N11137

Part: DOUBLER — DAMAGED (FRAMES 64-66) · airframe 43,520 hrs · 27,129 cycles

2 REPAIR DOUBLER ON LOWER REAR FUSE 1, BETWEEN FR 64-66 AND BETWEEN STR 19L-20R. 2 EXISTING DOUBLER REMOVED FOR ENGINEER REVIEW. AFTER FURTHER INVESTIGATION, MORE DAMAGE FOUND UNDERNEATH FWD DOUBLER AND CUT OUT ENLARGED TO REMOVED ALL DAMAGE FOR ENGINEERING REVIEW. REAR FUSELAGE 1 LOWER SKIN BETWEEN FR 63 & 66 AND BETWEEN STR 19L & 20R REPAIRED.

Part: DOOR — CRACKED (EMERGENCY EXIT) · airframe 43,520 hrs · 27,129 cycles

RIGHT HAND OVER WING EMERGENCY DOOR CRACKED AT MULTIPLE LOCATIONS ON DOOR FRAMES. RIGHT HAND OVER WING EMERGENCY DOOR REPLACED. INSTALLED AND ADJUSTED. PART: EMERGENCY HATCH, RT P/N: 145-25737-405 S/N 145719.

Part: SKIN — DAMAGED (FRAME 12) · airframe 43,520 hrs · 27,129 cycles

MULTIPLE DAMAGES ON LT FWD FUSE 2, IN RSVM AREA BETWEEN FR 12-JUNCTION 02 AND BETWEEN STR 13L-17L. ON LT FWD FUSE 2, IN RSVM AREA BETWEEN FR 12-JUNCTION 02 AND BETWEEN STR 13L-17L SKIN STRIPES. ON LT FWD FUSE 2, IN RSVM AREA BETWEEN FR 12-JUNCTION 02 AND BETWEEN STR 13L-17L DAMAGED. REPAIRED LT FWD FUSE 2 IN RSVM AREA BETWEEN FR 12-JUNCTION 02 AND BETWEEN STR 13L-17L PAINTED. RSVM SKIN WAVINESS MAPPING PERFORMED. NO FAULT DENT REPAIRED.

Part: DOUBLER — DAMAGED (FRAMES 19-20) · airframe 43,520 hrs · 27,129 cycles

REPAIR DOUBLER ON LEFT HAND CENTER FUSE I, BETWEEN FR 19-20 AND STR 11L-13L. ON LEFT HAND CENTER FUSE 1 BETWEEN FR 19-20 AND STR 11L-13L REPAIR DOUBLER REMOVED FOR INVESTIGATION ON LEFT HAND CENTER FUSE 1 BETWEEN FR 19-20 AND STR 11L-13L DAMAGE FOUND UNDERNEATH EXISTING DOUBLER REPAIR CARRIED OUT.

Part: SENSOR — INOPERATIVE (FUEL SYSTEM) · airframe 42,676 hrs · 26,430 cycles

FUEL 2 LOW LEVEL WARNING ON EICAS DURING TAKE OFF. DEFERED FUEL LOW INDICATION ON DMI CONTROL # 70063754, MEL 28-44-00. REPLACED LOW LEVEL SENSOR. OPS CHECK GOOD.

Part: ANTI-ICE VALVE — FAILED (WING) · airframe 42,671 hrs · 26,425 cycles

WING ANTI ICE FAIL DURING ICING CONDITIONS. R&R WING ANTI ICE VALVE. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,472 hrs · 25,455 cycles

STRONG ELECTRICAL ODOR COMOING FROM ROW 6CD-- DEFERRED SIDEWALL LIGHT FIXTURE (AT) ROW 6CD ON OPEN CTRL # 70054935 PER MEL 33-20-00-02 CAT C AUTHORIZED BY MX CTRL RANDY ROUBIQUE- DISCREPANCY WILL BE CLEARED ONCE DEFERRAL FOR THIS ITEM IS CLEARED. THERE WILL BE AN ADDITION TO THIS SDR . ** ADDITIONAL INFORMATION** DEFERRAL FOR LIGHT WAS CLEARED BY REPLACING LIGHT ASSY OPS CHECK GOOD.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 41,430 hrs · 25,426 cycles

