beechcraft Bonanza 36 35 parts & service manual

Bonanza iileechcraft F33A SERIALS CE-613 THRU CE-;I;I1 EXCEPT CE~748 Bonanza Bonanza Bonanza F33C V35B A36 SERIALS CJ1105 SERIALS D8818 SERIALS E-710, THRU CJ-148 THRU P10119 E1763 THRU 6-1240 EXCEPT D-10097 EXCEPT E-llll "0~~ WIRING DIAGRAM MANUAL 14 VOLT ELECTRICAL SYSTEM COPYRIGKT 0 BEECH 1982 P/N 35-590102-78 P/N 35~f~0102-1Bi Reissued: April 28, 1916 Revised: September 3, 1982

PUBLISHED BY COMMERCIAL PUBLICATIONS BEECH AIRCRAFT CORPORATION WICHITA, KANSAS 67201 U. S. A. ~3eechrxaft 8 Mamb´•r ol GAMA GenaralPlviation A ~Py~hson Company Monufacturere Alloti.lion

LIST OF EFFECTIVE REVISIONSI Always destroy superseded pages when you inser: revised pages. Title Page......................................September 3, 1982 Logo Page........................................................ "A" Page. ................... ................... ..,...,......."B1" LOG OF R~1~SIONS Part Number Date Chapters Affected 35-590102-7 June 11, 1976 Original 35-590102-7B April 28, 1978 B Reissue 35-590102-7B1 September 3, 1982 Introduction, Alpha- Numeric Index, 21. NOTE: A list of the etfective pages will be found in the front of each chapter I st Basic publications are assigned a part number which appears on the title page with the date of the issue. Subsequent revisions are identified by the addition of a revision code alter the part number. Al after a part number denotes the first revision to the basic publication. A2 the second. etc. Occasionally. it is necessary to completely reissue and reprint a publication for the purpose of obsoleting a previous issue and outstanding revisions thereto As these replacement reissues are made, the code will also change to the next successive letteiol the alphabet at each issue. For example. B for the first reissue, C for the second reissue. etc. When ordering a handbook, give the basic number. and the reissue code when applicable. if a complete up-to-date publication is desired. Should only revision pages be required. give the basic number and revision code for the particular set of revision pages you desire

BEECHCRAFT BONANZA WIRING DIAGRAM MANUAL INTRODUCTION LIST OF PAGE EFFECTII~N CHAPTER SECTION SUBJECT PAGE DATE INTRODUCTION-EFFECTIVITY 1 September 3, 1982 INTRODUCTION 1 April 28, 1978 Thru 15 April 28, 1978 INTRODUCnON-EFFECTIVm Page 1 September 3, 1982

BEECHCRAFT BONANZA WIRING DIAGRAM MANUAL INTRODUCTION aration between Airframe Systems and the Aircraft Power Plant. NOTE System/Chapter The various groups are broken down into major systems such as Air Conditioning, Electrical Service Publications reissues or revisions are Power, Landing Gear, etc. The systems are arranged not automatically provided to the holders of this more or less alphabetically rather than by precedence or manual. For information on how to obtain reis- importance. They are assigned a number, which becomes sues or revisions applicable to this manual, refer the first element of a standardized numbering system. to BEECHCRAFT Service Instructions No. 0250- Thus, the element "28" of the number 28-00-00 refers to 010, Rev. IV or subsequent revisions. the chapter "Fuel". Everything concerning the fuel system will be covered in this chapter. The BEECHCRAFT Bonanza Wiring Diagram Manual is pre- Sub-System/Section The major systems of an airplane pared in accordance with the GAMA Spec. No 2 (General are broken down into sub-systems. These sub-systems Aviation Manufacturing Association). This Wiring Diagram are identified by the second element of a standard num- Manual is supplemented by the following publications: (1) bering system. The number "40" of the number 28-40-00 The BEECHCRAFT Debonair 33 series and Bonanza 33 is for the indicating portion of the fuel system. series Shop Manual, P/N 33-590011-1C, (2) the BEECHCRAFT Bonanza 35 series Shop Manual, P/N 35- Unit/Subject The individual units within a sub-system 5900968, (3) the BEECHCRAFT Bonanza 36 series Shop may be identified by the third element of the standard Manual, P/N 36-590001-38, (4) the BEECHCRAFT Bonanza numbering system, such as 28-40-01. This number is Parts Catalog, P/N 33-590010-7C, (5) the BEECHCRAFT assigned by the manufacturer and may, or may not, be Bonanza Parts Catalog, P/N 35-590102-58, (6) the used and will vary in usage. BEECHCRAFT Bonanza Parts Catalog, P/N 36-590001-1C. APPLICATION NOTICE Any publication conforming to the GAMA format will use the same basic numbering system. Thus, whether the manual be Beech Aircraft Corporation expressly reserves a BEECHCRAFT Baron 58P Wiririg´• Diagram Manual, or a the right to supersede, cancel and/or declare BEECHCRAFT Bonanza Wiring Diagram Manual, the perso? obsolete any part, part numbers, kits or publica- wishing information concerning the indicating portion of the tion that may be referenced in this manual with- fuel system, would refer to the System/Chapter Tab "28, out prior notice. Fuel." The table of contents in the front of this chapter will provide a list of sub-systems covered in the chapter. CORRESPONDENCE For example: If a question should arise concerning the care of your air- 28-00 General plane, it is important to include the airplane serial number in 28-10 Storage any correspondence. The serial number appears on the (Tanks, cells, necks, model designation placard inboard of the right hand flap on caps, instruments, etc.) the fuselage. 28-20 Distribution (Fuel lines, pumps, valves, ASSIGNMENT OF SUBJECT MA TERIAL controls, etc.) 28-30 Dump The content of this publication is organized at four levels: (If in-flight dumping system is Group, System/Chapter, Sub-System/Section, and Unit/Sub- installed, it would appear here.) ject. 28-40 Indicating (Quantity, temperature, pressure, Group Identified by different colored divider tabs. These etc., does not include engine are primary divisions of the manual that enable broad fuel flow or pressure.) separation of content. Typical of this division is the sep- INTRODUCTION Pagel Apr 28/78

