N53545

Part: CABLE — BROKEN (DOOR) · airframe 34,037 hrs · 40,169 cycles

FLIGHT: 4052 EYW/FLL AIRSTAIR DOOR WILL NOT OPEN. REPLACED AIRSTAIR DOOR LOWER CABLE, OPERATIONAL CHECK OK.

Part: HINGE — CORRODED (ELEVATOR) · airframe 33,484 hrs · 39,470 cycles

DURING SCHEDULED ROUTINE C-6 INSPECTION DISCOVERED RIGHT ELEVATOR OUTBOARD HINGE HAS CORROSION. REPLACED RIGHT ELEVATOR OUTBOARD HINGE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,299 hrs · 39,269 cycles

FLIGHT: 4040 FLL/FLL PILOT REPORTED ON TAKEOFF BURNING PLASTIC SMELL IN COCKPIT WHEN BLEEDS WERE OPENED. VISUALLY INSPECTED BLEED LINES IN WINGS FUSELAGE AND CABIN NO DEFECTS NOTED PERFORMED ENGINE RUNS AT DIFFERENT POWER SETTINGS WITH BLEEDS ON AND OFF, NO SMELL OR DEFECT NOTED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 32,296 hrs · 39,263 cycles

DURING SCHEDULED C-5 INSPECTION DISCOVERED LEFT FUSELAGE SKIN CRACK BETWEEN FS 378.25 TO 393.25. REMOVED SKIN CRACK AND INSTALLED FILLER AND DOUBLER REPAIR.

Part: SKIN — CORRODED (RT WING) · airframe 32,572 hrs · 38,462 cycles

DURING SCHEDULED ROUTINE INSPECTION, DISCOVERED RT WING TOP TRAILING EDGE UPPER SKIN NEAR OUTBOARD FLAP BRACKET HAS TWO AREAS OF MILD SURFACE CORROSION. REMOVED DAMAGED AREA OF SKIN AND INSTALLED REPAIR FILLER AND AN EXTERNAL DOUBLER RAPAIR.

Part: PRINTED CKT BOARD — LOOSE (COCKPIT) · airframe 32,444 hrs · 38,310 cycles

FLIGHT 9248 PNS/MCO DURING CLIMB BOTH AUTOFEATHER ANNUNCIATOR AND AUTOFEATHER REPEATER LIGHT FLICKER INTERMITTENTLY LEFT SIDE. RESECURED ANNUNCIATOR PC BOARD ASSEMBLY (A129) OPERATIONAL CHECK GOOD.

Part: PRINTED CKT BOARD — FAULTY (AUTOFEATHER SYS) · airframe 32,432 hrs · 38,298 cycles

FLIGHT 9183 PNS/TPA PILOT REPORTED LEFT AFX AND GREEN LEFT AUTOFEATHER ANNUNCIATOR SIMULTANEOUSLY FLICKERS ON AND OFF WITH AUTO FEATHER ARMED. REPLACED AUTOFEATHER PCB.

Part: PRINTED CKT BOARD — MALFUNCTIONED (WARNING SYSTEM) · airframe 32,421 hrs · 38,284 cycles

FLIGHT 2254 PNS/TPA PILOT REPORTED LEFT AFX AND LEFT AUTOFEATHER ANNUNCIATOR BLINKING ON AND OFF WHEN AUTOFEATHER IS ARMED. RERACKED ANNUNCIATOR FAULT CONTROL PCB OPERATIONAL CHECK GOOD.

Part: SPAR — CORRODED (LT WING) · airframe 32,012 hrs · 37,792 cycles

DURING SCHEDULED ROUTINE X-RAY INSPECTION DISCOVERED CORROSION ON LEFT WING FORWARD SPAR AFT FLANGE WS 128.50. REMOVED CORROSION FROM FORWARD SPAR AFT FLANGE AND INSTALLED REINFORCEMENT DOUBLER STRAP.

Part: SKIN — CORRODED (BS 258 S15R) · airframe 31,994 hrs · 37,769 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED CORROSION ON EXTERIOR SKIN AT STRINGER 15R, APPROX FS 258. REMOVED CORROSION AND INSTALLED 3 X 5 INCH INSERTION PATCH AND 5 X 8 INCH COVER PATCH.

