N87557

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 31,141 hrs · 36,752 cycles

FLIGHT: 4016 FPO/FLL NOSE GEAR INDICATOR DID NOT ILLUMINATE MANUALLY PUMPED GEAR AND LANDED, INDICATOR ILLUMINATED ON TAXI INTO GATE. REPLACED NOSE LANDING GEAR ACTUATOR OPERATIONAL CHECK GOOD.

Part: DOWNLOCK SWITCH — DEFECTIVE (NLG) · airframe 31,140 hrs · 36,750 cycles

FLIGHT:4021 TCB/FLL DURING APPROACH NOSE WHEEL GEAR GREEN INDICATOR DOWN LIGHT DID NOT ILLUMINATE ON EXTENSION BULB TESTED OK. REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH AND ANNUNCIATOR PCB OPERATIONAL CHECK NORMAL.

Part: DOWNLOCK SWITCH — DIRTY (NLG) · airframe 31,130 hrs · 36,738 cycles

FLIGHT: 4012 TPA/FLL NOSE GEAR GREEN LIGHT DID NOT COME ON LEFT AND RIGHT MAIN GEAR LIGHTS NORMAL. CLEANED NOSE GEAR DOWNLOCK SWITCH, OPERATIONAL CHECK NORMAL.

Part: ANNUNCIATOR — INOPERATIVE (COCKPIT) · airframe 31,059 hrs · 36,631 cycles

FLIGHT: 4017 TPA/FLL NOSE GEAR POSITION INDICATOR NOT LIGHTING. REMOVED AND REPLACED ANNUNCIATOR ASSEMBLY, OPERATIONAL CHECK NORMAL.

Part: ATTACH BRACKET — CRACKED (ENGINE MOUNT) · airframe 31,044 hrs · 36,608 cycles

DURING MAGNETIC PATRICLE INSPECTION DISCOVERED ENGINE TRUSS ENGINE MOUNT ATTACH BRACKET WELD AREA CRACKS. PERFORMED WELD REPAIR TO ENGINE MOUNT ATTACH BRACKET WELD AREAS.

Part: SKIN — CORRODED (RT WING) · airframe 30,941 hrs · 36,490 cycles

REPROT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT WING TRAILING EDGE SKIN HAD CORROSION AT WS 159.51. REMOVED CORROSION DAMAGE AND INSTALLED FILLER AND EXTERNAL DOUBLER REPAIR.

Part: LINE — LOOSE (OIL SYSTEM) · airframe 30,904 hrs · 36,432 cycles

FLIGHT:3989 MCO/PNS RIGHT ENGINE WAS LOSING OIL PRESSURE IN FLIGHT SECURED RIGHT ENGINE WITH 50 PSI STILL SHOWING ON THE GAUGE. DIVERTED TO GNV LANDED WITHOUT INCIDENT. SECURED OIL PRESSURE LINE TO TORQUE TRANSMITTER OPERATIONAL CHECK GOOD. NO LEAKS NOTED.

Part: SKIN — CORRODED (LT WING) · airframe 30,043 hrs · 35,373 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING TRAILING EDGE TOP HAS HOLE AT WING STATION 153.50. REMOVED DAMAGE AND INSTALLED AN EXTERNAL REPAIR DOUBLER.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 30,005 hrs · 35,336 cycles

FLIGHT: 4005 TPA/TPA DURING CLIMBOUT LOUD POP CAME FROM LEFT ENGINE FOLLOWED BY SMOKE COMING FROM PILOT AIR VENTS. SECURED AND SHUT DOWN LEFT ENGINE. NO PRIMARY OR SECONDARY INDICATION OF A FIRE. RETURNED TO TPA LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE.

Part: CIRCUIT BREAKER — INOPERATIVE (WARNING SYS) · airframe 29,585 hrs · 34,885 cycles

FLIGHT: TLH/FLL PILOT REPORTED LANDING GEAR WARNING HORN YOU CANNOT SILENCE IT. REPLACED CIRCUIT BREAKER (CB-1) ON RIGHT CIRCUIT BREAKER PANEL OPERATIONAL CHECK GOOD.

