N11192

Part: LIGHT — MISINSTALLED (ZONE 200) · airframe 41,682 hrs · 27,463 cycles

LH OVERWING EXTERNAL EMERGENCY LIGHT INSTALLED UPSIDE DOWN. REORIENTATED LH OVERWING EXTERNAL EMERGENCY LIGHT IN CORRECT ORIENTATION. OPS CHECK SAT

Part: RADOME — DELAMINATED (UNKNOWN) · airframe 39,351 hrs · 25,337 cycles

ELECTRICAL SMELL AND VISIBLE ARCING AT RADOME WHILE RADAR ON AND IN CLOUDS. PERFORMED DVI OF RADAR. OPS CHECKED. STBY SWITCH IN NORMAL POSITION, OPS CHECKED GOOD - NO FAULTS FOUND. PERFORMED DVI OF RADOME. FOUND DELAMINATION ON RADOME AND BOTH BONDING JUMPERS LOOSE - REMOVED AND REPLACED RADOME AND RESECURED BONDING JUMPERS. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,225 hrs · 25,223 cycles

EMERGENCY ENGINE #1 OUT IN FLIGHT. PERFORMED #1 ENGINE BORESCOPE INSPECTION AND FOUND MISSING AND DESTROYED VARIABLE BLADES AND COMPRESSOR BLADES. FOUND NO DAMAGE TO AIR INLET AND T/R. REMOVED AND REPLACED #1 ENGINE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 39,062 hrs · 25,069 cycles

RF1, CARGO DOOR SURROUND STRUCTURE AFT L-SHAPE AT FR 68 FOUND CORRODED. SHEAR CLIP REPAIRED WITH A SPLICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 39,062 hrs · 25,069 cycles

RF1, CARGO DOOR SURROUND STRUCTURE FWD L-SHAPE AT FR 65 FOUND CORRODED. SHEAR CLIP REPAIRED WITH A SPLICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,062 hrs · 25,069 cycles

RF1 LH CRACK FOUND ON FRAME SECTION FR 68, UNDER CARGO DOOR AFT RAIL. Z FRAME REPAIRED WITH A SPLICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 39,062 hrs · 25,069 cycles

AT REAR FUSE 1 EXT, BELLY SKIN FOUND CORRODED ON FR 67 AND BTW STR 20L-20R. SKIN REPAIRED WITH A DOUBLER AND INTERNAL STRAP SPLICED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,062 hrs · 25,069 cycles

CRACKS SUSPECTED (10X) ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. AFTER NDT INVESTIGATION, 7 CRACKS FOUND, SKIN REPAIRED WITH 1 REPAIR DOUBLER AND 6 BUSHINGS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,062 hrs · 25,069 cycles

VERT STAB, RH SKIN DENT AT AFT OF SPAR 41% AND 1 INCH UNDER RIB ZV 2799.0. SKIN REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 39,062 hrs · 25,069 cycles

CF4, MIDDLE GUSSET IN TOILET AREA BTW FR 59-61 FOUND CORRODED. AFTER GUSSET REMOVAL, OMEGA BEAM FOUND CORRODED. BEAM REPAIRED WITH A DOUBLER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 39,062 hrs · 25,069 cycles

CF1, CORROSION FOUND ON RH OMEGA BEAM AT FR 18 ON FLOOR STRUCTURE AREA. BEAM REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,062 hrs · 25,069 cycles

EXISTING REPAIR TO INVESTIGATE ON LH FWD FUSE 1 SKIN, BTW FR 6-7 AND AT STR 15L, UNDER GPU ACCESS DOOR. SKIN REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 39,062 hrs · 25,069 cycles

AT REAR FUSE 1 EXT, RADIO ALT ANTENNA NO 2 AFT LOWER DOUBLER AND BELLY SKIN FOUND CORRODED BTW FR 68-70. SKIN REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 39,062 hrs · 25,069 cycles

CF4, CORROSION FOUND ON CENTER OMEGA BEAM #6 LH FLANGE BTW FRAME 52-59. BEAM REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 39,062 hrs · 25,069 cycles

AT LH TR ASSY, AFT OUTBD SIDE, CORROSION SUSPECTED UNDER SKIN. LH TR ASSY REMOVED AND REPLACED. OPS CHECK SAT.

