N13979

Part: ACTUATOR — FAULTY (HORIZ STAB) · airframe 44,472 hrs · 33,965 cycles

THE CREW REPORTED MAIN PITCH TRIM INOP IN FLIGHT. AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED HORIZONTAL STAB ACTUATOR IAW 27-40-02. OPERATIONAL CHECKS WERE GOOD.

Part: HINGE FITTING — FAILED (RUDDER) · airframe 44,144 hrs · 33,694 cycles

THE CREW REPORTED A LOW FREQUENCY VIBRATION THROUGH THE AIRFRAME. THE AIRCRAFT LANDED AT JAN WITHOUT INCIDENT. MX INSPECTED THE AIRCRAFT AND FOUND THAT ALL OF THE RUDDER TWO HINGE FITTINGS TO BE DAMAGED WITH THE UPPER FITTING TO BE SHEARED. REMOVED AND REPLACED BOTH RUDDER 1 AND RUDDER 2. THE RUDDER II UPPER HINGE FITTING WAS DETERMINED TO BE THE CAUSE OF THE MALFUNCTION.

Part: ACTUATOR — MALFUNCTIONED (NLG)

EXPERIENCED A STRONG SHIMMY & SWERVING MOVEMENT FROM THE NOSE WHEEL AREA RIGHT AT V1. MAINTENANCE REPLACED THE NWA IAW AFDL A968286. LUBED NLG TORQUE LINKS IAW AMM 32-20-10. OCF REQUIRED FOR OPS CHECK IAW AFDL A968288. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (ROWS 23A-24A) · airframe 43,902 hrs · 33,480 cycles

MAINTENANCE REPORTED THE AISLE EMERGENCY LIGHT STRIP AT ROW 23A AND 24A WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT. OPS CHECKED GOOD.

Part: ENGINE — LEAKING (NR 1) · airframe 42,555 hrs · 32,382 cycles

THE CREW REPORTED FUMES IN THE COCKPIT AND FORWARD CABIN FROM PACK 1, THE AIRCRAFT RETURNED TO DEPARTURE, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 42,247 hrs · 32,139 cycles

PILOT REPORTED EMERGENCY EXIT LIGHT NR 3 INOPERATIVE. MX PERFORMED OPERATIONAL CHECK, CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MOUNT — CRACKED (ENGINE) · airframe 41,033 hrs · 30,912 cycles

DURING A C-CHECK. RIGHT FWD LOWER ENGINE MOUNT CRACKED. REMOVED AND REPLACED ENGINE MOUNT IAW EC5450-01211. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 35,956 hrs · 27,189 cycles

DURING C-CHECK, THE LT OTBD FLAP INBD FLAP TRACK ROOT FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FITTING IAW EC5750-01630. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (RT WING TE FLAP) · airframe 35,956 hrs · 27,189 cycles

DURING C-CHECK THE RT OTBD FLAP INBD FLAP TRACK ROOT FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FITTING IAW EC5750-01631. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (FRAME 60-61) · corrosion level 2 · airframe 35,956 hrs · 27,189 cycles

DURING C-CHECK THE LAV WASTE DRAIN VALVE SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,406 hrs · 25,256 cycles

DURING MX INSPECTION, THE SEAT 12BC EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. R & R EMERGENCY EXIT & OPS CHECKED SUCCESSFUL. ACFT RETURNED TO SERVICE.

Part: TRANSDUCER — FAULTY (WHEEL SPEED) · airframe 31,932 hrs · 24,074 cycles

CREW REPORTED ON LANDING ROLLOUT-BRAKING WAS ALMOST NIL UNTIL 100KTS, THEN NORMAL BRAKE RESPONSE CAME BACK TO NORMAL. MX R & R NR 2 WHEEL SPEED TRANSDUCER WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DIRTY (LAVATORY) · airframe 31,895 hrs · 24,043 cycles

CREW REPORTED INTERMITTENT LAVATORY SMOKE ON EICAS WITH NO SMOKE OR ANY FIRE NOTED IN LAVATORY BY F/A. MX CLEANED THE LAVATORY SMOKE SENSOR AND R & R THE SMOKE DETECTOR PANEL, OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,752 hrs · 23,919 cycles

