N34111

Part: SKIN — DAMAGED (PAX DOOR) · airframe 43,228 hrs · 26,611 cycles

PAX DOOR EXT SKIN DAMAGED AT AFT LOWER VERTICAL EDGE. BLENDED OUT AFFECTED AREA IAW ETD2019-145-102337.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 43,228 hrs · 26,611 cycles

CARGO Z ANGLE SHOWS SIGNS OF CORROSION. R&R CARGO DOOR Z ANGLE.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 43,228 hrs · 26,611 cycles

AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 66 UPPER SUPPORT ANGLE IS CRACKED. R&R AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 66 UPPER SUPPORT ANGLE.

Part: TEE FITTING — CRACKED (FUSELAGE) · airframe 43,228 hrs · 26,611 cycles

AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 67 UPPER SUPPORT ANGLE IS CRACKED. R&R AFT CARG DOOR LOWER THRESHOLD T PROFILE AT FRME 67 UPPER SUPPORT ANGLE.

Part: TEE FITTING — BENT (FUSELAGE) · airframe 43,228 hrs · 26,611 cycles

AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 67 IS BENT. R&R AFT CARGO DOOR T PROFILE AT FRAME 67.

Part: TEE FITTING — BENT (FUSELAGE) · airframe 43,228 hrs · 26,611 cycles

AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 66 IS BENT. R&R AFT CARGO DOOR LOWER THRESHOLD T PROFILE AT FRAME 66.

Part: HINGE — CRACKED (TE FLAP) · airframe 43,228 hrs · 26,611 cycles

LT WING O/B FLAP SHROUD O/B HINGE HALF IS CRACKED AT BOTH ENDS. R&R THE LT O/B FLAP LOWER SHROUD O/B HINGE.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 42,735 hrs · 26,231 cycles

WING A/ICE FAIL W/ ICE COND I/ICE INOP. INSPECTED AND FOUND A LEAKING BLEED DUCT JOINT IN THE PYLON. RESECURED CLAMP AND LEAK CHECKED SYSTEM, NO LEAKS NOTED. PERFORMED A/ICE TEST WITH CREW. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (NLG) · airframe 42,363 hrs · 25,958 cycles

LANDING GEAR AIR/GROUND FAIL. R/R NOSE GROUND PROX SENSORS. OPS CHECK GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

AFT CARGO LT FLOOR SILL AFT OF CARGO DOOR HAVE LIGHT CORROSION AROUND NUTPLATES. INSTALLED NEW SILL FS 68 FS 74.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

MAIN CABIN LT FLOOR SILL HAVE CORROSION ON UPPERSURFACE FROM FR 31THRU 35. REMOVED AND REPLACED CABIN LT FLOOR SILL FROM FRAME 31-35 IAW SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

RT FLOOR SILL HAVE CORROSION ON UPPER SURFACE BETWEEN STA 56AND 27. REMOVED AND PEPLACED FLOOR SILL BETWEEN STA 56 ADN 57 IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

MAIN CABIN CENTER OMEGA BEAM SEAT TRACK HAVE CORROSION AT FRAME 52. REMOVE AND REPLACED CENTER OMEGA BEAM SEAT TRACK AT FRAME 52.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

MAIN CABIN LT FLOOR SILL HAVE CORROSION ON UPPER SURFACE FROM STA 42 THRU 47. REMOVED AND DRILLED NEW HOLES IN NEW LT FLOOR SILL AT FRAME 42-47 STARTED INSTALLING SILL LT AT FRAME 42 STILL NEEDS FASTENERS FINISHED INSTALLING SILL LT FRAME 42 IAW SRM51-40-02.

Part: RADIO ALTIMETER — CORRODED (CARGO BAY) · airframe 41,264 hrs · 25,065 cycles

AFT CARGO AFT RADIO ALTEMETER AT FRAME 68 HAS 3 BROKEN OFF RIVETS AND SIGN OF CORROSION BETWEEN BASE AND FUSELAGE SKIN. C/W ETD 2018-145-09121.

