Maintaining the safety and performance of your aircraft is paramount, and staying informed about the latest service information is a crucial part of that responsibility. For owners and maintenance professionals working with classic Beechcraft models 19, 23, 24, and 77, Raytheon (now part of Textron Aviation) issued a series of Service Bulletins, Service Letters, and Service Instructions to address potential issues and recommend improvements.
This article provides a comprehensive overview of these essential service communiqués, offering direct links to PDF downloads for each document. We extend our sincere gratitude to Bill Manhein for his dedication in scanning, cleaning up, and performing OCR on these documents, making this valuable resource readily available.
Understanding Service Bulletins, Service Letters, and Service Instructions
Raytheon utilized different types of communiqués to disseminate service information. While the specific criteria for each type aren’t explicitly defined, it’s understood that all of them contain information worthy of careful review and potential action. These documents are categorized by manufacturer number for easy reference.
Your Go-To Resource for Beechcraft Service Information
Below, you’ll find a sortable table listing each Service Bulletin (SB), Service Letter (SL), and Service Instruction (SI) along with a brief description. Clicking on the “Communique” link will open the corresponding PDF document. The table also indicates which Beechcraft models (19, 23, 24FG, 24R, 76, 77) are affected by each communique.
| Communique | Description | 19 | 23 | 24FG | 24R | 76 | 77 |
|---|---|---|---|---|---|---|---|
| SB-1 | ADDITION OF GENERATOR TERMINAL NIPPLES AND DEFLECTOR REWORK | 23 | |||||
| SB-2 | MODEL 23 IMPROVEMENT CHANGES | 23 | |||||
| SB-3 | ENGINE BREATHER LINE MODIFICATION | 23 | |||||
| SB-4 | INSPECTION OF THE SPAR SPLICE PLATES FOR: 1. SECURITY OF ATTACHMENT OF THE HUCKBOLTS COLLARS; 2. A KNIFE EDGE ON THE AFT VERTICAL FLANGE OF THE UPPER SPAR SPLICE PLATE | 23 | |||||
| SB-5 | INSTALLATION OF AN21-10 BOLTS IN AILERON CABLE CHAIN CONNECTING LINKS | 23 | |||||
| SB-6 | ADDITION OF RIVETS TO CABIN DOOR HINGE | 23 | |||||
| SB-7 | RE-ROUTING OF STATIC LINES | 23 | |||||
| SB-8 | INSPECTION OF CONTROL CABLES FOR PROPER CLEARANCE | 23 | |||||
| SB-9 | TORQUE OF BOLTS IN LANDING GEAR SUPPORT ASSEMBLY | 23 | |||||
| SB-63-2 | SAFETY OF AILERON AND FLAP BOLTS | 23 | |||||
| SB-63-3 | IMPROVED METHOD OF ATTACHING BRAKE PEDAL AND BRAKE MASTER CYLINDER | 23 | |||||
| SB-63-4 | INSTALLATION OF IMPROVED THROTTLE AND MIXTURE CONTROL HOUSING CLAMPS, REINFORCEMENT OF ENGINE CONTROL MOUNTING BRACKET, AND CHANGE OF THROTTLE CONTROL RIGGING | 23 | |||||
| SB-63-5 | INSPECTION OF WELD AT JUNCTURE OF EXHAUST TUBE WITH MUFFLER | 23 | |||||
| SB-63-8 | COMPLIANCE WITH LYCOMING DIVISION – AVCO CORPORATION SERVICE INSTRUCTION NO. 1008A | 23 | |||||
| SB-63-9 | RELOCATION OF EXHAUST TAIL PIPE BRACE | 23 | |||||
| SB-64-1 | MODIFICATION OF HEATER/MUFFLER SHROUD AT THE EXHAUST OUTLET TUBE | 23 | |||||
| SB-64-2 | INSPECTION OF STABILATOR TRIM TAB | 23 | |||||
| SB-64-3 | CHECKING THE STABILATOR FOR PLAY | 23 | |||||
| SB-64-11 | INSPECTION OF INDUCTION AIR SYSTEM DUCTS | 23 | |||||
| SB-64-22 | INSPECTION OF THE FUSELAGE STRUCTURE AT THE AFT BULKHEAD | 23 | |||||
| SB-65-5 | INSPECTION OF FUEL RETURN LINE ON THE AFT SIDE OF THE FIREWALL | 23 | |||||
| SB-65-13 | INSPECTION OF AILERON CONTROL COLUMN LINK | 23 | |||||
| SB-65-18 | INSPECTION OF LANDING GEAR SHOCK ABSORBER ROD AT COMPRESSION PLATE | 23 | |||||
| SB-66-47 | COMPLIANCE WITH SENSENICH PROPELLER BULLETIN NUMBER R-12A | 23 | |||||
| SB-66-48 | TORQUING AND SAFETYING THE FUEL STRAINER (GASKOLATOR) RETAINING BOLT | 19 | 23 | ||||
| SB-66-55 | IMPROVED METHOD OF ATTACHING ADF NOISE SUPPRESSOR CAPACITORS | 23 | |||||
| SB-67-6 | IMPROVED FUEL AND OIL PRESSURE LINE INSTALLATION | 19 | 23 | ||||
| SB-67-23 | INSTALLATION OF PLACARDS AND MARKING TRAVEL LIMITS ON THE STABILATOR TAB INDICATOR | 19 | 23 | ||||
| SL-1 | STABILATOR RIGGING TOOL 169-620000/807 | 23 | |||||
| SL-2 | MODEL 23 IMPROVEMENT KITS | 23 | |||||