ELECTRICAL BURNING SMELL FROM ROWS 6 AND 7 -- INSP CEILING AND SIDEWALLS AT ROWS 3-9 AND FOUND NO INDICATIONS OF ELECTRICAL BURNS. FOUND CEILING LIGHT BALLAST ABOVE ROW 7 WARMER THAN OTHER BALLASTS IN ROWS 3-9. R&R CEILING LIGHT BALLAST ABOVE ROW 7A. DURING INSP FOUND NO SMELL OF ELECTRICAL BURNING AT ANY TIME. RAN APU WITH PACK 1 & 2, NO BURNING SMELL AT ALL, RAN ENGINES WITH PACK(S) 1&2 NO BURNING SMELL. AC OK FOR SERVICE

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

FR. 16 CENTER OMEGA BEAM RT SUPPORT BRACKET CRACKED. REMOVED FR 16 CENTER OMEGA BEAM RT SUPPORT BRACKET. INSTALLED FR 16 CENTER OMEGA BEAM RT SUPPORT BRACKET.

Part: GUSSET — DAMAGED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

LT OMEGA BEAM UPPER GUSSET IN AFT CARGO BETWEEN FRAME 65 THRU 68 IS DAMAGED. REMOVED LT OMEGA BEAM GUSSET BETWEEN FR 65 & FR 68 IN CARGO BAY. REPLACED LT OMEGA BEAM GUSSET IN CARGO FROM FR 65-68.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

COCKPIT FRAME 10 RH IS CRACKED BELOW FO'S SLIDING WINDOW. REMOVED AND DRILLED RT COCKPIT @ FR 10, TEMPORY INSTALL. TRIMED AND CUT COCKPIT FRAME INSTALLED FASTENERS SEVERAL FASTENERS REMAINING TO BE INSTALLED. COMPLETED INSTALL FR 10 RT E/O'S SLIDING WINDOW.

Part: SUPPORT BRACKET — CRACKED (COCKPIT) · airframe 41,291 hrs · 25,311 cycles

CAPT'S CENTER POST GRAB HANDLE SUPPORT BRACKET I/B & O/B ATTACH POINT IS CRACKED. REMOVED DAMAGED AREAS AND LOCATED HOLES. REPAIRED GRAB HANDLE SUPPORT I/B & O/B OF CENTER POST.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

RT FWD BAGGAGE FLOOR SILL HAS 5 EA CORRODED NUTPLATE LOCATIONS BETWEEN FR.61-65. REMOVED RT FLOOR SILL AT FR 61-65. INSTALLED RT FLOOR SILL STILL NEEDS NUTPLATES INSTALLED. INSTALLED NUTPLATES.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

RT OMEGA BEAM I/B LOWER SUPPORT IS CRACKED @ FR 47. REMOVED HI LOCKS IN LOWER FLANGE. REMOVED ALL CHERRY RIVETS & REMOVED I/B LOWER SUPPORT. MATCH DRILLED REPLACEMENT ANGLES. ALODINED & PRIMED. INSTALLED ALL HI LOCKS & CHERRY RIVETS. REPLACE ANGLE.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

LT FLOOR SILL HAS CORROSION AT FR 57. REMOVED LT FLOOR SILL AT FR 57, BEGAN LOCATING AND DRILLING NEW FLOOR SILL. INSTALLED LT FLOOR SILL AT FR 57.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

