ࡱ> Root Entry F@@siqCompObjnWordDocument!|ObjectPool X  !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSYZ`abcdefghijklmnopqrstuvwxyz{|}~SummaryInformation( V@Y@D7iG@PZMicrosoft Word 6.018ࡱ>  FMicrosoft Word 6.0 Document MSWordDocWord.Document.69qࡱ_Oh+'0$ H l   D h0*0*0*C:\MSOFFICE\WINWORD\NORMAL.DOT BEECHCRAFT Scott Perdue Scott Perdue@"ܥe3 ey!|**&&&&&$jLT'%jLjLjLjL(LzjLX{? O O O O O O O OPPPPPQ]R{T{6{R(& OTUi O O O O{R O&& O Oear. MechInsp40. CARBURETOR HEAT SYSTEM - Check for blockage, security, operation and wear. MechInsp41. CARBURETOR - Clean the screen and check for damage. Drain the inlet chamber and rear section. Install screen and check for leaks. Check the primer solenoid for operation and to ensure secure mounting. MechInsp42. FUEL INJECTION CONTROL VALVE - Clean the screen and check for damage. Install screen and check for leaks. MechInsp43. FUEL INJECTION SYSTEM - Inspect all fuel injection components, lines and fittings for evidence of fuel leaks, fraying and cracking. MechInsp44. OIL SEPARATOR (Vacuum System) - Clean the screen as directed in Section 3 of PEN 35-5p0096B Shop Manual (or subsequent). Check for condition, mounting and proper operation. Install the screen and check for security. Inspect for cracks. MechInsp45. VACUUM SYSTEM AIR FILTER (Located behind instrument panel) - Check for security of attachment, replace as required. MechInsp46. VACUUM RELIEF VALVE - Clean and inspect filter, check for security of attachment. MechInsp47. ELECTRIC PROPELLER DEICER - Check as follows: 1. Check for service damage to the deicer heaters, brush rods, springs and brushes. Check for attachment and security. 2. Check the lead strap and all other clamps, connectors and wiring for electrical soundness, security and attachment. 3. Check the slip rings for roughness, cracks, burned or discolored areas and for deposits of oll, grease or dirt. Check for security and attachment. 4. Check deicer boots for wrinkles, loose or torn areas. MechInsp48. TURBOCHARGER SYSTEM - Check as follows: 1. Inspect the system for oil leaks, exhaust system leaks, cracks and attachment. 2. Inspect the compressor wheel for nicks, cracks or broken blades and freedom of movement. 3. Inspect the bypass valve (wastegate) for proper operation and inspect all linkage for interference, condition, security and attachment. 4. Inspect all exhaust system components for worn or damaged areas, loose clamps, cracks and leaks. 5. Inspect lubrication system components for worn or damaged areas, loose clamps, cracks and leaks. 6. Inspect the upper deck pressure reference lines and the fuel injection reference manifold for loose connectlons, leaks and possible chafing. 7. Check and calibrate the turbine inlet temperature in accordance with Sectlon 6 of PEN 36-590001-3B Shop Manual or Chapter 77-00-00 of PEN 36-590001-9 Main tenance Mamarily respon-sible for the airworthiness of the airplane, the wrier or operator should select only qualified personnel to maintain the airplane. While this guide may be used as an outline, detailed information of the many systems and components in the airplane will be found in the various sectionsuchapters of ins shopamaintenance manual and the pertinent vendor publications. It is also recommended that reference be made to the applicable Maintenance Handbooks, previously issued Ser-vice Instructions, Beechcraft Service Bulletins, applicable FAA regulations and Publi-cations, Vendors Bulletins and Specifications for torque values, clearances, settings, tolerances, and other requirements. It is the responsibility of the owner or operator to ensure that the airframe and power plant mechanic inspecting the airplane has access to the previously noted documents as well as to this inspection guide. Beech Aircraft Corporation issues service information for the benefit of owners and operators in the form of two classes of Service Bulletins. MANOATORY (Red Border) Ser-vice Bulletins are changes, irespections or modifications that could affect safety. The factory considers compliance with these Service Bulletins mandatory OPTIONAL (No Bor-der) Service Bulletires cover changes, notifications, improvements or inspections whick may benefit the owner. One to the wide range of information covered by the OPTIONAL Ser-vice Bulletin, each owner or operator is responsible for conducting a thorough review of each Optional Service Bulletin to determine if compliance is required based on the applicability of the OPTIONAL Service Bulletin to his particular set of operating concfi-tions. In the final analysis :t is -he responsibility of the owree or operator to ensure treat all previously issued Class : and :I Service InstrlJctfons arid Beechcraft Servfce Bulle-tins which are pertirient ~o his particular operation are complied with. In addition to the inspections prescribed by this schedule, the altimeter instrument and static system and all ATC transponders MUST be tested and inspected at 24-month intervals in compli-ance with the requirements specified in FAR Part 91. A. OPERATIONAL INSPECTION 1. STARTER - Check for proper operation, unusual noises and dragging. Check starter energized light (if installed) andror load meter to ensure starter disengagement when the starter switch is released. 2. FUEL PRESSURE - Check for proper fuel pressure limits and fluctuations. 3. CYLINDER HEAD TEMPERATURE - Check for proper operation, j temperature and fluctuations. Page 2 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) OPERATIONAL INSPECTION (Contd) ALTERNATOR / GENERATOR - Check for proper output and unusual noises. STANDBY GENERATOR - Check for proper operation in test mode. Perform a functional test as outlined in Chapter 24-31-00 of the Bonanza Series Maintenanoe Manual. Check wiring for security and condition. STANDBY INSTRUMENT AIR (Airplane serials E-2164 and after, and EA-422 and after) - Check for proper operation. Check plumbing and wiring for security and condition. PROPELLER OPERATION - Cyole propeller and oheok for i proper rpm drop and smoothness of operation. 8. PROPELLER DEIGER - Cheok for proper operation and f amperage draw on ammeter. 3. OIL PRESSURE AND TEMPERATURE - Gheok for proper pees- i sure, temperature limits and unusual fluctuations. MAGNETOS - Cheok the performance of the magneto as out-lined under the heading NORMAL PROLEDURES in the appro-priate Pilots Operating Handbook. ; 11. POWER OHEvK - Refer to NORMAL PROGEDURES in the appro-priate Pilots Operating Handbook. j 12. AMMETER - Cheok for proper indication and unusual fluo- f +ll=+innt i 13. HEATING AND VENTILATING SYSTEM - Gheok for proper opera- 1 lion, heat and airflow output. Gheok controls for free-dam of operation. Page 3 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) A. OPERATIONAL Inspection (Contd) MechInsp14. FIREWALL SHUTOFF VALVE - Check for proper operation and freedom of movement. MechInsp15. IDLE RPM AND MIXTURE SETTINGS - Cheok for both proper rpm and mixture settings. Cheok controls for freedom of operation. MechInsp16. IDLE CUT-OFF - Cheok for proper operation and freedom of movement. MechInsp 17. IGNITION SWITCH - Rotate the ignition switch through the OFF position to the extreme limit of switch travel if the engine stops firing, the switch is normal. If the engine continues to run with the switch held in the past OFF position, it is an indication that one magneto is still hot or ungrounded. When the switch is released from the past OFF position, it should automatically return to normal OFF and the engine should stop running. However, any ignition switch exhibiting this abnormal condition should be replaced. MechInsp 18. ALL ENGINE CONTROLS - With the engine running, oheok for proper operational limits, engine response and rigging. Cheok friction looks for proper operation. MechInsp 19. FUEL OUANTITY GAGES - Cheok for proper operation and unusual fluctuations. MechInsp 20. AUXILIARY FUEL PUMP - Cheok pump for proper operation, unusual noise and fluctuations. MechInsp 21. FUEL TANK SELECTOR - Cheok for proper operation and feel for positive detent and proper placarding. MechInsp 22. ALL LIGHTS - Cheok for condition, attachment, cracked or broken lenses. Cheek switches, knobs and circuit break-ers for looseness and operation. MechInsp Page 4 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) A. OPERATIONAL INSPECTION (Contd) 23. STALL WARNING SYSTEM - Check for proper operation. MechInsp 24. RAOIO OPERATION - Check for proper operation, security of switches and knobs. MechInsp 25 FLAPS - Check for noisy operation, full travel and prop-er indication. MechInsp 26. PITOT HEAT - Check amperage draw on ammeter and for proper heating of the unit. MechInsp 27. FLIGHT INSTRUMENTS - Check for condition and proper operation. MechInsp 28. BRAKES - Check for condition and wear, ease of operation and proper release of the parking brake. Check for gnu suet brake chatter. MechInsp 29. EMERGENCY LOCATOR TRANSMITTER - Check for proper opera-lion and assure that the ELT fs armed when the airplane is returned to service. MechInsp 30. AIR CONDITIONER - Operate the alr conditioner and verify that the retractable condenser moves to the ground extended position when turned on and returns to the retracted position when turned off. Check for proper operation and unusual noise. MechInsp 31. OXYGEN SYSTEM - Functfonally check the oxygen system for proper operation. Check the oxygen bottle shutoff valve for proper operation. MechInsp 32. SWITCHES, CIRCUIT BREAKERS - Check for proper operation. MechInsp Page 5 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION (INCLUDES TURBOCHARGED AIRPLANES) A. OPERATIONAL INSPECTION (Contd) 33. FLIGHT CONTROLS, TRIM CONTROLS AND TRIM INDICATOR -Check freedom of movement and proper operation through full travel with and without flaps extended. Check electric trim controls for operation. MechInsp 1. COWLING SKIN - Check for deformation and obvious damage or cracks. Check for loose or missing rivets. MechInsp 2. COWLING STRUCTURE - Check for cracks and deformation. Check for loose or missing rivets and concealed damage. MechInsp 3. COWLING - Check for