| SL-3 | SEAT LOCK MODIFICATION ON THE MUSKETEER | 23 | |||||
| SL-4 | RELOCATION OF FUEL BOOST PUMP AFT OF FIREWALL | 23 | |||||
| SL-5 | NEW SPRING PREVENTS ACCIDENTAL BRAKE SETTING | 23 | |||||
| SL-63-3 | AILERON-RUDDER INTERCONNECT SYSTEM: PART 1, MODIFYING BUNGEE CLEVIS ENDS; PART 2, RIGGING BUNGEE CABLES AND SPRINGS; | 23 | |||||
| SL-63-9 | AN AID TO INSTALLING AND REMOVING FUEL CAPS | 23 | |||||
| SL-63-10 | NEW ENGINE LORD MOUNT ABSORBS STARTING TORQUE | 23 | |||||
| SL-63-12 | NOSE WHEEL STEERING INSTALLATION FOR MUSKETEERS | 23 | |||||
| SL-63-13 | REPAIR OF CRACKS IN ROYALITE COMPONENTS | 23 | |||||
| SL-63-15 | ENLARGED HOLES IMPROVE DRAIN CONDITIONS IN MUSKETEERS | 23 | |||||
| SL-63-16 | ADDED SUPPORT FOR ROTATING BEACON | 23 | |||||
| SL-63-17 | LANDING GEAR TORQUE KNEE PINS REQUIRE LUBRICATION | 23 | |||||
| SL-64-2 | CHANGE OF STABILATOR TRAVEL | 23 | |||||
| SL-64-4 | PREVENTIVE MAINTENANCE FOR FUEL SYSTEM | 19 | 23 | 24FG | 24R | 76 | 77 |
| SL-64-8 | HEAVY DUTY BATTERY FOR MUSKETEER | 23 | |||||
| SL-64-9 | SHOCK MOUNTS FOR INSTRUMENT PANEL | 23 | |||||
| SL-64-10 | NEW SHIMMY DAMPER FOR THE MUSKETEER | 23 | |||||
| SL-64-11 | WINTER BAFFLE FOR THE MUSKETEER OIL COOLER | 23 | |||||
| SL-64-30 | MODIFICATION OF FUEL VENT SYSTEM FOR OPERATION DURING INCLEMENT WEATHER | 23 | |||||
| SL-64-32 | CHECKING THE ATTACH BOLTS OF THE VERTICAL STABILIZER ON MUSKETEERS FOR TORQUE | 23 | |||||
| SL-64-36 | RELOCATION OF SHUTTLE VALVES | 23 | |||||
| SL-65-2 | IMPORTANCE OF COMPLYING WITH BRITTAIN SERVICE BULLETIN A-003 | 23 | |||||
| SL-65-10 | PART I LARGER TIRES FOR MUSKETEER MODEL 23; PART II MAIN GEAR WHEEL ALIGNMENT | 23 | |||||
| SL-65-12 | WINDSHIELD REPLACEMENT | 23 | |||||
| SL-65-19 | INSPECTION OF WING TIP LIGHTS FOR PROPER COLOR | 19 | 23 | 24FG | 24R | 76 | 77 |
| SL-66-5 | AFT COWL REINFORCEMENT | 23 | |||||
| SL-66-11 | ENGINE BAFFLE REINFORCEMENTS ON MUSKETEER SUPER III | 23 | |||||
| SL-66-24 | INCREASE IN BAGGAGE LOAD ALLOWANCE FOR THE BEECHCRAFT MUSKETEER | 23 | |||||
| SL-66-30 | INSPECTION FOR CUSHION CLAMP ON THE MUSKETEER CABIN AIR DUCT | 23 | |||||
| SL-67-2 | OVER-PRIMING THE BEECHCRAFT MUSKETEER | 23 | |||||
| SL-67-9 | APPROVED SPINS ON THE BEECHCRAFT MUSKETEER | 19 | 23 | ||||
| SL-67-12 | BRAKE INSTALLATION IMPROVEMENT ON THE BEECHCRAFT MUSKETEER | 19 | 23 | ||||
| SL-67-19 | A NEW THROTTLE CONTROL FOR THE BEECHCRAFT MUSKETEER | 19 | 23 | ||||
| SL-67-22 | AN IMPROVED METHOD OF FITTING THE BEECHCRAFT MUSKETEER FUEL CELL RIB TO THE SPAR AT THE LANDING GEAR FITTING | 19 | 23 | ||||
| SL-67-23 | TEST INSPECTION OF ALTIMETERS | 19 | 23 | 24FG | 24R | 76 | 77 |
| SL-67-28 | NEW PROPELLER CONTROL FOR THE BEECHCRAFT MUSKETEER SUPER III | 23 | |||||
| SL-67-31 | IMPROVED MUFFLER | 23 | |||||
| SI-0021-248 | PROPELLER – 2-BLADED AND 3-BLADED – PART I, McCAULEY SERVICE BULLETIN NO. 92, CYLINDER ATTACHMENT IMPROVEMENT – PART II, McCAULEY SERVICE BULLETIN NO. 93, COUNTERWEIGHT ATTACHMENT IMPROVEMENT | 24FG | |||||
| SI-0032-241 | POWER PLANT, REDUCTION OF PROPELLER DIAMETER | 23 | |||||
| SI-0042-031 | FUSELAGE – INSPECTION OF FORWARD WING ATTACH POINT | 19 | 23 | 24FG | 24R | ||
| SI-0051-317 | SEATS (SPECIAL) REPLACEMENT OF SEAT BELT FOR SIXTH SEAT | 24FG | |||||
| SI-0053-133 | STABILATOR AND TAB, ADDITION OF DRAIN HOLES | 19 | 23 | 24FG | |||
| SI-0055-351 | ELECTRICAL (COCKPIT), INSPECTION OF THE WIRING TO THE OVERVOLTAGE RELAY | 19 | 23 | 24FG | |||
| SI-0067-394 | PITOT AND STATIC SYSTEM, IMPROVED STATIC AIR FITTINGS | 19 | 23 | 24FG | |||
| SI-0092-220 | BRAKE MASTER CYLINDER, MODIFICATION OF VHR625NL MASTER CYLINDER (PILOTS) TO OBTAIN CLEARANCE FOR THE LEFT PARKING BRAKE VALVE ACTUATING ARM | 19 | 23 | 24FG | |||
| SI-0105-241 | POWER PLANT, INSTALLATION OF OIL FILTER ON LYCOMING ENGINE | 19 | 23 | ||||
| SI-0117-207 | NOSE GEAR WHEEL, INSTALLATION OF IMPROVED NOSE WHEEL CENTERING CABLE | 19 | 23 | 24FG | |||
| SI-0146-240 | POWER PLANT, INSPECTION OF CONSTANT SPEED PROPELLER INSTALLATION | 24FG | |||||
| SI-0166-258 | POWER PLANT – INSPECTION OF FLEXIBLE AIR DUCTS | 19 | 23 | 24FG | 24R | ||
| SI-0179-258 | INDUCTION SYSTEM, IMPROVED CARBURETOR AIR BOX ASSEMBLY | 19 | 23 | ||||
