N14180

Part: NONE — NONE · airframe 37,398 hrs · 23,379 cycles

MCD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R&R MCD EXT EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: SKIN — DENTED (LT WING LE) · airframe 36,920 hrs · 22,945 cycles

LH WING INBD LEADING EDGE HAS A DENT. ACCOMPLISHED PERMANENT REPAIR TO THE LEFT HAND WING LEADING EDGE 1 BY REMOVING DAMAGE, NDT PERFORMED. FABRICATED AND INSTALLED REPAIR PARTS

Part: FLOOR SUPPORT — CORRODED (FRMS 23-59) · airframe 36,920 hrs · 22,945 cycles

CABIN FLOOR SUPPORTS IN MIDDLE SECTION (FR 23-FR 59) POSSIBLE CORROSION. EVALUATED AREA RH FLOOR SUPPORT BTW FR 23-25, FR53-57. FOUND TO BE IN LIMIT, APPLIED ALODINE AND PRIME. AREA AT RH BTW FR 25-36, FR 37-41, LH BTW FR 21-23, FR 23-25, FR 28-40, FR 29-35, FR 48-53 FOUND TO BE OUT OF LIMITED. REMOVED DAMAGE SILL AND INSTALLED NEW SILL. FABRICATED SILL SECTION AND SPLICE BTW FR 21-23, LH SIDE STR 13L INSTALLED SILL SECTION AND SPLICE. NR # 2340

Part: FLOORBEAM — CORRODED · airframe 36,920 hrs · 22,945 cycles

LAV FLOOR BEAMS BL 19L, BL 0, BL 19R SIGNS OF CORROSION. EVALUATED AND REMOVED CORROSION ON LAV FLOOR BEAMS. FOUND TO BE 100% OUT OF LIMITS. REMOVED AND INSTALLED NEW GUSSETS ON BL 0 AND BL 19. REMOVED AND FABRICATED NEW GUSSET FOR LBL19 AND INSTALLED NEW GUSSET. TREATED, PRIMED AND TOP COATED GUSSETS. NR # 1172

Part: SEAT TRACK — DAMAGED (LT COCKPIT) · airframe 36,920 hrs · 22,945 cycles

LH COCKPIT SEAT TRACK HAVE ELONGATED HOLES (LH AND RH SIDE) AND CHAFFED. EVALUATED LH COCKPIT SEAT TRACK. FOUND TO BE OUT OF LIMITS. COUNTER SIDE EXCEEDS THE MINIMUM REQUIREMENT. REMOVED AND REPLACED SEAT TRACK LH.

Part: FLOOR SUPPORT — CORRODED (FRMS 16-24 BL0) · airframe 36,920 hrs · 22,945 cycles

CABIN FLOOR SUPPORTS IN FWD SECTION (FWD OF FR 23) POSSIBLE CORROSION. REMOVED CORROSION ON GUSSET AND BEAM ASTER EVAL. FOUND BOTH PARTS TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW GUSSET AND BEAM AT FR 16 TO FR 24 BL-O AND FR 20 BL-O. TREATED, PRIMED, TOP COATED AND APPLIED CIC ON THE AREA.

Part: SEAT TRACK — DAMAGED (CABIN) · airframe 36,920 hrs · 22,945 cycles

RH COCKPIT SEAT TRACK HAVE ELONGATED HOLES (LH SIDE AND RH SIDE) AND CHAFED. REMOVED AND REPLACED 2 EA TRACKS AT RH COCKPIT (LH SIDE AND RH SIDE).

Part: REINFORCEMENT — CORRODED (PAX THRESHOLD) · airframe 36,920 hrs · 22,945 cycles

PAX DOOR THRESHOLD REINFORCING STRUCTURE HAS CORROSION THREE DIFFERENT BRACKETS. REMOVED AND REPLACED 2 NEW BRACKETS ON PAX DOOR OUTBD BRACKETS PAINT DAMAGE ONLY.

Part: FLOORBEAM — CORRODED (FRM 23 S15R) · airframe 36,920 hrs · 22,945 cycles

FRM 23, 15R, RBL 0.0'-27.0" FLOOR BOARD SUPPORT BEAM HAS CORROSION (FLOOR STRUCTURE). REMOVED AND REPLACED ANGLE (SUPPORT).

