~)eechcraft - AeroElectric

issue and all outstanding revisions thereto. As these replacement reissues are made, the code will also change to the next successive letter of the alphabet at each issue. For example, B for the first reissue, C for the second reissue, etc. When ordering a manual, 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. Beec~aft BONANZA SERIES SHOP MANUAL LIST OF EFFECTIVE PAGES Always destroy superseded pages when you insert revised pages A Page 819 Mar 22, 1996 2-22A and 2-228 89 Feb 10, 1977 8 Page 819 Mar 22, 1996 2-23 89 Feb 10, 1977 C Page 819 Mar 22, 1996 2-24 814 Sep 27, 1979 D Page 819 Mar 22, 1996 2-25 84/18 Sep, 1971 Record of 2-26 814 Sep 27, 1979 Revision 2-27 84/18 Sep, 1971 Record of 2-28 B11 May 12, 1978 Temporaty 3-1 Original Revision 3-2 thru 3-28 84"11 Dec, 1969 1-1 816 Jan 31, 1986 3-2C 817 Aug 28, 1987 1-2 thru 1-4 86 Nov 29, 1974 3-3 83 Oct 22, 1965 1-5 thru 1-108 817 Aug 28, 1987 3-4 thru 3-6K 817 Aug 28, 1987 1-11 817 Aug 28, 1987 3-7 811 May 12, 1978 1-12 thru 1-128 813 Mar 15, 1979 3-8 thru 3-10A 817 Aug 28, 1987 1-13 813 Mar 15, 1979 3-11 817 Aug 28, 1987 1-14 and 1-14A 811 May 12, 1978 3-12 87 Jun 5, 1975 1-148 814 Sep 27, 1979 3-12A thru 3-12C 819 Mar 22, 1996 1-15 814 Sep 27, 1979 3-13 819 Mar 22, 1996 1-16 and 1-17 86 Nov 29, 1974 3-14 thru 3-14C 817 Aug 28, 1987 2-1 Original 3-148 86 Nov 29, 1974 2-2 89 Feb 10, 1977 3-148 thru 3-14G 817 Aug 28, 1987 2-3 82 Jan 15, 1964 3-15 84/20 Nov, 1972 2-4 and 2-5 Original 3-16 84 Feb 11, 1966 2-6 83 Oct 22, 1965 3-16A and 3-168 86 Nov 29, 1974 2-7 81 Oct 27, 1961 3-1 6C 84/20 Nov, 1972 2-8 83 Oct 22, 1965 3-17 thru 3-18C 813 Mar 15, 1979 2-9 81 Oct 27, 1961 3-19 813 Mar 15, 1979 2-10 and 2-11 Original 3-20 82 Jan 15, 1964 2-12 815 Feb 3, 1984 3-21 thru 3-22A 86 Nov 29, 1974 2-13 816 Jan 31, 1986 3-23 84/18 Sep, 1971 2-14 86 Nov 29, 1974 3-24 Original 2-15 819 Mar 22, 1996 3-25 818 May 18, 1989 2-16 819 Mar 22, 1996 3-26 and 3-26A 86 Nov 29, 1974 2-17 84/17 Jun, 1971 3-27 Original 2-18 and 2-19 84 Feb 11, 1966 3-28 and 3-28A 84/17 June, 1971 2-20 and 2-20A 86 Nov 29, 1974 3-288 84/18 Sep, 1971 2-208 thru 2-201 817 Aug 28, 1987 3-28(= 811 May 12, 1978 2-21 and 2-22 811 May 12, 1978 819 Qeed~craft BONANZA SERIES SHOP MANUAL LIST OF EFFECTIVE PAGES Always destroy superseded pages when you insert revised pages 3-29 thru 3-30A 811 May 12, 1978 5-13 84 Feb 11, 1966 3-308 thru 3-30F 89 Feb 10, 1977 5-14 83 Oct 22, 1965 3-308 thru 3-30K 817 Aug 28, 1987 5-15 84*11 Dec, 1969 3-30L thru 3-308 89 Feb 10, 1977 5-16 thru 5-18 86 Nov 29, 1974 3-31 84116 Mar, 1971 6-1 811 May 12, 1978 3-32 811 May 12, 1978 6-2 84"1 2 Jan, 1970 3-32A and 3-328 86 Nov 29, 1974 6-2A 88 Oct 17, 1975 3-33 and 3-34 84117 Jun, 1971 6-28 85 Nov 1, 1973 3-34A thru 3-34F 813 Mar 15, 1979 6-3 Original 3-35 thru 3-36A 814 Sep 27, 1979 6-4 81 Oct 27, 1961 3-368 thru 3-36H 86 Nov 29, 1974 6-5 thru 6-7 Original 3-37 811 May 12, 1978 6-8 and 6-3A 85 Nov 1, 1973 3-38 82 Jan 15, 1964 6-9 81 Oct 27, 1961 3-39 thru 3-408 811 May 12, 1973 6-10 and 6-11 Original 3-41 thru 3-428 86 Nov 29, 1974 6-12 81 Oct 27, 1961 3-43 thru 351 82 Jan 15, 1964 6-13 thru 6-16 Original 3-52 thru 3-54 84 Feb 11, 1966 6-17 and 6-18 81 Oct 27, 1961 3-55 thru 3-61 86 Nov 29, 1974 6-19 Original 4-1 Original 6-20 81 Oct 27, 1961 4-2 thru 4-4S 815 Feb 3, 1984 6-21 thru 6-24 Original 4-5 81 Oct 27, 1961 6-25 81 Oct 27, 1961 4-6 thru 4-68 819 Mar 22, 1996 6-26 and 6-27 Original 4-7 82 Jan 15, 1964 6-28 thru 6-31 B1 Oct 27, 1961 4-8 thru 4-88 84/19 Mar, 1972 6-32 and 6-33 88 Oct 17, 1975 4-9 89 Feb 10, 1977 6-34 and 6-35 Original 4-10 thru 4-10H 819 Mar 22, 1996 6-36 thru 6-39 81 Oct 27, 1961 4-11 and 4-12 819 Mar 22, 1996 6-40 Original 4-13 and 4-14 813 Mar 15, 1979 6-41 thru 6-47 B1 Oct 27, 1961 4-15 and 4-16 84 Feb 11, 1966 6-48 thru 6-52A 84*12 Jan, 1970 4-17 thru 4-19 86 Nov 29, 1974 6-53 84"1 2 Jan, 1970 5-1 thru 5-4 Original 6-54 84118 Sep, 1971 5-5 84*11 Dec, 1969 6-54A and 6-548 84/21 Dec, 1972 5-6 Original 6-54(; and 6-548 810 Mar 7, 1977 5-7 82 Jan 15, 1964 6-55 and 6-56 84*12 Jan, 1970 5-8 and 5-8A 84*11 Dec, 1969 6-56A and 6-568 84/21 Dec, 1972 5-9 and 5-10 84*11 Dec, 1969 6-57 810 Mar 7, 1977 5-11 84 Feb 11, 1966 658 and 6-59 84"1 2 Jan, 1970 5-12 86 Nov 29, 1974 6-60 84/21 Dec, 1972 819 QeechcraR BONANZA SERIES SHOP MANUAL LIST OF EFFECTIVE PAGES Always destroy superseded pages when you insert revised pages 6-60A B10 Mar 7, 1977 6-868 and 6-86(= B10 Mar 7, 1977 6-61 thru 6-63 B10 Mar 7, 1977 6-87 84*12 Jan, 1970 6-64 84’12 Jan, 1970 6-88 B10 Mar 7, 1977 6-64A and 6-648 84/21 Dec, 1972 6-88A 84/18 Sep, 1971 6-64(= 85 Nov 1, 1973 6-89 84/21 Dec, 1972 6-641) 814 Sep 27, 1979 6-90 84/18 Sep, 1971 6-648 85 Nov 1, 1973 6-90A 84/21 Dec, 1972 6-65 814 Sep 27, 1979 6-908 B10 Mar 7, 1977 6-66 B10 Mar 7, 1977 6-90C thru 6-90F 84/21 Dec, 1972 6-67 84"12 Jan, 1970 6-91 and 6-92 84"12 Jan, 1970 6-68 85 Nov 1, 1973 6-92A 84/18 Sep, 1971 6-68A B10 Mar 7, 1977 6-93 B10 Mar 7, 1977 6-69 B10 Mar 7, 1977 6-94 thru 6-96 84"12 Jan, 1970 6-70 84´•12 Jan, 1970 6-96A 84/18 Sep, 1971 6-71 and 6-72 B10 Mar 7, 1977 6-968 85 Nov 1,1973 6-73 B4*~2 Jan, 1970 6-97 B10 Mar 7, 1977 6-74 84/18 Sep, 1971 6-98 and 6-98A 84/21 Dec, 1972 6-74A 88 Oct 17, 1975 8-988 85 Nov 1, 1793 6-748 B10 Mar 7, 1977 6-98(= and 6-988 B10 Mar 7, 1977 6-75 84’12 Jan, 1970 6-76 84/18 Sep, 1971 6-988 88 Oct 17, 1975 6-76A 88 Oct 17, 1975 6-99 B10 Mar 7, 1977 6-768 B10 Mar 7, 1977 6-100 88 Oct 17, 1975 6-77 88 Oct 17, 1975 6-100A B10 Mar 7, 1977 6-78 and 6-78A 84/18 Sep, 1971 6-1008 85 Nov 1, 1973 6-788 B10 Mar 7, 1977 6-100C 810 Mar 7, 1977 6-78C 88 Oct 17. 1975 6-101 thru B10 Mar 7, 1977 6-79 810 Mar 7, 1977 6-104A 6-80 84/21 Dec, 1972 6-105 thru 6-107 B10 Mar 7, 1977 6-80A B10 Mar 7, 1977 7-1 thru 7-19 819 Mar 22, 1996 6-81 and 6-82 84*12 Jan, 1970 8-1 B1S Feb 3, 1984 6-82A and 6-828 84/18 Sep 18, 1971 8-2 thru 8-28 819 Mar 22, 1996 6-83 and 6-84 84/18 Sep 18, 1971 8-3 819 Mar 22, 1996 6-85 84/21 Dec, 1972 8-4 814 Sep 27, 1979 6-86 and 6-86A 88 Oct 17, 1975 8-5 819 Mar 22, 1996 819 I SECTION 1 Introduction SECTION I THE BONANZA SHOP MANUAL The Shop Manual is directed toward helping the experi- out prior notice. enced mechanic in his day-to-day work in the shop. Simple, repetitive maintenance and removal procedures are left out; at the same time we have tried to add key points of special- NOTE ized procedures so organized that reading through many pages of descriptive text is not required to find them. We Service publication reissues or revisions are not think the results are a shop manual that the mechanic can automatically provided to the holders of this use every day. It is small in size but large in scope and manual. For information on how to obtain a revi- usability. sion service applicable to this manual, refer to the latest revision of BEECHCRAFT Service Bul- IAs distinguished from the Bonanza Owner’s Manual which letin No. 2001. contains flight procedures, servicing information, and the minor maintenance that the owner needs to know, the Bo- nanza Shop Manual furnishes the experienced mechanic WARNING with detailed instruction and information peculiar to the BEECHCRAFT Bonanza. Illustrations, diagrams, and tables Use only genuine BEECHCRAFT or are used to present complex information in a concise form. BEECHCRAFT approved parts obtained from Text is kept brief while covering important points in mainte- BEECHCRAFT approved sources, in connec- nance and overhaul, tion with the maintenance and repair of Beech airplanes. The Bonanza Shop Manual will grow as new information be- comes available. Revisions will be issued whenever needed Genuine BEECHCRAFT parts are produced and inspected to keep information current and to add more of the type in- under rigorous procedures to ensure airworthiness and suit- formation included in the original issue. The wiring diagrams ability for use in Beech airplane applications. Parts pur- for those airplane serials prior to D-9818, are contained chased from sources other than BEECHCRAFT, even within Section 6 of this Shop Manual. though outwardly identical In appearance, may not have had the required tests and inspections performed, may be differ- Refer to the BEECHCRAFT Bonanza Wiring Diagram Manu- ent in fabrication techniques and materials, and may be al P/N 35-590102-7 for the wiring diagrams pertaining to the dangerous when installed in an airplane. Bonanza Model V35B, airplane serials D-9818 through D-10119 except D-10097. Salvaged airplane parts, reworked parts obtained from non- BEECHCRAFT approved sources, or parts, components, or For serials D-10097, D-10120 and after refer to structural assemblies, the service history of which is un- BEECHCRAFT Bonanza Wiring Diagram Manual P/N known or cannot be authenticated, may have been subject- 35-590102-9. ed to unacceptable stresses or temperatures or have other hidden damage, not discernible through routine visual or CORRESPONDENCE usual nondestructive testing techniques. This may render the part, component or structural assembly, even though If a question should arise concerning the care of your air- originally manufactured by BEECHCRAFT, unsuitable and plane, it is important to include the airplane serial number unsafe for airplane use. with your inquiry. The serial number is stamped on the model designation plate, located in one of the following lo- BEECHCRAFT expressly disclaims any responsibility for cations: on the fuel selector cover, on the belly of the air- malfunctions, failures, damage or injury caused by use of plane forward of the differential mechanism inspection non-BEECHCRAFT approved parts. cover or on the fuselage inboard of the RH flap. NOTE NOTICE It shall be the responsibility of the ownerl Beech Aircraft Corporation expressly reserves operator to ensure that the latest revision of the right to supersede, cancel and/or declare publications referenced in this handbook are obsolete any part, part numbers, kits or publica- utilized during operation, servicing, and mainte- tion that may be referenced in this manual with- nance of the airplane. 1-1 B16 BEECHCRAFT BONANZA 35 SERIES SHOP MANUAL TABLE OF CONTENTS SECTION PAGE INTRODUCT1ON....... .............~~~~~~ ~ . . . . . . . ~ . . ~ ~ . ~ ~ ~ 1,1 1I GENER.-\L INFORF~I.I\TION ...............~~~~ . ~ ~ . ~ ~ . . . . . ~ . . ~ 2~1 III SYSTEMS DESCRIPTION XND M~INTEN~NCE .. ~ ~ . ~ . . ~~ ~~~ ~..3-1 IV MAJOR DISXSSEMBLY ..................~ ~ . . . . . ~ . ~ ~ . . . . ~ . ~ ~ . 4_1 V ~1.-\10R ~1.-\INTENANCE AND OVERHAUL .......... ~ . ~ . ~ ~ ~ . ~ ~5-1 VI ELECTRICAL WIRING DIAGRAMS .................~ . ~ . ~ ~ . ~ ~ . . 6-1 vil PERIODIC INSPECTION GUIDE ........._ .....~ ~ . . . . . ~ ~ . . ~ 7~1 VIII OVERH.~UL.-\ND REPLXCE~IENT SCHEDULE .......... ~ . . . . . ~ 8-1 817 1-3 ALPHABETICAL INDEX A A Access Openings Air Conditioning System, Refrigerative (Cont’d) Fuselage........ ......... ........., ........., ........., Illus. 2-4 Condenser Wing.......................................................... Illus, 2-5 Control Rigging........... .................................. 3-30C Actuator Electric Installation....,... .......................................... 3-30C Trim Tab ................................................. Illus. 3-6G Removal................ ..................... .........,, 3-3013 Actuator, Flap......... ......................................I1lus. 5-13 Evaporator Assembly ................................ .................... .....5-12 Filter Replacement ................ ......... ...............3-30D Disassembly.............................. ........................ 