condition, security and adjustment of latches. Open the upper cowling and clean. Inspect for cracks. MechInsp 4. COWL FLAPS - Check for travel, deformation and security. Inspect for cracks. MechInsp S. SPARK PLUGS - Clean, inspect, regap, test and replace as necessary. Tighten spark plugs to proper torque and check lgnltlon harness condition and for proper attach-merit. MechInsp 6. COMPRESSION - Perform differential compression test. MechInsp 7. BATTERY - Inspect for clean, tight connections and add distilled water to maintain a level of 3/8 inch above the top of the separators. Inspect the vents and over-flow tube for obstructions. Check for security and proper attachment. Check for corrosion. Make certain the battery is clean. Water or dirt on battery surfaces can cause the battery to discharge. MechInsp 8. PLUMBING - Inspect plumbing and associated accessories for condition touch as cracks) and attachment. Check plumbing clearance and secure against possible chafing. MechInsp _ Page 6 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) 8. POWER PLANT (Contd) g. BRAKE FLUIO RESERVOIR - Check reservoir for security, attachment, open vent, proper fluid level and for leaks. MechInsp 10. ENGINE OIL TANK OR SUMP - Check for cracks, leaks, prop-er fluid level, deformation and security. MechInsp 11. CRANKCASE - Check security of crankcase half bolts. MechInsp 12. OIL SUMP DRAINS ANO SCREENS - Clean screens, check for holes in the screens and for obstructions. Check for proper torque after fnstallatlon. MechInsp 13. OIL COOLER - Check oll cooler, lines and fittings for condition, security, chafing and leaks. MechInsp 14. PROPELLER AND MOUNTING BOLTS - Check for condition and security. Check the tip of the blades for evidence of lightning strikes. If there is evidence of lightning strikes, consult the propeller manufacturer, the engine manufacturer, and Beech Afrcraft Corporation. Inspect the blades for cracks, dents, nicks, scratches, erosion, corrosion, security and movement in the hub. MechInsp 18. PROPELLER SPINNER - Check for deformation, security and cracks. MechInsp 16. PROPELLER HUB - Check for cracks, excessively leaking seals and condition. MechInsp 17. ALTERNATORIGENERATOR - Check for condition and attach-merit. Check wiring for proper attachment and possible chafing. Check for unusual noise. MechInsp Page 7 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) 8. POWER PLANT (Contd) MECH INSP MechInsp 18. ALTERNATOR - Remove and disassemble the alternator as necessary to inspect the rotor shaft bearings for condo ton and replace ff necessary. For Prestolfte only, refer to BEECHCRAFT Service Bulletfn 0546-389 RevoII or subsequent. MechInsp 19. STARTER - Check for condition, attachment and chafed or loose wires. MechInsp 20. GENERATOREALTERNATOR BELT - Check for proper tension and worn or frayed condition. Check tension adjustment bolt for tightness. MechInsp 21. STANOBY GENERATOR - Check for condition, attachment, security of wires and for chafing. MechInsp 22. MAGNETOS - Cheok contact points for proper clearance. Points with deep pits or excessively burned areas must be discarded. Inspect the cam follower felt pad for proper lubrication and clean the compartment with a clean, dry cloth. Check ignition harness for proper connection, security and fraying. Check timing. MechInsp 23. MAGNETO PRESSURIZATION FILTER - Check for condition, cleanliness and security. MechInsp 24. CYLINOERS AN0 BAFFLES - Check cylinders and exhaust man-ifold for obvious leaks, security and cracks check baffles for cracks and security. Check cylinders for broken cooling ffns and loose or missing base nuts. MechInsp 2i. EXHAUST SYSTEM - Check for deformation, security, cracks, leaks, loose or missing nuts and clamps. Check for thin wall condition which may occur due to normal internal erosion on stacks which have long service tfme. MechInsp 26. FIREWALL - Check for wrinkles, damage or cracks. Check all electrical and control access holes for proper seal-trig. MechInsp Page B of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) 1 8. POWER PLANT (Contd) 27. HOSE ANO OUCTS - Check all fuel, oft and aft hose or duct for leakage, cracks, deterforatfon and damage. Check ffttfngs for security. MechInsp 28. ENGINE ACCESSORIES - Check for condftfon, security and leaks. Check wfrfng, hoses and tubes for chafing, sect city and leaks. MechInsp 29. ENGINE MOUNTS - Check for cracks, corrosion and secure ty. Inspect rubber cushions, mount bolts and nuts and grounding straps for condftfon and security. MechInsp 30. CABIN HEATER SYSTEM - Check for cracks, dfstortfon, cor-roslon, leaks and obstructions per Section 3 of PEN 35-5900968 Shop Manual, Sectfon 10 of PEN 36-590001-38 Shop Manual or Chapter 21-40-00 of PEN 36-590001-9 Mafn-tenance Manual (or subsequent). MechInsp 31. PROPELLER GOVERNOR - Check for leaks and control arm fnr security. MechInsp 32. ENGINE CONTROLS - Check controls and associated equip-merit for condftfon, attachment, alignment and rfggfng. MechInsp 33. IGNITION HARNESS - Inspect for fraying and attachment. MechInsp 34. ELECTRICAL WIRING ANO EQUIPMENT - Inspect electrical wfrfng and associated equipment and accessories for fraying and attachment. MechInsp 35. ALL DRAINS AND PLUGS - Check for condition, security and obstructions. Check for leaks and correct tightness. MechInsp 36. PRESSURE PUMP INTAKE FILTER - Inspect fflter for condo lion, cleanliness and security. Check filter container for cracks. MechInsp Page 9 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE ( INCLUDES TURBOCHARGED AIRPLANES) 8. POWER PLANT (Contd) 37. AIR CONDITIONER COMPRESSOR - Check for security and attachment. Check refrigerant and oil levels. Check belt for tension and worn or frayed condition. (See Section 2 and 3 of PEN 35-5900g68 Shop Manual, Section 2 and 10 of PEN 36-590001-38 Shop Manual or Chapters 12-10-00 and 21-50-00 of PEN 36-590001-9, or subsequent, Maintenance Manual). MechInsp 38. INOUCTION AIR FILTER - Cheok for oonditfon, oleanlfness and security. MechInsp 39. INDUCTION SYSTEM AND ALTERNATE AIR - Check the hot and cold flexible air ducts for delamination of the inner lining. Check the alternate aft valve for blockage, security, cracks, operation and wear. MechInsp 40. CARBURETOR HEAT SYSTEM - Check for blockage, security, operation and wear. MechInsp 41. CARBURETOR - Clean the screen and check for damage. Orafn the inlet chamber and rear section. Install screen and check for leaks. Check the primer solenofc for operation and to ensure secure mounting. MechInsp 42. FUEL INJECTION CONTROL VALVE - Clean the screen and check for damage. Install screen and check for leaks. MechInsp 43. FUEL INJECTION SYSTEM - Inspect all fuel fnjectfon com-portents, lines and ffttlngs for evidence of fuel leaks, fraying and cracking. MechInsp 44. OIL SEPARATOR (Vacuum System) - Clean the screen as directed in Sectfon 3 of PEN 35-5g00968 Shop Manual (or subsequent). Check for condition, mounting and proper operation. Install the screen and check for security. Inspect for cracks. MechInsp Page 10 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) 8. POWER PLANT (Contd) 45. VACUUM SYSTEM AIR FILTER (Located behind instrument pan-el) - Check for security of attachment, replace as required. MechInsp 46. VACUUM RELIEF VALVE - Clean and inspect filter, check for security of attachment. MechInsp 47. ELECTRIC PROPELLER DEICER - Check as follows: 1. Check for service damage to the defcer heaters, brush rods, springs and brushes. Check for attach-merit and security. 2. Check the lead strap and all other clamps, conned tors and wlrfng for electrical soundness, security and attachment. 3. Check the slip rfngs for roughness, cracks, burned or discolored areas and for deposits of oll, grease or dirt. Check for security and attachment. 4. Check deicer boots for wrinkles, loose or tar.. areas. MechInsp Page 11 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 lOD-HO UR O R ANN UAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHA RGED AIRPLANES) 8. POWER PLANT (Contd) 48. TURBOCHARGER SYSTEM - Check as follows: 1. Inspect the system for oll leaks, exhaust sys leaks, cracks and attachment. 2. Inspect the compressor wheel for nicks, cracks or broken blades and freedom of movement. 3. Inspect the by-pass valve (wastegaie) for proper operation and inspect all linkage for interference, condition, security and attachment. 4. Inspect all exhaust system components for worn or damaged areas, loose clamps, cracks and leaks. 5. Inspect lubrication system components for worn or damaged areas, loose clamps, cracks and leaks. 6. Inspect the upper deck pressure reference lines and the fuel injection reference manifold for loose con-nectlons, leaks and possible chafing. 7. Check and calibrate the turbine inlet temperature in accordance with Sectlon 6 of PEN 36-590001-38 Shop Manual or Chapter 77-00-00 of PEN 36-590001-9 Main tenance Manual (or subsequent). 