Dr7r60-89 Ðt7t 3t -l or 7r 60-3 Dt 7t60-4 Dt7l60-6 aN3t0-5 AN380-2-t aN960-5r6 aN4-r I aN3t0-4 aN960-4r6 Dt7t32-S ;ATT XAII PANEL _VII{G TI? T¡INFOICIIIG IOTTOM PANEL_VINC TI' TE|NFOICING UÞ?ET ROD ASSEM¡LY_LOYE¡, VING TIE ROD AsS¡MILY_LOIVER YINC TIE IOTTOM ASSEM]LY-¡JOVEI YINC lANf, COMPAI.TMENÌ EDGE ASSEMILY_LOYEI VING L:ADI¡{GI LH EDCE ASSÍMILY_I.oVEI YII{G LEADII'G IH BR,ACf,ET ASSEMILY_WIXG TANX CIOYIT. BTÂCKCÎ AS'IM¡LY_MEÍ T wlNG TANr COVEI. LH STTIP ASSEMBLY*LOVEI VING III SITAIGHTENÊT STTIP ASSÊMILY_LOVEI VING TII STTAICHTENER sP n assEMBlY-¡.ovEt vrNc rloNÏ Span ASSEMtLY-l¡vEr v¡xc Lo\yEt tEAt Slocr( AssrMrLY-LowEr TANK COyEt SrAr STR.IP ASSEMILY_VI]IIG TI' FOTUET covEt AssEMf LY-V¡NG Ttt FNAME ASSEMBLY_ III¡S'ACTION FITTING_VING TOOT LTI SUPPORT - EXIEIXAL TIE IOD FAIIIC RIB ASSEMBLY_LOVEI VIIIG IOOT RIB ASSEMILY_ NO.' I.o\fEI wl¡{G RtB ASSEMSLY-XO.8, I, rO, ¡.OVEl Rt3 ^SSEMBLY-NO- tt t.ovEr V¡NG Rlr aSSEMSLY-NO. 12 rOVEr VtñC RIB ASSEMBLY_IIO. t' LOVET, VING n18 ASSEM¡LY-'r|O- la I.oVEI Vlllc Rr¡ A35ËM¡!Y-NO. rt LoVEr V|NG TII ASSEMILY_NO. 16 LOWEI VING RrB ASSEMsLY-Í{O. 17 |þVER VrNc RI' ASSEM¡LY_NO. II I-oVEß VINC RIB ASSTMILY_NO. T9 LOVEl VING RII ASSEMSLY_LOITET YING NO. I NOSE R¡¡ ASSEMELY-r.OVEr V|XG NO.2,3, /r,5,6, NOSE ¡,¡B ASSEMBLY-|-OìyEr NO. l,2, ¡, ,t, 5, TAIL RIB ASSEM'LY_NO 20 LOVET R.IB ASSEMBLY_NO, 2I 1jO\YEI TIE_NO.6 LOVER, wlNG TAIL MEMBER ASSEMTLY_ LOWE¡ VINC COMPRISIIION MEMS¡I ASSEMBLY_I¡VEI VING COMPB,ESSION MEMBEI ASSEMBLY_LOVEI, VING COMP¡,ESSION FLAP DI7I60 SPAR ASSËMBLY_FLAP NIB ASSEMELY_FL.A? N,IB ASSEMELY_FLAP INIOARD RIB ASSEMSLY_'IA? RI¡ ASSEMBLY_FLAP N,IB ASSEMBLY_FLA? RIB ASSEMBLY-FLAP GU55ET ASSEMBLY_FLAP ßEINFORCINC BN,ACE _ TLAP R.E¡NFORCIMENl SRACE _ FLAP REIN'ORCEMENT CUSSET ASSEMBLY_FLAP REINFOß,CING IT,ACE _ FLAP IEINFOTCEMENT RI8 ASSEMBLY_'IA? N,IB ASSEM8LY_FLAP EDGE_FLA' TRAILING RI8 ASSEMSLY_FLAP OUTBOAN.D FITTING ASSEMSLY_ FLAÞ HINGE ¡LOCK_S?AR REINFOR,CEMËNT ELOCK_ SPAI REINfORCEMENT BLOCK_SPAR R¡INFORCEMÊNT NUT PIN VASHER BOLT NUI VASHER, fUSE_FLA? TTAILING EDGE WING ASSEMBLY-LOWER ¡&. xo- {o 4t 42 13 a4 45 16 17 t9 76 77 ?ATT NAÍ¡ HINGE ASSEMBLY-FLAP HINGE ASSEMBLY_FLAP HINCE ASSEMELY_TLA? MECHÂNISM ASSEMSLY_FLAP OPERÂTING VING HOUSING ASSEMSLY_FLEXIILI SHAFT IN VING ERACE - LOVER. VINC ILOCK_LOWIR VING BOLT (IHIS IS NOT ON PARIS LIST) STNAP ASSEMBLY_VING ÍUEL TANK FITTINC_STTUÍ LOVER FRONT FITTINC_REAR STRUT 48 50 5l 52 53 t4 55 56 57 58 59 60 6l 6Z 63 64 65 6 67 68 59 7A 7t 72 7? 74 75 BEECHCRAFT MODEL IZ A IíING ASSEMBLY_LOIIER r I f l ( I ( !.* BEECHCRAFT MODEL T7 Dt 78711-t Dltt?rr Dr 78?ró XNOS-TAIL VHEEL LOCX CONINOL LEVER LEVER ASSÊM8LY_IAII \IHEEL LOCK CONIROL CASIE ASSTÀ,I8LY_IA[ VHEEL LOCK 1. PC f ó0! cLwß PIN AN !¡GI.' COIÍER ñN r. AN 393-t3 PIN Añ 3sùi-t collEl BN 3. ^N liGrGrO SCaEV, A< 3ótl03l NUr, AX9óO.rO VAS}IER, I 00605.x1 G60l I SPACER 4. AN 3-tO 80L¡ AN 3IO.3 NUT ^N 3e3-4 PtN AN 9ó&IO VASIHER 5. AN 5tér3t.ô scnBv ^N 3¿&8 Nul Añ 935.8 v^sHE¡ ô. ^N 59ê83tó S(nÉv AN 3,'û8 NUI AN 935-a VASHEI r, ^N 3-7 80Ll AN 3IG3 NT,l AN !¡GI.' COTTE¡ PfN '. SEAK€ LINE VALVE 9. ^N 31G8 NUr DI'83G7 AXLE AN ô'O AOL' AN 316 ¡¿l,T I l. Dl tl,at EXT€NDING Tt 8€ rl, VHÊ€L AS$EMBLy r ¡. FAI¡|NG ASSiEM&-v r,a. AN }f 3 BOLÎ ,\N 3rO-3 Nt f 1t. Drtí5.7 SUSHING sl1¡-rl BOLI AN !IG5 NIJI ró. sHocK A8SOI8€R r'. ELEED€¡ VALVI 1I. '¡AKE LIÑE I 9. RÊAR LTG f Dlt8rc-l I Dr 757ó I Dr 7801 0 4 Þr 7ætl 5 017S1t ô D178013 t Dt?aø4 8 D1?8015 9 Dlt80r6 sHo(K ABSOREEX ASS€MSI-v COVER ASSEMELY - HYDRAULIC ERAKE VHÉTL <A8LE ASSËM8IY_]AIL VHEEL RETRACIING CHAIN ASSEMSLY - LANDING GEAR RETRACIING CASIE ASSEMELY-TAIL VH€EL REIRACfING CÔRD-'AIL VHEEL REIRACIING CASLE CORD ASSEMBLY - fAIL VHÊËL EXÍENDING SHOCK CABLE ASSEMSLY_IAIL VHEEL EXIENDING CHAIN .ASSEMBLY- LANDING GEAR RETR.\CTING CROSS SHAFl CHAIN ASSEMELY-LANDING GEA¡ NEIRACIING MOTOR SHO(r A85ON8fi ASSEMSLY - TAIL VHEEL LEG ASS€M8LY-LANDING GEAR DIAGONAL UNIVERS¿\L - LANDING GEAR UNIVE¡S,\L - LANOING GE^R Lll UNIVERSAL - LANDING GEAR RH LEG ASSÉMBLY - LAND¡NG GEAR REAR LH LEG ASSEMELY_ LANDING 6ÊAR REAR ¡H AXLE AND fOiOUË ARM ASSIMBLY_LANOING GEAR LH SOLT - AXLE TUEE ASSEMBLY _SHOC( ABSORBER EXIENDING CRANT ASSEMELY-LANDING GEAT RflRACfING SHAFI ASSEMALY-LANOING GEAR CROSS SLIDC ASSÊMBLY _ LANDING GEAR LH SLIOÊ ASSEMSLY _ LANDING GÉAR RH IUSE_ LANDING GEAR SLIDE SLIDE ^SSEMBLY _IAIL VHEEL IUBE ASS€MALY - IAIL VHEEL SLIOE HOUSING ASSEMBLY_IAIL \THEEL FOTX ARM ASSEMBLY-TAIL VHETL LO<I(NG ROD - TAIL VHEËL LO<IING IOP TORK ASSEMELY-TAIL VHEÊI SPRING -TA¡L VHESI SVIVEL MOfOR ASS€MEIY-IAÑDING GÊAR ¡TTXA(NNG PULLEY PULLEY PULLEY _ CONTROL VHEET ASSEMÊLY - LANOING GÊAR (GOODYEAR) VHEGL ASSEMSLY-fO INCH (GOODYEAR' TIRE - LANDING GEAR FRONT (GOODY€AR) ÍIRE_ LANDING GEAR REAi (GOODYEAR) 10 Dtt80l7 rt Dl78!0"t 11 D1t06G1 1t Þ1781Gr 13 D1?815.1 r¡ D1781t-t LH 14 Þrt815.t nH !5 Dtttm LH 15 Dr7llo RH tó Di78!O-1 LH 18 19 ¡o l1 ?1 tt l¡ ta t5 9ó 97 l8 r 30 Í¡t 33 a1 It 3ó 3t Di?8¡rn D1t85Gt Þ1785G14 DI73'GIó LH Þr 78Stó RH D1785d38 Þr 78ô0-r Þt7@-ro ot t8ô5 Drt8ô5-t9 Drlaó5-30 Dr78701 81 787r Dr 78900 /\.t38 ANtl04^ tl8t4M 5r6.g NO NUMEER NO NUME€ß r. }í PIPE PLUG i. D1784r SPRING 3. Df78¡.¡-t LOCK NUT ¡. Dl78¡a+f PACKING NUT s- t')tu t ){ WELD ROD ó. Dlts.r3 P|STON ?. Dr78¡15 EUSHING 8. Dl:s/r8 PACKING RINGS 9. D'78,'ó BUSHING fo. D178,tor-f RU88ÉR BUSHING 11. Dr7840-t toRl( ASSEMBLy lt. D!78,(Ls UPPER SHOCK STRIJT A$EMBLY SEE IUSR'CAT/ON CHART PAGT 35 FOT SHÕCK slluf r¿UlD SPÈC,FlCi{rlON. LANDING GEAR AND TAIL WHEEL LOCK ASSEMBLY BEECHCRAFT MODEL Iz 1. Ac3ós"g3t NUf, AN59ê83r-fl BOLT t. Bf 7871 SPRING 3. AN31G3 NUT, AN3.,I BOLT, AN38O.9.q COffER PIN, AN9óO-'O VASHER ,a. AN3lo-10 NUl, 95-917-10" AXLE, 9s-9r&fo" SPACÊRS 5. AN3.IO BOLÌ, AN31G3 NUT, ,\N380.'