5-12 Installation....... ...................... ......... .........,..3-30D Overhaul....... .................... ........................... ....5-12 Removal............. .................. ......... .........,.3-30D Removal and Installation.. ................................... 4-6A Functional Test........ ........................................ 3-30B Actuator, Landing Gear........... ........................Illus. 5-15 Leak Detection ......................... .................. .....3-30B Overhaul .......................................................... 5-14 Maintenance .............................. ................... ..3-30A Removing and Installing........ ....... .........,.,,, .......4-5 Precautionary Measures .........,,, .........,..,.. ....3-30B Adjustment and Troubleshooting............................................... 3-30F Test Procedure ....,....,..,.., ....... ..................... .3-36B Ventilation Blower .........,.., .........,,,,, ..........3-30D Adjustment Installation............. ..................... .................3-3OD Brake Master Cylinder Removal........... ........ .........,,. .........,,,, .3-30D Linkage......... .........,..,., ........., .........,.., 3-26 Air Filters, Gyro instrument .........,...,.. .........,..., 3J05 Cabin Entrance Door .........,,, .........,, ........3-32B Airplane Three Dimensional View........ .......................2-2 Carburetor Idler......... ........................ .........,..,, 3-34 Alternator ................... ................... ....3-34F, Illus. 3-20 Compressor Belt .........,,,,. ...... .........,,. .2-23, 3-30D Installation..................... .............. ...................... 3-34F Engine Fuel Pump ............................................3-14A Removal...................................... ...................... 3-34F Flap Limit Switch........... ...... .........,, 3-18, Illus. 3-19 New Alternator Preparation............. ......................3-34F Landing Gear Troubleshooting...............................................3-40D Microswitch ........................... ..........,.. ........3-18A Approved Engine Oils ..........................................2-20A Landing Gear Position Arm, Control Column Light ............................................................ 3-22 Instailation......... ... .........,..,, . ...................... ....3-2 Landing Gear Pressure Removal.................................. ...................... .....3-2 Switch ................................... ..................... 3-18B Assembly Nose Wheel Travel Gerdes, Master Cylinder ...................... . 5-17, IUus. 5-18 Stop ........., ............, ................ ................ 3-22A Main Gear Strut ................................................ 5-8A Stall Warning Switch..................... ....... 3-28, Illus. 3-20 Nose Gear Shock Strut ............... ......................... 5-14 Static Ground Cable..................... ....................... 2-23 Paramount, Master Cylinder .........,.,., 5-16, Illus. 5-18 Suction Relief Valve ............... ..........................3-30G Assist Step........................................................... 3-25 Voltage Regulator.................. ................. 3-34C, 3-34D Adjustment......... ........................................ ...... 3-25 Aileron Autopilot Balancing ............................ .........,3-11.4, Illus. 3-12 BEECHCRAFT New-Matic ............ .........,.,.... 3-301( Control System ............................ ................ Illus. 3-3 Illus. 3-30K, 3-30L, 3-30M Control Trimmer......... .........,.,.. .........................3-5 Troubleshooting Guide ......................................3-30N Rigging CD-I through D-1500) ..................................3-2 Rigging @-1501 and after) ......................................3-2 Tabs ..................................................................3-5 B Air Conditioning System, Evaporative........ .........,, 3-29 Balancing WickJig ....................................................mus. 3-29 Aileron.......................................... 3-10A, Illus. 3-12 Air Conditioning System, Refrigerative...................... 3-30 Control Surfaces ............................................. 3-10A Illus. 3-30C, 3-30E ElevatortRudder ............................. 3-12A, Illus. 3-13 Charging......................................................... 2-22B Battery............................................. 2-20H, Illus. 3-20 Compressor Beach Brake Installlp.tion ..................................................3-30D Disassembly.............. ..........................................4-8 Oil Level ..................................................... 2-22B Lining Wear ...................................................... 3-26 Rtmoval......................................................3-30D Rcassembly,........................................................4-8 Compressor Belt Replacement .......................................................4-8 Installation............................................. ......3-30B BEECHCRAFT Removal...................................................... 3-3013 New-Matic Autopilot .......,..,.,, ............., ........3-30X. Tension................................................2-23. 3-30B Illus. 3-30K, 3-30L, 3-30M 1-5 B1P ALPHABETICAL INDU( B C Belt Adjustment Cabin Door´•(Cont’d) Compressor .........................´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´• 2-23, 3-30D Lock.............................................................. 3-32B Generator .Illus. 3-20 Teleflex Cable, Removing and Bladder Type Fuel Cell Installing .......................................... ............. 4´•10 Removal and Installation................................... 3-14E Cabin Trim, Cleaning ............................................. 2-22 Repair............................´•´•´•.´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´• 3-14F Cable Blower, Ventilation . ...................................´•´•´•´•´•´•´•´•3-30D Adjustment. Static Ground............. ............´•...´•..... 3-23 Boot Repair, Electric Installation, New Tab......................................... 3-6K Propeller Deicer................................................. 5-16 Tension, Temperature Effect on .................... Illus. 3-2C Brake System .......................................´•´•´•´•´•´•´•´• ´•Illus. 3-27 Capacities, Fuel Cell .................................... ........ ?-20B Bleeding, Dual Brake System................................ 3-25 Carburetor Idle Adjustment..................................... 3-34 Gravity Bleeding ............................................:... 3-25 Care and Repair of Fuel Cells................................. 3-14F Pressure Bleeding......................................´•...´•´•´•´•´• 3-2~ Inside Patch ....................................................3-14G Determining Goodyear Brake Outside Patch ........................................ .......... 3-14F Lining Wear ...............................................´•´•´•´• 3-26 Changes, Nose Gear Improvement.............. ............3-22A Firestone Brake Adjustment ........... ................. ..... 3-26 Chart Electrical Utilization Load............ ............... 3-36B Firestone Brake Overhaul ................................... 4-8A Circuit Breaker Panels................... ................. Illus. 3-20 Goodyear Brake Adjustment ................................ 3-26 Cleaning Goodyear Brake Lining, Removal Engine ...........................................................2-22A and Replacement Exterior .................................´•....´•´•´•...´•´•.´•´•´•´•´•´•´•´•´•´•´•´• 2-22 (One Pressure Cylinder Type) ........................ 4-6A Interior, Cabin Trim................... ............. ............2-22 ~wo Pressure Cylinder Type)...........................4-7 Oil Separator Screen .........................................3-30G Goodyear Brake Unit, Disassembly Oil Tank and Cooler (One Pressure Cylinder Type) ........... ............. 4-68 Prior to D-4866........................... ................ ..... 3-15 Goodyear Brake Unit, Disassembly Rubber Seals .................... ................ ................. 2-22 Repair and Reassembly of Suction Relief Valve Screen ............ ........... ........3-30G (Two Pressure Cylinder Type)....................... ....4-7 Windshield and Windows .............. ........... ............ 2-22 Master Cylinder ............................´•´•´•´•´•´• 3-26, Plus. 3-27 Clearing Static Lines ............................. ................. 3-28 Linkage Adjustment ....................................´•´•´•´• 3-26 Clutch, Magnetic Overhaul .................´•.´•´•´•´•´•´•´•´•´•´•´•-´•´• ´•´•´•´•´•´•´•´•´•´•´•´• ´•´•´•´•´•´•´•´•´•´•5-16 Installation................................ ..........................3-7 Removal and Installation.................................3-26A Removal......................................................... 3-6K Parking Brake.......................................´• ´•´•´•´•´•´•´•´•´•´•´•´• 2-19 Compressor, Air Conditioner Parking Brake Valve .......................... 3-26A, IUus. 3-27 Belt Tension....................... ......................2-23. 3-30D Servicing ............ .....................´•´•´•´•´•´•´•´•´•´•´•´• ´•´•´•´•´•´•´•´•´•´•´•2-20C Installation........................................ ..............3-30D Shuttle Valve....................................... 3-26A, Illus. 3-27 Oil Level .................................... .................. ..2-228 Breaker Point Adjustment, Removal.........................................................3-30D Magneto ..........................................´•´•´•´•´•´•´•´•´•´• ´•´•´•´•´•3-34A Condenser, Air Conditioner Brush Control Rigging.......................................´•´•..´•´• ´•´•´•3-30D Block Resistance Installation........................... ........... ................3-30D Check, Propeller .............................. 3-57, Illus. 3-57 Removal............................. . .........................´•.3-30D Generator, Minimum Length ........... ..............Illus. 3-20 Continuity Test, Propeller Generator, Replacement of............. ............ .......... 3-35 Deicer ..........................................´•´•..........´•.´•´•´•´•´•´•´•´•´•´•.´•´•´•´•´•´• 3-57 Replacement, Propeller Control Deicer.......................................´•...´• 3-55, Illus. 3-55 Column............................................................. Illus. 3-2B Starter, Minimum Length......................... .....Illus. 3-20 Arm Installation ...................................................... 3-2 Wear Limits Electrical Arm Removal ........................................................... 3-2 Trim Tab Actuator......................................´•´•´•´•´•´•´•3-7 Chain Rigging .......................................................... 3-2 Bulb Replacement Guide................. .................´•´•.´• 2-28 Single.........................................................´•´•´•´•´•´•´•´•´•´•´•´•´•´•´• 3-2 Bulkhead Inspection ................................´•´•´•´•´•´•´•´•´•´•´•´•3-32A Flight..............................................................´•´•..´•´•´•´•´•´•´•´•´•´• 3-2 Bullock Unit........................................´•´•´•´•´•´•´•´•´•´•´•´•´•´•´• 3-308 LOck ....................................´•...´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´• 2-19 Surfaces, Balancing................................................ 3-10A System Aileron............................................................