SERVICE DOOR LOWER THRESHOLD BETWEEN FR 20 THRU 22 HAS CORROSION ON UPPER SURFACE. REMOVED OLD SERVICE DOOR THRESHOLD SILL, PICKED UP HOLES ON NEW PART AND TEMP INSTALLED. WAITING ON HI LITES. INSTALLED NEW PART. NUTPLATE HOLES NEED TO BE LOCATED OFF FLOOR BOARD. INSTALLED NUTPLATES IN THE SVC DOOR THRESHOLD.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

MAIN CABIN FRAME 27 SHEER CLIP IS CRACKED AT STR 15RT. REMOVED FR 27R STR 15 SHEAR CLIP. REMOVED AND REPLACED FR 27 STR 15R SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

MAIN CABIN FRAME 16 SHEAR CLIP IS CRACKED AT STR 15R. REMOVED FR 16 STR 15R SHEAR CLIP. REMOVED AND REPLACED FR 16 STR 15R SHEAR CLIP.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

LT OMEGA BEAM I/B LOWER RAMP ANGLE SUPPORT HAS LIGHT CORROSION BETWEEN FR 19 & 20. REMOVED LT OMEGA BEAM I/B LWR RAMP SUPPORT ANGLE @ FR 19. REMOVED AND REPLACED LWR RAMP SUPPORT ANGLE AT FR 19-20.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

RT OMEGA BEAM UPPER STOP SIGN HAS CORROSION AT FR20. REMOVED RT OMEGA BEAM STOP SIGN AT FRAME 20. LOCATED AND DRILLED STOP SIGN. READY TO INSTALL NEW PART. INSTALLED RT OMEGA BEAM UPPER STOP SIGN AT FRAME 20.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

MAIN CABIN FRAME 15 SHEAR CLIP IS CRACKED AT STR 15R. REMOVED SHEAR CLIP FR 15 STR 15R. REMOVED AND REPLACED FR 15 STR 15R SHEAR CLIP.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

LT OMEGA BEAM SEAT TRACKS HAVE LIGHT CORROSION FROM FR 26 THRU 39. REMOVED AND REPLACED SEAT TRACKS THAT WERE FOUND TO BE OUT OF LIMITS.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

CENTER OMEGA BEAM UPPER SURFACE HAS CORROSION AT FR 61. REMOVED AND REPLACED CENTER OMEGA BEAM GUSSET, STILL REQUIRES NUTPLATES. INSTALLED NUTPLATES.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

FRAME 58 SHEAR CLIP IS CRACKED AT STR 15L. REMOVED FR 58 STR 15L SHEAR CLIP. REMOVED DAMAGED AND INSTALLED NEW FR 58 STR 15L SHEAR CLIP.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

RT OMEGA BEAM STOP SIGN HAS CORROSION AT FR 22. REMOVED OMEGA BEAM STOP SIGN AT FRAME 22 RT. LOCATED AND DRILLED NEW PART. OMEGA BEAM STOP SIGN READY FOR INSTALL. INSTALLED RT OMEGA BEAM STOP SIGN AT FRAME 22.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

LT OMEGA BEAM O/B LOWER SUPPORT IS CRACKED AT FR 47. STARTING REMOVING CRACKED LT O/B OMEGA BEAM LOWER SUPPORT AT FS 47, APPROX. 95% REMOVED. REMOVED & REPLACED LOWER SUPPORT AT FS 47 LT O/B OMEGA BEAM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

LT FLOOR SILL HAS CORROSION ON UPPER SURFACE AT FR 51. BEGAN REMOVING FASTENERS ON LT FLOOR SILL AT FR 51. COMPLETED REMOVAL OF LT FLOOR SILL AT FR 514, LOCATED FASTENER HOLES. REMOVED DAMAGED FLOOR SILL REPLACED WITH NEW FLOOR SILL.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

