N16951

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,622 hrs · 27,141 cycles

DURING PREFLIGHT INSPECTION, CREW REPORTED THAT THE LAST TWO ROWS OF AISLE PATH LIGHTING WERE INOPERATIVE. MX RESET THE EMERGENCY LIGHT SYS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FAILED (LEFT) · airframe 35,457 hrs · 27,029 cycles

THE CREW REPORTED SMOKE IN THE CABIN. THE ACFT DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. MX OPERATED THE APU AND ENGINES WITH THE FLIGHT CREW, VERIFIED THE SMOKE WAS COMING FROM THE NR 1 PACK, PLACED THE NR 1 PACK ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT WAS REPOSITIONED TO AIRPORT WHERE MX R & R THE NR 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, REMOVEDTHE MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,396 hrs · 26,189 cycles

DURING ROUTINE MX THE RT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED LAMP . OPS CHECKED GOOD.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK CORROSION AROUND LOWER NUTPLATES ON SERVICE DOOR. MX PERFORMED REPAIR AROUND LOWER NUTPLATES ON SERVICE DOOR IAW EC5210-01154. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK, RIVET AT FRAME 79, STRINGER 3R SHOWS VISUAL INDICATION OF CRACKS. MX PERFORMED REPAIR OF FUSELAGE SKIN AT FRAME 79, STRINGER 3R IAW EC 5330-02673. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK RT OMEGA BEAM CORRODED AT FRAME 23. MX R & R RT OMEGA BEAM BETWEEN FR 16-24 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — DAMAGED (VERTICAL TO FUSE) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK, FRAME 75 STR 2L-2R IS FRETTING AT BOLTS FOR VERTICAL STAB TO FUSELAGE BRACKET. MX PERFORMED REPAIR AT FRM 75 STR 2L-2R AT VERTICAL STAB TO FUSELAGE BRACKET IAW EC5310-01317. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK RIVET AT FRAME 79, STRINGER 3L SHOWS VISUAL INDICATION OF CRACKS. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 79, STRINGER 3L IAW EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK, MAIN DOOR LOWER FRAME HAS CORRODED SCREW HOLES. MX PERFORMED REPAIR ON MAIN DOOR LOWER FRAME SCREW HOLES IAW EC5210-01154, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK RIVET AT FRM 78, STR 5R SHOWS VISUAL INDICATION OF CRACKS. MX REPAIRED FUSELAGE SKIN AT FRM 78, STR 5R IAW EC5330-02673, REV ORIGINAL. THE AVFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (SPOILER) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK, LT WING SPEED BRAKE CENTER HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT SPEED BRAKE CENTER HINGE INBD HAT BUSHING IAW EC5750-01415, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK CORROSION AROUND LOWER NUTPLATE ON AFT SIDE OF SERVICE DOOR. MX PERFORMED REPAIR AROUND LOWER NUTPLATE ON AFT SIDE OF SERVICE DOOR IAW EC5210-01154, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (ZONE 500) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK LT WING GROUND SPOILER CENTER HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER CENTER HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (SPOILER) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK, LT GROUND SPOILER CENTER HINGE INBD HAT BUSHING MIGRATED. MX R & R LT WING GROUND SPOILER CENTER HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (RT WING) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK RT WING SPEED BRAKE CENTER HINGE ATTACHMENT INBD LOBE HAS MIGRATED HAT BUSHING. MX R & R CENTER HINGE INBD HAT BUSHING IAW EC5740-01152, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (ZONE 500) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK LT WING GROUND SPOILER INBD HINGE ATTACHMENT OTBD LOBE HAT BUSHING MIGRATED. MX R & R LT GROUND SPOILER INBD HINGE ATTACHMENT BRACKET IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (ZONE 200) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK SMOKING RIVETS AT FRM 78 STR 3R. MX PERFORMED REPAIR ON FUSELAGE SKIN AT FRM 78 STR 3R IAW EC5330-02673. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (ZONE 100) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK SMOKING RIVETS AT FRM 77, BETWEEN STRS 3R-5R. MX PERFORMED REPAIR OF FUSELAGE SKIN AT FRM 77 BETWEEN STRS 3R-5R IAW EC5330-02673, REV ORIGINAL. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH ANGLE — CORRODED (ZONE 300) · corrosion level 2 · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK, PANEL 321DR ATTACHMENT FLANGE HAS CORRODED SCREW HOLES. MX PERFORMED REPAIR AT PANEL 321DR ATTACHMENT FLANGE SCREW HOLES IAW EC5510-01297. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — WORN (SPOILER) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK LT WING GROUND SPOILER OTBD HINGE ATTACHMENT INBD LOBE HAT BUSHING MIGRATED. MX R & R LT WING GROUND SPOILER OTBD HINGE ATTACHMENT IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — WORN (ZONE 600) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK, RT GROUND SPOILER INBD HINGE OTBD HAT BUSHING MIGRATED. MX R & R RT GROUND SPOILER INBD HINGE BRACKET IAW EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE — DAMAGED (RUDDER) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK, RUDDER NR 1 AFT CENTER UPPER HINGE DAMAGE GOUGED. MX R & R RUDDER NR 1 AFT CTR UPPER HINGE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — DAMAGED (ZONE 200) · airframe 34,372 hrs · 26,170 cycles