| SI-0209-241 | POWER PLANT, REPLACING THE CARBURETOR | 23 | |||||
| SI-0253-151 | AILERON AND AILERON TAB CONTROLS, INSTALLATION OF AN IMPROVED AILERON CENTERING CABLE | 19 | 23 | 24FG | |||
| SI-0277-204 | MAIN LANDING GEAR DOORS, REMOVAL OF SEALS | 24R | |||||
| SI-0295-392 | INSTRUMENT PANEL (FIXED), TACHOMETER MODIFICATION | 23 | |||||
| SI-0307-282 | FUEL SYSTEM (ENGINE SECTION), DRAINING AND FLUSHING OF MARVEL-SCHEBLER CARBURETORS | 19 | 23 | ||||
| SI-0345-018 | AIRFRAME, INSPECTION OF CABIN INTERIOR STRUCTURE | 19 | 23 | 24FG | |||
| SI-0357-248 | PROPELLER (TWO-BLADE), RECONDITIONING OF SENSENICH PROPELLERS | 23 | |||||
| SI-0364-289 | FUEL SYSTEM – FUEL SELECTOR VALVE – INSPECTION OF FUEL SELECTOR VALVE | 19 | 23 | 24FG | 24R | ||
| SI-0377-257 | OIL SYSTEM, INSPECTION OF OIL RETURN LINE | 24FG | 24R | ||||
| SI-0382-190 | DRY AIR (VACUUM) PUMP, REPLACEMENT OF DRIVE OIL SEAL | 19 | 23 | 24FG | 24R | ||
| SI-0384-241 | POWER PLANT – MANIFOLD PRESSURE LINE MODIFICATION | 24FG | 24R | ||||
| SI-0390-241 | POWER PLANT, INSPECTION OF THE PROPELLER GOVERNOR DRIVE ACCESSORY HOUSING | 24FG | 24R | ||||
| SI-0398-212 | NOSE GEAR RETRACT MECHANISM, INSTALLATION OF ORIFICE FITTING IN NOSE GEAR HYDRAULIC RETRACT LINE | 24R | |||||
| SI-0402-354 | ELECTRICAL (FUSELAGE SECTION), INSULATION OF CIRCUIT BREAKER BUS BAR AND INSTALLATION OF AMMETER CIRCUIT FUSES | 19 | 23 | 24FG | 24R | ||
| SI-0405-206 | NOSE GEAR ASSEMBLY, INSPECTION OF THE NOSE WHEEL AXLE FOR CORROSION | 24R | |||||
| SI-0411-240 | POWER PLANT, INSTALLATION OF RESTRICTORS IN FUEL PRESSURE AND OIL PRESSURE LINES | 19 | 23 | 24FG | 24R | ||
| SI-0413-354 | ELECTRICAL (FUSELAGE SECTION), INSTALLATION OF A SWITCH FOR STROBE LIGHT AND/OR ROTATING BEACON OPERATION | 19 | 23 | 24FG | 24R | ||
| SI-0414-231 | LANDING GEAR HYDRAULIC SYSTEM, MODIFICATION OF PLUMBING AT MAIN GEAR ACTUATOR CYLINDER AND UPLOCK CYLINDER | 24R | |||||
| SI-0415-161 | FLAP MECHANISM, ELECTRIC FLAP SYSTEM MODIFICATION | 19 | 23 | 24FG | 24R | ||
| SI-0416-202 | MAIN GEAR ASSEMBLY – MODIFICATION OF MAIN GEAR UP-LOCK CYLINDERS | 24R | |||||
| SI-0420-151 | AILERON AND AILERON TAB CONTROLS, IMPROVEMENT OF CABLE GUARD | 24R | |||||
| SI-0438-211 | LANDING GEAR RETRACT MECHANISM, MODIFICATION OF NOSE GEAR RETRACT INSTALLATION | 24R | |||||
| SI-0449-200 | LANDING GEAR – TIRE CLEARANCES | 24R | |||||
| SI-0452-359 | ELECTRICAL (ALTERNATOR) – INSTALLATION OF ALTERNATOR COOLING FAN | 19 | 23 | 24FG | |||
| SI-0456-392 | INSTRUMENTS – INSTRUMENT PANEL (FIXED) – INSTALLATION OF IMPROVED OIL PRESSURE AND TEMPERATURE GAGE | 19 | 23 | 24R | |||
| SI-0462-210 | LANDING GEAR – NOSE GEAR STEERING – MODIFICATION TO PREVENT OR ELIMINATE SHIMMY | 24R | |||||
| SI-0465-202 | LANDING GEAR – MODIFICATION OF HOUSING INSTALLATION | 19 | 23 | 24FG | |||
| SI-0481-241 | POWER PLANT – ATTACH FITTINGS – MODIFICATION OF THROTTLE CONTROL INSTALLATION | 24R | |||||
| SI-0487-359 | ELECTRICAL – ALTERNATOR – PART I, INSPECTION OF ALTERNATOR MOUNTING BRACKET; PART II, INSTALLATION OF NEW ALTERNATOR HOUSING THROUGH BOLTS; PART III, CLEARANCE CHECK BETWEEN ALTERNATOR AND ALTERNATOR MOUNTING BRACKET; PART IV, RECLAMPING OF ALTERNATOR WIRING BUNDLE | 19 | 23 | 24FG | 24R | ||
| SI-0504-312 | CARPET AND FLOORBOARDS, INSTALLATION OT STRAPS AND ATTACHMENTS TO SECURE TOW BAR AND BAGGAGE | 19 | 23 | 24FG | 24R | ||
| SI-0510-032 | WING – WING ASSEMBLY – INSTALLATION OF STRAP BELOW WING AILERON PUSH ROD OPENING | 19 | 23 | 24FG | 24R | ||
| SI-0529-289 | FUEL SYSTEM – FUEL SELECTOR VALVE – INSPECTION OF THE FUEL SELECTOR VALVE WASHER AND GUARD MARKINGS | 19 | 23 | 24FG | 24R | ||
| SI-0548-241 | POWER PLANT – RELOCATION OF THE OIL COOLER INSTALLATION | 24FG | 24R | ||||
| SI-0551-241 | POWER PLANT INSTALLATION – INSPECTION OF THE PROPELLER GOVERNOR OIL LINE | 24R | |||||
| SI-0560-210 | LANDING GEAR (NOSE GEAR STEERING) – MODIFICATION OF NOSE GEAR CENTERING CABLE | 24R | |||||
| SI-0564-202 | LANDING GEAR (MAIN GEAR ASSEMBLY) – MODIFICATION AND ADJUSTMENT OF MAIN LANDING GEAR ACTUATOR | 24R | |||||
| SI-0566-241 | POWER PLANT – INSPECTION AND REPLACEMENT OF INDUCTION AIR DUCTS | 19 | 23 | 24FG | |||
