N11176

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 45,127 hrs · 31,700 cycles

CAPT WINDSHIELD CRACKED. REMOVED AND REPLACED CAPT WINDSHIELD. OPS CHECK SAT.

Part: LIGHT — MISSING (ZONE 200) · airframe 43,988 hrs · 30,637 cycles

PHOTO-LUMINESCENT LIGHTING STRIP MISSING AT FRONT OF AIRCRAFT. INSTALLED MISSING LIGHT STRIP

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 43,658 hrs · 30,334 cycles

MULTIPLE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 43,276 hrs · 29,994 cycles

COCKPIT EMERGENCY LIGHT OUT. REMOVED AND REPLACED BULB. OPS CHECK SAT.

Part: PROCESSOR — INOPERATIVE (UNKNOWN) · airframe 42,069 hrs · 28,917 cycles

AIRSPEED MISMATCH BTWEEN CAPT, FO AND ISIS AT 35000. INSPECTED AND DRAINED WATER FROM PITOT 1 AND 2 DRAIN LINES. PERFORMED OPERATIONAL CHECK OF ADC AND PITOT/STATIC HEATING SYSTEM. ADC AND PITOT/STATIC HEATING CHECKS WERE SATISFACTORY. REMOVED AND REPLACED ADC #1. OPS CHECK FAILED. FOUND PITOT AND STATIC HOSE CONNECTING TO ADC 1 PLUS STATIC HOSE CONNECTING TO ADC 2 CRACKING AND DAMAGED. PITOT SYSTEM 1 UNSAT, PITOT SYSTEM 2 SAT. FOUND FITTING FOR #1 STATIC HOSE LOOSE AT ANEMOTRIC STATIC PORT #1, RESECURED FITTING. PERFORMED PITOT SYSTEM 1 AND 2 LEAK CHECK. BOTH 1 AND 2 SAT.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 41,436 hrs · 28,329 cycles

ROW 7 AISLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED ROW 7 AISLE EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 41,436 hrs · 28,329 cycles

LH OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT BULB. OPS CHECK SAT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,240 hrs · 28,167 cycles

LEFT EMERG EXIT SEAL COMING OFF DEFERED PER NEF PLACARD  APPLIED. RESECURED LH EMERGENCY EXIT SEAL. PLACARD REMOVED. NEF CLEARED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,168 hrs · 28,104 cycles

RVSM CRITICAL REGION FAILED INSPECTION FOR SKIN WAVINESS. LH RVSM DOUBLER REWORKED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,168 hrs · 28,104 cycles

DAMAGE FOUND ON LH RUDDER II SKIN AROUND NUTPLATE BTW RIB ZV 2067.0 AND RIB 2357.0. SKIN REPAIRED WITH A DOUBLER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,168 hrs · 28,104 cycles

CF1, CRACK FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 23-24. CF1, CRACK FOUND LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 23-24 REPAIRED WITH A DOUBLER

Part: NONE — NONE · airframe 41,058 hrs · 28,005 cycles

RH EXTERNAL OVER WING EMERGENCY LIGHT INSTALLED UPSIDE DOWN. REMOVED AND REORIENTED RH EXTERNAL OVER WING EMERGENCY LIGHT. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,706 hrs · 27,687 cycles

MULTIPLE EMERGENCY LIGHTS IN GALLEY AND EXTERNAL RH FWD EMERGENCY LIGHTS INOPERATIVE. FOUND EMERGENCY LIGHT BATTERY PACK NOT SECURED TO CHARGER. REINSTALLED AND SECURED BATTERY PACK. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE · airframe 40,346 hrs · 27,362 cycles

EMERGENCY STRIP WALL LIGHTING ROW 1 LOOSE. RESECURED EMERGENCY STRIP

Part: NOT REPORTED — NOT REPORTED · airframe 39,782 hrs · 26,853 cycles

EMERGENCY FLOOR LIGHT STRIP MISSING IN FRONT OF 1A. INSTALLED EMERGENCY FLOOR LIGHT STRIP IN FRONT OF SEAT 1A

Part: NOT REPORTED — NOT REPORTED · airframe 39,563 hrs · 26,661 cycles

EMERGENCY FLOOR ISLE STRIP BY SEAT 18C AND 20C IS DETACHED FROM FLOOR. RE SECURED EMERGENCY STRIP. NO DEFECTS NOTED AT THIS TIME.