THE FLOOR PATH EMERGENCY LIGHT AT ROW 12 WAS FOUND INOPERATIVE. R & R THE FLOOR PROX EMERGENCY LIGHT AT ROW 12 WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CAP — LOOSE (OIL SYSTEM) · airframe 31,582 hrs · 23,794 cycles

SMOKE AND STRONG ODOR OF BURNED FLUID AFTER SHUTTING DOWN NR 1 ENGINE AT THE GATE COMING OUT THE BACK OF THE ENGINE. POSITIONED NR 1 ENGINE OIL FILLER CAP AND CLEANED RESIDUAL OIL FROM COWLING. CHECKED FLUID LEVEL AND PERFORMED ENGINE RUN WITH NO LEAKS NOTED. ACFT RELEASED AND RETURNED TO SERVICE.

Part: BUSHING — MIGRATED (ATTACH BRACKET) · airframe 31,009 hrs · 23,331 cycles

DURING C-CHECK RT GROUND SPOILER INBD ATTACHMENT FITTING, OTBD HAT BUSHING IS MIGRATED (ON WING). MX R & R RT GROUND SPOILER INBD ATTACHMENT FITTING IAW AMM 57-51-02 AND EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ATTACH BRACKET) · airframe 31,009 hrs · 23,331 cycles

DURING C-CHECK, LT GROUND SPOILER INBD ATTACH BRACKET OTBD HAT BUSHING MIGRATED. MX R & R ATTACH BRACKET IAW AMM 57-51-02 AND EC5740-01288. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ZONE 500) · airframe 31,009 hrs · 23,331 cycles

DURING C-CHECK, LT GROUND SPOILER OTBD ATTACHMENT BRACKET INBD HAT BUSHING MIGRATED ON WING. MX R & R LT GROUND SPOILER OTBD ATTACHMENT BRACKET IAW AMM 57-51-02 AND EC5740-01288. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (ATTACH BRACKET) · airframe 31,009 hrs · 23,331 cycles

DURING C-CHECK, LT GROUND SPOILER CENTER ATTACH BRACKET INBD HAT BUSHING MIGRATED ON WING. MX R & R ATTACHING BRACKET ON WING IAW AMM 57-51-02 AND EC5740-01288. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,009 hrs · 23,331 cycles

DURING C-CHECK, FRAME 75 FITTING BETWEEN STR 2R-2L HAS CORROSION AT OTBD MAIN BOLT HOLES. MX PERFORMED REPAIR ON FRAME 75 FITTING BETWEEN STR 2R-2L IN IAW EC5310-01627 AND CPM 51-21-06. ACFT APPROVED FOR RETURN TO SERVICE.

Part: ATTACH FITTING — MIGRATED (ZONE 600) · airframe 31,009 hrs · 23,331 cycles

DURING C-CHECK RT GROUND SPOILER OTBD ATTACH FITTING INBD HAT BUSHING IS MIGRATED (ON WING). MX R & R RT GROUND SPOILER OTBD ATTACHMENT FITTING (ON WING) IAW AMM 57-51-02 AND EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (RT MLG) · airframe 29,694 hrs · 22,297 cycles

THE CREW REPORTED A LOUD BANGING NOISE FROM UNDER THE COCKPIT IN FLIGHT. REPORTED POSSIBLY NOSE GEAR DOOR SLAMMING SHUT. MX INSPECTED AND REPLACED BOTH RT GEAR WOW PROXIMITY SWITCHES. BOTH WERE FOUND TO PRODUCE AN INTERMITTENT FAULT. OPS CHECKS WERE GOOD.