Part: STRINGER — DEBONDED (BS 378-398) · airframe 31,994 hrs · 37,769 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED STRINGER 15R DEBONDED AT APPROXIMATELY FS 378 AND FS 398. INSTALLED EXTERNAL REPAIR DOUBLER STRINGER 15R FROM FS 478 TO FS 400.

Part: STRINGER — DEBONDED (BS 412) · airframe 31,994 hrs · 37,769 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED STRINGER 15L DEBONDED AT APPROXIMATELY FS 412. INSTALLED EXTERNAL REPAIR DOUBLER STRINGER 15L FROM FS 404 TO FS 421.

Part: STRINGER — DEBONDED (BS 235 S15R) · airframe 31,994 hrs · 37,769 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED STRINGER 15R DEBONDED AT APPROXIMATELY FS 235. INSTALLED EXTERNAL REPAIR DOUBLER STRINGER 15R FROM FS 229 TO FS 241.

Part: STRINGER — DEBONDED (BS 412-398 S14L) · airframe 31,994 hrs · 37,769 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED STRINGER 14L DEBONDED AT APPROXIMATELY FS 412 AND FS 398. INSTALLED EXTERNAL REPAIR DOUBLER FROM FS 392 TO FS 412.

Part: DOOR FRAME — CRACKED (CARGO DOORWAY) · airframe 31,994 hrs · 37,769 cycles

DURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED CRACK 5.0 INCHES INTERIOR UPPER CARGO DOOR FRAME APPROX AT FS 496 TO 501. STOP DRILLED CRACK AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 31,993 hrs · 37,768 cycles

PILOT REPORTED NR 1 ENG N1 AND TORQUE DECREASED CONTINUOUSLY IN FLIGHT WHEN TORQUE REACHED 0 ENGINE SECURED. DIVERTED, LANDED WITHOUT INCIDENT. (OPEN)

Part: FUEL CONTROL — FAILED (LT ENGINE) · airframe 31,992 hrs · 37,767 cycles

PILOT REPORTED INFLIGHT THE LEFT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED, DECLARED AN EMERGENCY DIVERTED TO JAX SECURED THE ENGINE LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL CONTROL AND HIGH PRESSURE FUEL PUMP GROUND PERFORMANCE CHECK WITH POWER ASSURANCE RUN OPERATIONAL CHECKED GOOD.

Part: HEATER — DAMAGED (FUEL/OIL) · airframe 31,992 hrs · 37,767 cycles

PILOT REPORTED LT ENGINE N1 AND TORQUE DECREASED CONTINUOUSLY IN FLIGHT TORQUE, WHEN TORQUE REACHED ZERO. DIVERTED, SECURED THE LT ENGINE, LANDED WITHOUT INCIDENT. REPLACED LT ENGINE FUEL TO OIL HEATER. OPS CHECKED GOOD, TEST FLIGHT SATISFACTORY. PREVIOUSLY SUBMITTED (OPEN GUUA94531031511A)

Part: SKIN — DAMAGED (BS 408 BELLY) · airframe 31,906 hrs · 37,660 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED FUSELAGE BELLY SKIN DAMAGE AT FS 408.25 NEAR NR 2 COMM ANTENNA. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: ISOLATION MOUNT — CRACKED (LEFT) · airframe 31,707 hrs · 37,439 cycles

DURING MAGNETIC PARTICLE INSP DISCOVERED LT LOWER ISOLATOR MOUNT WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE TRUSS TUBE WELD AREAS.

Part: AUTOFEATHER SYS — DISENGAGED (PROPELLER) · airframe 31,663 hrs · 37,396 cycles

PILOT REPORTED AFTER DEPARTURE ( AROUND 2000 FT) LT AUTO FEATHER DISARMED AND WOULD NOT ARM AGAIN. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED AUTOFEATHER PCB A-123, OPS CHECK GOOD.

Part: AUTOFEATHER SYS — FAILED (PROPELLER) · airframe 31,663 hrs · 37,396 cycles

PILOT REPORTED UPON CLIMB OUT LT AUTO FEATHER FAILED TO ARM, DIFFERENT TORQUE SETTINGS WILL MAKE IT FLICKER BUT 10 SECONDS LATER IT WILL FAIL. RETURN TO DEPARTURE, LANDED WITHOUT INCIDENT. SECURED LOOSE PIN AT PCB A129, OPS CK GOOD.

