N13123

Part: SENSOR — FAILED (OIL TEMP) · airframe 43,312 hrs · 26,508 cycles

E2 HI OIL TEMP ON FINAL APPROACH, E2 TEMP SHOT TO 218C, CREW REDUCED TLA'S TO IDLE AND TEMP WENT INTO GREEN RANGE. ON 2ND ATTEMPT E2 OIL TEMP OIL TEMP WENT IMMEDIATELY INTO RED BAND AND DID NOT COME DOWN WHEN TLA'S REDUCED TO IDLE. POST 1 MINUTE CREW SHUT DOWN E2 AND LANDED WITH ONE ENG. ALL OTHER ENG PARAMETERS NORMAL INDICATIONS--- SWAPPED OIL TEMP SENSORS SIDE TO SIDE, #2 OPS CHECKED GOOD, SO THEN REPLACED #1 OIL TEMP SENSOR OPS CHECK GOOD

Part: SENSOR — INOPERATIVE (ENGINE OIL) · airframe 43,312 hrs · 26,508 cycles

E2 HI OIL TEMP ON FINAL APPROACH, E2 TEMP SHOT TO 218C, CREW REDUCED TLA'S TO IDLE AND TEMP WNET INTO GREEN RANGE. ON 2ND ATTEMPT, E2 OIL TEMP WENT IMMEDIATELY INTO RED BAND AND DID NOT COME DOWN WHEN TLA'S REDUCED TO IDLE. POST 1 MINUTE , CREW SHUT DOWN E2 AND LANDED WITH ONE ENGINE. ALL OTHER ENGINE PARAMETERS NORMAL INDICATIONS. SWAPPED OIL TEMP SENSORS SIDE TO SIDE. #2 OPS CHECK GOOD. REPLACED #1 OIL TEMP SENSOR. OPS CHECK GOOD.

Part: SKIN — CHAFED (FUSELAGE) · airframe 42,054 hrs · 25,524 cycles

LT FUSELAGE SKIN INSIDE PYLON ACCESS PANEL 424DB IS CHAFFED FROM LANYARD. REMOVED AND REPAIRED FUSELAGE SKIN IN PYLON ACCESS PANEL 424DB.

Part: DOOR FRAME — CORRODED (FRAME 65) · airframe 42,054 hrs · 25,524 cycles

CORROSION ON LH SIDE OF CARGO DOOR FRAME AT FR 65 AROUND NUT PLATE HOLE- REMOVED CORREDED DOOR FRAME STRUCTURE AT FR 65 LH SIDE AND INSTALLED NEW FRAME STRUCTURE.

Part: HOLDER — CRACKED (CARGO DOOR) · airframe 42,054 hrs · 25,524 cycles

CARGO BAY DOOR ROD HOLDER IS CRACKED....R&R CARGO BAY DOOR ROD HOLDER

Part: SHEAR TIE — CRACKED (FRAME 16) · airframe 42,054 hrs · 25,524 cycles

RT SHEAR TIE AT FRAME 16, STRINGER 15 WAS CRACKED. REMOVED AND REPLACED THE SHEAR TIE

Part: SHEAR TIE — CRACKED (FRAME 15) · airframe 42,054 hrs · 25,524 cycles

RT SHEAR TIE AT FRAME 15, STRINGER 15 WAS CRACKED, REMOVED AND REPLACED THE SHEAR TIE.

Part: STRINGER — CRACKED (FRAME 20) · airframe 42,054 hrs · 25,524 cycles

L/H FR 20 STR 3 IS CRACKED....R&R L/H FR 20 STR 3 IS CRACKED.

Part: BRACKET — CRACKED (FRAMES 16-17) · airframe 42,054 hrs · 25,524 cycles

CENTER OMEGA BEAM GUSSET BT FR 16-17 ANGLE BRACKET IS CRACKED....R&R CENTER OMEGA BEAM ANGLE BRACKET AT FR 16-17

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 42,054 hrs · 25,524 cycles

CARGO DOOR AFT TORSION BAR LOWER & UPPER SUPPORT IS CRACKED. REMOVED CARGO DOOR AFT TORSION BAR LOWER AND UPPER SUPPORT. INSTALLED CARGO DOOR AFT TORSION BAR LOWER AND UPPER SUPPORT.