Part: HINGE — CRACKED (PAX DOOR) · airframe 36,920 hrs · 22,945 cycles

PAX DOOR, LWR SIDE HINGE ATTACHMENT FITTING HAS CRACK MARK. BLENDED OUT DAMAGE.

Part: HINGE — WORN (PAX DOOR) · airframe 36,920 hrs · 22,945 cycles

PAX DOOR, UPPER SIDE HINGE ATTACHMENT FITTING HAS WEAR MARKS AND GAUGING. BLENDED OUT DAMAGE.

Part: LIGHT — OVERHEATED (CABIN) · airframe 36,887 hrs · 22,921 cycles

IAH - FLIGHT 4328, THE CREW REPORTED CEILING LIGHT SMOKE SMELL 1A & 2A. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE AFFECTED CEILING LIGHT ON MEL 33-20-00-2, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 03/10/20 IAH MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS. THE MEL WAS REMOVED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GROUND STUD — DAMAGED (EMERGENCY LIGHTS) · airframe 35,486 hrs · 21,857 cycles

CREW REPORTED ROW 18 EMERGENCY LIGHTS WILL NOT ILLUMINATE FACING A/C FRONT BACK SIDE WORKS. MX INSPECTED AND FOUND W192-8819-22N (GROUND STUD GS8517DC) DAMAGED REPAIRED ITEMS OPERATIONAL CHECKS GOOD IAW EMB 145 XRJ AMM 33-50-50 (20-13-05) A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 34,145 hrs · 20,867 cycles

DURING MX INSPECTION THE LOWER EMERGENCY LIGHT ON THE SERVICE DOOR WAS INOP. MX REMOVED AND REPLACED THE NR 2 INVERTER WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (NR 1 ENGINE) · airframe 34,090 hrs · 20,829 cycles

TYS A/C CAME IN FOR A 2A INSPECTION WHEN INSPECTION FOUND THE LEFT ENGINE LOWER FWD AFT FITTING CRACKED AND VERIFIED BY NDT METHODS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EA 26-2014-063. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AFTER ALL WORK IS C/W.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,054 hrs · 18,668 cycles

DURING C-CK. FUSELAGE SKIN CRACK AT FR 75 BTW STR 2L-3L. REPAIRED FUSELAGE SKIN IAW SRM 53-31-01. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COMPUTER — MALFUNCTIONED

THE CREW REPORTED THE AIRCRAFT GOES INTO A ROLL AND GA MODE DURING TAKOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 IC600 COMPUTER. OPS CHECKED GOOD.

Part: COMPUTER — FAULTED (ZONE 100) · airframe 30,408 hrs · 18,192 cycles

CREW REPORTED THE ACFT GOES INTO R/O AND G/A MODE DURING TAKEOFF AND ON APPROACH AND UNABLE TO SWITCH OUT OF IT. MAINTENANCE R & R IC-600 NR 2 WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 2 NACELLE) · airframe 28,203 hrs · 16,593 cycles

DURING MAINTENANCE THE NR 2 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND CRACKED. MAINTENANCE REPLACED THE NR 2 ENGINE YOKE FITTING IAW STS EA 26-2014-063.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,769 hrs · 16,299 cycles

DURING PREFLIGHT THE EXIT ROW EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — FAILED (COCKPIT TEMP) · airframe 27,116 hrs · 15,875 cycles

THE CREW REPORTED WINDSHIELD HEAT NR 1 FAIL RESULTING IN ELECTRICAL OVERHEAT SMELL. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD HEAT TEMP CONTROLLER, OPS CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,127 hrs · 15,200 cycles

DURING MAINTENANCE INSPECTION, THE FWD EMERGENCY EXIT ROW AISLE LIGHT WOULD NOT ILLUMINATE. MX R & R THE NR 6 EMERGENCY LIGHT SYSTEM INVERTER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 25,999 hrs · 15,127 cycles

THE CREW REPORTED OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 DID NOT ILLUMINATE DURING TEST. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY EXIT LIGHT AT ROW 12. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (SEAT 18C) · airframe 25,393 hrs · 14,712 cycles