LT OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AROUND NUTPLATE HOLE AT FR 61. BLENDED DAMAGED AREA ON LT GUSSET AT FR 61 FOUND TO BE WITH IN LIMITS REMAINING THICKNESS .057" REQUIRES NDI. PERFORMED HFEC INSPECTION OF BLENDED AREA CRACK FOUND. REMOVED LT OMEGA BEAM UPPER DIGITAL SUPPORT, INSTALLED NEW LT OMEGA BEAM UPPER DIGITAL SUPPORT AT FR 61. REMOVED DAMAGED AND INSTALLED NEW LT OMEGA BEAM UPPER DIGITAL SUPPORT AT FR 61.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

PAX DOOR LOWER THRESHOLD 2EA NUTPLATES "Z" ANGLE HAS CORROSION AROUND NUTPLATE HOLES. R&R PASSENGER DOOR LOWER THRREHOLD "Z" ANGLES. NUTPLATE HOLES NEED TO BE PICKED UP. LOCATED AND INSTALLED NUTPLATES ON PASSENGER DOOR LOWER THRESHOLD "Z" ANGLES.

Part: FLOOR SUPPORT — GOUGED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

LT OMEGA BEAM I/B LOWER FLANGE GOUGED BETWEEN FR 35 & 35. PERFORMED CUTOUT AS REQUIRED BY DAMAGE LOCATION. INSPECTION REVEALED CUT OUT WAS OUT OF TOLERANCE. SUBMITTED ETD (REF ETD 2019-145-034617). INSTALLED LT OMEGA BEAM I/B LOWER FLANGE REPAIR DOUBLER.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

RT FLOOR SILL FWD OF SERVICE DOOR HAS CORROSION AT FR 20. REMOVED SILL AND REMOVED PROFILE. REPLACED SILL AND REPLACED PROFILE.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

RT OMEGA BEAM O/B LOWER SUPPORT IS CRACKED @ FR 47. REMOVED HI LOCKS IN LOWER FLANGE. REMOVED ALL CHERRY RIVETS & REMOVED O/B LOWER SUPPORT. MATCH DRILLED REPLACEMENT ANGLES, ALODINED & PRIMED. INSTALLED ALL HI LOCKS & CHERRY RIVETS. REPLACED ANGLE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

CARGO DOOR LOWER THRESHOLD 'Z' ANGLE HAS CORROSION AROUND NUTPLATE HOLES AND FASTENERS. REMOVED CARGO DOOR LOWER "Z" ANGLE THRESHOLD ON FUSELAGE. DRILLED NEW "Z" ANGLE HOLES FOR LOWER CARGO DOOR FUSELAGE THRESHOLD. INSTALLED LOWER CARGO DOOR FUSELAGE THRESHOLD LOWER "Z" ANGLE.

Part: ATTACH ANGLE — BENT (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

CARGO DOOR LOWER THRESHOLD 'T' PROFILE AT FR 66 BENT. REMOVED CARGO RAMP 'T' PROFILE, LOWER ATTACH ANGLE. R/R THE UPPER RAMP ANGLE ATTACH AT FR 66. REPLACED "T" PROFILE, LOWER ATTACH ANGLE & PLATE FOR CARGO RAMP ON FR66.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

CARGO DOOR TORSION BAR AFT SUPPORT BRACKET LOWER MOUNT IS CRACKED. REMOVED 2(EA) CRACKED BRACKET AT CARGO DOOR TORSION BAR AFT SUPPORT BRACKET ASSY. P/N 145-37862-001 AND 145-25677-003. PARTIALLY INSTALLED 2 EA BRACKETS SAME AS ABOVE. INSTALLED BRACKETS 2 EA AT AFT CARGO DOOR TORSION BAR BRACKET ASSY. P/N'S 145-37862-001, AND 145-25677-003.

