N11121

Part: HOSE — LEAKING (THERMOSTAT) · airframe 41,713 hrs · 25,502 cycles

BLEED 1 OVERHEAT EICAS MSG IN ICING CONDITION WITH CARROT IN RED. EXITED ICING CONDITIONS . ALL INDICATIONS RETURNED TO NORMAL. INSPECTED ENGINE 1 BLEED IN PYLONS AND THERMOSTAT LINES. FOUND AFT THERMOSTAT HOSE LEAKING FROM PYLON. R&R HOSE AND COMPLIED WITH OPS CHECK OF AIR BLEED SYSTEM. OPS CHECK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

LT FLOOR SILL HAS CORROSION BETWEEN FR48-FR52. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LT FLOOR SILL AT FR48-FR52.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

LT FLOOR SILL HAS CORROSION BETWEEN FR42-FR47. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LT FLOOR SILL AT FR42-FR47.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

RT FLOOR SILL HAS CORROSION BETWEEN FR36-FR41. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED RT FLOOR SILL AT FR36-FR41.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

RT FLOOR SILL HAS CORROSION BETWEEN FR42-FR47. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED RT FLOOR SILL AT FR42-FR47.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

LT FLOOR SILL HAS CORROSION BETWEEN FR36-FR41. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LT FLOOR SILL AT FR36-FR41.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

PAX DOOR ENTRANCE RAMP O/B UPPER SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED RAMP O/B UPPER SUPPORT ANGLE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

CARGO BAY RAMP FWD SUPPORT HAS SIGNS OF CORROSION. REMOVED CORROSION, FOUND TO BE CRACKED. REMOVED AND REPLACED CARGO RAMP FWD SUPPORT.

Part: FRAME — CRACKED (FRM 25) · airframe 41,713 hrs · 25,501 cycles

FRAME 25 IS CRACKED BETWEEN STR 15R AND 16R... REPAIRED FR25 BETWEEN STR 15R AND 16R PER ETD 2018-145-117736

Part: BRACKET — CHAFED (FRAMES 68-69) · airframe 41,713 hrs · 25,501 cycles

L/H CTR FUSELAGE BLEED SYS SUPPORT BRACKET BETWEEN FR 38 AND FR 39 HAS CHAFF DAMAGE... REMOVED AND REPLACED SUPPORT BRACKET

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

LT FLOOR SILL HAS CORROSION BETWEEN FR19 AND FR23. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED AND REPLACED LT FLOOR SILL AT FR19-FR23.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

RT FLOOR SILL HAS CORROSION BETWEEN FR22 AND FR23. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED RT FLOOR SILL AT FR22 AND FR23.

Part: ATTACH BRACKET — CORRODED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

PAX DOOR ENTRANCE FLOOR BOARD ATTACH BRACKETS HAVE CORROSION. REMOVED CORROSION, FOUND AFT ATTACH BRACKET TO BE OUT OF LIMITS. REMOVED AND REPLACED BRACKET.

Part: BRACKET — CHAFED (FRAMES 38-39) · airframe 41,713 hrs · 25,501 cycles

L/H CTR FUSELAGE BLEED SYS SUPPORT BRACKET BETWEEN FR 38 AND FR 39 HAS CHAFF DAMAGE... REMOVED AND REPLACED SUPPORT BRACKET..

Part: BRACKET — CHAFED (FRAMES 38-39) · airframe 41,713 hrs · 25,501 cycles

L/H CTR FUSELAGE BLEED SYS SUPPORT BRACKET BETWEEN FR 38 AND FR 39 HAS CHAFF DAMAGE... REMOVED AND REPLACED SUPPORT BRACKET..

Part: BRACKET — CRACKED (PACK VALVE) · airframe 41,713 hrs · 25,501 cycles

EXTERNAL FUSELAGE PACK VALVE MOUNTING BRACKETS ARE DAMAGED... REMOVED AND REPLACED PACK VALVE MOUNTING BRACKET...

Part: ANGLE — CRACKED (ZONE 100) · airframe 41,713 hrs · 25,501 cycles

FUSELAGE L/H SIDE FWD OF WING L/E ANTI-ICE SHUTOFF BRACKET IS CRACKED IN HALF... REMOVED AND REPLACED BRACKET...