Part: TRANSFER TUBE — LEAKING (NR 1 ENGINE) · airframe 29,424 hrs · 34,675 cycles

FLIGHT: 4017 BIM/FLL PILOT REPORTED STRONG FUEL SMELL IN CABIN NOTICED WHEN BOTH ENGINES RUNNING AND LEFT BLEED OPEN. REPLACED FOUR TRANSFER TUBES AND ORINGS ON NUMBER ONE ENGINE FUEL NOZZLES AT SIX O`CLOCK POSITION LEAK CHECK GOOD.

Part: STRINGER — CORRODED (LT WING) · airframe 29,004 hrs · 34,178 cycles

DURING SCHEDULED X-RAY INSP, DISCOVERED .3750 INCH DIAMETER HOLE OF CORROSION ON THE LT WING "J" STRINGER AT WS 114.25. REMOVED CORROSION AND REPAIRED STRINGER.

Part: STRINGER — CORRODED (LT WING) · airframe 29,004 hrs · 34,178 cycles

DURING SCHEDULED X-RAY INSP, DISCOVERED MINOR SPOT OF CORROSION ON THE LT WING "J" STRINGER JUST OTBD OF WS 114.25. REMOVED CORROSION AND REPAIRED STRINGER.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,946 hrs · 34,062 cycles

DURING SCHDULED ROUTINE STRUCTURAL INSP, DISCOVERED RT WING TO FUSELAGE CLOSING ANGLE CRACKED 2.0 INCHES AT FORWARD END. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 28,946 hrs · 34,062 cycles

DURING SCHDULED ROUTINE STRUCTURAL INSP DISCOVERED CARGO DOOR FRAME CRACKED APPROX 2.0 INCHES AT TOP FORWARD AREA OF FRAME BETWEEN FS 456 AND FS 468.25. STOP DRILLED ENDS OF CRACK AND INSTALLED 10.0 INCH REPAIR DOUBLER.

Part: SKIN — CORRODED (BS 258) · airframe 28,946 hrs · 34,062 cycles

DURING SCHDULED ROUTINE STRUCTURAL INSPECTION, DISCOVERED SMALL AREA OF CORROSION APPROX .25 INCH DIAMETER FS 258 AT STRINGER 13L. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED 4.75 X 6.25 INCH COVER PATCH.

Part: HANDLE — LACK OF LUBE (EMERGENCY EXIT) · airframe 28,842 hrs · 33,951 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT FWD EXIT OUTER HANDLE STIFF TO OPERATE. LUBED RT FWD EMERGENCY EXIT OUTER HANDLE.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 28,679 hrs · 33,758 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL CANTED STABILIZER RIB CRACKS AT LEFT NR 2, 3 AND 4 STRINGERS AND RIGHT NR 3 STRINGER AT STATION 54.026. STOP DIRILLED ALL CRACKS VERTICAL STABILIZER RIBS LEFT AND RIGHT SIDE AND INSTALLED REPAIR DOUBLERS.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 28,679 hrs · 33,758 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED VERTICAL CANTED STABILIZER RIB CRACKS AT RIGHT NR 4 STRINGER AT STATION 89.184. STOP DIRILLED CRACK AT RIGHT VERTICAL STABILIZER RIB NR 4 STRINGER AND INSTALLED REPAIR DOUBLERS.

Part: HANDLE — STIFF (EMERGENCY EXIT) · airframe 28,679 hrs · 33,758 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT INNER HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT INNER AND OUTER HANDLES.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 28,679 hrs · 33,758 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED RT FWD EMERGENCY EXIT OUTER HANDLE STICKS WHEN OPERATED. LUBRICATED RT FWD EMERGECNY EXIT DOOR INNER AND OUTER HANDLES.

Part: LINE — LOOSE (BRAKE SYS) · airframe 28,581 hrs · 33,654 cycles

PILOT REPORTED LT BRAKE LINE LOOSE, LT PEDAL WENT TO THE FLOOR. SECURED BRAKE LINE BLED BRAKE AND SERVICED RESERVOIR LEAK CHECK OK.

Part: HANDLE — INOPERATIVE (EMERGENCY EXIT) · airframe 28,218 hrs · 33,213 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT DOOR OUTER HANDLE WILL NOT SPRING OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR OUTER HANDLE OPS CHECK GOOD.

Part: HANDLE — BINDING (EMERGENCY EXIT) · airframe 28,218 hrs · 33,213 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT FWD EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED RT FWORWARD EMERGENCY EXIT HANDLE, OPS CHECK GOOD.