8. Check manifold pressure controller llnkaae for wear. MechInsp C. CABIN AND BAGGAGE COMPARTMENT 1. SKIN - Inspect skins for deformation, cracks and loose or missing rivets. If damage is found, check adjacent structure. MechInsp 2. STRUCTURE - Check for cracks and deformation. Check for loose or missing rivets and concealed damage. MechInsp 3. CABLES AND PULLEYS - Check the flight control camps nents, cables and pulleys. Replace control system camps nents (push rods, turn buckles, end fittings, castings, etc.) that have bulges, splits, bends, or cracks. Check control cables, pulleys, and associated equipment for condftlon, attachment, alignment, clearance and proper operation. Replace cables that have broken strands or evidence of corrosion. Check cables for proper tension at the first inspection and every 100-hours thereafter. MechInsp Page 12 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) C. CABIN ANO BAGGAGE COMPARTMENT (Contd) 4. AILERON QUADRANT (Del through D-1500) - Inspect for con-titian, attachment and proper operation such as binding. MechInsp 5. LANDING GEAR GEARBOX AND ACTUATING LINKAGE - Check for leakage, wear, condition and attachment. Check for gnu suet noise. Check oil level by engaging and turning the emergency hand crank turn to determine that oil is being picked up on the worm gear. The oil level should be maintained no more than necessary to cover of the diameter of the worm gear. MechInsp 6. FLAP MOTOR ANO SHAFTS - Check for condition, security and wear at all points. Check cable housing for secure ty and check jam nuts for tightness. MechInsp 7. AUXILIARY FUEL PUMP AND FUEL LINES - Check for condo lion, security and leaks. Check lines for signs of chafing or cracks. MechInsp 8. BRAKE MASTER CYLINDER AND PARKING BRAKE VALVE - Check for condition, security and leaks. Check lines for signs of chafing or cracks. MechInsp g. RUDDER PEDALS - Check for freedom of movement. Check cables, pushapull rods, bell cranks, pulleys, turnbucklestand fair leads for proper routing, condition and security. Check rudder pedal fore and aft positions for wear. Check locks and pins to ensure positive lock. MechInsp 10. CONTROL COLUMN, TRIM CONTROL AND INDICATOR (Electric and Manual) - Check for freedom of movement. Inspect pulleys, sprockets, bearings, actuators, chains and turn buckles for condition, security and operation. Check trim indicator for proper indication. MechInsp 11. ENGINE CONTROLS - Check for ease of operation through full travel. Check friction locks for proper operation. MechInsp Page 13 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) C. CABIN AND BAGGAGE COMPARTMENT (Contd) 12. ELECTRICAL WIRING AND EOUIPMENT - Check for condition, security and signs of chafing. MechInsp 13. PLUMBING - Check all plumbing and connections for sect city, leakage and general condition. MechInsp 14. WINDOWS AND DOORS - Inspect windows for scratches, crazing and general condition. Inspect doors for sect city of attachment. Check latching mechanism for proper engagement and ease of operation. MechInsp 15. INSTRUMENTS AND INSTRUMENT PANEL - Inspect instrument panel, sub panels, placards and instruments for condition and attachment. Check all knobs for security. Inspect shock mounts, ground straps for cracks and security. MechInsp 16. SEATS, SEAT BELTS AND SHOULDER HARNESSES - Inspect cabin seats, seat belts and shoulder harnesses for proper operation, condition and security of attachment. Inspect floorboards for condition and seat attachment. Check for operation of the seat stops. MechInsp 17. OXYGEN SYSTEM - Check condition of the oxygen system and check the oxygen masks for cleanliness and stowage. MechInsp 18. VENTILATING SYSTEM - Check all fresh air and heat outlet vents for proper movement and operation. MechInsp 19. FUEL SELECTOR VALVE - Inspect for leakage, security, freedom of movement, proper detent feel and condition. Clean strainers and inspect for condition. Check for proper placarding. MechInsp Page 14 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) C. CABIN AND BAGGAGE COMPARTMENT (Contd) 20. FILTERS - Inspect pressure system lnllne filter for con-Dillon, cleanliness and security. Replace pressure sys-tem lnllne filter and all other lndlvldual instrument air filters andror time change master filter on vacuum system airplanes in accordance with the Servlce Chart in Sectlon B of PEN 35-5900968 Shop Manual, the Servlce Chart in Sectlon 2 of PEN 36-590001-38 Shop Manual or the Overhaul And Replacement Schedule in Chapter 5-10-00 of PEN 36-590001-9 (or subsequent) Malntenance Manual. MechInsp 21. EMERGENCY EXIT HATCH - Check emergency release handle and latch assembly for proper operation. Check that the hatch moves out freely. Check the complete latch assem-big for condition and all movlno parts for proper opera-lion. With the hatch installed, check for proper latching and seal. Resafety the emergency exit with .020 inch diameter copper wire after opening. MechInsp 22. STATIC SYSTEM - Check and drain water from the static lines. MechInsp D. WINGS AND CARRY-THROUGH STRUCTURE 1. SKIN - Check for deformation and obvious damage. Check for cracks, loose or missing rivets. If damage is found, check adjacent structure. Check for lndlcatlons of hard landing or excessive flight loading. MechInsp 2. STRUCTURE - Check for cracks, deformation and concealed damage. Check for loose or missing rivets. MechInsp 3. ACCESS DOORS AND PANELS - Inspect for cracks, proper fit and attachment. MechInsp Page 15 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) D. WINGS AND CARRY-THROUGH STRUCTURE (Contd) 4. CABLES, PULLEYS AND TURNBUCKLES - Check the wing flight control components, cables and pulleys. Replace control system components (push rods, turn buckles, end ffttfngs, castings, etc.) that have bulges, splfts, bends, or cracks. Check control cables, pulleys, and associated equipment for condftfon, attachment, alignment, clear-ance, and proper operation. Replace cables that have broken strands or evidence of corrosion. Check cables for proper tension at the first fnspectfon and every lDD-hours thereafter. MechInsp 5. AILERONS - Check for condftfon and security. Check for cracks, loose or mfssfng rivets and freedom of movement. Check hinge bearings and brackets for condftfon, push-pull rods for security and rod ends for corrosion. MechInsp 6. FUEL TANKS, CAPS AND VENTS - Inspect fuel tank vent lfnes and ffller caps as directed fn Sectfon 3 of PEN 3i-5900968 Shop Manual, Sectfon B of PEN 36-590001-38 Shop Manual or Chapter 28-20-00 of PEN 36-i90001-9 (or subsequent) Mafntenance Manual. MechInsp 7. PLUMBING - Check for leakage, chafing, condftfon and security. MechInsp 8. ELECTRICAL WIRING AND EQUIPMENT - Inspect for chafing. damage, security and attachment. MechInsp 9. FLAP LIMIT SWITCHES - Check for condftfon and security. freedom of operation. MechInsp ID. FLAPS AND ACTUATORS - Check for condftfon, security, blndfng or chafing of actuator cables. Check flap skin and structure for cracks, loose or mfssfng rivets. Check roller bearings and tracks for condftfon. Check stop area for condftfon and damage. MechInsp 11. FLAP POSITION TRANSMITTER - Check for security and oper-atfon. MechInsp Page 16 of 25 BEECHC RAFT BONANZA 33, 35 AN D 36 lOO-HO UR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) D. WINGS AND CARRY-THROUGH STRUCTURE (Contd) 12. WING SPAR CAP - Inspect the wing spar cap for corrosion as outlined fn Sectfon 4 of PEN 35-i900968 Shop Manual, Sectfon 3 of PEN 36-590001-38 Shop Manual or Chapter 57-00-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. MechInsp 13. WING 80LTS - Check wing bolts for proper torque at the first 100-Hour fnspectfon and at the first 100-Hour fnspectfon after each refnstallatfon of the wing attach bolts. Refer to Sectfon 4 of PEN 35-5900968 Shop Manual, Sectfon 3 of PEN 36-590D01-38 Shop Manual or Chapter 57-00-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual for wing bolt, nut and ffttfng fnspectfon crate Ron and frequency. MechInsp 14. RADAR ANTENNA COVER - Check the fiberglass for security, attachment and cracks. MechInsp 15. FUEL VENTS, AIR INLETS, PITOT TUBE AND STALL WARNING VANE - Check for condftfon and obstructions. MechInsp 16. DRAIN PORTS - Check the drafn ports fn the upper wing attach ffttfngs to assure they are open and free of obstruction. MechInsp E. NOSE GEAR 1. WHEEL AND TIRE - Check wheel for cracks and tfre for wear, damage, condftfon and proper fnflatfon. Check wheel bearings for condftfon and wear. MechInsp 2. LANDING GEAR STRUT - Inspect the shock strut and camps nents for cracks, attachment, proper fnflatfon and evf-dence of leakage. MechInsp 3. ACTUATING LINKAGE - Check for wear at attach points. Check for cracks and security. MechInsp Page 17 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) E. NOSE GEAR (Contd) 4. GEAR DOORS AND LINKAGE - Check doors for damage and cracks to the structure and skins. Check linkage for wear and cracks at the attach points. Check for condo ton and security. MechInsp 5. NOSE GEAR STEERING LINKAGE - Inspect linkages for tightness, condftfon and security and linkage boots for condftfon. MechInsp 6. SHIMMY DAMPER - Check for condftfon and attachment. Check attach points for cracks. Check flufd level per the Shop/ Mafntenance Manual. MechInsp 7. STRUT FLUID LEVEL - Check and mafntafn the proper hydraulic flufd level fn the strut as outlined fn See ton 2 of of PEN 35-5900968 and PEN 36-590001-38 Shop Manuals and fn Chapter 12-20-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. MechInsp 8. STRUT AND A-FRAME HINGE 80LTS - Inspect for cracks and security of attachment. MechInsp 9. STATIC CABLE (If installed) - Inspect for condftfon and proper clearances and attachment. MechInsp 10. VISUAL INDICATDR - Check for condftfon. MechInsp F. MAIN GEAR AND BRAKES 1. BRAKES, LINES, LINING AND DISCS - Check for condftfon, wear and security. Check lfnes for chafing and signs of leakage or cracks. Check discs for wear or warping. Check brake discs for cracks. MechInsp 2. WHEELS AND TIRES - Check wheels for cracks and tfres for wear, damage, condftfon and proper fnflatfon. Check wheel bearings for condftfon and wear. MechInsp Page 18 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) F. MAIN GEAR AND BRAKES (Contd) 3. ACTUATOR GEARBOX, MOTOR AND SWITCHES - Check for leakage, condftfon and security. MechInsp 4. LANDING GEAR STRUTS - Inspect the shock struts and com-portents for cracks, attachment, proper fnflatfon and evidence of leakage. MechInsp 5. ACTUATING LINKAGE - Check for wear and cracks at attach points. Check for condftfon and security. MechInsp 6. GEAR DOORS AND LINKAGE - Check doors for damage and cracks to the structure and skins. Check linkage for wear and cracks at the attach points. Check for condo ton and security. Determine that all clefs retafnfng pfns are fn place and secured with cotter pfns. MechInsp 7. STRUT FLUID LEVEL - Check and mafntafn the proper hydraulic flufd level fn the struts as outlined fn See lion 2 of PEN 35-59D0968 and PEN 36-590001-38 Shop Manu-als and fn Chapter 12-20-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. MechInsp 8. STRUT AND A-FRAME HINGE 80LTS - Inspect for cracks and security of attachment. MechInsp Page 19 of 25 BEECHCRAFT BONANZA 33, 35 and 36 100-HOUR OR ANNUAL LONG FORM fNSPECTlON GUIDE (INCLUDES TURBOCHARGED AIRPLANES) G. MAIN GEAR OPERATION Sfnce battery voltage fs not sufffcfent to properly cycle the landing gear for thfs fnspectfon, use only an external power source capable of delfverfnq and mafntafnfng either 14.25 t .25 or 28.25 + .25 VDC (according to the afrplanes electrical system throughout the extension and retraction eye es when per-forming the landing gear retraction fnspectfon. For more specfffc fnformatfon which may be necessary to accomplish the following ftems, refer to Sectfon 5 of PEN 35-5900968 Shop Manual, Sectfon 5 of PEN 36-590001-38 Shop Manual or Chapter 32 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. 