N11119

Part: TORQUE LINK — LACK OF LUBE (NLG) · airframe 43,704 hrs · 27,369 cycles

DURING TAKEOFF A LOUD POP WAS HEARD WHEN GEAR BECAME UNLOADED---- LUBRICATED NOSE LANDING GEAR AND TORQUE LINKS--ADDITIONAL ENTRIES MADE TO INSP LAND GEARS SIGNED OFF AS FOLLOWS--PERFORMED DETAILED VISUAL OF NLG NO FAULTS FOUND, PERFORMED DETAILED VISUAL INSP OF BOTH MLG NO FAULTS FOUND.

Part: VALVE — INOPERATIVE (NR 1) · airframe 43,618 hrs · 27,287 cycles

ON CLIMB OUT, BLEED 1 OVERTEMP MESSAGE. FOLLOWED QRH THEN GOT BLEED 2 OVERTEMP MOMENTARILY. R&R #1 FAN AIR VALVE. OPS CHECK OF #1 AND #1 BLEEDS. OPS CHECK GOOD.

Part: COUPLING — LEAKING (NR 2 A/C PACK) · airframe 43,048 hrs · 26,850 cycles

A/C DIVERTED DUE TO CREW REPORTING PACK 1 INTERMITTENT AND PACK 2 ALREADY DEFERED. INSPECTRED AND FOUND PACK 2 COUPLING LEAKING AT THERMO SWITCH. R/R COUPLING. OPS AND LEAK CHECK GOOD OF BOTH PACKS.

Part: CLAMP — LOOSE (DUCT) · airframe 43,027 hrs · 26,834 cycles

PACK #1 SHUT OFF ON FLIGHT AND WOULD NOT COME BACK ON. COMPLETED EMERGENCY DESCENT--- FOUND LOOS CLAMP ON RUBBER COUPLING AND AFT OF PACK #1. R&R COIPLING AND CLAMP. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 42,245 hrs · 26,223 cycles

AFT EMERGENCY FLASHLIGHT WILL NOT ILLUMINAT, APPEARS TO BE CHARGING..... DEFERRED SFT EMERGENCY FLASHLIGHT. WILL PROVIDE MORE INFORMATION WHEN AVAILABLE

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 41,064 hrs · 25,286 cycles

SVC DOOR FRAME DOOR SILL HAS CORROSION... REMOVED AND REPLACED SVC DOOR FRAME SILL..

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 41,064 hrs · 25,286 cycles

BAGGAGE DOOR BOTTOM I/B ANGLE PROFILE HAS CORROSION AT NUTPLATE LOCATIONS. REMOVED AND REPLACED DAMAGED "L" ANGLE PROFILE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 52-61) · airframe 41,064 hrs · 25,286 cycles

CENTER OMEGA BEAM BETWEEN FR 52 AND 61 HAS COROSION AT NUTPLATE LOCATIONS... CUT OUT DAMAGE AND REPAIRED WITH DOUBLER IAW SRM 53-24-10

Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

CTR OMEGA MEAM GUSSET BETWEEN FR59 AND FR61 HAS CORROSION. REMOVED AND REPLACED CTR OMEGA BEAM GUSSET IAW SRM 51-40-02.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

LT OMEGA BEAM GUSSET BETWEEN FR59 AND FR61 HAS CORROSION. REMOVED AND REPLACED LT OMEGA BEAM GUSSET.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

RT OMEGA MEAM GUSSET BETWEEN FR59 AND FR61 HAS CORROSION. REMOVED AND REPLACED CTR OMEGA BEAM GUSSET BETWEEN FR59 AND FR61 IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

WIRING LATERAL SUPPORT BETWEEN FR19 AND FR30 AT STRINGER 4L IS CRACKED. REMOVED CRACKED WIRING SUPPORT. INSTALLED NEW WIRING SUPPORT BRACKET.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

AFT CARGO RT FLOOR SILL BETWEEN FR 65 AND FR 68 HAS CORROSION. REMOVED AND REPLACE GUSSETS BETWEEN FRAMES 65 AND 68.

Part: SILENCER — CRACKED (TAIL CONE) · airframe 41,064 hrs · 25,286 cycles

TAIL CONE SILENCER IS CRACKED... REMOVED AND REPLACED TAIL CONE SILENCER...