´•Illus. 3-3 C Elevator .....................................................´•´•´•´•´•´• Illus. 3-4 Inspection ....................................................´•´•´•´• ´•´•´•´•´•´•´•´•´• 3-2 Cabin Door Rigging ......................................´•´•´•´•..........´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´• 3-2 Adjustment ................................. .........´•´•´•´•´•´•´•´•´•´•´• 3-328 Illus. 3-3, 3-4, 3-8 1´•6 817 ALPHABETICAL INDEX C E Control (Cont’d) Elevator System (Cont’d) Balancing ........._._.,.. .....3-12A, Illus. 3-13 Rudder .................~~ ~ ~ ~~~~~~~~~~~lllus. 3-8 Control System .........,._._.. ......... Illus. 3-4 Controller, Turbocharger ......3-368 Illus. 3-36C, 3-36D Rigging (D-l through D-2680) ................... .3-5 Converter Troubleshooting, Strobe Light ..........3-30S Rigging (D-2681 through D-5725) ...............3-6A Correcting End Play in Main Gear Fitting ........3-22A Rigging (D-5726 and after) ................... ..3-6C Cowl Flap Rigging ................~~~~~~~~~~~~3,16C Tab Hinges Inspection ................... .....3-6J Forward Cowl Flap Rigging .................~..3-17 Tab Indicator Rigging ................... .....,3-61 Cylinder Retesting, Oxygen ................~ ~ ~ ~ ~ ~2-23 Tab Inspection ................... ........._3-68 Tab Rigging ´• ................... ........._.._3-68 D Tab Rigging to Correct for Yaw ........._., 3-6J Trim Tab Installation ........._._._.. ...lllus. 3-68 Deicer Inspection Procedure, Trim Tab Actuator Removal ........._._._.. .3-6H Electric Propeller ........., ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 7,1 Trim Tab Actuator Installation ..............._ .3-6H Deicer Resistance Check, Propeller ........._._., 3-57 Emergency Locator Transmitter ........._._.. 3-32A Deicer Timer Check, Propeller ..................~ .3-56 Empennage, Removal and Installation ............4-108 Deicing, Electric Propeller ..................~ ~ ~ ~ ~ ~3-55 Engine Dimensions, Aircraft ................... ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~2-2 Approved Alternate ................... .......4-108 Disassembly Change Requirements ................... .....4-13 Beech Brakes. ................~~~ ~~~~~~~~~~~...4-8 Cleaning ................... .........._., ..2-22A Gerdes, Master Cylinder ............5-16, Illus. 5-18 Fuel Pump Adjustment ... ...................3-14A Main Gear Strut ..............5-5, Illus. 5-6, 5-7, 5-8 Instruments ................... .........._._ 3-30J Nose Gear Strut .................. 5-4, Illus. 5-2, 5-3 Mounts ................................,.....4-13 Paramount, Master Cylinder ..........5-16, Illus. 5-18 Oils ......,............ ................... ..2-20A Shimmy Dampener .................. 5-8A, Illus. 5-9 Removal and Installation ................... ...4-108 Door Adjustment, Cabin Entrance. .............. .3-328 Starting ................... .................. .2-18 Door Adjustment, Landing Gear ......3-188, Illus. 3-23 Stopping ................................,,..2-lg Door Lock, Cabin ................... ...~ ~ ~ ~ ~ ~ ~ ~3-328 Turbocharger ................... ...lllus. 4-11, 4-12 Drop-Off Check, Magneto ................~ ~ ~ ~ ~ ~3-34(; Evaporator, Air Conditioner Dual Brake System Bleeding ................... ~ ~ ~3-25 Filter Replacement ................... .......3-30F Installation ................... ............... 3-30F Removal .................................,..3-30F E Exterior Cleaning ................... ................ .2-22 Electric Paints ................... ................... 2-24 Propeller Deicing .........,._.,.. ..~ ~ ~ ~ ~ ~ ~ ~ ~ 3-55 Extended Storage and High Wind, Mooring ........2-19 Trim Tab Actuator ..................~ ~ ~ ~ ~ Illus. 3-6G Brush Wear Limits ........._._.,., .~ ~ ~ ~ ~ ~ ~ ~ 3,7 Installation ..................~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ 3-6K F Removal .................~~ ~ ~ ~ ~ ~ ~.~ ~ ~ ~~~~~~3-6J Trim Tab System ................... . ~ ~ ~ ~ ~ ~ ~ ~ 3-6J Filters Electrical System ................... ...~ ~ ~ ~ illus. 3-20 Gyro Instrument Air ................... .......3-30J´• Alternator ..............~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ Illus. 3-20 Pressure System .............._ 3-30H, Illus. 3-30H Battery .........____ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ Illus. 3-20 Firestone Brake Adjustment ................... ...3-26 Circuit Breaker Panels ................., .Illus. 3-20 Flap Actuator ................._ .....4-6A, Illus. 5-13 Flap Limit Switches ................... ...lllus. 3-19 Assembly ................._ ................ .5-12 Flap Motor ................... ..~ ~ ~ Ilius. 3-19, 3-20 Disassembly ................... ...............5-12 Fuel Transmitters ..................~ ~ ~ ~ ~ ~lllus. 3-20 Overhaul ....;...............................5-12 Generator Brushes ................ 3-34D, Illus. 3-20 Flap System ................... .......3-17, Illus. 3-19 Magnetos ................... .3-34A, 4-13, Illus. 3-20 Limit Switches ................... ...3-17, Illus. 3-19 Stall Warning Switch ................... ...lllus. 3-20 Motor ................... ................ .3-18, 4-5 Starter ................... ~ ~ ~ ~ ~ ~ ~ ~ ~ ~~~~~~lllus. 3-20 Illus. 3-19 Starter Solenoid ................... .......lllus. 3-20 Position Indicator and Utilization Load Chart ................... ....~3-36H Adjustment ................... ...3-18, Illus. 3-19 Voltage Regulator ..........3-34D, 3-348, Illus. 3-20 Settings ................... .............lllus. 3-19 Wiring Diagrams Index ................... ......~6-2 Shaft ................., ................. 4-5, 4-6 817 1-7 ALPHABETICAL INDEX F G Track Inspection ................... ...........4-6 Heat Exchanger Inspection ................... ...3-29 Track Wear Limits ................... .........4-6A Heat Test, Propeller Deicer ................... ...3-56 Flaps, Cowl ...........................,,..,..3-16C Heater Exchanger, Inspection .........,.,.,.. .3-29 Rigging Forward, TSIO Engine ................. .3-17 Hinges Inspection, Elevator Tab ................. 3-6J Flares ................... ................... ..3-34 Hoisting ................... ....... Flight Controls ................... ...............3-2 Flyable Storage. ................... ........... 2-208 Freeing Turbocharger Shafts ................... .3-368 1 Front Seats Installation ................... ...............3-33 Idler Adjustment, Carburetor ................... .3-34 Removal ................... ................. 3-33 Ignition ................... ........... Fuel Cell Indicator Rigging, Elevator Tab .................. 3-61 Capacities ................... ............... 2-208 Index, Electrical Wiring Diagrams .................. 6-2 Flapper Valve Inspection ......................3-15 Inspections Fuel Level Replacement Transmitters in the Main Control System ................... .............3-2 FuelCell ..........3-148, 4-14, Illus. 4-14, 4-15, 4-16 Deicer, Electric Propeller ................... .....7-1 Fuel Pump Adjustment Engine .........,.,., .3-14A Elevator Tabs ................... ........., 3-68 Fuel System ..... 3-14, Illus. 3-14D, 3-16A, 3-168 Elevator Tab Hinges ................... ...... 3-6J Auxiliary ................... .............llius. 3-16 Flap Track ................... ............. Bladder Type Fuel Cells ................... ...3-148 Fuel Tank Vent Lines ........................3-148 Fuel Cells, Care and Repair .................. 3-14F Fuselage Bulkheads ............... .......3-32A Patch, Outside ................... .........3-14F Guide ................... ................ .7-1, 7-2 Patch, Inside ................... ...........3-14G Heat Exchanger ................... ...........3-30 Servicing ................... ............... 2-208 Heat and Vent ................... ........... Transmitters ................... .............3-148 Main Fuel Cell Flapper Valve ..................3-15 Vent Lines, Inspection ................... .....3-148 Periodic ......................................7-1 Fuel Unit ................... ............... Illus. 5-11 Installation Assembly ................... ................ .5-10 Compressor, Air Conditioner .................. 3-30D Disassembiy ................... .............5-10 Compressor Belt, Air Conditioner .........,..3-30D Repair ......................................5-10 Condenser, Air Conditioner .................. 3-30D Testing ................... ................... 5-10 Control Column Arm ................... ....... Fuselage Bulkheads, Inspection of ..............3-32A Electric Trim Tab Actuator ................... .3-6J Fuselage and Empennage Skin Plating ........lllus. 2-7 Elevator Trim Tab ................... .... Illus. 3--6F Elevator Trim Tab Actuator ................... .3-6H Empennage ................................4-108 G Engine... ............... ................... .4-108 Evaporator, Air Conditioner .........,._.__ 3-30F Generator G35 Front Seats ................... ...........3-33 Belt Adjustment ................... .......lllus. 3-20 Light Tray ............ ................. 2-28 Brush Replacement .................. .......3-348 Magnetic Clutch ................... .............3-7 Overvoltage Relay ................... .........3-36 Magnetos ................... ............... 3-34A Standby System ................... ...........3-35 New Tab Cable ................... .......... 3-6K Goodyear Propeller Deicer Boot............... .4-17, Illus. 4-18 Brake Adjustment ................... .........3-26 Teleflex Cable ......................,.......4-10A Brake Linings, Removal and Replacement Vacuum Pump ................... ...........3-30G (One Pressure Cylinder Type) ................ 4-6A Velcro Tape with Replacement Cells........... .3-148 (Two Pressure Cylinder Type) ................. .4-7 Windshield ..................................4-17 Brake Unit, Disassembly Wing Tip Tank ..............................3-14C (One Pressure Cylinder Type) ................ 4-6A Instrument Brake Unit, Disassembly Engine ................... ..........,...., 3-30J Repair and Reassembly of Pressure ................... ..............., 3-30H (Two Pressure Cylinder Type) ................4-7 Filters ................... ................. 3-301 Gravity Bleeding ................... ............3-25 Wedge Lighting ................... ...........2-28 Grimes Strobe Light ................... .........3-32 Interior, Cleaning ................... .............3-22 Ground Cable and Adjustment, Static .........,.2-23 Guide, Autopilot Troubleshooting ................ 3-30N J Guide Inspection ................................7-1 Gyro, Autopilot Troubleshooting ................ 3-30N Jacking ................... ................... ..2-17 Heat and Vent System, Inspection of ..3-29, Illus. 3-28C- Jig, Air Conditioner Wick .........,.,.,., .Illus. 3-30 ~-8 B17 ALPHABETICAL INDEX L M Landing Gear Main Landing Gear Actuator Overhaul ........._._._. 5-14, Illus. 5-15 Fitting, Correcting End Play .................. 3-22A Actuator, Removing and Installing ............,..4-5 Removal and Installation ................... .....4-5 Correcting End Play in Main Strut Landing Gear Fitting ................._ ...3-22/1\ Assembly ................... ...............5-8A Door Adjustment ................. .3-188, Illus. 3-23 Disassembly ................ 5-5, Illus. 5-6, 5-7, 5-8 Limit Switches ..............................3-18A Repair ................... ................... 5-5 Motor, Removing and Installing .................. 