| SI-0574-241 | POWER PLANT – MODIFICATION OF CARBURETOR AIRBOX VALVE | 19 | 23 | ||||
| SI-0589-159 | ENGINE CONTROLS – MODIFICATION OF CARBURETOR THROTTLE ARM ATTACHMENT | 19 | 23 | ||||
| SI-0598-491 | AVIONICS – ANTENNA INSTALLATION – REINFORCEMENT OF EMERGENCY LOCATOR ANTENNA MOUNT | 19 | 23 | 24R | |||
| SI-0603-394 | INSTRUMENTS – PITOT AND STATIC SYSTEM – MODIFICATION OF STATIC AIR SYSTEM TO REDUCE MOISTURE ACCUMULATION | 19 | 23 | 24FG | |||
| SI-0608-159 | FLIGHT CONTROLS – ENGINE CONTROLS – INSPECTION AND/OR REPLACEMENT OF FUEL MIXTURE CONTROL AND CARBURETOR HEAT CONTROL | 19 | 23 | ||||
| SI-0614-351 | KLIPVOLT SUPPRESSOR REMOVAL-SUBSTITUTION | 19 | 23 | 24FG | 24R | 76 | 77 |
| SI-0616-010 | GENERAL – GROSS WEIGHT MODIFICATION | 19 | |||||
| SI-0619-090 | FUSELAGE – INSTALLATION OF KIT TO ALLOW INTENTIONAL SPINS | 19 | 23 | ||||
| SI-0620-204 | LANDING GEAR – MAIN GEAR AND DOORS – REPLACEMENT OF THE DOOR ATTACHING BOLT WITH A BOLT CONTAINING A LUBRICATION FITTING | 24R | |||||
| SI-0624-281 | FUEL SYSTEM – REPLACARDING TO INDICATE MINIMUM FUEL FOR TAKE OFF AND INCREASE AMOUNT OF UNUSABLE FUEL | 19 | 23 | 24FG | 24 | ||
| SI-0626-032 | WING – WING ASSEMBLY – PART I, INSPECTION AND REPLACEMENT OF JO-BOLTS ON THE MAIN LANDING GEAR FORWARD SUPPORT CASTINGS; PART II, INSPECTION AND REPLACEMENT OF THE MAIN LANDING GEAR AFT SUPPORT CASTINGS | 24R | |||||
| SI-0627-159 | ENGINE CONTROLS – POWER CONTROL – MODIFICATION OF ENGINE QUADRANT CONTROLS FRICTION MECHANISM | 19 | 23 | 24R | |||
| SI-0628-281 | FUEL SYSTEM – INSPECTION OF FUEL VENT LINES FOR POSSIBLE OBSTRUCTION | 19 | 23 | 24R | |||
| SI-0635-159 | FLIGHT CONTROLS – ENGINE CONTROLS – INSTALLATION OF SPACER BETWEEN BRACKET AND MIXTURE CONTROL CABLE CLAMP | 23 | |||||
| SI-0638-240 | POWER PLANT – INSPECTION OF PLUMBING FITTINGS AT THE FIREWALL | 19 | 23 | 24FG | 24R | ||
| SI-0649-200 | LANDING GEAR – MODIFICATION OF THE HYDRAULIC SHUTTLE VALVE | 24R | |||||
| SI-0651-112 | FUSELAGE – ASSIST STEP – REPLACEMENT OF CABIN ASSIST STEPS | 24R | |||||
| SI-0654-391 | INSTRUMENT PANEL – MODIFICATION OF THE AIRSPEED INDICATOR MARKINGS | 19 | |||||
| SI-0663-600 | MISCELLANEOUS – TIME LIMITS – OBSERVING INITIAL TIME BETWEEN OVERHAUL | 19 | 23 | 24FG | 24R | 76 | 77 |
| SI-0667-241 | POWER PLANT – REPLACEMENT OF THE CARBURETOR AND MODIFICATION OF THE CARBURETOR AIR BOX | 19 | 23 | ||||
| SI-0678-016 | PLACARDS – INSTALLATION OF A CLEANING INSTRUCTIONS DECAL FOR PLASTIC INTERIOR TRIM | 19 | 23 | 24R | |||
| SI-0679-395 | INSTRUMENT – SUBPANEL – INSPECTION OF FUEL QUANTITY AND OIL TEMPERATURE INDICATION SYSTEMS | 19 | 23 | 24R | |||
| SI-0682-202 | LANDING GEAR – MAIN GEAR ASSEMBLY – INCREASED TIRE CLEARANCE ON MAIN LANDING GEAR STRUTS | 19 | 23 | 24FG | 24R | ||
| SI-0683-394 | INSTRUMENTS – PITOT AND STATIC SYSTEM – INSTALLATION OF OPTIONAL EMERGENCY STATIC AIR VALVE | 19 | 23 | 24FG | 24R | ||
| SI-0685-106 | FUSELAGE – BAGGAGE DOOR (AFT) – ADDITION OF DECAL | 24R | |||||
| SI-0692-258 | POWER PLANT – INDUCTION SYSTEM – INSTALLATION OF A CLAMP ON THE INDUCTION AIR HOSE | 19 | |||||
| SI-0698-359 | ELECTRICAL – ALTERNATOR – MODIFICATION OF ALTERNATOR ATTACHMENT AND SECURITY OF WIRING | 19 | 23 | 24FG | 24R | ||
| SI-0700-157 | FLIGHT CONTROLS – PEDESTAL OR CONSOLE STRUCTURE – REPLACEMENT OF QUADRANT CONTROL COVER | 19 | 23 | 24R | |||
| SI-0702-194 | VACUUM OR PRESSURE SYSTEM (INSTRUMENT) – REPLACEMENT OF VACUUM PUMP HOSE | 19 | 23 | 24R | |||
| SI-0717-159 | FLIGHT CONTROLS – ENGINE CONTROLS – INSPECTION OF MIXTURE CONTROL AND CARBURETOR HEAT CONTROL CABLES | 19 | 23 | 24FG | 24R | ||
| SI-0728-206 | LANDING GEAR – INSTALLATION OF IMPROVED NOSE LANDING GEAR LIMIT SWITCH | 24R | |||||
| SI-0731-114 | DOORS – REPLACEMENT OF DOOR HANDLES AND CABIN DOOR LATCH BOLTS | 19 | 23 | 24R | |||
| SI-0742-241 | POWER PLANT – MANIFOLD PRESSURE FITTING MODIFICATION | 24FG | 24R | ||||
| SI-0747-155 | FLIGHT CONTROLS – INSPECTION OF THE CONTROL COLUMN AND THE MIXTURE CONTROL CABLE FOR CLEARANCE | 23 | |||||
| SI-0751-157 | FLIGHT CONTROLS – PEDESTAL STRUCTURE – INSPECTION OF FLAP AND STABILATOR CONTROL PEDESTAL | 19 | 23 | 24R | |||
