N14168

Part: SKIN — DENTED (ZONE 100) · airframe 42,067 hrs · 29,886 cycles

FUSELAGE EXTERNAL SKIN, LH, AT FR 9, STR 17L. REPAIRED DENT IN FUSELAGE EXTERNAL SKIN, LH AT FR 9 STR 17L

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION 3 LOCATIONS STR 16 R FRAME 19 TO 20. PERFORMED BLEND OUT ON 3 LOCATIONS AT STR 16 R, FRAME 19 TO 20. AT SPOTS 1 & 2 NO CORROSION WAS PRESENT. AT SPOT 3 INSTALLED FABRICATED DOUBLER FOR FWD FLOOR SILL REPAIR.

Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE LH SILL AT FRAME 29. REMOVED AND INSTALLED NEW SILL ON THE LH AT FRAME 29

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE RH SILL FRAME 29-35. INSTALLED NEW RH FLOOR SILL AT FR 29-35

Part: GUSSET — CORRODED (ZONE 800) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON GUSSET AFT OF SERVICE DOOR AT FR 22. REMOVED CORROSION ON GUSSET AFT OF SERVICE DOOR AT FR 22 AND REPAIRED GUSSET BUY INSTALLED FABRICATED DOUBLER FOR AFT FLOOR SILL REPAIR BETWEEN FR 22 - 23

Part: THRUST REVERSER — DAMAGED (NR 2) · airframe 42,067 hrs · 29,886 cycles

NUMBER 2 ENGINE LOWER THRUST REVERSER IB LOWER CORNER HAS DAMAGED COMPOSITE. REPAIRED DAMAGE TO #2 ENGINE LOWER CORNER ON LOWER THRUST REVERSER REPAIRED

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION FOUND ON FLOOR BEAM CROSS SUPPORT STRUCTURE AT FR 24, BETWEEN CENTER OMEGA BEAMS. REMOVED AND REPLACED THE FLOOR BEAM CROSS SUPPORT STRUCTURE AT FR24 BETWEEN CENTER OMEGA BEAMS

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

TOILET WASTE VALVE SURROUND STRUCTURE HAS CORROSION. INSTALLED NEW DOUBLER ON TOILET WASTE VALVE SURROUND STRUCTURE

Part: DOOR FRAME — CORRODED (ZONE 200) · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE LH SILL FRAMES 48 THRU 51. INSTALLED NEW FROM STOCK THE LH SILL AT FR 48 THRU 51

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE RT SILL FRAME 48 TO 51. COMPLETELY INSTALLED NEW RT FLOOR SILL FR 48 TO 51

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE RT INBOARD SEAT TRACK AT STR 17R BETWEEN FRAMES 24-25. REMOVED OLD SEAT TRACK AND INSTALLED NEW SEAT TRACK FROM STOCK TO RH INBOARD SEAT TRACH AT STR 17R BETWEEN FRAMES 24-25

Part: RIVET — DAMAGED (ZONE 200) · airframe 42,067 hrs · 29,886 cycles

EXTERNAL SKIN MID SECTION, LT, FROM FR 2 TO FR 3, DAMAGED. INSTALLED NEW RIVET AND WASHER FOR DAMAGE B AT FR 2 - FR 3 STRG 15L AND INSTALLED NEW RIVET AND WASHER DAMAGE A AT FR 1 - FR 2 STRG 15L

Part: FLOOR SUPPORT — CORRODED (ZOEN 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE LH SILL AT FRAMES 57. REMOVED ORIGINAL LH SILL FROM FRAME 53 TO FRAME 59, INSTALLED NEW FROM STOCK

Part: GUSSET — CORRODED (ZONE 100) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION IN THREE LOCATIONS STR 21R AT FRAME 20. "REMOVED AND INSTALLED NEW FROM STOCK GUSSET ON RT STR 21 BETWEEN FS 19 AND FS 23"