Part: SHEAR TIE — CRACKED (FRAME 26) · airframe 42,054 hrs · 25,524 cycles

RIGHT SHEAR TIE AT FRAME 26, STRINGER 15 WAS CRACKED. R & R THE SHEAR TIE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 36-41) · airframe 42,054 hrs · 25,524 cycles

LH FL SILL BT FR 36-41 IS CORRODED. REMOVED & REPLACED LH FL SILL BT FRAME 36-41.

Part: FLOOR SUPPORT — CORRODED (FRAMES 58-60) · airframe 42,054 hrs · 25,524 cycles

FL SILL ON CENTER & LH OMEGA BEAM BT FR 60-58 IS CORRODED. R&R THE CENTER OMEGA BEAM GUSSET FROM FR 58-60. R&R THE L/H OMEGA BEAM GUSSET FROM FR 58-60.

Part: STRINGER — CRACKED (FRAME 20) · airframe 42,054 hrs · 25,524 cycles

L/H FR 20 STR 3 IS CRACKED....R&R L/H FR 20 STR 3 IS CRACKED.

Part: BRACKET — CORRODED (FRAME 17) · airframe 42,054 hrs · 25,524 cycles

MAIN DOOR THRESHOLD FWD U SHAPED BRACKET IS CORRODED AT FRAME 17. REMOVED & REPLACED THE BRACKET.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 42,054 hrs · 25,524 cycles

SHEAR CLIP ABOVE CARGO DOOR AT FR 68 IS CRACKED....REMOVED AND INSTALLED SHEAR CLIP AT FR 68

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 42,054 hrs · 25,524 cycles

LH SHEAR CLIP AT FR 73 BT STR 9 & 10 IS CRACKED. REMOVED SHEAR CLIP AND PICKED UP HOLES IN NEW CLIP. INSTALLED SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FRAME 71) · airframe 42,054 hrs · 25,524 cycles

L/H SHEAR CLIP AT FR 71 STR 17 IS CRACKED. REMOVED AND REPLACED SHEAR CLIP AT FR71 STR 17 L/H

Part: GUSSET — CRACKED (FRAME 16) · airframe 42,054 hrs · 25,524 cycles

L/H OMEGA BEAM GUSSET AT FR 16 HAS CRACKED BRACKET. REMOVED AND RAPLACED L/H OMEGA BEAM GUSSET AT FR 16.

Part: ANGLE — CRACKED (FRAME 48) · airframe 42,054 hrs · 25,524 cycles

LH OVERWING ANGLE AT FR 48 CRACKED. REMOVED LH OVERWING ANGLE AT FR 48, DRILLED NEW ANGLE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 36-41) · airframe 42,054 hrs · 25,524 cycles

RH FL SILL BT FR 36-41 IS CORRODED, R&R RH FL SILL BT FR 36-41.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 42,054 hrs · 25,524 cycles

LH FR 73 BT STR 15-16 CRACKED SHEAR CLIP. REMOVED SHEAR CLIP. INSTALLED NEW SHEAR CLIP FR 73 STR 15-16

Part: FLOOR SUPPORT — CORRODED (FRAME 43) · airframe 42,054 hrs · 25,524 cycles

RH FL SILL AT FR 46 IS CORRODED. REMOVED RH FLOOR SILL. PICKED UP HOLES AND PARTIALLY INSTALLED RH FL SILL. INSTALLED FLOOR SILL.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-27) · airframe 42,054 hrs · 25,524 cycles

L/H SILL BT FR 24-27 IS CORRODE....R&R L/H FLOOR SIL AT FR 24-27

Part: FLOOR SUPPORT — CORRODED (FRAMES 30-35) · airframe 42,054 hrs · 25,524 cycles

LEFT FLOOR SILL BT FR 30-35 IS CORRODED....R&R L/H FL SILL BT 30-35.