Part: CONNECTOR — FAILED (AUTOFEATHER SYS) · airframe 31,663 hrs · 37,396 cycles

PILOT REPORTED ON DESCENT, LT AUTOFEATHER ANNUNCIATION FAILED FOLLOWED BY RT AUTOFEATHER ANNUNCIATION ON THE GROUND. REPLACED PCB A129 CONNECTOR, OPS CHECKED NORMAL.

Part: SWITCH — INTERMITTENT (WARNING HORN) · airframe 31,320 hrs · 37,036 cycles

PILOT REPORTED GEAR WARNING HORN CANCELLATION BUTTON INTERMITTENTLY INOPERATIVE. REPLACED LANDING GEAR WARNING HORN SILENCE SWITCH. LANDING GEAR OPS CHECK GOOD.

Part: POWERPACK — INOPERATIVE (MLG) · airframe 31,270 hrs · 36,973 cycles

DURING APPROACH, WHEN THE LANDING GEAR HANDLE WAS LOWERED THE LANDING GEAR CIRCUIT BREAKER POPPED AND THE GEAR FAILED TO EXTEND. THE GEAR HANDLE WAS RAISED, CIRCUIT BREAKER RESET, AGAIN WITH THE SAME RESULTS. MANUALLY EXTENDED THE LANDING GEAR THE GEAR ACCOMPLISHED ALL 3 GREEN LIGHTS. REPLACED LANDING GEAR POWER PACK MOTOR OPERATIONAL CHECK GOOD.

Part: POWERPACK — INOPERATIVE (MLG) · airframe 31,270 hrs · 36,973 cycles

DURING APPROACH WHEN THE LANDING GEAR HANDLE WAS LOWERED, THE LANDING GEAR CIRCUIT BREAKER POPPED AND THE GEAR FAILED TO EXTEND. THE GEAR HANDLE WAS RAISED, CIRCUIT BREAKER RESET AGAIN WITH THE SAME RESULTS. MANUALLY EXTENDED THE LANDING GEAR. THE GEAR ACCOMPLISHED ALL 3 GREEN LIGHTS. REPLACED LANDING GEAR POWERPACK MOTOR. OPS CHECK GOOD.

Part: COUPLING — LEAKING (FUEL SYSTEM) · airframe 30,908 hrs · 36,569 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED FUEL LEAKING FROM BOTTOM OF RT NACELLE. REPLACED WIRE HARNESS TUBING COUPLING ASSY AT FUEL ACCESS PANELS 642 BB AND 642CB APPLIED SEALANT AT COUPLING AND REPLACED PRC AROUND CONDUIT NEXT TO AUX PUMP LEAK CHECK GOOD.

Part: SPAR — DAMAGED (WING) · airframe 30,015 hrs · 35,581 cycles

COMPLIED WITH COLD EXPANSION OF FASTENER HOLES IN THE WING REAR SPAR LOWER CAP IAW FAA APPROVED DATA CONTAINED IN THE MFG ACFT COMPANY KIT 118-4014-0003.

Part: LIGHT — INOPERATIVE (MLG HANDLE) · airframe 29,750 hrs · 35,279 cycles

DURING APPROACH LANDING GEAR HANDLE BOTTOM HANDLE LIGHT INOPERATIVE. SECURED LANDING GEAR HANDLE BOTTOM LIGHT OPS CHECK GOOD.

Part: ACTUATOR — STUCK (MLG) · airframe 29,728 hrs · 35,251 cycles

DURING EXTENDED DOWNWIND LANDING GEAR WARNING HORN SILENCE BUTTON DOES NOT SILENCE GEAR WARNING HORN WHEN POWER LEVERS REDUCED BELOW 87 PERCENT N1 AND LOWER. TROUBLESHOT SYS FOUND STEERING DISCONNECT ACTUATOR STUCK. REPLACED STEERING DISCONNECT ACTUATOR.

Part: UPLOCK SWITCH — OUT OF ADJUST (MLG) · airframe 29,346 hrs · 34,808 cycles

DURING CLIMB, RED GEAR WARNING LIGHT IN HANDLE STAYS ILLUMINATED IN FLIGHT WITH GEAR IN THE UP POSITION. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ADJUSTED NOSE GEAR UPLOCK SWITCH. LANDING GEAR OPS CHECK GOOD.