Part: HANDLE — STICKING (EMERGENCY EXIT) · airframe 27,737 hrs · 32,671 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT EMERGENCY EXIT OUTER HANDLE STICKING. LUBED LT EMERGENCY EXIT OUTER HANDLE.

Part: O-RING — LEAKING (FUEL FILTER) · airframe 27,275 hrs · 32,159 cycles

DURING TEST FLIGHT WITH BLOWERS AND ENVIRONMENTAL ON AN EXTREME ODOR OF JET FUEL COMES THROUGH ACFT. FOUND FUEL LEAK AT RT FUEL FILTER BOWL REPLACED O-RING. PERFORMED ENGINE RUNS, NO EVIDENCE OF FUEL SMELL.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 27,275 hrs · 32,158 cycles

PILOT REPORTED CHECK FOR BIRD STRIKE ON RT OTBD WING. FOUND BIRD STRIKE ON RT OTBD WING L/E REPAIRED DAMAGED SECTION OF WING.

Part: CABLE — OUT OF TOLERANCE (PAX DOOR) · airframe 26,787 hrs · 32 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED AIRSTAIR DOOR CABLE TENSIONS AT 20 LBS. READJUSTED FWD AND AFT AIRSTAIR DOOR CABLE TENSIONS. OPS CHECK GOOD.

Part: TORQUE TUBE — CORRODED (LT ELEVATOR) · airframe 26,709 hrs · 31,563 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED LT ELEVATOR TORQUE TUBE, SHOWS SIGNS OF EXFOLIATION. REPLACED LT ELEVATOR TORQUE TUBE ASSY.

Part: SWITCH — OUT OF ADJUST (MLG) · airframe 26,656 hrs · 31,499 cycles

FLIGHT: 9271 FP PERCENT N1 ON LEFT ENGINE. ADJUSTED LANDING GEAR WARNING SWITCH AT LEFT ENGINE. TEST FLIGHT SATISFACTORY.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,041 hrs · 30,812 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED EMERGENCY EXIT 6F HAS SKIN DAMAGE UNDER WINDOW PAN. BLENDED DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER REPAIR.

Part: SKIN — CORRODED (BS 2280 S14L) · airframe 26,041 hrs · 30,812 cycles

DURING SCHEDULED ROUTINE MX, DISCOVERED CORROSION ON FUSELAGE BELLY SKIN AT FS 228, STRINGER 14L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER REPAIR.

Part: SNUBBER — STIFF (PAX DOOR) · airframe 25,804 hrs · 30,555 cycles

FLIGHT: 9130, PILOT REPORTED CABIN DOOR SNUBBER NEEDS TO BE SERVICED DIFFICULT TO CLOSE. SERVICED CABIN DOOR SNUBBER.

Part: CONTROL CABLE — BROKEN (AIRSTAIR DOOR) · airframe 25,740 hrs · 30,494 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED AIRSTAIR DOOR FWD LWR CONTROL CABLE BROKEN. REPLACED AIRSTAIR DOOR FWD LWR CONTROL CABLE.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 25,163 hrs · 29,897 cycles

DURING SCHEDULED INSP, HOLE FOUND IN LT SEAT TRACK INBD FWD CABIN SEAT BETWEEN FS 258.25 AND FS 273.25. REPAIRED LT SEAT TRACK BY INSTALLING A RIVET.

Part: ACTUATOR — INOPERATIVE (MLG) · airframe 25,092 hrs · 29,823 cycles

AFTER TAKEOFF WHEN GEAR SELECTED UP NOTHING HAPPENS ( NO RED HANDLE LIGHT NO GEAR MOTOR) FOR APPROX 2 SECONDS THEN LOUD NOISE JUST BEFORE GEAR STARTS TO RETRACT. REPLACED NOSE GEAR ACTUATOR, OPS CHECK NORMAL.

Part: CABLE — BROKEN (PAX DOOR) · airframe 24,852 hrs · 29,581 cycles

FLIGHT: 9244 FLL/GGT - PILOT REPORTED DOOR CABLE BROKEN. REPLACED TOP AFT AIRSTAIR DOOR CABLE AND LOWER FORWARD DOOR CABLE OPERATIONAL CHECK OK.

Part: CABLE — BROKEN (PAX DOOR) · airframe 24,852 hrs · 29,581 cycles

FLIGHT:9244 FLL/GGT - PILOT REPORTED DOOR CABLE BROKEN. REPLACED TOP AFT AIRSTAIR DOOR CABLE AND FORWARD AIRSTAIR DOOR CABLE. OPERATIONAL CHECK NORMAL.

