N31131

Part: BATTERY PACK — DISCONNECTED (ZONE 200) · airframe 49,028 hrs · 31,691 cycles

ALL OVERWING EMERGENCY LIGHTS INOPERATIVE. FOUND BPS #4 DISCONNECTED, RECONNECTED BPS #4. OPS CHECK SAT.

Part: BATTERY — DISLODGED (ZONE 200) · airframe 48,874 hrs · 31,549 cycles

LEFT EXTERNAL FWD EMERGENCY LIGHT INOPERATIVE. FOUND EMERGENCY BATTERY 1 HAS FALLEN OFF OF ASSEMBLY. REINSTALLED THAT EMERGENCY BATTERY. OPS CHECK SAT.

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 48,723 hrs · 31,401 cycles

EXIT MARKING SIGN AT LH EMERGENCY EXIT UPPER POSITION INOP R/R EXIT MARKING SIGN. OPS CHECK SAT.

Part: HANDLE — UNSECURE (ZONE 800) · airframe 48,437 hrs · 31,116 cycles

MCD UNABLE TO OPEN FROM INSIDE CABIN. RESECURED INTERNAL MCD HANDLE. OPS CHECK SAT AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 47,769 hrs · 30,498 cycles

ELECTRICAL BURNING SMELL IN CABIN DURING TAKE OFF. INSPECTION OKAY AT THIS TIME. CONDUCTED HIGH POWER RUN. NO SMELL NOTED DURING MULTIPLE CONFIGURATIONS OF BLEED AIR AND PACK SELECTIONS. NO OIL OVER SERVICING NOTED ON #1 ENGINE, #2 ENGINE OR APU. NO LEAKS NOTED ON PACK 1 OR PACK 2. INSPECTED CABIN LIGHTING SYSTEM. NO DEFECTS NOTED.

Part: INVERTER — INOPERATIVE (ZONE 200) · airframe 47,738 hrs · 30,466 cycles

LH AFT EXIT ROW EMERGENCY EXIT ILLUMINATED PLACARD INOPERATIVE. REMOVED AND REPLACED #4 INVERTER. OPS CHECK SAT.

Part: SEAL — LEAKING (UNKNOWN) · airframe 47,152 hrs · 29,921 cycles

ABOVE 15,000 FT MCD STARTED VERY LOUD WHISTLE NOISE THAT DIDN’T STOP UNTIL BELOW 10,000 FT. REMOVED AND REPLACED MAIN DOOR FRAME RUBBER SEAL. PRESSURIZED AIRCRAFT. NO LEAKS NOTED COMING FROM MCD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,151 hrs · 29,920 cycles

LOUD WHISTLING COMING FROM MCD ABOVE FL 180 UNTIL DESCENDED BELOW 10000 FT. PERFORMED PRESSURIZATION CHECK. FOUND MULTIPLE LEAKS & MARKED W/TAPE. RESEALED LEAKING AREA. PERFORMED MANUAL PRESSURIZATION PROCEDURE. NO FURTHER LEAKS FROM MCD NOTES AT THIS TIME.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 46,608 hrs · 29,451 cycles

HYD 2 LOW QTY ON EICAS. REMOVED #2 ENGINE DRIVEN HYD PUMP. REMOVED #2 ENGINE DRIVEN HYD PUMP MAGENTIC CARBON SEAL ASSEMBLY. INSTALLED #2 ENGINE DRIVEN HYD PUMP. INSTALLED #2 ENGINE DRIVEN HYD PUMP MAGNETIC CARBON SEAL. OPS AND LEAK CHECK SAT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,521 hrs · 29,377 cycles

LH OVERWING INTERNAL AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED #5 AC/DC INVERTER. OPS CHECK SAT

Part: NONE — INOPERATIVE · airframe 45,949 hrs · 28,883 cycles

EXIT MARKING SIGN ASSEMBLY AT SEAT 18A INOPERATIVE. REMOVED AND REPLACED EXIT MARKING SIGN ASSEMBLY AT SEAT 18A. OPS CHECK SAT.

Part: PROXIMITY SWITCH — FAILED · airframe 45,885 hrs · 28,831 cycles

LANDING GEAR AIR/GROUND SYSTEM FAILURE. EICAS MSG LG AIR/GND FAIL APPEARED AFTER TAKEOFF. LG WOULD NOT RETRACT. HANDLE WOULD NOT MOVE. REMOVED AND REPLACED NOSE GEAR "WOW" PROX SWITCH -PERFORMED OPS CHECK, OPS CHECK GOOD

Part: NONE — INOPERATIVE · airframe 45,475 hrs · 28,461 cycles

EMERGENCY EXIT LIGHT AT LEFT EMERGENCY HATCH INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT LEFT EMERGENCY HATCH. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE · airframe 45,433 hrs · 28,423 cycles

UPPER EMERGENCY LIGHT INOPERATIVE AT ROW 18A. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK SAT

Part: NOT REPORTED — NOT REPORTED · airframe 45,388 hrs · 28,384 cycles

LARGE INTERIOR EMERGENCY LIGHT ROW 18A LEFT SIDE INOPERATIVE. ZONE 251 LH CABIN ESCAPE HATCH. LH EXIT MARKING SIGN ASSEMBLY CONNECTORS FOUND TO BE LOOSE. OPS CHECK SAT. NO FURTHER DEFECTS NOTED AT THIS TIME

Part: NONE — NONE · airframe 44,925 hrs · 27,983 cycles

FOUND LH UPPER EMERGENCY EXIT LIGHT INOPERATIVE ON OVERWING HATCH SIDEWALL. REMOVED LIGHT. TROUBLESHOT LIGHT AND FOUND CONNECTORS TO LIGHT TO BE NOT PROPERLY SEATED, RESEATED CONNECTORS AND REINSTALLED LIGHT. OPS CHECK SAT

Part: LIGHT — NO TEST (ROW 18A) · airframe 44,871 hrs · 27,938 cycles

EMERGENCY EXIT LIGHT AT ROW 18A, LT OVER WING EMERGENCY EXIT FAILED OPERATIONAL CHECK.