1. DOORS - Check door operation, fft and fate. Check Fe unusual nofse. MechInsp 2. POSITION LIGHTS - Check for security, adjustment, wfrfng for breaks, condftfon of fnsulatfon, loose connections and proper fndfcatfon. MechInsp 3. WARNING HORN - Check for proper operation. MechInsp 4. UPLOCK CABLE TENSION - Check unlock cable mechanism for condltfon and security. Check unlock cable for proper tension and for possible fraying. MechInsp 5. EMERGENCY EXTENSION - Check system for freedom of opera-ton and posftfve engagement of the down locks. Check for unusual nofse. MechInsp 6. DOWNLOCK TENSION - Check for proper deflection force on the main gear knee joints. MechInsp Page 20 of 25 BEECHCRAFT BONANZA 33, 35 AND 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE ( INCLUDES TURBOCHARGED AIRPLANES) G. MAIN GEAR OPERATION (Contd) 7. UPLOCK ROLLERS - Check condftfon and clearance of unlock rollers and lubricate as fndfcated fn the appropriate Shop/ Mafntenance Manual. Check for bfndfng. MechInsp 8. LIMIT SWITCH RIGGING - Check for security and proper adjustment of the lfmft swftches. Refer to the ShopaMafntenance Manual for correct landing gear gearbox internal clearance. MechInsp 9. SAFETY SWITCH - Check for security, proper rfg and oper-atfon. MechInsp 10. GENERAL OPERATION - Place the airplane on jacks and cycle the landing gear whfle checking to ascertain that the posftfon light swftches operate fn condunctfon with the posftfon of the landing gear. Check the condftfon and operation of complete landing gear system. MechInsp 11. DYNAMIC BRAKING ACTION - Verffy proper operation of dynamic braking action (12-volt system) and dynamic brake relay (24-volt system). MechInsp 12. ASSIST STEP (If Installed) - Inspect the retractable step for cable and safety lfnk condftfon, proper adjust-merit and operation. Check ffxed lfnk condftfon, proper adjustment and operation. Check ffxed steps for secure ty. MechInsp Page 21 of 25 BEECHCRAFT BONANZA 33, 35 and 36 lOO-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) H. NOSE GEAR OPERATION Sfnce the battery voltage fs not sufffcfent to properly cycle the landing gear for thfs fnspectfon, use only an external power source capable of delfverfng and mafntafnfng either 14.25 _ .25 or 28.25 _ .25 VDC (according to the afrplanes electrical system) throughout the extension and retraction cycles when per-forming the landing gear retraction fnspectfon. For more specfffc fnformatfon which may be necessary to accomplish the following ftems, refer to Sectfon 5 of PEN 35-5900968 Shop Manual Sectfon 5 of PEN 36-590001-38 Shop Manual or Chapter 32 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. 1. DOORS - Check door operation, fft and fate. Check for 1 unusual nofse. MechInsp 2. NOSE GEAR UP TENSION - Check the up tension on the nose gear as fndfcated fn the appropriate ShopaMafntenance Manual. MechInsp 3. DOWNLOCK TENSION - Check the down lock tension on the nose gear as fndfcated fn the appropriate ShopaMafntenance Manual. MechInsp 4. GENERAL OPERATION - Place the airplane on jacks and cycle the landing gear whfle checking to ascertain that the posftfon light swftches operate fn conjunction with the landing gear posftfon. Check the condftfon and operation of the complete landing gear system. MechInsp 5. VISUAL INDICATOR - Inspect for proper adjustment a operation. MechInsp 6. NOSE GEAR STEERING - Check for condftfon and security. MechInsp Page 22 of 25 BEECHCRAFT BONANZA 33, 35 and 36 lOO-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) _ I. REAR FUSELAGE AND EMPENNAGE 1. SKIN - Check for deformation, cracks and obvious damage. Check for loose or mfssfng rivets. If damage fs found, check adjacent structure. MechInsp 2. INTERNAL FUSELAGE STRUCTURE - Check for cracks and deformation. Check for loose and mfssfng rivets. Check bulkheads, door posts, strfngers and doublers for cores soon, cracks and buckles. MechInsp 3. STRUCTURE - Inspect the two most aft bulkheads for cracks, dfstortfon, loose rivets or other obvious dam-age. MechInsp 4. CABLES, PULLEYS AND TURNBUCKLES - Check the elevator and rudder flight control components, cables and pulleys. Replace control system components (push rods, turn buckles, end ffttfngs, castings, etc.) that have bulges, splfts, bends, or cracks. Check control cables, pulleys, and associated equipment for condftfon, attach-merit, alignment, clearance, and proper operation. Replace cables that have broken strands or evidence of corrosion. Check cables for proper tension at the first fnspectfon and every 100-Hours thereafter. MechInsp 5. CONTROL SURFACES - Check for deformation, cracks, sect rfty, freedom of movement and travel lfmfts. Check for loose or mfssfng rivets. Check for security of hinges and bond cable. Check the inboard elevator hinge casting (on the aft bulkhead) for cracks fn mounting bolt holes. MechInsp 6. TRIM TABS AND ACTUATORS - Check for security and wear. Check allowable free play per Sectfon 3 of PEN 35-5900968 and PEN 36-590001-38 Shop Manuals and per Chapter 27-30-00 of PEN 36-590001-9 (or subsequentRoot Entry F@]q\CompObjnWordDocument!|ObjectPool X  !"#$%&'()*+,-./0123456789:;<=>?@ABCDEFGHIJKLMNOPQRSVYZ[^`abcdefghijklmnopqrstuvwxyz{|}~SummaryInformation( nual (or subsequent). 8. Check manifold pressure controller linkage for wear. MechInspC. CABIN AND BAGGAGE COMPARTMENT 1. SKIN - Inspect skins for deformation, cracks and loose or missing rivets. If damage is found, check adjacent structure. MechInsp2. STRUCTURE - Check for cracks and deformation. Check for loose or missing rivets and concealed damage. MechInsp3. CABLES AND PULLEYS - Check the flight control components, cables and pulleys. Replace control system components (push rods, turn buckles, end fittings, castings, etc.) that have bulges, splits, bends, or cracks. Check control cables, pulleys, and associated equipment for condition, attachment, alignment, clearance and proper operation. Replace cables that have broken strands or evidence of corrosion. Check cables for proper tension at the first inspection and every 100-hours thereafter. MechInsp4. AILERON QUADRANT (D-l through D-1500) - Inspect for condition, attachment and proper operation such as binding. MechInsp5. LANDING GEAR GEARBOX AND ACTUATING LINKAGE - Check for leakage, wear, condition and attachment. Check for unusual noise. Check oil level by engaging and turning the emergency hand crank turn to determine that oil is being picked up on the worm gear. The oil level should be maintained no more than necessary to cover of the diameter of the worm gear. MechInsp6. FLAP MOTOR AND SHAFTS - Check for condition, security and wear at all points. 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MechInsp7. AUXILIARY FUEL PUMP AND FUEL LINES - Check for condition, security and leaks. Check lines for signs of chafing or cracks. MechInsp8. BRAKE MASTER CYLINDER AND PARKING BRAKE VALVE - Check for condition, security and leaks. Check lines for signs of chafing or cracks. MechInsp9. RUDDER PEDALS - Check for freedom of movement. Check cables, push/pull rods, bell cranks, pulleys, turnbuckles and fairleads for propeILM[^rsv˦>?Pڧܧ0wyӨר!"30 \_RS}ʪ5<OShs|˫̫ݫ-.Tg !j#$'¬(Ŭ)̬*+./2MNqO_`acdntx̭ح߭9Mf{خ $0234Ey{Ưʯͯί߯  Y[@CDU GJQl`aró=?Z`ewyմִ wx  ߵ123456 8(9*:mpqO P TUɶVضYZ [\G]K^U_Y`[ab$' ( 9 < D    ظ  * +/Q[iuxyιѹٹ  !r*+,/0,1.0 \_r routing, condition and security. Check rudder pedal fore and aft positions for wear. Check locks and pins to ensure positive lock. MechInsp10. CONTROL COLUMN, TRIM CONTROL AND INDICATOR (Electric and Manual) - Check for freedom of movement. Inspect pulleys, sprockets, bearings, actuators, chains and turn buckles for condition, security and operation. Check trim indicator for proper indication. MechInsp 11. ENGINE CONTROLS - Check for ease of operation through full trav2:3I4u5w67ĻŻ8ֻ9 ;)<M=O_`>? ADde01fBijkϽ loZp`q_bX[ j G      -=> O    7 8 0; ? @ A B C G T U V W &f *,-g ?k Yl [jkm | p s v     # ' Mkl }      % 1 V b       )*:?Times New Roman Symbol &Arial 1Courier"hd m !6 BEECHCRAFT Scott Perdue Scott Perdueࡱ> TWU     123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ]^_`abcdefghijklmnopqrstuvwxyz{|}~]ܥe3 ey!