DURING PREFLIGHT THE CREW REPORTED THAT THE EMERGENCY LIGHT WAS INOPERATIVE OVER SEAT 18C ON THE FORWARD SIDE. MAINTENANCE R & R THE AFFECTED LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FRAME 78) · airframe 25,088 hrs · 14,522 cycles

DENT ON REAR FUSELAGE SKIN, FRAME 78 STRINGER 6L. REPAIRED DENT IAW EC 5330-02473.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 25,088 hrs · 14,522 cycles

WASTE DRAIN VALVE COMPARTMENT CORRODED. R & R WASTE DRAIN VALVE COMPARTMENT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 49) · airframe 25,088 hrs · 14,522 cycles

CORROSION ON LT FLOOR SUPPORT AT FRAME 49. BLENDED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-23-10. NDT PERFORMED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 25,088 hrs · 14,522 cycles

CORROSION ON RT FLOOR SUPPORT AFT OF FRAME 50. R & R RT FLOOR SUPPORT FROM FRAMES 48-52 IAW SRM 51-40-02, 51-20-03.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 25,088 hrs · 14,522 cycles

CORROSION ON RT FLOOR SUPPORT FRAMES 41-48. R & R RT FLOOR SUPPORT IAW SRM 51-40-02, 51-40-04, 51-40-06.

Part: FLOORBEAM — CORRODED (FRAME 23) · airframe 25,088 hrs · 14,522 cycles

RT FLOORBEAM ANGLE CORRODED AT FRAME 23. R & R RT FLOORBEAM ANGLE IAW SRM 51-40-02, WO 80225, WC 1183.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 25,088 hrs · 14,522 cycles

CORROSION ON LT SUPPORT AT FRAME 64 S15L. BLENDED CORROSION MATERIAL LOSS WAS .003" WITHIN LIMITS IAW SRM 53-31-10.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 25,088 hrs · 14,522 cycles

CORROSION ON LT FLOOR SUPPORT. R & R LT FLOOR SUPPORT FROM FRAMES 18 - 24 IAW SRM 51-40-02, 51-40-09, 51-20-03.

Part: CHANNEL — CORRODED (ZONE 100) · airframe 25,088 hrs · 14,522 cycles

SERVICE DOOR FRAME CHANNEL CORRODED AT THREE NUT PLATE LOCATIONS. R & R SERVICE DOOR FRAME CHANNEL IAW SRM 51-40-02, 51-20-03.

Part: CAP — CORRODED (TRUNNION) · airframe 25,088 hrs · 14,522 cycles

LEFT NLG TRUNNION CAP HAS PITTING. REMOVED MINOR PITTING ON LT NLG TRUNNION CAP IAW SRM 53-11-08, WO 80225, W/C 1177.

Part: BEAM — CORRODED (ZONE 100) · airframe 25,088 hrs · 14,522 cycles

LAV LT BEAM CAP CORRODED. BLENDED CORROSION, REMOVED .005" OF MATERIAL LOSS. FOUND TO BE WITHIN LIMITS IAW SRM 53-24-10, WO 80225, WC 1184.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,088 hrs · 14,522 cycles

CORROSION UNDER LAV FLOOR PANEL 261DF ON FLOORBEAM. R & R FLOORBEAM ANGLE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 65) · airframe 25,088 hrs · 14,522 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT FRAME 65. BLENDED CORROSION IAW SRM 53-31-10, FOUND TO BE WITH IN LIMITS IAW SRM 53-31-10, SWPM 20-21-00, AND CPM 51-21-04, 51-21-05. NDT PERFORMED, NO DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-36) · airframe 25,088 hrs · 14,522 cycles

RIGHT FLOOR SUPPORT FROM FRAMES 24-36 IS CORRODED. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-4-02, AND SWPM 20-21-00.

Part: SPLICE — CORRODED (FLOOR SUPPORT) · airframe 25,088 hrs · 14,522 cycles

FLOOR SUPPORT CONNECTION SPLICE CORRODED AT FRAME 35 UNDER FLOORBOARD 252AF. BLENDED CORRODED AREA IAW SRM 53-23-10, AREA LESS THAN 10 PERCENT MATERIAL LOSS, FOUND TO BE WITH IN LIMITS.