Part: DOOR — DAMAGED (NOT REPORTED) · airframe 38,425 hrs · 24,490 cycles

RH MLG AUX DOOR HAS COMPOSITE DAMAGE ON STIFFNER. RAR RH MLG AUX DOOR. ALL GAP CHECKS GOOD. GEAR SWINGS PERFORMED. ALL OPS CHECKS SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,146 hrs · 24,242 cycles

LH WING LOWER EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH EXT EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: PANEL — LOOSE · airframe 37,619 hrs · 23,762 cycles

18 A EXIT ROW PANEL NOT STAYING ON. RESECURED EXIT ROW 18A ACCESS PANEL

Part: PANEL — MISSING · airframe 37,566 hrs · 23,717 cycles

LEFT SIDE EMERG EXIT PANEL FALLING OFF. RESECURED LEFT EXIT HANDLE COVER

Part: BATTERY PACK — INOPERATIVE · airframe 37,507 hrs · 23,665 cycles

FOUND BOTH OVERWING EMERGENCY LIGHTS INOP. SUSPECT BATTERY #4 IS NOT HOLDING A CHARGE. R&R EMERGENCY LIGHT BATTERY POWER SUPPLY #4

Part: LAMP — INOPERATIVE · airframe 37,340 hrs · 23,514 cycles

EXTERNAL LH REAR EMERGENCY LIGHT LAMP INOPERATIVE. REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 36,932 hrs · 23,180 cycles

NUMBER ONE EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT

Part: INVERTER — FAULTED (EMERGENCY LIGHTS) · airframe 36,476 hrs · 22,764 cycles

EMERGENCY LIGHT ON AFT GALLEY WALL INOPERATIVE. SWAPPED CANNON PLUGS ON EMERGENCY LIGHT INVERTERS 2 AND 3, FAULT FOLLOWED ON INVERTER 3. REMOVED INVERTER 3. REPLACE INVERTER FOR EMERGENCY LIGHTS. OPS CHECK GOOD.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 36,142 hrs · 22,464 cycles

DURING C-CHECK INSPECTION THE LAVE DRAIN VALVE SUPPORT WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DRAIN VALVE SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 36,142 hrs · 22,464 cycles

DURING C-CHECK INSPECTION THE BAGGAGE COMPARTMENT DOOR SILL BEAM WAS FOUND TO BE CORRODED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL BEAM, AND THE AIRCXRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,973 hrs · 21,586 cycles

MAINTENANCE REPORTED THE EXIT SIGN ABOVE FA JUMPSEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE #1 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 34,886 hrs · 21,516 cycles

DURING MX INSPECTION THE EMERGENCY EXIT LIGHT ABOVE FLT ATTENDANT SEAT WILL NOT ILLUMINATE. MX REMOVED AND REPLACED EXIT MARKING SIGN ASSEMBLY WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (RUDDER) · airframe 33,244 hrs · 20,315 cycles

TYS A/WAS IN FOR A A-CHECK WITH A RUDDER INSPECTION TASK CARD AND FOUND THE RUDDER 1 LE SKIN DENTED ON THE LEFT SIDE APPROXIMATELY 3 FEET FROM THE BOTTOM OF THE RUDDER. MAINTENANCE CUTOUT A 4 INCH X1.5 INCH SECTION OF SKIN AND INSTALLED A FILLER AND DOUBLER IAW ETD 2018-145-056520. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AFTER ALL CHECKS AND BACKLASHES ARE PERFORMED.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 33,091 hrs · 20,208 cycles

DURING INSPECTION, A CREASED DENT WAS FOUND AT FRAME 4 ABOVE STRINGER 17L. MEASUREMENTS ARE L=3.5", W=3.25", D=.005". DAMAGE WAS CUT OUT AND A DOUBLER REPAIR WAS APPLIED PER ETD2018-145-040730.

