N29917

Part: DISPLAY — SHORTED (COCKPIT) · airframe 39,088 hrs · 29,956 cycles

THE CREW REPORTED THAT EICAS FAIL IN FLIGHT WITH ODOR OF BURNING ELECTRICAL. THE AIRCRAFT DIVERTED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE DISPLAY UNIT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 38,242 hrs · 29,331 cycles

PILOT REPORTED BURNING ODOR COMING FROM GALLEY ABOVE THE COFFEE POTS. MX PERFORMED OPERATIONAL CHECK OF COFFEEMAKERS WITH NO BURNING ODOR NOTED AT THIS TIME. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (ENGINE MOUNT) · airframe 36,477 hrs · 27,959 cycles

DURING C-CHECK, THE RT ENGINE LOWER FWD MOUNT YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE R & R THE FITTING IAW EC5450-01199. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 36,477 hrs · 27,959 cycles

DURING C-CHECK THE LT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS AT FRAME 75 STR 1L-2L. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03099. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 75) · airframe 36,477 hrs · 27,959 cycles

DURING C-CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS AT FRAME 75 AND STRINGERS 2R-3R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5330-03099. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: OIL SYSTEM — LEAKING (LEFT ENGINE) · airframe 34,987 hrs · 26,753 cycles

CREW REPORTED AN OIL ODOR COMING FROM NR 1 ENGINE BLEED. MAINTENANCE R & R NR 1 ENGINE. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — DIRTY (CABIN AIR) · airframe 34,975 hrs · 26,745 cycles

THE CREW REPORTED A VERY STRONG ODOR OF OIL IN FLIGHT. STRONGER IN DESCENT. MAINTENANCE INSPECTED AND CLEANED AIR DUCTS IAW 21-20-00. NO ODOR WAS NOTED AND ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 32,464 hrs · 24,790 cycles

CREW REPORTED THE AFT CABIN FLASHLIGHT WAS INOPERATIVE. INTIALLY WAS PLACED ON MEL 25-60-05. MAINTENANCE R & R THE FLASHLIGHT WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: GUSSET — CORRODED (FRAMES 14-18) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, CORROSION WAS FOUND AROUND TWO NUTPLATES ON CENTER OMEGA BEAM GUSSET, Y-0.0, BETWEEN FRAMES 14 & 18. R & R GUSSET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (FRAME 65-68) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, CARGO DOOR THRESHOLD FOUND CORRODED AT NUTPLATE HOLES. MAINTENANCE R & R THRESHOLD IAW SRM 51-40-02 AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: NUT PLATE — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 31,889 hrs · 24,356 cycles

DURING C-CHECK, CORROSION AROUND TWO NUTPLATES ON CENTER OMEGA BEAM GUSSET , Y-0.0, BETWEEN FRAMES 14 AND 18 AS MARKED IN CENTER FUSELAGE I. MAINTENANCE R & R GUSSETT AND 3 EA DOUBLERS ON FWD CENTER BEAM NR FRAME 14 IAW SRM 51-40-02, APPLIED PRIMER AND TOPCOAT IAW CPM 51-21-05, 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THRESHOLD — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,889 hrs · 24,356 cycles

DURING C-CHECK, CARGO DOOR THRESHOLD HAS CORROSION, AT NUTPLATES HOLES. R & R CARGO DOOR THRESHOLD IAW SRM 51-40-02 AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 53) · corrosion level 2 · airframe 31,889 hrs · 24,356 cycles

DURING C-CHECK, RT FLOOR SUPPORT AT FRAME 53 HAS CORROSION. MAINTENANCE R & R RT FLOOR SUPPORT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 31,889 hrs · 24,356 cycles

DURING C-CHECK, FOUND CORROSION AROUND NUTPLATE ON GUSSETT RT OMEGA BEAM, Y=479.0, FRAME 20. MAINTENANCE DETERMINED CORROSION AROUND NUTPLATE IN GUSSETT IS 100 PERCENT MATERIAL LOSS, R & R RT GUSSETT IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 61-63) · corrosion level 2 · airframe 31,889 hrs · 24,356 cycles

DURING C-CHECK RT FLOOR SILL IN CARGO AREA FRAMES 61-63 IS CORRODED. MAINTENANCE R & R FLOOR SILL AND SPLICE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 31,889 hrs · 24,356 cycles