Part: SKIN — DENTED (FUSELAGE) · airframe 41,291 hrs · 25,311 cycles

FUSELAGE EXTERIOR SKIN HAVE DENT AT FRAME 9 @ STR 19L. STRIPPED THE PAINT AT AND AROUND DENT AT FR 9, STR 19L. MAPPED OUT RIVET PATTERN AND CUT OUT ON SKIN. CUT OUT DAMAGE, DRILLED & MADE DOUBLER & FILLER & COUNTER SUNK HOLES. INSTALLED REPAIR ON FUSELAGE SKIN AT FR 9, STR 19L, RESTORED TO ORIGINAL FINISH.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 41,291 hrs · 25,311 cycles

CARGO DOOR FWD LOWER EDGE 'L' SUPPORT FLANGE IS CRACKED ON FWD LOWER END OF DOOR. REMOVED DAMAGE. INSPECTED DAMAGE AREA AFTER CUT OUT, NO DEFECTS NOTED. INSTALLED REPAIR. REFERENCE NRWO 22517-539 FOR PAINT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 29,276 hrs · 23,669 cycles

PAC 1 VALVE CLOSED EICAS MSG DISPLAYED IN FLIGHT. SWAPPED DTC 1 & DTC 2 FOR TROUBLESHOOTING. OPS CHECK GOOD AT THIS TIME.

Part: PACKING — FAILED (NLG STRUT)

ON LANDING GEAR RETRACTION AFTER TAKEOFF, THE NOSE GEAR SOUNDED LIKE IT DID NOT RETRACT, HAD A LOUD AUDIBLE SOUND ASSOCIATED WITH NSW DOWN, GEAR AURAL WARNING SOUNDED, NO OTHER INDICATIONS. INSPECTED THE NLG AND FOUND THE INNER STRUT BINDING, REPACKED THE STRUT, .FOUND A BAD PACKING. PERFORMED GEAR SWING, FOUND NORMAL.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 38,916 hrs · 23,374 cycles

NR 1 ENGINE EXECEEDENCE DURING FLIGHT, PRECAUTIONARY SHUTDOWN PEFORMED. R & R THE NR 1 ENGINE. OPS AND LEAK CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 38,861 hrs · 23,328 cycles

EICAS CAUTION, LANDING AIR-GROUND FAILED IN FLIGHT DURING CLIMB OUT. R & R THE NLG AIR GROUND PROXIMITY SENSOR. OPS CHECKED GOOD.

Part: SEAL — DIRTY (PAX DOOR) · airframe 37,928 hrs · 22,486 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. CLEANED PAX DOOR RUBBER SEAL AND OPS CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 37,668 hrs · 22,258 cycles

EMERGENCY EXIT SIGN INOPERATIVE AT 3C. RECONNECTED WIRES ON EMERGENCY EXIT SIGN AT 3C (#14). OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,185 hrs · 21,840 cycles

COCKPIT EXIT SIGN INOPERATIVE. R & R THE SIGN, OPS CHECKED GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 37,185 hrs · 21,840 cycles

RT SILL AT FR 49 HAS LEVEL 3 CORROSION. INSTALLED NEW RT SILL AT FR 49.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,169 hrs · 21,826 cycles

LEFT FWD WING TO FUSELAGE FAIRING EXTERIOR FLOOD LIGHT INOPERATIVE. R & R THE LIGHT, OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,837 hrs · 20,002 cycles

MAINDOOR EXTERIOR FLOOD LIGHT LOCATED ON BOTTOM SIDE OF THE PLUG DOOR HING IS INOPERATIVE. R & R BULB ON MAINDOOR EXTERIOR FLOOD LIGHT ON BOTTOM SIDE OF PLUG DOOR HING. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,499 hrs · 19,726 cycles

PAX DOOR SWING ARM EMERGENCY LIGHT IS INOPERATIVE. R & R PAX DOOR SWING ARM EMERGENCY LIGHT INOPERATIVE BULBS. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,716 hrs · 35,548 cycles

PAX DOOR EMERGENCY FLOOD LIGHT NR 1 INOPERATIVE. R & R PAX DOOR EMERGENCY FLOOD LIGHT NR 1. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 60-61) · corrosion level 2 · airframe 33,708 hrs · 19,095 cycles