Part: HORN — CORRODED (ELEVATOR TRIM) · airframe 24,656 hrs · 29,369 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR INBD TRIM TAB HORN EXFOLIATED. REPLACED RT ELEVATOR ASSY.

Part: UPLOCK SWITCH — SHORTED (LT MLG) · airframe 24,375 hrs · 29,106 cycles

AFTER TAKEOFF, LANDING GEAR UNSAFE RED LIGHT IN HANDLE REMAINS ON AFTER GEAR UP IS SELECTED. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED LT MAIN UPLOCK SWITCH. OPS CHECK NORMAL.

Part: DOOR — STUCK (AIRSTAIR) · airframe 24,153 hrs · 28,890 cycles

PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO OPEN. HANDLE OPERATES NORMALLY, BUT DOOR GETS STUCK. ADJUSTED AIRSTAIR DOOR CAMLOCK LATCHES.

Part: DOOR — STIFF (AIRSTAIR) · airframe 24,153 hrs · 28,890 cycles

PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO OPEN. HANDLE OPERATES NORMALLY, BUT DOOR GETS STUCK. ADJUSTED AIRSTAIR DOOR CAMLOCK LATCHES.

Part: POWERPACK — SLUGGISH (HYDRAULIC SYS) · airframe 23,786 hrs · 28,508 cycles

PILOT REPORTED LANDING GEAR EXTENSION AND RETRACTION TAKES EXTREME LONG TIME. REPLACED HYDR POWER PACK. OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — CONTAMINATED · airframe 23,769 hrs · 28,486 cycles

FLIGHT 9193 FLL/TLH - DURING APPROACH TRIED TO EXTEND THE LANDING GEAR AND THE LANDING GEAR CIRCUIT BREAKER POPPED. RESET THE CIRCUIT BREAKER AND THE GEAR EXTENDED. CONTINUED TO TLH LANDED WITHOUT INCIDENT. INSPECTED THE LANDING GEAR SYSTEM BLED AIR FROM THE SYSTEM. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL.

Part: LANDING GEAR — MALFUNCTIONED · airframe 23,765 hrs · 28,484 cycles

FLIGHT 9260 MIA/TPA - PILOT REPORTED NOSE LANDING GEAR TAKES EXTREMELY LONG TIME TO RETRACT AND EXTEND. PERFORMED LANDING GEAR SYSTEM OPERATIONAL CHECK. NO DEFECTS NOTED.

Part: KEELBEAM — CRACKED (LT NACELLE) · airframe 23,756 hrs · 28,474 cycles

DURING SCHEDULED ROUTINE MAINT DISCOVERED LT NACELLE INBD KEEL HAS A 1.0 INCH CRACK FWD OF LANDING GEAR TRUNION BOLT. REMOVED AND REPLACED LT NACELLE INBD KEEL.

Part: MOTOR — MALFUNCTIONED (LANDING GEAR) · airframe 23,606 hrs · 28,317 cycles

FLIGHT 9126 - NAS/FLL - AFTER TAKEOFF LANDING GEAR RETRACTION TOOK 14 SECONDS. REPLACED HYDRAULIC MOTOR. OPERATIONAL CHECK NORMAL.

Part: MOTOR — SLUGGISH (LANDING GEAR) · airframe 23,606 hrs · 28,317 cycles

FLIGHT 9126 - NAS/FLL - PILOT REPORTED GEAR RETRACTION TOOK 14 SECONDS. REMOVED AND REPLACED HYDRAULIC MOTOR.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR)

DURING SCHEDULED ROUTINE MX DISCOVERED LT ELEVATOR OTBD HINGE BRACKET CORRODED. REPLACED LT OTBD ELEVATOR HINGE BRACKET.

Part: CAM — OBSTRUCTED (PAX DOOR)

CABIN DOOR RT SIDE SECOND CAM FROM TOP IS RUBBING ON CAM LOCK MAKING DOOR HARD TO OPEN AND CLOSE. CLEANED EXCESSIVE GREASE AND GUM OUT OF CAM. (K)

Part: HINGE BRACKET — CORRODED (RT ELEVATOR)

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR OUTBOARD HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OUTBOARD HINGE BRACKET. (A)

Part: HINGE BRACKET — CORRODED (RUDDER) · airframe 23,059 hrs · 27,715 cycles

DURING SCHEDULED ROUTINE MAINT, DISCOVERED UPPER RUDDER HINGE BRACKET EXFOLIATED. REPLACED UPPER RUDDER HINGE BRACKET.