Part: RADIO ALTIMETER — CORRODED (CARGO BAY) · airframe 41,264 hrs · 25,065 cycles

AFT CARGO COMP FWD RADIO ALT AT FRAME 65 HAVE CORROSION BETWEEN CASE AND FUSELAGE SKIN. C/W ETD 2018-145-091731.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

REAR FUSELAGE LOWER SKIN CORROSION UNDER FWD AND AFT RADIO ALTIMETER. PERMANENT REPAIR WORK STARTED ON ETD2018-145-091731. WHEN AVAILABLE, DETAILS FOR THIS REPAIR WILL BE EMAILED TO [email protected], WITH SUBJECT 34111 SDR RAIA201808220001.

Part: SKIN — CHAFED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

REAR FUSELAGE 1 SKIN, CHAFING INSIDE RT PYLON. PERMANENT REPAIR. WORK STARTED ON ETD2018-145-090204. WHEN AVAILABLE, DETAILS FOR THIS REPAIR WILL BE EMAILED TO [email protected], WITH SUBJECT 34111 SDR RAIA201808210001.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

MAIN CABIN FLOOR STEPUP SUPPORT AT FRAME 23 HAVE CORROSION AT FRAME 23 HAVECORROSION ON FWD FACE BETWEEN CENTER AND RT OMEGA BEAM. REMOVED AND INSTALLED NEW STEP UP SUPPORT AT FRAME 23 IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

PASSENGER DOOR LOWER THRSHOLD AFT Z ANGLE NUTPLATE SUPPORT HAVE CORROSION AROUND NUTPLATE HOLES. REMOVED AND REPLACED PASSENGER DOOR LOWER THRESHOLD AFT Z ANGLE NUTPLATE SUPPORT IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

FRAME 16 RT SHEER CLIP IS CRACKED AT STR 15R. INSTALLED NEW SHEER CLIP AT STR 15 FRAME 16 IAW SRM 51-40-02.

Part: FITTING — CRACKED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

REMOVED CRACKED SHEAR CLIP. LOCATED DRILLED AND INSTALLED NEW SHEAR CLIP AT FRAME 57 LT AT STR 15.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

RT OMEGA BEAM LOWER LT SUPPORT IS CRACKED AT FRAME 47. REMOVE ANGLE, CUT DOWN ORIGINAL ANGLE IAW SRM 51-40-03 AND SRM-53-22-02. DRILLED UP FWD ANGLE, INSTALLED BOTH ANGLES IAW SRM 53-23-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,264 hrs · 25,065 cycles

COCKPIT FRAME 10 IS CRACKED BELOW LT DV WINDOW. REMOVED AND REPLACED FRAME 10 BELOW LT DV WINDOW.

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 41,264 hrs · 25,065 cycles

PASSENGER DOOR INTERIOR DOOR HANDLE SUPPORT BRACKET CRACKED. REMOVER AND REPLACED PASSENGER DOOR HANDLE SUPPORT.

Part: DUCT — NOT REPORTED (BLEED AIR SYS) · airframe 40,228 hrs · 24,190 cycles

BLEED 1 LEAK EICAS WARNING AND INSCRIPTION. DEFERRED BLEED 1 SYSTEM. ON 02/13/18, SWAPPED Y DUCTS OFF OF LT & RT PRSOV OPS TEST GOOD.

Part: LINE — LEAKING (NR 1 BLEED) · airframe 40,207 hrs · 24,178 cycles

NR 1 BLEED LEAK IN FLIGHT. R & R BLEED LINE UNDER CARGO FLOOR. TEE DUCT FROM NR 2 ENGINE BLEED, GROUND START TO FWD BLEED LINES. LEAK CHECKED AND OPS CHECKED GOOD.

Part: DUCT — LEAKING (PNEUMATIC SYS) · airframe 39,949 hrs · 23,970 cycles

BLEED 1 LEAK. SECURED THE LEAK AT DUCT 9, BLEED NR 1. OPS CHECKED WITH NO DEFECT NOTED.

Part: OXYGEN MASK — BROKEN (CAPTAIN'S) · airframe 39,940 hrs · 23,962 cycles

CAPTAIN`S OXYGEN MASK BROKEN. R & R THE OXYGEN MASK. OPS CHECKED GOOD.