DURING C-CHECK DAMAGE, AT FRM 77, STR5R, MX PERFORMED REPAIR AT FRM 77, STR 5R IAW EMB-145 EC5330-02501. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 33,441 hrs · 25,415 cycles

AFTER TAKEOFF, THE CREW REPORTED SMOKE IN THE CABIN AND ELECTED TO RETURN TO DEPARTURE WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION, MX FOUND THE SOURCE OF THE SMOKE TO BE A SEIZED NR 1 AIR CYCLE MACHINE (ACM). MX REPLACED THE ACM, PERFORMED OPS CHECKS AND CLEARED THE DISCREPANCY.

Part: PUMP — OVERHEATED (NR 2 ENGINE) · airframe 31,279 hrs · 23,734 cycles

HYD SYSTEM 2 OVERHEAT/FAIL IN FLIGHT. REMOVED AND REPLACED ENG NR 2 HYD PUMP AND MANIFOLD IAW EMB145 AMM 29-10-03 & 29-10-07. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 30,061 hrs · 22,766 cycles

DIVERTED FOR EICAS AIRSPEED MESSAGE IN AMBER AT CRUISE. TYS R & R ADC NR1, OPS AND LEAK CHECKS GOOD. (CLOSED)

Part: PROXIMITY SENSOR — FAULTY (SPOILER) · airframe 29,725 hrs · 22,522 cycles

DURING FLIGHT THE CREW RECEIVED SPOILER FAIL AND SPOILER OPEN MESSAGES. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE REPLACED A SPOILER PROXIMITY SENSOR. OPERATIONAL CHECKS WERE PERFORMED AND THE DISCREPANCY WAS CLEARED.

Part: ACTUATOR — LEAKING (NLG DOOR) · airframe 29,719 hrs · 22,518 cycles

ON APPROACH INTO FAR THE CREW RECEIVED A GEAR AIR/GROUND FAIL MESSAGE. THE CREW ELECTED TO ABORT THE APPROACH AND THE MESSAGE EXTINGUISHED HOWEVER ON THE SECOND GEAR EXTENSION THE MESSAGE APPEARED AGAIN. THE AIRCRAFT LANDED IN FAR WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO KANSAS CITY, MO (MCI) GEAR DOWN WHERE THE LEFT NOSE LANDING GEAR DOOR ACTUATOR WAS REPLACED. OPERATIONAL CHECKS WERE PERFORMED AND THE DISCREPANCY CLEARED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,375 hrs · 22,227 cycles

SHV - DURING C-CHECK - SKIN CRACKS AROUND RIVETS BETWEEN FR 77-79 STR 4L TO 8L. REPAIRED CRACKS IAW EC5330-02342. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — DAMAGED (AILERON) · airframe 29,375 hrs · 22,227 cycles

SHV - DURING C-CHECK - LT AILERON 2ND FROM I/B HINGE I/B HAT BUSHING MIGRATED. REPLACED FITTING IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — DAMAGED (SPOILER) · airframe 23,353 hrs · 12,555 cycles

