| AD Number: | AD Subject: | SB Reference: |
|---|
| 1-022 REV.E |
INSPECTION OF PROPELLER HUB ASSEMBLIES |
DOWTYROTOL 340-61-54 |
| 1-033 REV A |
A/C GENERATORS P/N31342-001 FROM LAPEC |
340-24-016 |
| 1-034 |
NACELLE - INSPECTION OF DRAG STRUT BOLTS, LOWER FITTINGS AND ATTACH FASTENERS |
340-54-026 |
| 1-036 REV.A |
STABILIZER - REINSPECTION OF TOP CLOSURE RIB |
SAAB340-55-022, SAAB340-55-023 |
| 1-038 REV.A |
YAW OSCILLATIONS |
340-55-026R1 |
| 1-041 |
CORRECTION OF WIRE SIZE IN THE AUTOPILOT ELECTRICAL SYSTEM |
SAAB 340-34-068 |
| 1-042 |
INSPECTION AND IF FOUND OUT OF LIMITS INSTALLATION OF NEW AVIBANKS LATCH TRIGGERS ON THE FORWARD TOILET SERVICE DOOR |
340-71-035 |
| 1-044 REV.A |
REINFORCEMENT / IMPROVEMENT OF FORWARD TOILET SERVICE DOOR |
SAAB340-52-013R1 |
| 1-045 |
CHANGE OF CIRCUIT BREAKER IN AIRCRAFT WITH FORWARD OR AFT LAVATORY |
SAAB340-25-181 |
| 1-046 |
INSPECTION OF THE INNER WING FUEL TANKS FOR FOREIGN OBJECTS |
SAAB340-28-013 |
| 1-047 |
EMERGENCY LIGHTING -REDUCTION OF EXIT LIGHT AND DOME LIGHT OPERATING CURRENT |
SAAB340-33-030 |
| 1-048 |
PASSENGER DOOR HANDLE- INSPECTION AND MODIFICATION OF THE DOOR HANDLE MECHANISM. |
340-52-014 |
| 1-049 REV A |
NACELLE -INSPECTION OF LOWER DRAG STRUT ASSY |
SAAB340-54-027R1 |
| 1-050 |
DISCONNECTION OF ELECTRICAL POWER TO REFUEL/DEFUEL PANEL LIGHT |
|
| 1-051 |
STABILIZER DECING |
340-30-039 |
| 1-052 |
WING INSPECTION AND MODIFICATION OF FUEL ACCESS DOOR AREA |
SAAB340-57-020 |
| 1-054 |
RELOCATION OF SENSOR LOOPS FOR BLEED AIR LEAK DETECTION |
SAAB340-36-006 |
| 1-055 |
INSTALLATION OF STRUCTURE PROTECTIVE SHIELD |
SAAB340-53-028 |
| 1-056 |
MOTOR OPERATED FUEL VALVES |
340-28-016 |
| 1-057 |
INSTALLATION OF NEW PART NUMBER AC GENERATOR CONTROL RELAYS |
SAAB340-24-22 |
| 1-060 REV A |
INSPECTION AND REPAIR OF ELEVATOR AND AILERON COVES |
SAAB340-51-012 |
| 1-061 |
MAIN LANDING GEAR RETRACT ACTUATOR BRACKET RETAINING BOLT FAILURES |
SAAB340-32-094 |
| 1-064R1 |
OPERATIONAL TEST OF PROPELLER -BRAKE VALVE LIMIT SWITCH |
SAAB340-61-032, SAAB 340-61-033 |
| 1-065 |
OVERWING EMERGENCY EXIT BEAMS |
340-53-047 |
| 1-067 |
ENGINE CONTROLS -CONTROL QUADRANT -INSTALLATION OF A BETA STOP MECHANISM |
SAAB340-76-034 |
| 1-070R1 |
ENGINE CONTROLS -INSTALLATION OF FLIGHT IDLE STOP -CONTROL QUADRANT |
SAAB340-76-032, 031,034, SAAB 340-32-100 |
| 1-072 |
WINGS -FLAPS -INSPECTION AND MODIFICATION OF THE FLAP FITTINGS AT WS 123.38 |
SAAB340-57-027 |
| 1-074 |
STABILIZERS -RUDDER -INSPECTION / REINFORCEMENT OF NOSE RIB |
SAAB340-55-032 |
| 1-075R1 |
LANDING GEAR -BRAKES -INSPECTION OF THE BRAKE STACK FOR DAMAGED CARBON AND INSTALLATION OF TORQUE TUBE HEAT SHIELD |