DURING C-CHECK CORROSION ON RT OMEGA BEAM BETWEEN FRAMES 60-61. MAINTENANCE COMPLETED REPAIR TO RT OMEGA BEAM FRAME 60-61 AT NUTPLATE REGION IAW EC5320-02035. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-60) · corrosion level 2 · airframe 33,708 hrs · 19,095 cycles

DURING C-CHECK, CORROSION, LOCAL LEVEL 2, ON CENTER OMEGA BEAM BETWEEN FRAMES 59-60. MAINTENANCE COMPLETED REPAIR TO CENTER OMEGA BEAM FRAMES 59-60 IAW EC5320-02035 ORIG AND IS DETERMINED TO BE A MAJOR IAW EC. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 79) · airframe 33,708 hrs · 19,095 cycles

DURING C-CHECK, LT FUSELAGE SKIN AT FRAME 79, STRINGER 5L-6L RIVET SKIN CRACKED. MAINTENANCE REPAIRED LT FUSELAGE SKIN AND INSTALLED SKIN BUSHING AND RESTORED ORIGINAL FINISH ON LT FUSELAGE SKIN AT FRAME 79, STRINGER 5L-6L IAW EC5330-03009. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FRAME 65) · corrosion level 2 · airframe 33,708 hrs · 19,095 cycles

DURING C-CHECK MOUNTING HOLE FOR RADIO ALTIMETER SKIN HAS CORROSION, LOCAL LEVEL 2, FRAME 65, AC SKIN. MAINTENANCE COMPLETED SKIN REPAIR AT FRAME 65 AROUND RADIO ALTIMETER IAW EC5330-03010. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 33,708 hrs · 19,095 cycles

DURING C-CK. CARGO DOOR CUTOUT LOWER BEAM CORRODED. R & R CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (LAVATORY LIGHT) · airframe 31,484 hrs · 17,610 cycles

THE CREW REPORTED A BURNING ODOR IN THE REAR OF ACFT. MAINTENANCE INSPECTED THE ACFT AND FOUND THE LIGHT BALLAST BEHIND THE LAV MIRROR TO BE OVERHEATED. R & R THE LIGHT BALLAST, OPS TESTED WITH NO DEFECTS. ACFT APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 30,239 hrs · 16,840 cycles

CREW REPORTED A LAVATORY SMOKE WARNING DURING CLIMBOUT AT APPROXIMATELY 10,000 FEET. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND R & R NR 2 ENGINE, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — FAULTY (SMOKE DETECTION) · airframe 30,086 hrs · 16,739 cycles

THE CREW REPORTED A LAV SMOKE INDICATION DURING CLIMB. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR PANEL. OPS CHECKS WERE GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,908 hrs · 16,636 cycles

CREW REPORTED EMERGENCY EXIT LIGHT ABOVE ENTRANCE DOOR INOPERATIVE. R & R DOOR BULB AND OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (ZONE 200) · airframe 28,913 hrs · 16,012 cycles

DURING C-CHECK SHEAR TIE AT FRAME 65, STRINGER, 2R CRACKED. MX PERFORMED TEMPORARY REPAIR ON SHEAR TIE AT FRAME 65, STR 2R. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,913 hrs · 16,012 cycles

DURING C-CHECK, CARGO DOOR CUTOUT LOWER BEAM CORRODED IN MULTIPLE AREAS. MXE R & R CARGO DOOR CUTOUT LOWER BEAM IAW SRM 51-40-02 AND CPM 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 28,164 hrs · 15,531 cycles

THE CREW REPORTED THAT AFTER TAKE OFF THE F/A CALLED WITH A VISUAL VENTING FROM THE RT WING. THE CREW RAN THE QRH AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX R & R THE RT FUEL TANK FLAPPER VALVE AT RIB 19, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — SMOKE (NR 1) · airframe 26,983 hrs · 14,753 cycles

SMOKE WAS SEEN IN THE CABIN DURING ENGINE RUNS AND WAS ISOLATED TO THE NR 1 ENGINE. MX REMOVED AND REPLACED ENGINE IAW TASKCARD 6271001. ALL WORK WAS ACCOMPLISHED AND THEN RELEASED UPON COMPLETION OF OPS CHECKS AND LEAK CHECKS.