| SI-0758-155 | FLIGHT CONTROLS – CONTROL COLUMN – INSPECTION OF CONTROL COLUMN INSTALLATION | 24R | |||||
| SI-0760-010 | GENERAL – INSPECTION AND/OR REPLACEMENT OF CONTROL ROD END BEARINGS | 19 | 23 | 24R | |||
| SI-0765-254 | PROPELLERS – REPLACEMENT OF PROPELLER GOVERNOR | 24R | |||||
| SI-0793-106 | DOORS – INSTALLATION OF IMPROVED LATCH ASSEMBLY ON LARGE BAGGAGE DOOR | 24R | |||||
| SI-0801-287 | FUEL SYSTEM – REPLACEMENT OF THE FUEL CAP AND ADAPTER | 23 | |||||
| SI-0807-356 | ELECTRICAL POWER – MODIFICATION TO THE BATTERY BOX INSTALLATION | 19 | |||||
| SI-0823-491 | COMMUNICATIONS – COMPLIANCE WITH FEDERAL AIR REGULATIONS 91.177 | 19 | 23 | 24R | |||
| SI-0824-035 | WINGS – INSPECTION OF THE MAIN SPAR | 19 | 23 | 24FG | 24R | ||
| SI-0831-161 | FLIGHT CONTROLS – INSPECTION AND MODIFICATION OF THE FLAP CABLE BLOCK | 19 | 23 | 24R | |||
| SI-0833-293 | ENGINE FUEL AND CONTROL – INSPECTION OF MIXTURE CONTROL SHAFT | 24R | |||||
| SI-0835-111 | NACELLES – MODIFICATION OF THE ENGINE FIREWALL | 19 | 23 | 24FG | 24R | ||
| SI-0838-289 | FUEL SYSTEM – REPLACEMENT OF THE FUEL SELECTOR VALVE | 19 | 23 | 24FG | 24R | ||
| SI-0843-313 | EQUIPMENT/FURNISHINGS – MODIFICATION TO PILOT AND COPILOT SEATS | 19 | 23 | 24FG | 24R | ||
| SI-0858-151 | FLIGHT CONTROLS – INSPECTION AND/OR REPLACEMENT OF ROD ENDS | 19 | 23 | 24FG | 24R | ||
| SI-0861-281 | FUEL – REPLACEMENT OF THE FUEL BOOST PUMP | 19 | 23 | ||||
| SI-0871-090 | FUSELAGE – INSTALLATION OF KIT TO ALLOW INTENTIONAL SPINS | 19 | 23 | ||||
| SI-0874 | ELECTRICAL POWER – REPLACEMENT OF VOLTAGE REGULATOR AND OVERVOLTAGE RELAY | 19 | 23 | 24FG | 24R | ||
| SI-0878-248 | PROPELLERS – PROCEDURE FOR DOME INSTALLATION OF HARTZELL FEATHERING COMPACT PROPELLERS | 76 | |||||
| SI-0883 | POWER PLANT – INSPECTION OF THE INDUCTION AIR FILTER INSTALLATION | 19 | 23 | 24FG | 24R | ||
| SI-0892 | VACUUM SYSTEM – RELOCATION OF AIR FILTER | 19 | 23 | 24FG | 24R | ||
| SI-0904 | FUEL SYSTEM – REPLACEMENT OF THE FUEL BOOST PUMP | 24R | |||||
| SI-0908 | ELECTRICAL POWER – REPLACEMENT OF THE ALTERNATOR FIELD CIRCUIT BREAKER | 19 | 23 | 24R | |||
| SI-0929 | PLACARDS – INSTALLATION OF A FUEL RETURN DECAL | 23 | |||||
| SI-0933 | VACUUM SYSTEM – SERVICE LIFE LIMITATION OF AIRBORNE DRY AIR PUMPS | 19 | 23 | 24FG | |||
| SI-0940 | FLIGHT CONTROLS – REPLACEMENT OF THE FLAP CONTROL WELD ASSEMBLY | 19 | 23 | 24FG | 24R | ||
| SI-0967 | LANDING GEAR – INSPECTION FOR VENT HOLE IN BRAKE FLUID RESERVOIR | 19 | 23 | 24R | |||
| SI-0994 | FLIGHT CONTROLS – INSPECTION OF THE STABILATOR TRIM TAB ACTUATOR ROD | 19 | 23 | 24R | |||
| SI-0998 | POWER PLANT – INSPECTION AND/OR REPLACEMENT OF HOSE ASSEMBLIES | 19 | 23 | ||||
| SI-1009 | INSTALLATION OF STATIC DISCHARGE WICKS | 76 | |||||
| SI-1010 | EQUIPMENT/FURNISHINGS – IMPROVED SUN VISOR INSTALLATION | 19 | 23 | 24R | 76 | ||
| SI-1017 | FLIGHT CONTROLS – INSPECTION OF THE CONTROL COLUMN BEARING ASSEMBLIES | 19 | 23 | 24R | 76 | ||
| SI-1027 | ELECTRICAL PANELS, PARTS & INSTRUMENTS – INSPECT FOR LOCKWASHERS ON CUTLER-HAMMER ROCKER SWITCHES AND INSTALL AS NECESSARY | 19 | 23 | 24R | 76 | ||
| SI-1032 | LANDING GEAR – INSPECTION OF THE NOSE LANDING GEAR LIMIT SWITCH INSTALLATION | 24R | |||||
| SI-1034 | NAVIGATION/PITOT AND EMERGENCY STATIC AIR SOURCE VALVE | 76 | |||||
| SI-1035 | LIGHTS – INSTALLATION OF A MOUNTING PLATE FOR WING TIP MOUNTED NAV AND STROBE LIGHT ASSEMBLIES | 19 | 23 | 24FG | 24R | 76 | |
| SI-1038 | ELECTRICAL POWER – MODIFICATION OF ELECTRICAL SYSTEM AND IMPROVED ALTERNATOR PARALLELING | 76 | |||||
| SI-1039 | OIL – IMPROVED GROUNDING OF THE OIL PRESSURE TRANSDUCERS | 76 | |||||
| SI-1041 | STABILIZERS – INSPECTION OF ELEVATOR TRAILING EDGE BOND THICKNESS | 76 | |||||
| SI-1044 | POWER PLANT – REPLACEMENT OF COWL FLAP HINGE ASSEMBLIES | 76 | |||||
| SI-1045 | ENGINE FUEL AND CONTROL – MODIFICATION OF CARBURETOR | 76 | |||||
| SI-1048 | EQUIPMENT/FURNISHINGS – REMOVAL OF LITHIUM SULFUR DIOXIDE BATTERIES | 19 | 23 | 24FG | 24R | 76 | |
| SI-1050 | EQUIPMENT/FURNISHINGS – PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL REVISION REQUIREMENTS | 76 | |||||