Part: FLOOR SUPPORT — CORRODED (FRAMES 55-60) · airframe 42,054 hrs · 25,524 cycles

LH FL SILL BT FR 55-60 IS CORRODED- R&R THE L/H FLOOR SILL FROM FR 55-60.

Part: SHEAR TIE — CRACKED (FRAME 65) · airframe 42,054 hrs · 25,524 cycles

LH SHEAR CLIP AT FR 65 STR 18 IS CRACKED. R & R LT SHEAR CLIP AT FR 65 STR 18.

Part: FLOOR SUPPORT — CORRODED (FRAMES 23-29) · airframe 42,054 hrs · 25,524 cycles

RH FL SILL BT FR 23-29 IS CORRODED. REMOVED SILL, MATCH DRILLED. INSTALLED FLOOR SILL.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 42,054 hrs · 25,524 cycles

RH SHEAR TIE AT FRAME 24, STRINGER 15 IS CRACKED. R & R THE RT SHEAR TIE.

Part: ANGLE — CRACKED (FRAME 46) · airframe 42,054 hrs · 25,524 cycles

LEFT OVERWING ANGLE AT FR 46 CRACKED- REMOVED AND FAB NEW ANGLE. INSTALLED ANGLE, STILL REQUIRES 2 HI-LOK TO BE INSTALLED AND NUTPLATE HOLES TO BE PICKED UP FROM FAIRING. INSTALLED HI-LOKS, APPLIED SEALANT AND PICKED UP NUT PLATE HOLES.

Part: ANGLE — CRACKED (FRAME 41) · airframe 42,054 hrs · 25,524 cycles

R/H OVERWING ANGLE AT FR 41 CRACKED.... R&R R/H OVERWING ANGLE AT FR 41.

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 42,054 hrs · 25,524 cycles

LH SHEAR CLIP AT FR 72 AT STR 17 IS CRACKED. R&R LH SHEAR CLIP AT FR 72

Part: FRAME — CRACKED (FRM 10) · airframe 42,054 hrs · 25,524 cycles

LEFT FRAME 10 WAS CRACKED. R & R FRAME 10.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-68) · airframe 42,054 hrs · 25,524 cycles

RH CARGO BAY FL SILL BT 65-68 IS CORRODED- REMOVED RH CARGO BAY FL SILL AND PICKED UP THE HOLES ON NEW PART, NEEDS INSTALLED ON A/C. INSTALLED RH CARGO BAY FL SILL.

Part: ENGINE — HUNG START (NR 2) · airframe 40,870 hrs · 24,587 cycles

E2 HUNG START WITH SMOKE COMING FROM ENGINE DURING START UP. RAN BOTH ENGINES, #1 AND #2, OPS CHECK GOOD AT THIS TIME.

Part: SKIN — CRACKED (LT WING) · airframe 40,611 hrs · 24,368 cycles

FOUND 2 1/2 INCH CRACK ON BOTTOM OF LT WING 8 INCHES BEHIND PANEL 531DB (FOUND CRACK TO BE SEEPING FUEL). C/W RIB 9 LEFT WING LOWER SKIN REPAIR REFERENCE EO EMB145-57-019-0.

Part: DOOR — LACK OF LUBE (MAIN CABIN)

MAIN CABIN DOOR STICKING. CLEANED AND LUBED MAIN CABIN DOOR. OPS CHECKED GOOD.

Part: UNKNOWN — LEAKING (LT WING) · airframe 40,144 hrs · 23,977 cycles

FUEL LEAK COMING FROM LEFT WING IN FLT. INSPECTED THE LT WING AND FOUND FUEL TO BE IN A TYPE 4 AREA AND THE LEAK CLASSIFIED AS A STAIN IN THE LT WING STUB.

Part: BUTTON — FAILED (PITCH TRIM) · airframe 39,714 hrs · 23,621 cycles

MAIN PITCH TRIM INOPERATIVE IN FLIGHT. R & R MAIN PITCH TRIM SYSTEM CUTOUT PUSH BUTTON AND PERFORMED OPS CHECK GOOD.