Part: LINE — BROKEN (PORTABLE O2) · airframe 26,532 hrs · 14,457 cycles

DIVERTED. DISCOVERED AFT PORTABLE O2 BOTTLE HAD A PARTIALLY CRACKED & BROKEN LINE FROM THE BOTTLE TO THE MASK.

Part: ENGINE — FAILED (NR 1) · airframe 24,637 hrs · 13,334 cycles

DURING TAKEOFF, THE CREW HEARD A LOUD BOOM FOLLOWED BY THE LOSS OF TEMP INDICATION ON THE NR1 ENGINE. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE GATE WITHOUT INCIDENT. ON INSPECTION NR 1 ENGINE TURBINE WAS FOUND TO BE DAMAGED. SUP: R & R THE NR ENGINE, OPS AND LEAK CHECKED WITH NO DEFECTS, AND AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 24,319 hrs · 13,156 cycles

TYS - A/C DIVERTED TO TYS FROM GSO TO IAH WITH A NR 1 ENGINE BLEED LEAK INDICATION ON THE EICIAS. MAINTENANCE COMPLIED WITH THE NR 1 BLEED SYSTEM CHECK IAW EMB 145XR AMM 36-00-00-700-803A. OPS CHECK GOOD, COULD NOT DUPLICATE THE PROBLEM AND WAS RELEASED BACK TO SERVICE.

Part: STRUCTURE — CORRODED (E&E DOOR) · airframe 24,140 hrs · 13,046 cycles

DURING C CHECK INSPECTION THE REAR ELECTRONICS DOOR WAS NOTED HAVING CORROSION UNDER THE FORWARD LOWER TEFLON GUIDE. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED FILLER IAW EC5240-01055.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 24,058 hrs · 12,996 cycles

IAH - FLIGHT 2100, DURING POST FLIGHT THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRECOOLER — FAULTY (BLEED AIR SYS) · airframe 23,081 hrs · 12,422 cycles

IAH - FLIGHT 5982, THE CREW REPORTED A BLEED ONE OVERTEMP ON CLIMBOUT OF DEN. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE PRECOOLER, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SLEEVE — DAMAGED (ANTI-ICE SYS) · airframe 22,950 hrs · 12,319 cycles

FLIGHT 5819 - IND-DAY - FLIGHT CREW DIVERTED FLIGHT TO IND DUE TO WING ANTI ICE/RA FAIL, ASSOCIATED TO PACK 1 VALVE CLOSED AND PACK 2 OVERHEAT. EWR MX PERFORMED WING ANTI ICE TEST AND COULD NOT DUPLICATE MESSAGE. MX REMOVED AND REPLACED LARGE DUCT CONNECTED TO AFT SIDE OF DUAL TEMP CONTROL VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: VALVE — INOPERATIVE (NR 1) · airframe 22,411 hrs · 11,958 cycles

FLIGHT 2717 - EWR - FLIGHT CREW REPORTED BLEED NR 1 OVERTEMP IN EICAS. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 1 FAN AIR VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — INOPERATIVE (NR 2 TAT) · airframe 21,299 hrs · 11,346 cycles

IAH - FLIGHT 2184, THE CREW REPORTED A TAT 2 INOP MESSAGE ON EICAS ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO TAT HEAT SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,163 hrs · 10,178 cycles

SHV - DURING C-CHECK SKIN HAS CRACKS AROUND RIVETS AT FR 76 STR 2L-3L. REPAIRED SKIN IAW EC 5330-02053. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,163 hrs · 10,178 cycles