| SI-1051 | DOORS – REPLACEMENT OF THE DOOR LOCK ASSEMBLIES | 76 | |||||
| SI-1054 | FUEL – PART I, INSTALLATION OF A CHECK VALVE ON THE FUEL TANK OUTLET; PART II, INSTALLATION OF AN IMPROVED FUEL SELECTOR VALVE | 76 | |||||
| SI-1055 | ENGINE FUEL AND CONTROL – INSTALLATION OF IMPROVED CARBURETOR AIRBOXES | 76 | |||||
| SI-1057 | FLIGHT CONTROLS – REPLACEMENT OF THE ELEVATOR AND RUDDER TAB PUSH RODS | 76 | |||||
| SI-1058 | ENGINE FUEL AND CONTROL – INSPECTION OF BENDIX FUEL INJECTOR ASSEMBLIES ON AVCO LYCOMING ENGINES | 24FG | 24R | ||||
| SI-1061 | WINGS – INSPECTION OF FUEL TANK OUTBOARD RIB ATTACH BOLTS | 76 | |||||
| SI-1064 | FUSELAGE – INSPECTION OF SEALS ON THE WINDSHIELD, CABIN WINDOWS, THE ENGINE FIREWALL AND F.S. 68.00 FRAME | 19 | 23 | 24FG | 24R | ||
| SI-1065 | ENGINE INDICATING – INSPECT THE ENGINE INSTRUMENT CLUSTER ASSEMBLY | 76 | |||||
| SI-1066 | ENGINE CONTROLS – INSTALLATION OF AN IMPROVED ENGINE CONTROL QUADRANT COVER | 76 | |||||
| SI-1071 | WINGS – INSPECTION AND REPAIR OF THE WING SPAR CENTER SPLICE PLATES | 76 | |||||
| SI-1073 | LANDING GEAR – INSTALLATION OF AN IMPROVED FLATHEAD PIN ON THE MAIN LANDING GEAR FORK PIN | 76 | |||||
| SI-1074 | NAVIGATION – REPLACEMENT OF ANTENNA CABLES ON FACTORY INSTALLED COLLINS ADF-650 INSTALLATIONS | 23 | 24R | 76 | |||
| SI-1076 | DOORS – REPLACEMENT OF THE DOOR STOP ASSEMBLIES | 76 | |||||
| SI-1081 | ENGINE INDICATING – REPLACEMENT OF MANIFOLD PRESSURE FITTING | 76 | |||||
| SI-1084 | LANDING GEAR – INSTALLATION OF A CLAMP TO SECURE THE BRAKE LINE TO THE LANDING GEAR FORK | 19 | 23 | 24FG | |||
| SI-1085 | IGNITION – INSTALLATION OF A CAP ON THE UNUSED MAGNETO TACHOMETER CONTACT | 76 | |||||
| SI-1087 | FLIGHT CONTROLS – INSPECTlON AND/OR REPLACEMENT Of THE STOP BOLT NUTS FOR THE AILERON AND RUDDER BELL CRANKS | 76 | |||||
| SI-1088 | WINGS – INSPECTION OF WING ATTACH BOLTS AND ATTACH BOLT NUT PLATE THREADS | 77 | |||||
| SI-1089 | NAVIGATION/PITOT STATIC – PROVIDE AN IMPROVED GROUND FOR THE NAV ANTENNA CABLE | 19 | 23 | 24R | |||
| SI-1091 | LIGHTS – GROUNDING THE SHIELD ON THE STROBE LIGHT WIRING | 76 | |||||
| SI-1098 | LANDING GEAR – INSTALLATION OF AN IMPROVED BRAKE HOSE | 76 | |||||
| SI-1101 | ENGINE FUEL AND CONTROL – REPLACEMENT OF THE ENGINE DRIVEN FUEL PUMP | 23 | 76 | ||||
| SI-1105 | PNEUMATIC – INSTALLATION OF IMPROVED INSTRUMENT AIR LINES | 76 | |||||
| SI-1116 | STABILIZERS – INSTALLATION OF DRAIN HOLES IN THE RUDDER AND RUDDER TRIM TAB | 76 | 77 | ||||
| SI-1117 | ELECTRICAL POWER – REPLACEMENT OF LOAD METER 15 AMP FUSES AND SPARES WITH 5 AMP FUSES AND SPARES | 76 | |||||
| SI-1119 | FLIGHT CONTROLS – REPLACEMENT OF AILERON TORQUE TUBE BEARINGS | 77 | |||||
| SI-1122 | ENGINE CONTROLS – INSTALLATION OF IMPROVED FEATHERING STOP SPRING | 76 | |||||
| SI-1124 | CONTROL COLUMN – INSTALLATION OF A FOOT GUARD | 77 | |||||
| SI-1128 | ELECTRICAL POWER – INSTALLATION OF BUS BAR ON ALTERNATOR, BATTERY AND ENGINE GROUND CONNECTIONS | 77 | |||||
| SI-1131 | PLACARDS AND MARKINGS – REPLACEMENT OF THE NOSE GEAR STRUT SERVICING PLACARD | 77 | |||||
| SI-1132 | POWER PLANT – MODIFICATION OF THE ALTERNATE AIR DOOR | 24FG | 24R | ||||
| SI-1134 | PLACARDS AND MARKINGS – INSPECTION TO VERIFY INSTALLATION AND CONDITION OF ALL INTERIOR AND EXTERIOR PLACARDS AND MARKINGS | 19 | 23 | 24FG | 24R | 76 | |
| SI-1135 | FLIGHT CONTROLS – REPLACEMENT OF THE ELEVATOR CONTROL ARM BUSHINGS | 77 | |||||
| SI-1136 | FLIGHT CONTROLS – INSTALLATION OF IMPROVED CONTROL LOCK ASSEMBLY | 76 | |||||
| SI-1139 | EQUIPMENT/FURNISHINGS – INSPECTION AND/OR REPLACEMENT OF COLLINS/COMMUNICATIONS COMPONENTS CORPORATION EMERGENCY LOCATOR TRANSMITTERS AND/OR BATTERY PACKS | 19 | 23 | 24FG | 24R | 76 | 77 |
| SI-1142 | EXHAUST – INSPECTION AND/OR REPLACEMENT OF THE MUFFLER ASSEMBLY AND INSTALLATION OF A CARBON MONOXIDE DETECTOR AND DECAL | 77 | |||||
| SI-1144 | INDICATING/RECORDING SYSTEMS – INSTALLATION OF AN IMPROVED ELECTRIC HOUR METER PRESSURE SWITCH | 76 | |||||
| SI-1145 | LANDING GEAR – INSTALLATION OF AN IMPROVED MAIN LANDING GEAR SIDE BRACE SPRING PIVOT ASSEMBLY AND BUSHING | 76 | |||||
| SI-1146 | ELECTRICAL POWER – INSTALLATION OF AN ALTERNATOR OUTPUT CURRENT LIMITER | 19 | 23 | 24R | |||