Part: LIGHT — MISSING (SEAT 5A) · airframe 44,590 hrs · 27,666 cycles

PHOTO LUMINESCENT STRIP MISSING SEAT 5A. FOUND AND REPOSITIONED PHOTO ILLUM LIGHT STRIP AS NEEDED REF EMB 145XRMM 33-50-00 .

Part: SUPPORT — CORRODED (FRM 25 S15-16R) · airframe 44,463 hrs · 27,546 cycles

CF2 RH SILL #1 CORRODED. CF2 RH SIDE FRAME 25 UNDER SILL NO 1 CUT FOR REPAIR. CF2 RH SIDE FRAME 25, BTW STR 15R-16R T BAR REMOVED FOR ACCESS. CF2 RH SIDE FRAME 25 UNDER SILL NO 1 REPAIRED. CF2 RH SIDE FRAME 25, BTW STR 15R-16R T BAR REINSTALLEDD.

Part: FRAME — CRACKED (FRM 59 S14-15L) · airframe 44,463 hrs · 27,546 cycles

CF4 BTW STR 15L-14L, FR 59 CRACKED. FR 59 REMOVED FOR REPLACEMENT. LH AND RH FRAME SPLICE AND FLOOR SILL RH SIDE AFT OF FR 59 REMOVED FOR ACCESS. CF4 FR59 BTW STR 15L-14L REPLACED BY NEW ONE. LH AND RH FRAME SPLICE AND FLOOR SILL RH SIDE AFT OF FR 59 REINSTALLED. AT STR 20R-19R AND 21L-20L X2 PROFILES PROTECTING FROM CABLE TO CHAFFE FOUND CRACKED, X2 PROFILES REPLACED WITH NEW ONES.

Part: FRAME — CORRODED (FRM 65 S15-16L) · airframe 44,463 hrs · 27,546 cycles

AT RF1, FR65 BTW STR 15-16 LH CORROSION FOUND ON FRAME. AT RF1, FR65 BTW STR 15-16 LH CORROSION ON FRAME REMOVED AND FOUND OUT OF LIMITS. SPLICE FABRICATED. FR 65 CUT BTW STR 13L AND 15L, SPLICE CHANNEL TRIMMED AND FIT TO FRAME 65 SEGMENTS. FR 65 AND SPLICE DRILLED. FR65 BTW STR 13L-16L, FRAME REPAIRED WITH REPAIR SPLICE AT STR 14L-15L.

Part: WINDOW POST — CRACKED (COCKPIT LEFT) · airframe 44,463 hrs · 27,546 cycles

FF2 LH COCKPIT WINDSHIELD LATERAL POST TOP EXTERNAL SKIN ONE RIVET HOLE FOUND CRACKED. SKIN CUT OUT DONE. UPPER STIFFENER ABOVE PILOT WINDOW FOUND CRACKED. CRACK ON LH COCKPIT WINDSHIELD LATERAL POST EXTERNAL SKIN REPAIRED. UPPER STIFFNER ABOVE PILOT WINDOW REPLACED

Part: YOKE — CRACKED · airframe 44,463 hrs · 27,546 cycles

LH AND RH PYLON YOKES I AND II UPPER FLANGE HOLES (X1 EACH SIDES) FOUND WITH CRACK AFTER NDI INSP. LH AND RH PYLON YOKES UPPER FLANGE HOLES (2X) OPENED AT FIRST REWORK DIAMETER (0.3281). AFTER NDT INSPECTION, DAMAGE IS STILL PRESENT AT LH AND RH PYLON YOKES UPPER FLANGE HOLES. AREA REWORKED AT SECOND PERMISSIBLE DIAMETER (0.420). BUSHINGS LOCALLY FABRICATED. 2 BUSHINGS FLUSH-PYLON. REPAIR BUSHINGS (4X) INSTALLED.

Part: FLOOR SUPPORT — CORRODED (FRMS 45-53) · airframe 44,463 hrs · 27,546 cycles

CF3, LH OMEGA BEAM LOWER FLANGE CORRODED FROM FR 45-46 TO 52-53. LH OMEGA BEAM LOWER FLANGE FROM FR 45-46 TO 52-53 IS OUT OF LIMIT. LH OMEGA BEAM FR 45-46 TO 52-53 REMOVED FOR REPLACEMENT. LH OMEGA BEAM CROSS BEAM O/B FR49 AND CROSS BEAM MIDDLE FR49-50 REMOVED FOR ACCESS. AT CF3 OMEGA BEAM FR45-46 TO 52-53 LH REPLACED . AT CF3 LH OMEGA BEAM CROSS BEAM O/B FR 49 AND CROSS BEAM MIDDLE FR 49-50 REINSTALLED

Part: FLOOR SUPPORT — CORRODED (FRMS 21-23) · airframe 44,463 hrs · 27,546 cycles

CF1 BTW FR 21-23, LH BEAM FLOOR SUPPORT LIP CORRODED. CF1 BTW FR 21-23, LH BEAM FOUND CRACKED AFTER INVESTIGATION. CF1 BTW FR 21-23, LH BEAM REPLACED.