Part: SEALANT — MISSING (RT MLG) · airframe 38,365 hrs · 25,585 cycles

RH MLG LOWER SIDE ARM LOWER FLANGE BEARING HAS MISSING SEALANT. APPLIED SEALANT TO RT MLG LOWER SIDE ARM FLANGE BEARING.

Part: SKIN — DAMAGED (RT WING) · airframe 38,263 hrs · 25,491 cycles

RH WING LE NOSE SKIN AT VORTILLONS NO 2, NO 3, AND NO 4. AT RH WING LE NOSE SKIN AT VORTILLON NO 2, NO 3, AND NO 4 REPAIRED.

Part: SKIN — CRACKED · airframe 38,263 hrs · 25,491 cycles

LH WING L/E NOSE SKIN CRACKED AT VORTILLON NO 2, NO 3, AND NO 4. AT LH WING LE NOSE SKIN CRACKED AT VORTILLON NO 2, NO 3, AND NO 4 REPAIRED.

Part: RIB — CRACKED · airframe 38,263 hrs · 25,491 cycles

RH WING LE2 IN.B MACHINED RIB CRACKED. MACHINED RIB ASSEMBLY REPLACED.

Part: SHEAR TIE — CRACKED (FRAME 66) · airframe 38,263 hrs · 25,491 cycles

SHEER CLIP FOUND CRACKED AT LH FRAME 66 BTW STR 6L-7L. SHEAR CLIP AT L/H FR 66 BTW STR 6L-7L REMOVED FOR REPLACEMENT. SHEAR CLIP REPLACED.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 38,263 hrs · 25,491 cycles

SHEER CLIP FOUND CRACKED AT LH FRAME 68 AND BTW STR 6L-7L. LH ENGINE PRECOOLER TO ENGINE BLEED VALVE DUCT AND "Y-SHAPED" DUCT AFT OF BLEED VALVE REMOVED FOR ACCESS. SHEER CLIP AT LH FRAME 68 BTW STR 6L-7L REPLACED. LH ENGINE PYLON BLEED AIR "Y' DUCT INSTALLED. LH ENG BLEED AIR DUCT INSTALLED.

Part: SHEAR TIE — CRACKED (FRAME 62) · airframe 38,263 hrs · 25,491 cycles

SHEER CLIP FOUND CRACKED AT RH FRAME 62 BTW STR 6R-8R. SHEAR CLIP FOUND CRACKED AT LH FRAME 62 BTW STR 6R-8R REPLACED

Part: DOUBLER — CORRODED (FWD DOOR FRAME) · airframe 38,263 hrs · 25,491 cycles

FWD DOOR CUT OUT L SHAPE DOUBLER REPAIR FOUND CORRODED BTW STR 16L-17L. FWD DOOR CUT OUT L SHAPE DOUBLER REPAIR FOUND CORRODED BTW STR 16L-17L. DOUBLER REPAIRED.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 38,263 hrs · 25,491 cycles

SHEER CLIP FOUND CRACKED AT LH FRAME 67 AND BTW 6L-7L. CRACKED SHEER CLIP AT LH FRAME 6-7 BTW 6L-7L REPLACED.