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 41,064 hrs · 25,286 cycles

LT T/R DOOR LOWER ACTUATOR SEAL BRACKET IS CRACKED. REMOVED AND INSTALLED NEW BRACKET IAW SRM 51-40-02.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 41,064 hrs · 25,286 cycles

L/H T/R DOOR UPPER ACTUATIR SEAL BRACKET IS CRACKED... REMOVED AND REPLACED BRACKET

Part: SUPPORT — BENT (CARGO BAY) · airframe 41,064 hrs · 25,286 cycles

9 EA LT AND RT BAGGAGE BAY SIDEWALL LINER SUPPORT TABS BENT OVER BETWEEN FRAMES 61 AND 73. REMOVED AND REPLACED 9EA BAGGAGE BAY SIDEWALL LINER SUPPORT TABS.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 41,064 hrs · 25,286 cycles

CARGO DOOR FWD LOWER CORNER SKIN IS DAMAGED. REMOVED DAMAGED PROFILE. INSTALLED NEW PROFILE ON FWD LOWER CARGO DOOR.

Part: SUPPORT BRACKET — BENT (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

2 EA BENT WIRE BUNDLE SUPPORT BRACKETS AT FRAMES 66 AND 67 I/B OF BAGGAGE DOOR UNDERFLOOR. REMOVED AND REPLACED 2 BENT WIRE BUNDLE SUPPORT BRACKETS AT FRAMES 66 AND 67.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

SVC DOOR ENTRANCE SILL HAS CORROSION AROUND SCREW HOLES. INSTALLED NEW SVC DOOR SILL IAW SRM 51-40-02.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

LT OVERWING ANGLE AT FRAME 48 IS CRACKED. REMOVED AND REPLACED LT OVERWING ANGLE AT FRAME 48 IAW SRM 51-40-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

CTR AISLE RAMP PANEL LT UPPER BRACKET IS CRACKED. REMOVED AND REPLACED CTR AISLE RAMP PANEL LT UPPER SUPPORT BRACKET IAW SRM 51-40-02.

Part: FRAME — SCRATCHED (FRM 61) · airframe 41,064 hrs · 25,286 cycles

FRAME 61 HAS SCRATCHES NEAR STRINGER 13R... BLENDED OUT SCRATCHES. PERFORMED NDT.COMPLEATED REPAIR REF ETD2018-145-094488

Part: FRAME — CHAFED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

FRAME 62 HAS CHAFE MARK FROM CARGO LINER HDW NEAR STRINGER 12R. REMOVED FRAME 62, INSTALLED NEW FRAME 62 IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

SVC DOOR ENTRANCE STOP SIGN SUPPORTS HAVE MINOR CORROSION AROUND SCREW HOLES. REMOVED AND REPLACED AFT SVC DOOR STOP SIGN SUPPORTS IAW SRM 51-40-02.

Part: SUPPORT — CRACKED (CARGO DOOR) · airframe 41,064 hrs · 25,286 cycles

AFT CARGO DOOR SUPPORT ROD CUP HOLDER SUPPORT BRACKED IS CRACKED ON BACK SIDE AND HAS BROKEN RIVETS... REMOVED AND REPLACED AFT CARGO DOOR SUPPORT ROD CUP HOLDER SUPPORT IAW SRM 51-40-02

Part: BRACKET — CRACKED (FUSELAGE) · airframe 41,064 hrs · 25,286 cycles

MAIN CABIN FRAME 47 STR END FITTING BRACKET IS CRACKED BELOW LT FLOOR SILL. INSTALLED AND SEALED NEW SUPPORT BRACKET AT FRAME 47.

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 40,767 hrs · 25,059 cycles

E1 DROPPING 1 QT OIL EVERY 30 MINS. SERVICED NR 1 ENG TO FULL PERFORMED POWER RUNS W/ CREW FOR 5 MINS NO LEAKS NOTED.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 39,978 hrs · 24,435 cycles

PAX DOOR SWING ARM, NR 1 EMERGENCY LIGHT LENS IS CRACKED. R & R THE LENS.

Part: CLAMP — LOOSE (BLEED SYSTEM) · airframe 38,077 hrs · 22,820 cycles

NR 1 BLEED LEAK. FOUND CLAMPS LOOSE ON E1 PRSOV, TIGHTENED CLAMPS. ALSO R2 BLEED SEALS AT POS 9, 17 AND 23 IAW EMB 145 AMM 36-11-09. OPS CHECK GOOD IAW AMM 36-11-05.