Part: STRIKER — CORRODED (FRAME 65) · airframe 41,713 hrs · 25,501 cycles

CARGO DOOR CUTOUT FWD LOWER CORNER AT FRAME 65 STRIKER PLATE HAVE CORROSION AROUND AND UNDER STRIKER PLATE... REPAIRED IAW E0-EMB145-53-059-R1 AND ETD 2018-145-119292 REV D

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 41,713 hrs · 25,501 cycles

BAGGEGE DOOR MECHANISM FWD TORTION BAR SUPPORT MOUNTING STRUCTURE BRACKET IS CRACKED IN 2 PLACES... REMOVED AND REPLACED MOUNTING BRACKET...

Part: SUPPORT — CRACKED (FRAME 74) · airframe 41,713 hrs · 25,501 cycles

BLEED AIR PIPE SUPPORT CLAMP BRACKET CRACKED NEAR R/H FRAME 74...REMOVED AND REPLACED BLEED AIR PIPE SUPPORT CLAMP BRACKET

Part: FRAME — DAMAGED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

RT FUSELAGE FRAME 64 HAS HOLE IN FLANGE BETWEEN STR 6R-7R. DRILLED AND INSTALLED FASTENER IN RT FUSELAGE FR64 PER ETD2018145-115640.

Part: DOOR — CRACKED (E/E BAY) · airframe 41,713 hrs · 25,501 cycles

COCKPIT UNDERFLOOR HATCH 123BL IS CRACKED BELOW HINGE BRACKET... INSTALLED DOUBLER AND FILLER TO COCKPIT UNDERFLOOR HATCH IAW SRM 52-42-02...

Part: SUPPORT — BROKEN (FUSELAGE) · airframe 41,713 hrs · 25,501 cycles

CARGO DOOR LIFTING AND LOWERING SYSTEM SUPPORT IS BROKEN. REMOVED AND REPLACED SUPPORT.

Part: SUPPORT FRAME — DAMAGED (FUSELAGE) · airframe 41,712 hrs · 25,501 cycles

CARGO DOOR LIFTING LOWERING SYSTEM SUPPORT FRAMES ARE DAMAGED. REMOVED AND REPLACED SUPPORT FRAMES.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 39,478 hrs · 23,609 cycles

NR 1 ENGINE FWD MOUNT, LOWER, FWD FITTING HAS A CRACK INDICATION. REMOVED AND REPLACED THE 1 ENGINE FWD MOUNT YOKE FITTING.

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB) · airframe 38,074 hrs · 22,414 cycles

SWITCH TRIM BACKUP INOPERATIVE IN FLT. R & R HSCU OPS CHECKED GOOD AT THIS TIME.

Part: BLEED VALVE — INOPERATIVE (NR 2) · airframe 37,547 hrs · 21,973 cycles

BLEED 2 OVERTEMP. R & R BLEED VALVE NR 2. OPS CHECK GOOD.

Part: DETECTOR — INOPERATIVE (ICE) · airframe 37,524 hrs · 21,950 cycles

ICE DETECTION CONDITION EICAS AT FL320 T- 30C WITH NO ICING PRESENT. REMOVED AND REPLACED THE NR 1 AND 2 ICE DETECTORS. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 35,750 hrs · 20,420 cycles

CEILING EMERGENCY EXIT LIGHT AT ROW 18, FWD SIDE, LIGHT NR 18A IS INOPERATIVE. DISCONNECTED AND CLEANED CONNECTOR FOR LIGHT NR 18A. RECONNECTED AND PERFORMED OPS CHECK. OPS CHECK GOOD.

Part: SEAL — LEAKING · airframe 35,430 hrs · 20,142 cycles

LOUD NOISE, MID CABIN IN FLT WITH NO LOSS OF PRESSURIZATION. MAINTENANCE FOUND ADF LOOP ANTENNA LEAKING, SEAL WAS BLOWN. MAINTENANCE REPLACED SEAL, LEAK AND OPS CHECK GOOD.