Part: FLOOR SUPPORT — CORRODED (FRAME 26) · airframe 25,088 hrs · 14,522 cycles

CORROSION ON FLOOR SUPPORT FWD OF FRAME 26 LT SIDE. REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-40-02, 51-20-03, 51-40-06, AND SWPM 20-22-00.

Part: WINDOW FRAME — CORRODED (ZONE 200) · airframe 25,088 hrs · 14,522 cycles

RIGHT WINDSHIELD ASSY FRAME IS CORRODED IN MULTIPLE AREAS. BLENDED CORRODED AREAS IAW ACMM 56-10-01, FOUND TO BE WITHIN LIMITS IAW MM 56-10-01. NDT PERFORMED, NO DEFECTS NOTED.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 25,088 hrs · 14,522 cycles

CORROSION ON FLOORBEAM. R & R FLOORBEAM IAW SRM 51-40-02, 51-20-03 AND, 51-40-02.

Part: WINDOW FRAME — CORRODED (COCKPIT) · airframe 25,088 hrs · 14,522 cycles

LEFT WINDSHIELD ASSY FRAME IS CORRODED IN MULTIPLE AREAS. BLENDED CORRODED AREAS IAW ACMM 56-10-01, FOUND TO BE WITHIN LIMITS IAW ACMM 56-10-01. NDT PERFORMED, NO DEFECTS NOTED.

Part: WIRE — DAMAGED (FLASHLIGHT) · airframe 21,732 hrs · 12,394 cycles

CREW REPORTED THE F/O'S FLASHLIGHT WAS NOT CHARGING. MX REPAIRED THE WIRE ON THE F/O'S FLASHLIGHT CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 20,565 hrs · 11,658 cycles

DURING POST FLIGHT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT SHUTOFF. SWITCHES WERE CYCLED ON AND OFF AND THE LIGHTS EXTINGUISED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,826 hrs · 11,155 cycles

FWD FACING CEILING EMERGENCY SIGN OVERWING FOUND INOPERATIVE. MX R & R EMERGENCY EXIT CEILING SIGN WITH OPS CHECK SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 19,587 hrs · 10,983 cycles

CREW REPORTED SMOKE IN THE LAVATORY. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ENGINE LEAKING, MX REPLACED THE NR 2 ENGINE. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 19,331 hrs · 10,817 cycles

SPLICE BRACKET CRACKED AT THE LT OMEGA BEAM BETWEEN FR 16 AND 17. MX R & R THE SPLICE BRACKET IAW SRM 51-20-03 AND 51-40-02. ACFT WILL BE RELEASED AT THE END OF THE CHECK.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 19,331 hrs · 10,817 cycles

SHEAR TIE CRACKED AT FR 73, BETWEEN STR 8BR AND 9BR. MX R & R THE SHEAR TIE IAW SRM 51-10-03 AND 51-40-02.

Part: THRESHOLD — CORRODED (ZONE 100) · airframe 19,331 hrs · 1,817 cycles

CORROSION WAS FOUND IN THE CARGO CUTOUT LWR THRESHOLD AT SCREW HOLES FROM FR.65 TO FR. 68. CORROSION WAS OUT OF LIMITS AFTER BLENDING AND MX R & R THE THRESHOLD IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 19,331 hrs · 10,817 cycles

CORROSION WAS FOUND ON THE LT SILL FROM FRAME 42 TO 44 AT THE SCREW HOLES. MX BLENDED THE CORROSION IAW SRM 51-10-03, WAS OUT OF LIMITS IAW SRM 53-22-10. R & R SILL IAW SRM 51-20--03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 19,331 hrs · 10,817 cycles

CORROSION WAS FOUND IN THE BUTT SPLICE RT OMEGA BEAM AT FR 22. BLENDED AREA AND WAS OUT OF LIMITS IAW SRM 53-21-10. R & R THE DOUBLER IAW SRM 51-20-03 AND 51-40-02. ACFT WILL BE RELEASED AT THE END OF THE CHECK.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 19,331 hrs · 10,817 cycles

SHEAR TIE CRACKED AT FRAME 68 BETWEEN STR 6L AND 7L. MX R & R THE SHEAR CLIP IAW SRM 51-20-03 AND 51-40-02. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: CROSSBEAM — CRACKED (ZONE 100) · airframe 19,331 hrs · 10,817 cycles