Part: STRUCTURE — CORRODED (FRAME 68) · airframe 38,263 hrs · 25,491 cycles

AFT CARGO DOOR CUTOUT L SHAPE AT FR 68 CORROSION FOUND BETWEEN STR 16L-18L. AFT CARGO DOOR CUTOUT L-SHAPE AT FRAME 68 CORROSION FOUND BTW STR 16L-18L REPAIRED.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 38,263 hrs · 25,491 cycles

SHEAR CLIP FOUND CRACKED AT LH FRAME 73 AND STR 8L-9L. SHEER CLIP AT LH FRAME 73 AND STR 8L-9L REMOVED FOR REPLACEMENT. SHEAR CLIP AT LH FRAME 73 BTW STR 8L-9L REPLACED

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 38,263 hrs · 25,491 cycles

SHEER CLIP FOUND CRACKED AT LH FRAME 65 BTW STR 7L-9L. SHEAR CLIP FOUND CRACKED AT LH FRAME 65 BTW STR 7L-9L REPLACED.

Part: SKIN — DENTED (FRAMES 25-26) · airframe 38,263 hrs · 25,491 cycles

CF2, BTW FR 25-26, STR 11L, SKIN DENTED. CENTER FUSELAGE -2 BTW FR 25-26 AND STR 11L, SKIN DENT REPAIRED.

Part: SKIN — CRACKED (ZONE 200) · airframe 38,263 hrs · 25,491 cycles

MULTIPLE CRACKS FOUND ON LH SKIN ON FRAMES 77, 78, 79, 80 BTW STR 3L-10L. MULTIPLE CRACKS FOUND ON LH SKIN ON FRAMES 77, 78, 79, 80 BTW STR 3L-10L REPAIRED

Part: FRAME — CRACKED · airframe 38,263 hrs · 25,491 cycles

MULTIPLE CRACKS FOUND ON RH SKIN ON FRAMES 77-78-79 AND BTW STR 3R-10R. CRACKS (X7) ARE REPAIRED

Part: SHEAR TIE — CRACKED (FRAME 62) · airframe 38,263 hrs · 25,491 cycles

SHEER CLIP FOUND CRACKED AT LH FRAME 62 AT STR 6L-8L. SHEER CLIP INSTALLED WITH NEW FASTENERS.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 38,263 hrs · 25,491 cycles

RH FUSELAGE BTW FR 16-17 BTW STR 10-12, REPAIR DOUBLER NOT PROPERLY INSTALLED. RH FUSELAGE BETWEEN FRAME 16-17 AND BTW STR 10R-12R REPAIR DOUBLER NOT PROPERLY INSTALLED. REPAIR REWORKED.

Part: SKIN — CORRODED (ZONE 100) · airframe 38,263 hrs · 25,491 cycles

CF1, BTW FR 17-18 AND BTW STR 21L-21R, SKIN CORRODED. CF1, BTW FRAMES 17-18 AND BTW STR 21L-21R CORRODED SKIN REPAIRED.

Part: SKIN — CANNING (FRAMES 22-23) · airframe 38,263 hrs · 25,491 cycles

OIL CAN FOUND ON LH SKIN BTW FR 22-23 AND STR 11L-12L. DAMAGE REPAIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,308 hrs · 23,638 cycles

EMERGENCY LIGHTS FOUND IN ARMED POSITION. EMERGENCY LIGHTS WILL NOT ILLUMINATE. R&R EMERGENCY LIGHTS 1-4. OPS CHECK SAT. (#1 PN 2013-1A SN 101459 TSN:55547:56 CSN: 23980 #2 PN ABS-2013-1A SN 38159 TSN: 1389:01 CSN: 1204 #3 PN: ABS-2013-1A SN 48554 TSN: 1389.01 CSN: 1204 #4 PN ABS-2013-1A SN 48553 TSN: 1389.01 CSN: 1204)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,998 hrs · 22,509 cycles

RT AFT EMERGENCY LIGHT ABOVE WING INOPERATIVE. R&R AFT EMERGENCY LIGHT ABOVE WING. OPS CHECK SAT.

Part: DOOR FRAME — CORRODED (FRAME 65) · airframe 34,959 hrs · 22,467 cycles

BAGGAGE DOOR CUTOUT "Z" FRAME AT STGR 16L, FR65 CORRODED. REPAIRED BAGGAGE DOOR CUTOUT "Z" FRAME AT STGR 16L, FR65. CORROSION FOUND TO BE LEVEL 1.