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE LT GUSSET FRAMES 60-61. INSTALLED NEW GUSSET AT LH FR60-FR61

Part: SKIN — DENTED (ZONE 200) · airframe 42,067 hrs · 29,886 cycles

FUSELAGE EXTERNAL MID SKIN AT FR 8, LH, HAS DAMAGE. PERFORMED RECONTOUR TO DENTED AREA BTW FR 8 - 9, AT STGR 17L

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 42,067 hrs · 29,886 cycles

GOUGES ON THE CENTER FLOOR SEAT TRACK AT FRAME 57. REMOVED GAUGES IN THE CENTER FLOOR SEAT TRACK AT FRAME 57

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE LT FLOOR SUPPORT, FRAMES 59 AND 61. INSTALLED A NEW FLOOR SUPPORT AND SPLICE AT LT FR 59-61.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE RT SILL AT FRAME 57. REMOVED RH SILL FROM FRAME 53 TO FRAME 59, INSTALLED NEW FROM STOCK

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORROSION ON THE CENTERLINE GUSSET FRAMES 59-60. REMOVED AND REPLACED WITH NEW FROM STOCK CENTERLINE GUSSET FRAMES 59-60

Part: FRAME — CORRODED (ZOEN 100) · corrosion level 2 · airframe 42,067 hrs · 29,886 cycles

CORRODED FRAME 22 STR 17R. REMOVED AND INSTALLED NEW FROM STOCK GUSSET AT FRAME 22 STR 17R

Part: SKIN — DENTED (ZONE 100) · airframe 42,067 hrs · 29,886 cycles

FUSELAGE EXTERNAL SKIN AT FR 25, RH, STR 20R, HAS PROTRUSION. RECONTOURED PROTRUSION ON FUSELAGE EXTERNAL SKIN AT FR 25, RH, STR 20R

Part: ELEC CONNECTOR — INOPERATIVE (ZONE 200) · airframe 41,999 hrs · 29,818 cycles

LH FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. NO FIX. FOUND PIN ON HOUSING BURNT (NPIS). REMOVED AND REPLACED LH EXT EMERGENCY LIGHT ASSEMBLY. NO FIX. FOUND NO VOLTAGE ON CANNON PLUG. REMOVED AND REPALCED FUSE ON #1 EMERGENCY BATTERY POWER SUPPLY TRAY. OPS OKAY AT THIS TIME.

Part: INVERTER — FAULTED (ZONE 200) · airframe 41,649 hrs · 29,470 cycles

EMERGENCY LIGHT ON AFT GALLEY PARTITION INOP. T/S TO FAULTY INVERTER, R&R INVERTER. OP CHECK GOOD, OK FOR CONT SERVICE

Part: TRIM PANEL — UNSECURE (ZONE 800) · airframe 41,186 hrs · 29,022 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. FOUND LOOSE TRIM ON MCD, RESECURED TRIM. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 41,064 hrs · 28,901 cycles

AISLE FWD EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED AISLE FWD EMERGENCY CEILING LIGHT. OPS CHECK SAT.

Part: SEALANT — OVERSERVICED (ZONE 800) · airframe 40,514 hrs · 28,377 cycles

MCD REQUIRES FORCE FROM INSIDE AND OUTSIDE TO OPEN. FOUND EXCESSIVE SEALANT ON FWD TOP CORNER OF SEAL TRIMMED EXCESSIVE SEALANT. OPS CHECKED SAT FROM BOTH OUTSIDE AND INSIDE

Part: LIGHT — DETACHED (ZONE 200) · airframe 40,487 hrs · 28,349 cycles

FLOOR PROXIMITY LIGHT STRIP MISSING FROM ALONGSIDE SEAT 20C. REINSTALLED FLOOR PROXIMITY LIGHT STRIP.