Part: STRUT — DISCHARGED (NLG) · airframe 37,138 hrs · 22,015 cycles

LANDING GEAR AIR GROUND FAIL. SERVICED NOSE LANDING GEAR STRUT. GEAR SWING OPS CHECKED GOOD.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 37,084 hrs · 21,972 cycles

DURING CLIMB OUT, F/A ADIVSED A FOUL ODOR IN THE CABIN. INSPECTED AND FOUND OIL LEAKING FROM NR 2 ENGINE AT NR 4 CARBON SEAL. REMOVED AND REPLACED THE NR 2 ENGINE.

Part: LIGHT — MALFUNCTIONED (FA SEAT) · airframe 36,848 hrs · 21,753 cycles

EMERGENCY LIGHT ABOVE FA SEAT IS INOPERATIVE. PERFORMED OPS CHECK OF EMERGENGY LIGHT, OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,042 hrs · 21,124 cycles

MAIN DOOR EXTERIOR FLOOD LIGHT IS INOPERATIVE. R & R PAX DOOR EMERGENCY LIGHT ASSY AND NR 1 EMERGENCY POWER SUPPLY. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,625 hrs · 20,799 cycles

AISLE FLOOD LIGHT 16D INOPERATIVE. R & R BULB IN AISLE FLOOD LIGHT 16D. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 35,341 hrs · 20,557 cycles

SERVICE DOOR EMERGENCY FLOOD LIGHT NR 2 INOPERATIVE. REPAIRED BROKEN POWER WIRE TO NR 2 EMERGENCY FLOOD LIGHT ON SERVICE DOOR. OPS CHECK GOOD.

Part: WIRE — BROKEN (HEADSET JACK) · airframe 35,106 hrs · 20,363 cycles

BURNING ODOR FROM COCKPIT. MAINTENANCE INSPECTED AND FOUND A BROKEN WIRE ON F/O HEADSET JACK. SOLDERED WIRE, OPS CHECKED GOOD.

Part: FRAME — CORRODED (FRM 66) · corrosion level 2 · airframe 34,778 hrs · 20,136 cycles

DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15L-16L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-03015. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 34,778 hrs · 20,136 cycles

DURING C-CHECK, THE FRAME 65 SHEAR TIE WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15L-16L. MAINTENANCE R & R THE SHEAR TIE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 33,839 hrs · 19,515 cycles

DURING POSTFLIGHT INSPECTION, THE CREW REPORTED THE EXIT SIGN ABOVE THE F/A JUMPSEAT TO BE INSOPERATIVE. MAINTENANCE INSPECTED THE ACFT AND RESET THE AFFECTED EMERGENCY EXIT SIGN, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — FAULTY (FIRE CONTROL) · airframe 32,026 hrs · 18,328 cycles

THE CREW REPORTED DURING FINAL APPROACH, RECEIVED AN APU FIRE INDICATION. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU FIRE CONTROL MODULE. OPS CHECKS WERE GOOD.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,391 hrs · 16,659 cycles

DURING C-CHECK LT UPPER SEAT TRACK SUPPORT HAS CORROSION (LOCAL LEVEL 2) AT FRAME 50. MX PERFORMED REPAIR AND INSTALLED FABRICATED REPAIR DOUBLER AND FILLER AT LT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EC5320-01522, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,391 hrs · 16,659 cycles

DURING C-CHECK, RT UPPER SEAT TRACK SUPPORT HAS CORROSION AT FRAME 50. MX PERFORMED REPAIR AND INSTALLED FABRICATED DOUBLER REPAIR AT RT UPPER SEAT TRACK SUPPORT AT FRAME 50 IAW EC5320-01522, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,391 hrs · 16,659 cycles

DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68 AND STRINGERS 15-16L. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSOR — INOPERATIVE (LAVATORY SMOKE) · airframe 27,133 hrs · 15,188 cycles

CREW REPORTED A LAVATORY SMOKE WARNING ON EICAS WITH NO SMOKE DETECTED. ACFT LANDED WITHOUT INCIDENT. MX R & R THE LAVATORY SMOKE SENSOR, AND THE LAVATORY SMOKE DETECTOR PANEL, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — INOPERATIVE (SMOKE DETECTION) · airframe 27,133 hrs · 15,188 cycles