|**&&&&&$jLT'%jLjLjLjL(LzjLX{? O O O O O O O OPPPPPQ]R{T{6{R(& OTUi O O O O{R O&& O O O O O O& O& OP$&n&&&&& OP O OBEECHCRAFT BONANZA 33, 35 and 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) Reissued: March,1985 _____________________________________ ____________________________________________________ OWNERS NAME O O O O& O& OP$&n&&&&& OP O OBEECHCRAFT BONANZA 33, 35 and 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) Reissued: March,1985 _____________________________________ ____________________________________________________ OWNERS NAME ADDRESS STATE ZIP _________________________ ________________ ____________ _______________________________ lDENTlFlCATlON NUMBER SERIAL NUMBER HOURS DATE INSPECTION COMPLETED _____________________________________ _____________________________________________________ SERVICING AGENCY ADDRESS STATE ZIP The time periods for the inspections noted in this schedule are ~ased on gnment, clearance, and proper operation. Replace cables that have broken strands or evidence of corrosion. Check cables for proper tension at the first fnspectfon and every 100-Hours thereafter. MechInsp5. CONTROL SURFACES - Check for deformation, cracks, sect rfty, freedom of movement and travel lfmfts. Check for loose or mfssfng rivets. Check for security of hinges and bond cable. Check the inboard elevator hinge casting (on the aft bulkhead) for cracks fn mounting bolt holes. MechInsp6. TRIM TABS AND ACTUATORS - Check for security and wear. Check allowable free play per Sectfon 3 of PEN 35-5900968 and PEN 36-590001-38 Shop Manuals and per Chapter 27-30-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. Check hinges and trfm tab actuator for security and wear. Check trfm tabs for cracks and control rods for attachment. Lubricate trfm tab hinges per Sectfon 2 of PEN 35-5900968 Shop Manual, Sectfon 2 of PEN 36-590001-38 Shop Manual or Chapter 12-20-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. MechInsp7. STATIC PORTS - Check for obstruction and clean as nPrP<- MechInsp Page 23 of 25 I. REAR FUSELAGE AND EMPENNAGE (Contd) 8. PLUMBING - Check for leakage, cracks, chafing, condftfon and security. MechInsp9. ELECTRICAL WIRING AND EQUIPMENT - Inspect for chafing, damage, security and attachment. MechInsp10. STATIC LINES - Check condftfon of static lfnes and drafn. MechInsp11. ASSIST STEP BUNGEE - Inspect for condftfon and attach-merit. MechInsp12. ANTENNAS - Check for condftfon and security MechInspJ. GENERAL 1. Airplane cleaned and serviced. MechInsp2. Airplane lubricated, after cleaning, fn accordance with the appropriate ShopaMafntenance Manual lubrfcatfon chart and BEECHCRAFT Safety Communfque No. 57 dated June 3, 1981. MechInsp3. Inspect all placards to assure that they are easily readable and securely attached. MechInsp4. Assure that all afrworthfness Dfrectfves, BEECHCRAFT Servfce Bulletfns and previously issued Servfce Instructfons are reviewed and complied with as required. MechInsp5. For a complete or annual fnspectfon of the airplane, all ftems on the airplane that are noted fn thfs guide should be inspected. MechInsp Page 24 of 25 BONANZA 33, 35 and 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) Page 25 of 25  15. :<=P?@TU̟͟ !%&'+./01234569:;<=>?@ABEFGHILMNOPQRSTUVWYZ[\|}~UcuUb666;;~<<>>+@ADDGHHIIIIJJJJJJJKK KK0*0*0*0*0*lT  !%l  !%Z \ KKKKlKqKvKwKxKyKzKKKKKKKKLLLLLLL`MeMjMkMlMmMnMMMMMMMl  !%lT  !%%norms: usage under average environmental conditions. Airplanes operated in humid tropics, or in cold, damp climates, etc., may need more freauerat inspections for wear, corrosion, lubrication, andror lack of maintenance. Under these adverse conditions, perform per:-odic inspections in compliance with this guide at more frequent intervals until the own-er or operator can set his own inspection periods based or. the contingencies of ffed experience. Airplanes operated less than 100 hours a year must have a 100-Hour Inspection performed no later than 12 months following the date of the precediP; 100-Hour Inspection. The 100-hour interval between performance of the procedures speci-fied herein should NEVER be exceeded by more than 10 rourselAkich can be usec only if the additional time is required to reach a place where the inscectior can be satisfac40riy accomplished. :Jeowever, any extension of a 100-koJr interval mJst be subtra~-ed ffcm the following 100-hour iraterval, with no time extension, permitted. ror example, if a~ inspection is done at 110 hours, the next inspection. is due 90 hours later wiFP. no exper-sion allowed. Ascertain that all placards are in place and legible whenever the airplane has been repainted or touched up after repairs. Replace any placards that have been inadvertently defaced or removed. NOTE Beech Aircrafts Recommended Inspection Program in accordance with FAR Parts 43 and 91 consists of, but is not limited to, inspection items listed in this Inspection Buide, any applica-ble Airworthiness Directives issued against the airframe or any equipment installed therein, conformity to Type Certificate Data Sheet and Maintenance Manual Airworthiness Limitations Ohapter (Chapter 4) as applicable. The owner or operator is primarily responsible for maintaining the airplane in an airworthy condition, including compliance with all applicable Airworthiness OirectiJes as specified in Part 39 of the Federal Aviation Regulations. It is further the respon-sibility of the owner or operator to ensure that the airplane is inspected in conformity with the requirements of Parts 43 and 91 of the Federal Aviation Regulations. Beech Aircraft corporation has prepared this inspection guide to assist the owner or operator in meeting the foregoing responsibilities. This inspection guide is not intended to be all-inclusive, for no such guide can replace the good judgment of a certified airframe and power plant mechanic in the performance of his duties. As the one priiiiBiBi7. ecessary. 8. leakage, cracks, chafing, condii9. 10. iiii11. pect for condition and attachn12. iiJ. 1. 2. e lubricated, after cleaning, i/iiii3. 4. iiness Diiiiii 5. iiiii dddddeeeeeeeeeeYf^fdfefgffffffggggg#h(h.h/h1h2h"i'i-i.i0ijj ADDRESS STATE ZIP _________________________ ________________ ____________ _______________________________ lDENTlFlCATlON NUMBER SERIAL NUMBER HOURS DATE INSPECTION COMPLETED _____________________________________ _____________________________________________________ SERVICING AGENCY ADDRESS STATE ZIP The time periods for the inspections noted in this schedule are ~ased on norms: usage under average environmental conditions. Airplanes operated in humid tropics, or in cold, damp climates, etc., may need more freauerat inspections for wear, corrosion, lubrication, andror lack of maintenance. Under these adverse conditions, perform per:-odic inspections in compliance with this guide at more frequent intervals until the own-er or operator can set his own inspection periods based or. the contingencies of ffed experience. Airplanes operated less than 100 hours a year must have a 100-Hour Inspection performed no later than 12 months following the date of the precediP; 100-Hour Inspection. The 100-hour interval between performance of the procedures speci-fied herein should NEVER be exceeded by more than 10 rourselAkich can be usec only if the additional time is required to reach a place where the inscectior can be satisfac40riy accomplished. :Jeowever, any extension of a 100-koJr interval mJst be subtra~-ed ffcm the following 100-hour iraterval, with no time extension, permitted. ror example, if a~ inspection is done at 110 hours, the next inspection. is due 90 hours later wiFP. no exper-sion allowed. Ascertain that all placards are in place and legible whenever the airplane has been repainted or touched up after repairs. Replace any placards that have been inadvertently defaced or removed. NOTE Beech Aircrafts Recommended Inspection Program in accordance with FAR Parts 43 and 91 consists of, but is not limited to, inspection items listed in this Inspection Buide, any applica-ble Airworthiness Directives issued against the airframe or any equipment installed therein, conformity to Type Certificate Data Sheet and Maintenance Manual Airworthiness Limitations Ohapter (Chapter 4) as applicable. The owner or operator is primarily responsible for maintaining the airplane in an airworthy condition, including compliance with all applicable Airworthiness OirectiJes as specified in Part 39 of the Federal Aviation Regulations. It is further the respon-sibility of the owner or operator to ensure that the airplane is inspected in conformity with the requirements of Parts 43 and 91 of the Federal Aviation Regulations. Beech Aircraft corporation has prepared this inspection guide to assist the owner or operator in meeting the foregoing responsibilities. This inspection guide is not intended to be all-inclusive, for no such guide can replace the good judgment of a certified airframe and power plant mechanic in the performance of his duties. As the one pri>CHIJKL0*0*0*0*0*0*0*0*0*0*0*@ 3"T xl  !%lT  !% $)*+,--2789:;kpuvwxy0*0*0*0*0*0*0*lT  !%l  !%%ylqvwxyz*/456780*0*0*0*0*0*0*lT  !%l  !%%89:;<JKLMc!5                   0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*Z07 {T x%L WARNING VANE - Check for condii16. iiittiE. iiiiiii2. ooiii ii5. iiii6. iiii iiiiicioBBi36-590001-9 (or subsequent) Mai ii10. ii iili2. iiiiiii3. ii nii5. ii ttach points. Check for condiiviiniii iin the proper hydraulic fluiiict0BBi36-590001-9 (or subsequent) Mai8. BG. NOTE Siiiciiiiiingiiniirplanes electrical system) and retraction cycles when perming the landing gear iiiiiiiiBiBi1. iirforis2. iiiiiiindii3. 4. ii iiii6. 7. iiiiiiii8. ii /i9. ii10. iiiiel. Check friction locks for proper operation. MechInsp12. ELECTRICAL WIRING AND EOUIPMENT - Check for condition, security and signs of chafing. MechInsp13. PLUMBING - Check all plumbing and connections for security, leakage and general condition. MechInsp14. 