Part: HANDLE — LOOSE (ZONE 800) · airframe 27,645 hrs · 20,637 cycles

ACFT WAS FERRIED FOR A MAIN PAX DOOR THAT WOULDN'T OPEN FROM THE OUTSIDE. MX FOUND THE INTERNAL HANDLE BRACKET HARDWARE LOOSE AND THE DOOR STOPS SHIMS LOOSE. TIGHTEN ALL HARDWARE IAW AMM 52-18-00-820-801-A STEP 2I AND 52-18-00-820-014-A RESPECTIVELY; OPS CHECK WAS GOOD. REPLACE MAIN DOOR LINER IAW AMM2 25-23-09-400-801-A. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,022 hrs · 20,095 cycles

DEN - DURING MAINTENANCE INSPECTION THE FIRST FOUR AISLE PATH EMERGENCY LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 26,916 hrs · 20,006 cycles

ELP - FLIGHT 6085, THE CREW REPORTED THAT THE FORWARD FOUR EMERGENCY LIGHT STRIPS WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY OVER THE SERVICE DOOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,168 hrs · 19,438 cycles

SHV - DURING C-CHECK STRINGER 19L IS CORRODED (LEVEL 2 LOCAL) AT FRAME 61. MAINTENANCE REPAIRED STRINGER 19L AT FRAME 61 IAW EMB-145 SRM 53-00-03 FIG 205. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 26,168 hrs · 19,438 cycles

SHV - DURING C-CHECK LT HORIZONTAL STAB LEADING EDGE HAS CORROSION (LEVEL 2 LOCAL) AT UPPER AND LOWER SURFACE AROUND RIVETS. MAINTENANCE REMOVED CORROSION BY POLISHING THE HORIZONTAL STAB L/E IAW THE POLISHING TYPICAL REPAIR EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,168 hrs · 19,438 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) AT STINGER 18L BETWEEN FRAME 60 & 61. MAINTENANCE REPAIRED DAMAGED SECTION OF STRINGER 18L BETWEEN FRAME 60-61 IAW EMB-145 SRM 53-00-03 FIG 205. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,168 hrs · 19,438 cycles

SHV - DURING C-CHECK CORROSION (LEVEL 2 LOCAL) ON LT OMEGA BEAM AT CROSSBEAM FRAME 38. MAINTENANCE REPAIRED LT OMEGA BEAM AT CROSSBEAM AT FRAME 38 IAW EMB-145 SRM 53-10-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — BROKEN (FUSELAGE) · airframe 26,168 hrs · 19,438 cycles

SHV - DURING C-CHECK LT FRAME 10 BROKEN UNDER DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED LT FRAME 10 UNDER DV WINDOW FRAME IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,873 hrs · 18,487 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EXIT SIGN IN FRONT OF SEAT 3B INOPERATIVE. MX REMOVED AND REPLACED INVERTER NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: PROXIMITY SWITCH — LOOSE (RT MLG) · airframe 23,997 hrs · 17,828 cycles

TYS - A/C LEFT BNA WHEN THE GEAR WOULDN'T RETRACT, CREW MADE A UNSCHEDULED LANDING BACK TO BNA AND SWAPPED A/C. MAINTENANCE FOUND THE RIGHT SIDE PROX SWITCH LOOSE. RE-SECURED THE PROX SWITCH AND SWUNG THE GEAR SIX TIMES, LET SET FOR THIRTY MINUTES AND RE-SWUNG THE GEAR. ALL CHECKS WERE GOOD AND WAS RELEASED BACK TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 23,539 hrs · 17,467 cycles

IAH - DURING MAINTENANCE INSPECTION, A BURNING SMELL WAS NOTICED AT ROW 7A. MAINTENANCE INSPECTED AND PLACED THE LIGHT ON MEL 33-20-00/1, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE REMOVED AND REPLACED THE CABIN SIDEWALL LIGHT ASSEMBLY AT ROW 7A. OPERATIONAL CHECKS WERE GOOD. REMOVED FROM MEL.

Part: PROXIMITY SWITCH — INOPERATIVE (RT MLG) · airframe 23,029 hrs · 17,074 cycles

IAH - FLIGHT 2944 - THE CREW REPORTED, PERFORMED AN AIR RETURN DUE TO A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE RIGHT "A" PROX SWITCH, AND ADJUSTED THE AIR GAP ON THE LEFT WOW PROXIMITY SWITCH. OPERATIONALLY TESTS WERE PERFORMED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,164 hrs · 16,435 cycles