BEECHCRAFT BONANUI WIRING DIAGRAM MANUAL Carrying this example further, by turning to the Table of EQUIPMENTLIST Contents for ChaFjter 28, the following infonation might be found within the list: A listing of the component parts accompanies each wiring diagram to aid maintenance personnel in ordering spares CHAPTER replacements. An "R" appearing in the area between the SECTION reference designators and part number indicates a revision SUBJECT SUBJECT PAGE to the original. FUEL 28 The components are listed in the order of alpha-numeric sequence of the reference designators. Further, the aircraft Indicating 28-40 zone in which each component is installed is provided in the listing. Reference to the zone diagram, page 6 and 7 in the Fuel Quantity 28-40-01 1 thru 3 Introduction, will enable location of the component in the airplane. The material is arranged within the chapter in ascending numerical sequence. The Chapter-System Subject number ALPHABETIGAL INDEX and page number are found at the lower outside corner of each page. An alphabetical index, which may be found in the Introduc- tion, is also provided as an assistance in locating the desired EFFECnVIN circuit. The Alphabetical index provides the chapter and sub- chapter in which a circuit appears. LOG OF EFFECTIVE REVISIONS NUMERICAL INDEX The Log of Effective Revisio~o~s following the title page of the manual lists the revisions currently effective for the manual. All parts listed in the Wiring Diagram Manual are arranged alpha-numerically in the Numerical Index. The number of the LIST OF EFFECTIVE PAGES wiring diagram (diagrams) in which the component is found and the reference designator assigned to the component in The List of Effective Pages following each Chapter Divider- the wiring diagram accompanies each part number in the Tab, lists the issue date of each page that is effective for that Numerical Index. chapter. MICROFI%HE -AEROFIGHE WIRING DIAGRAMS The General Aviation Manufacturers Association has de- To facilitate locating components and tracing ihe circuitry of veloped a specification for microfiche and registered the individual diagrams, each wire is identified by the wire code it name Aerofiche for use by all GAMA Members. This manual beam in the aircraft. The individual circuit components are may be obtained in Aerofiche form from your local identified by a reference designator and name adjacent to BEECHCRAFT Parts and Service Outlet. each item. The diagrams show the terminals, wire numbers, switches, etc., in a manner which will make the operation of WIF~E CODES each component easily understandable. The circuits are shown consistent with the position of switches and conditions The wire codes used in the BEECHCRAFT Bonanza closely noted on the diagrams. Symbols used in the wiring diagrams follow the military numbering system. Each wire and cable appear in the introduction of this manual. are identified by a combination of numbers and letters imprinted on the wire and cable as illustrated in Figure i. Each OP;TIONAL EQUIPMENT wire or cable is identified within 3 inches of each junction. No code is required for short wires or cables less than 3 inches in This manual does not in all cases differentiate between op- length. A nonmetalic sleeve carrying identification will appear tional and standard equipment. In order to facilitate the instal- on wires where imprinted codes cannot be affixed. lation of certain wire harnesses used to connect optional equipment, these harnesses will be installed in all airplanes. Circuit function letters indicate a relationship to a particular Wires will be dead ended in airplanes that do not require the system (noted in the list of circuit function designations). Wire equipment. numbers are provided to differentiate between wires in a circuit. INTRODUCTION Page 2 Apr 28n8