Part: SKIN — DENTED (RUDDER) · airframe 44,463 hrs · 27,546 cycles

RUDDER II, LH SKIN DENTED AT RIB 615, LOWER SPAR CAP. RUDDER II, RIB PN 120-20723-001 HAVE DEFORMATION DUE TO A DENT. RIB REMOVED FOR REPLACEMENT. RUDDER II, LH SKIN AT RIB 615, LAY OUT FOR PATCH DOUBLER CUT OUT. RUDDER II, LH SKIN AT RIB 615, LOWER SPAR CAP REPAIRED WITH REPAIR DOUBLER. RUDDER II, LT RIB REPLACED. DATAPLATE REINSTALLED ON NEW RIB ON RUDDER.

Part: DOUBLER — DENTED (FRMS 22-23) · airframe 44,463 hrs · 27,546 cycles

AFTER DENT VISUAL INSPECTION, TOOL MARK AND RIVETS NOT PROPERLY INSTALLED ON PREVIOUS REPAIR DOUBLER AT FR 22-23, BTW STR 10R-12R. ON EXTERNAL SKIN AT FR 22-23, BTW STR 10R-12R LAYOUT COMPLETED FOR DOUBLER REPAIR. REPAIR DOUBLER AT FR 22-23, BTW 10R-12R. REPAIR DOUBLER AT FR 22-23, BTW STR 10R-12R REPLACED.

Part: SKIN — CRACKED (FRM 75 S2R) · airframe 44,463 hrs · 27,546 cycles

RF1 RH EXT FUSE SKIN AT FRAME 75 ONE RIVET HOLE CRACKED JUST BELOW STR 2R. RF1 EXT FUSE SKIN AT FR 75 SKIN STRIPPED. RIVETS REMOVED AND SKIN + ANGLE CUTOUT CARRIED OUT. RF1 EXT FUSE SKIN AT FR 75 REPAIRED. NR # 53-2238

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 44,460 hrs · 27,543 cycles

REPAIR DOUBLER ON CF1 BETWEEN FRAMES 20-22, STR 10-12L. DOUBLER ON CTR FUS-1, BETWEEN FR 20-22 AND STR 10L-12L REPAIRED.

Part: SKIN — DENTED (FUSELAGE FWD) · airframe 44,460 hrs · 27,543 cycles

FWD FUSELAGE I, MULTIPLE DENT FOUND BETWEEN FR 6-9, AND BETWEEN STR 13L-17L. FWD FUS-I MULTIPLE DENTS BETWEEN FR 6-9 AND BETWEEN 13L-17L. 7 DEBTS ARE ACCEPTABLE. CHAFING REPAIRED.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 44,460 hrs · 27,543 cycles

REPAIR DOUBLER ON CF1 BETWEEN FRAMES 20-21 AND STR 14-16L. DOUBLER ON CTR FUS-1, BETWEEN FR 20-21 AND STR 14L-16L REPAIRED.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 44,460 hrs · 27,543 cycles

DOUBLER ON RT FWD FUSELAGE 1, BETWEEN FRA 2 & 3 AT STR 17R. REPAIR DOUBLER ON RT FWD FUSELAGE I, BETWEEN FR 2-3 AT STR 17R.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,460 hrs · 27,543 cycles

REAR FUSELAGE II, MULTIPLE DAMAGES FOUND LT LATERAL SKIN PANEL BETWEEN FR 77-81 AND BETWEEN STR 11L-14L. REAR FUSELAGE II, MULTIPLE DAMAGES FOUND LT LATERAL SKIN PANEL BETWEEN FR 77-81 AND BETWEEN STR 11L-14L REPAIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,460 hrs · 27,543 cycles

REAR FUSELAGE I, LT LATERAL SKIN PANEL DAMAGED AFT OF FR 74 AND BETWEEN STR 11L-12L. REAR FUSE I, LT LATERAL SKIN PANEL DAMAGE AFT FR 74 AND BETWEEN STR 11L-12L REPAIRED.

Part: SWITCH — MALFUNCTIONED (CARGO DOOR) · airframe 42,030 hrs · 25,687 cycles

BAGGAGE DOOR OPEN ON EICAS AFTER TAKE OFF. PRESSURIZED A/C. DEFERED CARGO DOOR OPEN INDICATION ON DMI # 70052597. MORE INFORMATION PROVIDED ONCE AVAILABLE. SUPPEMENTAL INFORMATION. ADJUSTED FWD BAGGAGE DOOR MICROSWITCH TO CLEAR DMI. OPS CHECK GOOD.