THE AVIONICS RACK HAS A CRACK JUST INSIDE DOOR PANEL 272DR. MX R & R THE CROSSBEAM IAW SRM 51-20-03 AND 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

LEFT SUPPORT AT FRAME 49 CORRODED BEYOND LIMITS. R & R SUPPORT.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

LT CARBON CROSS MEMBER SUPPORT AT LT FLOOR SILL AT FRM 61 CORRODED BEYOND LIMITS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

LT FLOOR SUPPORT AT FRM 29-35 CORRODED BEYOND LIMITS. R & R SILL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

SILL CORRODED BEYOND LIMITS AT FRM 35. R & R SILL.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

RT CARBON CROSS BEAM SUPPORT AT RT FLOOR SILL AT FRM 61 CORRODED BEYOND LIMITS. R & R SILL.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

RT FLOOR SUPPORTCORRODED BEYOND LIMITS AT FRM 59. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

ONE SMALL AREA OF CORROSION ON RT FLOOR SUPPORT AT FRM 61 SPLICE. CORRODED BEYOND LIMITS. R & R SUPPORT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

RT FLOOR SUPPORT CORRODED BEYOND LIMITS AT FRM 48-53. REMOVED AND REPLACED FLOOR SUPPORT.

Part: GUSSET — CORRODED · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

CORROSION BEYOND LIMITS AROUND 2 NUT PLATES ON GUSSET. R & R GUSSET.

Part: SILL — CORRODED · corrosion level 2 · airframe 19,331 hrs · 10,817 cycles

SILL CORRODED BEYOND LIMITS AT FRM 36-40. R & R SILL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,016 hrs · 10,084 cycles

IAH - DURING MAINTENANCE INSPECTION THE FORWARD CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND THREE EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 18,016 hrs · 10,084 cycles

IAH - DURING MAINTENANCE INSPECTION THE FORWARD CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND THREE EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 18,013 hrs · 10,082 cycles

FRAME 78 BETWEEN STRINGERS 5L AND STRINGER 6L HAS A DENT WITH A CREASE. PERFORMED CUTOUT AND DOUBLER REPAIR, SEALED, ALODINED, PRIMED AND PAINTED IAW ETD 2011-145-103765.

Part: INVERTER — DEFECTIVE (CABIN) · airframe 17,553 hrs · 9,824 cycles

TYS - A/C IN FOR A SERVICE ROUTINE WHEN INSPECTION FOUND THE RT FWD LWR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD AND WAS RELEASED.

Part: ACTUATOR — LEAKING (NR 2 ENGINE) · airframe 26,945 hrs · 20,362 cycles

FLIGHT 5821 - IAD - FLIGHT CREW REPORTED SMOKE SMELL IN LAV AREA DURING TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. IAD MX REMOVED AND REPLACED ENG NR 2 CVG ACTUATOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 14,454 hrs · 8,137 cycles

SHV - DURING C-CHECK THE LT AFT UPPER SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 2-10L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS TO THE AFFECTED FASTENERS IAW EC5330-02156. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 14,454 hrs · 8,137 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT BEAM BETWEEN FRAME 65-68 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT BEAM BETWEEN FRM 65-68 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 14,454 hrs · 8,137 cycles

SHV - DURING C-CHECK THE RT AFT UPPER SKIN WAS FOUND TO BE CRACKED AROUND A FASTENER AT FRAME 79 AND STRINGER 5R. MAINTENANCE REMOVED THE CRACK AND PERFORMED A BUSHING REPAIR IAW EC 5330-02157. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 3 · airframe 14,454 hrs · 8,137 cycles

SHV - DURING C-CHECK FRAME 65 SHEAR CLIP CORRODED (LEVEL 3 LOCAL) AT LOWER CORNER OF CARGO DOOR CUTOUT. MAINTENANCE INSTALLED A SPLICE REPAIR AT FRAME 65 SHEAR CLIP IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 13,873 hrs · 7,824 cycles

FLIGHT 2321 - EWR - FLIGHT CREW REPORTED NR 1 MFD INOPERATIVE WITH BURNING SMELL. EWR MX REMOVED AND REPLACED MFD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ACTUATOR — SLOW (NLG DOOR) · airframe 9,913 hrs · 5,685 cycles

CLE FLIGHT 2141 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE WHEN PUTTING LANDING GEAR DOWN DURING APPROACH INTO CLE. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR DOOR LEFT ACTUATOR. OPERATIONAL CHECKS WERE GOOD.