IAH - DURING MX INSPECTION THE EMERGENCY EXIT SIGN AT SEAT 3BC BULKHEAD WAS FOUND TO BE INOPERATIVE. MX R&R THE AFFECTED EMERGENCY EXIT SIGN, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (AC BAY) · airframe 21,814 hrs · 16,165 cycles

RSW - FLIGHT 3146 - THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN AND PASSENGERS REPORTED HEARING A LOUD POPPING SOUND WHILE CLIMBING THROUGH 14,000 FEET. THE CREW FOLLOWED THE QRH PROCEDURES, AND THE AIRCRAFT RETURNED TO RSW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO PACK ON MEL 21-24-01/1 CAT C CTL NR 158685, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ACM, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED

AC WAS ENROUTE WHEN THEY GOT A LG AIR/GND FAIL MESSAGE. AC DIVERTED WHERE MAINT PERFORMED MULTIPLE GEAR RETRACTIONS AND THE GEAR RETRACTED NORMALLY. NO INDICATIONS. AC RELEASED TO SERVICE IAW EMB 32-30. (K)

Part: FIREWALL — CRACKED (APU) · airframe 21,296 hrs · 1,578 cycles

SHV DURING C-CHECK APU FIREWALL CRACKED AT LT UPPER, RT LOWER APU MOUNTS. MX REPAIRED APU FIREWALL LT UPPER, RT LOWER APU MOUNTS IAW EC5330-01838. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,495 hrs · 15,246 cycles

FLIGHT 2172 -FLIGHT CREW REPORTED ELECTRICAL BURNING SMELL IN AC. MX PERFORMED EXTENSIVE INSPECTION AND ELECTRICAL TESTS, BUT COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 19,933 hrs · 14,895 cycles

FLIGHT 2142 - MKE - CREW REPORTED LANDING GEAR AIR/GRND FAIL MESSAGE ON EICAS. AIR/GRND C/B WAS RESET AND MESSAGE WAS CLEARED ON EICAS. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 18,857 hrs · 14,163 cycles

PILOT REPORTED BURN SMELL IN COCKPIT. MAINTENANCE OPS CHECKED TAT & PITOT HEAT RELAYS, CHECKED COOLING FANS IN FWD AVIONICS ALL OPS CHECKED GOOD. COULD NOT DUPLICATE PROBLEM. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (LT MLG) · airframe 17,999 hrs · 13,546 cycles

IAH - FLIGHT 2099, THE CREW REPORTED A LANDING GEAR AIR/GRND FAILURE INDICATION ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND WEIGHT ON WHEELS PROXIMITY SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 16,243 hrs · 12,134 cycles

SHV - DURING C CHECK, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (CABIN) · airframe 16,243 hrs · 12,134 cycles

SHV - DURING C CHECK AN EDDY CURRENT INSPECTION OF THE MAIN DOOR STOP ATTACHMENT HOLE ON FRAME 15 AT STR 14L INDICATED A CRACK. MAINTENANCE REAMED THE AFFECTED HOLE AND SUBSEQUENT DYE PENETRANT INSPECTION IAW EC 5310-01386 REVEALED NO RELEVANT INDICATIONS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 16,243 hrs · 12,134 cycles

SHV - DURING C CHECK, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — FAULTY (CABIN) · airframe 16,059 hrs · 11,992 cycles

EWR, CREW REPORTED THE EMERGENCY EXIT LIGHT STRIP [AISLE] AT ROW 11/12 IS NOT OPERATING. MAINTENANCE REMOVED AND REPLACED AISLE PATH STRIP AT ROW 11/12 IAW EMB145 MM 33-50-12, OPS CHECKED GOOD.

Part: FIRE LOOP — FAULTY (NR 2 ENGINE) · airframe 15,555 hrs · 11,595 cycles

EWR-CO3206, CREW REPORTED, ENGINE TWO FIRE DETECTOR FAIL INDICATION DURING CRUISE ON EICAS. MESSAGE DISAPPEARED AFTER 30 MINUTES UPON LEVELING OFF AT 16,000 FT. MAINTENANCE REMOVED AND REPLACED NUMBER TWO ENGINE FIRE DETECTION LOOP IAW EMB145 AMM 26-11-01 AND EMB 145 AMM 26-10-01. SYSTEM OPS CHECKED GOOD.