THE CREW REPORTED A LAV SMOKE WARNING ON EICAS WITH NO SMOKE DETECTED IN THE LAV. ACFT LANDED WITHOUT INCIDENT, MX R & R THE LAVATORY SMOKE SENSOR, AND THE LAVATORY SMOKE DETECTOR PANEL, OPS TESTED WITH NO DEFECTS, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,306 hrs · 13,359 cycles

IAH - DURING MAINTENANCE INSPECTION THE EXIT MARKER AT ROW 12 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — DEFECTIVE (LT MLG) · airframe 23,834 hrs · 12,965 cycles

TYS - A/C WAS EN ROUTE FROM ORD TO PNS WHEN A WARNING INDICATION OF AIR-GROUND FAIL MESSAGE APPEARED ON THE ICIAS. THE CREW DIVERTED TO TYS WHERE MAINTENANCE REMOVED AND REPLACED BOTH LT MLG WOW PROX SENSORS IAW EMB 145XR AMM 32-36-01. OPS CHECK GOOD AND WAS RELEASED. S/N OF PROX SWITCHES OFF-1169 AND 1114.

Part: VALVE — INOPERATIVE (BLEED AIR SYS) · airframe 22,841 hrs · 12,217 cycles

IAH - FLIGHT 2334, DURING CLIMB THE CREW REPORTED A BLEED TWO OVERTEMP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO FAN AIR VALVE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — FAULTY (AC PACK) · airframe 19,990 hrs · 10,655 cycles

EWR FLT 2101 - THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT/CABIN. THE AIRCRAFT DIVERTED INTO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED PACK 2 DUCTS P/N 145-22277-405 AND 145-22285-403. DUCTS WERE MELTED. MAINTENANCE ALSO REPLACED THE NR 2 PACK OVER TEMP SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR · airframe 19,962 hrs · 10,640 cycles

IAH - FLIGHT 2354, THE CREW REPORTED A VERY STRONG ODOR COMING FROM PACK 2 IN FLIGHT, AND THE INABILITY TO DUPLICATE ON THE GROUND. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED NR 1 & NR 2 ENGINE GROUND RUNS AT VARIOUS CONFIGURATIONS, INSPECTED THE AIRCRAFT ALL WITH NO SMELL OR DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,937 hrs · 10,620 cycles

CLE FLT 2181 THE CREW REPORTED A ABNORMAL SMELL ASSOCIATED WITH THE NR 2 PACK IN ICING CONDITIONS. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE NR 2 PACK AND NO DEFECTS OR SMELLS WERE FOUND.

Part: DUCT — LOOSE (AC BAY) · airframe 19,895 hrs · 10,596 cycles

IAH - FLIGHT 2160, THE CREW REPORTED THAT THE PACK TWO VALVE WOULD NOT OPEN AFTER TAKEOFF AND COULD NOT GET IT OPEN AFTER MULTIPLE RESETS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED A DUCT ON THE NR 2 PACK DUAL TEMP CONTROL VALVE, OPERATIONAL AND LEAK CHECKS COMPLETED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 19,843 hrs · 10,566 cycles

JAX - FLIGHT 2436, THE CREW REPORTED A BURNT RUBBER / ELECTRIC TYPE SMELL THROUGHOUT THE AIRCRAFT FROM DEPARTURE THROUGH 15000. THE AIRCRAFT RETURNED TO JAX, LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED GVI OF PACK DUCTING WITH NO DEFECTS, INSPECTED THE CABIN LIGHTING OPERATIONALLY TESTED NR 1 & 2 PACKS AND PERFORMED ENGINE RUNS ALL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 19,285 hrs · 10,260 cycles

TYS - DURING A ROUTINE CHECK THE EMERGENCY EXIT LIGHT ON SIDEWALL AT ROLL 19A WAS FOUND INOP. MAINTENANCE REPLACED THE INVERTER FOR THE EXIT EMERGENCY LIGHT IAW AMM 33-50-11. OPS CHECK GOOD. A/C RELEASED TO SERVICE.