SHV - DURING C-CHECK - LT GROUND SPOILER O/B HINGE O/B HAT BUSHING MIGRATED. REPLACED HINGE FITTING BRACKET IAW EMB 145 SRM 51-20-03. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,375 hrs · 22,227 cycles

SHV - DURING C-CHECK STRINGER 21R BETWEEN FRAMES 12 AND 13 IS CORRODED. MAINTENANCE PERFORMED REPAIR OF STRINGER 21R BETWEEN FRAMES 12 AND 13 BY INSTALLING STRINGER REPAIR AT FRAMES 10-12 IAW EMB-145 SRM 53-00-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,375 hrs · 22,227 cycles

SHV - DURING C-CHECK FRAME 10 L BRACKET AT STRINGER 10L AND 9L CRACKED. MAINTENANCE REMOVED AND REPLACED FRAME 10 L BRACKET AT STRINGER 10L-9L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 29,375 hrs · 22,227 cycles

SHV - DURING C-CHECK FRAME 10 AT STRINGER 10L AND 9L CRACKED. MAINTENANCE REMOVED AND REPLACED FRAME 10 AT STRINGER 10L AND 9L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 29,319 hrs · 22,184 cycles

CLE FLT 2629 THE CREW REPORTED A STRONG ELECTRICAL SMELL AND A WINDSHIELD HEAT NR 2 FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT CONTROLLER. OPERATIONAL CHECKS WERE GOOD.

Part: ACM — SEIZED (NR 1) · airframe 29,310 hrs · 22,178 cycles

IAH - FLIGHT 2380, THE CREW REPORTED NOISE AND A SMOKE SMELL COMING FROM THE NUMBER ONE PACK. MAINTENANCE FOUND THE NR 1 ACM TO BE SEIZED, AND PLACED THE LEFT COOLING PACK ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. LATER ON 12/13/10 THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT ACM, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — OVERHEATED (CABIN) · airframe 27,697 hrs · 20,925 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL AT ROW 4. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED CEILING LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED OF RETURN TO SERVICE.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 26,302 hrs · 19,900 cycles

MEM - FLIGHT 2291, THE CREW REPORTED FUEL LEAKING FROM THE LEFT WING ON CLIMB. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT WING FLAPPER VALVE, LEAK CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,620 hrs · 19,386 cycles

FLIGHT CREW REPORTED THAT EMERGENCY LIGHTS WERE INOPERATIVE. MX PERFORMED SYS RESET SUCCESSFULLY AND ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED · airframe 25,388 hrs · 19,204 cycles

FLIGHT 3134 - EWR - FLIGHT CREW REPORTED NOSE EXCESSIVELY HEAVY ON TAKE OFF AND LANDING AND CREW HAD TO USE FULL NOSE UP TRIM ON LANDING. CREW DECLARED EMERGENCY AND LANDED ACFT UNEVENTFULLY. EWR MX CHECKED CABLE TENSION AND FOUND TO BE WITHIN LIMITS. FLIGHT CREW PERFORMED A TEST FLIGHT AND IT WAS DONE SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: STOP FITTING — DEFECTIVE (PAX DOOR)

MAIN CABIN DOOR WILL NOT CLOSE. REMOVED AND REPLACED FWD AND AFT DOOR STOP HARDWARE, REPOSITIONED DOOR SEAL AND RIGGED DOOR. REMOVED AND REPLACED FWD AND AFT UPPER DOOR STOPS, CHECKED AND ADJUSTED AS REQUIRED IAW EMB 145 AMM 52-18-00-820-808. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,963 hrs · 18,909 cycles

IAH - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHTING BETWEEN ROWS 6-8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 24,881 hrs · 18,846 cycles

IAH - DURING POST-FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE SLOW TO CHARGE, AND SOME BLINK ON AND OFF. MX R&R THE NR 3 EMERGENCY LIGHT INVERTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 24,878 hrs · 18,844 cycles

IAH - FLIGHT 2749, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERATIVE. MX INSPECTED THE ACFT, RESET THE ELECTRICAL SYSTEM, OPS TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 24,878 hrs · 18,844 cycles