BEECHCRAFT BONANZA WIRING DIAGRAM MANUAL A wire segment is a conductor between two terminals or J Ignition connections. Alphabetical sequency is usually followed. Wire K Engine Control; starter, prop pitch, prop synchronizer, segment A indicates the power source, B next segment, etc. etc. L Lighting The wire size number is used to identify the size of the wire or M Miscellaneous electric; windshield wiper, etc. cable. P DC power Q Fuel and oil; fuel valves, fuel pump motors, throttle A suffix to the wire identification code (N) identifies any wire control, oil pumps, etc. or cable that completes the circuit to ground network. R Radio; RC-radio command, RM-marker beacon, etc. S Radar; SA-altimeter, SS-search, etc. Phase letter "A", "B" or "C" used as a suffix identifies three- T Special electronics; TK-telemetry, TR-receivers, etc. phase wiring in ac systems. U Miscellaneous electronics (other than R, S or T) V DC power for AC systems The phase letter "V" is used as a suffix identifying an un- W Warning andemergency grounded wire or cable in a single phase system. X AC power Y Armaments special systems For thermocouple wire, the following suffixes are applicable: CHROM Chromel CONST Constantan ALME Alumel COP Copper IRON Iron ALUM Aluminum ~P 52 CIRCUIT FUNCTION LETTE RS A List of Circuit Function Designations Follows: WIRE NUMBER A Armaments WIRE SEGMENT LETTE R B Photographic WIRESIZE (A.W.G.) C Control surfaces; automatic pilot D Instruments other than flight or engine instrument; am- SUFFIX meter, landing gear position, free air temperature, ca- 5TD´•369´•24 bin pressure, etc. E Engine instrument; fuel flow, fuel quantity, tachometer, synchroscope, etc. F Flight Instrument G Landing gear; actuator, retraction, warning, down lock, etc. Wire Codes H Heating; ventilating, deicing Figure 1. INTRODUCTION Page 3 Apr 28/78

BEECHCRAFT BONANZA WIRING DIAGRAM MANUAL ELECTRICAL SYMBOLS AIRCRAFT LOCATION SYMBOLS ADJUSTABILITY BATTERIES BUS QQ O~ww QQ ~ -111~ GENERAL GENERAL MULTICELL LEFT RIGHT LEFT RIGHT LEFT RIGHT FIREWALL WHEEL WELL FIRE SEAL CABLES AND CONDUCTORS ~ r-r if SHIELDED conxlAL SINGLE SHIELDED SHIELDED TWISTED PAIR TWISTED TWISTED CABLE GROUPING OF LEADS CONDUCTOR TWISTED TWISTED TRIPLE OUAD PAIR TRIPLE CAPACITOR CIRCUIT BREAKERS CONNECTORS GENERAL ba a~b 6~/5 ~ ~ ~ cB~~~ BASIC PUSH PUSH-PULL SWITCH BREAKER BREAKER BREAKER RECEPTACLE PLUG MATED PLUG AND RECEPTACLE DIODE FUSE GROUNDS ´•-L~nI~r tL ~-~F GENERAL ZENE~ ZENER G GROUND OR GROUND TO UNIDIRECTIONAL BIDIRECTIONAL SCR CIRCUIT CHASSIS RETUIN (WITH TERMINAL) SHIELD GROUNDED TO 8:TKSHeLL C~,r~, iWMINAL) HEATER ELEMENT HORN IGNITOR LAMPS -~n~G I o m T~c~ ^^^ ’ Ilcr’ SIGNAL LIGHT INUINDESCENT COMMUNICATION FLOURESCENT ’(LETTER TO SWITCH BOARD TYPE DENOTE COLOR) INDICATING LAMP METER MISC I MOTOR POTENTIOMETW PIN JACK POLARITY O eB O~----( FURN (LETTER TO DENOTE WHAT TYPE OF METER WITH POSITIVE NEGATIVE SUCH AS "I" FOR INDICATING METER) EOUIP TERMINAL BOARD RELAYCOIL RESISTORS SPLICES r~T1 RHEOSTAT tcI~-~3~ TESTPOINT TnERMOtOUPLE ´•--´•´•´•‘4~~* rl ~ tNfi ~ t-f--~ WITHITERMINALS GENERAL GENERAL SHOWN I I ADJUSTABLE CONTACT) I DISCONNECT WITH 4 TERMINALS SHOWN AND Z BUSSED TOGETHER TRANSFORMERS TRANSISTORS --FC~-- ’U~~"’ ’"’"’ 3f ti ~fT 1~ GENERAL (TRANSDUCER) T Tl~elNII~TORP*III PNP NPN (DARLINGTON) 311~ TR[sYL II(MINI COll~ OTHIITI~N RIV\YI SINGLE PHASE NON SATURATING -----~X~-- TYn? rrm 3-WINDING WITH CORE GENERAL WINDINGS. INDUCTOR REACTOR OR CHOKE INTRODUCTION Page4 Apr 28n8