Part: BOOT — LEAKING (NR 1 BLEED) · airframe 39,487 hrs · 23,594 cycles

BLEED 1 LEAK ON EICAS. SECURED THE BLEED DUCT COUPLING BOOTS, OPS AND LEAK CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,297 hrs · 23,426 cycles

LEFT AFT WING TO BODY FAIRING EXTERIOR FLOOD LIGHT IS INOPERATIVE. R & R THE BULB, OPS CHECKED GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,399 hrs · 21,861 cycles

CABIN ALTITUDE CLIMBED IN FLIGHT IN AUTO MANUAL NOT TRIED. INSPECTED OUTFLOW VALVE FITTING & CONNECTORS. INSPECTED FOR FOD CONDUCTED PRESSURIZATION CHECKED IN AUTO & MANUAL. OPS CHECKED GOOD AND NO DEFECTS NOTED.

Part: SEAL — PEELING (WINDOW) · airframe 36,397 hrs · 21,055 cycles

LOUD KNOCKING NOISE ON F/O'S WINDOW. F/O'S HUMP SEAL PEELING.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,871 hrs · 20,507 cycles

WING TO FUSELAGE FAIRING FWD EMERGENCY FLOOD LIGHT NR 4 INOPERATIVE. R & R WING TO FUSELAGE FAIRING FWD EMERGENCY FLOOD LIGHT BULB NR 4. OPS CHECK GOOD.

Part: ACM — OVERHEATED (NR 1) · airframe 35,341 hrs · 20,183 cycles

CREW REPORTED SMOKE IN CABIN WITH ODOR OF BURNING RUBBER. MAINTENANCE INSPECTED AND FOUND PACK 1 TO BE OVERHEATED AND INOPERATIVE. PACK 2 OPERATES NORMALLY, DEFERRED PACK 1. MAINTENANCE REPLACED NR 1 ACM, OPS CHECK GOOD, CLEARS DEFERRAL.

Part: RIB — CRACKED (FRAME 10) · airframe 34,088 hrs · 19,318 cycles

DURING C-CHECK THE RIB BELOW FRAME 10 AND STRINGER 1L - 1R WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A REPAIR IAW EC5310-01824. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — WORN (LT AILERON) · airframe 34,088 hrs · 19,318 cycles

DURING C-CHECK THE LT AILERON PCA FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE FITTING IAW EC5760-01044. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — GOUGED (RT AILERON) · airframe 34,088 hrs · 19,318 cycles

DURING C-CHECK, THE RT AILERON PCA FITTING WAS FOUND TO BE GOUGED. MAINTENANCE R & R THE FITTING IAW EC5760-01044, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — GOUGED (FRAME 7) · airframe 34,088 hrs · 19,318 cycles

DURING C-CHECK THE FUSELAGE SKIN AT FRAME 7 AND STRINGER 14L WAS FOUND TO BE GOUGED. MAINTENANCE BLENDED THE DAMAGE AND PERFORMED A DOUBLER REPAIR IAW SRM 53-11-01. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRUNNION — CRACKED (LT MLG) · airframe 34,088 hrs · 19,318 cycles

DURING C-CHECK THE LT MLG FORWARD TRUNNION WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE CRACKS BY REAMING THE BOLT HOLES IN THE TRUNNION IAW EC5750-01655. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 34,088 hrs · 19,318 cycles

DURING C-CHECK THE RT ENGINE FORWARD LOWER MOUNT YOKE FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5450-01124. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,689 hrs · 19,058 cycles

DURING CREW INSPECTION, THE LT EMERGENCY EXIT DOOR SIDEWALL LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 31,619 hrs · 17,716 cycles

THE CREW REPORTED A CARGO SMOKE MESSAGE ON EICAS. MAINTENANCE INSPECTED THE ACFT AND R & R THE FORWARD CARGO BAY SMOKE DETECTOR, OPS TESTED WITH NO DEFECTS.

Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK LT HORIZONTAL STAB L/E HAS CORROSION AROUND RIVET HEADS. MX PERFORMED REPAIR OF THE LT HORIZONTAL STAB L/E IAW EC5530-01116. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (ENGINE MOUNT) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, NR 1 ENGINE FWD LOWER MOUNT YOKE FWD EAR HAS VISUAL INDICATION OF CRACK BEYOND STOP DRILL. MX R & R RT 1 ENGINE FWD LOWER MOUNT YOKE FWD EAR IAW EC5450-01028. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ZONE 600) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK RT AILERON INBD AND OTBD HAT BUSHINGS MIGRATED AT OTBD PCA ROD. MX PERFORMED REPAIR ON RT AILERON INBD AND OTBD HAT BUSHINGS IAW AMM 27-10-00-400-801-A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, RIVET AT FRAME 78, STR 5L HAS VISUAL INDICATION OF CRACK. MX PERFORMED REPAIR TO FUSELAGE SKIN AT FRAME 78, STR 5L IAW EC5330-02674. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, STR SPLICE 21R CORRODED BETWEEN FRMS 13-14. MX PERFORMED REPAIR OF STR SPLICE 21R BETWEEN FRM 13-14 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK DMI 0841573 - LT FWD LWR ENGINE YOKE FWD FITTING CRACKED. MX R & R LT FWD LWR ENGINE YOKE FWD FITTING IAW EC5450-01028. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, LT UPPER SEAT TRACK SUPPORT HAS CORROSION (LEVEL 2 LOCAL) AT FRM 46. MX R & R LT UPPER SEAT TRACK SUPPORT AT FRM 42-47 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, RT UPPER SEAT TRACK SUPPORT AT FRM 50 HAS CORROSION. MX INSTALLED DOUBLER REPAIR AND FILLER ON RT UPPER SEAT TRACK SUPPORT AT FRM 50 IAW SRM 51-40-02 AND EC5320-01522, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK CORROSION DAMAGE AT INSIDE SURFACE OF FWD LOWER SKIN BETWEEN STR 21L-21R, BETWEEN FR 12-11. MX PERFORMED REPAIR OF FWD FUSELAGE SKIN LWR AT FRAME 11-12, STR 21L AND 21R IAW EC5330-02678. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, RT HORIZONTAL L/E HAS CORROSION AROUND RIVET HEADS. MX PERFORMED REPAIR ON RT HORIZ L/E IAW EC5510-01214. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — MIGRATED (SPEED BRAKE) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK RT SPEED BRAKE CENTER INBD HAT BUSHING MIGRATED. MX R & R RT SPEED BRAKE CENTER MOUNT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ZONE 600) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK RT SPOILER CENTER INBD HAT BUSHING MIGRATED. MX PERFORMED REPAIR TO RT SPOILER CENTER INBD HAT BUSHING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK CIRCUMFERENTIAL SPLICE CORRODED BETWEEN FRMS 13-14, STR 20L-19R. MX COMPLETED INSTALL OF SKIN SPLICE STRAP REPAIR AT FRM 13-14 STR 20L-19R IAW SRM 53-00-02, FIG 201. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK RT UPPER SEAT TRACK SUPPORT AT FRAME 46 HAS CORROSION. MX FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EC5320-01522, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, STR 21L CORRODED BETWEEN FRMS 12-13. MX R & R STR 21L BETWEEN FRM 9-13 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK RIVET AT FRAME 79, STR 3L HAS VISUAL INDICATION OF CRACK. MX PERFORMED REPAIR TO SKIN AT FRM 79, STR 3L IAW EC5330-02674. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK BAGGAGE DOOR CUT OUT LOWER BEAM CORRODED. MX PERFORMED INSTALLATION OF LWR BEAM CUT OUT ON BAGGAGE DOOR IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (LT WING SPOILER) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, LT SPOILER INBD FITTING OTBD HAT BUSHING MIGRATED. MX PERFORMED REPAIR ON LT SPOILER INBD FITTING, OTBD HAT BUSHING IAW EC5740-01152. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK CORROSION DAMAGE AT INSIDE SURFACE OF FWD LOWER SKIN BETWEEN STRS 21L-21R BETWEEN FRM 11-10. MX PERFORMED REPAIR ON FWD FUSELAGE 2 SKIN AT FRAME 10-11, STR 21L AND 21R IAW EC5330-02678. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, STR 21R CORRODED BETWEEN FRMS 12-13. MX R & R STR 21R BETWEEN FRM 9-13 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, STRINGER SPLICE 21L CORRODED BETWEEN FRMS 13-14. MX PERFORMED REPAIR AND INSTALLATION OF STR SPLICE 21L BETWEEN FRM 13-14 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK RIVET AT FRAME 77, STR 5L HAS VISUAL INDICATION OF CRACK. MX PERFORMED REPAIR TO SKIN AT FRM 77, STR 5L IAW EC5330-02674. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 28,802 hrs · 15,917 cycles

DURING C-CHECK, RIVET AT FRAME 79, STR 5L HAS VISUAL INDICATION OF CRACK. MX PERFORMED REPAIR TO FUSELAGE SKIN AT FRM 79, STR 5L RIVETS IAW EC5330-02674. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,523 hrs · 15,076 cycles