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. MechInsp15. INSTRUMENTS AND INSTRUMENT PANEL - Inspect instrument panel, sub panels, placards and instruments for condition and attachment. Check all knobs for security. Inspect shock mounts, ground straps for cracks and security. MechInsp16. SEATS, SEAT BELTS AND SHOULDER HARNESSES - Inspect cabin seats, seat belts and shoulder harnesses for proper operation, condition and security of attachment. Inspect floorboards for condition and seat attachment. Check for operation of the seat stops. MechInsp17. OXYGEN SYSTEM - Check condition of the oxygen system and check the oxygen masks for cleanliness and stowage. MechInsp18. VENTILATING SYSTEM - Check all fresh air and heat outlet vents for proper movement and operation. MechInsp19. FUEL SELECTOR VALVE - Inspect for leakage, security, freedom of movement, proper detent feel and condition. Clean strainers and inspect for condition. Check for proper placarding. MechInsp20. FILTERS - Inspect pressure system inline filter for condition, cleanliness and security. Replace pressure system inline filter and all other individual instrument air filters and/or time change master filter on vacuum system airplanes in accordance with the Servlce Chart in Sectlon B of PEN 35-590096B Shop Manual, the Servlce Chart in Sectlon 2 of PEN 36-590001-3B Shop Manual or the Overhaul And Replacement Schedule in Chapter 5-10-00 of PEN 36-590001-9 (or subsequent) Malntenance Manual. MechInsp21. EMERGENCY EXIT HATCH - Check emergency release handle and latch assembly for proper operation. Check that the hatch moves out freely. Check the complete latch assembly for condition and all moving parts for proper operation. With the hatch installed, check for proper latching and seal. Resafety the emergency exit with .020 inch diameter copper wire after opening. MechInsp22. STATIC SYSTEM - Check and drain water from the static lines. MechInspD. WINGS AND CARRY-THROUGH STRUCTURE 1. SKIN - Check for deformation and obvious damage. Check for cracks, loose or missing rivets. If damage is found, check adjacent structure. Check for indications of hard landing or excessive flight loading. MechInsp2. STRUCTURE - Check for cracks, deformation and concealed damage. Check for loose or missing rivets. MechInsp3. ACCESS DOORS AND PANELS - Inspect for cracks, proper fit and attachment. MechInsp4. CABLES, PULLEYS AND TURNBUCKLES - Check the wing flight control components, cables and pulleys. Replace control system components (push rods, turn buckles, end fittings, castings, etc.) that have bulges, splits, bends, or cracks. Check control cables, pulleys, and associated equipment for condition, attachment, alignment, clearance, and proper operation. Replace cables that have broken strands or evidence of corrosion. Check cables for proper tension at the first inspection and every l00-hours thereafter. MechInsp5. AILERONS - Check for condition and security. Check for cracks, loose or missing rivets and freedom of movement. Check hinge bearings and brackets for condition, push-pull rods for security and rod ends for corrosion. MechInsp6. FUEL TANKS, CAPS AND VENTS - Inspect fuel tank vent lines and filler caps as directed in Sectfon 3 of PEN 35-590096B Shop Manual, Section B of PEN 36-590001-3B Shop Manual or Chapter 28-20-00 of PEN 36-590001-9 (or subsequent) Maintenance Manual. MechInsp7. PLUMBING - Check for leakage, chafing, condition and security. MechInsp8. ELECTRICAL WIRING AND EQUIPMENT - Inspect for chafing, damage, security and attachment. MechInsp9. FLAP LIMIT SWITCHES - Check for condition and security, freedom of operation. MechInsp10. FLAPS AND ACTUATORS - Check for condition, security, binding or chafing of actuator cables. Check flap skin and structure for cracks, loose or missing rivets. Check roller bearings and tracks for condition. Check stop area for condition and damage. MechInsp11. FLAP POSITION TRANSMITTER - Check for security and operation. MechInsp 12. WING SPAR CAP - Inspect the wing spar cap for corrosion as outlined fn Sectfon 4 of PEN 35-i900968 Shop Manual, Sectfon 3 of PEN 36-590001-38 Shop Manual or Chapter 57-00-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. MechInsp13. WING 80LTS - Check wing bolts for proper torque at the first 100-Hour fnspectfon and at the first 100-Hour fnspectfon after each refnstallatfon of the wing attach bolts. Refer to Sectfon 4 of PEN 35-5900968 Shop Manual, Sectfon 3 of PEN 36-590D01-38 Shop Manual or Chapter 57-00-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual for wing bolt, nut and ffttfng fnspectfon crate Ron and frequency. MechInsp14. RADAR ANTENNA COVER - Check the fiberglass for security, attachment and cracks. MechInsp15. FUEL VENTS, AIR INLETS, PITOT TUBE AND STALL WARNING VANE - Check for condftfon and obstructions. MechInsp16. DRAIN PORTS - Check the drafn por) Mafntenance Manual. Check hinges and trfm tab actuator for security and wear. Check trfm tabs for cracks and control rods for attachment. Lubricate trfm tab hinges per Sectfon 2 of PEN 35-5900968 Shop Manual, Sectfon 2 of PEN 36-590001-38 Shop Manual or Chapter 12-20-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. MechInsp 7. STATIC PORTS - Check for obstruction and clean as nPrP<- MechInsp Page 23 of 25 BEECHCRAFT BONANZA 33, 35 AN D 36 100-H OUR O R ANN UAL LONG FO RM INSPECTION GUIDE (IN CLUDES TURBOCHARGED AIRPLANES) _ I. REAR FUSELAGE AND EMPENNAGE (Contd) 8. PLUMBING - Check for leakage, cracks, chafing, condftfon and security. MechInsp 9. ELECTRICAL WIRING AND EQUIPMENT - Inspect for chafing, damage, security and attachment. MechInsp 10. STATIC LINES - Check condftfon of static lfnes and drafn. MechInsp 11. ASSIST STEP BUNGEE - Inspect for condftfon and attach-merit. MechInsp 12. ANTENNAS - Check for condftfon and security MechInsp J. GENERAL 1. Airplane cleaned and serviced. MechInsp 2. Airplane lubricated, after cleaning, fn accordance with the appropriate ShopaMafntenance Manual lubrfcatfon chart and BEECHCRAFT Safety Communfque No. 57 dated June 3, 1981. MechInsp 3. Inspect all placards to assure that they are easily readable and securely attached. MechInsp 4. Assure that all afrworthfness Dfrectfves, BEECHCRAFT Servfce Bulletfns and previously issued Servfce Instructfons are reviewed and complied with as required. MechInsp 5. For a complete or annual fnspectfon of the airplane, all ftems on the airplane that are noted fn thfs guide should be inspected. MechInsp Page 24 of 25 BONANZA 33, 35 and 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) Page 25 of 25 MechInspMechInspMechInsp MechInspSMechInspMech qW X kl.<0<QR`uu¡:y§çǧȧɧ˧̧Чѧէ֧ק٧ڧۧߧ,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,u]cUU]c ` !Oq-./f Z _ 0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0* 0*0*0*0*K0*0*0*0*0*0*0*0*0*0*Z8 \ Z Z $:;<IJUk$_d0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*0*.> VV%  ! L Q V W X Y Z =!B!G!H!I!J!K!!!!!!!!!0*0*0*0*0*0*0*0*0*lT  !%l  !%$      !"#$%&'()*+,-./[123456789:;<=>?@ABCDEFGHIJKLMNOPQRSTUVWXYZ]^jklopq           7 8 ; ? @ A B C G T U V W f g k l m p s v                                  Ucu^         0*0*0*0*0*0*0*0*       &:.T5Q=kEPWajqaz΀*VSeR;~o  T , Lyx !q./f`e NSYZ\BGMNP %+,.@EKLN       !!"!(!)!+!!!!!!!" " " """""""""""H#M#S#T#V######$ $$$$\$a$g$h$j$$$$$%%%%%%&&&&&&&;'@'F'G'I''''''h(m(s(t(v(((((((r)w)})~))** * **_*d*j*k*m*+$+*+++-+e+j+p+q+s+,,,,,-----,.1.7.8.:...........//////0 0 0 01111111111F2K2Q2R2T22222233333D4I4O4P4R444444F5K5Q5R5T566666 777777788888888w9|9999::#:$:&::::::Y;^;d;e;g;k<p<v<w<y<<<<<<@=E=K=L=N=O=P=Q======(>->3>4>6>>>>>>7?CDCECGCCCCCCSDXD^D_DaD]EbEhEiEkEts fn the upper wing attach ffttfngs to assure they are open and free of obstruction. MechInspE. NOSE GEAR 1. WHEEL AND TIRE - Check wheel for cracks and tfre for wear, damage, condftfon and proper fnflatfon. Check wheel bearings for condftfon and wear. MechInsp2. LANDING GEAR STRUT - Inspect the shock strut and camps nents for cracks, attachment, proper fnflatfon and evf-dence of leakage. MechInsp3. ACTUATING LINKAGE - Check for wear at attach points. Check for cracks and security. MechInspge 17 of 25 E. NOSE GEAR (Contd) 4. GEAR DOORS AND LINKAGE - Check doors for damage and cracks to the structure and skins. Check linkage for wear and cracks at the attach points. Check for condo ton and security. MechInsp5. NOSE GEAR STEERING LINKAGE - Inspect linkages for tightness, condftfon and security and linkage boots for condftfon. MechInsp6. SHIMMY DAMPER - Check for condftfon and attachment. Check attach points for cracks. Check flufd level per the Shop/ Mafntenance Manual. MechInsp7. STRUT FLUID LEVEL - Check and mafntafn the proper hydraulic flufd level fn the strut as outlined fn See ton 2 of of PEN 35-5900968 and PEN 36-590001-38 Shop Manuals and fn Chapter 12-20-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. MechInsp8. STRUT AND A-FRAME HINGE 80LTS - Inspect for cracks and security of attachment. MechInsp9. STATIC CABLE (If installed) - Inspect for condftfon and proper clearances and attachment. MechInsp10. VISUAL INDICATDR - Check for condftfon. MechInspF. MAIN GEAR AND BRAKES 1. BRAKES, LINES, LINING AND DISCS - Check for condftfon, wear and security. Check lfnes for chafing and signs of leakage or cracks. Check discs for wear or warping. Check brake discs for cracks. MechInsp2. WHEELS AND TIRES - Check wheels for cracks and tfres for wear, damage, condftfon and proper fnflatfon. Check wheel bearings for condftfon and wear. MechInsp Page 18 of 25 F. MAIN GEAR AND BRAKES (Contd) 3. ACTUATOR GEARBOX, MOTOR AND SWITCHES - Check for leakage, condftfon and security. MechInsp4. LANDING GEAR STRUTS - Inspect the shock struts and com-portents for cracks, attachment, proper fnflatfon and evidence of leakage. MechInsp5. ACTUATING LINKAGE - Check for wear and cracks at attach points. Check for condftfon and security. MechInsp6. GEAR DOORS AND LINKAGE - Check doors for damage and cracks to the structure and skins. Check linkage for wear and cracks at the attach points. Check for condo ton and security. Determine that all clefs retafnfng pfns are fn place and secured with cotter pfns. MechInsp7. STRUT FLUID LEVEL - Check and mafntafn the proper hydraulic flufd level fn the struts as outlined fn See lion 2 of PEN 35-59D0968 and PEN 36-590001-38 Shop Manu-als and fn Chapter 12-20-00 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. MechInsp8. STRUT AND A-FRAME HINGE 80LTS - Inspect for cracks and security of attachment. MechInsp Page 19 of 25 G. MAIN GEAR OPERATION Sfnce battery voltage fs not sufffcfent to properly cycle the landing gear for thfs fnspectfon, use only an external power source capable of delfverfnq and mafntafnfng either 14.25 t .25 or 28.25 + .25 VDC (according to the afrplanes electrical system throughout the extension and retraction eye es when per-forming the landing gear retraction fnspectfon. For more specfffc fnformatfon which may be necessary to accomplish the following ftems, refer to Sectfon 5 of PEN 35-5900968 Shop Manual, Sectfon 5 of PEN 36-590001-38 Shop Manual or Chapter 32 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. 