IAH - FLIGHT 3097, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THAT THE LT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MX CHARGED THE NR 3 EMERGENCY LIGHT BATTERIES, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BONDING STRAP — CORRODED (WING) · airframe 24,821 hrs · 18,807 cycles

PANEL 191 WAS FOUND CORRODED AND MX R&R THE BONDING STRIP IAW EMB EC 5750-01315, ACFT WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: BONDING STRAP — CORRODED (WING) · airframe 24,821 hrs · 18,807 cycles

PANEL 193 BONDING STRIP WAS FOUND CORRODED AND MX R&R 193 BONDING PLATE IAW EMB EC 5750-01315. ACFT WILL BE RELEASED TO SERVICE AFTER THE C-CHECK IS COMPLIED WITH.

Part: PANEL — CORRODED (WING) · airframe 24,821 hrs · 18,807 cycles

PANEL 192AL WAS FOUND CORRODED AND MX R&R THE PLATE IAW EMB EC 5750-01315. ACFT WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: BONDING STRAP — CORRODED (WING) · airframe 24,821 hrs · 18,807 cycles

PANEL 192 WAS FOUND WITH A CORRODED BONDING STRAP AND MX R&R THE PLATE IAW EMN EC 5750-01315. ACFT WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: ENGINE — FAULTY (NR 2) · airframe 24,566 hrs · 18,625 cycles

CLE - FLIGHT 2311 - THE CREW REPORTED AT FL320 THE NR 2 ENGINE ITT STARTED INCREASING SLOWLY TO 860 WITHOUT FULL THRUST. ASSENTING AT 91PERCENT N2 THE ENGINES HAD A 30 DEGREE DIFFERENCE. THE FUEL FLOW WAS ALSO NOTED TO BE 30 PPH HIGH. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,462 hrs · 18,556 cycles

LRD - FLIGHT 2858, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS WOULD NOT TEST. THE CREW CHARGED THE EMERGENCY LIGHT BATTERIES, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (AFT GALLEY) · airframe 24,317 hrs · 18,463 cycles

AFT GALLEY EMERGENCY LIGHT INOP. R&R LIGHT IAW EMB AMM 33-50-14. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED MAINT, THE NR 3 EMERGENCY AISLE LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT STRIP, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY. (K)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

DURING SCHEDULED MAINT THE GALLEY EMERGENCY EXIT IDENTIFIER LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED NR2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED THE SYS AND CLEARED THE DISCREPANCY. (K)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

DURING SCHEDULED MAINT THE EXTERNAL EMERGENCY EXIT LOCATER LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE LIGHT ASSY, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY. (K)

Part: ENGINE — SMOKE (NR 2) · airframe 22,284 hrs · 17,025 cycles

FLIGHT 2291 MEM TO EWR:CREW NOTED "SMOKE FROM NR 2 ENGINE WAS REPORTED FROM START OF TAKEOFF ROLL TO APPROX THREE MILES FROM DEPARTURE END OF RUNWAY. OIL PRESSURE RANGED 117-111 PSI DURING TAKEOFF ROLL WITH 12 QTS OF OIL IN THE ENGINE". MX INSPECTED NR 2 ENGINE FOR OIL LEAKS WITH NO LEAKS NOTED. RAN NR 2 ENGINE ON GROUND IAW EMB 145 AMM 71-00-01. NO SMOKE NOTED. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (CABIN) · airframe 21,613 hrs · 16,544 cycles

DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,482 hrs · 16,440 cycles

IAH - DURING MAINTENANCE INSPECTION, THE LEFT HAND EXIT HATCH AFT EMERGENCY EXIT SIGN 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: LIGHT — LOW (CABIN) · airframe 20,949 hrs · 16,060 cycles

DURING PREFLIGHT INSPECTION, THE EMERGENCY LIGHTS WERE FOUND TO BE DIM. NO SPECIFIC PROBLEM COULD BE DETECTED WITH THE LIGHTING SYSTEM AND THE EMERGENCY LIGHT BATTERIES WERE CHARGED THROUGH NORMAL AIRCRAFT POWER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 20,438 hrs · 15,666 cycles

TYS - DURING A CURRENT 2C INSPECTION A CRACK WAS FOUND AT A RIVET AT FRAME 75, BETWEEN STR 1L AND 2L. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED DOUBLERS, INSTALLED FILLERS AND DOUBLERS, ALODINED, PRIMED AND PAINTED IAW EC 53330-01681. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF C-CHECK INSPECTION.