.9 COTTER PIN, D178ó5-1 TUBE 6- Dl78018 TAIL WHEEL LOCK CAELE 7. D17T7OO TAIL VHEEL SVIVEL ÀND ÍORK ASSEMELY 8. WHEÊL ASSÊMBLY 9. ANs-tt 8OLT, AN3ro-5 NUl. ^N9ó051ó VASHER fo. AN5-r4 80Lr,'\N310.5 NUr, AN9óO-5fó VASHER 1r. Dl78óo SHOCX ABSORE€R I r. AC 89t-87o PLtG i. Df78óó SPRING ], 0178ó0-1 UPP€R ASSEMBTY ,.. Drlsóg-l LOCKING NUI 5. D178ó'.3 PACKING NUf ó. Dr?8ó4^ PISÌON t. Dl?só3.r EUSHING 8. D178ó8 PACKIÑG RINGS e. Di78ó3-r SUSHIñG IO. D1?8óG8 LOVIR ASSEMBLY SI]OCK ABSORBER rI. %r VELDING ROD r9. D1t8óO-14 EUSHING. st€ luSflcÂfroN cHARr PAGf 35 FoR sHoc( S¡RÚ FIUID SPECIF'CÂ''ON. EXPLODED TAIL\øHEEL ASSEMBLY ASSEMBLY...TAIL SURFACES ELEVATOR ASSEMBLY RUDDER ASSEMBLY itt. No. I 3 4 5 6 7 I 9 t0 tl t2 l3 t4 t5 t6 l1 t8 l9 20 ZI 22 23 24 25 26 27 ZE 29 30 3¡ 3Z 33 34 35 36 t7 PARÍ ÑO. r 05774-C-063 -01 0l 6 Dt 7620-2 Dr 7620- r 9 Dl7620-26 Dl 7620-4t D17620-42 Dr 7620-3 Dt7620.t5 D¡7t7¡8 D'171121-2 D't71725-t Dt 77721 -r K:I-L Dt77t3¡ aN320-3 Dt7773l AN3-¡O ac995-32-8 Dl777Z7-t s-r68 NO NUMB:R 4N3.6 aN960-4¡6L AN3tO-3 ÂN-380-2-2 D17776-t Dt 762t 0- I D I 762t 0-4 Dl 762! 0-6 Dt76t r2-l Dt76026 Dt 76029 Dr 76030 s-74-27 AN3 I 0-4 aN380-2"2 AN4.6 P^n? N^¡Ê trEr. I z 3 4 5 6 7 I 9 to ll l2 It t4 t5 t6 l7 ¡8 t9 20 2l 22 23 24 25 26 NO. PARI XO. Dt 76r O-2 Dt 76tO-25 Dr 76tO-4{' Dt76t0-4r D¡76t0¡ D¡76IOE Dr76t I 3 Dt76rr8 Dl76r r5 Dt7772l-2 Dt76t t6 Dt1772l-t Dt76tt7 Dt 7773t Dt ?7736 ot71134 Dt77724 aN3-t I K3-L s-t68 Dt 777¿6"3 D177726-4 Dt117t7 ¡ 05774-C-06t-O3too Dr76tII-4 D17176-t Dt 76025 Dt 7603 r Dt76032 AN4-6 aN3 | 0-4 4N380-2-2 aN960-4t 6L s-14-27 Dt76t I t-t Dt75t t2 'AIT XAMI sP^n - €lÊvafoR HOI,N ASSEMSLY _ CLEVAÎOÎ, BRACKÉT_ ELEVATOR IÊFT TA¡ MECHANISM AITAC}IING BRACKEÍ _ ELEVATOR TIGHT TAB M¡CHANISM AÏTACHING ARM ASS€MBLY _ IIEVATOR IALANCE BEARINC_ ELIVATON, SPAR HINCE IRACKEÍ _ILEVAIOR TA8 RHÊOSTAÌ SUFPORT VORM _ ELEVATOR TAE ¡,HEOSTAT PLAIÊ_ CLTVAIO¡. IÀB RHÉOSTAT VORM -CIEVATOR IAB CONÍROL ßI{EOSTAT _ ELSVATOR TA8 RHEOSTAT CEAI _ ELEVAÍOR IÁ.3 CONTROL GEAN, _ ¡LÊVATOR TA8 RHEOSTAT BOLT-ELEVATOR VORM CEAn r^t CONTROI- ADIITSTING SHAFI_ELEVATOR TAB CONTROL SI,ACKEI_ÌAB CONÎROL VORM CEAR ARM ASSEMELY_ELEVAÍOT TA8 CONTIOL MECHANISM BOLf BEAR,INC END_ELEYATOR TAg CONTROL ROÞ PIN _ HINGE EDC€_RUDDER TRAILING HOIN ASSÉMBLY _ R,UDDER, S?AI-RUDDER sRACI(ET -TAB MECHANISM ¡TÂCI(ET_RUDDÊR 1A8 CABLE CUIDE EDGE_RUDDEI, TIP VEICHT_RUDDER BALANCE SHAFT_ RUDDËR TA8 CONÍROL U/OI,M_TAE CONTROL ARM _ RUDDER TAB CONÏROL MECHANISM 6EAR_fA8 CONTROL 8¡ÂRING IFAFNIR) 8OLf-VORM GEAR TAB CONTROI ADIUSÏ|NC NUT BRACI(ET_TA8 CONTROL WORM CEAR BOLT VIRE FOR LOCKINC ROD_RUDDET TA8 CONIROL END_ ROD PIN toLT-atRcRAFl t0-12 VASHER NUT-^rtCR^tt CASÎLE ?IN-COTTER PULIEY_fAB CONTT,OL SKIN _¡,UDDEN, TÂB HINCE_RUDDER HALF IIINCE_RUDDER TAB HALF ARM_ÊLEV,ATON, TAB HINGE ASSEMILY_RUDDER CAP_ H'NCE ASSÊM8LY BASE_HINGE ASSÊMBLY BOLT NUT PIN toLf ROD_ELEVÁÍOT, TA8 CONTROL IH ROD_ELEV TOR TA8 CONTROL RH % WELD ROD 27 za 29 30 3T t2 33 34 35 36 COUPLINC _ ELEVÀTOR TA8 CONTROL SHAFT PIN - HINGE HTNCE_ELEVAIOX, TA8 PULLEY _ ELEVATOR TA8 CONÏROL HINCE ASSÊMBLY_ ELEVAIOR SPÀR 'ASE ÂSSEMBLY_ELEVATOR SPAT, HINCE CAP ASSEMBLY_ ELEVATOR, SPAN, HINCE sOLT NUT PIN VASHER SOLT SKIN_CLEVATOR TAB Â.RM SSEMBLY _ ELEVAIOR, TA3 l I I ( l l I ì I I f ì í i l { I ( f ì BEECHCRAFT MODEL TZ @---€ @--{? -_À qt \:t @ g-l @ K Õ EXPLODED RUDDER AND ELEVATOR ASSEMBLIES & ( i I ( 1 I i l I L, f : f I I I i l I L I i t fi f i L f I I BEECHCRAFT MODEL .T SAFETY VIRES. l--- ,,lF -rx ¡-- NOÍE-USE NO O OIL IN FLAP HOUSING CASE NO. f , r DlTtóór RH t Dl79óót 3 ,\N509-10-ó ¿ D1796ó3-l 5 D17r663-1 ó Dl7tóó3-5 7 D17tóó3-ó I Dtttó63-7 9 Df72ôô3-8 lo Di?Póó4"i 11 D172661-2 19 017266+3 13 Dr7?óó,r-ó 11 D179661-7 15 D172661-8 16 D179óó,1.9 f7 D179óó5-f 18 D112669 t9 4N315-3R 90 DfTlóó5-,1 91 Dr79ôóó¡ tt Dr79óóô9 t3 017qóó9-7 24 f)172óó9.16 95 Ð1726ô9-17 tó 4N509-rGf ,l r? K,l '8 K8A t9 AN3-11 ¡0 AN31È3 31 4N380-9-1 HOUSING-FLAP OPERATING MECHANISM RH VING COVER - IIOUSING FLAP OPERATING MECHANIST.^ SCREV _ AIRCRAFf FILLISTER HTAD GEAR -,'IIORM SLEÊVE HOLDÉR - FLAP MECHANISM EEARING HOUSING _ FLAP GEAR MECHANISM PLUG BUSHING PIN _ FLAP MECH,qNßM PIN _ FLAP MECHANISM PIN - FLAP MECHANISM SUSHING NUT - HEXAGONAL xui - xrx¡eoN¡t CAP GEAR ASSEMBLY _ FLAP OPSRAIING MECHANISM SVITCH ASSEMBLY-FLAP OPERATING MECHANISI,T VING LIMIÍ NUI DRIVE ASSEMBLY _ TLAP OPÉRATING MECHANISM GASKE _fLAP OPERATING MECHANISM FELI - FLAP OPËRATING MECHANISM BRACKET ASSEMBLY _ fLAP LIMIT SVÍTCH SLEEVE 9ACER SCREV BEARING-BALL (FAFNIR) BEARTNG -S,\LL (fArNrR) EOLI _ AIRCRAFT NUT_AIRCRAN CASÍL€ PIN _ COÍIER SAFEÏY VIRE FLAP SCREW AND LIMIT SWITCH ( i { i L f I L ( I I f { L- f I f I I ,* It t t¡ i* ( I I I I \-_ I i L I I I L- ç t I L- BEECHCRAFT MODEL T7 I Dr7750r\-5 CHAIN A55EM8LY - THROVOVER CONÏROL COLUMN LÉVER ASSEMBLY_THROVOVER CONIROL ARM r\SSEMBLY -CONTROL COLUMN THROVOVER CABLE ASSÉMBLY _ÍHROVOVER CONÍROL COLUMN CABLE ASSEMELY-THROVOVER CONTROL COLUMN PULLËY _ AILERON CONTROL BOLÎ _ A¡ßCRAN NUT _ CASÍLE PIN _ COTTER VASHER BEARING ASSEMBLY- THROVOVER CONTROL COLUMN BOLT_ROUND HEAD NUT _ CASTLE SPACER - THROVOVER CONTROL COLUMN SPRING _THROVOVER IATCH PIN PIN _ THRO\IOVER LATCH @-ú I Dlt750r 3 Dr7750t ,r D1?7003 5 Dl7700¡ õ---€ ó DrTtót-t 7 AN+1,0 8 AN3!(L¡[ 9 ,\N380-r-9 10 AN G,rló 1f Dr775r-fO It s-7t15 l3 AN3td'4 1,t 017751-rt t5 Dr775r-1,a ló Dl775f.15 f7 Dr7751-20 SPACER _IHROWOVER CONTROL COLUMN OUIER 18 Dl775t-t't SPACER -THROWOVER CONTROL COLUMN INNER 19 D177t1-27 KNOE - THROWOVER CONTROL COLUMN LAÎCH PIN to D17751-31 tr Dr775i-3t COVER_THROVOVER CONTROL :-.