Part: CONTROL UNIT — DEFECTIVE (COCKPIT) · airframe 14,372 hrs · 10,685 cycles

CLE FLIGHT 2266, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL MODULE AND THE LANDING GEAR ELECTRONIC UNIT. TEST FLIGHT WAS PERFORMED AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. P/N LANDING GEAR MODULE: 7-45550-3, S/N:0164 CSO:9073, TSO:11880.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 10,875 hrs · 8,118 cycles

EWR - FLIGHT 2879, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 10,875 hrs · 8,118 cycles

EWR - FLIGHT 2879, THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT STAY ON. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 11,385 hrs · 8,388 cycles

SHV- DURING C-CHECK THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE FOUND THE NR 1 EMERGENCY LIGHT BATTERY DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (CABIN) · airframe 11,385 hrs · 8,388 cycles

DURING C-CHECK STRINGER 19L WAS FOUND TO BE CORRODED. REPLACED STRINGER P/N 145-25768-017 USING SPLICE REPAIR TO THE AFFECTED STRINGER IAW EMB 145 SRM 53-00-03 ITEM 7 FIGURE 205. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (CABIN) · airframe 11,385 hrs · 8,388 cycles

SHV - DURING C-CHECK STRINGER 17L WAS FOUND TO BE CORRODED BETWEEN FRAME 61 TO 65. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRINGER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (CARGO DOOR) · airframe 10,703 hrs · 7,846 cycles

DURING A SCHEDULED MODIFICATION THE CARGO DOOR LOWER SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CARGO DOOR SILL AND THRESHOLD PLATE. INSTALL A NEW DOOR SILL IAW EMB 135/145 SRM 51-40-02. LEAK CHECKS GOOD IAW EMB 145 AMM 21-31-00. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED UPON COMPLETION OF ALL WORK.

Part: WIRE — BROKEN (CABIN)

A/C 979 WAS IN FOR A SERVICE CHECK AND MAINT FOUND ONE OF THE EMERGENCY LIGHT AISLE STRIPS INOP NR 4. MAINT REPAIRED THE BROKEN WIRE AT EMERGENCY STRIP NR 4 IAW EMB 145 AMM 20-21-00, OPS CHECK GOOD IAW EMB 145 AMM 33-50-00. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED TO SERVICE.

Part: LIGHT — INOPERATIVE (ROW 1-7)

DURING PREFLIGHT INSPECTION THE FLOOR PROXIMITY LIGHT AT ROWS 1 THROUGH 7 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED THE LIGHTING SYSTEM, AND CLEARED THE DISCREPANCY.

Part: LIGHT — INOPERATIVE (ROWS 8-9)

CLE FLIGHT 2623, THE CREW REPORTED THE EMERGENCY AILSE PATH LIGHTS WERE INOPERATIVE AT ROW 8-9. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 33-20-00.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 8,528 hrs · 6,124 cycles

A PUNCTURE WAS FOUND IN THE EXTERIOR SKIN APPROX 12 INCHES AFT OF THE SERVICE DOOR. MAINTENANCE CUT OUT THE DAMAGED AREA, FABRICATED A DOUBLER AND FILLER, AND INSTALLED. ALODINED, PRIMED AND PAINTED. PRESSURE CHECKED GOOD I/A/W-EMB-SRM-53-21-01, CMP-51-21-04/05/06. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE.

Part: LIGHT — FAULTY · airframe 7,778 hrs · 5,537 cycles

CLE---CO2245, CREW REPORTED, EMERGENCY LIGHTS ROWS 8AND9 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT STRIP IAW EMB145 AMM #33-50-10. OPS.CHECKED GOOD.

Part: FRAME — GOUGED · airframe 7,532 hrs · 5,334 cycles

TYS, During a scheduled inspection, the first frame behind the cargo compartment (frame 68) has several gouges, Maintenance burnished the gouges I/A/W-EMB145-SRM-51-10-02, CMP-51-21-04 and 05. Aircraft was released to service.