BEECHCRAFT BONANZA WIRING DIAGRAM MANUAL ELECTRICAL SYMBOLS CONTINUED: BASIC CONTACT SWITCH ASSEMBLIES PUSH BUTTON (MOMENTARY OR SPRING RETURN) Oa I o o ~Lo ~D o o CIRCUIT CIRCUIT CLOSED OPEN TRANSFER CLOSING OPENING TWO-CIRCUIT CONTACT CONTACT (MAKE) (BREAK) NON LOCKING (MOMENTARY OR SPRING RETURN) COMBINATION LOCKING AND NON LOCKING bLT i~O--T( ~Lo ~P ~ ,Pi 4 L-r CIRCUIT CIRCUIT CIRCUIT CLOSING OPENING OPENING TWO CIRCUIT TRANSFER (MAKE) OR CLOSING (BREAK) (MAKE OR BREAK) PRESSURE OR VACUUM ACTUATED TEMPERATURE ACTUATED 4T´•´•~ ~ oR CLOSES ON RISING OPENS ON RISING OPENS ON RISING CLOSES ON RISING PRESSURE PRESSURE TEMPERATURE TEMPERATURE LIMIT SWITCH (DIRECTLY ACTIVATED SPRING RETURNED) THERMAL SWITCHES ~ "o" ~ " OPEN NORMALLY NORMALLY NORMALLY NORMALLY OPEN OPEN CLOITD CLOlsD Noahu\lLY OPEN HELD CLOSED HELD OPEN (wlTH INTERNAL HEATER SHOWN) NORMALLY CLOSED SELECTOR OR MULTI POSITION SWITCH EXAMPLE OF ON- ON-ON SWITCH ACUTATION: ~P o %.. O TOGGLE IN "DOWN" POSITION (NOTE: ANY NO. OF TRANSMISSION PATHS Me,Y BCSHOWN) SWITCHES WITH TIME DELAY FEATVRE TOGGLE IN kp "CENTER" POSITION (NOTE: ALL APPLICABLE DIAGRAMS SHOW "r’ g" "r’ S" ON-ON-ON SWITCH IN THIS POSITION) OPEN CLOSED OPEN CLOSED I TOGGLEIN TIME- DTV\Y nMI-DEUY TIME-DLUY TIML-DPPIY DlP "UP* POSITION CLOSING OPENING OPENING CLOSING (NOTE: POINI OF ARROW INDICATES DIRECTION OF SWITCH OPERATION tN WHICH CONTACT ACTION IS DELAYED). INTRODUCTION Page 5 Apr 28/78

BEECHCRAFT BONANZA WIRING DIAGRAM MANUAL 330 253 310 231(232)7 ~-240 ~820 320’1 /~ / ~340 221 (222) -- 41 / I 370 I I- -I I ’ ’---I 160 140 280 270 --~ ~150 33~607-18 () indicates Right Side 100 BELOW FLOOR 300 AFT FUSELAGE AND EMPENNAGE 140 Firewall to Main Soar 310 Aft Fuselage 150 Main Soar to Rear Soar 320 Dorsal Fin (Aircraft with Aft of Rear Soar Conventional Tail) 330 Vertical Stabilizer (Air- 200 FORWARD FUSELAGE craft with Conventional Tail) 340 Rudder (Aircraft with 221 (222) Firewall (Attached to or Conventional Tail) Accessible from Forward Side) 370 Tail Cone 231(232) Firewall to Instrument Panel 410 ENGINE COMPARTMENT 240 Instrument Panel and Subpanel 800 DOORS 251 (252) Cabin (Floor Line to Headliner) 820 Cabin Entry Door 253 Cabin Headliner Area 830 Baggage or Cargo Door 270 Main Spar Carry-Through Structure INTRODUCTION Page 6 Apr 28n8

beechcraft Bonanza 36 35 parts & service manual

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