SHV - DURING C-CHECK LT OMEGA BEAM IS CORRODED (LOCAL LEVEL 2) AT FRAME 20. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 20 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — MISALIGNED (RUDDER) · airframe 19,163 hrs · 10,178 cycles

SHV - DURING C-CHECK RUDDER II ATTACHMENT BRACKET 2ND FROM BOTTOM NOT IN-LINE WITH OTHER 3 BRACKETS. MAINTENANCE REMOVED AND REPLACED RUDDER II ATTACHMENT BRACKET 2ND FROM BOTTOM IAW EMB-145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,163 hrs · 10,178 cycles

SHV - DURING C-CHECK (FRAME 45) LT UPPER SEAT TRACK SUPPORT ANGLE CORRODED (LEVEL 2 LOCAL) IN CURVE. MAINTENANCE PERFORMED REPAIR OF LT UPPER SEAT TRACK SUPPORT IAW EC5320-01515 ORIG AND IAW ETD 2009-145/10245. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 3 · airframe 19,163 hrs · 10,178 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION (LEVEL 3 LOCAL) AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FRAMES 18-24 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 18,480 hrs · 9,796 cycles

IAH - FLIGHT 2446 - THE CREW REPORTED A LANDING GEAR AIR / GROUND FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, RESET THE AIR/GROUND CIRCUIT BREAKERS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — MALFUNCTIONED (BLEED AIR SYS)

ENROUTE FROM IAH TO ORF WHEN THE CREW RECEIVED SEVERAL EICAS MESSAGES FROM BLEED NR 1 OVERTEMP FOLLOWED BY BLEED NR 2 OVERTEMP THROUGHOUT DESCENT TO EXIT, IN ADDITION TO ANTI-ICE FAIL AND ICE CONDITIONS. DIVERTED TO TYS, WHERE MX REMOVED R&R BOTH FWD FAN AIR THERMOSTATS. OPS CHECKS GOOD. WORK WAS IAW AMM 36-11-06 AND WAS RELEASED TO SERVICE.

Part: SCREW — LOOSE (DOOR FRAME)

DURING ROUTINE MAINTENANCE THE LT EMERGENCY EXIT HATCH WOULDN’T OPEN. MAINTENANCE INSPECTED AND FOUND SCREW LOOSE ON SIDE OF DOOR FRAME. THE SCREW WAS TIGHTENED AND OPERATIONAL CHECKS OF THE DOOR WAS GOOD. (A)

Part: PRESSURE SWITCH — FAULTY (RUDDER) · airframe 14,294 hrs · 7,537 cycles

CLE FLIGHT 2285 CLE-MHT - THE CREW REPORTED RUDDER SYSTEM NR 1 AND NR 2 INOP, AND RUDDER YAW DAMP INOP MESSAGES ILLUMINATED ON THE ECIAS DISPLAY. AN EMERGENCY WAS DECLARED AND THE A/C LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 AND NR 2 RUDDER PRESSURE SWITCHES. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — CORRODED (FUEL TANK) · airframe 9,418 hrs · 4,983 cycles

TYS - DURING A CURRENT 2C INSPECTION CORROSION WAS FOUND ON THE FORWARD SKIN OF THE VENTRAL TANK UNDERNEATH A SUPPORT BRACKET FOR AN ARRESTOR LINE. MAINTENANCE CUT OUT THE DAMAGED AREA, FABBED A DOUBLER AND FILLER, ALODINE AND PRIME, INSTALL DOUBLER, FILLER AND BRACKET. LEAK CHECKS GOOD. A/C WILL BE PUT IN SERVICE UPON COMPLETION OF THE 2C CHECK. ALL WORK WAS ACCOMPLISHED IAW EC2810-01025.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,283 hrs · 4,912 cycles

BOTH LT/RT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 3 AND NR 4 EMERGENCY BATTERY LIGHT CHARGERS IAW 145XR AMM 33-50-04. OPS CHECK GOOD.