Part: BUSHING — MIGRATED (HORIZ STAB) · airframe 20,438 hrs · 15,666 cycles

TYS - DURING A CURRENT 5C INSPECTION THE LT HORIZONTAL STAB HINGE FITTING WAS FOUND MIGRATED. MAINTENANCE REMOVED THE LT STAB BUSHING, REWORKED HOUSING TO THE 2ND OVERSIZE DIAMETER AND INSTALLED THE 2ND SIZE BUSHING IAW EMB 135/145 SRM 55-10-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 5C INSPECTION.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 20,438 hrs · 15,666 cycles

AIRCRAFT IN FOR C-CHECK. CARGO DOOR CUTOUT LOWER SILL HAS AREAS OF CORROSION. REMOVED AND REPLACED CORRODED SILL IAW EMB 135/145 SRM 51-20-03, 51-40-02. ALODINED, PRIMED AND PAINTED IAW EMB CPM 51-21-04, 05, 06. AIRCRAFT STILL IN C-CK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,935 hrs · 15,278 cycles

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

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,935 hrs · 15,278 cycles

MCI - DURING MAINTENANCE INSPECTION, THE AFT OVERWING EMERGENCY EXIT LOCATOR SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,076 hrs · 13,828 cycles

EWR - FLIGHT 2334, DURING POST FLIGHT INSPECTION THE EMERGENCY LIGHT ABOVE THE F/A JUMPSEAT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLIGHT ATTENDANT CONTROL PANEL, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 16,924 hrs · 12,923 cycles

IAH - DURING MAINTENANCE INSPECTION, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE MEL'D THE AFFECTED LIGHTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON FLIGHT 2472, IAH MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,536 hrs · 12,599 cycles

CLE FLIGHT 2748 THE CREW REPORTED THE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FORWARD ISLE OVERHEAD EMERGENCY LIGHT.OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (E/E BAY FAN) · airframe 16,011 hrs · 12,173 cycles

BHM - FLIGHT 3240, THE CREW REPORTED AN ELECTRICAL ODOR IN THE COCKPIT DURING CRUISE. THE AIRCRAFT LANDED AT BHM WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE FORWARD AVIONICS RECIRC FAN ON MEL. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH ON FLIGHT 2026 ON 06/13/05 WHERE MAINTENANCE REMOVED AND REPLACED THE INVERTER FOR THE AVIONICS FAN, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, REMOVED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,919 hrs · 12,101 cycles

DURING PRE-FLIGHT INSP, CREW REPORTED FORWARD BULKHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MX R & R NR 2 EMERGENCY LIGHT BATTERY CHARGER, OPS CHECKED WITH NO DEFECTS. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 15,919 hrs · 12,101 cycles

DURING PREFLIGHT INSP, CREW REPORTED THAT FWD BULKHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MX R & R NR 2 EMERGENCY LIGHT BATTERY PACK. OPS CHECKED WITH NO DEFECTS. ACFT RETURNED TO SERVICE.

Part: BLEED VALVE — STUCK (APU) · airframe 15,636 hrs · 11,870 cycles

CLE - THE CREW REPORTED A STRONG FUEL ODOR UPON APU START. MAINTENANCE REPLACED THE APU BLEED AIR VALVE AND OPERATIONAL CHECKS WERE GOOD WITH NO FUEL SMELL DURING START.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 15,568 hrs · 11,823 cycles

SHV - DURING C-CHECK LT ELEVATOR ACCESS PANEL 335 HB, CUTOUT BENT. MAINTENANCE ON FURTHER EVALUATION FOUND LT ELEVATOR ACCESS PNL (CUTOUT)CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EC5520-01070. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 15,568 hrs · 11,823 cycles

SHV - DURING C-CHECK CRACK FOUND ON STRINGER 14L FR 18 BOTTOM I/B HOLE ON MAIN DOOR FRAME. MAINTENANCE REAMED MAIN DOOR STOP ATTACH HOLE, FR 18 STR 14 BOTTOM I/B PER EC5310-01333. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LEVER — MALFUNCTIONED (MLG) · airframe 15,412 hrs · 11,689 cycles