Part: DOOR — LOOSE · airframe 39,423 hrs · 23,388 cycles

EXCESSIVE VIBRATION IN FLIGHT DURING ALL PHASES OF OPERATIONS WITH FLAPS SET AT ZERO. ONCE FLAPPS ARE MOVED ALL VIBRATION DISAPPEAS. VIBRATIONS FELT THROUGHT FLIGHT DECK AND GALLEY. VIBRATION IS ACCOMPANIED BY LOW RUMBLING SOUND. FOUND THE LT DIP STICK PANEL DOOR TO BE LOOSE.

Part: FLUID — LOW (HYDRAULIC SYS) · airframe 32,923 hrs · 22,969 cycles

HYDRAULIC SYSTEM 1 REQUIRES SERVICE HYD ONE LOW QUANTITY ADVISORY MESSAGE. SERVICE HYDRAULIC SYSTEM 1 TO FULL, PERFORMED GVI OF AIRCRAFT HYDRAULIC SYSTEM LINES AND ACTUATORS NONE FOUND RAN ENG OPERATED FLIGHT CONTROLS AND BRAKES NO LEAKS FOUND.

Part: ACTUATOR — MALFUNCTIONED (NLG DOOR) · airframe 37,866 hrs · 22,072 cycles

RH MLG DIDN’T RETRACT AFTER TAKE OFF. THE ACFT WAS DETERMINED TO BE SAFE FOR OPERATION IAW MX-017. R & R NOSE LANDING GEAR DOOR LT ACTUATOR AND NOSE GEAR PROXIMITY SWITCH. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,627 hrs · 20,269 cycles

CEILING EMERGENCY EXIT LIGHT AT ROW 7, LIGHT NR 16B, IS INOPERATIVE. R & R BATTERY POWER SUPPLY LOCATED IN THE 2 POSITION. OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,340 hrs · 20,031 cycles

NR 9 COCKPIT STEP EXIT INDENTIFIER LIGHT INOPERATIVE. R & R EMERGENCY LIGHT DC/AC INVERTER. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 35,340 hrs · 20,031 cycles

CABIN EMERGENCY LIGHTS NR 15 & NR 19 WILL NOT ILLUMINATE. INSPECTED AND FOUND LOOSE CONNECTION. SECURED, OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,340 hrs · 20,031 cycles

NR 2 EMERGENCY LIGHT BATTERY INOPERATIVE. R & R 2 EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 34,915 hrs · 19,717 cycles

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

Part: MOUNT — CRACKED (LT ENGINE) · airframe 34,915 hrs · 19,717 cycles

DURING C-CHECK THE LT ENGINE FORWARD LOWER MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01153. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,467 hrs · 19,409 cycles

DURING MAINTENANCE INSPECTION, THE FWD FACING OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 6 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,898 hrs · 16,541 cycles

DURING MX INSPECTION, THE NR 2 EMERGENCY LIGHT BATTERY TRAY WAS FOUND INOPERATIVE. MX R & R THE NR 2 EMERGENCY LIGHT BATTERY CHARGER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 100) · airframe 29,443 hrs · 16,259 cycles

DURING C-CHECK FUSELAGE CRACKED AT DENT FRAME 17-18, STRINGER 21L-21R VERIFIED WITH EDDY CURRENT. MX PERFORMED REPAIR AT FRAME 17-18, STRINGER 21L-21R IAW EC5320-01802. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (ZONE 200) · airframe 29,443 hrs · 16,259 cycles

DURING C-CHECK, FRAME 25 BETWEEN STRINGERS 15-16R IS CRACKED AT TOP FLOOR SILL RIVET. MX PERFORMED REPAIR OF FRAME 25 BETWEEN STRINGER 15R-16R IAW SRM 53-00-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 29,190 hrs · 16,098 cycles

DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT WHEN TURNING OFF THE EMERGENCY LIGHTS WITH EITHER THE APU ON OR GCU SELECTED, CAUSES THE EMERGENCY LIGHTS TO COME ON. MX INSPECTED THE ACFT AND R & R THE NR ONE EMERGENCY LIGHT BATTERY PACK POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 29,179 hrs · 16,092 cycles

DURING POST-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD ON; Y TURN OFF IN THE ARM POSITION. MX R & R THE NR 1 EMERGENCY LIGHT BATTERY PACK, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 28,844 hrs · 15,881 cycles

