N69547

Part: LINE — CRACKED (RT MLG) · airframe 31,700 hrs · 40,812 cycles

FLIGHT: 4068 DUJ PILOT REPORTS RIGHT MAIN LANDING GEAR DOES NOT FULLY RETRACT, NO INDICATION IN THE COCKPIT. FOUND PRESSURE RELIEF LINE CRACKED. REPLACED LINE, OPERATIONAL CHECKS GOOD.

Part: KEELBEAM — CORRODED (RT NACELLE) · airframe 31,142 hrs · 39,728 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT NACELLE INBOARD KEEL BEAM UPPER ATTACHMENT HOLE FOR TRUSS APPEARS TO HAVE A CRACK AND HAS CORROSION. REPLACED RIGHT NACELLE UPPER KEEL WEB.

Part: KEELBEAM — CORRODED (NACELLE) · airframe 31,142 hrs · 39,728 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT NACELLE INBOARD KEELBEAM LOWER ATTACHMENT HOLE FOR TRUSS APPEARS TO HAVE A CRACK AND HAS CORROSION. REPLACED RIGHT INBOARD LOWER KEEL WEB.

Part: CABLE — DEFECTIVE (CABIN DOOR) · airframe 30,398 hrs · 38,275 cycles

FLIGHT: 4069 CLE/DUJ PILOT REPORTED AFT CABIN DOOR LATCHES INOPERATIVE. REPLACED CABIN DOOR AFT LOWER CABLE OPERATIONAL CHECK GOOD.

Part: TRUSS — DAMAGED (ENGINE) · airframe 29,485 hrs · 36,490 cycles

REPORT: DURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS TUBE DAMAGED. PERFORMED ENGINE TRUSS REPAIR IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN DRAWING 1005272-5, 8110-3, DERT-510208-CE.

Part: BRAKE SYS — CONTAMINATED (LEFT) · airframe 30,122 hrs · 37,734 cycles

FLIGHT: 4070 FKL/DUJ PILOT REPORTED PLEASE INSPECT LEFT BRAKES WHEN TURNING LEFT BRAKE PEDAL FEELS WEAK. PERFORMED BRAKE SYSTEM BLEEDING OPERATIONAL CHECK GOOD.

Part: INDICATOR — INTERMITTENT (MLG) · airframe 29,816 hrs · 37,108 cycles

FLIGHT:9292 CLE/DUJ PILOT REPORTED NOSE GEAR ANNUNCIATOR LIGHT INTERMITTENT ON THE GROUND AND IN FLIGHT. RESEATED CONNECTION ON LEGEND ASSY LANDING GEAR OPS CHECKS GOOD.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 29,696 hrs · 36,878 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AFT CARGO DOOR FRAME CRACKED APPROXIMATELY 90% OF WIDTH AND 3.5 INCHES LENGTH AT APPROXIMATELY FS 509.50 STRINGER 10L. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED NEW SECTION OF FRAME.

Part: WIRE — CHAFED (MLG WARNING HORN) · airframe 29,696 hrs · 36,878 cycles

FLIGHT: 9294 ON DESCENT GEAR WARNING HORN COULD NOT BE SILENCED. REPLACED PCB A119 AND REPLACED FOUR INCH SECTION OF CHAFED WIRE G35A22 OPERATIONAL CHECK GOOD.

Part: CONTROL HANDLE — STIFF (MLG) · airframe 29,633 hrs · 36,758 cycles

PILOT REPORTED LANDING GEAR HANDLE STIFF TO LOWER IT FEELS LIKE ITS CATCHING. INSPECTED CLEANED J HOOK AND HANDLE SLIDE, ASSY CYCLED GEAR SEVERAL TIMES LANDING GEAR OPS CHECK GOOD, NO DEFECTS NOTED.

Part: CIRCUIT BOARD — LOOSE (AUTOFEATHER SYS) · airframe 29,629 hrs · 36,750 cycles

LT AUTOFEATHER-INOPERATIVE. FLASHES AFX ON TAKEOFF THEN GOES OUT. R & R PCB A123. OPS CHECKS NORMAL.

Part: SWITCH — OUT OF ADJUST (WARNING HORN) · airframe 29,417 hrs · 36,366 cycles

PILOT REPORTED GEAR WARNING HORN DOES NOT SOUND UNTIL 80 PERCENT N1. ADJUSTED LT AND RT GEAR WARNING HORN SWITCHES. OPS CHECK GOOD.