Part: SWITCH — FAULTY (CARGO DOOR) · airframe 42,008 hrs · 25,668 cycles

BAGGAGE DOOR OPEN IND IN FLIGHT. A/C WASN'T LOSING PRESSURIZATION DURING FLIGHT. AIRCREW PERFORMED QRH AND RETURNED TO GATE IN ORD. DEFERED DOOR INDICATION ON DMI 70052418. R/R AFT DOOR MICROSWITCH. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

FLOOR SUPPORT HAS CORROSION BETWEEN RT FLOOR SILL & RT OMEGA BEAM AT FR 61. BLENDED CORROSION ON PROFILE T RT FLOOR SUPPORT, WAS FOUND TO BE OUT OF LIMITS. MATERIAL REMOVED .026, REMOVED PROFILE T. INSTALLED PROFILE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 61-65) · airframe 42,005 hrs · 25,665 cycles

L/H FLOOR SILL FR 61-65 HAS CORROSION AROUND NUTPLATES- FLOOR SILL FOUND TO BE OUT OF LIMITS. STARTED REMOVING FLOOR SILL. REMOVED THE CARBON RING LOWER TO FOM. REMOVED FLOOR SILL, PROCURED NEW FLOOR SILL. REQUIRE LOCATING HOLES AND INSTALLATION. INSTALLED FLOOR SILL, REQUIRE COMPOSITE RING BOTTOM PART TO BE INSTALLED. INSTALLED BOTTOM CARBON FIBER RING AT FR 61.

Part: SUPPORT FITTING — CRACKED (RT AILERON) · airframe 42,005 hrs · 25,665 cycles

RH AILERON L/E PCA ROD END SUPPORT FITTING CRACKED- REMOVED RH AILERON PCA FITTING. INSTALLED RH AILERON PCA FITTING.

Part: FLOOR SUPPORT — CRACKED (FRAME 24) · airframe 42,005 hrs · 25,665 cycles

L/H FLOOR SILL SPLICE PLATE CRACKED AT FR 24- INSTALLED L/H FLOOR SPLICE AT FR 24.

Part: FLOOR SUPPORT — CORRODED (FRAME 46) · airframe 42,005 hrs · 25,665 cycles

RH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FR 46 RH- REMOVED FLOOR SILL. INSTALLED FLOOR SILL.

Part: RIB — DAMAGED (RUDDER) · airframe 42,005 hrs · 25,665 cycles

RUDDER #2 2ND NOSE RIB FROM BOTTOM DAMAGED AT L/H NUTPLATE- REMOVED DAMAGED RIB ON #2 RUDDER NOSE BOTTOM AT L/H AND STARTED LOCATING FASTNER HOLES. DRILLED UP AND INSTALLED NEW RIB ON RUDDER, PAINT REQUIRED. REMOVED & REPLACED #2 RUDDER 2ND LWR NOSE RIB, NOTE: SEE DMI CONTROL # 70041227 FOR TOP COAT.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

LT FLOOR SILL HAS CORROSION BETWEEN FR 54 & 55. REMVED & REPLACED LT FLOOR SILL AT FR 52-56.

Part: DRAIN VALVE — CORRODED · airframe 42,005 hrs · 25,665 cycles

EXTERNAL WASTE DRAIN VALVE HDW HAS SIGNS OF CORROSION- R&R EXTERNAL WASTE DRAIN VALVE HDW.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

LT FLOOR SILL HAS CORROSION BETWEEN FR 50 THRU 51. REMOVED LT FLOOR SILL, DRILLED UP, SEALED IN PLACE, STARTED INSTALLING FASTENERS. INSTALLED HI LOCS AND NUTPLATES.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 42,005 hrs · 25,665 cycles

FLOOR SUPPORT BETWEEN CENTER & LH OMEGA BEAM HAS CORROSION @ FRAME 20- R&R FLOOR SUPPORT BETWEEN CENTER AND LH OMEGA BEAM, NUTPLATE HOLES NEED PICKED UP. INSTALLED NUTPLATES ON NEW FLOOR SUPPORT. R&R FLOOR SUPPORT BETWEEN CENTER AND L/H OMEGA BEAM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

RT FLOOR SILL BETWEEN FR 50 & 51 HAVE CORROSION ON UPPER SURFACE. REMOVED CORRODED FLOOR SILL BETWEEN FRAMES 48-53 AND INSTALLED NEW FLOOR SILL. HI LOKS NEED TO BE INSTALLED. INSTALLED NEW FLOOR SILL AT FRAME 48-53 INSTALLED HI LOK FASTENERS.

Part: FLOOR SUPPORT — CORRODED (FRAME 22) · airframe 42,005 hrs · 25,665 cycles

CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AT FR 22 AROUND NUTPLATE HOLE- REMOVED CORRODED GUSSET AND REPLACED WITH NEW GUSSET SUPPORT AT FR 22 CENTER OMEGA BEAM.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-25) · airframe 42,005 hrs · 25,665 cycles

FLOOR SUPPORT BETWEEN LH & CENTER OMEGA BEAM HAVE CORROSION BETWEEN FRAME 24 & 25- R&R CROSS BEAM L/H BETWEEN FRAME 24 & 25.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

LT FLOOR SILL HAS CORROSION FROM FRAME 33 THRU 35 LT. REMOVED & REPLACED LT FLOOR SILL FROM FR 28-35.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 42,005 hrs · 25,665 cycles

LH FLOOR SILL HAS CORROSION AROUND FASTNER HOLE AT FRAME 61- LH FLOOR WAS FOUND TO BE OUT OF LIMITS. REMOVED DEFECTIVE LH FLOOR SILL. INSTALLED NEW L/H FLOOR SILL F/S 61.