4-5 Main Spar, Removal and Installation ..............4-2A Nose Gear Improvement Changes ..............3-22A Maintenance Position Light Adjustment ................... ...3-22 Air Conditioning System ................... ...3-308 Rigging ................... ...3-188, Illus. 3-23, 3-24 Emergency Locator Transmitter ..............3-32A Rigging Nose Wheel Steering Mechanism ......3-22A Propeller Blade ................... ...........2-22A Safety Switch Adjustment ..........3-18A, Illus. 3-23 Manufacturer’s Tolerance Table ................... .5-9 Safety System ..............................3-18A Master Cylinder, Brake ................ 3-26, Illus. 3-27 Shock Strut, Main........5-5, 5-8A, Illus. 5-6, 5-7, 5-8 Linkage Adjustment ................... .......3-26 Shock Strut, Nose ................ 5-4, Illus. 5-2, 5-3 Overhaul ....................................5-16 System ................... ...3-18, Illus. 3-23, 3-24 Removal and Installation ................... ...3-26A Throttle Warning Switch Microswitch Adjustment Landing Gear ..........3-188 Adjustment ................... ...3-25, Illus. 3-24 Models, Serials, Differences ................... ...1-16 Travel Stop Adjustment ................... ...3-22/1 Mooring (Extended Storage and High Wind)........2-19 Uplock Adjustment ............3-22A, Illus. 3-23, 3-24 Motor Uplock Roller Lubrication .........,.,._._ ...2-20 Flap ................. .3-18, 4-5, 4-6, Illus. 3-19, 3-20 Leading Edge, Wing, installation ........._._.__ 4-2A Landing Gear............. .4-5, Illus. 3-20, 3-23, 3-24 Leading Edge, Wing, Removal ........._.,.,._ .4-2A Leak Test Procedure, Turbocharger ..........._.3-368 Leak Detection, Air Conditioner .........._.,. 3-308 N Leveling. ................... ................... .2-17 Light New-Matic Autopilot, BEECHCRAFT ........... 3-30K, Bulb Replacement Guide .........,._._.. ...2-28 Illus. 3-30K, 3-30L, 3-30M Instrument, Wedge ................... .........2-28 New Tab Cable Installation .........,.,.,.. .. 3-6K Strobe ................... ........._._.,.. 3-32 Normal Tie-Down ..............................2-19 Tray Installation ................... ...........2-28 Nose Gear Limit Switch, Flap ................... .3-18, Illus. 3-19 Improvement Changes ............,..... .....3-22A Limit Switch, Landing Gear............ 3-188, Illus. 3-24 Removal and Installation ................... .....4-4 Load Chart, Electrical Utilization ........._.,.. 3-36H Shock Strut Assembly ............5-4, Illus. 5-2, 5-3 Locator, Emergency Transmitter ................ 3-32A Shock Strut Disassembly ..........5-4, Illus. 5-2, 5-3 Lock, Cabin Door ................... ........._3-328 Strut Repair ................... .............. Lock, Control ..................................2-19 Nose Wheel Locks, Roton ................... .....3-33, Illus. 3-34 Scraper ................... ................... 3-34 Lubrication ...........................,........2-lg Steering Mechanism ................... .......3-22A Diagram ................... .Illus. 2-14, 2-14A, 2-15 Travel Stop Adjustment ............,.,, ...3-22A Landing Gear Uplock Rollers .................. 2-20 M Oil System ...............................,...,3-15 Magnetic Clutch Servicing ..............,... ..........,.,.. 2-20 Installation ................... ..........,.,, 3-7 Tank and Cooler ................... ......... Removal ................... ................ 3-6K Oils, Approved Engine ................... .......2-20A Torque Test ................... .............,3-7 Openings, Access ................... ...lllus. 2-4, 2-5 Magneto, Bendix, Eismann, Slick ................ 3-348 Optional Stability Augmentation Breaker Point Adjustment ................... .3-34A System ................... ............... Illus. 3-14 Drop-Off Check ................... .........,3-34C Overhaul Installation ...........,.,., ...3-34A, 3-348, 4-13 Brake Master Cylinder ..............5-16, Illus. 5-18 Removal ....................................4-13 Replacement Schedule ................... .......8-2 Timing ................... ........._3-34A, 3-348 Shimmy Dampener ...........,...... .........5-8A Main Fuel Cell Flapper Valve Inspection .........,.3-15 Overvoltage Relay ................... .........3-34D B~f 1-9 ALPHABETICAL INDEX O R Oxygen System Removal and Installation (Cont’d) Cylinder Retesting ............,.,.. .......2-228 Condenser, Air Conditioner .........___, 3-300 Servicing ................... .........__, 2-22A Control Column Arm ................._ .........3-2 Electric Trim Tab Actuator ................._ 3-6J Empennage ................................4-108 P Engine............... .......................4-108 Evaporator ........._____ .........__, 3-30F Paints ................... ................... ..2-24 Flap Motor .........__,__ ...... Parking Brake ................... ...............2-19 Flap Shaft ........._,,,, ........._ Parking Brake Valve .................. 3-26A, Illus. 3-27 Front Seats ........._......_ ............._3-33 Pedal Rig Tool, Rudder ............... .3-10, Illus. 3-10 Landing Gear Actuator ................... .......4-5 Periodic Inspections ................... ...........7-1 Landing Gear Motor ................... .........4-5 Pitot System .................. 3-26A, 3-28, Illus. 3-288 Light Tray ................... ........._.,._ 2-28 Plating, Skin Magnetic Clutch ........._.,.,.. .......... 3-6K Fuselage ................... .........lllus. 2-7, 2-9 Main Landing Gear ................... .........4-5 Wing ................... ..............._ Illus. 2-11 Nose Landing Gear ................... ........ Position Indicator and Retract Rod ................... ...............4-5 Adjustment Flap ................... .3-18, Illus. 3-19 Teleflex Cable ..............................4-10A Position Light Adjustment Ventilation Blower, Air Conditioner ............3-30D Landing Gear ................... .............3-22 Vertical Instrument Instructions ................ 3-30J Positioning, Three Bladed Propeller ..............4-14 Windshield ..................................4-17 Pressure Wing Tip Tank ................... ...........3-14C Bleeding, Brakes ................... ...........3-25 Repair Switch Adjustment Landing Gear ..............3-188 Main Gear Strut ................... .............5-5 System, Instrument ................... .......3-30H Nose Gear Strut .........,.,.,.. .........,5-4 Illus. 3-30H, 3-301 Replacement Fuel Level Transmitters in Filters, Instrument ...........,.,. 3-30J, Illus. 3-301 the Main Fuel Cells ................... .......3-148, Propeller 4-12, Illus. 4-12, 4-13, 4-14 Brush’Block Resistance Check........3-57, Illus. 3-57 Replacement and Overhaul Schedule .........._..8-2 Deicer, Electric ................... .........,..3-55 Retract Rod Removal and Installation ..............4-5 Boot Installation ................. .4-17, Illus. 4-18 Rigging Boot Removal ............ ................ ..4-17 Control Column Chain ................... .......3-2 Boot Repair ................... .............5-16 Control Surfaces ................... ...........3-2 Brush Replacement ................ 3-55, Illus. 3-55 Cowl Flap ..................................3-16C Continuity Test ................... ...........3-57 Elevator Tab Indicator ................._ ..... 3-61 Heat Test ................... ...............3-56 Elevator Tab to Correct for Yaw .........,._.. 3-6J Inspection Procedure .........,.,.,., .....7-1 Forward Cowl Flaps ..........................3-17 Slip Ring Alignment .........,.,._.. .....3-57 Landing Gear ............,. .3-188, Illus. 3-23, 3-24 Timer Check ................... .............3-56 Nose Wheel Steering Mechanism ..............3-22A Propeller Blade Maintenance ................... .2-22A Roton Locks ................... .....3-33, Illus. 3-34 Publications, Supplementary Rubber Seals ................... ...............2-22 BEECHCRAFT ................._ .........,1-14A Rudder Control System ................... .. Illus. 3-8 Vendor ................... ................... 1-12 Rudder Pedal Rig Tool ................... ..lllus. 3-10 Rudder, Rigging ................... ...............3-9 R S Reassembly Safety Switch Adjustment, Landing Beech Brakes ................... .........,.,.4-8 Gear .........,........ .........3-18A, Illus. 3-23 Shimmy Dampener ................., .........5-9 Safety System, Landing Gear ................... .3-18A Relay, Overvoltage .........,.,.,.. .........3-348 Schedule. Overhaul and Replacement ..............8-2 Relief Valve Adjustment, Suction .................. 3-30 Scraper. Nose Wheel ................... .........3-34 Regulator Adjustment, Voltage............ 3-34D, 3_348 Seals, Rubber .........,.,._., ...............2-22 Removal and Installation Seats. G35 Front ................... ...........3-328 Bladdei Type Fuel Cell ................... ..I 3-148 Seats, H35 Front ................... .............3-33 Brake Master Cylinder ................... .....3-26A Servicing Compressor, Air Conditioner .................. 3-300 Air Conditioner ........._.,.,., .....2-22B, 3-29 Compressor Belt, Air Conditioner ..............3-30D Battery ................... ................ 2-20H 1-10 Bll BEECHCRAFT BONANZA 33/35 SERIES SHOP MANUAL ALPHABETICAL INDEX S Strobe Light Bullock ....................... 3-30S Servicing (Contld) Grimes 3-32 Brake System ´•´•´•´•´•´•: ´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´•´• 2-20D Trouble Analysts 3-30S Oxygen System ................. 2-22A Troubleshooting the Power Unit 3-30S Wing Tip Tanks 2-208 Converter Troubleshooting 3-30S Shimmy Damper Illus.5-9 Trigger Circuit Troubleshooting 3-30S Assembly 5-9 Suction Relief Valve, Adjustment 3-30A Disassembly .......... 5-8A,Illus.5-9 Suction Relief Valve Screen, Overhaul 5-8A Cleaning 3-30A Table of Tolerances 5-9 Supplementary Publications Testing :................... 5-10 BEECHCRAFT .. ................... 1-15 Shock Strut, Ma~n Illus.5-2,5-7 Vendor 1-12 Assembly ........................ 5-8 Switches Disassembly ..................... 5-5 Flap Limit ..:.:..... 3-18,Ilius.3-19 Repair 5-5 Landing Gear L~mit Illus.3-18A Servicing 2-20B Safety, Landing Gear Illus.3-23 Shock Strut, Nose Illus.5-2,5-3 Throttle Warning Illus.3-24 Assembly 5-4 Systems Disassembly 5-4 Aileron Control Illus.3-3 Repair """"’:~ 5-4 Air Conditioning, Evaporat~ve 3-30 Servicin :........, 2-208 Air Conditioning, Refrigerative 3-30A Shop Manua Introduct~on 1-1 Electric Trim Tab 3-65 Shuttle Valve, Dual Brake Electrical 2-22,111us.3-20 System 3-26A,Illus.3-27 Elevator Control .......... Illus.3-4 Single Control Column ............. 3-2 Filters, Pressure 3-30J,Illus.3-30I Skin Plating Illus.2-7,2-9,2-l1 Flap 3-17,Illus.3-19 Slip Ring Alignment 3-57 Flight Controls 3-2,Il~us.3-3,3-4,3-8 Spar, Main Removal Fuel, Servicing 2-20B,Illus.3-14D,3-16 and Installation 4-2,4-4 3-16A,3-16B Spark Plugs 3-34A Heat and Vent .................... 3-30 Special Tools ....:.... Illus.2-12,2-13 Inspection, Flight Control 3-2 Stability Augmentation System Illus.3-34 Landing Gear 3-18,4-4,Illus.3-23,3-24 Stall Warning Adjustment 3-28 Landing Gear Safety 3-18A Stall Warning Switch Illus.3-20 Oil, Servicing 2-20,3-15 Stall Warning System 3-28,Illus.3-20 Optional Stability Standby Generator System 3-36 Augmentation Illus.3-14 Starter 3-36,111us.3-20 Pitot and Static Air 3-26A,Illus.3-28E "’:"’’´•´•´•´•´•´•´• Starting tng~ne :......... 2-18 Pressure 3-30H,Il~us.3-30H,3-30I Starting Turbocharged Eng~ne 2-18 Rudder Control Illus.3-28 Static Air System ´•":"´•"’´•’´• 3-26A,Illus.3-28B Stability Augmentation Illus.3-14 Static Ground Cable and Vacuum .......................... 3-300 Adjustment :............... 