| SI-1147 | POWERPLANT – INSPECTION AND/OR REPLACEMENT OF THE ENGINE MOUNT ASSEMBLIES | 76 | |||||
| SI-1153 | POWER PLANT – INSPECTION OF THE ENGINE MOUNT ASSEMBLY TO FIREWALL ATTACH BOLTS | 77 | |||||
| SI-1155 | ELECTRICAL POWER – REPLACEMENT OF THE AVIONICS BUS FEED WIRE | 77 | |||||
| SI-1156 | LANDING GEAR – INSTALLATION OF A FITTING ON THE LANDING GEAR SAFETY SWITCH | 24R | 76 | ||||
| SI-1158 | EQUIPMENT/FURNISHINGS – INSPECTION AND POSSIBLE REWORK OF LAP BELT AND SHOULDER HARNESS ASSEMBLIES MANUFACTURED BY AMERICAN SAFETY EQUIPMENT CORPORATION | 19 | 23 | 24FG | 24R | 76 | 77 |
| SI-1166 | ENGINE CONTROLS INSTALLATION OF AN IMPROVED ENGINE CONTROL QUADRANT COVER | 76 | |||||
| SI-1167 | STABILIZERS – INSPECTION AND/OR REPLACEMENT OF THE HORIZONTAL STABILATOR AFT CENTER SPARS | 19 | 23 | 24FG | 24R | ||
| SI-1168 | LANDING GEAR – INSTALLATION OF AN IMPROVED GREASE SEAL AND AXLE SPACER | 19 | 23 | 24R | |||
| SI-1173 | FUSELAGE – INSPECTION OF THE SHOULDER HARNESS ATTACH BRACKET | 77 | |||||
| SI-1175 | ENGINE INDICATING – MODIFICATION AND CALIBRATION OF AIRCRAFT INSTRUMENT AND DEVELOPMENT INCORPORATED ENGINE INSTRUMENT CLUSTERS | 76 | 77 | ||||
| SI-1180 | ENGINE CONTROLS – MODIFICATION OF THE CARBURETOR MIXTURE CONTROL ARM | 23 | |||||
| SI-1182 | ENGINE AND FUEL CONTROL – INSTALLATION OF A GASKET BETWEEN THE CARBURETOR AIR BOX AND THE CARBURETOR | 76 | |||||
| SI-1185 | ELECTRICAL POWER – PART I, RELOCATION OF EXTERNAL ELECTRICAL POWER RECEPTACLE; PART II, INSPECTION AND MODIFICATION OF EXTERNAL POWER WIRING; PART III, INSTALLATION OF UPHOLSTERY RETAINER CLIP TO CLEAR EXTERNAL POWER WIRE ROUTING | 77 | |||||
| SI-1188 | WINGS – INSPECTION AND POSSIBLE REWORK OF THE FLAP HINGE BRACKETS | 76 | |||||
| SI-1193 | STABILIZERS – INSPECTION OF HORIZONTAL STABILIZER ATTACH BOLTS | 77 | |||||
| SI-1194 | FLIGHT CONTROLS – REPLACEMENT OF THE ELEVATOR TRIM TAB CABLE AND DRUM | 77 | |||||
| SI-1209 | LANDING GEAR – REPLACEMENT OF THE NOSE LANDING GEAR DOOR HINGE PINS AND REPLACEMENT OF BUSHINGS IN THE NOSE LANDING GEAR DOOR ACTUATING LINKAGE. | 76 | |||||
| SI-1217 | LANDING GEAR – REPLACEMENT OF THE NOSE LANDING GEAR AXLE | 77 | |||||
| SI-1218 | LANDING GEAR – REPLACEMENT OF THE NOSE LANDING GEAR ATTACHMENT BOLTS | 77 | |||||
| SI-1219 | LANDING GEAR – INSTALLATION OF 17.5 INCH DIAMETER TIRES AND MODIFICATION OF BRAKE ASSEMBLIES | 77 | |||||
| SI-1220 | POWER PLANT – MODIFICATION OF THE CRANKCASE BREATHER TUBE | 76 | 77 | ||||
| SI-1232 | ELECTRICAL POWER – IMPROVED ALTERNATOR FEED DIODE INSTALLATION | 76 | |||||
| SI-1233 | POWER PLANT – REPLACEMENT OF THE ENGINE MOUNT ASSEMBLY AND MODIFICATION OF THE ENGINE CONTROL LINKAGE | 77 | |||||
| SI-1234 | ENGINE CONTROLS – INSTALLATION OF AN IMPROVED CARBURETOR HEAT CONTROL SPRING DETENT | 76 | |||||
| SI-1237 | NACELLES – TO PROVIDE INSPECTION PLATES TO FACILITATE THE ENGINE MOUNT/NACELLE CHANNEL INSPECTION | 76 | |||||
| SI-1238 | FLIGHT CONTROLS – INSPECTION OF RUDDER TORQUE TUBE LOWER HINGE ADAPTER | 76 | |||||
| SI-1243 | POWER PLANT – INSTALLATION OF WASHERS ON THE ENGINE CONTROL ROD ENDS | 19 | 23 | 24FG | 24R | 76 | 77 |
| SI-1245 | FUSELAGE – INSPECTION FOR CORROSION AT THE FIREWALL AND F.S. 68.00 FRAME | 19 | 23 | 24FG | 24R | ||
| SI-1246 | LIGHTS – LANDING LIGHT WIRING MODIFICATION | 77 | |||||
| SI-1250 | FUSELAGE – INSTALLATION OF IMPROVED CABIN ENTRANCE STEPS | 77 | |||||
| SI-1256 | STABILIZERS – IMPROVED ATTACHMENT OF THE RUDDER BALANCE WEIGHT | 77 | |||||
| SB-2001 | GENERAL – BEECHCRAFT SERVICE PUBLICATIONS – WHAT IS AVAILABLE AND HOW TO OBTAIN IT | 19 | 23 | 24FG | 24R | 76 | 77 |
| SB-2003 | LANDING GEAR – INSPECTION AND/OR MODIFICATION OF COMPONENTS ON THE MAIN LANDING GEAR STRUT ASSEMBLIES | 77 | |||||
| SB-2004 | FUSELAGE – IMPROVED ATTACHMENT OF THE FORWARD CABIN SKIN AT F.S. 68.0 | 19 | 23 | 24R | |||
| SB-2006 | ELECTRICAL POWER – INSTRUMENT PANEL GROUND STRAP INSTALLATION | 19 | 23 | 24FG | 24R | ||
| SB-2009 | LANDING GEAR – INSPECTION OF NOSE LANDING GEAR ATTACH BOLTS AND INSTALLATION OF BUSHINGS | 76 | |||||
| SB-2014 | LANDING GEAR – REMOVAL OF FREE PLAY IN MAIN LANDING GEAR | 19 | 23 | 24FG | |||