Part: SIGN — DISCONNECTED (EMERGENCY LIGHTS) · airframe 32,442 hrs · 19,762 cycles

DURING A MAINTENANCE INSPECTION, THE EXIT SIGN AT SEAT 3C WAS FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE EMERGENCY LIGHT, OPS TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 23,096 hrs · 19,527 cycles

IAH - FLIGHT 4289 THE CREW REPORTED THAT BELOW 10000 PACKS PRODUCING A STRONG OIL SMELL WITH COMPLAINTS FROM BOTH CREW AND PASSENGERS. THE AIRCRAFT LANDED AT IAH WITH NO INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER ONE ENGINE. OPERATIONAL CHECKS WERE COMPLETED SUCCESSFULLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 10/24/17.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,705 hrs · 17,093 cycles

DURING MAINTENANCE INSPECTION THE LT & RT OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,563 hrs · 16,987 cycles

DURING MAINTENANCE INSPECTION THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,964 hrs · 13,272 cycles

UPPER CENTER EMERGENCY AFT LIGHT WAS REPORTED INOPERATIVE. MX R & R EMERGENCY LIGHT INVERTER, OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,307 hrs · 12,214 cycles

DURING MX INSPECTION A LARGE DENT FROM GROUND DAMAGE WAS DISCOVERED AT FRAME 20 BETWEEN STRINGERS 13L AND 14L. MX REMOVED THE DAMAGED SECTION OF SKIN, AND INSTALLED A FILLER AND DOUBLER REPAIR. LEAK CHECKS WERE PERFORMED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 05/01/13.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,467 hrs · 10,337 cycles

MAIN CABIN RT SIDE FLOOR SILL BETWEEN FRM 48 TO 52 CORRODED BEYOND LIMITS ON UPPER SURFACE. R & R SILL.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,467 hrs · 10,337 cycles

PAX DOOR THRESHOLD CORRODED AROUND SCREW HOLES. R & R U-SHAPED SUPPORTS AND SUPPORT ASSY.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,467 hrs · 10,337 cycles

LT SIDE SUPPORT CORRODED AT FRM 61 AT SILL. R & R SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,467 hrs · 1,037 cycles

LEFT OTBD FLOOR SUPPORT CORRODED. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 18,467 hrs · 10,337 cycles

AFT CARGO AT FRAME 61 RT OTBD FLOOR SUPPORT CORRODED BEYOND LIMITS AROUND NUT PLATES. REMOVED AND REPLACED FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,467 hrs · 10,337 cycles

LEFT OTBD FLOOR FLOOR SUPPORT AT FRM 42-44 CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 18,467 hrs · 10,337 cycles

RT OTBD FLOOR SUPPORT CORRODED BEYOND LIMITS AT FRAME 48-50. R & R FLOOR SUPPORT.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 18,467 hrs · 10,337 cycles

CORROSION BEYOND LIMITS ON GUSSET AT FRM 60 AND Y479. R & R GUSSET.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 18,467 hrs · 10,337 cycles

CARGO FLOOR SUPPORT CORRODED BEYOND LIMITS AT FRM 61. REMOVED AND REPLACED FLOOR SUPPORT.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 18,394 hrs · 11,434 cycles

LAVATORY SMOKE EICAS INDICATION REPORTED SHORTLY AFTER TAKEOFF. SMOKE FILLING CABIN FROM LAVATORY AREA AND FROM THE VENTS IN CABIN. FOUND NR 2 ENGINE OIL SYSTEM LEAKING. R & R NR 2 ENGINE IAW TASK CARD 6271001 WITH OPS AND LEAK CHECKED SUCCESSFUL. PERFORMED CONDITIONED AIR DUCT-OIL DECONTAMINATION IAW AMM 21-20-00 WITH NO SIGNS OF SMOKE. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OIL SYSTEM — LEAKING (NR 2 ENGINE) · airframe 18,393 hrs · 10,287 cycles

THE CREW REPORTED A LAVATORY SMOKE INDICATION SHORTLY AFTER TAKEOFF. SMOKE FILLED CABIN. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. FOUND NR 2 ENGINE OIL SYSTEM LEAKING, REPLACED THE NR 2 ENGINE. OPS CHECKED GOOD.