LANDING GEAR DISAGREE MESSAGE UPON ATTEMPTED RETRACTION OF L/G. ACFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER AND THE NLG PROXIMITY SENSOR. LANDING GEAR OPERATION CHECK SATISFACTORY. ACFT RELEASED TO SERVICE.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 15,412 hrs · 11,689 cycles

LANDING GEAR DISAGREE MESSAGE UPON ATTEMPTED RETRACTION OF L/G. ACFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY SENSOR. LANDING GEAR OPERATION CHECK SATISFACTORY. ACFT RETURNED TO SERVICE.

Part: HOSE — BROKEN (HYD SYSTEM) · airframe 10,160 hrs · 10,723 cycles

BPT - FLIGHT 2409, DURING CLIMB THE CREW REPORTED THE LOSS OF ALL HYDRAULIC FLUID FROM THE NUMBER ONE SYSTEM. THE AIRCRAFT RETURNED TO BPT WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE INBOARD HOSE ASSEMBLY, SERVICED THE HYDRAULICS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COUPLING — LOOSE (NR 4 BRAKE)

THE CREW REPORTED THE BRAKES WERE NOT VERY EFFECTIVE ON LANDING. THE ANTI-SKID WAS ENGAGED UNTIL 10 KNOTS. MAINTENANCE INSPECTED AND FOUND THE NR 4 BRAKE NOT WORKING ON NORMAL BRAKING. THE QUICK DISCONNECT COUPLING ON THE NR 4 BRAKE WAS RETIGHTED. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, THE NUMBER ONE EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY CHARGER IAW EMB 145 AMM 3350-50. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, THE NUMBER ONE EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT IAW EMB 145 AMM 33-50-12. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — GOUGED (FUSELAGE) · airframe 11,871 hrs · 8,883 cycles

SHV-DURING C CHECK FRAME 81 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5310-01246. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV-DURING C CHECK THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV-DURING C CHECK THE CENTER OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV- DURING C-CHECK, THE SERVICE DOOR CENTER SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — GOUGED (APU FIREWALL) · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, THE APU FIREWALL FRAME 81 WAS FOUND GOUGED AT BOTTOM CENTER. MAINTENANCE REMOVED DAMAGE AND PERFORMED A DOUBLER REPAIR ON AFFECTED FRAME IAW CONTINENTAL EXPRESS EC 5310-01246. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, THE CENTER FLOORBEAM WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOORWAY) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, THE CARGO DOOR CUT OUT LOWER BEAM WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED AND REPLACED AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV- DURING C-CHECK, THE CENTER FLOORBEAM RAMP ANGLE WAS FOUND TO HAVE CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV DURING C CHECK SERVICE DOOR AFT SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED SECTION IAW EMB 145 SRM 53-21-10 AND EC 5320-01089. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (CABIN) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, THE SERVICE DOOR FOWARD SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-05. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV DURING C CHECK SERVICE DOOR AFT SILL WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED SECTION IAW EMB 145 SRM 53-21-10 AND CONTINENTAL EXPRESS EC 5320-01089. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, A CRACK WAS FOUND AT THE APU FIREWALL BY RT UPPER MOUNT. MAINTENANCE REMOVED DAMAGED AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01267. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, FOWARD DIGITAL BUTTSTRAP WAS FOUND TO HAVE CORROSION AT FRAME 15. MAINTENANCE REMOVED DAMAGE AND REPAIRED AFFECTED AREA IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO HAVE CORRSION AND TOOLING MARKS BETWEEN FRAMES 18-23. MAINTENANCE REMOVED AND REPLACED AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV- DURING C-CHECK, THE LT FLOORBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — DAMAGED (NACELLE) · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK THE LEFT HAND UPPER COWLING INTERNAL STIFFENER WAS FOUND TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 54-10-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — GOUGED (NACELLE) · airframe 11,871 hrs · 8,883 cycles