SAAB340-32-105 & 110 |
| 1-079 |
FIRE PROTECTION -EXTINGUSHING -INSPECTION AND MODIFICATION OF WIRING TO THE NACELLE FIRE EXTINGUSHER |
SAAB340-26-015 |
| 1-080 |
FIRE HANDLE SWITCHES |
340-26-016 |
| 1-085R1 |
LANDING GEAR -ANTI-SKID SYSTEM -IMPROVED HUBCAP DRIVE COUPLING |
SAAB340-32-107 |
| 1-094R5 |
AIRWORTHINESS DIRECTIVES FOR ENGINES, PROPELLERS AND OTHER VENDOR EQUIPMENT |
NO BULLETIN |
1-103R1 |
CEILING AND LAVATORY LIGHTS |
340-33-040R1 |
| 1-105 |
REAR FUSELAGE-SEALING OF FIRE SHIELD AT APU |
340-53-052 |
| 1-106R1 |
FORWARD LAVATORY WASTE BIN FIRE EXTINGUISHER |
SAAB340-25-235 |
| 1-110R2 |
STABILIZERS -HORIZONTAL STABILIZERS -INSPECTION OF HOLES |
SAAB340-55-033R04 |
| 1-113R1 |
PAX-FLUORESCENT LIGHTING |
340-33-047R1 |
| 1-115R1 |
ICE & RAIN PROTECTION -WINDSHIELD WIPERS -INSPECTION OF THE WIPER ARM ASSEMBLY |
SAAB340-30-081 |
| 1-116 |
ENGINE CONTROLS -POWER CONTROLS -INSPECTION OF THE FLIGHT IDLE STOP OVERRIDE KNOB |
SAAB340-76-041 |
| 1-117R1 |
WINGS -FLAPS -REPLACEMENT OF SUPPORT STRAP |
SAAB340-57-033R02 |
| 1-118R1 |
BAGGAGE NET PLACARDS |
340-25-244 rev 1 |
| 1-119R1 |
ICE & RAIN PROTECTION -ENGINE AIR INTAKE -MODIFICATION OF THE DETACHABLE CENTER INLET |
SAAB340-30-073R1 |
| 1-120 |
ICE & RAIN PROTECTION-AIRFOIL DE-ICING -INTRODUCTION OF NEW IMPROVED CHECK VALVE |
340-30-080 |
| 1-125 |
LANDING GEAR-EXTENSION AND RETRACTION-INSPECTION OF RELAY 15GA AND RELATED SOCKET |
340-32-115 |
| 1-127 |
LANDING GEAR-INSPECTION OF THE INSTALLATION COMBINATION OF THE BRAKE ASSEMBLIES |
340-32-114 |
| 1-128 |
ENGINE CONTROLS-POWER CONTROLS-SECURING CONTROL QUADRANT POWER CAM SCREW |
340-76-042 |
| 1-133 |
HORIZONTAL STABILIZERS-COLD EXPANSION OF HOLES IN FRONT SPAR OF HORIZONTAL STABILIZERS |
340-76-042 |
| 1-134 |
LANDING GEAR-WHEELS AND TIRES-EXAMINE AND REMOVE FROM SERVICE NOSE WHEEL ASSEMBLIES AND SUBASSEMBLIES THAT ARE NOT CORRECTLY HEAT TREATED |
340-32-116R1 |
| 1-135R1 |
POWER PLANT-MOUNTS-INSPECTION OF ENGINE MOUNTS AND REPLACEMENT IF NECESSARY- |
340-71-057 |
| 1-139R1 |
LANDING GEAR-BRAKES-INSPECTION OF THE INSTALLATION COMBINATION OF THE BRAKE ASSEMBLIES |
340-32-114 |
| 1-141 |
FUSELAGE-MAIN FRAME-MODIFYING INSULATION TO PREVENT INTERFERENCE WITH AILERON CONTROL MECHANISM |
SAAB 340-53-061 |
| 1-143 |
ENGINE CONTROLS-CONTROL QUADRANTS-INSPECTION OF FLIGHT IDLE STOP SOLENOID BRACKET SCREW |
SAAB 340-76-043 |
| 1-145 |
HYDRAULIC POWER-INTRODUCTION OF NEW SWIVEL BRACKETS |
SAAB 340-29-009R2 |
| 1-146 |
WINGS-ATTACH FITTINGS-INSPECTION OF THE BEARING HOUSINGS OF THE MAIN LANDING GEAR SUPPORT ASSEMBLY-IMPROVED NDT METHOD |