Part: SEAL — DAMAGED (ZONE 800) · airframe 40,473 hrs · 28,336 cycles

MCD GETS STUCK WHEN OPENING. REPAIRED MAIN CABIN DOOR CUT OUT SEALS. OPS CHECK SAT

Part: GLOWSTRIP — MISSING (ZONE 200) · airframe 40,388 hrs · 28,252 cycles

EMERGENCY EXIT STRIP MISSING AT 8A. REPLACED MISSING AISLE ILLUMINATION STRIP.

Part: LIGHT — INOPERATIVE (ZONE 100) · airframe 40,305 hrs · 28,165 cycles

RH SIDE CENTER FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH WTF FAIRING EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 40,117 hrs · 27,987 cycles

RH FORWARD LOWER FAIRING EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD LOWER FAIRING EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT

Part: DOOR — LACK OF LUBE (MAIN CABIN) · airframe 39,607 hrs · 27,494 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN LUBED AND OPS CHECKED PAX DOOR; OPERATION GOOD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,001 hrs · 26,934 cycles

FOUND LH WING UPPER EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LH WING UPPER EXTERIOR EMERGENCY LIGHT. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 38,644 hrs · 26,587 cycles

MCD STUCK OPEN. FOUND MCD LINING CATCHING. RESECURED DOOR LINING. OPS CHECK SAT. NO DEFECTS NOTED

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,150 hrs · 25,238 cycles

LH OVER WING AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: NONE — NONE · corrosion level 2 · airframe 37,142 hrs · 25,227 cycles

FUSELAGE AFT LWR SKIN UNDER RAD ALT #2 ANTENNA HAS CORROSION. REPAIRED REAR FUSEALGE I AFT LWR SKIN UNDER RAD ALT #2 ANTENNA.

Part: NONE — NONE · corrosion level 2 · airframe 37,142 hrs · 25,227 cycles

AFT FUSELAGE SKIN HAS CORROSION WHERE RADIO ALTIMETER RECEIVER ANTENNA #2 IS LOCATED. REPAIRED SKIN AT RAR #2 ANTENNA LOCATION

Part: NONE — NONE · corrosion level 2 · airframe 37,142 hrs · 25,227 cycles

CORROSION IN SEVERAL LOCATIONS AS MARKED ON RH FLOOR BEAMS BETWEEN FRAME 20 AND FRAME 24 AT Y = +17. REMOVED PREVIOUS REPAIR ON SEAT TRACK RH FLOOR BEAM FRAME 20 AND INSTALLED NEW REPAIR DOUBLERS.

Part: NONE — NONE · corrosion level 2 · airframe 37,142 hrs · 25,227 cycles

CORROSION ON AISLE LH FLOOR OMEGA BEAM STARTING AT FR46, UNDER FLOOR PANEL 251FF. REPAIRED LH FLOOR OMEGA BEAM STARTING AT FR46 UNDER FLOOR PANEL 251FF.

Part: NONE — NONE · corrosion level 2 · airframe 37,142 hrs · 25,227 cycles

CORROSION ON LAV FLOOR OMEGA BEAM AT FR59 Y+0. REPAIRED LAV FLOOR OMEGA BEAM AT FR59-61 Y+0

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 35,209 hrs · 23,502 cycles

LH FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R LH FWD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: LIGHT — INTERMITTENT · airframe 34,869 hrs · 23,201 cycles

MCD HINGE FAIRING EMERGENCY LIGHT HOUSING INTERMITTENT GROUND. R & R MCD EMERGENCY LIGHT ASSEMBLY. OPERATIONS CHECK SATISFACTORY

Part: SKIN — CRACKED (VORTILON) · airframe 34,556 hrs · 22,892 cycles

SUSPECTED CRACK ON RT LEADING EDGE 3 AT OUTBOARD VORTILLON. CHECKED & CONFIRMED LEADING EDGE IS CRACKED. R&R LEADING EDGE. LEAK CHECK AND OPERATIONS CHECK SATISFACTORY.