2-23 Static Lines, Clear~ng 3-28 T Stations Diagram .................. 2-3 Steering Mechanism, Nose Wheel .. 3-22A Tab Step, Assist ..................... 3-25 Aileron ......................... 3-5 Stopping Engine .................. 2-19 Elevator Illus.3-6F,3-6E Storage Elevator Tab Actuator .......... 3-6H Flyable ....................... 2-20E Hinges Inspection, Elevator 3-65 Indefinite 2-20F Indicator Rigging, Elevator 3-61 Preparation for Service 2-21 Inspection, Elevator Tabs 3-60 Temporary 2-20F Rigging to Correct for Yaw ..... 3-63 817 1-10A BEECHCRAFT BONANZA 33/35 SERIES SHOP MANUAL Table Teleflex, Cable Installation 4-10 Manufacturer’s Tolerances 5-9 Temperature Effect on Cable Models, Serials, Differences 1-16 Tension .................. Illus.3-2C of Contents ................... 1-3 Testing, Emergency Locator of Lubricants 2-14 Transmitter ................... 3-32A of Torques, Wing Bolts 4-2 Testing, Shimmy Damper 5-10 Taxiing 2-19 Throttle Warning Horn Adjustment 3-25 1-108 817 ALPHABETICAL INDEX 7 7 Tie-Down, Normal ..............................2-19 Turbocharger (Cont’d) Tip Tank Exhaust and Air Induction ................ Illus. 4-11 Installation ................, .............. .3-148 Schematic ................... ..........´•lllus. 3-36G Removal ................... ................ .3-14C System .........................´•´•´•..´•´•´•´•´•...4-12 Servicing ................... ............... 2-208 Tires Recapped Not Recommended ................ 3-26A U Servicing ................... .............. .2-20D Tube Type Uplock Rollers, Lubrication of Dismounting ................... .............4-8A Landing Gear ................... ..´•..´• ´• ´• ´• ´• ´• ´• ´•2-20 Mounting ................... ...............4-88 Tubeless Type Converting Wheels for Inner Tubes ............4-10 V Dismounting ................... .............4-9 Inflation ................... ................. 4-9 Vacuum System ................... ......´• ´• . ´• Mounting ................... ................. 4-9 Adjustment of Suction Relief Valve ............3-30G Tool, Rudder Pedal Rig ................... ...lllus. 3-9 Cleaning Oil Separator ................... ...3-30G Tools, Special ................... .....lllus. 2-12, 2-13 Cleaning Suction Relief Valve Screen ..........3-30G Torque Test, Magnetic Clutch ................... ...3-7 Installing Vacuum Pump ................... ...3-30G Towing ........................................2-17 Replacing Gyro Instrument Air Filters ..........3-30G Transmitter, Emergency Locator ................ 3-32A Valve Travel Stop Adjustment, Nose Wheel ............3-22A Parking Brake ................... .3-26A, Illus. 3-27 Trigger Circuit Troubleshooting; Shuttle ................... .........3-26A, Illus. 3-27 Strobe Light ................... .............3-308 Suction Relief ..........................´•...3-10A Trim Tab Actuator, Electric ............3-6J, Illus. 3-6G Velcro Tape Installation with Brush Wear Limits ................... ...........3-7 Replacement Cells ..........................3-14E Installation ................... .............. 3-6K Vendor Publications, Supplementary ..............1-12 Trim Tab Installation, Elevator ................ Illus 3-6iF´• Vent Lines, inspection of Fuel Tanks .........,.3-148 Trouble Analysis, Strobe Light .........,....... .3-30S Ventilating System .................. 3-29, Illus. 3-28(= Troubleshooting Voltage Regulator ................... .Illus. 3-20, 3-34[) Air Conditioning System ................... ...3-308 Alternator System ................... .........3-400 Altimeter ................... ................. 3-49 W Directional Gyro ................... ...........3-50 Flap Control Indicator Circuit .................. 3-43 Warning Horn, Landing Gear ................... ...3-5 Fuel Quantity Indicator Circuit .................. 3-46 Warning System, Stall ................ 3-28, Illus. 3-20 Generator System ................... .......3-40C Wear Limits, Electrical Trim Tab Gyro Horiton ................... .............3-49 Actuator Brush ................... ............. Guide, Autopilot ................... .........3-30N Wheel Disassembly and Assembly ´•................ 4-88 Ignition System ................... ...........3-42 Wick Jig, Air Conditioner ................... .Illus. 3-30 Landing Gear Position Indicator ..............3-428 Windshield Magnetic Compass ................... .........3-50 and Window Cleaning ............,...... .......2-22 Manifold Pressure Gage ................... ...3-46 Installation ..............................´•...4-17 Navigation Light Circuit ................... .....3-45 Removal ................................´•...4-17 Pitot and Static Pressure System ..............3-51 Wing Propeller Deicer System .................. 3-58, 3-59 Adjustment ................... ................. 4-4 Rate of Climb Indicator ................... .....3-47 Leading Edge and Main Spar, Stall Warning Indicator Circuit .................. 3-44 Removal and installation ................... .4-2A Standby Generator ................... .........3-41 Mounting Bolts ................ Illus. 4-28, 4-2C, 4-3 Starter System ................... ...........3-40C Removal ................... ......´• ´• ´• ´• ´• ´• ´• ´• ´• ´• Strobe Light Converter ................... ...3-308 Tip Tank Removal ................... .......3-14C Turbocharger System ................... .......3-52 Removal and Installation Differences ..............4-2 Turbocharger ................... ...............3-36 Wiring Diagrams Index, Electrical ................6-2 Critical Altitude Test .............. 3-368, Illus. 3-36F B1’7 1-1~ SUPPLEMENTARY PUBLICATIONS Following is a list of publications providing servicing, overhaul and parts information on various components of the BEECHCRAFT Bonanza which you may obtain to supplement the Shop Manual. In most instances, you should obtain the publications directly from the manufacturer or his distributor. Beech supplementary publications, are available from BEECHCRAFT Aero or Aviation Centers and International Distributors and Dealers. Those which are so available are listed in the current Publications Price List. Since a wide variety of radio equipment is available and because radio manufacturers normally supply parts and servicing manual with each set, radio publications have not been included in the list. As publications on additional components become available, they will be added to this list of publications. VENDOR PUBLICATIONS ITEM PART NO. PUBLICATION PUBLICATION VENDOR NO. Engine E185-1 E165, E185, E225 Maintenance and X30016 Teledyne Continental Motors E185-8 Overhaul Manual Aircraft Products Division E185-ll P.O. Box 90 E225-8 Mobile, Alabama 36601 E185-1 E165, E185, E225 Parts Catalog X30017 Teledyne Continental Motors E185-8 Aircraft Products Division E185-II P.O. Box 90 E225-8 Mobile, Alabama 36601 E185-1 E165, E185, E225 Operators Hand- X30018 Teledyne Continental Motors E185-8 book Aircraft Products Division E185-11 P.O. Box 90 E225-8 Mobile. Alabama 36601 0-470-G Operators Handbook for 0-470 X30097 Teledyne Continental Motors Series Aircraft Products Division P.O. Box 90 Mobile, Alabama 36601 IO-470-G Maintenance and Overahul Manual X30022A Teledyne Continental Motors 1O-470-C for 0-470 and 10-470 Series Aircraft Products Division IO-470-N P.O. Box 90 Mobile, Alabama 36601 Illustrated Parts Catalog for 0-470 X30023A Teledyne Continental Motors and 10-470 Series Aircraft Products Division P.O. Box 90 Mobile, Alabama 36601 1O-470-C Operators Handbook for 10-470 X30024 Teledyne Continental Motors IO-470-N Series Aircraft Products Division P.O. Box 90 Mobile, Alabama 36601 1O-520-B Maintenance and Overhaul Manual X30039A Teledyne Continental Motors 1O-520-BA for 10-520 Series Aircraft Products Division 1O-520-BB P.O. Box 90 Mobile, Alabama 36601 1O-520-B ´• Illustrated Parts Catalog for 10-520 X30040A Teledyne Continental Motors 1O-520-BA Series Aircraft Products Division 1O-520-BB P.O. Box 90 Mobile, Alabama 36601 1-12 813 VENDOR PUBLICATIONS (COntinued) ITEM PART NO. PUBLICATION PUBuLjl3ATIONNO. VENDOR Engine 1O-520-B Operators Manual for 10-520 X30041 Teledyne Continental Motors (Cont’d) 1O-520-BA Series Aircraft Products Division 1O-520-BB P.O. Box 90 Mobile, Alabama 36601 TSIO-SZO-D Maintenance and Overhaul Manual X30042A Teledyne Continental Motors for TSIO-520 Series Aircraft Products Division P.O. Box 90 Mobile, Alabama 36601 ’TSIO-520-D Illustrated Parts Catalog for TSIO- X30043A Teledyne Continental Motors 520 Series Aircraft Products Division P.O. Box 90 Mobile, Alabama 36601 TSIO-520-D Operators Manual for TSIO-520 X30044 Teledyne Continental Motors Series Aircraft Products Division P.O. Box 90 Mobile, Alabama 36601 N/A Tips on Engine Care Teledyne Continental Motors Aircraft Products Division P.O. Box 90 Mobile, Alabama 36601 Fuel Overhaul Manual and Illustrated X30091 Continental Motors Corpo- Injector Parts Catalog for Continental ration Fuel Injection System Turbo- TE06 Overhaul Manual and Parts Catalog X30055 Continental Motors Corpo- charger for TE06 Turbocharger ration Propeller F12A-3 UNIVAIR Service Manual Universal, Aircraft Model F12 Constant speed Industries, Denver, Propeller Colorado PHC-A3VF41 Owner’s Manual, Optional Three Blade 1061 Hartzell Propeller, Inc., V8433-4R Propeller Piqua, Ohio PHC-A3VF41 Overhaul Instructions 114A Hartzell Propeller, V8433-4R Inc., Piqua, Ohio PHC-C3YF-IRF/ Hartzell Propeller 115C Hartzell Propeller, F84686R Owners Manual Inc., Piqua, Ohio PHC-C3YF-1R/ 8468-6R BHC-C2YF-1BF/ Hartzell Propeller 115C Hartzell Propeller, F8468 Owners Manual Inc., Piqua, Ohio BHC-C2YF-1B/ 8468 1-12A B13 Courtesy of Bomar Flying Service www.bomar.biz VENDOR PUBLICATIONS (Continued) ITEM PART NO. PUBLICATION PUBLICATION VENDOR NO. Propeller 2A36C23CP/ Service Manual and 720415 McCauley Indust- (Cont’d) 84B0 Parts Catalog rial Corp. 3A32C76S/ Service Manual and 720415 McCauley Indust- 82NB-2 Parts Catalog rial Corp. Governor C210452 Overhaul Manual with Parts 33017 Woodward Governor Co. List (10-520 Engine) D210680 Overhaul Manual with Parts List 33080 Woodward Governor Co. (10-520 Engine) Fuel RD-7420 Lear-Romec Handbook Service and Lear-Romec Division, Pump Overhaul Instructions with Parts Lear, Inc. Catalog, Aircraft Engine Fuel Pumps, Series RD-7420. RD-7430-2 Lear-Romec Handbook Overhaul Lear-Romec Division, Instructions with Parts Catalog Lear, Inc. Aircraft Engine Fuel Pumps, Series RD-7430 RD-7790 Romec Handbook Operation, Lear-Romec Division Service and Overhaul Instructions Lear, Inc. with Parts Catalog, Series RD-7750 and RD-7790 Aircraft Fuel Pumps TF-1900 Thompson Aircraft Engine-Driven Thompson Products, Inc. Fuel Pump, Model TF-1900 TF-1100 Thompson Aircraft Engine-Driven Thompson Products, Inc. Fuel Pump Model TF-1100-2 TF-100-1 Thompson Aircraft Engine-Driven Thompson Products, Inc. Fuel Pumps Generator 1101879 Test Specifications DR324S Delco-Remy Division, 1101886 General Motors Corporation 1101887 (533730)* 1101888 (539829)* 1101895 (535896)* 1101909 (626380)* Parts List Group 93-G Delco-Remy Division, General Motors Corporation Air Condi- Model 508 Abacus Automotive Air Condition- I.D. 160717 Abacus International tioner Com- ing Compressor Service Manual P.O. Box 327 presser Dallas, Texas 75221 Battery PS12-ll Service Manual GSM-1277 Teledyne Battery Products Redlands, California 1-128 813 VENDOR PUBLICATIONS (Continued) ITEM PART NO. PUBLICATION PUBLICATION VENDOR NO. Alternator 1100652 Service Bulletin. Tests and Main- 16-262 Delco-Remy Division. Gen- 1100643 tenance of "Delcotrons" etal Motors Corporation