Part: FILTER — DIRTY (FAN AIR VALVE) · airframe 16,788 hrs · 9,191 cycles

AMA - FLIGHT 5883, THE CREW REPORTED A BLEED ONE AND TWO OVERTEMP IN ICING CONDITIONS. THE AIRCRAFT DIVERTED TO AMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH FAN AIR VALVE FILTERS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COLLECTOR — LEAKING (ENGINE) · airframe 16,702 hrs · 9,121 cycles

ICT - FLIGHT 5914 THE CREW REPORTED THAT DUE TO OIL LOSS ENGINE ONE WAS SHUTDOWN AS A PRECAUTION. THE AIRCRAFT LANDED IN ICT WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ENGINE, REMOVED AND REPLACED THE CENTER SUMP SCAVENGE PUMP CHIP COLLECTOR, SERVICED THE OIL, PERFORMED HIGH POWER RUNS WITH THE CREW WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — FAILED (CARGO BAY) · airframe 15,680 hrs · 8,547 cycles

FLIGHT 2721 - FLIGHT CREW REPORTED BAGG SMOKE DET, NO TEST. EWR MX REMOVED AND REPLACED BAGG FAN RELAY K0630 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 13,474 hrs · 7,305 cycles

IAH - FLIGHT 2834, THE CREW REPORTED AUTO PRESSURIZATION FAILURE WITH THE MANUAL MODE INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MANUAL CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,460 hrs · 7,295 cycles

SHV - DURING C-CHECK FRAME 68 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 17-18L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — WORN (LT WING) · airframe 13,460 hrs · 7,295 cycles

SHV - DURING C-CHECK THE LT AILERON I/B HINGE BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,460 hrs · 7,295 cycles

SHV - DURING C-CHECK THE SHEAR CLIP ON FRAME 65 BETWEEN STRINGERS 17-18L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,460 hrs · 7,295 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 20-21. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,460 hrs · 7,295 cycles

SHV - DURING C-CHECK FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01505. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,010 hrs · 6,524 cycles

IAQH - FLIGHT 2471, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THE AISLE OVERHEAD EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MAINTENANCE RESET THE EMERGENCY LIGHTS, VERIFIED NORMAL OPERATION. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,873 hrs · 5,907 cycles

RIC MX - DURING SCHEDULED MAINTENANCE, FOUND EMERGENCY LIGHT INOPERATIVE IN FRONT OF SEAT 3B. MX REMOVED AND REPLACED EXIT SIGN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,403 hrs · 5,650 cycles

EMERGENCY EXIT SIGN AFT OF GALLEY, INOP. REMOVED AND REPLACED SIGN. OPS CHECK GOOD.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 10,331 hrs · 5,613 cycles

CREW REPORTED AT FL360, THE NR 2 ENGINE OVERTEMP TO 905C AND N2 WENT TO 101.1 PERCENT WITH THE FUEL FLOW 1400LBS MORE THAN THE NR 1 ENGINE FOR THE SAME N1. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE NR 2 ENGINE LT AND RT COMPRESSOR AIR DISCHARGE TUBES, AND REPLACED THEIR GASKETS, REMOVED AND REPLACED THE NR 2 ENGINE FPMU, AND CABV (COMPRESSOR ACCELERATION BLEED VALVE), OPS AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS BEING NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GASKET — FAILED (RT ENGINE) · airframe 10,331 hrs · 5,613 cycles

CREW REPORTED AT FL360, THE NR 2 ENGINE OVERTEMP TO 905C AND N2 WENT TO 101.1 PERCENT WITH THE FUEL FLOW 1400LBS MORE THAN THE NR 1 ENGINE FOR THE SAME N1. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE NR 2 ENGINE LT AND RT COMPRESSOR AIR DISCHARGE TUBES, AND REPLACED THEIR GASKETS, REMOVED AND REPLACED THE NR 2 ENGINE FPMU, AND CABV (COMPRESSOR ACCELERATION BLEED VALVE), OPS AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS BEING NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GASKET — FAILED (RT ENGINE) · airframe 10,331 hrs · 5,613 cycles