340-57-036 |
| 1-148 |
ENGINE CONTROLS -POWER CONTROLS -INSPECTION OF THE FLIGHT IDLE STOP OVERRIDE KNOB |
SAAB340-76-041 |
| 1-149 |
ELECTRICAL AND ELECTRONIC INSTALLATIONS-INSPECTION OF CHAFING AND INSTALLATION OF ADDITIONAL CHAFE PROTECTION ON HARNESS ROUTED IN THE CABIN COMPARTMENT CEILING |
340-92-027 |
| 1-151 |
FIRE PROTECTION-CARGO COMPARTMENT SMOKE DETECTORS-REPLACE FENWALL SMOKE DETECTOR WITH CERBERUS SMOKE DETECTOR |
340-26-023 |
| 1-152 |
WINGS-FLAPS-IDENTIFICATION AND FOR AFFECTED FLAPS, INSPECTION AND REPLACEMENT OF BOLT AND BUSHING INSTALLATION AT WS 123.38 |
340-57-035 |
| 1-153 |
WINGS-FLAPS-INSPECTION OF AFT ATTACHMENT LUG OF FLAP FITTINGS AT WS 123.38 |
340-57-037 |
| 1-155 |
LANDING GEAR-EXTENSION AND RETRACTION SYSTEM -INSTALLATION OF NEW CIRCUIT BREAKER FOR THE LANDING GEAR FUNCTION |
340-32-120 |
| 1-156 |
FUEL-INDICATION-INSPECTION OF THE ELECTRICAL CONNECTOR TO THE REFUEL/DEFUEL PANEL |
340-28-022 |
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1-161R2 |
STRUCTURES-INSPECTION OF REPAINTED AIRCRAFT FOR REMOVED PROTECTIVE COATING (ADHESIVELY BONDING PRIMER) AND POSSIBLE PITTING CORROSION |
340-51-020 |
| 1-167 |
NAVIGATION-PITOT AND STATIC SYSTEM-CHANGE OF MAIN PITOT STATIC TUBES |
340-34-145 |
| 1-169 |
ELECTRICAL POWER-REMOVAL OF TEST SWITCHES |
340-24-023 Rev 2 |
| 1-170 |
HYDRAULIC POWER-LIFE LIMITATION OF HYDRAULIC HOSES |
340-29-022 |
| 1-173 |
LANDING GEAR-INSTALLATION OF NEW RETRACT ACTUATOR BRACKET ATTACHMENT BOLT |
340-32-124 |
| 1-176 |
NACELLES-STRUCTURE-INSPECTION OF INTERNAL STRUCTURE |
340-54-043 |
| 1-184 |
FIRE PROTECTION-NACELLES/PYLONS-INSTALLATION AND MODIFICATION OF TAILPIPE HOT DETECTION HARNESS OR CHANGE OF THE SEALING AROUND THE TERMINAL LUGS ON THE FIRE DETECTORS AS APPLICABLE |
340-26-029 or 340-26-030 |
| 1-185 Cancelled |
LANDING GEAR-MAIN LANDING GEAR-REPLACEMENT OF ASSISTOR SPRING |
340-32-126 |
| 1-186 |
LANDING GEAR-MAIN LANDING GEAR-INSPECTION OF THE HARNESS FOR THE SEPARATION BOLT |
340-32-127 |
| 1-187 |
WINGS-PLATES/SKIN/MODIFICATION OF THE REFUELLING DOOR |
340-57-042 |
| 1-189 |
LANDING GEAR-MAIN LANDING GEAR-REPLACEMENT OF THE HARNESS FOR THE SEPARATION BOLT |
340-32-128 |
| 1-191 |
LANDING GEAR-MAIN LANDING GEAR-REPLACEMENT OF ASSISTOR SPRING |
340-32-126 |
| 1-192 |
POWER PLANT-MOUNTS-INSPECTION OF THE ENGINE BOTTOM MOUNTS FOR ELASTOMER TO METAL DEBONDING |
340-71-059 |
| 1-193 |
ICE & RAIN PROTECTION-WINDSHIELD WIPERS-INSPECTION OF THE WIPER ARM ASSEMBLY |
340-30-088 |
| 1-194 |
STRUCTURES-INSPECTION OF THE AILERON AND TRIM TAB FITTINGS |
340-51-025 |