Part: CABLE — DAMAGED (PAX DOOR) · airframe 29,417 hrs · 36,366 cycles

PILOT REPORTED AIRSTAIR DOOR LOWER RT CABLE GETS CAUGHT WHEN CLOSING DOOR FROM INSIDE AND HAS A DAMAGED COVER. REPLACED LWR FWD AIRSTAIR DOOR CABLE. OPS CHECK GOOD.

Part: NUT PLATE — MISSING (DOOR FRAME) · airframe 28,797 hrs · 35,268 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED AFT LOWER COUNTER BALANCE UPPER ATTACH POINT HAS A MISSING NUT PLATE. GAINED ACCESS THROUGH DOOR FRAME SKIN REPLACED BROKEN NUT PLATE AND INSTALLED DOUBLER REPAIR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,797 hrs · 35,268 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED CRACK APPROXIMATELY 1.75 INCHES AT RADIUS IN HEAVY ANGLE AT LEFT FS 288.0. STOP DRILLED END OF CRACK AND INSTALLED REPAIR ANGLE, CLIP AND FASTNERS .

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,797 hrs · 35,268 cycles

DURING SCHEDULED ROUTINE INSPECTION DISCOVERED CRACK APPROXIMATELY 1.75 INCHES AT RADIUS IN HEAVY ANGLE AT FS 288 AND CRACK APPROXIMATELY 1.5 INCHES AT RADIUS IN HEAVY ANGLE AT RIGHT FS 303.

Part: SAFETY SWITCH — INTERMITTENT (MLG) · airframe 28,661 hrs · 35,011 cycles

PILOT REPORTED LANDING GEAR WARNING HORN ACTIVATED AND GEAR HANDLE LIT UP AT 2,000 LBS OF TORQUE UNABLE TO SILENCE HORN. REPLACED RT SAFETY SWITCH OPS, CHECK GOOD. TEST FLIGHT SATISFACTORY.

Part: SAFETY SWITCH — OUT OF ADJUST (MLG) · airframe 28,621 hrs · 34,938 cycles

DURING FLIGHT, WITH FLAPS UP POWER AT 88 PERCENT N1 GEAR WARNING HORN SOMETIMES UNABLE TO CANCEL. WITH FLAPS 17 DEGREES, WERE ABLE TO CANCEL HORN. FLAPS 35 DEGREES TESTED FINE UNABLE TO CANCEL. GEAR WARNING HORN GOES OFF AT 88 PERCENT N1 ON THE LT AND RT THERE WAS AN INTERMITTENT CHIRP OF THE HORN AT 96.4 N1 AND 94.8 N1. REPLACED PUSH TO SILENCE SWITCH AND ADJUSTED RT MLG SAFETY SQUAT SWITCH, OPS CHECK NORMAL. TEST FLIGHT SATISFACTORY.

Part: CIRCUIT BOARD — DAMAGED (MLG) · airframe 28,621 hrs · 34,938 cycles

DURING FLIGHT, GEAR WARNING LIGHT ILLUMINATED WITH AURAL WARNING AT 96.3 N1 AND 94.8 N1. UNABLE TO SILENCE GEAR WARNING HORN. REPLACED PCB A119, OPS CHECK GOOD.

Part: BLOWER — SMOKE (CABIN AIRE) · airframe 28,232 hrs · 34,263 cycles

DURING FLIGHT BURNING ODOR IN COCKPIT WITH WHITE SMOKE. ODOR AND SMOKE STOPPED WHEN BLOWERS AND LT BLEED BROUGHT OFF LINE. REPLACED FWD VENT BLOWER OPS CHECK GOOD.

Part: SPAR — CORRODED (WING) · airframe 27,976 hrs · 33,868 cycles

REPORT: DURING SCHEDULED X-RAY INSPECTION DISCOVERED CORROSION INDICATIONS ON FORWARD LOWER SPAR ANGLE AT WS 125.5. BLENDED OUT CORROSION AND INSTALLED REINFORCEMENT STRAP.

Part: CONNECTOR — LOOSE (MLG) · airframe 27,755 hrs · 33,540 cycles

FLT 9291, DURING TAKEOFF LANDING GEAR UNSAFE LIGHTS FLICKERED. SECURED LOOSE CONNECTOR ON PCB E193. LANDING GEAR OPERATIONAL CHECK GOOD. SECURED LOOSE CONNECTOR ON PCB E173. LANDING GEAR OPERATIONAL CHECK GOOD.