Part: SQUAT SWITCH — INOPERATIVE (RT MLG) · airframe 29,044 hrs · 34,491 cycles

AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED RT LANDING GEAR SQUAT SWITCH. OPS CHECK OK.

Part: SAFETY SWITCH — LOOSE (MLG)

AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT GO TO THE UP POSITION, AFTER DOWN LOCK RELEASE HANDLE WENT UP GEAR HORN SOUNDED AND LOLLY POP WAS RED. CYCLED GEAR WITH NO CHANGE PUT GEAR DOWN GOT 3 GREEN INDICATION. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. RESECURED RT SAFETY SWITCH PROPERLY CHECKED RIGGING OF RT SAFETY SWITCH. ALL CHECKS NORMAL.

Part: HINGE — CORRODED (LT ELEVATOR) · airframe 28,208 hrs · 33,645 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR OTBD HINGE BLOCK SHOWING SIGNS OF EXFOLIATION. REPLACED LT ELEVATOR.

Part: TORQUE TUBE — CORRODED (RT ELEVATOR) · airframe 28,208 hrs · 33,645 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR TORQUE TUBE BASE SHOWS SIGNS OF EXFOLIATION. REPLACED RT ELEVATOR TORQUE TUBE.

Part: SPAR — CORRODED (LT WING) · airframe 27,699 hrs · 33,085 cycles

DURING SCHEDULED INSPECTION DISCOVERED BIO-CORROSION ON LEFT WING MAIN SPAR LOWER AFT SPAR FLANGE AT WS 117. BLENDED OUT ALL CORROSION FILLED AREA OF REPAIR AND INSTALLED REINFORCEMENT DOUBLER STRAP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,699 hrs · 33,085 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED .25 INCH CRACK, AND SKIN CORROSION ON FUSELAGE BELLY AT FS 438.25 STRINGER 16. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIRS.

Part: SKIN — CRACKED (BS 290) · airframe 27,699 hrs · 33,085 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED .5 INCH CRACK AT RIGHT FS 290.50 RBL 29.06. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER REPAIR.

Part: POWERPACK — MALFUNCTIONED (MLG) · airframe 27,762 hrs · 33,146 cycles

FLIGHT: 9142. DURING FLIGHT, LANDING GEAR POWERPACK MOTOR CYCLES ABOUT EVERY 15 TO 20 SECONDS LOAD METER SPIKES ABOUT 10 AMPS. REPLACED LT MLG ACTUATOR. OPERATIONAL CHECK OK.

Part: RELAY — SHORTED (MLG) · airframe 27,557 hrs · 32,915 cycles

FLIGHT NR 9201 EYW/FLL DURING APPROACH UPON LANDING GEAR EXTENSION LANDING GEAR CIRCUIT BREAKER POPPED. NOSE GEAR LOCKED INDICATION DID NOT APPEAR. MANUALLY PUMPED NOSE GEAR DOWN. REPLACED K3 LANDING GEAR MOTOR RELAY. OPS CHECK NORMAL.

Part: RESERVOIR — LOW (MLG) · airframe 27,534 hrs · 32,892 cycles

FLIGHT NR 9168 PNS/MCO DURING APPROACH, UPON LANDING GEAR EXTENSION LANDING GEAR CIRCUIT BREAKER POPPED. CLEANED, INSPECTED AND SERVICED THE MLG RESERVIOR. LANDING GEAR OPS CHECK NORMAL. NO DEFECTS NOTED.

Part: CAM — OUT OF ADJUST (ASD)

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AIRSTAIR DOOR DIFFICULT TO OPEN AND CLOSE. RE-ADJUSTED AIRSTAIR DOOR CAM. OPERATIONAL CHECK NORMAL.

Part: DOOR — STIFF (AIRSTAIR) · airframe 27,177 hrs · 32,537 cycles

FLT 9254- PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO CLOSE. PERFORMED OPERATIONAL CHECK OF AIRSTAIR DOOR. OPERATIONAL CHECK GOOD.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT)

DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT EMERGENCY EXIT DOOR DOES NOT CLOSE PROPERLY. READJUSTED LT EMERGENCY EXIT DOOR. (K)

Part: CABLE — FAILED (AIRSTAIR DOOR) · airframe 25,720 hrs · 30,961 cycles

PILOT REPORTED AIRSTAIR DOOR WILL NOT OPEN. REPLACED UPPER AIRSTAIR DOOR CABLES.