@ BEARING ASÊEMBLY _ CÔNTROL COLUMN CENÎER tl Dl7Of0,l 13 DrTróol 21 6132rsl 15 D177óOt-5 96 D177ó¡1 PLACARD - ÊLEVATOR ÌAB COMROL DISC _ ELEVATOR IAB CONÍROL SCREV_ROUND HEAD MACHINE COVER _ ELÊVAIOR T/\B EUSHING PULLTY BUSHING Drsc BUSHING Dtsc _ELEVATOR TAB CONTROL tr.Dr7:óo5 t8 Dr7760ó _ELEVAIOR TAB CONIROL _ELEVATOR TAB CONTROL f *-----€) 29 D117ó0t 30 AN3-5 3l D177óOg PULLE' _ ELEVAIOR IAB CONTROL EOLI _ AIRCRAFÍ GUARD - ELEVATOR IAB CONIROL CASLE SCREV FAIRING _ ELEV^IOR TAB CONIROL KREV SPROCKÊT -CONTROL COLUMN SHAFf -CEN1R,\L COLUMN VHEEL-CONTROL COLUMN PIN - DRILL ROD l(EY _ SOUARE IGY _ SOUARE BEARING (SCHAIZ) VASÞtER @ l@ 3t 4N505-8-ó 33 Dt?7óli 34 ,\N535-O¡ 35 D1785ô7 3ó r8r5r8 37 30t515 38 1Ot809.t25-ltt 39 r05ó93¡1150 ¡0 s.fi-3 ií HllO ,r9 r0095Í-so0&0rt CONTROL COLUMN ASSEMBLY BEECHCRAFT MODEL Tz ù Ð } ù A f, q ) ) ) ) REF, NO. 1 2 3 4 5 6 7 I 9 f0 11 12 13 11 PART NO. D179319-2 Dl79347 Dl 79349-1 Df 79348-1 D179318-2 Df 73986-f PART NAME PROPELLER CONTROL THROTTLE CONTROL MIXTURE CONTROL CARBURETOR HEAT CONTROL OIL HEAT CONTROL CABIN HEAT CONTROL OIL RADIATOR AIR DUCT CABIN HEATER CONTROL VALVE PROPELLER GOVERNOR PROPELLER CONTROL BRACKET I -.. ó Df7590724 Dl 759358 D1 79064 CAREURETOR MIXTURE CONTROL BRACKET CARBURETOR HEAT CONÏROL BRACKET CARBURETOR THROTTLE CONTROL SUPPORT ERACKET Dl 79078 ENGINE CONTROL SYSTEM r I f I L I I I ¡ fI I f I I { I ! f I i \- f I (* I I I t- II I ÍI I L fI I L- II i L BEECHCRAFT MODEL TZ t D.I79'óI TUBE_LEFT UPPER VING TANK 2 D179271 TUBE_FUEL PUMP DRAIN CENIER ? DI79'77 IUSE ASSEMELY _ ÍRAINER DRAIN UPPER 4 D119'78 TUSE_STRAINER fO TIJEL ruMP 5 D179279 TUBI -FUEL PUMP TO CARBURETOR ó D179:I8O TUBE ASSEMBLY-PR¡MER IO ENGINE 7 D179I83 IUBE ASSTMBLY_PRIMER TO ENGINE FORVARD 8 DT79i8,{ TUBE ASSEMBLY-PRIMER TO íRAINER 9 D179236 TUBE_VOBELE PUMP TO SIRAINER UPPER 'O D179I88 IUBEASSEMELY_CARBUREÍORfOENGINE GAGE II DI7999O TUBE ASSEMELY-CAREURETOR TO FUEL VARNING fI D179'9I IUEEASSIMBLY-FUELCOCKCONNECIING f 3 DI'9IgI ÌU8E_R,EL COCK IO VOBBLE PUMP I,I D179:93 TUBE_fUEL COCI( fO LEFI UPPER VING IANK 15 Df79995 ÍUEE_FUEL COCK TO LEFI LOVER VING TANK 1ó DI79I9ó fUEE_TUEL COCK TO RIGI{Ï UPPER VING IANK 17 D119791 IUBE_fUEL COCKIO RIGHT LOVER VING rANK 18 DI79999 IUBE-FRONÎFUSELAGEIANKIOVALVE f9 AN4OO+l VALVE-R'EL 'O Df79óOR T LfANK_UPPER VING RJEL 9I DI7973.,I TUEE-VING FUEL TANK VENT '' D17971 TANK_R'SELAGE FUEL e3 Dl7e7r1 NECK ASSEMBLy-fß9NT FUSELAG8 GAS TAM( NLLER ,4 817911 VENT ASSEMBLY_FUSELAGE G,{S IANK 95 D17975 R A LIANK- LO\IER VING FUEL LH Ió D17IO'ó UNII-VING TANT ft'EL LEVEL i7 C.1A (1939) STRAINER ASSEMSLY (LUNKENHEIMER) ?8 t$5 uNtr - tuEL PnESSuRÉ VARNTNG (PTONE8R) '9 R X D 15ó3 PUMP_VOBBLE (ROMEQ 30 re8e4 PRTMER (ECLTPSE) 31 AN,lloo FUEL ruMP GYPE G-ó) 32 D1'98,t.1 GAGE ASSEMBLY_fUSELAGE GAS TANK 33 5I GAS CAPS - MIDDLETOVN - 5 REQUIRED, 34 Dl79t9t TUBE AS5['lvtlLY 35 D'793I0 INSTALLATION_FUEL SELECTOR VALVES. I INSTALLATION-FUEL SYSÏEM BEECHCRAFT MODEL Iz FELT PADS 1 2 3 1 5 6 7 8 9 Dr789ó7r -1 ANr,r0-85 1 897,1ó D1 7S98o-r j STRAP ASSEMBLY - OIL T.\NK TURNBUCKLE ASSEMBLY -CASLE EYES F¡TTING ASSEMBLY - OIL PRESSURE RESIRICTÊD IANK ASSEMBLY - OIL D1759803 LH BRACKEI ASSEMBLY-OIL TANK SUPPORÍ LH Dr 79804 D1 7980ó D1 798r0 Dl 7981 l ÍUBI - OIL I,\NK REAR SUPPORT CAP A.SSEMELY _ OIL ÍANK TUBE - ENGINE OIL OUTLET IUBE - OIL R^DIATOR OUTLEI IUEE-OIL PRÉSsURE GAGE FRONI TUBE - OIL DRAIN TUEE - OIL 'TANK VENT ÏUBE ASSEMBLY_OIL PRESSURE GAGE REAR WELL ASSEMBLY-OIL TEMPERAÍURE BULB SÍICK - OIL MÉASURING SHEATH ASSEMBLY - OIL GAGE STICK RAOIAÍOR _ OIL SUPPORT - OIL R,\DIATOR DUCT FRONT VALVÉ ASSEMSLY_OIL RADIATOR AIR SCOOP DUCT ASSEMBLY-OIL RADIATOR REAR AIR DUCT ASSEMBLY_OIL RADIATOR MIDDLE AIR ARM ASSEMBLY-OIL BY.PASS VALVE COCK ASSEMBLY-Y OIL DRAIN v^LvE ASSEMBLy - By-PASS r0 Df798t3 1 r Dl 79814 11 Dl79t15 t3 017981ó 'f4 D179818 t5 Dl798t3 ló Dl798t¡l l7 9+189850 l8 Di79059 l9 Dl7987l t0 D17987ó xl 0r79878 tr 18s99t 93 3tDó11,ú-¿ t,r s80 25 s!1 75-5 5, f 9 !ó D179819 t7 Ac8so-ló !8 t8 - 980t t9 ,{10898 30 D1759óó5 3r Dr7S9ó7f-9 t CONIROL,\SSÊMBLY _ SHAKESPEARE PSS,{S4 FLEXIELÊ HOUSING IUBE-OIL TANK INLEI ETBOV _ HOSE. FUEL AND OIL COUPLING FLANGE (PR,ATÍ AND \IH¡ÍNEY) SUPPORÍ ASSÊM8LY _ OIL IANK FRONT S'RAP ASSEMBLY - OIL TANK INSTALLATION-OIL SYSTEM t t t t t t t t t L t t t t sEcïoN lll ELECTRICAL SYSTEMS MASTER WIRING DIAGRAM LANDING GEAR ELECTRICAL CIRCUIT FLAP ELECTRICAL CIRCUIT WIRING DIAGRAMS-LANDING AND POSITION LIGHTS- LAND¡NG GEAR MOTOR WIRING DIAGRAMS-MAGNETO, STARTER SOLENOID AND BATTERY-THERMOCOUPLE-PITOT-OUTSIDE AIR AND CARBURETOR TEMPERATURE wlRING DIAGRAMS-CABIN LIGHTING, FUEL ANALYZER AND COMPASS_FLARE UNIT-RECOGNITION LIGHTS- FUEL PRESSURE \IARNING UNIT WIRING DIAGRAM-GENERATOR-FUEL TANK DETECTOR AND GAGE UNIT-FLAP MOTOR MASTER WIRING DIAGRAM NOTE-_' DTNOTES I,EFERENCE ONLYI ITEMS MARKED IN THIS MANNIR ÂRE CALLED OUT ON OTHER ASSEMBLIES _ ?NOTECTION FON VINES ON SOLDER CUPS OF PLUCS AND RECEPIACLES SHALL BE IN ACCON,DANCE VITH ELECIRICAL SPTC. E. S. ZI7 - C26 TE¡ùt¡NAt- ,^36 T:RMINAL AñD C-7¡ TERMINAL MAY 8E PURCH SED FIOM THOMAS ¿' 3ETI5, ELIZABTTH, N. ,. - x8 vtRE-5o AMP- IETMINAL A.C. 66O-3---a REQ. xr2 AND #l{ VlrE-35 Alr?. TEIMINAL C-2é-56 nEQ. C-?t TEnMINAL-I nEQ. xl8 vlt¡-25 aMP. TERMINALS ^36-rr8 REQ. All SHI¡IP|NG CUT I INCH ttOU TETMINALS; VÌ.ÂP ENDS VITH COTÍON \YAXED CORD-AIMY 6-2t. NOTE A_GREIN LICHT BURNING-LAND'NC CEÂR DOVN 8-JVIfCH OPEN_LANDING CEAR DO.VN C_SWITCH CLOSE¡'-{ÀNDINC CEAR DOWN D-..SVITCH CLOSED_FLAP UP E_THIS ÍUsE MUST NOT IE CONNECTED TO IUSS BAR F---GOVER,NMENT FURNISHEO EQU¡PMENT 17 I qVITCHIENERATOT--C-H- I MôÎôDJI AD-DUMO¡E I( 1 MôIô!-¡ ANb¡NE CFÂT_DIIMôIF D.5 ¡ol NAMF ELECTRICAL EGIUIPMENT T I ----r---- l¡o. REo. ' 91-JZZZ0A " C-RED . C.--GREEN _.ETEfrY9¡;|UB- "606 TYÞÊ 14 . c-H_98t87 SPEC- PART NUMBEN, a 9:t NO. -RECULÀTOR.