Part: SEAL — TORN (EMERGENCY EXIT) · airframe 34,959 hrs · 22,467 cycles

R/H OVER WING EMERGENCY EXIT SEAL IS TORN AT FORWARD AND AFT SIDES. REMOVED AND REPLACED SEALS ON THE RIGHT OVER WING EMERGENCY EXIT.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 34,959 hrs · 22,467 cycles

FLOOR PANEL 252AF HAS MULTIPLE AREAS OF COMPOSITE DAMAGE AND REQUIRES ETD FOR REPAIR. FABRICATED, LOCATED AND INSTALLED REPAIR DOUBLER FROM MATERIAL.

Part: SEAT TRACK — CORRODED (FRAMES 47-50) · airframe 34,959 hrs · 22,467 cycles

CORROSION ON LH OTBD SEAT TRACK SUPPORT OVER WING BOX FR47-50 OTBD SIDE. REMOVED AND REPLACED LH OTBD SEAT TRACK SUPPORT OVER WING BOX FR47-50 OTBD SIDE.

Part: BEARING — CORRODED (NLG) · airframe 34,959 hrs · 22,467 cycles

NLG L/H AND R/H LOWER HALF BEARING CAPS HAVE CORROSION. REMOVED AND REPLACED NLG L/H AND R/H LOWER HALF BEARING CAPS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,693 hrs · 22,212 cycles

OVERHEAD EMERGENCY LIGHT INOP IN EMERGENCY EXIT ROW RIGHT SIDE. R&R OVERHEAD EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: CONTACTOR — INTERMITTENT (BUSS) · airframe 34,144 hrs · 21,652 cycles

EMERGENCY LIGHTS CYCLED ON AND OFF FROM 10,000 FEET TO LANDING. PERFORMED TROUBLESHOOTING FOR THE EMERGENCY LIGHTS AND FOUND THE NR 1 ESSENTIAL BUSS CONTACTOR WAS INTERMITTENT. R & R THE CONTACTOR. OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 33,861 hrs · 21,365 cycles

DURING A SERVICE CHECK. MAIN PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE W717-0003-20. REPAIRED BY SPLICING WIRES. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,396 hrs · 20,903 cycles

EMERGENCY LIGHTS INOPERATIVE AND FOUND IN THE ARMED POSITION. R & R THE BATTERY PACKS IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,380 hrs · 20,883 cycles

EMERGENCY LIGHT OVER SEAT 18A INOP. R&R EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: TIRE — FAILED (MLG) · airframe 33,375 hrs · 20,876 cycles

#3 TIRE BLOWOUT DURING TAKEOFF ROTATION. R&R #3 AND #4 MAIN WHEEL ASSY IAW EMB 145 AMM 32-49-02. OPSAND LEAK CHECKS OF BRAKE SYSTEM SAT. ADDED EVENT INSPECTIONS AND DAMAGE. DAMAGE TO #2 ENGINE INLET GUIDE VANES DUE TO #3 TIRE BLOWOUT - FURTHER INSP REQUIRED. R&&R DAMAGED FAN BYPASS VANES IAW RR MM 72-25-10. OPS CHECK SAT IAW RR MM 71-00-00. LEADING EDGE OF RIGHT FLAP DAMAGED DUE TO #3 TIRE BLOWOUT. COMPLIED WITH STS EA 25-2017-140. ACCEPTABLE FOR ONE NON REV FERR FLIGHT FROM ROC TO ALB. FLIGHT TO BE CONDUCTED AT A SUITABLE REDUCED SPEED AT THE CAPTAINS DISCRETION. RIGHT INBD FLAP REQUIRES PERMANENT REPAIR. LANDING GEAR TREAD FAILURE INSPECTION. COMPLIED WITH THREAD FAILURE INSPECTIONS IAW EMB 145 AMM 05-50-15. ALL DISCREPANCIES NOTED.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 33,128 hrs · 20,637 cycles

EMERGENCY LIGHT AT OVERHEAD EXIT ROW INOPERATIVE. FOUND THE CONNECTIONS LOOSE. SECURED THE CONNECTOR AND PERFORMED AN OPS TEST. OPS TESTED GOOD, NO DEFECTS NOTED.