Part: DOOR — DELAMINATED (EMERGENCY EXIT) · airframe 25,623 hrs · 30,847 cycles

FLIGHT: 5402, PILOT REPORTED LT EMERGENCY EXIT IS DELAMINATED. REPLACED LT EMERGENCY EXIT.

Part: ACTUATOR — BYPASSING (RT MLG) · airframe 25,622 hrs · 30,846 cycles

FLIGHT: 9149, DURING FLIGHT DC LOAD METERS BOTH SPIKE 20 PERCENT EVERY 20 SECONDS. REPLACED THE RT MLG ACTUATOR.

Part: HINGE — CORRODED (ELEVATOR) · airframe 25,071 hrs · 30,212 cycles

REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REPLACED LT OB ELEVATOR HINGE BRACKET.

Part: WIRE — CHAFED · airframe 24,963 hrs · 30,081 cycles

FLIGHT:9152 EYW/TPA DURING APPROACH ADF BEGAN SMOKING AND CIRCUIT BREAKER POPPED TURNED OFF ADF AND SMOKE CEASED. CONTINUED, LANDED WITHOUT INCIDENT. REPAIRED CHAFED WIRE SYSTEM OPERATIONAL CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,880 hrs · 29,983 cycles

FLIGHT: 2043 TNT/FLL, DURING FLIGHT AIRCRAFT COCKPIT SMELLS LIKE FUEL THE ODOR WAS OVERWELMING. INSPECTED AIRCRAFT FOUND NO EVIDENCE OF FUEL LEAK. PERFORMED ENGINE RUNS AT VARIOUS POWER SETTINGS NO FUEL ODOR NOTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 24,617 hrs · 29,653 cycles

FLIGHT:9249 DURING FLIGHT MILD CHEMICAL ODOR LIKE HYDRAULIC FLUID COMING THRU THE ENVIRONMENTAL SYSTEM. PERFORMED OPERATIONAL CHECK OF THE ENVIRONMENTAL SYSTEM COULD NOT DUPLICATE. OPERATIONAL CHECK GOOD.

Part: SQUAT SWITCH — LOOSE (MLG) · airframe 24,590 hrs · 29,623 cycles

FLIGHT: 9223 AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. ADJUSTED RT MAIN LANDING GEAR SQUAT SWITCH. LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: PIN — DIRTY (EMERGENCY DOOR) · airframe 23,984 hrs · 28,913 cycles

ON PRE-FLIGHT INSPECTION, 6A EMERGENCY EXIT DOES NOT FUNCTION PROPERLY LOCKED AND WILL NOT OPEN. LUBED AND ADJUSTED LOCK PINS.

Part: WIRE — UNSECURE (FIRE BOTTLE) · airframe 23,222 hrs · 28,000 cycles

FLIGHT:9193 NAS/FLL - DURING LANDING, THE NR 1 FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED THREE TIMES. SECURED WIRE ON THE NR 1 FIRE EXTINGUISHER BOTTLE.

Part: WIRE HARNESS — CHAFED (COCKPIT) · airframe 23,188 hrs · 27,958 cycles

FLIGHT: 9255, AFTER TAKEOFF SMOKE IN THE COCKPIT COMING FROM ADF. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. SECURED AND PROTECTED CHAFING WIRE BUNDLE BEHIND ADF CONTROL HEAD ADF ALSO REPLACED ADF CIRCUIT BREAKER OPERATIONAL CHECK NORMAL.

Part: SKIN — CORRODED (BS 363 S13L) · airframe 23,100 hrs · 27,866 cycles

AT SCHEDULED INSPECTION DISCOVERED LT FUSELAGE SKIN DAMAGE DUE TO CORROSION. LOCATED AT F.S.363.250 STRINGER 13L CUT OUT SECTION OF CORRODED SKIN 2.0 IN X 5.0 IN FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER IAW STRUCTURAL REPAIR MANUAL 51-70-06.

Part: ANNUNCIATOR — MALFUNCTIONED · airframe 23,100 hrs · 27,855 cycles

FLIGHT: 9128 VPS/TPA, DURING TAKEOFF LT DISCHARGE LIGHT ANNUNCIATED CONTINUED TO TPA, LANDED WITHOUT INCIDENT. INSPECTED DISCHARGE SYSTEM AND OPERATIONAL CHECK NO DEFECT NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 23,100 hrs · 27,855 cycles

FLIGHT: 9128 VPS/TPA DURING TAKEOFF LT DISCHARGE LIGHT ANNUNCIATED CONTINUED TO TPA LANDED WITHOUT INCIDENT. INSPECTED DISCHARGE SYSTEM AND OPERATIONAL CHECK NO DEFECT NOTED.

Part: UPLOCK SWITCH — OUT OF ADJUST (LT MLG) · airframe 22,859 hrs · 27,577 cycles

FLT 9292 JAX/TPA DURING FLIGHT THE LANDING GEAR HANDLE LIGHT ILLUMINATED AFTER TAKEOFF AND FLICKERED DURING FLIGHT WITH THE GEAR RETRACTED. CONTINUED, LANDED WITHOUT INCIDENT. ADJUSTED THE RT MAIN LANDING GEAR UPLOCK SWITCH, LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: BRAKE — WEAK (MLG)

FLIGHT:9196 GGT/FLL DURING TAXI LEFT BRAKE SINKS LOW TO THE FLOOR WHEN DEPRESSED. BLED LEFT BRAKES, OPERATIONAL CHECK GOOD.

Part: PRESSURE PANEL — CRACKED (NLG WW)

SEVERAL SMALL CRACKS IN NOSE WHEEL WELL CEILING FROM NOSE WHEEL TIRE IMPACT DUE TO NOSE UP LANDING. DAMAGE LOCATION AT FUSELAGE STA 81, WATER LINE 100.00 AT CENTER BUTT LINE. REMOVED DAMAGE AREA AND INSTALLED EXTERNAL DOUBLER IAW MM. (K)

Part: BRACKET — CORRODED (ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET.

Part: BRACKET — CORRODED (ELEVATOR)

AT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET.

Part: SPAR — CRACKED (HORIZONTAL STAB)

AT SCHEDULED EMPENNAGE ZONE INSPECTION, FOUR CRACKS FOUND RADIATING FROM PASSAGE HOLE IN FORWARD WEB OF THE HORIZONTAL STABILIZER FORWARD SPAR. STOP DRILLED CRACKS. FABRICATED AND INSTALLED AND EXTERNAL DOUBLER IAW FAA APPROVED DATA CONTAINED IN THE BEECH 1900D AIRLINER SERIES STRUCTURAL REPAIR MANUAL, CHAPTER 55-91-02. (M)

Part: RIB — CRACKED (VERTICAL STAB)

AT SCHEDULED ROUTINE INSPECTION, VERTICAL STABLIZER FORWARD TOP RIB HAS TWO CRACKS ON STRESS RELIEF HOLES. REPAIRED VERTICAL STABILIZER FORWARD TOP RIB BY INSTALLING TWO REPAIR DOUBLERS AT THE END OF CRACKS IAW BEECH 1900D STRUCTURAL REPAIR MANUAL 51-70-17, FIGURE 1, PAGE 2 JUNE/99. (M)

Part: TRUSS — CRACKED (RIGHT ENGINE)

AT SCHEDULED ROUTINE MAINTENANCE, RIGHT ENGINE TRUSS BRACKETS FOR COWLING CRACKS AT EXISTING WELD, LEFT UPPER, LEFT LOWER, RIGHT UPPER BRACKETS. REMOVED ENGINE TRUSS AND REPAIRED IAW FAA APPROVED DATA CONTAINED IN RAYTHEON KIT 129-9017, STEPS 17 THROUGH 22. (M)

Part: BEARING — WORN · airframe 14,297 hrs · 17,433 cycles

INTERMITTENT VIBRATION FELT IN CONTROL WHEEL IN FLIGHTDETERMINED RIGHT YOKE BEARING TO BE WORN, BUT WITHIN LIMITS. REPLACED RIGHT AILERON YOKE BEARING

Part: BLOWER — SHORTED (CABIN)

AFTER AIRCRAFT POWER IS TURNED ON SMOKE IN AIRCRAFT. INSPECTED AIRCRAFT. REMOVED AND REPLACED AFT VENT BLOWER. OPERATIONAL CHECK NORMAL.