DURING MX INSPECTION, THE AFT CABIN FLASHLIGHT WAS FOUND INOPERATIVE. MX R & R THE BATTERY PACK WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 28,053 hrs · 15,380 cycles

THE CREW REPORTED A BAGGAGE SMOKE INDICATION DURING CLIMB. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ACFT INSPECTED WITH NO EVIDENCE OF SMOKE FOUND. MX OPS TESTED THE BAGGAGE SMOKE DETECTION SYS WITH NO DEFECTS NOTED, REMOVED THE MEL AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 1) · airframe 26,263 hrs · 14,215 cycles

THE CREW REPORTED SMOKE IN THE COCKPIT. MX REPLACED THE NR 1 ENGINE. OPS CHECKS WERE GOOD.

Part: CONNECTOR — MISALIGNED (ZONE 100) · airframe 23,968 hrs · 12,802 cycles

IAH - FLIGHT 2020, DURING CRUISE FLIGHT THE CREW REPORTED AN SPS ADVANCE MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND FOUND CONNECTOR SP7148 TO BE MISALIGNED, MAINTENANCE CORRECTLY INSTALLED THE THE CONNECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — DEFECTIVE (HORIZ STAB) · airframe 23,763 hrs · 12,689 cycles

IAH - FLIGHT 2470, THE CREW REPORTED THE BACKUP PITCH TRIM TO BE INOPERATIVE DURING TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER ACTUATOR, OPERATIONALLY TESTED WITH NO DEFECTS, TEST FLEW SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LINE — LOOSE (CREW O2) · airframe 22,213 hrs · 11,845 cycles

EWR - FLT 3113 THE CREW REPORTED THE CREW OXYGEN SYSTEM WAS LEAKING DOWN IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A LOOSE LINE AT THE FIRST OFFICER'S OXYGEN MASK STOWAGE BOX. TIGHTENED LINE AND OPERATIONAL CHECKS WERE GOOD.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 20,636 hrs · 10,993 cycles

IAH - FLIGHT 2352, THE CREW REPORTED A FUEL SMELL AT HIGH POWER SETTINGS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, CONFIRMED THE ODOR TO BE COMING FROM ENGINE ONE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,190 hrs · 10,770 cycles

FLIGHT 2718 - EWR - FLIGHT CREW REPORTED AFTER T/O, APU BLEED SELECTED, MOMENTARY SMELL OF GAS. EWR MX RAN APU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY, COULD NOT DUPLICATE ANY SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 19,812 hrs · 10,557 cycles

CLE FLT 2586 THE CREW REPORTED A FUEL SMELL ON TAKEOFF ROLL. THE CONFIG WAS APU BLEED ON, ENGINE BLEEDS OFF, PACKS ON. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS ON APU WITH PACKS ON. NO FUEL SMELL WAS NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK VISUAL INDICATION OF CRACKS AROUND RIVET HEADS AT EXTERNAL FUSELAGE FRAME 79 STR 7L & 8L. MAINTENANCE REPAIR OF CRACKS AROUND RIVET HEADS AT EXTERNAL FUSELAGE FR 79 STR 7L & 8L IAW EMB-145XR EC5330-01985. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — CORRODED (RUDDER) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK RUDDER II UPPER CENTER FITTING HAT BUSHINGS CORRODED (LEVEL 2 LOCAL) AND WORN. MAINTENANCE REMOVED AND REPLACED RUDDER II UPPER CENTER HINGE FITTING AND BUSHINGS IAW EMB145 SRM 51-40-02 AND EMB-145XR AMM 20-10-08. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT AT FRAME 44 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF LT UPPER SEAT TRACK SUPPORT AT FRAME 44 IAW EMB-145XR EC5320-01487. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (RUDDER) · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK RUDDER II UPPER HINGE FITTING HAT BUSHINGS WORN. MAINTENANCE REMOVED AND REPLACED RUDDER II UPPER HINGE FITTING AND BUSHINGS IAW EMB-145 SRM 55-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK CHAFED DAMAGE ON STR 2L BETWEEN FRM'S 20-21. MAINTENANCE PERFORMED WORK ON CHAFED DAMAGE ON STR 2L BETWEEN FRM'S 20-21 IAW EMB-145 EC5310-01481. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT AT FRM 43 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF RT UPPER SEAT TRACK SUPPORT AT FRM 43 IAW EMB-145 EC5320-01487. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT AT FRAME 43 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED LT UPPER SEAT TRACK SUPPORT AT FRAME 43 IAW EMB-145XR EC5320-01487 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK LT OMEGA BEAM BETWEEN FRAMES 24-28 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED LT OMEGA BEAM FRAMES 24-28 IAW EMB-145 SRM 53-00-10 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT AT FRAME 45 CORRODED (LEVEL 2 LOCAL). MAINTENANCE REPAIRED LT UPPER SEAT TRACK SUPPORT AT FRAME 45 IAW EMB-145XR EC 5320-01487 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 20 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM AT FRAMES 18-25 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT AT FRAME 50 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF RT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EMB-145 EC5320-01487. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM AT FRAME 49 CORRODED (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR OF CENTER OMEGA BEAM AT FRAME 49 IAW EMB-145XR EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,083 hrs · 10,179 cycles

SHV - DURING C-CHECK MAIN DOOR AFT CUTOUT (FRM 18) HAS CORROSION (LEVEL 2 LOCAL) AROUND SCREW HOLES BETWEEN STR 14L-15L. MAINTENANCE PERFORMED REPAIR ON MAIN DOOR AFT CUTOUT (FRM 18)BETWEEN STR'S 14L-15L IAW EMB-145XR EC5310-01482. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 19,078 hrs · 10,175 cycles

CLE - FLT 2006 - THE CREW REPORTED THE F/A FLASHLIGHT BRACKET WAS BROKEN. MAINTENANCE INSPECTED AND REPLACED THE F/A FLASHLIGHT BRACKET. OPERATIONAL CHECKS WERE GOOD.

Part: DETECTION SYS — MALFUNCTIONED (CARGO BAY) · airframe 19,059 hrs · 10,163 cycles

CME - FLIGHT 2020 - THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON 3 MILE FINAL. THE AIRCRAFT LANDED AT CME WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT WITH NO EVIDENCE OF SMOKE OR FIRE DETECTED, AND PLACE THE AIRCRAFT ON MEL 26-15-00 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON FLIGHT 2021, THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE BAGGAGE COMPARTMENT FIRE BOTTLES, OPERATIONALLY TESTED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DAU — FAILED · airframe 18,889 hrs · 10,079 cycles

IAH - FLIGHT 2066, THE CREW REPORTED THAT THE DAU 2A FAILED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DAU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,901 hrs · 9,536 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND ROW 12 CEILING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 17,900 hrs · 9,535 cycles

FLIGHT 2105 - GRR - FLIGHT CREW ABORTED TAKEOFF DUE TO SMOKE IN THE CABIN. SMOKE FOUND TO BE COMING FROM PACK NR 2. EWR MX REMOVED AND REPLACED ENGINE NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR FILE OPEN.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 17,200 hrs · 9,164 cycles

SMOKE NOTICED IN CABIN AND LAV SMOKE INDICATION ON EICAS AFTER T/O. R&R ENG NR 1 "0" CARBON SEAL IAW RRMM 72-25-25 & 77-21-10. OPS AND LEAK CHECK GOOD, ACFT RELEASED AND RETURNED TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (CABIN) · airframe 16,090 hrs · 8,534 cycles

FLIGHT 2123 EWR FLIGHT CREW REPORTED SMELL OF SMOKE NEAR SEAT 1A. EWR MX R&R LIGHT CONTROL MODULE IAW EMB 145 AMM 33-21-01 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 16,004 hrs · 8,491 cycles

FLIGHT 2897 - EWR - FLIGHT CREW REPORTED STRONG FUEL ODOR DURING CLIMBING. ODOR WENT AWAY AFTER APU SHUT DOWN. NO ODOR NOTICED ON CRUISE. EWR MAINTENANCE PERFORMED OPERATIONAL CHECK OF APU SUCCESSFULLY. NO ODOR WAS NOTICED. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 14,391 hrs · 7,708 cycles