1. DOORS - Check door operation, fft and fate. Check Fe unusual nofse. MechInsp2. POSITION LIGHTS - Check for security, adjustment, wfrfng for breaks, condftfon of fnsulatfon, loose connections and proper fndfcatfon. MechInsp3. WARNING HORN - Check for proper operation. MechInsp4. UPLOCK CABLE TENSION - Check unlock cable mechanism for condltfon and security. Check unlock cable for proper tension and for possible fraying. MechInsp5. EMERGENCY EXTENSION - Check system for freedom of opera-ton and posftfve engagement of the down locks. Check for unusual nofse. MechInsp6. DOWNLOCK TENSION - Check for proper deflection force on the main gear knee joints. MechInsp Page 20 of 25 G. MAIN GEAR OPERATION (Contd) 7. UPLOCK ROLLERS - Check condftfon and clearance of unlock rollers and lubricate as fndfcated fn the appropriate Shop/ Mafntenance Manual. Check for bfndfng. MechInsp8. LIMIT SWITCH RIGGING - Check for security and proper adjustment of the lfmft swftches. Refer to the ShopaMafntenance Manual for correct landing gear gearbox internal clearance. MechInsp9. SAFETY SWITCH - Check for security, proper rfg and oper-atfon. MechInsp10. GENERAL OPERATION - Place the airplane on jacks and cycle the landing gear whfle checking to ascertain that the posftfon light swftches operate fn condunctfon with the posftfon of the landing gear. Check the condftfon and operation of complete landing gear system. MechInsp11. DYNAMIC BRAKING ACTION - Verffy proper operation of dynamic braking action (12-volt system) and dynamic brake relay (24-volt system). MechInsp12. ASSIST STEP (If Installed) - Inspect the retractable step for cable and safety lfnk condftfon, proper adjust-merit and operation. Check ffxed lfnk condftfon, proper adjustment and operation. Check ffxed steps for secure ty. MechInsp Page 21 of 25 H. NOSE GEAR OPERATION Sfnce the battery voltage fs not sufffcfent to properly cycle the landing gear for thfs fnspectfon, use only an external power source capable of delfverfng and mafntafnfng either 14.25 _ .25 or 28.25 _ .25 VDC (according to the afrplanes electrical system) throughout the extension and retraction cycles when per-forming the landing gear retraction fnspectfon. For more specfffc fnformatfon which may be necessary to accomplish the following ftems, refer to Sectfon 5 of PEN 35-5900968 Shop Manual Sectfon 5 of PEN 36-590001-38 Shop Manual or Chapter 32 of PEN 36-590001-9 (or subsequent) Mafntenance Manual. 1. DOORS - Check door operation, fft and fate. Check for 1 unusual nofse. MechInsp2. NOSE GEAR UP TENSION - Check the up tension on the nose gear as fndfcated fn the appropriate ShopaMafntenance Manual. MechInsp3. DOWNLOCK TENSION - Check the down lock tension on the nose gear as fndfcated fn the appropriate ShopaMafntenance Manual. MechInsp4. GENERAL OPERATION - Place the airplane on jacks and cycle the landing gear whfle checking to ascertain that the posftfon light swftches operate fn conjunction with the landing gear posftfon. Check the condftfon and operation of the complete landing gear system. MechInsp5. VISUAL INDICATOR - Inspect for proper adjustment a operation. MechInsp6. NOSE GEAR STEERING - Check for condftfon and security. MechInsp Page 22 of 25 I. REAR FUSELAGE AND EMPENNAGE 1. SKIN - Check for deformation, cracks and obvious damage. Check for loose or mfssfng rivets. If damage fs found, check adjacent structure. MechInsp2. INTERNAL FUSELAGE STRUCTURE - Check for cracks and deformation. Check for loose and mfssfng rivets. Check bulkheads, door posts, strfngers and doublers for cores soon, cracks and buckles. MechInsp3. STRUCTURE - Inspect the two most aft bulkheads for cracks, dfstortfon, loose rivets or other obvious dam-age. MechInsp4. CABLES, PULLEYS AND TURNBUCKLES - Check the elevator and rudder flight control components, cables and pulleys. Replace control system components (push rods, turn buckles, end ffttfngs, castings, etc.) that have bulges, splfts, bends, or cracks. 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Heading 1 < U]ck,@, Heading 2 < UV]c(@( Heading 3 <Uc*@* Heading 4 <UVc"A@"Default Paragraph Font/@Listh2@List 23@List 384@"List 4$D@2$ List Continuehx&E@B&List Continue 2x&F@R&List Continue 38x*>@b*Title < U]c kB@r Body Textx&C@&Body Text Indenthx&J@&Subtitle<V]cInspMechInspMechInspMechInspMechInspMechInsp MechInspMechInspons noted in this schedule are bimates, etc., may need more freqnr, corrosion, lubrication, and icommercially ngormance of the procedures specih which can be usedtorillyH hour interval mucte,,,,,,,,,,,,----- - -A-a-------------.44444 4 4 4 4 44444)444;;;}<<z={=HHIIIIJJJJ\\\}ۓ#$&'ߛV]Ucc]cUcU]cU]]UU]c uX,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,l  !%lT  !%&,,,,,,,,---- - - 4)4?4m444444 5K5L5M55666660*0*0*0*0*0*0*0*0*0*0*0*0*Z Z ZlT  !%l  !% ronteFnthG Dvmarily responone BEECHCRAFT BONANZA 33, 35 and 36 100-HOUR OR ANNUAL LONG FORM INSPECTION GUIDE (INCLUDES TURBOCHARGED AIRPLANES) Reissued: March,1985 _____________________________________ ____________________________________________________ OWNERS NAME ADDRESS STATE ZIP _________________________ ________________ ____________ _______________________________ lDENTlFlCATlON NUMBER SERIAL NUMBER HOURS DATE INSPECTION COMPLETED _____________________________________ _____________________________________________________ SERVICING AGENCY ADDRESS STATE ZIP The time periods for the inspections noted in this schedule are based on norms: usage under average environmental conditions. Airplanes operated in humid tropics, or in cold, damp climates, etc., may need more frequent inspections for wear, corrosion, lubrication, and or lack of maintenance. Under these adverse conditions, perform periodic inspections in compliance with this guide at more frequent intervals until the owner or operator can set his own inspection periods based or the contingencies of ffed experience. Airplanes operated commercially less than 100 hours a year must have a 100-Hour Inspection performed no later than 12 months following the date of the preceding 100-Hour Inspection. The 100-hour interval between performance of the procedures specified herein should NEVER be exceeded by more than 10 hours which can be used only if the additional time is required to reach a place where the inscectior can be satisfactorilly accomplished. However, any extension of a 100 hour interval must be subtracted from the following 100-hour interval, with no time extension, permitted. For example, if an inspection is done at 110 hours, the next inspection. is due 90 hours later with no extension allowed. NOTE Ascertain that all placards are in place and legible whenever the airplane has been repainted or touched up after repairs. Replace any placards that have been inadvertently defaced or removed. NOTE Beech Aircrafts Recommended Inspection Program in accordance with FAR Parts 43 and 91 consists of, but is not limited to, inspection items listed in this Inspection Guide, any applicable Airworthiness Directives issued against the airframe or any equipment installed therein, conformity to Type Certificate Data Sheet and Maintenance Manual Airworthiness Limitations Ohapter (Chapter 4) as applicable. The owner or operator is primarily responsible for maintaining the airplane in an airworthy condition, including compliance with all applicable Airworthiness Directives as specified in Part 39 of the Federal Aviation Regulations. It is further the respon-sibility of the owner or operator to ensure that the airplane is inspected in conformity with the requirements of Parts 43 and 91 of the Federal Aviation Regulations. Beech Aircraft corporation has prepared this inspection guide to assist the owner or operator in meeting the foregoing responsibilities. This inspection guide is not intended to be all-inclusive, for no such guide can replace the good judgment of a certified airframe and power plant mechanic in the performance of his duties. As the one primarily responsible for the airworthiness of the airplane, the owner or operator should select only qualified personnel to maintain the airplane. While this guide may be used as an outline, detailed information of the many systems and components in the airplane will be found in the various section chapters of ins shopamaintenance manual and the pertinent vendor publications. It is also recommended that reference be made to the applicable Maintenance Handbooks, previously issued Ser-vice Instructions, Beechcraft Service Bulletins, applicable FAA regulations and Publi-cations, Vendors Bulletins and Specifications for torque values, clearances, settings, tolerances, and other requirements. It is the responsibility of the owner or operator to ensure that the airframe and power plant mechanic inspecting the airplane has access to the previously noted documents as well as to this inspection guide. Beech Aircraft Corporation issues service information for the benefit of owners and operators in the form of two classes of Service Bulletins. MANDATORY (Red Border) Service Bulletins are changes, inespections or modifications that could affect safety. The factory considers compliance with these Service Bulletins mandatory. OPTIONAL (No Border) Service Bulletins cover changes, notifications, improvements or inspections which may benefit the owner. Due to the wide range of information covered by the OPTIONAL Service Bulletin, each owner or operator is responsible for conducting a thorough review of each Optional Service Bulletin to determine if compliance is required based on the applicability of the OPTIONAL Service Bulletin to his particular set of operating conditions. In the final analysis it is the responsibility of the owner or operator to ensure that all previously issued Class I and II Service Instructions arid Beechcraft Service Bulletins which are pertirient to his particular operation are complied with. NOTE In addition to the inspections prescribed by this schedule, the altimeter instrument and static system and all ATC transponders MUST be tested and inspected at 24-month intervals in compli-ance with the requirements specified in FAR Part 91. A. OPERATIONAL INSPECTION 1. STARTER - Check for proper operation, unusual noises and dragging. Check starter energized light (if installed) and/or load meter to ensure starter disengagement when the starter switch is released. MechInsp2. FUEL PRESSURE - Check for proper fuel pressure limits and fluctuations. MechInsp3. CYLINDER HEAD TEMPERATURE - Check for proper operation, temperature and