-ECLIPSE | : I "rrìr,r3 CHôTE AOX-ECLTPSI 'tl¡vz+ PLUG-FREE AIR TITERMOMETER l = Añrruo-r+)-z¡ clrfour-EcltPsE-TYPEl50-la I I I -ÞTÛFFIÚF.ÂNALYZERCELL I ¡ I AN3IO6-I4S¿L ffi I I I "Dr707r9 CÂALE AqSEM.-BÂTTÊN,Y ¡ I ¡ - Utrurt) -?¡L=-ññfrrY cPolrND CôNNEC.rION ' Dt 7y9l I I I LDtfø)2:' -ilt<a BAÞ-t H I I ' Dt t97 tz-+ L.U- VING TANK UNIT | ¡ I Utrtu>Þ i ÀMÞ ÁçqEM -C.LEÂR LENLIYPÊ E.I " 9{-J¿Jóq -TÀMF-.4-M -Âf,4 B FP t f llç--lYpF E-2 ' 91-1237+ LAMP ASSEM-_GREEN LENS_TIPI E.2 I r I t+-tz' t1 - IË<t3lôr-rNsrRuMENT I 37A5ZZZ-' FLÂIE UNII_TNTEN}!ÂTIôNÂL 3 " MK, I MOD. I NAME INO.REO. I PART NUMBER { t l t i r I s9EC. Or Þ Rf NO. lL¡NGrH -+råõ--ï'r¡ñ- J_-{-lå- J-xõ5ør'Äcrarro*å -1 SHIELDEô CA¡LÊ -=- .rr.l ,".". o" ,^0, *o- lr.nort zut r +t 18 lls6{8 PACKATD I 42 t{l¡çHlFl DßD a^nr Ft Á? tù¡ - t¿w Tz-1----1--r7- ro I I )) TI-f---1-.rr- lðt '' tlu¿ TE-f==-fr{¡- ytR: >) 56-- BEECHCRAFT MODEL IT .______@____ ¡r :q______ 6 €èi -t, a.ß I l^1 d. (r"E I \r 57 tor tù¿ iÄ I 97 a7 ?3 t6 ¡19 L 87 P EC ----159- i€ ilt t5\ tlt- ,J" I *T -t++ F MASTER WIRING DIAGRAM BEECHCRAFT MODEL IZ REVÉRSING swtTcH A MASTER swrfcH -r t78 -=- LANDlNG GEAR UP POSrf toN LIGHT FUSE BOX CONNÊClION BUSS 8AR A GREEN LIGHT BURNING-LANDING GEAR OOWN Ä swrrcx oPEN-LANoTNG GEAR oowN ¿\ swrrcr cLosEo-LÀNDING GEAR DowN G GEAR FUSE gOX AUSS BAR DOWN POSITION LIGHT CURRE¡T FLOVS FROM THT BATÎERY IO THE MASIER SVITCH. VHEN THE MASTER SVTTCH IS IURNED ON, CURRENT VILL TLOV IO TH€ BUSS BARS AND TROM fHE BUSS BARS THROUGH THE 40 AMP FUSE TO LANDING GEAR LIMIÍ SVIÍCH. THE CURRENT IHEN FLOVS IROM lHE LANDING GEAR LIMIT SVITCH TO IHE LANDING GEAR RTVERSING SWITCH. VHEN THE SVIICH IS IN lHE UP POSIIION, fHE CURRENT FLOWS THROUGH IHE REVERSING SWITCH TO IHE LAND¡NG GEAR MOTOR. VHEN THE SVITCH IS IN THE DOVN POSITION, IHE CURRENf FLOWS THROUGH IHE REVERSING SVIÍCH FROM fHE LOVER LIMIT SVITCH fO THE LANDING GÊAR MOTOR. f. CURRENÍ TLOVS FROM EAÎTERY IO MAÍER SVtrCH. '. VHEN MASÍER STV¡TCH IS TURNED ON CURR€NT FTOVS TO BUSS BARS. LANDING GEAR ELECTRICAL CIRCUIT 3. FROM BUSS BARS IHROUGH 40 AMP FUS€ TO IHÊ LANDING GEAR LIMfT s\flTcH. 4. FROM LANDINGGEAR LIMIT sVfTCH TO LANDING GEAR REVERSING SVIÏ(H. 5. VHEN SVNCH ß IN UP POSIIION CUR. RENT FLOVS THROUGH REVERS|NG SVIICH FROM UPPER LfMI¡ $V¡ICH TO LAND¡NG GEAR MOTOft. ó. VHEN SVÍCH tS tN DO!rN POSTflON CURRENT TLOVS IHROT'GH R€VENg ING SVITCH FROM LOVEN L'MIT siv[Í(H IO LANDING GEAN MOTOR. 1lï--1 r BEECHCRAFT MODEL IT ¿- IHE FLAP MOIOR REVERSING S\IITCH FROM FLAP MOÍOR REVERSING svtTcH To '. TO MASIER SVIÏCH. TROM MASÍER, svtTcH To, 3. THE BUSS BAR ÍHROUGH FUSE TO CURRENT FLOWS FROM THÉ EATTERY TO IHE MASTET, SVITCH. FROM fHE MAs. T€R SWITCH TO THE BUSS BAR IHROUGH A FUSE TO THE FLAP MOÎOR REVERSINC SVITCH. FROM THE FLAP MOTOR REVERSING SVITCH, CURRTNT VILL FTOVI TO IHE DOWN SIDE OF TH€ FLAP LIMIT S\YITCH WHTN THE FLAP R,EVERSING SVITCH 15 IN THE DOVN POS¡TION. FROM THE LIMIT S\YTTCH TO THE FLAP OPERATING MOTOR AND TO THE CROUND, \IHEN THE FLAP REACHES IIS DOWN IR,AVEL, THE LIMIT SVITCH OPINS FLAP MOIOR CTRCUTT. FON, FLAPS UP THE CURRTNT FLOWS THROUGH THE UP SIDE OF fHE N,EVERSING SVITCH TO THE UPPER, SIDT OI THE LIMIT SVIÎCH 10 ÏHE FLA,P OPTIATING MOTOR. \VHEN IHE FLÀPS ARE UP. THE LIMIT SWITCH OPE¡(! lHE CTRCUIT TO THE FLAP OPERATING MOTOR, ó. THE TLAP OPERAIING MOTOR AND ÏO GROUND. 5. TH€ DO\IN gDE OF THE FLAP LIMIT SVIICH VHEN FLAP REVERSING SVIICH IS IN TH€ DOVN POSITION FROM THE LIMII SVfTCH TO r. CURRENI FLOVS FROM B/qTTERY 8. FOR fLAPS UP THE CURRENI FLOVS THROUGH THE UP SIDË OF IHE RÊVERS. ING SVITCH TO IHE UPPER SIDE OF THÉ LIMIT svITcH To FL,\P oPERAf. ING MOÍOR. VHEN FL¿\PS ,{RE UP fHE LIMIT SVIICH OPENS CIRCUIÍ TO IHE FLAP OPERATING MOTOR. 7. VHEN FLAP REACHES ITS DOVN TRAVEL IHE LIMIf SVTTCH OPENS FLAP MOTOR ctRcurT. MASI'ER SV'ITCH 65 67 92 l+ -::- T_9t I: 32 35 34  I t48 to +34 nora /ñ, SWITCH CLOSEO FLAP UP FLAP ELECTRICAL CIRCUIT BEECHCRAFT MODEL .T LANDING AND POSITION LIGHTS LANDING GEAR MOTOR A t2 5¡ 7l 4 A 49 86 87 86 86 86 A 40 F6 I I _.i68 65 I I I L--_ 66 t -ì =65 ìez 68 7 I 9 67 REF. WIRE II8 MASTER 28 v/r r Es REF, WIRE I35 WIRING UAGRAM ER WIRING DIAGRAM DIAGRAM t 84 Hor:¿\-cnrtx LI6HT ¡uRNING-LANDTNG c€ R DovN A-srvrrcx oPEN-LAHDTNc cE^R DovN ,A-swrrcu cLosED-L^NDrNc cEAn DovN ELECÎAICAL ECIUIÞMEI{I D5-3843C Dl7E56 Dt7A550 Dt 78550 B9A B9A B9A 4GA 3AG 3AG B9^ #80 RtD XEO GREEN c-ß.ED ç-GßEEN Y:3226j.- 94-32204 ,1-JZZUA ABA P-4t Z-AB P.410-48 S.{IZ.FHT 5-,tl o-FHT olt Dt70't l2-+ Dt707t2-5 4.5'I ç") ö THE DUMORE CO. SEECH A¡RCRAFT CORP AffCH AIRCRAFT CORP. SEECH AIRCR,AFT CORP. CUTLER-i¡AMMER INC. CUTLER-HAMMÉK INç. CUTLER.H.AMMER INC. LITIELFU5E INç. LITTILFUSE INC. -ITTELFUSE INC. CUTLER.TIAMMER INC. E.'IAKE PILOTLIIE CO. DRAKE PILOTLITE CO. GRIMES AIRCRAFT LIGHTING GRIM¡5 AIRCRAf I LIGH f INç cqyl-Et¿B!¡¡.uÃD--GRIMES AIRCRAFT LICTIIIN( GRIME5 AIRCRAi'¡ LIGT.ITINC RADIOLAE, INC. H.OVA-RD,E. 'ONEs HOVARD 8. .|ON€S |towAx.D,B- loNE5 HOVARD B. IONES RADIOLAB. INC. BEECH AIRCRAFT CORP. SEECH AIRCRAFT CORP. THOMAS fr AETTS CO. lNC, IñqMA5 O ¡ETTs ç(,. INç. MOTOR,. LANDING GEAR sVrlCH - LDC. CEAR POSIï|ON SVITCH - LDG. GEAR UPPER, TCH-LDC. GEAR LOVER s\vITCH -RICHT LD6. LÍGHT SVITCH.LEFT LDC. LICHT SVITCH. POs¡T¡ON LIGHT FUSE - S ÂMP. FUSE. ZO AMP FUSE .6 AMP. 5rr¡Tctt REAR POSITION LIG}IT LAMP-LDC. CIAR VARNING LAMP.LDG. GEAR V/ARNING LÈìt rg)tttqN LAMP A55EM RIGTIT POSITION LAMP ASSEM RIG}II LANDING RESISTOR.IO VATT 25 OHM PLUG - FUSEBOX CONN. PLUG - fU5fðOX ÇONN. SOCKET - FUSEBOX CONN. SOCKET - FUSEBOX CONN. RESISTOR - ,z5 \¡/ATT Ig OHM BUSS BAR - L. II. IUSS 8AR - R. H. DISCONNÉCT SPLI€E gt)ç9NNiC¡ SPL|Ct 4 l2 t3 l4 ¡5 t6 zo 2l z3 z5 zó 40 4t 47 +ð 50 5t 52 65 6õ 67 68 8Z a{ 85 E6 öl 25 23 23 WIRING DIAGRAMS 85 ! : : l f { i I I ( I { i BEECHCRAFT MODEL Iz MAGNETO, STARTER