CREW REPORTED AT FL360, THE NR 2 ENGINE OVERTEMP TO 905C AND N2 WENT TO 101.1 PERCENT WITH THE FUEL FLOW 1400LBS MORE THAN THE NR 1 ENGINE FOR THE SAME N1. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE NR 2 ENGINE LT AND RT COMPRESSOR AIR DISCHARGE TUBES, AND REPLACED THEIR GASKETS, REMOVED AND REPLACED THE NR 2 ENGINE FPMU, AND CABV (COMPRESSOR ACCELERATION BLEED VALVE), OPS AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS BEING NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — STICKING (ROLL TRIM) · airframe 9,188 hrs · 4,985 cycles

EWR FLIGHT NR 2879 THE CREW REPORTED A ROLL TRIM SWITCH STUCK IN FLIGHT. THE ACFT DIVERTED AND LANDED IN CLE. MX INSPECTED AND CLEANED AND LUBRICATED THE ROLL TRIM SWITCHES. OPS CHECKS WERE GOOD. A COMPANY ECTM WORKSHEET WAS ISSUED AND THE TRIM SWITCH WAS REPLACED. OPS CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 8,566 hrs · 4,655 cycles

SHV-DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 17. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01417. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — WORN (RUDDER) · airframe 8,566 hrs · 4,655 cycles

SHV-DURING C-CHECK THE RUDDER CENTER UPPER HINGE BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED HINGE BRACKET IAW EMB 145XR SRM 55-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · airframe 8,566 hrs · 4,655 cycles

SHV-DURING C-CHECK THE CARGO DOOR LOWER CUT-OUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,566 hrs · 4,655 cycles

SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02 AND EC5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 8,566 hrs · 4,655 cycles

SHV - DURING C-CHECK RT AILERON CENTER O/B BRACKET HAS MIGRATING HAT BUSHING. MX REMOVED AND REPLACED RT AILERON CENTER O/B BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: GROUND WIRE — BURNED (CABIN) · airframe 8,555 hrs · 4,647 cycles

TYS - AIR RETURN - LAV SMOKE INDICATION ON CLIMBOUT. ONCE ON GROUND F/A REPORTED, THERE WAS A LOT OF HEAT COMING FROM BEHIND THE EXIT ROW, BUT NO VISIBLE SMOKE. MX FOUND AND REPAIRED A BROKEN GROUND WIRE ON THE THERMAL DISTRIBUTION SWITCH IAW EMB 145XR WM 20-21-00 AND OPS CHECKED GOOD IAW EMB 145XR AMM 21-20-00 AND EMB 145XR AMM 26-14-00. A SATISFACTORY TEST FLIGHT WAS ALSO PERFORMED AND THE A/C WAS RELEASED BACK TO SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION

FLIGHT CREW REPORTED E1 T/R DISAGREE ON T/O ROLL. FLIGHT CREW CYCLED NR 1 T/R AND COULD NOT DUPLICATE MSG. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (K)

Part: SMOKE DETECTOR — DIRTY (LAVATORY)

FLT 0210 - SMF - FLIGHT CREW REPORTED LAV SMOKE DETECTOR ACTIVATED ON CLIMB. MAINTENANCE REMOVED, CLEANED, REINSTALLED LAV SMOKE DETECTOR SENSOR ASSY. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: IGNITER — INOPERATIVE (ENGINE)