IAH - FLIGHT 2945. THE CREW REPORTED A DISTINCT THUMPING SOUND ON APPROACH WITH THE GEAR UP AND DOWN ON FINAL. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOWNLOCK HARNESS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 14,391 hrs · 7,708 cycles

IAH - FLIGHT 2945 - THE CREW REPORTED A DISTINCT THUMPING SOUND ON APPROACH WITH THE GEAR UP AND DOWN ON FINAL. THE AIRCRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOWNLOCK PROX SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MODULE — INOPERATIVE (CABIN PRESSURE) · airframe 14,277 hrs · 7,652 cycles

IAH - FLIGHT 2926, THE CREW REPORTED CABIN DECOMPRESSED AT FL340, CABIN PRESSURE FLUCTUATED BETWEEN 7200' & 14,200' CABIN ALT, OXYGEN MASKS DEPLOYED AUTOMATICALLY. THE CREW PERFORMED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE CABIN PRESSURE ACQUISITION MODULE (CPAM), OPERATIONALLY CHECKED WITH NO DEFECTS, THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — ACTIVATED (CARGO BAY) · airframe 14,125 hrs · 7,571 cycles

CME - FLIGHT 2021 THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON EICAS AND THE BAGGAGE EXTINGUISHER BUTTON WAS ILLUMINATED. THE AIRCRAFT WAS PLACED ON MEL 21-22-06 CTL 136538 CAT C, AND RELEASED FOR SERVICE. THE AIRCRAFT CAME TO IAH ON FLIGHT 2021 WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BAGGAGE SMOKE DETECTORS SYSTEM WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLEED VALVE — FAULTY (APU) · airframe 14,074 hrs · 7,547 cycles

IAH - FLIGHT 2025, THE CREW REPORTED THAT THE APU CAUSES FUEL SMELL IN THE CABIN. MAINTENANCE PLACED THE APU ON MEL49-00-00 CTL 136251, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE R &R THE APU SERVO BLEED VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND TEH AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 14,037 hrs · 7,529 cycles

IAH - FLIGHT 2694, THE CREW REPORTED A VERY STRONG FUEL SMELL ON TAKEOFF THAT GOES AWAY AFTER THE APU IS SHUTDOWN. THE AIRCRAFT LANDED AT IOAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND APU, OPERATIONALLY CHECKED THE APU & BLEED SYSTEMS WITH NO SEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,524 hrs · 6,748 cycles

IAH - FLIGHT 2901, THE CREW REPORTED A ODOR OF FUEL AND/OR BURNED RUBBER DURING AND IMMEDIATELY AFTER TAKEOFF. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PERFORMED HIGH POWER ENGINE RUNS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 12,451 hrs · 6,711 cycles

IAH - FLIGHT 2281, THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AFTER ROTATION THAT DISSIPATED AROUND 1000 TO 1200 FEET AGL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE GROUND RAN BOTH ENGINES AND APU, OPERATIONALLY CHECKED THE PACKS SYSTEM WITH NO DEFECTS OR LEAKS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 11,845 hrs · 6,394 cycles

CLE FLIGHT 2895 - THE CREW REPORTED A STRONG FUEL SMELL ON CLIMBOUT. THE CREW SWITCHED FROM APU BLEED TO ENGINE BLEED AND FUMES WENT AWAY. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE APU BLEED SYSTEM AND NO FUEL ODOR WAS NOTICED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — FAILED (COCKPIT) · airframe 11,788 hrs · 6,358 cycles

FLT 2177 - UPON ARRIVAL TO THE TERMINAL THE CAPTAIN REPORTED A STRONG ELECTRICAL ODOR IN THE CABIN AND COCKPIT. MAINTENANCE FOUND THE WINDSHIELD HEAT CONTROLLER TO HAVE FAILED CAUSING THE SMOKE SMELL. THE AFFECTED CONTROLLER WAS REPLACED, THE WINDSHIELD HEATING SYSTEM OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,618 hrs · 5,188 cycles