DURING TAXI THE CREW REPORTED THAT THE EMERGENCY LIGHTS GO ON AND OFF BY THEMSELVES WITH THE SWITCH IN THE "ARM" POSITION. THE CREW RETURNED TO THE GATE WHERE MX R & R THE F/A CONTROL PANEL, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — FAULTY (NR 2) · airframe 25,512 hrs · 13,778 cycles

THE CREW REPORTED A LAV SMOKE EICAS MESSAGE FOR 2 MINUTES THEN WENT AWAY. NO INDICATION OF FIRE OBSERVED BY THE F/A. MAINTENANCE INSPECTED AND RAN BOTH ENGINES. FOUND NR 2 ENGINE MAKES SMOKE IN THE CABIN THRU BLEED NR 2. THE NR 2 ENGINE WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD.

Part: DUCT — LOOSE (NR 2 PACK) · airframe 25,356 hrs · 13,681 cycles

ORD FLT 6147 - THE CREW REPORTED A LAV SMOKE EICAS WARNING MESSAGE ALSO REPORTED SMOKE IN CABIN FROM ROW 5-7 CEILING AND WALL. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESECURED THE NR 2 PACK DUCT. RAN BOTH ENGINES AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAPPER VALVE — LEAKING (RT WING) · airframe 25,015 hrs · 13,465 cycles

MEM - FLIGHT 2233, THE CREW REPORTED A FUEL LEAK FROM THE RIGHT WING ON TAKEOFF. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAPPER VALE AT RIB 19, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DAU — MALFUNCTIONED (NR 2) · airframe 24,469 hrs · 13,080 cycles

FLIGHT 2332 - EWR - FLIGHT CREW REPORTED BAGGAGE SMOKE DETECTOR DID NOT TEST. EWR MX RE-RACKED NR 2 DAU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ANTI-ICE VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 24,415 hrs · 13,053 cycles

IAH - FLIGHT 2027, DURING CLIMB THE CREW REPORTED AN E1 ANTI-ICE FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ENGINE ONE ANTI-ICE VALVE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — FAULTY (NR 1 ENGINE) · airframe 20,246 hrs · 1,078 cycles

IAH - FLIGHT 2333, THE CREW REPORTED ABNORMAL OIL PRESSURE NUMBER ONE ENGINE AT CRUISE ALTITUDE FL350 WITH 135 PSI. THE OIL PRESSURE REMAINED IN THE AMBER RANGE FOR 8 MINUTES, AND DURING DESCENT AT 6000FT THE OIL PRESSURE WENT BACK INTO THE AMBER RANGE FOR SIX MINUTES & 130 PSI, AND NOTED THAT THE OIL PRESSURE NEVER WENT INTO THE RED RANGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE EIS HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,174 hrs · 10,209 cycles

TYS - A/C IS IN C-CHECK WHEN INSPECTION FOUND THE RT FLOOR SILL CORRODED BETWEEN FRAMES 41 AND 48. MAINTENANCE REMOVED AND REPLACED THE FLOOR SILL IAW EMB 145XR SRM 51-20-03, 06, 02 AND CPM 51-21-04, 05, 06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. THE AREA WAS OUT OF THE MFG'S LIMITS.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,174 hrs · 10,209 cycles

TYS - A/C IS IN FOR A C-CHECK WHEN MAINTENANCE FOUND CORROSION AT THE BAGGAGE DOOR SILL FWD END. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR LOWER SILL. CORROSION WAS OUTSIDE OF THE MFG'S LIMITS. A/C WILL BE RELEASED AT THE END OF THE CHECK.

Part: RMU — INOPERATIVE (NR 2) · airframe 18,898 hrs · 10,062 cycles

IAH - FLIGHT 2492 - THE CREW REPORTED DURING CRUISE THAT THE NUMBER TWO RMU FAILED, WITH NO TRANSPONDER AND RADIO STUCK. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER TWO INTEGRATED COMM/TRANSPONDER UNIT, OPERATIONALLY TESTED ALL RADIOS AND TRANSPONDER WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 18,036 hrs · 9,597 cycles

DURING ROUTINE MAINTENANCE THE RIGHT FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 18,036 hrs · 9,597 cycles

DURING ROUTINE MAINTENANCE THE LEFT AND RIGHT OVERWING EMERGENCY LIGHT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: FUSE — BLOWN (CABIN) · airframe 17,648 hrs · 9,394 cycles

THE EXTERIOR RT AND LT OVERWING EMERGENCY LIGHTS WERE FOUND INOP. MX R&R THE TRAY FUSE AT THE NR 4 EMERGENCY BATTERY TRAY IAW RADIANT POWER CORP. CMM 25-60-03. OPS CHECK GOOD AND WAS RELEASED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN)

DURING ROUTINE MX THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD.