Part: INVERTER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 33,074 hrs · 20,584 cycles

EMERGENCY EXIT SIGN AT ROW 18 INOPERATIVE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS, OPS CHECK GOOD. INSPECTED THE WIRE SPLICES TO EXIT SIGN AND REPLACED THE NR 4 INVERTER AND THE NR 4 BATTERY CHARGER. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 33,070 hrs · 20,578 cycles

FWD FACING CEILING EMERGENCY EXIT SIGN INOPERATIVE. INSPECTED THE EMERGENCY LIGHT AND FOUND A SPLICED WIRE BROKEN OFF AND MISSING ATTACHMENT HARDWARE. REPAIRED THE WIRE AND OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (FWD CABIN) · airframe 33,068 hrs · 20,576 cycles

FWD EMERGENCY LIGHT INOPERATIVE. PERFORMED ADJUSTMENT AND TEST. OPS CHECKED GOOD, NO OTHER DEFECTS NOTED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,064 hrs · 20,571 cycles

CENTER AISLE CEILING EMERGENCY LIGHT FWD FACING INOPERATIVE. R & R THE NR 3 EMERGENCY LIGHT POWER SUPPLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,059 hrs · 20,565 cycles

EMERGENCY EXIT SIGN ROW 18 WILL NOT ILLUMINATE. R & R EMERGENCY EXIT SIGN AND SPLICED WIRES TO CONNECTOR.

Part: BULB — UNSECURE (EMERGENCY LIGHT) · airframe 33,014 hrs · 20,522 cycles

MID CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. SECURED THE BULB, OPS CHECKED SAT.

Part: LIGHT — UNKNOWN (CABIN) · airframe 32,996 hrs · 20,504 cycles

CABIN EMERGENCY LIGHT IN MID CABIN WILL NOT TEST, CENTER AISLE. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM. OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,996 hrs · 20,504 cycles

EMERGENCY LIGHTING SYSTEM REQUIRES OPERATIONAL CHECK. . FOUND AFT CENTER AISLE EMERGENCY LIGHT INOPERATIVE. R & R THE NR 4 BATTERY PACK, OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 32,980 hrs · 20,489 cycles

BACKSIDE OF EMERGENCY EXIT LIGHT NOT ILLUMINATING. FOUND THE CONNECTOR LOOSE. SECURED THE CONNECTOR.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,963 hrs · 20,476 cycles

EMERGENCY LIGHT BASE OF GALLEY WILL NOT ILLUMINATE. R & R THE INVERTER.

Part: LIGHT — INOPERATIVE (ROW 18) · airframe 32,953 hrs · 20,466 cycles

EMERGENCY LIGHTS ROW 18 INOPERATIVE. PERFORMED ADJUSTMENT. OPERATIONAL TEST SAT.

Part: LIGHT — UNKNOWN (CABIN) · airframe 32,851 hrs · 20,381 cycles

EMERGENCY CEILING LIGHT AT MID CABIN IS INOPERATIVE ON AFT SIDE. OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 32,832 hrs · 20,362 cycles

EMER EXIT ROW 18 LIGHT INOPERATIVE. FOUND A LOOSE CONNECTION TO LIGHT ASSY . SECURED THE WIRES. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 32,796 hrs · 20,329 cycles

OVERHEAD EMERGENCY AFT PORTION WILL NOT ILLUMINATE. FOUND CONNECTOR DIRTY. CLEANED AND RESEATED. OPS CHECKED SAT

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,763 hrs · 20,295 cycles

SERVICE DOOR THRESHOLD EXIT LIGHT INOPERATIVE. PERFORMED ADJUSTMENT AND TEST WITH NO FAULTS NOTED.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 32,720 hrs · 20,262 cycles

CABIN RED EXIT SIGN INOPERATIVE. R & R THE INVERTER. OPS CHECKED SATISFACTORY.