Part: WARNING SWITCH — INOPERATIVE (LANDING GEAR) · airframe 27,554 hrs · 33,242 cycles

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

Part: SCREW — OUT OF ADJUST (EMERGENCY DOOR) · airframe 27,426 hrs · 33,035 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED EMERGENCY DOOR AT SEAT 6A WILL NOT PULL OUT OF SEAT FREELY. ADJUSTED EMERGENCY EXIT INTERIOR LINING CONTOUR SCREW. OPS CHECK NORMAL.

Part: DOOR — STUCK (EMERGENCY EXIT) · airframe 27,012 hrs · 32,414 cycles

DURING SCHEDULED ROUTINE INSP, DISCOVERED EMERGENCY EXIT AT SEAT 6F WILL NOT PULL FREE FROM FRAME. ADJUSTED SIDE WALL TRIM AND RESET EMERGENCY DOOR.

Part: LENS — LOOSE (MLG HANDLE) · airframe 26,892 hrs · 32,241 cycles

DURING FLIGHT TOP RED LIGHT ON LANDING GEAR HANDLE INOPERATIVE. RESECURED LIGHT BULB RETAINING LENS ON GEAR HANDLE. OPS CHECK GOOD.

Part: LENS — LOOSE (GEAR HANDLE) · airframe 29,892 hrs · 32,241 cycles

DURING FLIGHT TOP RED LIGHT ON LANDING GEAR HANDLE INOPERATIVE. RESECURED LIGHT BULB RETAINING LENS ON GEAR HANDLE. OPS CHECK GOOD.

Part: DOWNLOCK SWITCH — OUT OF ADJUST (MLG) · airframe 26,776 hrs · 32,076 cycles

FLIGHT 9294 CLE/FKL AFTER TAKEOFF LANDING GEAR BROUGHT TO THE UP POSITION, RED INTRANSIT LIGHTS REMAINED ILLUMINATED AND ALL GREEN LIGHTS WERE EXTINGUISHED. CYCLED THE LANDING GEAR THE CONDITION REMAINED THE SAME. RETURNED TO CLE LANDED WITHOUT INCIDENT. ADJUSTED ALL THREE GEAR DOWNLOCK SWITCHES AND CLEANED ALL THREE UPLOCK SWITCHES. OPERATIONAL CHECK GOOD.

Part: RECEPTACLE — DIRTY (MLG INDICATOR) · airframe 26,737 hrs · 32,024 cycles

FLIGHT: 9294 FKL/DUJ DURING APPROACH GREEN "H" LANDING GEAR INDICATOR LIGHTS DO NOT ALWAYS STAY ILLUMINATED. CLEANED LIGHT RECEPTACLE TO RESTORE CONDUCTIVITY. OPS CHECK GOOD.

Part: UPLOCK SWITCH — DIRTY (RIGHT) · airframe 26,703 hrs · 31,979 cycles

FLIGHT NR 9291 DUJ/DUJ AFTER TAKEOFF LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED WITH THE HANDLE IN THE UP POSITION. CLEANED RT UPLOCK SWITCH. OPS CHECK NORMAL.

Part: ACTUATOR — CRACKED (NLG) · airframe 26,615 hrs · 31,845 cycles

FLIGHT 9294 FKL/DUJ - DURING APPROACH HEARD A BANG NOISE DURING THE LANDING GEAR EXTENSION. DID NOT NOTICE ANYTHING UNUSUAL OR ABNORMAL AS A RESULT OF THE NOISE. OBTAINED POSITVIE INDICATION THAT THE LANDING GEAR WAS DOWN AND LOCKED. CONTINUED TO DUJ LANDED WITHOUT INCIDENT. DURING POST FLIGHT NOTICED NOSE GEAR HYDRAULIC FLUID LEAKING ON THE GROUND. REPLACED NOSE LANDING GEAR ACTUATOR. LANDING GEAR OPERATIONAL CHECK NORMAL.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,333 hrs · 31,435 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED 1.875 INCH CRACK IN FUSELAGE BELLY SKIN SPAR AREA AT RBL 30.62. STOP DRILLED CRACK AND INSTALLED REINFORCEMENT DOUBLER REPAIR.

Part: CONNECTOR — DIRTY (ANNUNCIATOR) · airframe 25,817 hrs · 30,826 cycles

DURING FLIGHT AMBER DISCHARGE, ANNUNCIATOR ILLUMINATED. CLEANED CONNECTORS AT RT FIRE BOTTLE.