DURING C-CHECK, THE NUMBER 2 LOWER COWLING INTERNAL STIFFENER WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV-DURING C-CHECK, THE LEFT HAND SILL BETWEEN FRAMES 19 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,871 hrs · 8,883 cycles

SHV-DURING C-CHECK, THE LEFT HAND SILL BETWEEN FRAMES 59 AND 61 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

IAH- DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY LIGHTS AFT OF THE EMERGENCY ROW FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY (OVERHEAD GALLEY LOCATION), PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE

Part: LIGHT — INOPERATIVE (CABIN)

DURING MAINTENANCE THE MECHANIC NOTED THAT THE EMERGENCY LIGHTS AFT OF THE EMERGENCY ROW FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE LAST EMERGENCY LIGHT FLOOR STRIP, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FADEC — INOPERATIVE (E/E BAY)

ON TAKEOFF ROLL THE CREW NOTED LOW N1 ON ENGINE NR 1. THE CREW ABORTED TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE NR 1B FADEC, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SPAR — CRACKED

During mtx taxi of the aircraft, the R/H wing outbd. leading edge struck a storage shed causing damage to the R/H leading edge, wing tip, and fwd. spar. Maintenance spliced in a new section of spar 1, replaced rib 25, and replaced the outbd. leading edge and wing tip IAW EA5710-01036, EMB AMM, and EMB SRM. Aircraft perfomed satisfactory test flight following the repair and was returned to service.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG)

FLIGHT 3850, THE CREW NOTED DURING CLIMB THAT THE LANDING GEAR WOULDN'T RETRACT,RETURNED TO IAH, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT SHOCK ABSORBER PROXIMITY SWITCH, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TRANSMITTER — INOPERATIVE (NR 1 ENGINE)

CLE - FLIGHT 3171, THE CREW REPORTED THE NR 1 ENGINE FUEL FLOW INDICATION SHOWED 0 IN FLIGHT. THE ENGINE OPERATED NORMALLY. MAINTENANCE REPLACED THE NR 1 ENGINE FUEL FLOW TRANSMITTER. OPERATIONAL CHECKS WERE GOOD.

Part: FLAP — CRAZED · airframe 9,863 hrs · 7,224 cycles

TYS DURING A SCHEDULED ROUTINE CHECK THE LH INBD FLAP TRAILING EDGE,UPPER SURFACE AERODYNAMIC FILLER WAS FOUND CRAZING AND CRACKING. THE AREA WAS 18"L X8.25"W, WITH A AREA WITHIN THAT THAT WAS 1.25" X 1.5" THAT THE FILLER WAS MISSING. MAINT. REQUESTED A GST FOR THE FLAP AND WAS ISSUED GST-2155/02 WHICH ALLOWED MAINTENANCE TO PUT SPEED TAPE OVER THE AREA AND DO A GVI EVERY ROUTINE CHECK FOR 500FC IN THAT IT WILL BE REPAIRED OR REPLACED.ALL WAS C/W AND PUT ON DMI.

Part: SKIN — PUNCTURED (NOSE) · airframe 9,563 hrs · 6,987 cycles

TYS, Aircraft ferried in for skin damage on the right side between frames 1A and 2, stringers 14R and 15R. Maintenance removed and replaced the damaged skin and stringer 15R. I/A/W-EMB-135/145-SRM-51-40-02 and 51-21-04, 05 & 06. The repair procedure was satisfactory.

Part: UPLOCK — DEFECTIVE (NLG) · airframe 9,137 hrs · 6,672 cycles

EWR---CO3536, CREW REPORTED NOSE LANDING GEAR DID NOT RETRACT ON TAKEOFF, CONFIRMED BY EICAS AND WIND NOISE. RECYCLED GEAR ONCE, NOSE GEAR SUCCESSFULLY RETRACTED ON SECOND ATTEMPT. MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR UPLOCK BOX IAW EMB145 MM 32-33-07. OPS CHECKED, SYSTEM GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK — FAULTY (NLG)

EWR - FLT 3536 - CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT RETRACT WHEN THE GEAR HANDLE WAS SELECTED UP. THE CREW RECYCLED THE GEAR HANDLE AND THE NOSE GEAR RETRACTED. THE AIRCRAFT LANDED AT EWR WITHOUT FURTHER INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK BOX. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG)