Part: RECEPTACLE — DIRTY (EMERGENCY LIGHT) · airframe 35,194 hrs · 19,950 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. CLEANED BULB RECEPTACLE. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,397 hrs · 19,353 cycles

THE CREW REPORTED THE GALLEY EMERGENCY LIGHTS WERE INOPERATIVE, AND THAT THEY CAME ON IN FLIGHT AND COULD NOT BE TURNED OFF OR RESET. THE ACFT LANDED IN ELP WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND APPROVED A FERRY FLIGHT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R THE NR 2 EMERGENCY LIGHT BATTERY CHARGER AND NR 2 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,397 hrs · 19,353 cycles

THE CREW REPORTED THE GALLEY EMERGENCY LIGHTS WERE INOPERATIVE, AND THAT THEY CAME ON IN FLIGHT AND COULD NOT BE TURNED OFF OR RESET. THE ACFT LANDED IN ELP WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND APPROVED A FERRY FLIGHT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R THE 2 EMERGENCY LIGHT BATTERY CHARGER AND NR 2 EMERGENCY LIGHT BATTERY PACK. OPS CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (HORIZONTAL STAB) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK HORIZONTAL STABILIZER RT HINGE FITTING INBD AND OTBD PLAIN BUSHINGS MIGRATED. MAINTENANCE PERFORMED THE REPAIR OF THE HORIZONTAL STABILIZER RT HINGE FITTING INBD AND OTBD HOUSING IAW SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK RT AILERON 2ND INBD HINGE, INBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF RT AILERON 2ND INBD HINGE, INBD HAT BUSHING IAW EC5740-01152, REV F. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — DAMAGED (HORIZONTAL STAB) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, HORIZONTAL STABILIZER RT HINGE FITTING OTBD HOUSING NR 4 DAMAGED. MAINTENANCE PERFORMED THE REPAIR OF THE HORIZONTAL STABILIZER RT HINGE FITTING INBD AND OTBD HOUSING IAW SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (AILERON HINGE) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK RT AILERON INBD HINGE INBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED INSTALL OF RT AILERON INBD HINGE IAW SRM 51-40-02 AND IS DETERMINED TO BE MAJOR IAW SOP 5702. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (LT AILERON) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK PCA TO AILERON OTBD ATTACHMENT, OTBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF LT AILERON PCA BRACKET IAW EC5760-01044, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, RT PCA TO AILERON OTBD ATTACHMENT, OTBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF RT SPEED BRAKE ACTUATOR ATTACHMENT OTBD HAT BUSHING IAW EC5760-01044, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, RT AILERON 2ND FROM OTBD HINGE, OTBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF THE RT AILERON 2ND FROM OTBD HINGE, OTBD HAT BUSHING IAW EC5740-01152, REV F. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, LT EMERGENCY LIGHT ON 191 PANEL HAS BROKEN CONNECTOR PLUG WIRES. MAINTENANCE REPAIRED CONNECTOR PLUG WIRES ON LT EMERGENCY LIGHT ON 191 PANEL IAW AMM 33-50-00, OPS TEST PASSED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK INTERNAL SKIN CORRODED, LOCAL LEVEL 2, BETWEEN FRAMES 13-14 STRINGER 21R-20R. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN FRAMES 3-14 STRINGERS 21R-20R IAW EC5320-02000. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ACTUATOR) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, RT SPEED BRAKE ACTUATOR ATTACHMENT INDB HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR TO RT SPEED BRAKE ACTUATOR ATTACHMENT INBD HAT BUSHING IAW AMM 27-63-01, OPS CHECKED GOOD. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (GROUND SPOILER) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, RT GROUND SPOILER ACTUATOR ATTACHMENT, INBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF RT GROUND SPOILER ACTUATOR ATTACH FITTING INBD HAT BUSHING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 78) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, CRACKS AROUND 2 MARKED RIVETS ON FUSELAGE SKIN AT FRAME 78, STRINGER 5L-7L. MAINTENANCE PERFORMED REPAIR TO FUSELAGE SKIN AT FRAME 78, STRINGER 5L-7L SKIN IAW EC5330-02970. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LEG ASSY — DAMAGED (LEFT MLG) · airframe 3,428 hrs · 19,275 cycles