Part: SEAT TRACK — MISINSTALLED (FRAMES 48-52) · airframe 34,128 hrs · 22,477 cycles

REPLACEMENT OF RH LATERAL SEAT TRACK SUPPORT AT FR48 TO FR52 REQUIRED DUE TO ADDITIONAL HOLES AND INCORRECT CONFIGURATION. ADDITIONAL HOLES AND MARKED ELONGATED HOLES MEASURING .215", .196", AND .221" FOUND TO BE ACCEPTABLE. THIS IS A PERMANENT AUTHORIZATION.

Part: BULKHEAD — DAMAGED (NOT REPORTED) · airframe 34,128 hrs · 22,477 cycles

REPORT AND REWORK REPAIR TO FWD PRESS BULKHEAD. REWORKED REPAIR TO FWD PRESS BULKHEAD.

Part: BEAM — CORRODED (THRESHOLD) · corrosion level 2 · airframe 34,128 hrs · 22,477 cycles

DURING ZONE 131/132 INSPECTION FOUND CORROSION UNDER SERVICE DOOR THRESHOLD PLATE STRUCTURE AROUND NUT PLATE HOLDERS. REMOVED AND REPLACED FWD SERVICE DOOR LOWER BEAM. CORROSION FOUND TO BE LEVEL 2.

Part: ANGLE — CORRODED (FRAME 68) · corrosion level 2 · airframe 34,128 hrs · 22,477 cycles

BAGGAGE DOOR CUT OUT AFT LATERAL L-SHAPE CORRODED AT LOWER END AND THRESHOLD. REPAIRED L-ANGLE SPLICE AT FR68. CORROSION FOUND TO BE LEVEL 2.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,128 hrs · 22,477 cycles

253CLC FWD EMERGENCY EXIT LIGHT INCORRECTLY ATTACHED AND CRACKED. REMOVED AND REPLACED EXIT SIGN ON 253CLC.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,817 hrs · 22,230 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: SIGN — UNSECURE (CABIN) · airframe 33,284 hrs · 21,723 cycles

OVERHEAD EMERGENCY EXIT SIGN HANGING AT EMERGENCY EXIT ROW. RESECURED EXIT LOCATION SIGN. NO DEFECTED NOTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,846 hrs · 20,774 cycles

RT FORWARD EXTERNAL AND CEILING PANEL EMERGENCY LIGHTS INOPERATIVE. R&R BATTERY 2 POWER SUPPLY. OPS CHECK SAT.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,193 hrs · 20,777 cycles

PASSENGER CABIN FWD CEILING EMERGENCY LIGHT INOPERATIVE REAR EMERGENCY EXIT. R&R EMERGENCY LIGHT INVERTER NR 6. OPS CHECK SAT.

Part: CONNECTOR — DEFECTIVE (EMERGENCY LIGHT) · airframe 32,091 hrs · 20,694 cycles

FWD OVERHEAD EMERGENCY LIGHT NEXT TO SEAT 18A IS INOPERATIVE. DISCONNECTED AND RECONNECTED PIN CONTACTS. OPS CHECK SAT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,761 hrs · 20,392 cycles

CEILING EMERGENCY EXIT ROW SIGN INOP. R&R EMERGENCY LIGHT BATTERY. OPS CHECK SAT.

Part: HANDLE — OUT OF POSITION (EMERGENCY EXIT) · airframe 31,733 hrs · 20,362 cycles

RT EMERGENCY EXIT DOOR HANDLE UPSIDE DOWN. REMOVED AND INSTALLED UPPER RECESS CUP ON RT EMERGENCY DOOR TO THE CORRECT POSITION. NO DEFECTS NOTED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,823 hrs · 19,615 cycles

DURING MX INSPECTION, THE OVERHEAD AISLE EMERGENCY SIGN WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE OVERHEAD SIGN, OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — MALFUNCTIONED (ENGINE OIL) · airframe 26,476 hrs · 16,518 cycles