SOLENOID AND BATTERY ELECTR¡CAI EQUIPMEI{T 6T5-13-¡ MODEL I3 ÎYDE IO' Nr r 87 SPECT.AL D1707-I I It77 r520 654 JAC 3AG KV 606-TYPE I4 4N5790-6 NDZt439 4N5525- I AN55Z5- r P-{ I Z-Aö P-4t0-aB 5-4tZ-FHT 5-{ I 0-tH I 3202-35 9t tottL-, r tFFaq ¡ Dt707rz-) ( aEECll ì A'f )Á-rJ-J¿) Dt 79 jlt¡ AFF'HI Dr707r5 9t ru¿ to I RII'H ì Dt 707t 9 r erFaH ! ANJI06,I45-ZJ WIRES SPtCrftcÂlroNs L¡NGI8 IXIDE EATTERY CO. ÞÈlt añtt DHrÁ D^ N CO. I CUTLER,HAMMER INC. AEEC}I AIRCRAFT CORF vragtfÄ xÂNsÂs DELCU RÈMT ÂNñßO<^N tñh CUTLTR.HAMMER INC. V/E5TON ELEC. AIRCRAF] \VESTON ELEC. AIRCRAF] YESTAN ELEç. AIRGRAFI tNsT aô NFVÁ¡X N I PtoNEEt lNsT. CO. BßNbIX N I EEECII AIRCRAFT COR,P. VI'HITA KÂN<Âq THOMAS fr AETTS CO- I NC. CANNUN ILÈCI c9- I ^< ÀNatt l< a^t ¡E AEECH AIßCRAFT CORP vtaHlTÀ (^NsÀq BfEçñ AIRCRAf f C9KT, ,9Kr, EE€CH AIRCRAFT çORP. vrcHtlÀ KÂNsaq ECLIPSE AVIATI DÂ<fôÞÂNer ¡ FORD MOTOR CO !ÈÊçH At(lKAÌ vtaHtr^ (aN( !ÉñGtH WIRE NO, stzE BATT:RY STAR,TER SlvITC}I - MASTER 5U/ITCH. IG¡IIT¡ON STAR,TER BUTTON swtTcH - SoLENOtD SVITCH.?ITOT HEAT FUSE - IO AMP. FUSE - 6 AMP. cotl - loosTÉß AMMETER SlvITCII - SELECTOR REsISTANCE AULE.çARE. TEMP XÈ5II IANçE üULõ - OU ISIDI ÁtR rLUU tu)ÈÞgà tgN. FLUG - FUSEBOX CON. )QCKET FU5ÉðqX CON. )0lxÈ I tu)Èóqà tgN. PIIOT HIAT IUBE õu55 SAR L.Ë. öu)) úAK ¡.n. PLUG - CANNON I ¡ÈXt IKVVN9 NC CABLE ASSEMELY 6ATTERY CAöLI A55EMüLY soLtN9rD çAöLI A))ÈMÞLI )IAKIÈK tñÈa Arx ¡nÈÁmgMÈt3K tPtctftcaTloN5 srzt WIRE NO. I 3 6 7 8 9 ì8 24 25 1Z +6 ol 5Z 6J o{ o) 66 6I oð õ9 8{ E5 ðÞ ðö 'J THERMOCOUPLE r------ @ ------t THÉRMOCOUPLE 89578 ,.rJ--n 416 415 i?^ -|-.l88 t- 1--+--i trle I2O LONG 0755780 PITOÏ 43 I TEMP. GAUGE 7 wEsToN 6û¿ TYPE 2 r- iss L- l 7 42 OUTSIDE AIR ,AND CARBURETOR TEMPERATURE I I I L i86 I 64 ----t-66 z _ ___:68 3 REF. WIRE 90 MASTER WIRING DIAGRAM I I L f ' .85 f -86 REF. VTIRE I23 I ì I I I I 7 + I 46 { REF. ÌVIRE I37 MASTER WRING DIAGRAM 66 r ---- 7 l- I I A. -199 I I rL wtRE 69 366 Jo 84 I GND B ro o ï c T z4 \)IIRING DIAGRAMS 25 6l ELECTÞICAL ECIUIÞMÊNT 7Y6t E7 SPECTAI to 5v-75 3AG 3AG R l8-ZO I ô6¡17 ( ßFFaH r 80 RED 606 TYPE 14 6813-777 A Dt 7078 48lA-t377? s-l-A 5-t -a MK. I MOD. I 602 TYFE '7 P-4 I Z-Aö P-{t o-aa 5-{t z-fä¡ s-+tu-tñ I tðtü-JA Dt70E45 ( BFFCH I I eFFaÉ | CUTLER.HAMMER INC. CUTLER.HAMMER INC. MÍ VÀUKFF V¡q LITTELFUSI ¡NC. LITTELFUSE INC. aH¡aÀaô t¡ I CLAROSTAT CO EROOKLYN. N, Y. STEWARTVARNER CORP- STfWÂPTVÄPNFE CÔR9 DRAKE PILOTLITE CO. aH¡aacô !t I WISTON ELEC. AIRCRAF'T FORD MOTOR CO, ñç^ÞeôÞN Mtaq EEECH AIRCRAFT CORP FORD MOTOR ÇO. CAMERIDCE INST. CO. NßV YôÞK N Y CAMERIDGE INS INTERNAT¡ONAL FLARE SICNAL CO.. TIPPICANOI V'ESTON ELEC. AIRCRAF'T INçT Cô NFVÂIK N I NOVARD ö. IQNES ñ9WAXU ó, rgNÈ) aHtaacô il I HOWARD U. loNfs F9WAKU !, lVNt) aHrcÂnô il I FIONËËR INS I co. BEECH AIRCRAFT CORP. vraHrl kÄNs öÈIIE A¡KçKAI I CgKT, ìI/ICHIT KÀNS- SVITCH - MAsTER, SY/ITCH - MAP LIC'IT FUSE - ZO A.MP. FUSE-5 AM? RHEOSTAT S\À/ITCH INSTRU. MENT LIGHT ffiTÂB INDICÄTON LAMT - IUIL TKÈ))UKI VÂRNINN AMMETER LAMP A))ÈM,. çAöIN UgMÈ LAMP Á,55EM. INSTRUMENT MAF RÈADING INDICATOR . FUEL ANALYZER çELL. FUEL ANALYZER TIaR-E u]¡rr ç9TrëF:ñ¡Ã31Fñ'T[ÃñE- IND¡çAT9R - CARBURETOR {t ôIITSIòF ÂIR IFMPFEATIIIF rLuG-ru5Éõox coNN IU)ÈDUA LUNN. )QCKÈ I ru5rö9à coNN. TU5ÈóUA LgNN. g9Mfa)5 BU55 ¡AR-L.lt. 6 I9 za 25 26 5t6 {6 >t 5+ )) 56 >f E59 ót o> E+ BEECIICRAFT MODEL IT CABIN LIGHTING FLARE UNIT 55 46 REFERENCE MASTER WIRE I WIRING 60 53 54 RECOGNITION LIGHTS REF. ITEU MASTER 9 REF.ITEM 92 MASTER WRING DIA. 57 WIRING DIA. :: REr. wrRÈ rz MASTER WRING DIAGRAM 85 t9 87 97 80 7g I I 7 IREF'VYIRE 72 I MASTER lwRrNglrA. i-{-^LZ\_-L d FUEL PRESSURE WARNING UNIT REE W¡RE I32 MASTER TURING DIAGRAM 4_J 98 ï ìs ¿ 5 ) 66 6t ,t 65 -i es 56 -Ì1 67 FUEL YZER 35 I 85 73 25 84 7t COMPASS ìIIRING DIAGRAMS ?5 ( I { i I I L t- { i I 1 fj I I I I I f I f ( f i I ( I I L- il 2 G- BEECHCRAFT MODEL Tz GENERATOR FUEL TANK DETECTOR AND GAGE UN]T FLAP MOTOR 2 29 _@_. A 34 T --l I I -J 89 86 I I L__ 86 @ 33 1-- t2 86 r <- tt a_ I ¡o t- -t I 67 T-* - j66 t7 I t L- 3 7 _9æ _89 -f tol r02 J 85 84 ?2 84 nore/ôr.: swrroH cLosEo-FLAP uP 2t 74 ELECÎRICAL EQUIPMENT PART Trrdtf- tlll4l WIRES VTNF¡ JÈ LENC?H 74 '-'76- *654 PACKARD (H¡ßr ñFD aÁBt ß-TF- -Td- -r ¿, BETTS CO- I sPECtflCÂTtOX5 ^N-t-c-48 - lrz¡ -Tr -w vttÉ xo. vrcE Nô I stzÉ I s¡ÊctFtcÂTtoNs 36 I lzt -ãf--t--tzf- -:õã--f-ft-1-- +9 I tð I -ir-frã-f--T-1-rr-ræ PANI NO. s-{ I z-}ñ r 5j{TO:FFÏ- TT?77'rruEEr:HT* ï]lr- utttu)Þ rD3ß!n, Dt 707 I 2-4 ffi vrNDon tr:r xol NÂMI WIRING DIAGRAMS l f I BEECHCRAFT MODEL 17 2 V. EULBS REO. -,-5Wl ./ #tTCH A WIRE PACKARD SLACK 2 <-GAS GAUGE TANK UNIT LIGHT #48t-r37 SELEOTOR SWITCH GAS GAUGE \-c ts rl GROIJNDEO FUEL PRESSURE WARNING LIGHT SWITCH swrTcH TA8 INDI INSTRUMENT D UNIT RHEOSTAT ON ELEVATOR PERATURE lr /o\ ¡ Ir 'LTGHT \_/ ] I lr Ir Ir NAVIGATION 40A-4 IOO OHM IO WATT RESISTOR LITTÊLFUSE H. SWTToH - CAT. NO.8364-K2 FUSE BOX RM FLARES rl M FLARE SWITCH MAG MASTER STARTER BOOSTER COIL STARTER rl SoLENOtO SW 5,lt rlrlr GENERATOR CONTROL BOX LIMTT SW A RED I,VARñ¡ING LIGHT GREEN WARNING LIGHT rl BLACK SWITCH OPEN GEAR DOWN MOTOR A A LIGHT SWITCH CLOSED GREEN LIGHT BURNING MOTOR SWITCH CLOSED LANDING GEAR DOWN LIGHÎ SWIÎOH OPEN RED LIGHT BURNING LANOING GEAR UP sw. DowN LANDING GEAR APPI.¡GABLE TO DITS ANO DITR sERtaL NOS. 136 TO 424 lNC. I MOTOR RETRACTS + FIELD SIVITCH LITTELFUSE 4AG o LIMIT SW. UP FLAPS MASTER IíIRING DIAGRAM ( f i I I ( Ì I i t I f i { i Í f i f i SECTION IV SPECIFICATIONS, REPAIR AND BASIC MAINTENANCE LUBRICATION CHART SWINGING THE COMPASS AIRPLANE HANDLING IIING RIB AND SPAR REPAIR STEEL TUBE REPAIR TUBING SPECIFICATIONS CABLE SPECIFICATIONS fI I L I I t_ f I I I L, ( I t I I t_ f I 1 ( I 'l{ r I L f I r I L- f i i* II I L BEECHCRAFT MODEL TZ NOTE, ALL PARIS LUBRICAIED VITH S.A.E. NO. 1O MOTOR OIL UNLESS NOTED. 