DURING C-CHECK, LT MLG LEG HAS UPPER WASHERS MISSING ON UPPER BEARING CAP FWD AND AFT SIDE BOLTS. MAINTENANCE PERFORMED REPAIR TO LT MLG FWD TRUNNION IAW EC5750-01665. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 79) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, CRACKS AROUND 2 MARKED RIVETS FRAME 79 STRINGER 5L-7L. MAINTENANCE PERFORMED REPAIR TO SKIN FRAME 79 STRINGER 5L-7L IAW EC5330-02970. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, LT GROUND SPOILER ACTUATOR ATTACHMENT INBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF LT GROUND SPOILER ACTUATOR ATTACHMENT INBD HAT BUSHING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, RT EMERGENCY LIGHT ON 191 PANEL HAS BROKEN CONNECTOR PLUG WIRES. MAINTENANCE REPAIRED CONNECTOR PLUG WIRES ON RT EMERGENCY LIGHT ON 191 PANEL IAW AMM 33-50-00. OPS TEST PASSED. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (HORIZONTAL STAB) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK HORIZONTAL STABILIZER LT HINGE FITTING OTBD PLAIN BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF HORIZONTAL STAB LH HINGE FITTING OTBD PLAIN BUSHING HOUSING IAW SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (GROUND SPOILER) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, LT GROUND SPOILER CENTER ATTACHMENT INBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF LT GROUND SPOILER CENTER ATTACHMENT INBD HAT BUSHING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — GOUGED (FRAMES 19-20) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK EXTERNAL SKIN DENTED/GOUGED AT DENT CLUSTER BETWEEN FRAMES 19-20 STRINGER 11L. MAINTENANCE PERFORMED REPAIR TO SKIN FRAME 19-20, STRINGER 11L-12L IAW EC5330-02971. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (SERVICE DOOR) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK SERVICE DOOR AFT LOWER CORNER DENTED. MAINTENANCE PERFORMED REPAIR TO SERVICE DOOR AFT LOWER CORNER IAW EC5240-01089. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (AILERON HINGE) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK RT AILERON INBD HINGE OTBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF RT AILERON INBD HINGE IAW SRM 51-40-02 AND DETERMINED TO BE MAJOR IAW SOP 5702. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION, LOCAL LEVEL 2 AROUND 2 NUTPLATE HOLES, FRAME 59-61. MAINTENANCE PERFORMED REPAIR OF CENTER OMEGA BEAM AT 2 NUTPLATE HOLES FRAME 59 AND 61 IAW EC5310-01473, REV D. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 34,284 hrs · 19,275 cycles

DURING C-CHECK RT ENGINE FWD LOWER PYLON FWD YOKE FITTING CRACKED. MAINTENANCE R & R RT ENGINE FWD LOWER YOKE FITTING IAW EC5450-01133 AND SB-145-54-0013. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · airframe 34,284 hrs · 19,275 cycles

FWD FUSELAGE SKIN CORRODED BETWEEN FRAMES 12-13 STRINGERS 20R - 20L. R & R SKIN IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 78) · airframe 34,284 hrs · 19,275 cycles

CRACKS AROUND RIVETS FR 78, STR 5L-7L. REPAIRED SKIN IAW EC5330-02970. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FRAMES 10-14) · airframe 34,284 hrs · 19,275 cycles

STRINGER 21L HAS CORROSION BETWEEN FRAMES 10 - 14. R & R THE STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FRAMES 12-13) · airframe 34,284 hrs · 19,275 cycles

STRINGER 21R HAS CORROSION BETWEEN FRAMES 12 - 13. R & R THE STRINGER IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CLAMP — UNSECURE (BLEED SYS) · airframe 33,535 hrs · 18,792 cycles

CREW REPORTED A BLEED NR 2 LEAK INDICATION WITH STRONG ODOR. MX COULD NOT DUPLICATE STRONG ODOR BUT DID REPOSITIONED AND SECURED THE NR 2 BLEED VALVE CLAMP. OPS AND LEAK CHECKS RESULTS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 33,156 hrs · 18,547 cycles

THE CREW REPORTED LAVATORY SMOKE WARNING IN FLIGHT. MAINTENANCE INSPECTED AND CLEANED SMOKE DETECTOR SENSOR. OPS CHECKED GOOD.

Part: ACM — ODOR (NR 1) · airframe 31,106 hrs · 17,267 cycles

CREW REPORTED A DISTINCTIVE ELECTRICAL BURNING ODOR IN FLIGHT. CABIN EXPERIENCED SLIGHT HAZE. PASSENGER IN 11A STATED SMOKE SEEN COMING FROM ABOVE SEATS 8 AND 9CD. MAINTENANCE R & R NR 1 ACM WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — LOOSE (A/C PACK) · airframe 20,234 hrs · 16,316 cycles

CREW REPORTED DUAL UNANNOUNCIATED PACKS/PRESSURIZATION FAILURE DURING CLIMB OUT. RESULTED IN EMERGENCY DESCENT AND AIR RETURN. MX FOUND A BLOWN DUCT ON PACK 1 AND RESECURED DUCT TO HEAT EXCHANGER WITH PACK 1 OPS CHECK SUCCESSFUL. PACK 2 OPS CHECKED SUCCESSFUL. ACFT PRESSURIZATION CHECK GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CHAFED (NR 1 NACELLE) · airframe 28,783 hrs · 15,790 cycles

ACFT WAS FOUND WITH THE NR 1 ENGINE PYLON SKIN PANEL, CHAFED. MX REPAIRED THE PANEL IAW EC5330-02681. WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF ALL WORK.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 28,873 hrs · 15,790 cycles

LT OMEGA BEAN TOP CAP IS CORRODED BEYOND LIMITS. R & R TOP CAP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,873 hrs · 15,790 cycles

RIGHT FLOOR SUPPORT IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.

Part: ATTACH BRACKET — WORN (LT AILERON) · airframe 28,873 hrs · 15,790 cycles

LEFT AILERON PCA ATTACH BRACKET HAS A MIGRATED BUSHING. R & R PCA ATTACH BRACKET.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,873 hrs · 15,790 cycles

GALLEY AFT STEP-UP CORRODED BEYOND LIMITS. R & R LOWER PORTION OF GALLEY AFT STEP-UP.

Part: ACM — SMOKE (NR 1) · airframe 26,019 hrs · 14,019 cycles

THE CREW REPORTED SMOKE IN THE COCKPIT AFTER PACKS WERE SELECTED FOLLOWED BY PACK NR 1 OVERHEAT MESSAGE. THE ACFT RETURNED TO THE GATE. MX INSPECTED AND RELEASED ACFT IAW MEL PROCEDURES 21-51-00-3. MX REPLACED THE NR 1 PACK ACM. OPS CHECKS WERE GOOD.

Part: FUEL SYS — MALFUNCTIONED (APU) · airframe 25,397 hrs · 13,682 cycles

EWR FLT 4270 CREW REPORTED STRONG FUEL SMELL DURING T/O ROLL WHICH DISSIPATED AFTER THE T/O CHECK. EWR MX INSPECTED THE ENGINES AND APU FOR FUEL LEAKS AND FOUND FUEL RESIDUE ON APU COWLING FROM A FAILED APU START. MX RAN APU AND PACKS FOR 20 MINUTES WITH NO SMELL NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — SHORTED (COCKPIT) · airframe 24,195 hrs · 12,984 cycles

IAH - DURING MX INSPECTION THE NR 1 MFD WENT BLANK AFTER AN ELECTRICAL BURNING SMELL AND FLICKERING SCREEN. MAINTENANCE REMOVED AND REPLACED THE NR 1 MFD, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 29,193 hrs · 12,983 cycles

IAH - FLIGHT 2062, THE CREW REPORTED A STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT ON POWERUP, AND STATED THAT IT SEEMED STRONGER ON THE CAPTAINS SIDE. MAINTENANCE INSPECTED THE AIRCRAFT PERFORMED FIM TASKS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANTI-ICE VALVE — DEFECTIVE (NR 2 ENGINE) · airframe 24,151 hrs · 12,960 cycles

FLIGHT 2186 - EWR - FLIGHT CREW REPORTED, UNABLE TO MAINTAIN CLIMB PROFILE LEVELED OFF FL290 TO GAIN SPEED. CLIMB TO FL310 AT 1000 FT MIN FL310 TO 350 AT 600FT PER MIN ONLY ABLE TO MAINTAIN MACH .70 IN CRUISE IN THE CLOUDS, 74-.76 IN CLEAR AIR AT 370. EWR MX INFORMED THAT N1 TARGET NOT INCREASING DUE TO ENG 2 ANTI-ICE VALVE C/B OPENED. MX REMOVED AND REPLACED ENG 2 ANTI ICE VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTACTOR — BURNED · airframe 23,829 hrs · 12,784 cycles

FLIGHT 3081 - EWR - FLIGHT CREW REPORTED STRONG SMELL BURNING RUBBER IN FRONT OF ACFT AFTER LANDING. EWR MX REMOVED AND REPLACED CONTACTOR K0236 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (SUPPLEMENTAL CHANGED DIFF DATE TO 5/7, WAS 5/2)

Part: FLAPPER VALVE — DAMAGED (RT WING) · airframe 23,512 hrs · 12,616 cycles

CME - IAH DURING CLIMB THE RIGHT WING WAS FOUND TO BE VENTING FUEL. THE AIRCRAFT RETURNED TO CME AND LANDED WITHOUT INCIDENT. UPON INSPECTION MAINTENANCE FOUND THE RIGHT WING FLAPPER (CHECK) VALVE TO BE DAMAGED ALLOWING THE FUEL TO ESCAPE THROUGH THE VENT. THE VALVE WAS REPLACED AND THE DISCREPANCY CLEARED.

Part: THERMOSTAT — INOPERATIVE (BLEED AIR SYS) · airframe 20,183 hrs · 10,750 cycles

CVG - FLIGHT 2217, THE CREW REPORTED A BLEED 1 AND 2 OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO CVG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO FAN AIR CONTROL THERMOSTAT, AND THE AFT SERVO HOSE ON THE NR 1 SIDE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOSE — LEAKING (BLEED SYSTEM) · airframe 20,183 hrs · 10,750 cycles

CVG - FLIGHT 2217, THE CREW REPORTED A BLEED 1 AND 2 OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT RETURNED TO CVG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO FAN AIR CONTROL THERMOSTAT, AND THE AFT SERVO HOSE ON THE NR 1 SIDE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — INOPERATIVE (BLEED AIR SYS) · airframe 20,183 hrs · 10,749 cycles

FLIGHT 2217 - CVG - FLIGHT CREW REPORTED BLEED 1/2 OVERTEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED SENSE LINE AND NR 2 FAN AIR THERMOSTAT. SENSE LINE SDR C2XA10RI027 AND FAN AIR THERMOSTAT SDR C2XA10RI028.

Part: HOSE — LEAKING (BLEED SYSTEM) · airframe 20,183 hrs · 10,749 cycles

FLIGHT 2217 - CVG - FLIGHT CREW REPORTED BLEED 1/2 OVERTEMP ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED SENSE LINE AND NR 2 FAN AIR THERMOSTAT.

Part: RELAY — INOPERATIVE · airframe 19,885 hrs · 10,582 cycles

IAH - FLIGHT 2412, THE CREW REPORTED THAT THE NR 2 ADC FAILED AT 270FT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAYS K0039 AND K0040, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,747 hrs · 10,510 cycles

DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,442 hrs · 8,160 cycles

RIC - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT SIDE EMERGENCY EXIT LOWER SIGN NOT ILLUMINATING. MX REMOVED AND REPLACED NR 3 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 15,413 hrs · 8,146 cycles

EWR FLIGHT NR 2753, THE CREW REPORTED AT FL370 THE PRESSURIZATION STARTED CLIMBING TO 14,000 FT. EMERGENCY DESCENT STARTED AND THE PRESSURIZATION STARTED DESCENDING. THE FLIGHT DIVERTED TO CLE. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL PRESSURIZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: ACTUATOR — INOPERATIVE (RAT DOOR) · airframe 15,396 hrs · 8,134 cycles

IAH - FLIGHT 2172, DURING CLIMB THE CREW REPORTED A RAM AIR VALVE FAILURE MESSAGE WITH THE INABILITY TO HOLD CABIN ALTITUDE BELOW 10K' ABOVE 21K' AIRCRAFT ALTITUDE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT HAND RAM AIR DOOR LINEAR ACTUATOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (RIGHT) · airframe 14,243 hrs · 7,550 cycles

DFW - FLIGHT 3130, THE CREW REPORTED A LOSS OF OIL PRESSURE AND QTY ON THE NUMBER TWO ENGINE DURING CRUISE. THE NUMBER TWO ENGINE WAS SHUT DOWN AS A PRECAUTION, AND THE AIRCRAFT DIVERTED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (RIGHT) · airframe 14,240 hrs · 7,548 cycles

GJT - FLIGHT 3029, THE CREW REPORTED SMOKE IN THE CABIN FROM THE NUMBER TWO PACK. THE AIRCRAFT DIVERTED TO GJT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO PACK ON MEL 21-51-00 CTL NUMBER 136236. ON 01/02/08 MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE DUE TO INTERNAL OIL LEAKAGE, OPERATIONALLY CHECKED THE PACK SYSTEM WITH NO DEFECTS NOTED, CLEARED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 14,080 hrs · 7,469 cycles

THE REAR FUSELAGE LOWER SKINS AND ADJACENT STRUCTURE OF FRAME 66 WERE DAMAGED. MAINTENANCE INDUCED. REPLACED TWO SKIN PANELS AND SEVERAL SHEAR CLIPS AT FRAME 66 AND REPAIRED SEVERAL DENTS ON THE SKIN JUST FORWARD OF FRAME 66. REPAIRED IAW EA5330-01109. AIRCRAFT STILL IN C CHECK.