Part: YOKE — CRACKED (NR 2 PYLON) · airframe 19,142 hrs · 10,171 cycles

SHV - DURING C-CHECK, NR 2 ENG FWD LOWER ENG YOKE CRACKED. REMOVED AND REPLACED NR 2 FWD LOWER ENG YOKE IAW EC 5450-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — GOUGED (HORIZ STAB) · airframe 19,151 hrs · 10,176 cycles

SHV - DURING C-CHECK HORIZONTAL STAB LT HINGE PIN BUSHING HOUSING NR 1 (LEFT OUTBOARD) GOUGED. MAINTENANCE REMOVED AND INSTALLED NEW 2ND OVERSIZE BUSHING IN LT HORIZ STAB NR 1 HOUSING (LEFT OUTBOARD) AND REAMED INTERNAL DIAMETER IAW EMB-145XR SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — GOUGED (HORIZ STAB) · airframe 19,151 hrs · 10,176 cycles

SHV - DURING C-CHECK HORIZONTAL STAB RT HINGE PIN BUSHING HOUSING NR 4 (RIGHT OUTBOARD) GOUGED. MAINTENANCE REMOVED AND INSTALLED NEW 2ND OVERSIZE HOUSING BUSHING ON RIGHT HORIZ STAB HINGE PIN HOUSING 4 (RIGHT OUTBOARD) AND REAMED INTERNAL DIAMETER OF BUSHING IAW EMB-145XR SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — GOUGED (HORIZ STAB) · airframe 19,151 hrs · 10,176 cycles

SHV - DURING C-CHECK HORIZONTAL STAB RT HINGE PIN BUSHING HOUSING NR 3 (RIGHT INBOARD) GOUGED. MAINTENANCE REMOVED AND INSTALLED NEW 2ND OVERSIZE HOUSING BUSHING ON RT HORIZONTAL STABILIZER HINGE PIN HOUSING NR 3 (RIGHT INBOARD) AND REAMED INTERNAL DIAMETER IAW EMB-145XR SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 19,151 hrs · 10,176 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER BEAM CUTOUT HAS CORROSION (LEVEL 2) AT CORNER FRM 65. MAINTENANCE COMPLETED REPAIR OF CARGO DOOR LOWER BEAM CUTOUT IAW IC2009-145/07501A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · airframe 19,151 hrs · 10,176 cycles

SHV - DURING C-CHECK SHEAR CLIP AT FRM 65 HAS CORROSION (LEVEL 2) BETWEEN STR 19L-18L. MAINTENANCE COMPLETED REPAIR OF FRAME 65 SHEAR CLIP BETWEEN STRINGER 19L-18L IAW IC2009-145/07501A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — GOUGED (HORIZ STAB) · airframe 19,151 hrs · 10,176 cycles

SHV - DURING C-CHECK HORIZONTAL STAB LT HINGE PIN BUSHING HOUSING NR 2 (LEFT INBOARD) GOUGED. MAINTENANCE REMOVED AND INSTALLED NEW 2ND OVERSIZE HAT BUSHING ON HORIZ STAB HOUSING NR 2 (LEFT INBOARD) IAW EMB-145XR SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 19,151 hrs · 10,176 cycles

SHV - DURING C-CHECK FRAME 65 SUPPORT BETWEEN STR 18L-17L HAS CORROSION AT BEND. MAINTENANCE COMPLETED REPAIR OF FRAME 65 BETWEEN STR 17L-18L IAW IC2009-145/07501A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SENSE LINE — LOOSE (LT WING) · airframe 18,169 hrs · 9,655 cycles

IAH - FLIGHT 2240, THE CREW REPORTED A WING ANTI-ICE FAIL ON 1A TEST WHILE AIRBORNE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE SENSE LINE ON THE LEFT WING ANTI-ICE VALVE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 1) · airframe 17,982 hrs · 9,558 cycles

IAH - DURING MAINTENANCE INSPECTION A HAZE AND ODOR WAS REPORTED IN THE CABIN FROM THE NUMBER ONE ENGINE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 17,302 hrs · 9,194 cycles

FLIGHT 3066 - RIC - FLIGHT CREW REPORTED "LAV SMOKE" WARNING INDICATION IN EICAS AND STRANGE SMELL ON CLIMB. RIC MX R&R LAVATORY SMOKE DETECTOR AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — DEFECTIVE (SMOKE DETECTION) · airframe 17,302 hrs · 9,194 cycles