SHV - DURING C-CHECK RT OMEGA BEAM HAS AREA OF CORROSION AROUND NUT PLATE NEAR FRAME 23. MAINTENANCE REPAIRED RT OMEGA BEAM AROUND NUT PLATE NEAR FRAME 23 IAW EC5320-01228. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,326 hrs · 3,987 cycles

SDF - OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY CHARGER IAW EMB 145XR AMM 33-50-04. OPS CHECK GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,188 hrs · 3,908 cycles

DURING ROUTINE MAINTENANCE, THE LAST TWO EMERGENCY AISLE PATH LIGHT STRIPS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY — FAULTY (EMERGENCY LIGHT) · airframe 7,113 hrs · 3,867 cycles

CREW REPORTED EMERGENCY LIGHT AT EXIT ROW IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW EMB145 AMM NR 33-50-04. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 7,055 hrs · 3,835 cycles

SHV - RON MAINTENANCE FOUND EMERGENCY LIGHT BATTERY ABOVE SERVICE DOOR NOT WORKING. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ABOVE SERVICE DOOR IAW EMB 145 XR VCMM 25-60-03. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — ODOR (NR 2) · airframe 12,062 hrs · 9,165 cycles

CREW REPORTED, SMOKE IN CABIN. TURNED OFF PACK NUMBER 2 AND SMOKE CLEARED. ERW MAINTENANCE TROUBLESHOT, DETERMINED ENGINE NR 1 CAUSING SMOKE IN CABIN. AIRCRAFT MAINTENANCE FERRIED TO BTV WITH NR 1 BLEED OFF. BTV MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. OPS CHECKED AND LEAKED CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE IAW TASKCARD 6271001.

Part: SUMP — CRACKED (NR 1 ENGINE) · airframe 12,062 hrs · 9,165 cycles

CREW REPORTED SMOKE IN CABIN. TURNED OFF PACK NR 2 AND SMOKE CLEARED. EWR MAINTENANCE TROUBLESHOT, DETERMINED ENGINE NR 1 CAUSING SMOKE IN CABIN. AIRCRAFT MAINTENANCE FERRIED TO BTV WITH NR 1 BLEED OFF. BTV MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. OPS CHECKED AND LEAKED CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE IAW TASKCARD NR 6271001. FRONT SUMP CRACKED, SUMP WAS CRACKED ALLOWING OIL TO SEEP INTO BLEED AIR SYSTEM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 6,907 hrs · 3,753 cycles

MCI - DURING MAINTENANCE INSPECTION, THE LEFT AND RIGHT EXTERIOR REAR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — DAMAGED (EMERGENCY BATTER) · airframe 5,594 hrs · 3,043 cycles

TYS FLIGHT 3459 FROM AVL EMERGENCY LIGHTS ON WITH THE SWITCH IN OFF POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY TRAY AND OPS CHECK WAS GOOD. AIRCRAFT APPROVED FOR SERVICE. LOGGED IN LOG BOOK PAGE 1041870.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,101 hrs · 2,795 cycles

CLE - THE CREW TURNED OFF THE CABIN LIGHTS AND THE EMERGENCY LIGHTS CAME ON AND WOULD NOT EXTINGUISH. MAINTENANCE REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY AND ELECTRICAL CONNECTOR P8500.

Part: LIGHT — CRACKED (GALLEY)

IAH - DURING ROUTINE INSPECTION THE GALLEY EMERGENCY LIGHT STRIP WAS FOUND TO HAVE A CRACKED COVER. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — ODOR

DAY FLIGHT 2286 THE CREW REPORTED AFTER STARTING THE APU A MINOR BURNING ODOR WAS NOTED. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 49-00-00.

Part: PROXIMITY SWITCH — OUT OF ADJUST (MLG)

DURING CLIMB THE CREW REPORTED THAT THE LANDING AIR/GROUND FAIL MESSAGE ILLUMINATED AND THE GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE ADJUSTED THE MAIN LANDING GEAR PROXIMITY SWITCHES. THE GEAR WAS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.