Part: RIVET — CRACKED (VERTICAL STAB) · airframe 14,080 hrs · 7,469 cycles

TYS - DURING A CURRENT 3C INSPECTION THE RIGHT AFT FUSELAGE AT FR 76 WAS FOUND WITH SOME CRACKED RIVETS ON THE CONTOUR FLANGE OF THE VERTICAL STAB. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT FUSELAGE CONTOUR FLANGE DRAG ANGLE AT FR 76. ALL WORK WAS ACCOMPLISHED IAW EMB 145 XR SRM 51-46-02, 51-20-03 AND CPM 51-21-07. AIRCRAFT WILL BE RELEASED AT THE END OF THE CHECK.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 13,366 hrs · 7,100 cycles

TYS ECIAS SHOWED BAGGAGE SMOKE INDICATION DURING FIRE DETECTION TEST AND BAGGAGE LIGHT NOT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED NR 1 BAGGAGE DETECTOR IAW EMB 145 AMM 26-15-01. ALL OPS CHECKS WERE GOOD AND RELEASED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 10,676 hrs · 5,687 cycles

IAH - FLIGHT 2973, THE CREW REPORTED A VERY STRONG ODOR ON THE GROUND AFTER ENGINE START THAT WENT AWAY AND CAME BACK DURING ICE TEST IN FLIGHT, AND WHICH WENT AWAY AGAIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE ENGINES AND BLEED AIR SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOUSING — GOUGED (V STAB BEARING) · airframe 9,257 hrs · 4,950 cycles

LT VERT STAB SPHERICAL BEARING HOUSING GOUGED. REAMED RT AND LT HOUSING AND INSTALLED BEARINGS IAW COEX EC5510-01138.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,923 hrs · 3,708 cycles

MCI - DURING SCHEDULED MAINTENANCE, THE RIGHT OVERWING EMERGENCY EXIT MARKER WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER, OPERATIONALLY TESTED THE EMERGENCY LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY.

Part: PIN — INSTALLED (NOSE GEAR) · airframe 5,649 hrs · 3,023 cycles

CLE - CREW REPORTED THAT THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THAT THE NOSE GEAR SAFETY PIN HAD NOT BEEN REMOVED. MAINTENANCE REMOVED THE NOSE GEAR SAFETY PIN AND RETURNED AIRCRAFT TO SERVICE.

Part: CONNECTOR — DIRTY (INVERTER) · airframe 5,437 hrs · 2,923 cycles

IAH - FLIGHT 3252, THE CREW REPORTED THAT THE FORWARD EMERGENCY LIGHT IN THE GALLEY WAS INOPERATIVE. MAINTENANCE CLEANED THE INVERTER CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS PART IS NOT SERIALIZED, AND NO TIMES ARE AVAILABLE

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

IAH - FLIGHT 2556, DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT NUMEROUS EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK IAW EMB-145 AMM 33-50-04, OPERATIONALLY CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

THE EMERGENCY LIGHT AT THE PASSENGER DOOR ENTRANCE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ASSEMBLY, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY.

Part: LIGHT — INOPERATIVE (CABIN)

CREW REPORTED THAT THE EMERGENCY LIGHTS DID NOT WORK. AWAITING FURTHER INFORMATION TO COMPLETE THIS REPORT. THE EMERGENCY LIGHT SYSTEM WAS OPERATIONALLY TESTED AND THE DISCREPANCY COULD NOT BE CONFIRMED.

Part: FLIGHT RECORDER — FAULTY (COCKPIT) · airframe 1,751 hrs · 978 cycles

THE CREW RECIEVED A BAGGAGE SMOKE INDICATION AT FL270, THE FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT DIVERTED TO ATL. THE AIRCRAFT WAS INSPECTED AND DEEMED SAFE FOR A FERRY FLIGHT TO TYS. MAINTENANCE FOUND THE SSDFDR TO BE FAULTY AND WAS REPLACED IAW EMB M.M. 31-31-01, ALL OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB M.M. 31-31-00. THE AIRCRAFT WAS RELEASED FOR SERVICE.