Part: HINGE — CORRODED (RUDDER)

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LOWER RUDDER HINGE EXFOLIATED. REPLACED LOWER RUDDER HINGE. (A)

Part: HINGE — CORRODED (RUDDER)

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED UPPER RUDDER HINGE EXFOLIATED. REPLACED UPPER RUDDER HINGE. (A)

Part: SKIN — CORRODED (FUSELAGE) · airframe 22,236 hrs · 26,763 cycles

DURING SCHEDULED ROUTINE INSP DISCOVERED FUSELAGE SKIN EXFOLIATED AT FS 225.250. REMOVED CORRODED SECTION OF FUSELAGE AND INSTALLED REINFORCEMENT DOUBLER REPAIR.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,679 hrs · 2,614 cycles

FLIGHT: 9131- DURING FLIGHT, STRONG ODOR COMING FROM THE OVERHEAD BLOWERS. PERFORMED OPERATIONAL CHECK OF VCM COULD NOT DUPLICATE ODOR. OPERATIONAL CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,360 hrs · 25,731 cycles

FLIGHT: 9133 JAX/TPA - AFTER TAKEOFF WITH BOTH BLEED AIR VALVES OPEN AND HEAT APPPLIED IN THE MANUAL MODE BURNED ODOR PERSISTS. ODOR WENT AWAY WHEN BLEED AIR VALVES WERE CLOSED. RAN ENGINES WITH BLEED VALVES OPEN FOR SEVERAL MINUTES COULD NOT DUPLICATE PROBLEM.

Part: COUPLING — DIRTY (EMERGENCY EXIT) · airframe 21,338 hrs · 25,703 cycles

EMERGENCY EXIT 6A INOPERATIVE, UNABLE TO OPEN. CLEANED AND LUBRICATED COUPLING ATTACHED TO EXTERIOR HANDLE.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,146 hrs · 25,478 cycles

FLIGHT: 9297, DURING FINAL APPROACH STRONG SWEET ODOR OBSERVED UNTIL TOUCHDOWN. PREFORMED ENGINE RUNS FOR 20 MINUTES WITH DIFFERENT ACM, VCM AND BLEED VALVE SETTINGS COULD NOT DUPLICATE.

Part: UNKNOWN — ODOR (CABIN) · airframe 21,139 hrs · 25,469 cycles

FLIGHT: 9175, DURING FLIGHT SWEET ODOR EMINATING FROM BLOWERS. INSPECTED BOTH ENGINE OIL LINES FOR OIL LEAKS, INSPECTED BLEED AIR LINES RAN BOTH ENGINES VCM AUTO AND MANUAL NO DEFECTS NOTED.

Part: WIRE — LOOSE (NR 1 NACELLE) · airframe 20,234 hrs · 24,382 cycles

FLIGHT: 9286 EYW/FLL DURING FLIGHT NR 1 ENGINE DISCHARGE LIGHT ILLUMINATED. FOUND WIRE SPLICE LOOSE AT NR 1 ENGINE FIRE BOTTLE. RESPLICED WIRE FROM FIRE EXTINGUISHER BOTTLE, OPERATIONAL CHECK GOOD.

Part: TIRE — FAILED (MLG) · airframe 20,069 hrs · 24,186 cycles

FLIGHT: 9209 ELH/FLL DURING TAKEOFF NR 3 TIRE TREAD CAME OFF CONTINUED TO FLL LANDED WITHOUT INCIDENT. REPLACED NR 3 MAIN WHEEL AND TIRE ASSEMBLY.

Part: WIRE — UNSECURE (FIRE BOTTLE)

FLIGHT:9250 MIA/MCO DURING FLIGHT LEFT ENGINE FIRE BOTTLE DISCHARGE ANNUNCIATOR ILLUMINATES AND EXTINGUISHES THROUGHOUT THE FLIGHT. SECURED WIRES AT THE LEFT ENGINE FIRE BOTTLE, OPERATIONAL CHECK GOOD.