1- D17t750 FLAP OPERATING MECH. - OF FLAP OPERATING MECHANISM SHOULD EECOME NOISY.) LUBRICATE FLEXIBLE SfIAFT AND HOUSING VITH SPECITIED OIL t8 2. D1726Ún FLAP OPERATING MECH.-LUBRICATE GEARS VIÍH SPECIFIED OIL lle + 20 3. DI785GI,1ó LANDING GEAR SWITCH CONTROL SHAFT (BEHIND IN5IRUMENT PANET) *ll 1. D117119 HAND BRAKE CONÏROL ASSEMELY m# 5. D1779,I3 LOWER PARTS OT RUDDÉR PEDALS. PILOÎ ,{ND COPILOT POVDERED ó. D17850.38 SLIDÊ ÍUBES (GRAPHIÍE ONLÐ 1. D11820 UNTVERSAL OOP OF REAR LEG, LANDING GÉAR) lô zi ll8, DI784O UNIVERSAL (TOP OF SHOCI( ABSORBER I.ANDING GEAR) 9. DT?8IO DIAGONAL LEG (OIL CUP ON LOWER LEG) lo- D1781o UNTVERSAL (LOVER END OF DIAGON^L LEG LANDING GEAR) 11. Dt7840 SHOCK ASSORBER ASSEMELv (OlL CUPS ON EACH SIOE OF TORK) 1T. VHIEL EEARINGS (LUERICAIE WITH MOBIL ZERO GREASE PDit33 GRADË B SPECIFICATION AN35óo) 13. D178ó9-10 IAIL VHEÊL SLIDE IUBE POVDERED ONLY) 1¿, D1787OO AI BOTH ZERK FITTINGS USE MOBIL ZERO GREASE PD433 GRADE 8 sPËC. AN35óO f 5. DI?8?OO TAIL VH€EL HOUSING AND FORK ASSEMBLY_OIL ÍAIL VHEEL LOCK PLUNGER *i *s *6 i7 *8 I 1 f ó, T/\lL VHEEL BEARINGS (LUBRICA'ÍE WITH MOBIL ZERO GREASE PD433 GRADE 8 SPEC. AN35óO) 17, DI786O UNIVERSAL AT BOTH UPPER AND LO\VÉR ENDS OF SHOCK ABSORSER '8, D'7óO'ô RUDDÊR HINGES 19. O177791 RUDDER TAB CONIROL ROD(AT fAS TND) 'O. D1'?79ó ELTVAIOR TA8 CONTROL ROD OAB END) tl. Dl7óot5 ELEV,\IOR HINGES NOTE. SHOCI( STRUI FLUID FOR MAIN GEAR AND TAIL VHEEL SHOCK IS AC358OC, (REÐ COTOR TLUID) COMMERCIAL EOUIV- ALENÏ - UñlVlS No. 40. LUBRICATION CHART I I f , l ( I f i BEECHCRAFT MODEL IZ NV NE NV NV NE w E v E sw SE ERROR DUE NORÏH ERROR DUE E,\Sf ERROR HALF ERROR ERROR HALT ERROR COMPASSÉS SHOULD BE CHECKED FOR ERROR (DEVIATION FROM MAGNEÍIC HEADINGS, CAUSED BY MAGNETISM PRESENT IN rHE AIRCRAÐ AND COMPENSAÍED AT THE END OF EACH TOO- HOURS fLYING TIME, A1 EACH ENGINE OR ELECTRICAL EOUIPMENT CHANGE IF fHE LATTER IS LIKELY IO ATfÊCT COMPASSES, OR AT LEA'T ONCE DURING EACH THREE MONIH PERIOD. GROUND SWINGING OI IHE AIRPLANE COMPASS MAY 8E ACCOMPLISHED BY MEANS OF A MAGNEIIC EEARING SVINGING EASE (COMPASS ROs€ VITH DIRECIIONS GIVEN FROM MAGNEIIC NORIH), OR ,q MASTER COMPASS. USING fHÊ MAGNETIC S\IINGING BASE, HEAD THE AIRPLANE NORTH \IITH |fs LONGITUDINAL AXIS PARALLEL TO fHE N.S LINE. IF THE COMPASS DOES NOT INDICATE NORIH (O D€GREES), ADJUsI IHE N-S COMPENSAIOR. USE A NON- MAGNETIC SCREVDRIVER FOR MAKING IHE ADJUSIMENÍS- THEN, WITH ENGINES RUNNING Af SUFfICIENT RPM IO SHOV/ THE MAXI- MUM CH^RGE ON THE AMMÊTERS, RECHECK COMPASS, AND RE- ADJUST, IF NECESSARY. HE^D THE AIRPLANE EASI (9O DEGREES) AND RÉPEAT THE ABOVÊ PROCESS, ADJUSTING fHÉ E-\I COM- PENSAIOR, IF NECESSARY, HEAD THE AIRPLANÊ SOUTH (T80 DEGREES) AND IF THE COM. PASS DOES NOT INDICATE SOUTH AÞJUsI THE N.S COMPENSATOR ONE.HALF OF IHE ERROR. THEN HEAD THE AIRPLANÊ WEST (970 DEGREES) AND ELIMINATE ONÊ-HALF OF THE ERROR, IF ANY, 8Y AD.|USTING "THE E-W COMPENSATOR. fHE AIRPLANE SHOULÞ NEXI BE SVUNG ON E^CH SUCCESSIVE l5.DEGREE HEADING, AND THÊ READINGSRECORDED IN THE "R,\DIO OFF'' SPACE ON THE COMPASS CORRECIION CARD, FORM 57. IHEN, VÍIH IHE RADIO RECEIVER IN THE "ON'' POSIÍION, IHE AIRPLANE SHOULD AGAIN BE SVUNG ON EACH 15.DEGREE HEADING AND THE READINGS REEORDED IN THE "R,\DIO ON'' SPACE ON THE COMPASS CORRE€ÏION CARD. IO SVING THE AIRPLANE, USING A MAÍER COMPASS, TH€ SAME PROCEDURE VILL APPLY, EXCEPT IH,\T A SERVICEABLE, NONCOMPENSATED COMPASS, ATTACHED TO IHE WING TIP, VILL 8E US€D TO DETER,MINE THE POSITIONING (MAGNETrc HEADING) OF IHE AIRPLANE, ,/, .l'f ll ;: o f SWINGING THE COMPASS BEECHCRAFT MODEL IT VHËN REGULAR HOISIING EOUIPMENT IS NOT AVAIL. ABL€ 8E SURE TO USE SOME TYPE OF SPREADER BAR, IHIS VILL PREVENT BENDING LIfTING LUGS. AVOID JERKING OF AIRPLANÊ \IHILE HOISÌING. REMOVE HEAW BAGGAGÊ, EIC THESE CAUÏIONS ELIMINAIE DANGIR OT BREAI(ING LUGs, . , ,' rl,' 1. fHE AIRPLANE ls HOISIED BY T\lO HOISTING LUGS LOCAIED ON TOP CF IHE CABIN- A HOISTING SLING AS SHOWN IS FURNISHEÞ WIÍH ÊACH AIRPLANE, ,I. THE AIRPLANE SHOULD 8E .IACKED UP ONLY FOR MINOR REPAIR AND \IHEN LENGTH OF TIME NEC€sSARY TO MAKE REPAIR 15 OT SHORT DURAIION. NONE OF MAJOR COMPONENT PARIS SHOULD 8E REMOVED VHILE AIRPLANE lS ON JACKS. T\VO SEÍS Of J,\CK PADS ARE PROVIÐED, ONE sE'T AT LOVER END OT LANDING GEAR RIAR LEG AND THE O'ÍHER SET ON REAR FUSELAGE TRUSS NEAR WING ROOT AITACHMENT POINTS. lAlL Of FUSEL,\GE SHOULD BE WEIGHTED DO\IN. 5. THE IAIL VHEELSHOULD 8E MOORED EYTYING ,\ROUND THE SVIVÊL HOUSING JUSÍ ABOVÊ THE FORK. MOORING LUGS ARE PROVIDED ON LOVER SURFACE OF LOVER VINGS AI REAR SÍRUT ANACH. MENT POINTS, r. WHEN HOISTING AIRPLANE, APPROXIMATELY 3OO L8S. SHOULD BE TIÊD TO THE TUSELAG€ ON A Z" DIAMEÍER TUBE OR BAR IN. SERTED IN tIffING BRACK€ÍS NÊAR BOTTOM OT FUSELAGE AT LEADING ÊDGE OF Í,\BILIZER, TIE WEIGHTS VITH A ROPE OR CABLE LONG ENOUGH TO ALLOW TAIL TO RISÉ ABOUT 9 OR 3 TEEI SO TAIL WHEEI- CAN REIRACI. 3. TOWING LUGS ARE PROVIDED AT POINTS SHOWN IÑ ILLUSTRAIION. AIRPLANE HANDLING L I t i BEECHCRAFT MODEL 'T WING RIB REPAIR LACING FABRIC SPAR REPAIR t0.A t/4 A 5A ,,/, /4i, /' 'ITTINCS VITHIN THESE LI c 8.A 8A 5 TO I SLOPE E c I DIRECTION OF GRAIN IF SPRUCE. OR ACE CRAIN IF PL -,./., 3A ? 