Part: SUPPORT BRACKET — CRACKED (FRAME 46) · airframe 42,005 hrs · 25,665 cycles

FRAME 46 LOWER SUPPORT BRACKET IS CRACKED @ STR 15 BELOW RIGHT FLOOR SILL- REMOVED ALL FASTNERS. REMOVED & PICKED UP HOLES ON NEW BRACKET. INSTALLED RH LOWER SUPPORT BRACKET AT FR 46, FUEL TANK SEALANT NEEDS TO BE APPLIED. INSTALLED SEALANT 1440 B2 TO REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 37-40) · airframe 42,005 hrs · 25,665 cycles

LH FLOOR SILL HAS CORROSION ON UPPER SURFACE BETWEEN FRAME 37 THRU 40- REMOVED FL SILL. INSTALLED LH SILL.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 42,005 hrs · 25,665 cycles

RH OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AROUND NUTPLATE HOLE AT FRAME 59- UPPER DIGITAL SUPPORT FOUND TO BE OUT OF LIMITS. STARTED REMOVING UPPER DIGITAL. REMOVED UPPER DIGITAL SUPPORT. LOCATED, DRILLED NEW DIGITAL SUPPORT AND INSTALLED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

LT OMEGA BEAM I/B LOWER SPLICE ANGLE IS CRACKED BETWEEN FR 16 & 17. REMOVED & REPLACED SPLICE ANGLE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-23) · airframe 42,005 hrs · 25,665 cycles

LH FLOOR SILL HAS CORROSION FROM FRAME 19 THRU 23- R&R LH FLOOR SILL FROM FRAMES 19-23.

Part: FLOOR SUPPORT — CORRODED (FRAME 26) · airframe 42,005 hrs · 25,665 cycles

LH FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FRAME 26- REMOVED FLOOR SILL, LOCATED HOLES IN NEW FLOOR SILL AND INSTALLED EXCEPT FWD & AFT SILL SPLICE. SEE NRWO 22270-616 FOR FWD SPLICE. INSTALLED AFT FLOOR SILL SPLICE.

Part: SUPPORT BRACKET — CRACKED (FRAME 46) · airframe 42,005 hrs · 25,665 cycles

FRAME 46LH LOWER SUPPORT BRACKET IS CRAQCKED AT STR 15 BELOW LEFT FLOOR SILL- REMOVED ALL FASTNERS. INSTALLED LH LOWER SUPPORT BRACKET AT FR 46 STR 15L, FUEL TANK SEALANT STILL NEEDS TO BE APPLIED. INSTALLED SEALANT TO REPAIR.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · airframe 42,005 hrs · 25,665 cycles

CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION ATOUND NUTPLATE HOLES FROM FR 59 THRU 61- CORROSION IN THIS AREA WENT THROUGH UPPER DIGITAL OMEGA BEAM, UNDER DIGITAL NEEDS TO BE INSPECTED AFTER REMOVALE OF DIGITAL. REMOVED DIGITAL SUPPORT, NO DAMAGE FOUND ON OMEGA BEAM. LOCATED, DRILLED 7 INSTALLED NEW DIGITAL SUPPORTS.

Part: FLOOR SUPPORT — CORRODED (FRAMES 33-35) · airframe 42,005 hrs · 25,665 cycles

RH FLOOR SILL HAS CORROSION FROM FRAME 33 THRU 35 RH- R&R RH FLOOR SILL AT FR 33 TO 35.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

RT FLOOR SILL HAS CORROSION BETWEEN FRAME 37 & 38. R&R RT FLOOR SILL BETWEEN FR 37 & 38.

Part: FLOOR SUPPORT — CORRODED (FRAMES 41-43) · airframe 42,005 hrs · 25,665 cycles

RH FLOOR SILL HAS CORROSION ON UPPER SURFACE FROM FRAME 41 THRU 43- REMOVED FLOOR SILL. INSTALLED FLOOR SILL.

Part: SEAT TRACK — CORRODED (FRAMES 23-32) · airframe 42,005 hrs · 25,665 cycles

CENTER OMEGA BEAM SHORT SEAT TRACKS HAVE CORROSION FROM FRAME 23 THRU 32- REMOVED CENTER OMEGA BEAM SHORT SEAT TRACKS FROM FR 23 THRU FR 32. BLENDED PAX SEAT TRACKS BY FR 24/25, FR 28/29 & FR 30/31/32, THEY ARE WITHIN LIMITS. REPLACED CENTER OMEGA BEAM SHORT SEAT TRACKS FR 23 & FR 26/27. REINSTALLED SHORT SEAT TRACK BY FRAMES 24/25, 28/29, 30/31/32.

Part: FLOOR SUPPORT — CORRODED (FRAMES 40-41) · airframe 42,005 hrs · 25,665 cycles

LH OMEGA BEAM UPPER SURFACE HAS CORROSION BETWEEN FR 40 & 41- REMOVED FASTENERS & BLENDED AREA OF CORROSION. ORIGINAL THICKNESS=.040 BEFORE BLEND. THICKNESS AFTER BLEND = .010. .030 MATERIAL LOSS= OUT OF LIMITS. REMOVED LH OMEGA BEAM UPPER GUSSET BETWEEN FR 37-FR 45. STARTED INSTALLING NEW UPPER GUSSET ON LH OMEGA BEAM FR 37- FR 45. COMPLETED INSTALL OF NEW GUSSET ON LH OMEGA BEAM FR 37-45.