Part: HINGE — CORRODED (RT HORZ STAB)

AT SCHEDULED INSPECTION, DETERMINED RT ELEVATOR CENTER HINGE BRACKET TO BE EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET. (K)

Part: HINGE — CORRODED (LT HORZ STAB)

AT SCHEDULED INSPECTION, DETERMINED LT ELEVATOR CENTER HINGE BRACKET TO BE EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET. (K)

Part: BRAKE — INADEQUATE (RT MLG)

DURING TAXI, RT BRAKE INEFFICIENT. BLED RT BRAKES. (K)

Part: ODOR — DETECTED (COCKPIT)

FLT 9191 - EYW/MCO - DURING FLIGHT, SMELLED SMOKE IN THE COCKPIT. DIVERTED TO RSW. LANDED WITHOUT INCIDENT. CLEANED CARBON FROM INTERNAL SCAVENGE PUMP SCREEN. OPERATIONAL CHECK OF OIL PRESSURE AND OIL TEMPERATURE SYSTEMS NORMAL. NO SMOKE NOTICED IN THE COCKPIT. (M)

Part: SEAL — TORN (AIRSTAIR DOOR)

FLT 9197 - TPA/FLL - DURING FLIGHT, CABIN EXPERIENCED RAPID DECOMPRESSION. PAX OXYGEN MASKS DEPLOYED. DIVERTED TO RSW. LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. FOUND AIRSTAIR DOOR SEAL OUT OF TRACK AND TORN AT 12 O'CLOCK POSITION. REMOVED AND REPLACED DOOR SEAL AND STOWED OXYGEN MASKS. OPERATIONAL CHECK NORMAL. (M)

Part: CONTROLLER — SHORTED (NAVAGATION)

DURING APPROACH, ODOR OF ELECTRICAL SMOKE WAS PRESENT IN THE COCKPIT, AND NR 1 NAVIGATION CONTROLLER WAS INOPERATIVE. REMOVED AND REPLACED NR 1 NAVIGATION CONTROLLER. OPERATIONAL CHECK NORMAL.

Part: MOTOR — SHORTED (TE FLAPS)

AFTER LANDING, DURING POST FLIGHT, BURNING ELECTRICAL ODOR COMING FROM CARGO AREA. REMOVED AND REPLACED FLAP MOTOR. OPERATIONAL CHECK NORMAL. (M)

Part: ENGINE — DAMAGED (RIGHT)

DURING OIL FILTER INSPECTION METAL FLAKES DISCOVERED. FURTHER INSPECTION OF THE RT ENGINE DETERMINED EXCESSIVE DISCOLORED (BLACK OIL). REPLACED THE RIGHT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR.

Part: OIL SYSTEM — CONTAMINATED (RT ENGINE)

AT SCHEDULED ROUTINE INSPECTION (LINE CHECK) THE RIGHT ENGINE WAS DETERMINED TO HAVE DISCOLORED OIL. CHANGE OIL AND OIL FILTER. PLACED ENGINE ON OIL WATCH.

Part: BULB (COCKPIT)

CLE FLIGHT#3196 THE CREW REPORTED THE RED LIGHT ON THE GEAR HANDLE WAS INOPERATIVE.MAINTENANCE REPLACED THE BULB ON THE GEAR HANDLE AND OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RESERVOIR — LACK OF LUBE (HYD SYSTEM)

CLE FLIGHT 3307 THE CREW REPORTED WHEN THE LANDING GEAR WAS EXTENDED ON FINAL APPROACH THE RIGHT GEAR WAS DELAYED FOR ABOUT ONE MINUTE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE LANDING GEAR HYDRAULIC RESERVOIR. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE LOOP — SHORTED (RT ENGINE)

CLE FLT 3307 THE CREW REPORTED RIGHT ENGINE FIRE DETECTION SYSTEM WOULD NOT TEST. MAINTENANCE REPLACED RIGHT ENGINE FIRE DETECTION CABLE ASSEMBLY. OPERATIONAL CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — INTERMITTENT (RIGHT GEAR)

CLE FLIGHT#3196 THE CREW REPORTED THE RIGHT GEAR LIGHT DID NOT ILLUMINTE ON THE 1ST GEAR EXTENSION.THE 2ND EXTENSION THE LIGHT ILLUMINATED.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE RIGHT GEAR ACTUATOR.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LINE — LOOSE (HYD SYSTEM)