Part: BEAM — CORRODED (FUSELAGE) · airframe 7,532 hrs · 5,334 cycles

DURING A SCHEDULED INSPECTION THE LEFT OMEGA BEAM AT FRAME 20 HAS CORROSION AT CROSS BEAM. MAINTENANCE REPAIRED THE CORRODED AREA, PRIMED AND PAINTED. I/A/W-EMB-145-SRM-53-21-10. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE.

Part: BUSHING — LOOSE · airframe 7,532 hrs · 5,334 cycles

TYS, During a scheduled inspection, the left hand vertical stab spherical bushings where found loose. Maintenance reamed the hole for oversized bushing and alodined and installed bushings. I/A/W-EC5510-001045. The repair was satisfactory and the aircraft was released to service.

Part: CHECK VALVE — INOPERATIVE · airframe 7,532 hrs · 5,334 cycles

TYS, During a scheduled inspection, the parking brake system failed operational check of the return line valve. Maintenance removed and replaced the return line check valve. operational checked good. I/A/W-EMB-145-AMM-32-44-08 and 01. Aircraft released to service.

Part: SPEED BRAKE — DAMAGED · airframe 7,532 hrs · 5,334 cycles

TYS, During a scheduled inspection, composite damage was found to leading edge of left speed brake. Maintenance repaired the damage. I/A/W-EC5750-01190. The repair was satisfactory and the aircraft was released to service.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 7,532 hrs · 5,334 cycles

TYS, DURING A SCHEDULED INSPECTION THE RIGHT FUSELAGE Z CHANNEL AT FRAME 23 IS CORRODED. MAINTENANCE REMOVED AND REPLACED THE Z CHANNEL AT FRAME 23. IAW EMB-145 SRM 51-40-02. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WAS RELEASED TO SERVICE.

Part: FRAME — CHAFED (FUSELAGE) · airframe 7,532 hrs · 5,334 cycles

DURING A SCHEDULED INSPECTION, FRAME 63, FORWARD OF THE CARGO DOOR, HAS AREAS OF CHAFE MARKS. MAINTENANCE BURNISHED THE CHAFFED AREA, ALODINED, PRIMED AND PAINTED.IAW-EMB-145-SRM-51-10-02, 51-21-04, 05 AND 06. AIRCRAFT RELEASED TO SERVICE.

Part: CHANNEL — DISTORTED · airframe 7,532 hrs · 5,334 cycles

TYS, During a scheduled inspection a support channel between the cockpit floor beam and frame 13L was found distorted. Maintenance removed and replaced the channel. I/A/W-EMB-145-SRM-53-12-10 and 51-40-02. The repair was satisfactory and the aircraft was released to service.

Part: STRINGER — GOUGED · airframe 7,532 hrs · 5,334 cycles

TYS, During a scheduled inspection, External stringer 19L gouged at frame 54. Maintenance blended the gouge, fabricated a doubler, installed, primed and painted. I/A/W-EMB145-SRM-53-24-02, CMP-51-21-02, 04 and 06. The repair was satisfactory and the Aircraft was released to service.

Part: FRAME — CHAFED (FUSELAGE) · airframe 7,532 hrs · 5,334 cycles

DURING A SCHEDULED INSPECTION, FRAME 65, FORWARD OF THE CARGO DOOR, HAS AREAS OF CHAFE MARKS. MAINTENANCE BURNISHED THE CHAFED AREA, ALODINED, PRIMED AND PAINTED.I/A/W-EMB-145-SRM-51-10-02, 51-21-04, 05 AND 06. AIRCRAFT RELEASED TO SERVICE.

Part: BUSHING — GOUGED · airframe 7,532 hrs · 5,334 cycles

TYS, During a scheduled inspection, the right hand vertical stab spherical bushings where found gouged. Maintenance reamed the hole for oversized bushing and alodined and installed bushings. I/A/W-EC5510-001045. The repair was satisfactory and the aircraft was released to service.