Part: SKIN — CORRODED (CARGO DOOR)

SHV - DURING C-CHECK IT WAS FOUND THAT THE CARGO DOOR INNER SKIN HAD AREAS OF CORROSION. MAINTENANCE REMOVED THE CORROSION BY BLENDING AND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5230-01189. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,295 hrs · 4,634 cycles

FLT MX - ONT - WHILE PERFORMING INTERVALS 2A CHECK AT ONT AND PERFORMING AN OPERATIONAL CHECK FOR THE EMERGENCY LIGHTING SYSTEM, THE MX TECHNICIAN FOUND THAT THE EMERGENCY LIGHT IN GALLEY AREA WAS INOP. MX PERSONNEL REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY NR 2 LOCATED ABOVE THE SERVICE DOOR, OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE.

Part: PRESSURE SYSTEM — MALFUNCTIONED (CABIN) · airframe 7,893 hrs · 4,382 cycles

FLT 7657 - ZLO TO LAX - DURING CRUISE FLIGHT CREW REPORTED AIRCRAFT LOST PRESSURIZATION IN AUTO MODE AT FL 350. MX REMOVED AN REPLACED AUTO PRESSURIZATION CONTROLLER OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE

Part: UNKNOWN — SMOKE (CABIN) · airframe 7,871 hrs · 4,333 cycles

FLT 7682 - SLC TO LAX - DURING TAKEOFF ROLL FLIGHT CREW REPORTED SMOKE IN CABIN. CONTRACT MX PERFORMED RUN-OPS OF AIRCRAFT AND APU AT FULL FLOW PACKS. NO SMOKE FOUND AND NOTED. A/C WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. PROBLEM WAS CORRECTED WITHOUT EXCHANGING PARTS.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 5,179 hrs · 2,762 cycles

IAH - FLIGHT 2667, DURING PREFLIGHT INSPECTION THE PAX CABIN OVERHEAD CENTER FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 2,331 hrs · 1,249 cycles

IAH - FLIGHT 2510, THE CREW REPORTED A LAV SMOKE WARNING ON EICAS IMMEDIATELY AFTER T/O WITH NO SMOKE IN THE CABIN. THE WARNING CLEARED AFTER SEVERAL MINUTES WITH NO ACTION FROM THE CREW, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFICIENCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON FLIGHT 2960 THE CREW PERFORMED AN AIR RETURN DUE TO SMOKE IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SUBMITTED WITH CORRECT PART NAME AND NUMBER, CORRECTED PART CONDITION. RESUBMITTED FOLLOWING DELETION OF DUPLICATE RECORD IA005.

Part: OIL SYSTEM — OVERSERVICED (NR 2 ENGINE) · airframe 2,312 hrs · 1,237 cycles

IAH - FLIGHT 2891, DURING CLIMB THE CREW REPORTED SMOKE IN THE CABIN AND LAV WITH A SMOKE WARNING ON THE EICAS. THE CREW PERFORMED AN EMERGENCY DESCENT, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND THE NUMBER TWO ENGINE TO BE OVERSERVICED. MAINTENANCE REMOVED THE EXCESS OIL, REPLACED THE NR 2 ENGINE GENERATOR GARLOCK SEALS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — FAULTY (EMERGENCY LGIHT) · airframe 673 hrs · 361 cycles

EWR---CO2129, CREW REPORTED, EMERGENCY EXIT LOCATOR FOR EMERGENCY DOOR WILL NOT LIGHT UP.....MAINTENANCE REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY EXIT LOCATOR IAW EMB145 AMM #33-50-04, OPS.CHECKED GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 332 hrs · 185 cycles

CLE FLIGHT 3320 THE CREW REPORTED A MOMENTARY LAV SMOKE WARNING AFTER TAKEOFF. MAINTENANCE REPLACED THE LAV SMOKE DETECTOR AND THE OPERATIONAL CHECKS WERE GOOD.