CLE FLIGHT 3032 THE CREW REPORTED AFTER TAKEOFF THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. MAINTENANCE INSPECTED AND TIGHTENED THE PRESSURE LINE ON THE LANDING GEAR ACCUMULATOR AND SERVICED THE HYDRAULIC SYSTEM. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE LOOP — BROKEN (RT ENGINE)

CLE FLIGHT 3032 THE CREW REPORTED THE RIGHT FIRE LOOP AND FIRE T-HANDLE FLICKERED DURING FLIGHT FOR ABOUT 30 SECONDS AND STOPPED. ON FINAL APPROACH THE T-HANDLE STAYED ILLUMINATED AND THE MASTER WARNING ILLUMINATED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND THE CREW SHUT DOWN THE RIGHT ENGINE ON THE RUNWAY. THE CREW REPORTED THERE WAS NO FIRE DETECTED. MAINTENANCE INSPECTED AND FOUND THE RIGHT FIRE LOOP TO BE BROKEN. THE FIRE LOOP WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (LT GEAR)

CLE - FLT 3009 - AFTER TAKEOFF FROM CLE, THE LANDING GEAR WOULD NOT RETRACT. GREEN INDICATION LIGHTS REMAINED ON WITH NO INTRANSIT LIGHT. AIRCRAFT RETURNED TO CLE WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT MAIN LANDING GEAR ACTUATOR IAW BEECH MM 32-30-10. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: ACTUATOR — INOPERATIVE (LT MLG)

CLE - FLT 3009, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR IAW BEECH MM 32-30-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: HARNESS — FAILED (LANDING GEAR)

THE PILOT REPORTED THE RIGHT GEAR NEEDED TO BE CYCLED ONCE TO GET A DOWN AND LOCKED INDICATION LIGHT ON APPROACH. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT DOWN AND LOCKED SQUAT SWITCHES AND HARNESS IAW BEECHCRAFT MM 32-60-05, GEAR RETRACTION WAS GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: CONTROL HANDLE — FAILED (RT MLG)

THE PILOT REPORTED, ON FINAL APPROACH DID NOT GET A DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEAR. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW BEECHCRAFT MM 32-60-00 AND 32-30-00 OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: VERTICAL GYRO — MALFUNCTIONED (NR 2)

CLE - FLT 3056 - THE CREW REPORTED THE NR 2 EADI DISPLAY WENT BLANK IN-FLIGHT MOMENTARILY. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 VERTICAL GYRO IAW COLLINS CMM AND PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED TO SERVICE. (X)

Part: DEICE BOOT — FAILED (RT PROP)

CLE - FLT 3107 - CREW REPORTED AFTER TAKEOFF THE RIGHT PROP WAS ARCING WHEN PROP HEAT WAS TURNED ON, A GLOW WAS OBSERVED FROM THE SPINNER AND A BURNING SMELL WAS NOTICED. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE RIGHT PROP ASSEMBLY AND FOUD THAT ONE OF THE PROP BLADE BOOTS WAS BURNED. THE AIRCRAFT WAS RELEASED IAW MEL 30-10C CONTROL NR 127507. THE PROP ASSEMBLY WAS REMOVED AND REPLACED IAW B1900 MM 61-10-00 THE NEXT DAY. OPERATIONAL CHECKS SATISFACTORY. (M)

Part: BEARING — FAILED (NLG)

MBS - FLT 3242 - CREW REPORTED, ABORTED TAKEOFF DUE TO THE NLG WHEEL ASSEMBLY DEPARTING THE AIRCRAFT DURING THE TAKEOFF RUN. MAINTENANCE INSPECTED THE NLG AND WHEEL ASSEMBLY AND FOUND THE WHEEL BEARINGS TO BE FRICTION WELDED TO AXLE CAUSING THE DAMAGE. THE NOSE GEAR WHEEL ASSEMBLY WAS REMOVED AND REPLACED IAW B1900 MM 32-40-00. THE LOWER NLG STRUT ASSEMBLY WAS ALSO REMOVED AND REPALCED IAW B1900D MM 32-20-00, OPERATIONAL AND LEAKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: TUBE — BROKEN (LT WING)

CLE - FLT 3006 - CREW REPORTED THE RIGHT HAND BLEED AIR FAIL LIGHT ILLUMINATED IN-FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REPAIRED A BROKEN EVA TUBE IAW B1900D MM 26-11-00. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X)