IAH - FLIGHT 4160, FROM DAL TO IAH, THE CREW REPORTED AN AIR GROUND FAIL WARNING, AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR PROXIMITY SWITCH TO HAVE FAILED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJ (LT MLG)

IAH - FLIGHT 3929, THE CREW REPORTED THAT ON CLIMB-OUT A LANDING GEAR AIR GROUND FAIL MESSAGE APPEARED ON THE EICAS. THE CREW VERIFIED NORMAL OPERATION OF THE GEAR AND CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT HAND MAIN LANDING GEAR PROXIMITY SWITCH, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1 ENGINE)

IAH - FLT 3997 - THE CREW REPORTED A BURNING SMELL ORIGINATING FROM THE NR 1 BLEED AIR SYSTEM. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW AIRCRAFT INSPECTION PROGRAM TASK CARD 6271001, REV 49, REF EMB-145 AMM 71-00-00. THE NR 1 AIRCONDITIONING PACK WAS REMOVED FROM MEL AND THE AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)

Part: A/C PACK — MALFUNCTIONED (AC BAY)

IAH - FLT 4216 - THE CREW REPORTED RELAYS CLICKING AND A BURNING ODOR IN THE COCKPIT. MAINTENANCE DETERMINED THE SOURCE OF THE BURNING ODOR TO BE COMING FROM THE NR 1 AIRCONDITIONING PACK. THE NR 1 AIRCONDITIONING PACK WAS PLACED ON MEL REFERENCE 21-51-00, CATEGORY ''C'' CONTROL NR 003258. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ENGINE — LEAKING (RIGHT)

IAH - NR 2 ENGINE TAILPIPE FIRE UPON ENGINE SHUTDOWN AFTER MAINTENANCE TAXI. BOTH FIRE BOTTLES WERE DISCHARGED, AND THE FIRE WAS EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT AND NO DAMAGE TO THE AIRCRAFT WAS NOTED. MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE NR 2 ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: TAILPIPE — FIRE (NR 2 ENGINE)

IAH - NR 2 ENGINE TAILPIPE FIRE UPON ENGINE SHUTDOWN AFTER MAINTENANCE TAXI. BOTH FIRE BOTTLES WERE DISCHARGED, AND THE FIRE WAS EXTINGUISHED. MAINTENANCE INSPECTED THE AIRCRAFT AND NO DAMAGE TO THE AIRCRAFT WAS NOTED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE FIRST SECTION OF EMERGENCY AISLE PATH LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (EMERGENCY EXIT)

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE CLEANED THE LIGHT ASSEMBLY SOCKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BRACKET — BROKEN (RIGHT AILERON)

DURING SCHEDULED EA 2710-01012 IN NEWARK, MAINTENANCE FOUND RIGHT OUTBOARD AILERON ROD END MOUNT BRACKET BROKEN. MAINTENANCE REMOVED AND REPLACED MOUNT BRACKET AND RETURNED AIRCRAFT TO SERVICE. (M)

Part: SEAL — LEAKING (NR 2 ENGINE)

SEVERAL AIR RETURNS WITH SMOKE ODOR AND 'LAV SMOKE' LIGHT ON EICAS. FINAL FIX WAS REMOVED AND REPLACED NR 2 ENGINE FAN DRIVE SEAL AND CARBON SEAL ASSY. NO FURTHER ODORS OR 'LAV SMOKE LIGHTS' ON EICAS. (M)

Part: GUST LOCK — OUT OF RIG (FUSELAGE)

ICT - FLT 4154 - DURING PRE-FLIGHT INSPECTION, THE PILOT REPORTED THE GUST LOCK SYSTEM WAS BROKEN. MAINTENANCE INSPECTED THE GUST LOCK SYSTEM AND FOUND IT TO BE OUT OF RIG. FURTHER EXAMINATION OF THE AIRCRAFT REVEALED SUBSEQUENT DAMAGE TO THE LEFT AND RIGHT ELEVATORS. MAINTENANCE RIGGED THE GUST LOCK SYSTEM, AND THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REPAIRED THE DAMAGE TO THE ELEVATORS AND RETURNED THE AIRCRAFT TO SERVICE. (X)