Part: SWITCH — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 32,663 hrs · 20,213 cycles

EMERGENCY LIGHT BY GALLEY DOOR INOPERATIVE. RESET EMERGENCY LIGHT SWITCH, OPS CHECKED GOOD.

Part: SIGN — UNKNOWN (ROW 18) · airframe 32,569 hrs · 20,124 cycles

EMERGENCY EXIT SIGN, ROW 18 OVERHEAD FWD SIDE, INOPERATIVE. PERFORMED AN OPS TEST, OPS TESTED GOOD. NO DEFECTS NOTED.

Part: INVERTER — FAILED (EMERGENCY LIGHT) · airframe 32,556 hrs · 20,110 cycles

FWD EMERGENCY LIGHT NOT ILLUMINATING. R & R THE NR 1 INVERTER ASSY OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,461 hrs · 20,026 cycles

EMERGENCY LIGHTS CENTER CEILING ABOVE GALLEY & ROW 18. R & R THE NR 2 EMERGENCY BATTERY PACK, REMOVED AND RESEATED CONNECTOR PLUG ON NR 4 BATTERY PACK. OPS CHECKED SAT, NO DEFECTS NOTED.

Part: ACM — FAILED (NR 2) · airframe 32,298 hrs · 19,886 cycles

CREW REPORTED A NR 2 PACK OVERLOAD MESSAGE WITH A BURNING ODOR. LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE NR 2 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 32,276 hrs · 19,869 cycles

CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE, APU, AND PACK CHECKS WITH NO DEFECTS NOTED, CABIN INSPECTION REVEALED INOPERATIVE SIDEWALL LIGHTS AT SEATS 5A & 20A. MAINTENANCE DISCONNECTED THE AFFECTED BALLASTS. MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLASTS, OPS TESTED WITH NO DIFECTES NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 32,276 hrs · 19,869 cycles

CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE, APU, AND PACK CHECKS WITH NO DEFECTS NOTED, CABIN INSPECTION REVEALED INOPERATIVE SIDEWALL LIGHTS AT SEATS 5A & 20A. MAINTENANCE DISCONNECTED THE AFFECTED BALLASTS. REMOVED AND REPLACED THE BALLASTS, OPS TESTED WITH NO DEFECTS NOTED. APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 32,276 hrs · 19,869 cycles

CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE, APU, AND PACK CHECKS WITH NO DEFECTS NOTED, CABIN INSPECTION REVEALED INOPERATIVE SIDEWALL LIGHTS AT SEATS 5A & 20A. MAINTENANCE DISCONNECTED THE AFFECTED BALLASTS. REMOVED AND REPLACED THE LIGHT BALLASTS, OPS TESTED WITH NO DIFECTES NOTED, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,276 hrs · 19,869 cycles

CREW REPORTED SMOKE IN THE CABIN. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE, APU, AND PACK CHECKS WITH NO DEFECTS NOTED, CABIN INSPECTION REVEALED INOPERATIVE SIDEWALL LIGHTS AT SEATS 5A & 20A. MAINTENANCE DISCONNECTED THE AFFECTED BALLASTS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BALLASTS AT SEATS 5A & 20A, OPS TESTED WITH NO DIFECTES NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 30,962 hrs · 18,894 cycles

DURING C-CK. BAGGAGE DOOR CUTOUT LOWER BEAM HAS CORROSION FRAME 65-68. R & R CARGO DOOR LOWER CUTOUT IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SEDRVICE.