Part: SKIN — GOUGED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

FUSELAGE SKIN LH SIDE HAS GOUGE INSIDE PYLON ACCESS PANEL 414DB- REMOVED EXISTING DOUBLER FROM FUSELAGE SKIN, REMOVED POUGE AND DAMAGE FROM SKIN, BEGAN FABRICATING DOUBLER. CONTINUED FABRICATING DOUBLER, MAPPING AND LOCATING HOLES, ALODINE AND PRIMED DOUBLER AND FILLER. COMPLETED REPAIR, ADDED FASTNERS AND FILLER. SEALED REPAIR.

Part: SHEAR TIE — CRACKED (FRAME 16) · airframe 42,005 hrs · 25,665 cycles

MAIN CABIN FRAME 16 SHEER CLIP IS CRACKED AT STR 15 RH- REMOVED SHEER CLIP. INSTALLED SHEER CLIP AT FR 16 STR 15R.

Part: SHEAR TIE — CRACKED (FRAME 15) · airframe 42,005 hrs · 25,665 cycles

MAIN CABIN FRAME 15 SHEER CLIP IS CRACKED AT STR 15 RH- REMOVED SHEER CLIP AT FR15 STR15R. DRILLED UP NEW CLIP, INSTALLED WET RIVETS THRU SKIN AND FUSELAGE, NEEDS 2 STRINGER RIVETS INSTALLED. INSTALLED 2 RIVETS THROUGH THE STRINGER FROM THE SHEER CLIP AT FR15.

Part: SKIN — GOUGED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

FUSELAGE SKIN HAS DEEP GOUGES INSIDE OF PYLON ACCESS PANEL 424DB- REMOVED THE #2 ENG BLEED VALVE IN THE R/H PYLON & THE BLEED DUCTS. FABRICATED DOUBLER & FILLER & REMOVED DAMAGE FROM FUSELAGE IN R/H PYLON ACCESS PANEL 424DB. INSTALLED REPAIR DOUBLER & FILLER IN R/H PYLON ACCESS PANEL 424DB. REINSTALLED THE #2 ENG BLEED VALVE & BLEED DUCTS IN THE PYLON.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

AFT CARGO FRAME 72 SHEER CLIP IS CRACKED AT STR 15L. REMOVED AFT CARGO FR 72 SHEAR CLIP AT STR 15L. INSTALLED SHEAR CLIP AT FRAME 72 STR 15L.

Part: DOOR — CRACKED (FWD ACCESSORY) · airframe 42,005 hrs · 25,665 cycles

FWD ACCESSORY DOOR 123BL IS CRACKED UNDER HINGE BRACKET- CUT OUT DAMAGE, FITTED, FABRICATED PARTS. CUT OUT 3 CRACKS, REPAIRED AREA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,005 hrs · 25,665 cycles

AFT CARGO FRAME 65 SHEAR CLIP IS CRACKED AT STGR 16L. REMOVED & REPLACED CRACKED SHEAR CLIP FS 65 STR 16L.

Part: DUCT — UNSECURE (NR 2 BLEED SYS) · airframe 38,258 hrs · 22,559 cycles

NR 2 BLEED LEAK DURING CLIMB OUT. R & R THE BLEED AIR DUCT AND BOTH CLAMPS FWD OF THE VALVE IN NR 2 PYLON IAW AMM 36-11-05. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,189 hrs · 20,190 cycles

DURING ROUTINE MAINTENANCE, THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE RT OVERWING EMERGENCY LIGHT ASSY. OPS CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,717 hrs · 19,862 cycles

DURING MX INSPECTION THE RT & LT OVERWING AND AFT AISLE EMERGENCY LIGHTS WERE INOPERATIVE. MX R & R THE NR 4 BATTERY CHARGER AND INVERTER WITH OPS CHECKS GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — NO TEST (EMERGENCY LIGHT) · airframe 34,313 hrs · 19,574 cycles

THE CREW REPORTED MIDDLE EMERGENCY LIGHT WAS NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE AFT AISLE EXIT LOCATION SIGN. OPS CHECKS WERE GOOD.

Part: O-RING — LEAKING (RELIEF VALVE) · airframe 32,078 hrs · 18,110 cycles

CREW REPORTED FUEL VENTING FROM RT WING DURINHG FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE O-RING ON FITTING FOR VENT RELIEF VALVE ON RT WING. OPS CHECKS WERE GOOD. NO LEAKS FOUND.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 29,939 hrs · 16,764 cycles

DURING C-CHECK. RT OMEGA BEAM HAS CORROSION AT FR 23. REPAIRED RT OMEGA BEAM IAW EC5320-01443. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 29,939 hrs · 16,764 cycles

DURING C-CHECKK, RT OMEGA BEAM HAS CORROSION BETWEEN FR 59-61. REPAIRED RT OMEGA BEAM IAW EC5310-01473. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (ZONE 100) · airframe 29,939 hrs · 16,764 cycles

DURING C-CHECK, FR 65 HAS CORROSION BETWEEN STR 16 - 17L. REPAIRED FR 65 IAW EC5310-01505. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · airframe 29,939 hrs · 16,764 cycles

DURING C-CHECK, INTERNAL SKIN CORRODED AT FR 16-17, STR 21L-21R. REPAIRED SKIN IAW EC5320-01829. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 200) · airframe 29,939 hrs · 16,764 cycles

DURING C-CHECK, BAGGAGE DOOR UPPER CUTOUT HAS CORROSION BETWEEN 65-66. REPAIRED BAGGAGE DOOR UPPER CUTOUT IAW EC5310-01718. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 29,530 hrs · 16,499 cycles

DURING C-CHECK, CORROSION WAS FOUND AT THE AFT SERVICE DOOR SILL AROUND THE SCREW HOLES. MX BLENDED OUT THE CORROSION AND REPAIRED THE AREA AND INSTALL FABRICATED PART IAW SRM 53-21-10 AND CPM 51-21-06.