fluctuations. MechInsp4. ALTERNATOR / GENERATOR - Check for proper output and unusual noises. MechInsp5. STANDBY GENERATOR - Check for proper operation in test mode. Perform a functional test as outlined in Chapter 24-31-00 of the Bonanza Series Maintenanoe Manual. Check wiring for security and condition. MechInsp6. STANDBY INSTRUMENT AIR (Airplane serials E-2164 and after, and EA-422 and after) - Check for proper operation. Check plumbing and wiring for security and condition. MechInsp7. PROPELLER OPERATION - Cycle propeller and check for proper rpm drop and smoothness of operation. MechInsp8. PROPELLER DEICER - Check for proper operation and amperage draw on ammeter. MechInsp9. OIL PRESSURE AND TEMPERATURE - Check for proper pressure, temperature limits and unusual fluctuations. MechInsp10. MAGNETOS - Check the performance of the magneto as outlined under the heading NORMAL PROLEDURES in the appro-priate Pilots Operating Handbook. MechInsp11. POWER CHECK - Refer to NORMAL PROCEDURES in the appropriate Pilots Operating Handbook. MechInsp12. AMMETER - Check for proper indication and unusual fluctuations. MechInsp13. HEATING AND VENTILATING SYSTEM - Check for proper operation, heat and airflow output. Check controls for freedom of operation. MechInsp14. FIREWALL SHUTOFF VALVE - Check for proper operation and freedom of movement. MechInsp15. IDLE RPM AND MIXTURE SETTINGS - Check for both proper rpm and mixture settings. Check controls for freedom of operation. MechInsp16. IDLE CUT-OFF - Check for proper operation and freedom of movement. MechInsp17. IGNITION SWITCH - Rotate the ignition switch through the OFF position to the extreme limit of switch travel if the engine stops firing, the switch is normal. If the engine continues to run with the switch held in the past OFF position, it is an indication that one magneto is still hot or ungrounded. When the switch is released from the past OFF position, it should automatically return to normal OFF and the engine should stop running. However, any ignition switch exhibiting this abnormal condition should be replaced. MechInsp18. ALL ENGINE CONTROLS - With the engine running, check for proper operational limits, engine response and rigging. Check friction locks for proper operation. MechInsp19. FUEL OUANTITY GAGES - Check for proper operation and unusual fluctuations. MechInsp20. AUXILIARY FUEL PUMP - Check pump for proper operation, unusual noise and fluctuations. MechInsp21. FUEL TANK SELECTOR - Check for proper operation and feel for positive detent and proper placarding. MechInsp22. ALL LIGHTS - Check for condition, attachment, cracked or broken lenses. Check switches, knobs and circuit breakers for looseness and operation. MechInsp23. STALL WARNING SYSTEM - Check for proper operation. MechInsp24. RADIO OPERATION - Check for proper operation, security of switches and knobs. MechInsp25 FLAPS - Check for noisy operation, full travel and proper indication. MechInsp26. PITOT HEAT - Check amperage draw on ammeter and for proper heating of the unit. MechInsp27. FLIGHT INSTRUMENTS - Check for condition and proper operation. MechInsp28. BRAKES - Check for condition and wear, ease of operation and proper release of the parking brake. Check for unusual brake chatter. MechInsp29. EMERGENCY LOCATOR TRANSMITTER - Check for proper operation and assure that the ELT is armed when the airplane is returned to service. MechInsp30. AIR CONDITIONER - Operate the air conditioner and verify that the retractable condenser moves to the ground extended position when turned on and returns to the retracted position when turned off. Check for proper operation and unusual noise. MechInsp31. OXYGEN SYSTEM - Functfonally check the oxygen system for proper operation. Check the oxygen bottle shutoff valve for proper operation. MechInsp32. SWITCHES, CIRCUIT BREAKERS - Check for proper operation. MechInsp33. FLIGHT CONTROLS, TRIM CONTROLS AND TRIM INDICATOR -Check freedom of movement and proper operation through full travel with and without flaps extended. Check electric trim controls for operation. MechInspB. POWER PLANT 1. COWLING SKIN - Check for deformation and obvious damage or cracks. Check for loose or missing rivets. MechInsp2. COWLING STRUCTURE - Check for cracks and deformation. Check for loose or missing rivets and concealed damage. MechInsp3. COWLING - Check for condition, security and adjustment of latches. Open the upper cowling and clean. Inspect for cracks. MechInsp4. COWL FLAPS - Check for travel, deformation and security. Inspect for cracks. MechInsp5. SPARK PLUGS - Clean, inspect, regap, test and replace as necessary. Tighten spark plugs to proper torque and check ignition harness condition and for proper attachment. MechInsp6. COMPRESSION - Perform differential compression test. MechInsp7. BATTERY - Inspect for clean, tight connections and add distilled water to maintain a level of 3/8 inch above the top of the separators. Inspect the vents and overflow tube for obstructions. Check for security and proper attachment. Check for corrosion. Make certain the battery is clean. Water or dirt on battery surfaces can cause the battery to discharge. MechInsp8. PLUMBING - Inspect plumbing and associated accessories for condition (such as cracks) and attachment. Check plumbing clearance and secure against possible chafing. MechInsp9. BRAKE FLUID RESERVOIR - Check reservoir for security, attachment, open vent, proper fluid level and for leaks. MechInsp10. ENGINE OIL TANK OR SUMP - Check for cracks, leaks, proper fluid level, deformation and security. MechInsp11. CRANKCASE - Check security of crankcase half bolts. MechInsp12. OIL SUMP DRAINS ANO SCREENS - Clean screens, check for holes in the screens and for obstructions. Check for proper torque after fnstallatlon. MechInsp13. OIL COOLER - Check oil cooler, lines and fittings for condition, security, chafing and leaks. MechInsp14. PROPELLER AND MOUNTING BOLTS - Check for condition and security. Check the tip of the blades for evidence of lightning strikes. If there is evidence of lightning strikes, consult the propeller manufacturer, the engine manufacturer, and Beech Aircraft Corporation. Inspect the blades for cracks, dents, nicks, scratches, erosion, corrosion, security and movement in the hub. MechInsp15. PROPELLER SPINNER - Check for deformation, security and cracks. MechInsp16. PROPELLER HUB - Check for cracks, excessively leaking seals and condition. MechInsp17. ALTERNATOR/GENERATOR - Check for condition and attachment. Check wiring for proper attachment and possible chafing. Check for unusual noise. MechInsp18. ALTERNATOR - Remove and disassemble the alternator as necessary to inspect the rotor shaft bearings for condition and replace if necessary. For Prestolite only, refer to BEECHCRAFT Service Bulletfn 0546-389 Rev. II or subsequent. MechInsp19. STARTER - Check for condition, attachment and chafed or loose wires. MechInsp20. GENERATOR/ ALTERNATOR BELT - Check for proper tension and worn or frayed condition. Check tension adjustment bolt for tightness. MechInsp21. STANDBY GENERATOR - Check for condition, attachment, security of wires and for chafing. MechInsp22. MAGNETOS - Check contact points for proper clearance. Points with deep pits or excessively burned areas must be discarded. Inspect the cam follower felt pad for proper lubrication and clean the compartment with a clean, dry cloth. Check ignition harness for proper connection, security and fraying. Check timing. MechInsp23. MAGNETO PRESSURIZATION FILTER - Check for condition, cleanliness and security. MechInsp24. CYLINDERS AND BAFFLES - Check cylinders and exhaust manifold for obvious leaks, security and cracks; check baffles for cracks and security. Check cylinders for broken cooling ffns and loose or missing base nuts. MechInsp25. EXHAUST SYSTEM - Check for deformation, security, cracks, leaks, loose or missing nuts and clamps. Check for thin wall condition which may occur due to normal internal erosion on stacks which have long service time. MechInsp26. FIREWALL - Check for wrinkles, damage or cracks. Check all electrical and control access holes for proper sealing. MechInsp27. HOSE AND DUCTS - Check all fuel, oil and air hose or duct for leakage, cracks, deterioration and damage. Check fittings for security. MechInsp28. ENGINE ACCESSORIES - Check for condition, security and leaks. Check wiring, hoses and tubes for chafing, security and leaks. MechInsp29. ENGINE MOUNTS - Check for cracks, corrosion and security. Inspect rubber cushions, mount bolts and nuts and grounding straps for condition and security. MechInsp30. CABIN HEATER SYSTEM - Check for cracks, distortion, corrosion, leaks and obstructions per Section 3 of PEN 35-590096B Shop Manual, Sectfon 10 of PEN 36-590001-3B Shop Manual or Chapter 21-40-00 of PEN 36-590001-9 Maintenance Manual (or subsequent). MechInsp31. PROPELLER GOVERNOR - Check for leaks and control arm for security. MechInsp32. ENGINE CONTROLS - Check controls and associated equipment for condition, attachment, alignment and rigging. MechInsp33. IGNITION HARNESS - Inspect for fraying and attachment. MechInsp34. ELECTRICAL WIRING AND EQUIPMENT - Inspect electrical wiring and associated equipment and accessories for fraying and attachment. MechInsp35. ALL DRAINS AND PLUGS - Check for condition, security and obstructions. Check for leaks and correct tightness. MechInsp36. PRESSURE PUMP INTAKE FILTER - Inspect filter for condition, cleanliness and security. Check filter container for cracks. MechInsp37. AIR CONDITIONER COMPRESSOR - Check for security and attachment. Check refrigerant and oil levels. Check belt for tension and worn or frayed condition. (See Section 2 and 3 of PEN 35-590096B Shop Manual, Section 2 and 10 of PEN 36-590001-3B Shop Manual or Chapters 12-10-00 and 21-50-00 of PEN 36-590001-9, or subsequent, Maintenance Manual). MechInsp38. INDUCTION AIR FILTER - Check for condition, cleanliness and security. MechInsp39. INDUCTION SYSTEM AND ALTERNATE AIR - Check the hot and cold flexible air ducts for delamination of the inner lining. 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