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 30,962 hrs · 18,894 cycles

DURING C-CHECK THE LT ENGINE FORWARD LOWER MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01201. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 30,962 hrs · 18,894 cycles

DURING C-CHECK THE RT ENGINE FORWARD LOWER MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01201. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FUSE — BLOWN (EMERGENCY LIGHT) · airframe 30,212 hrs · 18,357 cycles

EMERGENCY LIGHTS ABOVE THE EXIT ROW WERE REPORTED INOPERATIVE. MAINTENANCE R & R THE FUSE IN THE NR 4 BATTERY POWER SUPPLY WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 28,268 hrs · 17,015 cycles

DURING MAINTENANCE INSPECTION, THE FWD EXIT LOCATOR OVERWING & AISLE LIGHT 3 EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT BATTERY CHARGER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,510 hrs · 16,528 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE PORT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE R & R THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — UNKNOWN (CABIN) · airframe 25,664 hrs · 15,327 cycles

CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT THE RT EMERGENCY EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE ACFT, OPERATIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 25,627 hrs · 15,308 cycles

DURING MX INSPECTION THE RT LOWER EMERGENCY EXIT SIGN DID NOT ILLUMINATE. MX SECURED LOOSE CONNECTOR ON EXIT SIGN WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 18,762 hrs · 10,716 cycles

MCI - FLIGHT 6049, THE CREW REPORTED THE MAIN PITCH TRIM TO BE INOPERATIVE. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT (HSCU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFTW AS APPROVED FOR RETURN TO SERVICE.

Part: ACM — INOPERATIVE (ZONE 100) · airframe 17,804 hrs · 9,997 cycles

FLIGHT 5869 THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NR 1 ACM ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,277 hrs · 9,577 cycles

FLIGHT 2191 - EWR - FLIGHT CREW REPORTED UPON APU START, FUEL SMELL IN CABIN. EWR MX PERFORMED OPERATIONAL CHECK AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CHAFED (FUEL TANK) · airframe 14,477 hrs · 8,009 cycles

TYS - BOTTOM CENTER OF VENTRAL TANK SKIN SHOWS EVIDENCE OF RUBBING FROM FAIRING 197BB. REPAIRED VENTRAL TANK LWR FWD SKIN BY INSTALLING A DOUBLER IAW EC2810-01057.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,330 hrs · 7,932 cycles

DURING ROUTINE MAINTENANCE THE OVERHEAD EXIT SIGNS AT THE OVERWING ESCAPE EXITS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,785 hrs · 7,643 cycles

FLIGHT 2807 - EWR - FLIGHT CREW REPORTED WINDOW EMERGENCY EXIT SIGN INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY EXIT SIGN LAMP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 13,380 hrs · 7,435 cycles

TYS A/C WAS FOUND TO HAVE THE LT EMERGENCY EXIT MARKER TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD AND WAS RELEASED.

Part: ENGINE — LEAKING (NR 2) · airframe 11,506 hrs · 6,450 cycles

IAH - FLIGHT 2411 - THE CREW REPORTED SMOKE IN THE CABIN AND LAV DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEALANT — SEPARATED (WINDSHIELD) · airframe 11,093 hrs · 6,230 cycles

IAH - FLIGHT 2079, THE CREW REPORTED THE BLACK SEALER ON THE CAPT SIDE WINDOW PEELED OFF IN FLIGHT AND WENT THROUGH THE NUMBER ONE ENGINE CAUSING A BURNING SMELL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED THE EXCESS SEALANT FROM THE CAPTAINS SIDE WINDOW, INSPECTED THE NUMBER ONE ENGINE WITH NO EVIDENCE OF INGESTION OF SEALANT NOTED, OPERATIONALLY CHECKED THE NUMBER ONE ENGINE WITH NO DEFECTS NOTED, REPAIRED THE CAPTAINS HUMPSEAL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — MALFUNCTIONED (LAVATORY) · airframe 11,033 hrs · 6,198 cycles

FLIGHT 2072 RIC-IAH - THE CREW REPORTED A MOMENTARY LAVATORY SMOKE WARNING DURING CRUISE. NO SMOKE CONDITIONS WERE NOTED AT THAT POINT AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED FUNCTIONAL TESTS OF THE LAVATORY SMOKE WARNING SYSTEM AND COULD NOT FIND AND COULD NOT DUPLICATE THE WARNING.