3 4 OF FACE OÍTAIN OF PLYWOOD LOCAL SPRUCE BLOCK LONCITUDINAL CRAC( HERRINCBONE TAPE SPECIÀL NEEDLE REQUI RED PRE-SPACED HOLES METHOD OF REINFORCING A LONGITUDINAL CRACK AND/Oß, LOCAL DAMACE IN A SOLID BAR B 6A I aT a lorNT oR EETWEEN IOTNTS ADD SPRUCE ELOCK {abcdef) HAVING SAME WIDTH AS CAPSTRIP VHEN SPLICE IS MAOE EETWEEN IOINTS. SIDE PLATES NEED ONLY EXTEND TO LOWER EDGE OF SPRUCE ELOCK IN Tl{rs cÂsE. A, B, C. D, E-ORIGINA,L D¡MENSIONS. REINFORCE. MENI PIATES SI{ALL BE PLYWOOD GLUED AND NAILEÞ. NAIL HEADS SHALL NOT BE IMBEDDED IN TI{E PLY- FABRIC \)íOOD. ÞAMACEÞ MEMBTRS SHALL B€ REPLACED ENTIRELY. FABR.IC RIB DIRECIION OF CRA'N IF SPRUCE OR OUÎER FACE CRAIN IF PLYWOOD HERR,I NCBONÊ METHOD OF SOLID 08. LAMINATED RECIANCUIAR SPAR TÁ.PE PINKED TAPI AT TRAILINC EDGI FAERIC ARROII/S INDICATE PLYWOOD CLAMPING PRÊSSURI \VRONC -CONCENTRÂT¡O PRTSSURE SPRUCE OR BASS \7OOD Rt8 DAMÄ.CED B FAERIC PR€SSURE BLOCKS RIGHT_EQUALIZED PR,ESSURE APPLYING PRESSURE FOR GLUEINC GLUE - PLASKON CORD*ARMY ó- 'i uN w \\ \IING RIB AND SPAR REPAIR TyPE r50-? BEECHCRAFT MODEL IT SPLICE VTH SLIP OVER STEEVES REINFORCING A DENT AT A STÊEL IUBE CLUSIÉR JOINT STEEL ]U8E FISH MOUÏH SPLICE AREA SNUG TIITING TELÉSCOPING SPLICE MEMBER ,<' MINIMUM RADIUS MAKE SQUARE CUIS AT THESE POINTS 4%D MINIMUM :roRr (A:B OR 8+) L (c-B OR B+) STUB ON ONE ËND TO FACILIIAIE SLIPPING SPLICE MEMBER OVER ORIGINAL ÎUBE L I D PREPARE SPLICE MEMBER AND DIAGONALLY CUI SLEEVE S (S:T OR T +) REINF()RCING I CUT AND FORM I,., MAXIMUM GAP SNUG I¡ÍTING TELESCOPING SPLICE MEMBER REPAIR ROTAÎED 90' CENTERING INNER SLEEVE IN STEEL ÍUBE VILL ÊND HERE INSERT SPLICE MEMBER IN CUT.AWAY PORTION MARK AT OT CUT SLIP SLEEVÉS OVER JOINIS AND VELD MARK, CUf, AND DRILI. TUBE END VÉLD ALL EDGES OF REINFORCING PLATE D DRILL NO. 40 HOLE SLANTED NOTE: SLEEVE MAY BE ROIATED TOR MAXIMUM REINFORCEMENT COMPLEÍED SPLICE USING DIAGONALLY CUT SLEEVÊ,S REINFORCING ARRESÍ ED GROVTH OF CRACK CORRECTING EGG SHAPED AREAS END'A. NO. 40 HOLE ,{T EACH END \IRENCH AND TIGHTEN SCREV DUTY SCRTV CLAMP PUSH I VELOING ROD THROUGH HOLE AND OUT END OF TUEE CRACK ÊND "8" I-[ B GROOVÊD METAL BLOCKS EGG SHAPED AREA WÊLD END "4" TO INSIDÉ OF SLEEVE MAKE MARK AROUND CÊNfER OF SLEEVE ARREST GROVTH OF CRACK SNUG FITIING SLEEVE CUT IN HALF CHAMFER END IO AID SLIDING CUT AND MARK SLEEVE AND WEID ON END OF SLEEVE PULL¡NG VIRE ORIGIN,\L sPLICE T PRÉPARÊ REINFCRCING SLÊEVE (r-8 oR NOTÊ. EGG SHAPËD AREA MAY BE HEATED TO A DULL RED AS AN AID TO RE- FORMING PULL END "8" INTERNAL SL€SVE 1\4D (MtNIMUM) INSERT SLEÊVE INTO SPLICE MEMBER AND ALIGN IUBES VELD SLEEVE OVER CRACK INTERNAL SLÊEVE ÌU8E VILL BE ROUNDED VHEN BLOCKs ORIGINAL ÍUBE %' MEMEER COME TOGÊTHER SLEEVE PULLING ROD AND WELD HOLE AFÍER COMPLETION OF REPAIR COMPLETE REPAIR ROTATED 90' STEEL TUBE REPAIR PULL VELDING ROD UNTIL CENÎER MARKS LINÊ UP i.- I I { : ( f i i I f l f r BEECHCRAFT MODEL 17 f> OIL SYSTil LINES ]í, DIAMEIER E OVEE SEE FIGUÎE FOR REFRENCE E E c D D FUEL SYÍEM LINES 'í. DIAMETER ¡ OVER S€E PAGE 95 FOR REFERÊKI a D D D D D D D c D %' DtAMÊlÊR & OVER FOÊ REFERENCE c C c c AIR 9SEM LINES 9,í' DIAMEIER ¿ OVER FOR R€TÊNENCE c c c c c c c B B c D D a oä de na B RB 8v8 Y n & 8R R R R R ß R R R R m 8tr BT B¡ BA VG VG VG VG VG VG VG VG VG VG trc \IG VG hÈ :> .6 _tq .24 19 ,18 .13 _t3 .Ð .18 -03 .t3 ,ó7 to -13 10 .6 ,33 .ot .14 .ot .03 .21 .94 ,12 t3 oa .æ .t8 .11 .o¿ -6 .o7 .11 .t5 -to .o7 ú 13 .11 -oJ .13 .æ .tr 5t -o7 .m .93 .fl .46 .11 .tó -21 .to ,d -11 -@ .19 .14 _@ .0ó .31 .03 .14 .o8 ,0t .lo .91 .10 .1t ot .0ó -91 .29 -o3 -05 .o? to .tl ta .06 6 fo .19 .o1 -11 -o7 .17 Oô sô; 2¡;a <<F ã 9? 171 ¿ 1.r i 19 tt 3,U rrll e¡.i 4Ìå s% 1% 5rt 2!.,á 1 4t/c rH t111 ei¡ 7% trt 93/ 3t¿ 3+* lt¿ 1* 1% ?% 19!Á I 1tt 33rt 101,1 IH 9.54 3 stÁ 8€ND NO. ,{ OJË <ô'! ã;ê 9-?â z 8€ND NO. 3 Éoü z L l5' L s' L9û L 105' L t7" 3 1% 11/4 1% rlí <ôù R 1ó5" 130 ì 1ô5" ó5' I t0 ri:âù2 8ri t ,14 a% 1% SIND NO. r z L ,l L48 L lr9 L83 L4T LS Ló5 Lt9 L 50" L 80¡ LS' LÐ" L6ü L 11. L 05 Læ L 99 Lt5 L35 L8s 3 9:4 1% 3 1t1 1'A r% lt/ 1 1% 1'l 1tá 1% 1V 1U 1r7 1% zi3 <oü õÉ: L lto" 0" t9ff 91' )' 90" f5' I 41" 90" 0' d 85' I tts' L 85' L 11' R rór (>^ 2UZ 3 e% 3 3 3 ,916 3 3% 3% 4V; 1% 3tá 31Á lor4 , 111 9ri BEND NO. 1 ãõ9 z NO BENDS L ót L95 L 50 L 1S LÆ L 11 Lca L99 L 58 L 3a L e NO BENDS Læ NO 8€NDS L70 L ll5' NO SENDS LS' L'? L 88 L88 L t5 L 180 L 88' L lt3' NO BENDS L ó5' L 90 L90 L 05 L 75 L83 L 90 L at L 90 Lø L90 L95 Lt5 L 53 L5t L90 de- zu= ;xs ã*g 3 3 e\ 2% 1ys 3 1' l r,; l\4 1tá 1\ ¡ 1rî tx th 1)4 3 1% 1% 1U 1rÁ 1 t/4 1% 1y; 1rí 1t4 1)a 1U 1% 1tá 1% 1t4 1% 1't 1 3 3 1% I 9 3tÁ 9 5% q 5% 2U 99 37 7% 9ré 9 1a)1 1% a% aarÁ t q% 316 lo 8 t7 2 11Á I t e% 91 r; 10tz 18 stz€ I =úo Átt 1 1rá 19t í a5'/Á 13t4 tTlt 1ó 1211 8å tf++ s, ll 11!z 10r:a 1t 1* 31rá 1y'¿ 38!å 191Á 8rí t9% 31H 1r'/Á rot; 1)á 17% a% 1311 99H 9t1 é 18% 153/6 5 t4ll 11 Ì5t4 o 0 .o49 .oß ,0a9 .049 ,o35 .ü9 .o19 .0¿9 .o¡r .035 ot5 .o35 .035 ,035 .035 .049 .o35 .o35 .&t .o¡i .o4c -ilÎ .o49 .04? .dt .o19 .049 .049 .u9 .o!! .03t .035 .o35 -o?5 ,o35 olt .03! .035 ,o¡5 _o49 .o12 .øt ¿i 6 I 1 % 9i 3A .1.6 1 I 1 ,t % ,6 ,4 ,t ,í, % % % tÅ 'Á ,l ,4 x % % t/6 tÁ 3:Á 9t % u ', % +í tÁ |,1 tí % ,i ',' MATERIA,L 560 52SO 5qso 5tso 59SO 59þ 59SO 59SO 5t50 <OPPER cmR coftR COPPER COPPER rso 52SO 59SO 5tso 5tso 5tso 5lso stso Stso trso 5?SO 5tso 59Ð srso 59SO sso 595O 5*O Srso sßÕ 5rso t9s 5tso 59SO 59SO 5tso 5tso s9so REF. 1 2 3 4 ó 7 8 9 l0 l1 t! 13 71 I5 ló 17 1g t9 20 91 e9 93 91 t5 26 97 9a 30 3t 3t ?? 11 35 36 37 38 39 & 41 42 13 PARI NO. D17S1t Dt79A1 1 D179017 Dl7m18 Dl 79019 D1tS85 D17598ù6 Di798rO Dl7981 1 Dl7981 5 Dl70f m-t D1701S-3 Dl70ls7 Dl 7019C8 Dl70t G9 D17971-1 1 D17026t Dt799ll DrTttTt D11997A ø7nD D17*85 Dt't918ó 0179i91 D179m Dt79535.9 Dr79535-3 D17953t9 Dl?oç1s-ro Df79535-1r D170312 Dl7031 3 Dr70314 D170319 D1703?9 D17032+3 or70¡3t D170333 Dr70336 Dt70a84 Dt7900! Dl7mS Df?ffi (1 fYPE A sEFoæ 8EM-] TYPE B FLARING OATA (9 ANGLE OF FLARE 25" 30¿ 30. 30" (9 T;í: FLÀRE 3s9 42t .484 .656 .78r .937 r.rg7 Ðo.0. oF IUSE t^ ,. ,I MINIMUM BEFORE BEND h ,4 "/6 7e þ'/s ,4 h h tuaE r yø h *ß yz 12 ,4 MIN. I I I T6 ,8 fvpE c TYPE D TYPE E OIAGRAM OF ÎUBE AENDING MACHINE OEdEE OF ROIAÍIONAL 9En0s reft SEXD ilofcÆo &0 lURN LEFI iIOHT I@IOE FIGHf - BEÐ iofatioN RML N DÉ@É PLAN V|EW ENO V|EW 8É¡6 PrcæEss FROil fRONI tO REARr L€FÎ 10 ircHt, oR IOP TO €OlfOÍ W¡fn 'USE |N5fÁLLEO 't A|RÞ!