Overview
The following table is a list of service communiques (their word) from Raytheon applicable to all Models 19/23/24/77.
Each link points to a PDF file, ranging in size from 75k to over 3MB. A big thanks to Bill Manhein for taking a huge amount of time to scan, clean-up, and OCR all of these documents.
Included below are Service Bulletins, Service Letters, and Service Instructions. It is not clear what the requirements are for each type of communique, but it is fairly clear that all of them are worthy of attention. These are provided in order by manufacturer number.
| 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
|
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 |