Part: CHARGER — DEFECTIVE (EMERGENCY LIGHTS)

FLIGHT 2391 - EWR - DURING ROUTINE MAINTENANCE, EWR MAINTENANCE FOUND MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE AT OVERWING EXITS. MAINTENANCE REMOVED AND REPLACED NR 3 EMERGENCY BATTERY CHARGER ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 13,951 hrs · 7,452 cycles

RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND NR 2 CEILING PANEL EMERGENCY LIGHT INOPERATIVE. MX FOUND SPLICE (SP9032) DEFECTIVE. MX REPAIRED SPLICE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 12,847 hrs · 6,869 cycles

IAH - FLIGHT 2556, DURING TAKEOFF THE CREW REPORTED A BAGGAGE SMOKE WARNING. THE FIRE EXTINGUISHERS WERE DISCHARGED AS A PRECAUTION, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NR 2 CARGO SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 12,847 hrs · 6,869 cycles

IAH - FLIGHT 2556, DURING TAKEOFF THE CREW REPORTED A BAGGAGE SMOKE WARNING. THE FIRE EXTINGUISHERS WERE DISCHARGED AS A PRECAUTION, AND THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NR 1 CARGO SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERCVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,777 hrs · 6,836 cycles

IAH - FLIGHT 2100, THE CREW REPORTED A STRONG ODOR OF FUEL JUST AFTER APU START. MAINTENANCE OPERATIONALLY CHECKED THE APU & PACKS SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR · airframe 12,770 hrs · 6,832 cycles

IAH FLIGHT 2139, THE CREW REPORTED A STRONG ODOR OF FUEL DURING APU STARTS. MAINTENANCE OPERATIONALLY CHECKED THE APU SEVERAL TIMES WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,546 hrs · 6,703 cycles

FLT 2130 - OMA - CREW REPORTED EMERGENCY EXIT SIGN OVER 12BC SEAT DOOR INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER NR 5 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,989 hrs · 2,637 cycles

DURING VISUAL INSPECTION AT C-CHECK THE CENTER OMEGA BEAM WAS CORRORDED AT FRAME 20. REMOVED AND REPLACED THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: LINE — BROKEN (CABIN AREA) · airframe 3,040 hrs · 1,601 cycles

CREW REPORTED, BLEED LEAK IN FLIGHT, LOUD DECOMPRESSION, AND ODOR OF SMOKE FROM NR 2 ENGINE. PERFORMED EMERGENCY LANDING IN NEWARK, AIRCRAFT LANDED UNEVENTFULLY. DURING TROUBLESHOOTING MAINTENANCE FOUND BLEED AIR TUBING ASSEMBLY WHICH CONTROLS NR 2 ENGINE THERMOSTAT (HT)&(LT) FORWARD AUTO LATCHING COUPLING TO BE BROKEN. REMOVED AND REPLACED NR 2 BLEED DUCT AT CARGO BAY POSITION UNDER FLOOR IAW EMB145 MM 36-11-09, OPS AND LEAK CHECKED GOOD OF BLEED SYSTEM IAW EMB145 MM 36-00-00. PRESSURIZATION CHECKED GOOD IAW EMB145 MM 21-31-00. INSTALLED FLOOR PANELS 272AF AND 272BF. AIRCRAFT RETURNED TO SERVICE.

Part: CONTACTOR — FAULTY (COCKPIT) · airframe 1,139 hrs · 595 cycles

EWR---CO2853, CREW REPORTED, STRONG ELECTRICAL ODOR IN COCKPIT. MAINTENANCE REMOVED AND REPLACED ESSENTIAL BUSS CONTACTOR (EBC) IAW EMB 145 XR MM 24-60-03. OPS CHECKED GOOD. NO ELECTRICAL ODOR SMELL WAS FOUND AT THIS POINT. AIRCRAFT RETURNED TO SERVICE.