¡E. ALLOIXANOE þ" ruBrNG FOR SPRINGEACK SENO 2riMORE ÀS " 2 jâ'¡toRÉ ) ( ¡O1Ê: aLL slE€vEs ato TuEE NUrs ae€ paRtÉR B[ rypEs TUBING SPECIFICATIONS \ BEECHCRAFT MODEL Iz NTTINGS USED Ê. Ê. 3r4 AN?7O.1óLL ANI 15-1r ANl 7û1 óRL AN17&IóRL ANt{,165 ANl 30.t1 L ANr 1J.3t ANt r5-3t ANI'G91NL ANI?G91 LL AN115.31 ^Nl 3GllL ANl ?G'tRL ^NtfJ.rf ANl 7OIóRL ^Nl70-ÍôRL ANl15-t1 ANITO.IlLL ^Nlr 5-3t AN1&-85 ANr 15.ró ANl15.8 AN1 30-1óS ANrt 5"8 AN16-1óS AN148S ^Nr00-4 ^N3EO-3-4 C ANtm-3 ¡@Fló- É-r@ t@Flô Étæ rw-ft& btm rM& Élm ^N38G3-3 ^N1@4 ANr00{ AN100-¡ ANfG ANl00-4 ANr@4 ANl@4 ANlm-4 ANI& AN1æJ ^Nro0-4 ANlm-4 ,\N100"3 AN100-4 AN1& 4N100-4 ANIG4 ANrO0-1 ANræ.3 ANlm-4 4N100-4 ANlæ-4 ANlm-4 ^Nrm-4 ANlß4 AN1o0.4 ANIOG4 ^N100-a 4N100-4 ANrm.4 AN100-4 ANIO0-4 ANr00-4 AN1æ-3 1ffi9&F10- o3-r@ AN1æ"4 AN'&4 ^Nr0ê4 AN!G AN1æ-4 ANI@3 ÂNt@3 IURNSUCKLE AARREL D1758lt VHEEL FAIRING 75899-t ? ¡ 7 PREFORMED 3ó I I 4N155-161 AN155i6L ÀN1 55-t1 L ANÍ55-9IL ANt 311óL ,AN155.1óL I c 2 t 3 3 4 5 6 1 8 9 10 11 1l t9 t3 !3 11 15 16 11 l9 90 ll 9t 93 91 SF 1 1 I 1 t 1 1 I I I 9 1 1 2 I I 1 1 1 1 1 I ol =Y !91 $ r17 tor; 18 21 lz 13 17 ri t 1'Á 938rí 2O5% e71 U 39% tl5 90ra 1ó 1t 5æ% &st4 9Sh t9)Á 193 4 98t4 ltofi 99"i <6 ,; l.í t4 lí ,1 I' rj t( DESCRIPIION OF CAELES r . c^R80N sÎÊÊL J ú CARBON SÏEEL ] J CANBON SfEEL I] CARBON STEÊL ld CAR8oN slÊ€L 7 r t9 PREFORMÊD 7 ¡ 19 PREFORMED Ii CARBON STEEL & CAREON SIEEL !1¡ CARBON STÊEL T CARBON STÊEL }/,{ CARBON ÍEEL ,I CAREON SÍEEL ]< CARBON STEÊL I' CARBON STEEL ]ú <AR8ON SÎEEL 7 ¡ 7 ffitFORMÊD ] ¡ 7 PREfORMED T COR. RES. CABLE ¡Ì CARBON STEEL 7 ¡ 19 PREFOßMED !r1 CARBON íEEL 'í COR. R€S. CÂBLE 7 ¡ l9 PREFORMÊD 7 ¡ 7 PREFORMED 7 ¡ 7 PRÉTORMED MADE UP )¡ CABLE! Di Ì7001-2 D17700!.t Drûm9-3 Di77003-9 Dr770Ét Dr?r005-9 D177m5-4 D17700é? Þ1 7t007-i Dl77@8-? Dl77@-t Dl 77010-t D1 7701 G3 Dt?7û I -q Dl 7?01 1.3 DI7701 ?-? D111111-1 D171613-1 D17??l 0-9 Dt119&-1 D177955-1 oltæ1Gl Drtsol t-r D1 t80f5-t D17871&1 D178116-9 ASSEMBL' NAME AILERÔN RIGHT AILERÔN CONTROL COLUMN CONIROL COLUMN REAR CHECK fRONT CHECK EIEVAIOR Iæ ttEv^toR 80noM ELEVATOR REAR RUDDÊR LEf AILERON RUDDER CONTROL L.ER. RUDOÊR STOP ELEVAIOR TAB CONIROL RUDDER TA8 CONTROL PARKING BRAXÊ SRAKE BALANCE lAIL VHEEL NSÍRACTING TAIL VHEEL RSRACÍre TAIL \IHEEL RÍRAõING TAIL VHEEL LO<K CASLE ASSEMBLY NUMBER Dr77@r 'Dr7700: Dl 77003 D17rO01 D177æ5 D!7t& Dr7700t Dl 77008 ù7tm 'DrTtoro 'Dr ?tol I Þ1 7701 I Dt?t1r1 Dl 7?ô1 3 Ù177710 Þ1r79ß Dr7U5 Dr ?aoro Dt t80t 9 D178015 Þr t871ó F--LENGIH GIVEN ON CH/\RT cHARfNO.f,90 B D c CHARI NO. 9, 1,5, 6,7, A,9,10,',t1,11,19,19,21, rt,91,24 D CHARI NO. 3,19, 13 B c CHART NO. '5 LENGTH NOTE: WHERE IHE ASTERISI( IS S¡-IOVN THÊ T\vO CABLES ARE SPLICED TO MAKE ONE, CABLE SPECIFICATIONS CHART NO. Tó, 17 t ( f r f SECTION V PERFORMANCE DAÏA SEA LEVEL TAKE.OFF OPTIMUM ALTITUDE CRUISING CLIMB MAXIMUM LONG RANGE CRUISING TAKE-OFF OOOO, OPERATING CHARTS ( { : ; f*" ã'* ç ùb"+,. _" "¡;. , È tl BEECHCRAFT MODEL .T ï o<'.1 l¡ 0 /f-\(r I a FLAPS ia lHROTTLE ^V/ MIXÏURE @@ @ O o, 4 4 2 2 lìUl{8 tlP 00gr{ ts CARB SID€ a!8 ÀlR sEA LEVEL TAKE-OFF þ'þ' f i._ f i L I L I I I I I r I f I f I I ( I II L t I \- ( I I î i._ , I L- BEECHCRAFT MODEL T; OPTIMUM ALTITUDE CRUISING 6s% ?ov,ER @ O @@ 1\ '! \s f Í L I I t- t_ ç I L L L I L ,f L tL. L L L t_ L BEECHCRAFT MODEL IT íñ p "r*€ ABOVE 5OOO FEET RATE OF CLIMB IIILL BE REDUCED APPROXIMATELY ó5 FEET PER TOOO FEET MANIFOLD PRESSURE WILL BE REDUCED T INCH PER IOOO FEET REDUCE INDICi\TED AIR SPEED T MILE PER 1OOO FEET OF ALTITUDE MIXTURE FULL RICH UP TO 5OOO FEEI 2 3 4 @ O â\ (, a FLßPS ta THROTTLE @ tvttXñfnf s 0ì 99fl ¡¡R Sttfo --00- ,fEMP 'lEMP l-caRg AIR AIR @@ CL!MB BEECHCRAFT MODEL Iz ;.ÈùX"î;,,I n,ìfr{,:r:. þñ" I , . ,1,+,r¡.,i**i:s :.' i: . '¡ Wl$ffi -'*'çp-ffi .*r*rrl'.q+r -\**" -{-' _ry i k þ oa FLåPs to THROTTLE @ ITïXTIJRE FCARE ÀlR AR @ o @@ MAXIMUM LONG R,\NGE CRUISING I I *y---'ç#:'F+--' !.#øf - jtùJt;ltii I BEECHCRAFT MODEL TZ '.----'æ.1r' ><ì8 6 /í\ (, a FL4PS ! a THROTTLE @ MIXlURE @@ @ (D ód' s 3 \ ÂIR fEVÞ Âr8 |EMF TAKE.OFF óooo, I l f i I i fi I I I ÍI i f I l f L f I I I L ( I I I I I I 1 I I rli 29 Ozs - U' l¡l2T T oz ia l¡l É f(n 25 af¡J E Àa' ôJ Bzt z 2æ MA¡¡¡6LO PRESSURE AT ITOO R.PM. WÍTH BEST POflER MIXTTJRE ALTITUDE FERFORMANCE hþRSE POT,iJER ÂND MANIFOLD PRESSURE. ENGINE FUGHT GATIBRAT¡ON CIJRÚES AIRPLAF¡E ÍVÐO€L É¡¡EU'¡E UæEI UG43 6 GBz PåW. IflASPJR. pRoPLr'ns-r3-as R-985-AN13 RÊDUOTION GEAR RATIO. NOf{É COtlPFlÉSslOfi¡ RAïIO- 6: I SUPEROHARGEF TYPE_ GEAREO BLOWER GEAR RATIO-IO:I CAREURETION_fI¡A- R98 FUEL_ 9I OCÎANE APPRo\/EO-OATE- MAXlMth/i RÊCO¡MEN0ED FOR CRIJ]S¡NG U' (t, lrl æ & 500 (ó ô: =l¡t l- eoo ci l-<J' t- { soo É t¡l =oô- 200 t¡J CT, É. oI uj roo Y G m TAKE.OFF Af{O ÉÍERGENCY MAXTMUÍ{ 5 MTilUTES nt. coôtTrNUous o roæ m Sooo 4m sæo eooo 70@ aoæ 90æ rqooo npæ ppoo ' PRESSURE ALT¡TUDE IN FEET ECONOTìI|CAL tAXltUr É f,I c 4fo I v, oJ z It-fL =f,(t, z. o() J ¡À¡ -L IE() l¡J È l,l r000 t6 t600 taoo ñæ -600 . soo .45O:'. ..:. - .... :.: -. NOTÊ: THE SP€CIFIC FIÆL COi'SUI'P1K}i¡S SI{OTN ABOÍE ARF INTENDED FoR LEVEL FLIG}iT oPERATIoN AND ARE OETAINAS-E ONLY WTH THE I'SE OF THE ilAIII'AL MIXTURE C¡¡ITROLAI{D WITH NOl TIORE THA'{ 3I IÍ{CHES üERCURY ASSOLUTE Oil Ti{E EXHAJSÍ NOTE: APPLIES TO NÂR.gC¿ ANO I¡AR-98 (SEE T-66A FOR RE€) cl -t- at, lllltllltÍrl CRUISING SPECIFIC FUEL @¡¡SJilPTIOTI ON AN R-9A5-A[- r,-2,- 4,-5,- 68 wasp JR. orrm/E T_662- F PRAIT €. WHIT'IEY AIRCRAFT DATE: 9.4-40 ALTITUDE-FEET I BEECHCRAFT MODEL T7 i ::l ',..;-:.'." OPËRATING CHARTS I l j f i ( i f ; 5 I ( I fI I fL f I I t i I I Í Ì f l I f I