Part: CONNECTOR — LOOSE (SQUAT SWITCH) · airframe 25,699 hrs · 30,688 cycles

FLIGHT 9271, AFTER TAKEOFF, LANDING GEAR CONTROL HANDLE WOULD NOT RETRACT. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. RESECURED CONNECTOR ON RT MLG SQUAT SWITCH.

Part: LANDING GEAR — MALFUNCTIONED · airframe 25,636 hrs · 30,616 cycles

FLIGHT:9197, AFTER TAKEOFF LANDING GEAR TOOK MANY ATTEMPTS TO RETRACT EVEN WITH THE (J) HOOK PUSHED DOWN. CONTINUED, LANDED WITHOUT INCIDENT. PERFORMED LANDING GEAR OPERATIONAL CHECK NO DEFECTS NOTED.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 24,915 hrs · 29,832 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OB HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 24,915 hrs · 29,832 cycles

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (LT ELEVATOR) · airframe 24,915 hrs · 29,832 cycles

REPORT: DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE BRACKET.

Part: HINGE BRACKET — CORRODED (RT ELEVATOR) · airframe 24,915 hrs · 29,832 cycles

DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED RT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OB HINGE BRACKET.

Part: CONNECTOR — LOOSE (FIRE BOTTLE) · airframe 24,895 hrs · 29,813 cycles

DURING FLIGHT RT FIRE BOTTLE DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED LOOSE CONNECTION AT RT FIRE BOTTLE.

Part: CONNECTOR — DIRTY (FIRE BOTTLE) · airframe 24,889 hrs · 29,808 cycles

DURING FLIGHT RT FIRE BOTTLE DISCHARGE ANNUNCIATOR ILLUMINATED. CLEANED CONNECTIONS AT RT FIRE BOTTLE SQUIB.

Part: DOOR — OUT OF ADJUST (EMERGENCY EXIT)

DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT AFT EMERGENCY HATCH INNER HANDLE HARD TO OPEN. ADJUSTED RT AFT EMERGENCY HATCH HANDLE.

Part: WIRE — LOOSE (FIRE BOTTLE) · airframe 23,480 hrs · 28,206 cycles

FLIGHT 9253- DURING FLIGHT RT DISCHARGE LIGHT ILLUMINATED ON AND OFF. SECURED WIRES ON THE RT FIRE BOTTLE.

Part: WIRE — LOOSE (ZONE 400) · airframe 23,216 hrs · 27,877 cycles

FLIGHT:9253 TBI/FLL DURING FLIGHT RT ENGINE FIRE EXTINGUISHER DISCHARGE ANNUNCIATOR ILLUMINATED. SECURED WIRE ON RT ENGINE FIRE BOTTLE.

Part: TUBE — CHAFED (ENGINE TRUSS) · airframe 23,199 hrs · 27,855 cycles

DURING INSP DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 HAD CHAFING DAMAGE AT 2.50 INCHES AFT OF FIRE SEAL FLANGE ON INBD SIDE. PERFORMED ENGINE TRUSS REPAIR TO CHAFED AREA, IAW FAA APPROVED DATA.

Part: TRUSS — CHAFED (ZONE 400)

AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED ENGINE TRUSS TUBE PN 129-910032-101 CHAFING DAMAGE AT 2.5 INCHES AFT OF FIRE SEAL FLANGE ON IB SIDE. PERFORMED TRUSS REPAIR TO CHAFFED AREA IAW APPROVED DATA CONTAINED IN THE DWG NR 070226,DERT 510305-CE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,153 hrs · 27,804 cycles

AT SCHEDULED INSPECTION, DISCOVERED ONE CRACK AT AFT COMM ANTENNA (FS400) CRACK 3.0 INCHES RUNNING LONGITUDINALLY FORWARD FROM FS 400. STOP DRILLED CRACK AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW STRUCTURALREPAIR MANUAL 51-70-06.

Part: SKIN — CRACKED (FUSELAGE) · airframe 23,154 hrs · 27,804 cycles

DURING SCHEDULED ROUTINE MX DISCOVERED AFT LOWER FUSELAGE SKIN AT AFT COMM ANTENNA FS 400 HAD CRACK. STOP DRILLED CRACK FABRICATED AND INSTALLED AN EXTERNAL REINFORCEMENT DOUBLER REPAIR.

Part: WIRE — LOOSE (RT FIRE BOTTLE) · airframe 23,046 hrs · 27,681 cycles

FLIGHT: 9176, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE CONNECTION AT THE RT FIRE BOTTLE.