Part: FRAME — CHAFED (FUSELAGE) · airframe 7,532 hrs · 5,334 cycles

DURING A SCHEDULED INSPECTION, FRAME 64, FORWARD OF THE CARGO DOOR, HAS AREAS OF CHAFE MARKS. MAINTENANCE BURNISHED THE CHAFFED AREA, ALODINED, PRIMED AND PAINTED.I/A/W-EMB-145-SRM-51-10-02, 51-21-04, 05 AND 06. AIRCRAFT RELEASED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 7,532 hrs · 5,334 cycles

DURING A SCHEDULED INSPECTION THE RIGHT HAND SERVICE DOOR SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST 1927/02A, EMB-145 SRM 51-40-02, CPM 51-21-04, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: FLOOR SUPPORT — CORRODED (CENTER FLOOR) · airframe 7,532 hrs · 5,334 cycles

DURING A SCHEDULED INSPECTION THE CENTER FLOOR SUPPORT HAT BEAM TOP CAP WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A DOUBLER REPAIR IAW EMB SRM 53-21-10, CPM 51-21-04, & 05, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 7,532 hrs · 5,334 cycles

DURING A SCHEDULED INSPECTION THE LT HAND SERVICE DOOR SILL PLATE WAS FOUND TO BE CORRODED. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST 1927/02A, EMB-145 CPM 51-21-04,05 & 06, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: ANGLE — CORRODED (GALLEY FLOOR) · airframe 7,532 hrs · 5,334 cycles

DURING A SCHEDULED INSPECTION THE RT GALLEY RAMP ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RAMP ANGLE IAW EMB-145 SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: CONTROL HANDLE — INTERMITTENT (COCKPIT)

CLE FLIGHT 3051 THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM CLEVELAND. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR CONTROL ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ODOR — DETECTED (CABIN)

IAH- THE CREW NOTED THAT FUMES IN THE CABIN, ISOLATED TO NR 2 PACK. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE NR 2 PACK, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BELLCRANK — CRACKED (ELEVATOR) · airframe 6,027 hrs · 4,156 cycles

TYS DURING A SCHEDULED EA INSPECTION EA 2730-01044 A CRACK WAS FOUND IN LEFT BELL CRANK ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE QUADRANT IAW AMM 27-31-03. OPS CHECK WAS GOOD AND WILL BE RELEASED UPON COMPLETION OF ALL CHECKS.

Part: INVERTER — BLOWN (CABIN) · airframe 5,614 hrs · 3,875 cycles

TYS DURING A SCHEDULED INSPECTION THE AFT EMERGENCY LIGHTS WERE INOP. MAINTENANCE R/R THE THE AFT EMERGENCY LIGHT INVERTER IAW EMB.145MM 33-50-04. OPS CHECK WAS GOOD AND AIRCRAFT WAS REL. FOR SERVICE.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 5,614 hrs · 3,875 cycles

TYS DURING A SCHEDULED INSPECTION THE EMERGENCY BATTERY AT #4 COMPARTMENT WAS INOP. MAINTENANCE R/R THE EMERGENCY BATTERY IAW EMB. 33-50-04. OPS CHECK WAS GOOD AND WAS REL. FOR SERVICE.

Part: BATTERY — DISCHARGED

BNA - The last two emergency aisle path lights were found to be inoperative. Maintenance removed and replaced the #4 emergency light battery pack. An operational test of the aisle path lighting was performed successfully and the aircraft was returned to service.

Part: BATTERY — DISCHARGED (CABIN)

IAH- DURING POST FLIGHT THE CREW NOTED THAT THE REAR EMERGENCY FLOOR LIGHTS FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY BATTERY, PERFORMED A OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (INTERIOR)

EWR---CO4130, "FLOOR EMERGENCY LIGHT WILL NOT COME ON, AND TOP EMERGENCY SIGN." MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT DC/AC INVERTER IAW EMB145 AMM #33-50-11. OPS.CHECKED GOOD.

Part: BATTERY — DISCHARGED (CABIN)

IAH- DURING PERFLIGHT THE CREW NOTED THAT THE EMERGENCY ISLE PATH LIGHTING FAILED TO ILLUMINATE. IAH- MAINTENANCE REMOVED AND REPLACED THE BATTERY, PERFORMED A OPERTIONAL CHECK,NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - FLIGHT 4256, DURING PREFLIGHT INSPECTION, THE CREW REPORTED AN AISLE PATH EMERGENCY EXIT LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.