Part: VALVE — FAULTY (NR 1) · airframe 11,012 hrs · 6,183 cycles

CLE FLIGHT NR 2986 THE CREW REPORTED A BLEED 1 OVER TEMP WARNING DURING CLIMB IN ICING CONDITIONS. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 FAN AIR VALVE. OPS CHECKS WERE GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (SMOKE WARNING) · airframe 10,612 hrs · 5,964 cycles

FLIGHT 2761 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING FLIGHT. EWR MX PERFORMED OPERATIONAL CHECK OF LAVATORY SMOKE INDICATION SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 10,564 hrs · 5,935 cycles

IAW FLIGHT 2703 DURING CRUISE THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS. THE ACFT RETURNED TO IAW WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT WITH NO EVIDENCE OF SMOKE FOUND, R&R THE LAV SMOKE DETECTOR. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — INOPERATIVE (TIRE TEMP)

FLIGHT CREW ABORTED TAKEOFF AT 30-40 KNOTS FOR BRAKE OVERHEAT EICAS MSG. MX PERSONNEL FROM LAX WAS ON SITE AND THEY REMOVED AND REPLACED NR 3 RT IB BRAKE TEMP SENSOR. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (K)

Part: BLEED AIR SYS — WARNING MESSAGE

FLT 7661 -ABQ- FLIGHT CREW REPORTED BLEED 1/2 OVERTEMP. SYSTEM WAS RESET SUCCESSFULLY AS PER MX CTRL. CREW RAN BOTH ENG AND BLEED SYSTEM AND COULD NOT DUPLICATE. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: DISPLAY — BURNED OUT (COCKPIT) · airframe 9,738 hrs · 5,392 cycles

FLT 7693 - ONT - FLIGHT CREW REPORTED EICAS SCREEN FAILED, EICAS DISPLAY CIRCUIT BREAKER POPPED AND LOTS OF SMOKE EMITTED FROM ABOVE EICAS UNIT, SWAPPED MFD W/EICAS PLACED FO'S MFD. MX REMOVED AND REPLACED EICAS DISPLAY UNIT OPERATIONALLY CHECK SATISFACTORY. AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,557 hrs · 5,257 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW EMB 145 XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: INLET — OBSTRUCTED (APU) · airframe 8,626 hrs · 4,677 cycles

FLIGHT 7735 - GEG TO LAX - FLIGHT CREW REPORTED DURING TAXI APU HIGH TEMP AND APU FIRE INDICATION ON EICAS. SPOKANE AIRWAY CONTRACT MECHANICS REMOVED ICE FROM APU INLET AND VERIFIED NORMAL OPERATION. A/C WAS RELEASE IN AIRWORTHY CONDITIONS TO RETURN FOR SERVICE.

Part: INLET — OBSTRUCTED (APU) · airframe 8,626 hrs · 4,677 cycles

FLIGHT 7735 - GEG TO LAX - FLIGHT CREW REPORTED DURING TAXI APU HIGH TEMP AND APU FIRE INDICATION ON EICAS. SPOKANE AIRWAY CONTRACT MECHANICS REMOVED ICE FROM APU INLET AND VERIFIED NORMAL OPERATION. A/C WAS RELEASE IN AIRWORTHY CONDITIONS TO RETURN FOR SERVICE.

Part: LIGHT — FAILED (CABIN) · airframe 4,632 hrs · 2,441 cycles

EWR - CREW REPORTED EMERGENCY LIGHT STRIP NOT OPERATING. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLOOR LIGHT STRIP IAW EMB145 33-50-00, OPS CHECKED GOOD.

Part: BATTERY — OVERTEMP (NR 1 MAIN) · airframe 1,842 hrs · 959 cycles

CLE - FLIGHT 2995, THE CREW REPORTED A BATTERY ONE OVERTEMP IN CRUISE. THE AIRCRAFT DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT, AND MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE MAIN BATTERY. OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.