ALX-9405 Equipment List, Service Parts List OE-AI Prestolite Company 511 Hamilton St. ALV-9407 Toledo, Ohio 43694 ALT-9422 642056A 1 Service and Overhaul X30~31 Teledyne Continental Motors Aircraft Products Division Instructions P.O. Box 90 Mobile. Alabama 36601 Starter I 109660 Test Specifications DR 3243 Delco-Remy Division. Gen- eral Motors Corporation Parts List Group 70 Delco-Remy Division, Gen- eral Motors Corporation Yaw YKh31 Automatic Flight Systems Bulletin No. 75R Edo-Air Mitchel P. O. Box 610 Damper Mineral Wells. Texas 76067 1-13 813 VENDOR PUBLICATIONS (Continued) ITEM PART NO. PUBLICATION PUBLICATION VENDOR NO. Starter 1109471 Test Specifications DR324S Delco-Remy Division, Gen- (Cont’d) (535856)* eral Motors Corporation Parts List Group 67 Delco-Remy Division, Gen- eral Motors Corporation 397-13 Overhaul Manual for E-80 1912 Utica Division, Bendix Direct-Cranking Electric Starters Aviation Corporation Catalog L, Chapter 46, Part B 36E14-1-C Direct-Cranking Electric Starter, 544-15 Utica Division, Bendix Types 36E14-1-B and 36E14-I-C Aviation Corporation Overhaul Instructions MHJ-4003 Equipment List, Service Parts OE-A 1 Prestolite Company List Toledo, Ohio 43694 I511 Hamilton St. Carburetor PS-SC Overhaul Instructions for Injection 15-144 Bendix Products Division, Carburetor Model PS-SC, Parts List Bendix Aviation Corporation Numbers 380208-7, 380223-4, 391318-5, 391330-7, 391583-1, 391629-3 Illustrated Parts Breakdown for 15-139A Bendix Products Division Injection Carburetor Model PS-SC Bendix Aviation Corporation Parts List Numbers 380208-7, 380223-4, 391318-5, 391330-7, 391583-1, 391629-3 Bendix PS Series Carburetor Manual 15-186 Bendix Products Division, Bendix Aviation Corporation PSH-SBD Overhaul Instructions for Injection 15-137 Bendix Products Division, Carburetor, Model PS-SBD** Bendix Aviation Corporation Illustrated Parts Catalog for Injection 15-127A Bendix Products Division Carburetor, Model PS-SBD** Bendix Aviation Corporation Vacuum 3P-194F Service Manual with Parts Catalog, Pesco Products Division, Pump Standard Engine-Driven Vacuum Pumps Borg-Warner Corporation G450 Overhaul Manual with Parts List for Garwin, Inc. the G450 Series Vacuum Pump A-S13-DB Operation, Service and Overhaul In- The Aro Equipment A-S13-DA structions with Illustrated Parts Corporation Breakdown for Aro Model A-J13-DB Air Pump Magnetos S6LN-21 User Operating Instructions, Bendix L-239-3 Scintilla Division, Bendix Aircraft Magnetos Aviation Corporation Service Instructions, Bendix L-205-5 Scintilla Division, Bendix Aircraft Magnetos Aviation Corporation Service Parts List, Bendix L-223-5 Scintilla Division, Bendix Aircraft Magnetos Aviation Corporation 1-14 811 VENM)R PUBLICATIONS (Contlnued) ITEM PART NO. PUBLICATION PUBLICATION VENDOR NO. Magnetos S6RN-201 Installation, Maintenance and L-526 Scintilla Division, Bendix (Cont’d) S6RN-205 Operation Instructions Aviation Corporation S6RN-1201 Service Instructions, Bendix L-609 Scintilla Division, Bendix S6RN-1205 Aircraft Magnetos Aviation Corporation Service Parts List, Bendix L-608 Scintilla Division. Bendix Aircraft Magnetos Aviation Corporation S-600 Series Overhaul Instructions L-551 Scintilla Division, Bendix Aviation Corporation S-600 Series Service Parts List L-552 Scintilla Division, Bendix Aviation Corporation 400 and 600 Parts Catalog and Service Manual, 1012 Slick Electro Inc. Series Slick Magnetos Voltage 1118263 Test Specifications DR324S Delco-Remy Division, Gen- Regulator eral Motors Corporation Parts Lists Group 6-A Delco-Remy Division, Gen- eral Motors Corporation 1118358 Test Specifications DR 3248 Delco-Remy Division, Gen- 1118384 ’ eral Motors Corporation 1118385 Parts Lists Group 6-D Delco-Remy Division, Gen- eral Motors Corporation 1118713 Test Specifications DR 324S Delco-Remy Division, Gen- (537486)* eral Motors Corporation Parts List Group 6-E Delco-Remy Division, Gen- eral Motors Corporation 1118891 Test Specifications DR 3243 Delco-Remy Division, Gen- eral Motors Corporation Parts List Group 6-H Delco-Remy Division, Gen- eral Motors Corporation 9000590 Service Bulletin, Test and Adjust- 1R-273 Delco-Remy Division, Gen- ments of Transistor Regulators eral Motors Corporation Autopilot B-5 Flight Control System Ground 3952 Brittain Industries and Flight Check Procedures P.O. Box 51370 Tulsa, Oklahoma 74151 Autopilot B-5 Automatic Flight Control 3950 Brittian Industries System Maintenance Manual P.O. Box 51370 Tulsa, Oklahoma 74151 B-7 Flight Control System, Flight 3959 Brittain Industries Procedures Manual P.O. Box 51370 Tulsa, Oklahoma 74151 1-14A VENDOR PUBLICATIONS (Continued) ITEM PART NO. PUBLICATION PUBLICATION VENDOR NO, Autopilot B-7 Troubleshooting Manual 3%0 Brittain Industries (Cont’d) P.O. Box 51370 Tulsa, Oklahoma 74151 Strobe 1000 Instruction and Service Manual 50082 BulLock Magnetics Corp. Light Pomona, California Strobe Light 60-1750-3 Overhaul Manual with 33-40-58 Grimes Manufacturing Power Supply Illustrated Parts List Company, 515 North Russell Street Urbana, Ohio 43078 Landing 27-4 (35-380094) Component Maintenance 32-31-24 Electro-Mech, Inc. Gear 27-8 (96-380022-5) Manual with Parts List Wichita, Kansas Motor *Continental Motors Corporation part number. **Same as Model PS-SBD except PSH-SBD is mounted horizontally. 1-148 814 SUPPLEMENTARY BEECHCRAFT PUBLICATIONS 92-30582 Servicing and Maintenance Instructions and Illustrated Parts Manual for: Main Wheel Assembly P/N 95-300001-1, -5, -6, -67 and -73. Nose Wheel Assembly P/N 95-32669 and P/N 95-32926. Beech Aircraft Corporation 130376A New-Matic B-4 Autopilot Operating Servicing Instructions. Beech Aircraft Corporation. 130409 New-Matic Autopilot Maintenance Instructions. Beech Aircraft Corporation. 98-35850 Electronics Components Maintenance Manual and Parts Breakdown B-5, B-5A, B-7, B-VII, B-VIII Autopilot Beech Aircraft Corporation. 98-35012 Servicing Maintenance Instructions and Illustrated Parts Breakdown for the Main Whuul. Nose Wheel and Brake Asbembly (P9193 and after) I 98-35776 Maintenance Information and Illustrated Parts Breakdown for 35-380094 Landing Gear Motor 91(-35655 B-5 and B-7 Owner’s Manual Automatic Flight Control System 98-36486 Overhaul Instructions for Vertical Display Engine Indicators used on BEECHCRAF~ Bonanza series aircraft 98-33’81B Servicing and Maintenance Instructions and Illustrated Parts Breakdown for the Main Wheel, Nose Wheel and Brake Assembly (D-7923, D-8461 thru D-9192) 1 98-36234 Installation, Maintenance and Illustrated Parts Breakdown for the 35-380093-2 Voltage Regulator 98-33690B Installation, Maintenance and Illustrated Parts Breakdown for 35-380093 and 35-380093-1 Voltage Regulator 1-15 814 MODELS, SERIALS, DIFFERENCES Model Year Serials Gross Wt. Engine Propeller Major Changes 35 1947-8 D-l through D-1500 2550 E-185-1 R-203 A35 194’) D-1500 through D-2200 2650 E-185-I B-200 Steerable nose wheel replaced full swivel nose wheel. Delco- Remy starter replaced by E80. Tubular steel carry-through structure replaced by aluminum extrusion carry-through. B35 1’)50 D-2201 through D-2h80 2650 E-185-8 B-200 30 degree flaps. C35 0-2681 through 0-3400 2700 E-185-11 215(88") Aluminum alloy propeller blades replaced plastic covered wooden blades. 35 amp generator replaced 25 amp generator. Wing root fillet added. Larger stabiliz- er incorporated. D35 1953 D-3401 through D-3698 2725 E-185-11 2 1 5(88") 36E 14 starter replaced E80 starter. E35 1()54 D-365)9 through 0-3998 2725 E-185-1 1 215(88") Aileron trim control. or or Electric engine primer. E-225-8 215(84") F35 1955 D-3909 through 0-439 1 2750 E-225-8 215(84") Optional auxiliary wing fuel tanks. G35 1956 D-4392 through D-4865 2775 E-225-8 215(84") H35 1957 0-4866 through D-5330 2’)00 O-470-C ’78(84") Hydraulic governor. Front seats individually adjustable in flight. 535 1958 0-533 1 through D-5 725 2900 1O-470-C 278(82") Fuel injection engine. Electric fuel boost pump. K35 195’) D-5726 through 0-6161 2’)50 1O-470-C 278(82") Gross weight increase. In- crease fuel capacity. Optional fifth seat. M35 1’)60 0-6 1 6 2 through 0-6 56 1 2950 IO-470-C 278(82") New wing tips. N35 1961 0-6562 through 0-6842 3125 IO-470-N 278(82") New engine. Gross weight in- crease. Increased fuel capacity. P35 1962 0-6842 through 0-7309 3125 1O-470-N 278 (8?") New instrument panel. or F12A-3 (82") or Universal seats. 2A36C23-CP (84") S35 1964 0-7310 through 0-7639 3300 IO-520-B New engine. Larger cabin. 2A36C23-CP(84") Increased gross weight V35 1965 0-7640 through 0-7967 3400 IO-520´•B One piece windshield. 2A36C23-CP(84") Flap indicator gage. Improved fresh air system. Increased heater capacity. Increased gross weight. 1-16 Bg M~ODELS, SERIALS, DIFFERENCES (Cont’d) Model Veer Serials Gross Wt. Engine/Propeller Major Changes V35 1966 D-7968 through 3400 10-5 20-B Exhaust gas temperature & D-8301 2A36C23-84B-0 Indicator. 3 blade V35TC: propeller. TSIO-520-D External power re- 2A36C82T/84B-? versal protection. Oxygen system change. Turbocharged engine. V35 1967 D-8302 through 3400 10-5 ?0-B New subpanel styling. & D-8598 2A36C23-84B´•0 V35TC TSIO-5 20-D Optional deicer system. 2A36C82T/84B-2 Wing tip tanks. V35A 1968 D-8599 through 3400 1O-520-B New magnetos. & D-8871 2A36C23-84B-0 Relocation of pressure V35A- air filter. TC TSIO-5 20-D Steerable landing 2A36C82T/84B-2 light. Electric pitch trim system. V35B 1969 0-8872 through 3400 1O-50-BA One piece windshield. & D-9068 2A36C23-84B-0 Vertical instruments. V35B- TC TSIO-520-D 2A36C82T/84B-2 V35B 1970 D-9069 through 3400 1O-520-BA Optional strobe light. & D-9204 and 2A36C23-84B-0 New parking brake V35B- D-9207 through TSIO-520-D system. TC D-9211 2A36C82T/84B-2 B7 autopilot. Instrument wedge lighting. New fuel cell. New fuel gaging transmitters. V35B 1971 D-9205,D-9206, 3400 IO-520-BA New propeller gov. D-9212 through 2A36C23-84B-0 Optional post lights D-9286 Digital hour meter. Fuel gage relocation. V35B 1972 D-9287 through 3400 1O-520-BA Moulded seat cushion. D´•9390 Up-lock roller grease bolt. 3 light strobe light. Standby generator. Emergency locator transmitter. V35B 1973 D-9391 through 3400 1O-520-BA Annunciator light change. D-9537 Improved air pump filter. Vertical instruments removed. Adjustable door actuating pin. V35B 1974 D-9538 and after 3400 10-5 20-BA Oust lock improvement. Aft cowl door handle. Improved battery. Pressure pump change. Bg 1-17 SECTION 2 General Information (Servicing) SECTION II GENERAL INFORMATION SECTION II GENERAL INFORMATION Some of the most important information about the Bonanza... lubrication, cleaning, shop handllng....will be found in this section. Particular at- tention should be paid to these items, since they are among the items which the customer sees and consequently can influence directly his decision to come back again, or to go elsewhere. The section includes a three-view drawing giving the major dimensions of the Bonanza; a table of hangar clearance dimensions; and an access opening illustration. A skin plating diagram gives the material and gage of each wing, empennage and fuselage skin, as a guide for making minor skin repairs. Two full page illustrations shaw the special tools, with their part numbers, which will make maintenance of the Bonanza simpler. Together with the tool part number is a serial designation showing which model Bonanza the tool is used on. 2-1 10’ 5 9/16" (D-2881 and after) 32’ 9-7/8" 5-1/2" (D-6162 and after) -I 25’ 1-1/4" 28’ 4-5/8" D-7310 and After .1--::..-.i 81 s-~/2"11\ ’ ~, ~ 7’’ (0-2681 and after) 7’ 1" 8. 5 (Normal ground attitude loaded to gross weight. ) ~ P.Lor to DJ189 4. 75 (Min clearance tire and shock deflated. ) 11. 5 (Normal ground attitude. )6. 75(Min. Clearance tire and shock deflated. ) D-3999 thnn D-5330 and D-13~n% after 7. 8 (Min Clearance with nose tire and shock deflated ) D-5331 thru D-7309 12. 5 (Normal ground attitude loaded to gross weight. ) :/*7; I- 9’ 7-1/8" ´•1 v3s~eo7-tz *Prior to D-3999 **D-3999 thru D-5330 and D-7310 and after ***:D-5331 thru D-7309 i Figure 2-1. Dimensions of Airplane 2-2 ´• B9 9 a 4 65.550 ~~ r 1-" 56.250---~~;r ,,, IP 35.750 ~-- 25.500 ; 131.60 15.250 1M).00 ’t i.’ 68.00 117.187 1 84.125 58.50 - In ,,,,, i ,,,~, 246.30 _~-~-233.50 207.00 /I 79.00 ~ Y 151.00 23.81 45.00 ,.w 80.047 ~= ~-94.094 108.281 23.881 122.750 31.75 39.375 i 148.875 "~oo 1 175.281 4.50 12.125 33.345 49.00 59.00 94.0941 j- ~\J .191´•00 66.00 103.641 113.172 122.75 O 136.188 162.563 ,,., 17,.281 E r 191.00 1 m n ´•3 cjO clZ ~J O w Figure 2-2. Stations Diagram Z# SECTION II GENERAL INFORMATION 1) \(2)1(3 ..; (6) ~ 12) (4 9)(10) (11 n~ a)l7 (i~ ~ 19) 35-1 3´•9 i. Elevator Tab Cable Pulley LH 11. Oil Filler Neck (Prior to D-4866) 2. Upper Stabilizer Spar Bolts (D-l to 0-2680) 12. Lower Stabilizer Spar Bolt (D-l to D-2680) 3. Elevator Tab Cable Pulley RH. 13. Differential Mechanism LH 4. Empennage Control Linkage 14. Carburetor Air Screen 5. Baggage Compartment 15. Differential Mechanism, Lower 6. CabinEntrance 16. Rudder and Elevator 7. Access Plates for Engine Cables 8. Hinge Bolts for Nose Wheel Strut 17. Rear Spar Jack Point 9. Engine Cowl 18. Landing Gear Actuator 10. Oil Filler Neck (D-4866 & after) 19. Fuel Strainer Figure 2-3. Fuselage Access Openings 2-4 SECTION II GENERAL INFORMATIO~ 5 5 ~2)n~ 4 )( 3 )(2) i) (7) (7) (j TOP LEFT TOP RIGHT ~~~~J)~~ 888 (F~~ (i~ (i~s~(is~ (Fi BOTTOM RIGHT BOTTOM LEFT 35-( 2-6 i. Optional Main Fuel Cell Filler Neck (D-6562 and after) 2. Auxiliary Tank Filler Neck (D-4000 to D-6561) 3. Main Fuel Cell Transmitter 4. Main Fuel Cell 5. Standard Main Fuel Cell Filler Neck 6. ~pper Front and Rear Spar Bolts 7. Flap Hinge Bolts 8. Fuel and Pitot Lines (D-6562 and after) 9. Auxiliary Fuel Tank (D-4000 to D-6561) 10. Fuel Lines (Pltot Lines in LH Wing) (Prior to D-g56;2) 11. Landing Light (Prior to D-6562) (Fuel Lines D-6562 and after) 12. Main Fuel Cell (D-6562 and after) 13. Landing Gear Hinge Bolt and Main Fuel Cell 14. Lower Front and Rear Spar Bolts 15. Auxiliary Fuel Tank (D-4000 to D-6561) 16. Aileron Cables and Fuel Lines 17. Aileron Bellcrank 18. Flap Limit Switch (D-l to D-3702) (Wheel Well) Figure 2-4. Wing Access Openings 2-5 SECTION II GENERAL INFORMATION Legend for Figure 2-5. (Sheet 1 of 2) INDEX GAGE DESCRIPTION SERIAL 1. .020 2024-SO D-l & after 2. .020 2024-T3 D-l & after 3. .020 2024-SO D-~ & after 4. .025 2024-’13 D-l & after 5. .016 2024-’13 D-1575 thru D-6561 .032 2024-T3 D-6562 & after 6. .016 2024-’13 D-1575 & after replaced with index no. 6 & 8 7. .025 2024-T3 D-1575 thru D-2681 .032 2024-T3 D-2682 & after 8. .020 2024-T3 D-1575 & after replaced with index no. 7 9. .020 2024-T3 D-1575 & after 10. .016 2024-T3 D-1575 & after replaced with index no. 9 & 11 11. .016 2024-T3 D-1575 thru D-2076 .020 2024-T3 D-2077 & after 12. .025 2024-0 D-l thru D-4865 .032 2024-0 D-4866 & after 13. .025 2024-T3 D-l & after *14. .020 2(324-0 D-l & after 15. .025 2024-T3 D-l & after 16. .016 2024-T3 D-l thru D-6561 .032 2024-T3 D-6562 & after 17. .020 2024-T3 D-4866 thru D-6561 18. .025 2024-T3 D-l & after 19. .040 6161-0 D-l & after 20. .020 2024-SO D-l & after 21. .020 2024-50 D-l & after 22. .025 2024-T3 D-l & after .025 2024-T3 D-7310 and after 2-8 Revised October 22, 1965 SECTION 1 GENERAL INFORMATION 1 2 3 4 * 5 6 7 8 13 12 11 10 9 LEFT IJAM) VIEW 14 15 16 17 35-1310 TOP VIEW +Skin Splice Moved Aft to Sta.179 as Shown. Effective D-8747 and After Figure 2-5. Fueelage and Empennage Skin Plating (sheet 1 of 2) Revised October 27, 1961 2-7 SECTION II GENERAL INFORMATION Legend for Figure 2-5. (Sheet 2 of 2) INDEX GAGE DESCRIPTION SERIAL 1. .025 2024-T3 D-1575 & after replaced with index no. 2 2. .025 2024-T3 D-1575 thru D-2680 .032 2024-’13 D-2681& after 3. .016 2024-T3 D-1515 & after replaced with index no. 2 & 4 4. .016 2024-T3 D-1575 thru D-6561 .032 2024-T3 D-6562 & after 5. .025 2024-T3 D-l thru D-3998 .032 2024-T3 D-3999 & after 6. .020 2024-50 D-l & after 7. .025 2024-T3 D-2801& after 8. .025 2024-T3 D-2801& after 9. .025 2024-T3 D-l & after *10. .020 2024-T3 D-l & after 11. .025 2024-T3 D-l & after 12. .025 2024-T3 D-l thru D-4865 .032 2024-T3 D-4866 & after 13. .016 2024-T3 D-1575 thru D-2076 .020 2024-T3 D-2077 & after 14. .016 2024-T3 D-1575 & after replaced with index no. 13 & 15 15. .020 2024-T3 D-1575 & after 16. .025 2024-T3 D-l & after 17. .016 2024-T3 D-l & after 18. .016 2024-T3 D-l & after 19. .020 2024-T3 D-l & after 20. .020 2024-T3 I)-l & after 21. .016 CRES D-l & after 22. .016 CRES D-l & after 23. .020 2024-T3 D-l thru D-1885 .032 2024-T3 D-1885 & after 24. .020 2024-T3 D-l & after 25. .016 2024-T3 D-l & after 26. .025 2024-T3 D-l & after .025 2024-T3 D-7310 and After 2-8 Revised October 22, 1965 SECTION II GENERAL INFORMATION 1)(2) (3) (4) ,* (5)(6) (7) (8 02) RIGHT HAND VIEW * Skin Splice Moved Aft to Sta.179 as Shown. Effective D-6747 and After i IY 18) (19) (20) (21 26t-t 1 /(25 24) (23) (22 BOTTOM VIEW 36-13-11 Figure 2-5. Fuselage and Empennage Skin Plating (Sheet 2 of 2) Revised October 27, 1961 2-9 SECTION II GENERAL INFORMATION Legend for Figure 2-6. INDEX GAGE DESCRIPTION SERIAL 1. .032 6150 D-l & after 2. .020 245-T3 D-l to D-1501 .025 245-’13 D-1501 to D-3999 .032 245-T3 D-3999 & after 3. .025 24S-T3 D-l to D-1501 .032 2024-T3 D-1501& after 4. .025 245-’13 D-l to D-1501 .032 2024-T3 D-1501 to D-4866 .040 2024-T3 D-4866 & after 5. .032 2024-T3 D-l & after 6. .016 24 STAL D-l to D-1245 .020 24 STAL D-1245 & after 7. .016 245-T3 D-l to D-1821 .020 2024-T3 D-1821& after 8. .016 24S-T3 D-l to D-1693 .020 2024-T3 D-1693 & after 9. .016 245-T3 D-l to D-1245 .020 2024-T3 I)-1245 & after 10. .032 2024-T3 D-l & after 11. .025 24S-T3 I)-l to D-1501 .032 2024-T3 D-1501 to D-4866 .040 2024-T3 D-4866 & after 12. .025 24S-T3 D-l to D-1501 .032 2024-T3 D-1501& after 13. .020 245-T3 D-l to D-1501 .025 24S-T3 D-1501 to D-3999 .032 24S-T3 D-3999 & after 14. .016 245-T3 D-l to D-1245 .020 2024-T3 D-1245 & after 15. .016 24S-T3 D-l to D-1693 .020 2024-T3 D-1693 & after 16. .016 24S-T3 D-l to D-1821 .020 2024-T3 D-1821& after 17. .016 24 STAL D-l to D-1245 .020 24 STAL D-1245 & after 18. .025 2~S-T3 D-l & after 19. .025 24S-T3 D-l & after 20. .016 245-T3 D-l & after 21. .016 2024-T3 D-l & after 22. .032 ~ 2024-T3 D-l & after 23. .020 2024-T3 D-l & after 24. .025 2~S-T3 D-l & after 25. .016 2024-T9 D-l & after 26. .016 24S-T3 D-l & after 27. .016 2024-T3 D-l & after 28. .016 24S-T3 D-l & after 29. .016 245-T3 D-l & after 30. .016 2024-T3 D-l & after 31. .025 245-T3 I)-1& after 32. .020 2024-T3 D-l & after 33. .032 2024-T3 D-l & after 2-10 ~I 1 (10) (11) (i2) (ij~ ---’---- I (7) (6) 09) Os) (17) ~s) (i~ 28~ (21 27 I 26) ~25) ~4) C23) (22) (33) (32) (31) (30) (I(j) 35-1 2-7 r Figure 2-6. Wing Skin Plating tt# TS1222-3 TS1171-1 TS1222-4 TS1171-2 TS1222-6 TS1176-1 TS1222-8 TS1176-2 50-590013 SPECIAL TOOLS TS1222-4 UPPER FORWARD WING BOLT WRENCH (9/16 TS1171-1 UPPER AFT WING NUT TORQUE WRENCH or inch hex for NAS1S0 bolts used D-l thru D-9414 or ADAPTER. TS1222-8 except D-9379) TS1176-1 or TS1222-6 UPPER FORWARD WING BOLT WRENCH (1/2 50-590013 inch hex for MS20010 bolts used interchangeable with NAS150 bolts on airplane serials D-9344 thru TS1222-4 LOWER FORWARD WING BOLT WRENCH (D-l D-9414 except D-9379). or thru D-1500). TS1222-8 TS1222-3 UPPER FORWARD WING BOLT WRENCH (5/8 inch hex for NAS152 bolts used interchangeable TS1222-3 LOWER FORWARD WING BOLT WRENCH (D- j with MS20012 and 131790-1 bolts on airplane 1501 thru D-7309). serials D-9379, D-9415 thru D-10119 except D- 10097). TS1222-4 LOWER FORWARD WING BOLT WRENCH (D- or 7310 thru D-10119 except D-10097). TS1222-4 UPPER FORWARD WING BOLT WRENCH (9/16 TS1222-8 or inch hex for MS20012 and 131790-1 bolts used TS1222-8 interchangeably with NAS152 bolts on airplane TS1171-1 LOWER FORWARD WING NUT TORQUE serials D-9379, D-9415 thru D-10119 except D- or WRENCH ADAPTER (D-l thru D-1500). 10097). TS1176-1 or TS1171-1 UPPER FORWARD WING NUT TORQUE 50-590013 or WRENCH ADAPTER (D-1 thru D-9414 except D- TS1176-1 9379). TS1171-2 LOWER FORWARD WING NUT TORQUE or or WRENCH ADAPTER (D-1501 thru D-10119 ex- 50-590013 TS1176-2 cept D-10097). TS1171-2 UPPER FORWARD WING NUT TORQUE TS1222-4 LOWER AFT WING BOLT WRENCH. or WRENCH ADAPTER (D-9379, D-9415 thru D- or TS1176-2 10119 except D-10P97). TS1222-8 TS1222-4 UPPER AFT WING BOLT WRENCH. TS1171-1 LOWER AFT WING NUT TORQUE WRENCH or or ADAPTER. TS1222-8 TS1176-1 or 50-590013 35-176 NOTE POINTING HAND DENOTES CHANGE Figure 2-7. Special Tools (Sheet 1 of 2) 2-12 815 35-660040/810-5 Elevator Check Fixture L.H. 35-660040-1/810-5 Elevator Check Fixture R.H. 35-660043-1 8 2/810 Trim Tab Jig 35-590067 Fittings 35-590006 Main Wheel Jack Differential Mechanism Adapter Neutralizer Shaft Assemblies ~ ~ 35-590064 koisting Sling 35-000001/932-5-68 Bolt 35-590076 "D-1 thru D-5725 ’35-590052 Adapter Used with 35-590076 assemblies when rigging airplanes 0-2681 and after 932-5 35000001 Jack Differential Mechanism TK1518 Jack Paint Adapter 35-590087 D-2681 and after (0-9379, D-9415 and after) ~cC~a Ct~l Q NOTE ’35-590087-9 Stop Used with 35-590087 assembly when POINTING HAND DENOTES CHANGE rigging airplanes 0-5725 and after Tow Handle 36-590015 replaces Tow Handle 35-590002 4 ´•~ ,-7~J~ , 35-590021 Tail Tie-down Assembly 45-590074 Landing Gear Tension Gage Assembly 35-590009 Throttle Retaining Nut Wrench 35-17-7A Figure 2-7. Special Tools (Sheet 2 of 2) 816 2-13 ITEM NO. LOCATION LUBRICANT INTERVAL "*DETAIL A 1 Propeller pitch control motor (I) MIL-G-23827 500 Hr. 2 Propeller actuator bearings(l) MIL-G-23827 250 Hr. 3 Propeller blade bearings (2) MIL-G-81322 250 Hr. 4 Propeller actuator mechanism (1) MIL-G-81322 250 Hr. DETAIL B Nose shock stru t (1 ) MI L-H-5 606 AR 2 Shimmy Dampener(l) MIL-H-5606 AR 3 Nose gear hinge points (2) MIL-G81322 100 Hr. 4 Nose gear linkage (3) MIL-G-81322 100 Hr. 5 Nose gear torque knee (6) MIL-G-81322 100 Hr. G "A" frame pivot points (2) MIL-G-81322 100 Hr. 7 Nose wheel bearings (2) MIL-G-81322 100 Hr. 8 Nose gear swivel (2) MIL-G-81322 100 Hr. 9 Felt pads (2) SAE No. 10 100 Hr. 10 Rod end fitting(l) MI~L-G-81322 100 Hr. DETAIL C 1 Steering mechanism linkage (3) MIL-G-8133,2 100 Hr. 2 Steering mechanism (2) MIL-G-81322 100 Hr. DETAIL D 1 Control column linkage (18) SAE No. 20 100 Hr. 2 Control column head (6) SAE No. 20 100 Hr. 3 Control column aileron link (3) SAE No. 20 100 Hr. DETAIL E I Trim tab control (1) SAE No. 20 100 Hr. DETAIL F 1 Door handle (2) SAE No. 20 100 Hr. 2 Door handle (1) SAE No. 20 100 Hr. DETAIL G Landing gear motor gear box(l) MIL-G-81322 300 H1´•. 2 Landing gear actuator gear box (I) Mobil Compound GGh 300 Hr. DETAIL H 1 Fuel unit linkage (3) SAE No. 20 100 Hr. 2 Fuelunit shaft (1) MIL-G-81322 100 Hr. DETAILI Flap motor gear box (1) MIL-G-23827 300 Hr. DETAIL J Differential control arm (2) SAE No. 20 100 Hr. 2 Differential control assembly (4) MIL-G-81322 100 Hr. DETAIL K Elevator tab reel(l) MIL-G-81322 100 Hr. 2 Elevator tab linkage (4) SAE No. 20 100 Hr. DETAIL L Flap actuator (2) MIL-L-6086 1000 Hr. Grade M DETAIL M 1 Aileron control linkage (6) SAE No. 20 100 Hr. DETAIL N 1 Main shock struts (2) MIL-H-5606 AR Hinge pts. (D-l to D-7 13 3) & retract links (8) MIL-G-81322 100 Hr. 3 Landing gear torque knee (12) M1L-G-81322 100 Hr. 4 Main wheel bearings (4) MIL-G-81322 100 Hr. 5 Landing gear up-lock roller (2) Refer to detailed LUBRICATION OF LANDING GEAR UP-LOCK ROLLERS in this section. DETAIL 0 1 Landing gear door hinge(l0) SAE No. 20 100 Hr. IL: DETA ILP 1 Control pedals (8) SAE No. 20 100 Hr. 2-’14 Bs Qeechcraft BONANZA SERIES SHOP MANUAL DETAIIA t~Z~’~ DETAILJJ83 DETAIL O ^ Y\ 4 O E F G ii I,T ~2~F i i i r ~i (L II :I: gjll DETAIL K DETAIIP ABi K DETAILB S~i~ 2 ~L~4r~X rf: RIGHT AND LEFT SIDE i~t -ir L ~b~b~ DETAIL Q s R BP O DETAILL/ N if DETAIIE i~ DETAIL H DETAIL C 9 i’ r( D14Yj TO ~Z901 I RIGnT AND LEFT SIDE ´•---,~~ ~ ii DETAILR ’´•’ D-1 THROUGH D-39S82 I ’ 03 1 DETAILF RIGHT AND LEFT SIDE DETAIIM I LI ’~""~"~ I DETAILD /i 2 DETAILI DETAIL N Except D-5058, D-5126 thru D-5156 and D-5159 RIGHT AND LEFT SIDE ZFFECTTVE SERIAL D-4866 thru D-5162, ~t~ /jl OETAILS ~c~L~3; 1 DETAIL G j:.r j "i t~jt* a 50 hours j~ 100 hours ~7.250 hours O 300 hours ~ 500 hours O As required O 10DO hours Figure 2-8. Lubrication Diagram B19 2-15 ~)eechcr~ft BONANZA SERIES SHOP MANUAL ITEM NO. LOCATION LUBRICATION INTERVAL DETAIL Q 1 Cowl flap hinges (6) SAE No. 10W/30 100 Hr. I DETAIL R 1 Engine tachometer drive adapter (1) MIL-G-81322 100 Hr. DETAIL S 1 Nose wheel door hinges (4) SAE No. 10W/30 100 Hr. DETAIL T 1 Flap flexible drive MIL-G-23827A 900 Hr. NOTES 1. MIL-G-81322 grease may be used in place of MIL-G-23827 grease in all normal climates, however in extremely cold climates, MIL-G-23827 should be used. 2. Landing gear components may require lubrication 25 or 50 hours, depending on operation. 3. Care should be exercised when using grease MIL-G-81322 and MIL-G-23827 since they contain a rust preventive which will discolor painted surfaces. 4. MIL-G-81322 grease is NOT compatible with Aeroshell #5 grease. DO NOT MIX. I X Do not overfill. When properly filled, the oil level measured on a dip stick inserted through the filler hole will be approximately 114 inch. *k Propeller lubrication is shown for the Model 215 propeller. No lubrication between overhauls is recommended for the Model 278, F12A or 2A36C23-CB propellers. () Indicates number of places to lubricate. DETAIL T Q 2-16 619 JACKING. remove the cabin door, the left front window and the front seat. Attach a sling to the front wing spar in LWARNINCI the fuselage,~ ~n~t~e, B"d a third line to the hoist fitting on The main landing gear on serial D-5791 and Ic~unoNI after and the nose landing gear on serial D-6562 and after, no longer incorporates a A spreader must be used above the cabin to rebound controlassembly. On this type gear, prevent damaging the door moulding and do not attempt to remove the torque knees, window frame. the torque knee pins or the bolt connecting the torque knees, when the airplane has been LEVE LINC. placed on jacks, without first deflating the shock absorber assembly. The torque knees On airplanes prior to D-3401 longitudinal leveling provide the extension stop for the lower holes are located in each side of the baggage door shock absorber cylinder assembly. When frame. Insert a suitable straight edge in the holes in they are disconnected the cylinder is free the baggage door and lay a spirit level on it. Adjust to slide out of the upper barrel assembly, by raising or lowering the tail so the airplane is level longitudinally. Anchor the tail to a stationary object One jack point is located on the under side of each to keep it in this position. Serials D-3401 and after forward fuselage wing attaching fitting and a third have two external screws in the bulkhead aft of the point, for use with a special jack, is located in the baggage compartment on the left side for longitudinal middle of the fuselage at the rear wing spar. This leveling. Longitudinal leveling is accomplished by third point is a threaded socket. To use, install an attaching a plumb bob and a piece of string to the eyebolt with at least 10 threads screwed into the upper screw. The airplane is level when the string socket. A special jack (figure 2-7) must then be used passes through the center of the lower screw. For which will fit the two front jack points and attach to lateral leveling, remove the front seat and lay the the eyebolt at the third point. The rear jack point pin level along the top of the front wing spar fuselage should be safetied in place. If the jack is fitted with carry through structure. Adjust the height of the casters, the airplane may be rolled in the hangar or jacks so the airplane is level laterally. on other paved surfaces as desired. When using only the two front jack points, secure the tail skid to a TOWING stationary object and place 100 pounds of sand bags on the fuselage between the stabilizers. MAIN WHEEL JACKING. IWARNINO) A wheel jack adapter is included with each aircraft I prior to aircraft serialD-9222. The adapter is On fuel injection aircraft if the engine is available as optional equipment,serials D-9222 and warm, and it is necessary to move the pro- after. Before raising the airplane, be sure the shock peller to attach the tow bar, stand clear of strut is properly inflated to the correct height. If the the area of rotation and move the propeller strut is not inflated to the recommended height it will against the normal direction of rotation. be impossible to insert the jack adapter into the main Make certain the magneto switch is off. While wheel axle. A scissor type jack is recommended for the engine is warm, residual fuel in the in- individual wheel jacking. When lowering the airplane take ports and injectors may ignite and cause caution should be exercised so the shock strut will the engine to kick. not become compressed and force the landing gear door against the jack adapter. The two lugs on the nose gear lower torque knee are used with the hand tow bar, furnished with each air- 1‘CAUT7C~~ plane, and carried in the baggage compartment. One man can move the Bonanza easily on a smooth and Do not walk on the wing walk while the air- level surface with the tow bar. plane is on the main wheel jack. HOISTMG. An improved hoisting sling assembly has been de- After moving the airplane, always remove the signed which permits hoisting without removal of the tow bar and replace it in the baggage compart´•´• left window, cabin door or engine cowling. The 35- ment. Never turn the engine over with the tow 590064-1 sling assembly uses hoist fittings which bar attached to the fork, as the propeller will attach to the upper forward wing mounting bolts and a not clear the tow bar. strap assembly installed around the propeller blade shanks. On airplanes prior to D-1501 the wing In a hangar and where movement is restricted, two mounting bolts must be reversed in order to accom- men may pivot the airplane on the main wheels; one modate the new hoist fitting. If the airplane must be man should push on the leading edge of a wing tip hoisted and the 35-590064-1 sling is not available, while the other workman lifts the nose wheel from Issued: June, 1971 2-17 SECTION Ii GENERAL INFORMATION the ground by applying his ~eig]lt on the fuselage just forward of the stabilizers. Points where pushing is permitted are the leading edge of the wing, wing tip, and the fuselage forward of the stabilizer leading Airplanes before Serial D-551 have a one- way check valve installed in the bottom of edge. the oil tank. If this check valve has not been modified and the propeller is turned ~A~FT7;0-~jl backwards, pressure may be built up in the line causing the hose connections to blow off. On these airplanes, always Do not push on the propeller or the con- check the oil line hose connections if trol surfaces. the engine kicks backwards or is turned opposite to the normal direction of rota- tion. To tow the airplane with a tractor or tug, attach the tow bar to the tow lugs on the nose gear lower torque knee. Always observe the turn limits of the STARTING THE TS1O-520-D TURBOCHARGED nose gear when making turns. Turns greater than ENGINE: these limits can cause extensive damage to the nose gear. Also, exercise care when removing the tow bar from the nose gear lower torque knee to pre- NormalStart: position the throttle half open, turn vent damage to the lubrication fittings on the land- auxiliary fuel pump switch to "High Boost". When the fuel flow reaches 8 gph, turn the auxiliary fuel ing gear. pump switch to "OFF". Reduce throttle to idle posi- tion and then engage starter, opening the throttle NOTE approximately 3 to 4 turns. Do not attempt to tow the airplane backward Hot Start: place the auxiliary fuel pump switch by the fitting in the tail skid. This tail skid momentarily to "High Boost" immediately before was designed only to protect the tail in a tail- engaging starter; after engine starts turn auxiliary low landing and to provide attachment for the fuel pump switch to "Low Boost" as needed to purge tail tie-down. vapor from the system during ground operation. STARTING ENGINE. I‘CAU~iPdN~I Generator Switch. On Alternator (Dn after englne’starts) Off Battery Switch. On Do not over-prime engine. In event of Ignition . Both flooding, place mixture in Idle-Cut-Off Radio Switch Off and operate the starter until excess fuel Cowl Flaps . .Open is removed, then repeat hot engine Mixture . Full Rich starting procedure. Propeller HI RPM Parking Brake. On Throttle . i/4 inch from closed If the auxiliary pump switch is left in the "High Boost" position with the engine-driven pump operat- On Bonanzas D-l through D-5330 operate the hand ing, an over-rich mixture and slight power loss may fuel pump to maintain 9 to 10 psi before engaging the occur. starter. Airplanes D-5331 through D-6841 are equip- ped with an electric boost pump which should be op- perated until the pressure reaches 2 to 2-1/2 psi before the starter is engaged. On airplanes D16842 When switching fuel tanks, if one tank is allowed to and after the electric boost pump should be operated run completely dry it may be necessary to turn the until the fuel flow reaches 8 gph before engaging the auxiliary fuel pump to "Low Boost" position and starter. The throttle should not be pumped in an place the mixture control to Full Rich to aid in re- effort to prime the engine. As soon as the engine is starting the engine. Close the throttle as necessary started, check the oil pressure gauge for an indic- to prevent engine overspeed on restarting. As soon ated pressure. If the gauge does not indicate pres- as the engine starts, turn the auxiliary pump switch sure within one-half minute, stop the engine and to the "OFF" position. determine the trouble. 2-18 Revised February 11, 1966 SECTION IJ GENERAL INFORMATION j~T~j On Serials D-3989 through D-4865 a parking brake control knob replaces the control handle; airplanes D-4866 and after have a flush mounting control in the When the oil temperature is in the low right subpanel. operating range apply full throttle slowly to avoid a supercharger overboost condition which may exceed the manifold pressure CONTROL LOCK. limitation of 32. 5 inches Hg. A control lock is provided for the control column and the aileron controlwheel. The lock secures the aile- TAXIING. ron control wheel in neutral and the control column in 5" down elevator position. The lock holds the throttle closed, covers the ignition switch and pre- The airplane should be taxied with the wing flaps up, vents accidental starting of the engine or attempted and the engine cowl flaps open. On airplanes prior to take-off. D-1501, the brakes may be used in turning, and on any firm surface, the airplane can be turned in the radius of