CREW REPORTED ENGINE NR 1 HIGH OIL TEMP AND ENGINE NR 1 SHUTDOWN IN FLIGHT. MAINTENANCE TROUBLESHOT AND R & R ENGINE NR 1 OIL TEMP SENSOR WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 25,978 hrs · 16,170 cycles

THE CREW REPORTED CRUISING AT FL320 FELT A PRESSURE BUMP. NO EICAS WARNING BUT CABIN ALT BOX AMBER AND QUICKLY STARTED TO CLIMB. CLIMBED TO ABOUT 12000 FT. THE CREW RAN A RAPID CABIN DEPRESSURAZTION AND EMERGENCY DESCENT. DECLARED EMERGENCY AND DESCENDED TO 10,000FT. SHORTLY THERE AFTER, PRESSURIZATION STARTED WORKING. CABIN ALT WENT FROM 10,000 TO 2,000. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R & R CPAM, DIGITAIL CONTROLLER, AND ELECTO PNEUMATIC OUTFLOW VALVE. OPS CHECKS WERE GOOD.

Part: WIRE HARNESS — BURNED (CABIN LIGHT) · airframe 24,211 hrs · 14,940 cycles

LIGHT ASSY END BURNED AT SEAT 7A. REMOVED LAMP AND PLACED ON MEL.

Part: BUSHING — MIGRATED (SPEED BRAKE) · airframe 23,358 hrs · 14,380 cycles

DURING C-CHECK, LEFT SPEED BRAKE UPPER ACTUATOR ATTACHMENT INBD HAT BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR OF LT SPEED BRAKE IAW EC5740-01152, REV F, STEP 5.0 OF EC5750-01415, REV D. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FRAMES 9-10) · airframe 23,358 hrs · 14,380 cycles

DURING C-CHECK, SKIN DENT AT STRINGER 16L FRAMES 9-10. MAINTENANCE REPAIRED DENT IAW EC5330-02318, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-19) · corrosion level 2 · airframe 23,358 hrs · 14,380 cycles

DURING C-CHECK, CORROSION FOUND ON RT OMEGA BEAM FRAMES 18-19. REPAIRED IAW EC5320-01986. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 77) · airframe 23,358 hrs · 14,380 cycles

DURING C-CHECK, FOUND A SKIN CRACK AT FRAME 77, STRINGER 6L. REPAIRED SKIN IAW EC5330-02949. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 23,358 hrs · 14,380 cycles

DURING C-CHECK, SHEAR CLIP CRACKED AT FRAME 68, STRINGER 7L-9L. REPAIRED SHEAR TIE IAW EC5320-01985. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — CRACKED (SERVICE DOOR) · airframe 23,358 hrs · 14,380 cycles

DURING C-CHECK, 272DR CRACKED BETWEEN RIVETS AND AT RADIUS FOR SLIDE PIN RING. MAINTENANCE PERFORMED REPAIR ON 272DR IAW EC5240-01086. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 32,278 hrs · 24,727 cycles

DURING C-CHECK CARGO DOOR LOWER SILL CORRODED, FRAMES 65-68. MAINTENANCE R & R CARGO DOOR LOWER SILL AT FRAME 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,098 hrs · 13,552 cycles

EMERGENCY LIGHTS LOCATED ABOVE THE FWD F/A JUMPSEAT, COCKPIT STEP AND CEILING NEXT TO THE GALLEY WERE INOPERATIVE. MAINTENANCE R & R THE NR 1 BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — BROKEN (RT MLG) · airframe 21,758 hrs · 13,334 cycles

THE CREW REPORTED THAT THEY HEARD A LOUD SOUND ON GEAR EXTENSION, AND AFTER LANDING WITHOUT INCIDENT, FOUND THE ACTUATOR ASSY ON THE RML GEAR TO BE BROKEN. MAINTENANCE INSPECTED THE ACFT AND R & R THE RMLG LEG AND MANEUVERING ACTUATOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,139 hrs · 12,939 cycles