Part: BOLT — LOOSE (VERTICAL STAB)

AT SCHEDULED ROUTINE INSPECTION VERTICAL SPAR SECURITY CHECK ATTACH BOLTS REQUIRED RETORQUE. RETORQUED FOUR LOWER VERTICAL BOLTS IAW MM.

Part: EXTINGUISHER — MALFUNCTIONED (LT ENGINE)

FLT 9317 - FLL/ELH - AFTER TAKEOFF, THE LEFT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED, THEN WENT OUT. AIRCRAFT RETURNED TO FLL AND LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE FIRE EXTINGUISHER ASSEMBLY. (M)

Part: SQUIB — DIRTY (LT FIRE BOTTLE)

FLT 9242 - FPO-FLL - DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED. INSPECTED AND CLEANED LEFT FIRE BOTTLE SQUIB. OPS CHECK NORMAL. (M)

Part: SQUIB — DIRTY (LT FIRE BOTTLE)

FLT 9242 - FPO-FLL - DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED. INSPECTED AND CLEANED LEFT FIRE BOTTLE SQUIB. OPS CHECK NORMAL. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

FLT 9144 - FPO/FLL - DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT CAME ON. SECURED FIRE SQUIB WIRES ON LEFT SIDE. SYSTEM OPS TEST NORMAL. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

FLT 9476 - MCO/MIA - DURING FLIGHT, LEFT FIRE EXTINGUISHER DISCHARGE LIGHT CAME ON. INSPECTED SYSTEM. CLEANED WIRES OF OIL. SYSTEM OPS TEST NORMAL. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (FIRE PROTECTION)

FLT 9481 - PBI/TPA - DURING FLIGHT, LEFT ENGINE FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR CAME ON. PERFORMED OPERATIONAL TEST OF LEFT ENGINE FIRE EXTINGUISHER ANNUNCIATOR. COULD NOT DUPLICATE. OPERATIONAL TEST NORMAL. (M)

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

FLT 9481 - PBI-TPA - DURING FLIGHT, LEFT ENGINE FIRE DISCHARGE ANNUNCIATOR ILLUMINATED. PERFORMED OPERATIONAL TEST OF LEFT ENGINE. DISCHARGE ANNUNCIATOR, OPS TEST NORMAL. (M)

Part: INDICATOR — FAULTY (COCKPIT)

FLT 9507 - EYW-TPA - DURING FLIGHT, LEFT ENGINE OIL TEMPERATURE WENT TO 130 DEGREES AND BANGING NOISES WERE HEARD COMING FROM THE ENGINE. TROUBLESHOT OIL TEMPERATURE SYSTEM. DETERMINED OIL TEMPERATURE INDICTOR TO BE AT FAULT. REMOVED AND REPLACED INDICATOR. PERFORMED ENGINE RUNS, NO BANGING NOISES DETECTED. OPERATIONAL CHECK NORMAL. (M)

Part: SWITCH — FAILED (NR 1 ENGINE)

CLE - FLT 3001 - THE CREW REPORTED THE NR 1 ENGINE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PULL HANDLE SWITCH ASSEMBLY IAW BEECHCRAFT MM 26-20-00. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: INDICATOR — FAILED (RT ENGINE)

CLE - FLT 3129 - THE CREW REPORTED THE RIGHT TQ DID NOT INCREASE OR RISE DURING TAKEOFF, IT WAS STUCK AT 300. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT TQ INDICATOR IAW B1900D MM 77-10-00 OPERATIONAL CHECK WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: PROP ASSEMBLY — WORN (LT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, THE LEFT HAND PROPELLER ASSEMBLY WAS FOUND TO HAVE ONE BLADE WITH EXCESSIVE FORE/AFT AND SIDE/SIDE MOVEMENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND PROPELLER ASSEMBLY IAW B1900 MM 61-10-00. THE OPERATIONAL LEAK CHECKS INCLUDING BALANCE WERE SATISFACTORY. ACFT TOTAL TIME 3,272.6 HOURS. ACFT TOTAL CYCLES, 4,191. (X)

Part: COMPRESSOR — BLADES DAMAGED (RT ENGINE)

CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND ENGINE COMPRESSOR BLADES WERE FOUND DAMAGED BEYOND LIMITS BY UNKNOWN FOREIGN OBJECTS. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE IAW B1900D MM 71-00-00. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. ACFT TT: 3,272.6 HOURS. ACFT TC 4,191. (X)