Part: WIRE — LOOSE (RT FIRE BOTTLE) · airframe 23,046 hrs · 27,674 cycles

FLIGHT: 9175, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE AT RT ENGINE FIRE BOTTLE.

Part: WIRE — LOOSE (RT FIRE BOTTLE) · airframe 23,032 hrs · 27,665 cycles

FLIGHT: 9147, DURING FLIGHT RT ENGINE FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCIDENT. RESECURED LOOSE WIRE AT RT FIRE BOTTLE.

Part: CIRCUIT BREAKER — FAILED (MLG) · airframe 22,952 hrs · 27,569 cycles

FLIGHT: 9167, AFTER TAKEOFF LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED. CONTINUED, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR INDICATION CIRCUIT BREAKER,OPERATIONAL CHECK NORMAL.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 22,877 hrs · 27,485 cycles

FLIGHT: 9232, DURING FLIGHT, F/O FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED AND FLICKERED. CLEANED AND INSPECTED THE F/O FIRE EXTINGUISHER ANNUNCIATOR , COULD NOT DUPLICATE.

Part: CONNECTOR — CONTAMINATED (DETECTION SYS) · airframe 22,867 hrs · 27,472 cycles

FLIGHT: 9171, DURING FLIGHT FIRST OFFICERS FIRE DISCHARGE LIGHT ILLUMINATED. CONTINUED TO MIA LANDED WITHOUT INCIDENT. FOUND WET CONNECTOR AT RT ENGINE FIRE BOTTLE, DRIED AREA OPERATIONAL CHECK GOOD.

Part: SENSOR — FAULTY (AIR CYCLE MACHNE)

FLIGHT:9137 SAQ/FLL AFTER TAKEOFF ENVIRONMENTAL FAIL ANNUNCIATOR ILLUMINATED SMELL OF SMOKE OBSERVED WHEN THE BLEED WAS OPEN. REPLACED AIR CYCLE MACHINE OVERTEMP SENSOR.

Part: ODOR — DETECTED (CABIN)

TPA/TLH DURING FLIGHT AT CRUISE CREW NOTICED BURNING SMELL. REMOVED STANDING WATER ALONG CENTER AISLE UNDER FLOORBOARDS AND INSPECTED ELECTRICAL SYSTEMS, NO DEFECTS NOTED COULD NOT DUPLICATE.

Part: SKIN — DENTED (FUSELAGE)

EYW/FLL DENT FOUND EIGHT INCHES BELOW CARGO DOOR. FABRICATED AND INSTALLED EXTERNAL DOUBLER REPAIR IN ACCORDANCE WITH 1900 STRUCTURAL REPAIR MANUAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,052 hrs · 25,312 cycles

DURING INSP DISCOVERED LT FUSELAGE HAD (3) FLAT DENTS 8 INCHES BELOW CARGO DOOR BETWEEN FS 468.250 THROUGH 482.250. FILLED DENTS WITH AERODYNAMIC FILLER , FABRICATED AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER REPAIR OVER ALL (3) DENTS.

Part: HINGE — CORRODED (VERT STAB)

AT SCHEDULED INSPECTION, DETERMINED VERTICAL FIN CENTER RUDDER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL FIN CENTER RUDDER HINGE BRACKET. (K)

Part: HINGE — CORRODED (VERTICAL STAB)

AT SCHEDULED INSPECTION, DETERMINED VERTICAL FIN UPPER RUDDER HINGE BRACKET TO BE EXFOLIATED. REPLACED VERTICAL FIN UPPER RUDDER HINGE BRACKET. (K)

Part: ENGINE — FAILED (RIGHT)

DURING AM ENGINE RUNUPS, RT ENGINE WENT INTO FEATHER AND WOULD NOT COME OUT. ALL OTHER PARAMETERS NORMAL. AFTER FURTHER INSPECTION, DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. NOTE: SUSPECT NR 2 PT BLADE FAILURE.

Part: BLADE — FAILED (RT ENGINE)

DURING AM ENGINE RUNUPS, RT ENGINE WENT INTO FEATHER AND WOULD NOT COME OUT, ALL OTHER PARAMETERS NORMAL. AFTER FURTHER INSPECTION, DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (CLOSED 5/4/05) (K)

Part: BRACKET — CORRODED (RT ELEVATOR)

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

Part: BRAKE — MALFUNCTIONED (MLG)

FLT 9227 - NAS-FLL - AFTER LANDING, BRAKES ARE SPONGY AND LOSE PRESSURE WHILE TURNING AND STOPPING. BLED BRAKES. LEAK CHECK OK. OPERATIONAL CHECK NORMAL. (M)

Part: SPAR — CRACKED (HORIZ STAB)

AT SCHEDULED EMPANNAGE ZONAL INSPECTION, FOUR CRACKS FOUND RADIATING FROM PASSAGE HOLE IN FORWARD WEB OF THE HORIZONTAL STABILIZER FORWARD SPAR. REMOVED SECTION OF CRACKED SKIN. FABRICATED AND INSTALLED SHIM AND DOUBLER IAW FAA APPROVED DATA CONTAINED IN DER 8110-3, REPORT NR 030715. (M)

Part: RIB — CRACKED (VERTICAL STAB)

AT SCHEDULED EMPANNAGE ZONAL INSPECTION, VERTICAL STABILIZER TOP FORWARD RIB SHOWING CRACK ON RIGHT SIDE. STOPPED DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER REPAIR IAW 1900D STRUCTURAL REPAIR MANUAL, CHAPTER 51-70-05. (M)

Part: ENGINE — FAILED (LEFT)

FLT 9214 - MIA - DURING TAKEOFF JUST AFTER BRAKE RELEASE, AN EXPLOSION WAS HEARD IN THE LEFT ENGINE. ABORTED TAKEOFF. REMOVED LEFT ENGINE. DETERMINED POEWR SECTION HAS MAJOR INTERNAL DAMAGE. REPLCED LEFT ENGINE. ROUTED FAILED ENGINE FOR FURTHER ANALYSIS AND REPAIR. (M)

Part: BLADE — FAILED (LT ENGINE)

DURING TAKEOFF JUST AFTER BRAKE RELEASE, AN EXPLOSION WAS HEARD IN THE LT ENGINE. ABORTED TAKEOFF. REMOVED LEFT ENGINE. DETERMINED POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LEFT ENGINE. ROUTED FAILED ENGINE FOR FURTHER ANALYSIS AND REPAIR. VENDOR DETERMINED TO BE 2ND STAGE POWER TURBINE BLADE FAILURE WITH SUBSTANTIAL DAMAGE TO HOT SECTION.

Part: ACTUATOR — BYPASSING (LT MLG)

DURING APPROACH WHEN LANDING GEAR IS SELECTED DOWN THE AIRCRAFT JOLTS AS THE LEFT GEAR LIGHTS ILLUMINATE. REMOVED AND REPLACED LEFT MLG ACTUATOR. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL.

Part: TRUSS — CHAFED (ENGINE)

AT SCHEDULED ROUTINE MAINTENANCE, CHAFING DAMAGE AT 3 INCHES AFT OF FIRE SEAL FLANGE ON INBOARD SIDE. PERFORMED TRUSS REPAIR TO CHAFED AREA IAW FAA APPROVED DATA CONTAINED IN RAYTHEON FIELD REPAIR FR-CO-00706 REV. (M)

Part: PULLEY BRACKET — LOOSE (AILERON)

AT SCHEDULED THIRD 200 HOUR INSPECTION, DISCOVERED THE AILERON LEFT DOWN CONTROL CABLE TO BE FRAYED. DETERMINED CABLE FRAYING CAUSED BY INCOMPLETE INSTALLATION OF PULLEY MOUNTING BRACKET. SECURED BRACKET , AND REPLACED PULLEY AND CABLE. (M)

Part: LIGHT — INOPERATIVE (COCKPIT)

FLT 9505 - EYW/TPA - LANDING GEAR DOWNLOCK INDICATOR HAS ONE LAMP INOPERATIVE. REPLACED BURNED LAMP INOPERATIVE. REPLACED BURNED LAMP IN DOWNLOCK INDICATOR. OPERATIONAL CHCK SATISFACTORY. (M)

Part: SWITCH — FAILED (LANDING GEAR)

CLE - FLT 3178 - CREW REPORTED THEY HAD A RED GEAR UNSAFE LIGHT THAT WOULD NOT EXTINGUISH UPON GEAR RETRACTION. AIRCRAFT DIVERTED TO CVG WITHOUT FURTHER INCIDENT, THE AIRCRAFT WAS THEN MAINTENANCE FERRIED TO CLE. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL SWITCH IAW B1900 MM 32-60-00, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. AIRCRAFT TT: 7,282.8 HOURS. TOTAL CYCLES: 9,056. (X)