Part: FLOOR SUPPORT — CORRODED (CENTER FUSELAGE) · airframe 29,530 hrs · 16,499 cycles

DURING C-CHECK INSPECTION, CORROSION WAS FOUND AT THE LT FLOOR SUPPORT AT FR 18 THRU FR 23. CORRROSION WAS BLENDED TO OUT OF LIMITS. R & R IAW SRM 51-40-02 AND SRM 51-21-01.

Part: CONTROL MODULE — INOPERATIVE (CABIN LIGHTS) · airframe 26,439 hrs · 14,509 cycles

DURING PREFLIGHT INSPECTION THE CREW REPORTED SMOKE IN THE CABIN ABOVE SEAT 1A. CONTRACT MX INSPECTED THE ACFT AND R & R THE CABIN LIGHT CONTROL MODULE, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,952 hrs · 14,181 cycles

DURING SCHEDULED MX INSPECTION, COCKPIT AND FORWARD LT OTBD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY CHARGER, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — CORRODED (SMOKE DETECTOR) · airframe 25,452 hrs · 13,811 cycles

DURING CRUISE, CREW RECEIVED DAU MISCOMPARE WITH BAGGAGE FIRE DETECTION WARNING MESSAGES. CREW ELECTED TO DISCHARGE CARGO COMPARTMENT FIRE BOTTLES IAW QRH AND DIVERTED, ACFT LANDED WITHOUT INCIDENT. MX REPLACED THE DAU COMPUTER AND FOUND THE CARGO COMPARTMENT SMOKE DETECTOR TO HAVE A CORRODED ELECTRICAL CONNECTOR. THE DETECTOR AND ITS ASSOCIATED CONNECTOR WERE REPLACED. OPS CHECKS WERE SATIFACTORY AND THE DISCREPANCIES WERE CLEARED.

Part: CONTROL UNIT — FAULTY (MLG) · airframe 25,101 hrs · 13,628 cycles

FLT NR 4163 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON SHORT FINAL. MX INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (LANDING GEAR) · airframe 24,399 hrs · 13,215 cycles

IAH - FLIGHT 2511, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESASAGE EICAS MESSAGE ON FINAL APPROACH DURING GEAR EXTENSION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE CLEANED THE CONNECTORS ON THE WEIGHT ON WHEELS PROXIMITY SENSORS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 24,391 hrs · 13,210 cycles

IND - FLIGHT 2298, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON APPROACH TO IND. THE AIRCRAFT WAS INSPECTED AND FERRIED TO IAH WHERE IT AGAIN LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FUNCTIONAL CHECKS OF THE AIR GROUND SYSTEM, WITH NO DEFECTS NOTED, AND THE AIRCRATF WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT BRACKET — CORRODED (AILERON) · corrosion level 2 · airframe 24,155 hrs · 13,077 cycles

LT LOWER SUPPORT BRACKET FOR AILERON DISCONNECT CORRODED AT SKIN. REMOVED AND REPLACED BRACKET IAW EMB 145XR SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,154 hrs · 13,076 cycles

CARGO CUTOUT THRESHOLD HAS AREAS OF CORROSION. REMOVED AND REPLACED DOOR SILL IAW EMB 145XR SRM 51-40-02.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 23,083 hrs · 12,207 cycles

OKC FLIGHT 6017 AC N31131 LG AIR/GND FAIL/MX FERRY TO SHV FOR REPAIRS/LP 2735979. MFY TO SHV FOR REPAIR. MAINTENANCE ADJUSTED RT MLG PROX TARGET. REMOVED AND REPLACED NLG PROX SWITCH IAW EMB-145 AMM 32-60-00 AND 32-61-01. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE.

Part: ANTENNA — INOPERATIVE (ILS) · airframe 19,712 hrs · 10,363 cycles

TUL - FLIGHT 2415, THE CREW REPORTED THAT ON APPROACH INTO MCI THE ILS SYSTEM WAS INOPERATIVE. THE AIRCRAFT DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE ILS ON MEL 34-32-00/1 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED BOTH VOR/ILS ANTENNAS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANTENNA — INOPERATIVE (ILS) · airframe 19,712 hrs · 10,363 cycles

TUL - FLIGHT 2415, THE CREW REPORTED THAT ON APPROACH INTO MCI THE ILS SYSTEM WAS INOPERATIVE. THE AIRCRAFT DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE ILS ON MEL 34-32-00/1 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED BOTH VOR/ILS ANTENNAS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,536 hrs · 10,402 cycles

IAH - FLIGHT 2238, THE CREW REPORTED RECEIVING TWO BRIEF EMERGENCY LIGHTS NOT ARMED MESSAGES DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, FUNCTIONALLY TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — MISALIGNED (CARGO DOOR) · airframe 18,588 hrs · 9,753 cycles