DURING MX INSPECTION THE LT OVERWING EMERGENCY EXIT UPPER INTERIOR EXIT SIGN WAS DISCOVERED INOPERATIVE. MX R & R NR 5 EMERGENCY EXIT LIGHT SYSTEM INVERTER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHECK VALVE — LEAKING (ZONE 600) · airframe 19,527 hrs · 11,905 cycles

THE CREW REPORTED A POSSIBLE FUEL LEAK FROM THE RT WING ON TAKEOFF. THE ACFT RETURNED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE OTBD CHECK VALVE (FLAPPER VALVE) ON THE RT WING, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 14,640 hrs · 8,703 cycles

CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING CRUISE, MESSAGE CLEARED AFTER 1 MIN. R & R NR 2 ENGINE WITH OPS AND LEAK CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 14,640 hrs · 8,703 cycles

FLIGHT 2398 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING CRUISE, MESSAGE CLEARED AFTER 1 MIN. EWR MX REMOVED AND REPLACED NR 2 ENGINE AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR FILED OPEN

Part: TEST PANEL — DEFECTIVE (SMOKE WARNING) · airframe 14,637 hrs · 8,701 cycles

FLIGHT 2224 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED SMOKE DETECTOR TEST PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANTENNA — DAMAGED (ELT) · airframe 13,474 hrs · 8,026 cycles

IAH - FLIGHT 2586 IAH-IND, THE CREW REPORTED AN EXCESSIVELY LOUD NOISE IN THE AFT CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE ELT ANTENNA, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (PITOT/STATIC SYS) · airframe 12,659 hrs · 7,362 cycles

THE CREW REPORTED A PITOT NR 1 HEAT FAIL IN CRUISE. THE AIRCRAFT DIVERTED INTO CID AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RE-SECURED THE CONNECTOR ON NR 1 PITOT TUBE. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INTERMITTENT (CABIN) · airframe 11,770 hrs · 6,666 cycles

FLIGHT 995 - RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND PAX DOOR EMERGENCY LIGHT INTERMITTENT. MX REMOVED AND REPLACED EXIT IDENTIFIER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,507 hrs · 6,491 cycles

TYS - DURING ROUTINE MX THE MAIN DOOR EMERGENCY LIGHT WAS FOUND INOP. THE MAIN DOOR EMERGENCY LIGHT WAS REMOVED AND REPLACED IAW EMB 145 AMM 33-50-06 AND OPS CHECKED GOOD. A/C WAS RELEASED TO SERVICE.

Part: FLAPPER VALVE — WORN (RT WING)

FLT 7671 - SLC - PAX NOTIFIED CREW OF FUEL LEAK RT WING AND CREW NOTICED 300LBS OF FUEL LOST. MX PERSONNEL REMOVED AND REPLACED RT FLAPPER VALVE. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (A)

Part: CONTROL UNIT — INOPERATIVE (STAB TRIM)

FLT 7665 - ONT - FLIGHT CREW REPORTED MAIN PITCH TRIM INOPERATIVE. MX PERSONNEL REMOVED AND REPLACED HORIZONTAL STAB CONTROL UNIT. OPERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (A)

Part: PRESSURE SWITCH — BLOWN (NR 1 PACK) · airframe 9,864 hrs · 5,392 cycles

FLT 7775 - SEA TO SEA - FLIGHT CREW REPORTED PACK 1 OVERLOAD - ICE DET FAIL. FLIGHT CREW RETURNED TO BLOCK WITHOUT INCIDENTS. MX PERSONNEL REMOVED AND REPLACED PRESSURE SWITCH OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 7,881 hrs · 4,207 cycles

IAH - DURING MAINTENANCE INSPECTION THE LT AND RT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,226 hrs · 3,849 cycles

IAH - FLT 2213, DURING POST FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE CABIN DOOR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT LIGHT BULB, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 6,990 hrs · 3,713 cycles

IAH - FLIGHT 2358, THE CREW REPORTED A STRONG ELECTRICAL ODOR IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE ENGINES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.