FLT 0519 - AUS - FLIGHT CREW REPORTED E2 DRIPPING FUEL WHILE RUNNING ACCORDING TO GROUND RAMP. MAINTENANCE INSPECTED AND FOUND FUEL FROM PREVIOUS ABORTED/HUNG START (NOT DRIPPING WHEN RUNNING). FOUND E2A IGNITER INOPERATIVE. MAINTENANCE PLACED ON MEL. ON 06/18/2008 FLIGHT CREW REPORTED DURING START ENG NR 2 WAS LEAKING A STREAM OF FUEL FROM LOWER COWLING - FOLLOW THE START FUEL STILL LEAKING BUT AT REDUCED RATE. MAINTENANCE REMOVED AND REPLACED IGNITERS. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN TO SERVICE. (S)

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 7,291 hrs · 3,932 cycles

FLT 982 - ONT - FLIGHT CREW REPORTED LAV SMOKE INDICATION. DECLARED EMERGENCY, LANDED SAFELY WITHOUT INCIDENT. MIX PERSONNEL CLEANED SMOKE DETECTOR OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 6,679 hrs · 3,612 cycles

AUS - DURING MAINTENANCE INSPECTION, THE LOWER RIGHT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — BURNED (CARGO BAY) · airframe 6,173 hrs · 3,367 cycles

FLT 16 - SAT TO ONT - FLIGHT CREW REPORTED BAGGAGE FIRE TEST LIGHT WILL NOT COME ON DURING TEST. MX PERSONNEL AT ONT REMOVED AND REPLACED RELAY K0629 IAW EMB145XR WM 20-13-02 AND 26-10-00, OPERATIONALLY CHECKED SYSTEM AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY CONDITION.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 6,259 hrs · 3,406 cycles

FLT 0017 - ONT TO SAT - CREW REPORTED LAV SMOKE EICAS MASTER WARNING IN FLIGHT. A/C HAD JUST BEEN DEICED MESSAGE CLEARED FO CKD LAV AND THERE WAS NO SIGN OF SMOKE. MX PERSONNEL PERFORMED OPERATIONAL CHECK AND NO FAULTS WERE NOTED AT THAT TIME. A/C WAS RELEASED IN AIRWORTHY CONDITIONS.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 6,092 hrs · 3,327 cycles

SAT - FLIGHT 216, THE CREW REPORTED A LAV SMOKE EICAS MASTER WARNING IN FLIGHT AFTER THE AIRCRAFT HAD JUST BEEN DEICED IN OKC. THE MESSAGE CLEARED BY ITSELF, AND THE FO VERIFIED NO SMOKE IN THE LAV. THE AIRCRAFT CONTINUED TO SAT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — ODOR (NR 1) · airframe 4,306 hrs · 2,345 cycles

WHILE CLIMBING THROUGH 10,000 FT, CABIN CREW REPORTED A VERY STRONG ACRID ODOR FROM MAIN CABIN DOOR BACK THROUGH SEAT 4A. CONTRACT MX REMOVED PANELS, INSPECTED LIGHTS BALLAST AND BULBS CONTACTS FROM PASSENGER SEAT 1A THRU 4A, ALSO REMOVED CD PLAYER AND INSPECTED WIRING. A/C WAS RELEASE ON A FERRY FLIGHT FROM SMF TO ONT. MX REMOVED AND REPLACED NR 1 ENG IAW TASKCARD 6271001 ALL LEAKS AND OPERATIONAL CHECKS SUCCESSFULLY. THE A/C WAS APPROVED TO RETURN FOR SERVICE. [07-27-07] MX REMOVED AND REPLACED NR 1 ENG IAW TASKCARD 6271001. ALL LEAK AND OPERATIONAL CHECKS SUCCESFULLY.THE A/C WAS APPROVED TO RETURN FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 3,028 hrs · 1,671 cycles

DENT AND GOUGE ON RIGHT SIDE OF AIRCRAFT BELOW PYLON BETWEEN FR66 AND 68, STR 13R AND 15R. CUT OUT DAMAGE, FABRICATED DOUBLER, FILLER AND INSTALLED, IAW EC 5330-01617 PRESSURE CK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: CONTROLLER — BURNED (WINDSHIELD HEAT) · airframe 2,444 hrs · 1,333 cycles

IAH - FLIGHT 2749, THE CREW REPORTED A BURNING SMELL IN THE CABIN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.