IAH - FLIGHT 2581, THE CREW REPORTED A BAGGAGE DOOR OPEN INDICATION DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT VERIFIED THE DOOR AS CLOSED AND PLACED THE INDICATION ON MEL. ON 08/12/09 MAINTENANCE ADJUSTED THE BAGGAGE DOOR MICRO SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (MLG) · airframe 17,133 hrs · 8,963 cycles

FLIGHT 2401 - EWR - FLIGHT CREW REPORTED "LG AIR/GND FAIL" MSG ON EICAS DURING POWER UP. EWR MX R&R RT SHOCK ABSORBER PROXIMITY SWITCH AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONDITIONER — INOPERATIVE (WING FUEL)

FLIGHT 2753 - EWR - FLIGHT CREW REPORTED LOSS OF FUEL QUANTITY INDICATION AND FUEL LOW LEVEL WARNING ON EICAS. CREW DECLARED EMERGENCY AND LANDED ACFT WITHOUT INCIDENT. EWR MAINTENANCE REMOVED AND REPLACED WING FUEL CONDITIONER UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: PROXIMITY SENSOR — INOPERATIVE (NLG) · airframe 15,254 hrs

DGO - FLIGHT 2036, DURING CLIMB OUT THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS, AND THE LANDING GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO DGO WEHRE IT LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO IAH WHERE MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SENSOR. OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: ELECTRONIC UNIT — INOPERATIVE (MLG)

DGO - FLIGHT 2036. DURING CLIMBOUT THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS, AND THE LANDING GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO DGO WHERE IT LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO IAH WHERE MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE LGEU. OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,078 hrs · 6,345 cycles

IAH - DURING MAINTENANCE INSPECTION THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DEFECTIVE (EMERGENCY LIGHT) · airframe 10,524 hrs · 5,538 cycles

RIC MX - DURING ROUTINE MAINTENANCE, MX FOUND AFT RIGHT WING AND AFT AISLE EMERGENCY LIGHTS INOP. AFTER TROUBLESHOOTING THE SYSTEM FOUND EMERGENCY BATTERY NR 4 NOT HOLDING CHARGE. MX REMOVED AND REPLACED EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 9,881 hrs · 5,190 cycles

FLIGHT 2496 - DURING TESTING THE CEILING PANEL EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT ASSEMBLY AND FOUND A LOOSE CONNECTOR. THE LIGHT ASSEMBLY CONNECTOR WAS RESECURED AND THE EMERGENCY LIGHTS OPERATIONALLY TESTED GOOD.

Part: SILL — CORRODED (FUSELAGE) · airframe 9,695 hrs · 5,085 cycles

TYS DURING A CURRENT 2C INSPECTION CORROSION WAS FOUND ON THE RIGHT FLOORBOARD SILL AT FR 41 THRU FR 44. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL, ALODINED AND PAINTED IAW EMB 145XR SRM 51-40-02; CPM 51-21-04,05. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE COMPLETION OF ALL WORK.

Part: BRACKET — GOUGED (RT AILERON) · airframe 9,695 hrs · 5,085 cycles

DURING A SCHEDULED INSPECTION THE RT PCA BRACKET ON THE AILERON IS GOUGED. MAINTENANCE REMOVED AND REPLACED THE PCA BRACKET IAW EC5750-01177.

Part: ENGINE — SMOKE (NR 2) · airframe 9,308 hrs · 4,870 cycles

IAH - FLIGHT 3214, THE CREW REPORTED A LAV SMOKE WARNING. THE AIRCRAFT RETURNED TO IAH 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: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 6,065 hrs · 3,189 cycles

DURING ROUTINE INSP FOUND EMERGENCY LIGHTS SYSTEM NR 1 TO BE FAULTY. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY PACK IAW EMB145XR AMM NR 33-50-04. OPS CHECKED GOOD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 4,822 hrs · 2,542 cycles

DURING C-CHECK THE FUSELAGE EXTERNALLY HAS 2 GOUGES BETWEEN FR 2 AND 3 STR 17 R. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EMB 145XR SRM 53-11-01 FIG 201 SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 4,822 hrs · 2,542 cycles

DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVE THE DAMAGED AREA AND PERFORMED A REPAIR IAW 145XR SRM 53-21-10 FIGURE 201 SHEET 2. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR — OUT OF ADJUST (MAIN PAX)

IAH - FLIGHT 2568, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT THE PASSENGER DOOR WAS EXTREMELY HARD TO OPEN AND CLOSE. MAINTENANCE ADJUSTED THE PASSENGER DOOR IN ACCORDANCE WITH EMB-145 AMM 52-18-06, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PUMP — LEAKING (NR 1 ENGINE)

THE CREW REPORTED A NR 1 HYDRAULIC LOW QUANTITY AND A ENGINE NR 1 HYDRAULIC PUMP FAIL MESSAGE ON THE EICAS AFTER TAKEOFF.THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE HYDRAULIC PUMP LEAKING BETWEEN THE PUMP HOUSING AND VALVE PLATE.THE PUMP WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: MODULE — FAULTY (CABIN)

IAH FLIGHT 2106 THE CREW REPORTED A BURNING ODOR FROM THE CABIN LIGHT CONTROL MODULE. MAINTENANCE REPLACED THE CABIN LIGHT CONTROL MODULE. OPERATIONAL CHECKS WERE GOOD.