| SB-2018 | NACELLES – INSTALLATION OF INSPECTION PLATES AND INSPECTION OF ENGINE MOUNT/NACELLE CHANNELS | 76 | |||||
| SB-2020 | POWER PLANT – INSTALLATION OF SPACER BETWEEN THE CARBURETOR AND ENGINE | 76 | |||||
| SB-2031 | EQUIPMENT/FURNISHINGS – NOTICE OF AVAILABILITY OF SHOULDER HARNESS KITS | 19 | 23 | 24FG | 24R | ||
| SB-2038 | WINGS – INSTALLATION OF WASHERS ON THE WlNG LOWER SPLICE PLATE BOLTS AND INSPECTION OF THE WING UPPER SPLICE PLATE | 76 | |||||
| SB-2045 | FUEL – MODIFICATION OF FUEL FILLER AND REPLACEMENT OF FUEL FILLER CAPS | 19 | 23 | 24FG | 24R | 76 | |
| SB-2050 | LANDING GEAR – INSTALLATION OF AN IMPROVED FLATHEAD PIN ON THE MAIN LANDING GEAR FORK PIN | 24R | |||||
| SB-2052 | ELECTRICAL POWER – REMOVAL OF TRANZORB FROM BATTERY RELAY | 23 | 24R | ||||
| SB-2053 | FUEL SYSTEM – ADDITION OF A DECAL AND A FUEL SELECTOR STOP TO THE FUEL SELECTOR VALVE GUARD | 19 | 23 | 24FG | 24R | ||
| SB-2063 | FUEL – INSPECTION AND/OR MODIFICATION OF THE FUEL STRAINER PRIMER LINE OUTLET FITTING | 19 | 23 | ||||
| SB-2081 | LANDING GEAR – INSPECTION OF MAIN LANDING GEAR SIDE BRACE OVER CENTER TRAVEL AND LIMIT SWITCH ADJUSTMENT | 76 | |||||
| SB-2090 | DOORS – REPLACEMENT OF CABIN ENTRANCE ASSIST STEPS | 24R | |||||
| SB-2148 | IGNITION – REMOVAL OF GROUNDING TAB FROM IGNITION SWITCH | 76 | |||||
| SB-2165 | ENGINE CONTROLS – REPLACEMENT OF THE MIXTURE CONTROL CABLE ASSEMBLY | 19 | 23 | 24R | |||
| SB-2176 | FLIGHT CONTROLS – MODIFICATION OF FLAP AND LANDING GEAR SELECTOR SWITCH KNOBS | 19 | 23 | 24R | 76 | ||
| SB-2182 | FLIGHT CONTROLS – INSPECTION OF STABILATOR HINGE BRACKETS FOR WORKING RIVETS | 19 | 23 | 24FG | 24R | ||
| SB-2187 | LANDING GEAR – INSPECTION AND/OR MODIFICATION OF NOSE LANDING GEAR SHIMMY DAMPER | 19 | 23 | 24FG | 24R | ||
| SB-2198 | FLIGHT CONTROLS – INSPECTION AND/OR REPLACEMENT OF AILERON PUSH ROD FORWARD ROD END | 19 | 23 | 24FG | 24R | ||
| SB-2201 | ELECTRICAL POWER – REMOVAL OF REVERSE CURRENT DIODE FROM ALTERNATOR SYSTEM | 77 | |||||
| SB-2202 | EQUIPMENT/FURNISHINGS – INSPECTION AND/OR REBONDING OF CREW CHAIR SEAT SLINGS | 19 | 23 | 24FG | 24R | 76 | |
| SB-2217 | FUEL – REPLACEMENT OF THE ELECTRIC FUEL PUMP | 24FG | 24R | ||||
| SB-2241 | LANDING GEAR – INSPECTION/REPLACEMENT OF NOSE LANDING GEAR FORK | 77 | |||||
| SB-2243 | LANDING GEAR – INSTALLATION OF MAIN GEAR SINGLE PIECE BRACE NUT AND COLLAR AND ELLIPTICAL BUSHING RETAINER | 77 | |||||
| SB-2266 | PROPELLERS – ANNOUNCEMENT OF HARTZELL PROPELLER SERVICE BULLETIN | 76 | |||||
| SB-2357 | DOORS – CABIN DOOR LATCHING WARNING PLACARD | 19 | 23 | 24FG | 24R | 76 | 77 |
| SB-2381 | FUEL – REPLACEMENT OF THE FUEL BOOST PUMP | 19 | 23 | ||||
| SB-2405 | PLACARDS AND MARKINGS – INSPECTION TO VERIFY INSTALLATION AND CONDITION OF ALL INTERIOR AND EXTERIOR PLACARDS AND MARKINGS [NOTE: COMMERCIAL MODELS ONLY] | 19 | 23 | 24FG | 24R | 76 | 77 |
| SB-2526 | FUEL – DUKES INC. ELECTRIC FUEL BOOST PUMP INSPECTION AND MODIFICATION/OVERHAUL/REPLACEMENT | 23 | |||||
| SB-2598 | EQUIPMENT/FURNISHINGS – EMERGENCY LOCATOR TRANSMITTER PLACARD INSTALLATION | 19 | 23 | 24FG | 24R | 76 | 77 |
| SB-2640 | POWER PLANT – NOSE COWL SPLIT CONFIGURATION MODIFICATION | 19 | 23 | 24FG | |||
| SB-2670 | PLACARDS AND MARKINGS – INSTALLATION OF FUEL SELECTOR PLACARD | 19 | 23 | 24FG | 24R | 76 | 77 |
| SB-2683 | LANDING GEAR – NOSE GEAR DOWN LOCK SWITCH INSTALLATION | 24R | |||||
| SB-00-3000 | GENERAL – PUBLICATIONS – INFORMATION ON THE INTRODUCTION OF A NEW SERVICE BULLETIN FORMAT AND NUMBERING SYSTEM | 19 | 23 | 24FG | 24R | 76 | 77 |
| SB-24-3735 | ELECTRICAL POWER – CIRCUIT BREAKER SWITCH REPLACEMENT | 77 | |||||
| SB-27-3954 | FLIGHT CONTROLS – INSTALL FLAP INSPECTION ACCESS PANELS ON CERTAIN AERO CENTER PRODUCTS | 19 | 23 | 24FG | 24R | 76 |
Note: This article is focused on providing information about Raytheon Service Bulletins for Beechcraft aircraft. If you are looking for service bulletins for a 2006 Mercedes SL500, this list is not relevant to your search. To find service bulletins for your Mercedes vehicle, you should consult official Mercedes-Benz resources or reputable automotive repair databases.