FLIGHT 3066 - RIC - FLIGHT CREW REPORTED "LAV SMOKE" WARNING INDICATION IN EICAS AND STRANGE SMELL ON CLIMB. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. RIC MX R&R LAVATORY SMOKE DETECTOR PANEL AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGNAL COND UNIT — INOPERATIVE (FUEL SYSTEM) · airframe 16,008 hrs · 8,479 cycles

FLIGHT 3000 - EWR - FLIGHT CREW REPORTED, LOST ALL FUEL INDICATION AFTER TAKEOFF (RT AND LT) AND HAD INTERMITTENT FUEL LOW LEVEL INDICATION ON EICAS. CREW PERFORMED AIR RETURN WITHOUT INCIDENT. EWR MX REMOVED AND REPLACED FUEL CONDITIONING SIGNAL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: SMOKE WARNING — MALFUNCTIONED (CARGO BAY) · airframe 14,263 hrs · 7,585 cycles

IAH - FLIGHT 2208, THE CREW REPORTED A BAGGAGE SMOKE INDICATION AFTER THE RECIRC FAN CIRCUIT BREAKER POPPED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE RECIRC FAN ON MEL 21-22-06 CAT CCTL 136433, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 01/07/07, THE AIRCRAFT RON'D IN SHV WHERE MAINTENANCE OPERATIONALLY CHECKED THE BAGGAGE COMPARTMENT VENTILATION SYSTEM WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 14,262 hrs · 7,583 cycles

SHV - DURING C-CHECK CORROSION ON LEFT HAND OMEGA BEAM LOWER FLANGE AT FR 20. MX REPAIRED LT OMEGA BEAM LOWER FLANGE AT FR 20 IAW EMB 145 SRM 51-30-01, 51-40-04, 51-40-06, 51-40-02 AND IAW EMB 145 CPM 51-21-04, 51-21-05, 51-21-06. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 14,262 hrs · 7,583 cycles

SHV - DURING C-CHECK CORROSION ON SERVICE DOOR THRESH HOLD SILL. MX REMOVED AND REPLACED SVC DOOR CENTER SILL IAW EMB 145 SRM 51-40-02, INSTALLED NUT PLATES IAW EMB EC 5320-0437. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 14,262 hrs · 7,583 cycles

SHV - DURING C-CHECK CORROSION ON SERVICE DOOR THRESH HOLD SILL. MX REMOVED AND REPLACED SVC DOOR CENTER SILL IAW EMB 145 SRM 51-40-02, INSTALLED NUT PLATES IAW EMB EC 5320-0437. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: DETECTION SYS — MALFUNCTIONED (LAVATORY) · airframe 13,454 hrs · 7,159 cycles

IAH - FLIGHT 2163, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A LAV SMOKE WARNING. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 4,932 hrs · 2,622 cycles

DURING C-CHECK THE LEFT OMEGA SHAPE CORRODED AT FRAME 20. REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW 53-21-10. AIRCRAFT RETURNED TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 4,932 hrs · 2,622 cycles

DURING C-CHECK THE CARGO DOOR CUTOUT LOWER FLOORBEAM WAS FOUND TO BE CORRODED. REPLACE THE BEAM IAW 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 2,081 hrs · 1,117 cycles

CREW REPORTED AFTER TAKEOFF THROUGH 5000 FEET, BAGGAGE FIRE WARNING CAME ON, BLEW BOTH BOTTLES, AND AIR RETURNED TO DAY. MEL'D BAGGAGE COMPARTMENT AND CONTINUED FLIGHT TO EWR. EWR MAINTENANCE INSPECTED BAGGAGE COMPARTMENT FOR EVIDENCE OF SMOKE OR FIRE. NONE NOTED. PERFORMED TEST OF BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM, CHECKED GOOD. REMOVED AND REPLACED BOTH FIRE EXTINGUISHER BOTTLES (PART NUMBER: 33700027-1) IAW EMB145 MM 26-23-01. CLEARED MEL AND RETURNED THE AIRCRAFT TO SERVICE.

Part: VALVE — LEAKING (NR 1)

PSP - PILOT REPORTED THAT THE LEFT WING WAS LOSING FUEL DURING CLIMB. THE AIRCRAFT RETURNED TO PSP AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 VENT VALVE. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE.