Raytheon Beechcraft Bonanza 35 Series Shop Manual Download

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Beech



Bonanza

Model

35 Series

Shop

Manual

35-590096B2

Volume 1 of 1

Summary of Contents for Beechcraft Bonanza 35 Series

Page 1: ...Beech Bonanza Model Model 35 Series 35 Series Shop Manual 35 590096B21 Volume 1 of 1...

Page 2: ...e Record of Revisions page of this manual The Highlights Page may be retained with the manual for future reference HIGHLIGHTS Volume Chapter Section Description of Change Revised format of manual 7 Ch...

Page 3: ...BONANZA 35 SERIES D 1 thru D 10119 except D 10097 Shop Manual Copyright Raytheon Aircraft Company 2003 P N 35 590096B P N 35 590096B21 Reissued November 15 1960 Revised August 29 2003...

Page 4: ......

Page 5: ...set of revision pages you desire A BONANZA 35 SERIES SHOP MANUAL LIST OF EFFECTIVE REVISIONS PART NUMBER DATE SECTIONS AFFECTED 35 590096B November 15 1960 B Reissue 35 590096B1 October 27 1961 2 4 an...

Page 6: ...A 35 SERIES SHOP MANUAL LIST OF EFFECTIVE REVISIONS Continued PART NUMBER DATE SECTIONS AFFECTED 35 590096B19 March 22 1996 2 3 4 7 and 8 35 590096B20 September 3 2001 2 and 3 35 590096B21 August 29 2...

Page 7: ...74 20B thru 20I Aug 28 87 21 and 22 May 12 78 22A and 22B Feb 10 77 23 Feb 10 77 24 Sep 27 79 SECTION PAGE DATE 25 Sep 1971 26 Sep 27 79 27 Sep 1971 28 May 12 78 3 1 Original 2 thru 2B Dec 1969 2C Au...

Page 8: ...11 66 14 Oct 22 65 15 Dec 1969 16 thru 18 Nov 29 74 6 1 May 12 78 2 Jan 1970 2A Oct 17 75 2B Nov 1 73 3 Original 4 Oct 27 61 SECTION PAGE DATE 5 thru 7 Original 8 and 8A Nov 1 73 9 Oct 27 61 10 and 11...

Page 9: ...83 and 84 Sep 1971 85 Dec 1972 86 and 86A Oct 17 75 86B and 86C Mar 7 77 87 Jan 1970 88 Mar 7 77 88A Sep 1971 89 Dec 1972 90 Sep 1971 SECTION PAGE DATE 90A Dec 1972 90B Mar 7 77 90C thru 90F Dec 1972...

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Page 455: ...feel the deicer boots on the propeller for the proper sequence of heater operation The presence of local hot spots indicate severe damage to the deicer heaters which should be repaired before more ser...

Page 456: ...If the run out over 360 degrees of rotation is over 0 005 inch or in excess of 0 002 inch in any 4 inch arc refer to Section 3 for the paragraph on slip ring alignment h Examine the brush mounting bra...

Page 457: ...lowing method 1 Remove the compressor inlet duct assembly by loosening the four clamps and removing the two boots Loosen the alternate air duct control as necessary and lower the duct 2 Inspect the co...

Page 458: ...CTION GUIDE The owner or operator is responsible for maintaining the airplane in an airworthy condition including compliance with all applicable Airworthiness Directives as specified in Part 39 of Tit...

Page 459: ...irplane has access to the previously noted documents as well as to this Inspection Guide NOTE Any time an airplane is repainted or touched up inspect all placards and decals to assure that they are no...

Page 460: ...siders compliance with these Service Bulletins mandatory OPTIONAL and or RECOMMENDED No Border Service Bulletins cover changes modifications improvements or inspections which may benefit the owner Due...

Page 461: ...g Handbook 11 POWER CHECK Refer to NORMAL PROCEDURES in the appropriate Pilot s Operating Handbook 12 AMMETER Check for proper indication and unusual fluctuations 13 HEATING AND VENTILATING SYSTEM Che...

Page 462: ...IONER Evaporative System Drain unit to remove dirt and other foreign particles from the wick box drain line and overflow line Remove wick assembly from box and flush with water Refer to AIR CONDITIONE...

Page 463: ...s Check for metal particles or foreign matter on screens and filters Check for proper torque after installation 13 OIL COOLER Check oil cooler lines and fittings for condition security chafing and lea...

Page 464: ...ration and damage Check fittings for security 29 ENGINE ACCESSORIES Check for condition security and leaks Check wiring hoses and tubes for chafing security and leaks 30 ENGINE MOUNTS Check for cracks...

Page 465: ...ected in this shop manual Check for condition mounting and proper operation Install the screen and check for security Inspect for cracks 46 VACUUM SYSTEM AIR FILTER Located forward of the instrument p...

Page 466: ...COMPARTMENT 1 SKIN Inspect skins for deformation cracks and loose or missing rivets If damage is found check adjacent structure 2 STRUCTURE Check for cracks and deformation Check for loose or missing...

Page 467: ...WINDOWS AND DOORS Inspect windows for scratches crazing and general condition Inspect doors for security of attachment Check latching mechanism for proper engagement and ease of operation Check that r...

Page 468: ...Check control cables pulleys and associated equipment for condition attachment alignment clearance and proper operation Replace cables that have more than 3 broken strands in any 3 foot length of cabl...

Page 469: ...strut and components for cracks attachment proper inflation and evidence of leakage 3 ACTUATING LINKAGE Check for wear at attach points Check for cracks and security 4 GEAR DOORS AND LINKAGE Check doo...

Page 470: ...r condition and security Determine that all clevis retaining pins are in place and secured with cotter pins 7 STRUT FLUID LEVEL Check and maintain the proper hydraulic fluid level in the struts as out...

Page 471: ...ration of the complete landing gear system 11 DYNAMIC BRAKING ACTION Verify proper operation of dynamic brake relay 12 ASSIST STEP If Installed Inspect the retractable step for cable and safety link c...

Page 472: ...for condition attachment alignment clearance and proper operation Replace cables that have more than 3 broken strands in any 3 foot length of cable or evidence of corrosion Check cables for proper te...

Page 473: ...J GENERAL 1 Airplane cleaned and serviced 2 Airplane lubricated after cleaning in accordance with this shop manual lubrication chart 3 Inspect all placards to ensure that they are easily readable and...

Page 474: ...ppage WHEN OPERATING IN AREAS OF HIGH DUST CONTENT Nose Landing Gear Shock Strut Clean off and wipe dry exposed polished surfaces Routine Instrument Air Filters Replace instrument line supply filters...

Page 475: ...for distortion deterioration and proper fit and security Every 100 hours and or annually b Brake Units 1 Check cylinders and associated lines for damage and leaks Routine 2 Check for evidence of over...

Page 476: ...tified as ready for further flight The inspections are conducted at two levels The first level consists of determining if any external damage has occurred and looking for evidence of internal structur...

Page 477: ...ilure e Check tips of propeller for damage f Check propeller spinner and backplate for evidence of interference with cowling g Inspect wheel well structure for damage or cracks Check area surrounding...

Page 478: ...inspection Landing Gear a Place airplane on jacks and check shock strut for free up and down movement b Remove tires and inspect internally for cuts or broken areas c Disassemble and examine wheels r...

Page 479: ...d wiring for proper operation Fuselage Center and Aft Section a Examine stringers frames and sidewalls for deformation structural failure b Test plumbing and wiring for proper operation c Inspect heat...

Page 480: ...egligible a close inspection of the internal supporting structure may reveal serious damage General Appearance Determine that the airframe components wings fuselage and empennage are in their normal c...

Page 481: ...age surfaces for damage and free movement c Inspect for skin wrinkles at the juncture of the fuselage and empennage SECOND LEVEL INSPECTION As required NOTE Because G loading may be transmitted along...

Page 482: ...iring d Examine the control cables pulley mountings and the cable clearance at areas the cables pass through the structure Ensure a smooth normal operation Empennage a Inspect elevator pushrods torque...

Page 483: ...ers manuals prior to returning the airplane to service following any lightning strikes or other impact damage Propeller a At times the difficulty is not in inspecting the airplane but in determining i...

Page 484: ...ting b From the point of entry the strike usually spreads aft in a series of small holes or burn marks After the points of entry and exit are found the structure between these points should be careful...

Page 485: ......

Page 486: ...onstitute a guarantee the item will reach the period without malfunction as the aforementioned factors cannot be controlled by the manufacturer Use only genuine Raytheon Aircraft Company or Raytheon A...

Page 487: ...ours Master Cylinder On condition Main Gear Assembly On condition Leaking or collapsed struts that cannot be corrected by seal replacement will constitute the On condition requirement Any pitting corr...

Page 488: ...Air Pressure Pump Airborne Pumps refer to Airborne Replacement Schedule SI 300 17 or subsequent See Supplier Data CAUTION at the end of this section Aero Accessories Pumps Part Number AA442CW replace...

Page 489: ...s first Engine Baffle Seals Replace as necessary or every 10 years of service Main Engine Fuel Pump TRW or Thompson Model TF1900 Overhaul every 900 hours Refer to TRW Service Bulletin ESD 182D or subs...

Page 490: ...ndicator On condition Attitude Gyro On condition Clock On condition Directional Gyro On condition Flap Position Indicator On condition Free Air Temperature Indicator On condition Fuel Flow Gage On con...

Page 491: ...ry four years whichever comes first Refer to TCM Service Bulletin 643 STRUCTURE Wing Attach Bolts 4 each side Replace 10 years after initial inspection or on condition Refer to Section 4 MISCELLANEOUS...

Page 492: ...Page 7 B21 Aug 29 03 Section 8 Supplier Data is subject to change Users of this manual should refer to the Parker Hannifin website www parker com airborne for the latest information regarding Parker...

Page 493: ...Beech Debonair Model Model 33 Series Shop Manual 33 590011 1C17 Volume 1 of 1...

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