DURING C-CHECK LAVATORY UNDER FLOOR OMEGA BEAM CAP IS CORRODED, LOCAL LEVEL 2, AS MARKED ON RT SIDE AROUND NUTPLATE. MAINTENANCE BLENDED CORROSION AROUND NUTPLATE 100 NR MATERIAL LOSS, R & R OMEGA BEAM CAP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 22) · corrosion level 2 · airframe 31,889 hrs · 24,356 cycles

DURING C-CHECK, CORROSION AROUND NUTPLATE BOTH NUTPLATES ON GUSSETT AT RT OMEGA BEAM, Y+479.0, FRAME 22. MAINTENANCE DETERMINED CORROSION AROUND NUTPLATE HAS 100 PERCENT MATERIAL LOSS, R & R RT GUSSETT IAW SRM 41-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 31,889 hrs · 24,356 cycles

DURING C-CHECK, CORROSION AROUND NUTPLATE ON CENTER OMEGA BEAM, Y=0.0, GUSSET AT FRAME 20. MAINTENANCE BLENDED CORROSION AROUND NUTPLATE ON CENTER OMEGA BEAM GUSSET AT FRAME 20, MATERIAL LOSS IS WITHIN LIMITS IAW SRM 53-21-10. PREPPED, ALODINED, PRIMED AND TOPCOATED IAW CPM 51-21-04, 51-21-05, 51-21-06. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (FRAME 81) · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED INBD OF STRINGER 12L WHERE THE APU CONTROL HARNESS CONNECTS. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW SRM 53-32-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CRACKED (FRAME 20) · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, STRINGER 3L AT FRAME 20 IS CRACKED. MAINTENANCE R & R STRINGER IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (FRAME 65) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK THE FRAME 65 SHEAR CLIP WAS FOUND TO BE CORRODED BETWEEN STRINGERS 15-16L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PARTITION — CORRODED (FRAME 61) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK CORROSION ON RT WALL DOUBLER AT FRAME 61 AT FLOOR LEVEL. MAINTENANCE DETERMINED CORROSION 100 PERCENT MATERIAL LOSS, REMOVED WALL DOUBLER, LOCATED, DRILLED, ALODINED AND INSTALLED NEW RT WALL DOUBLER AT FRAME 61 IAW SRM 51-20-03 AND SRM 51-40-02 AND CPM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — BROKEN (FRAME 10) · airframe 31,890 hrs · 24,356 cycles

FRAME 10 BENEATH PILOT'S DV WINDOW BROKEN. MAINTENANCE REMOVED BROKEN FRAME 10, LOCATED, DRILLED, ALODINED AND INSTALLED NEW FRAME 10 IAW SRM 53-00-04, 51-40-02, AND CPM 51-21-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 59-61) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK LAVATORY UNDER FLOOR OMEGA BEAM CAP IS CORRODED AS MARKED ON LT SIDE AROUND NUT PLATE. MAINTENANCE DETERMINED CORROSION ON OMEGA BEAM CAP LT SIDE FRAMES 59-61 IS 100 PERCENT MATERIAL LOSS IAW SRM 53-24-10. MAINTENANCE R & R LT GUSSET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — BROKEN (FRAME 10) · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, FRAME 10 BENEATH CO-PILOT'S DV WINDOW BROKEN. MAINTENANCE REMOVED BROKEN FRAME 10, LOCATED, DRILLED, ALODINED, AND INSTALLED NEW FRAME 10 IAW SRM 51-20-03, 51-40-03 AND CPM 51-14-05. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FRAME 20) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK THE CENTER AISLE CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK RT WING ACCESS PANEL 532AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION AND REMAINED WITHIN ALLOWABLE LIMITS IAW EC5720-01178. ACFT APPROVED FOR RETURN TO SERVICE.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, RT WING ACCESS PANEL 632AB FOUND CORRODED ON BACKSIDE AROUND FASTENER HOLES. MAINTENANCE BLENDED CORROSION. REMAINED WITHIN ALLOWABLE LIMITS IAW EC5720-01178. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (65) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, FRAME 65 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16-17L. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-31-04. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PARTITION — DAMAGED (ZONE 200) · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, BOTH SHOT BOLT HOLES FOR LT COCKPIT PARTION ARE ELONGATED. MAINTENANCE REMOVED CHAFED UPPER PIN GUIDE FABRICATED, LOCATED AND DRILLED UPPER PIN GUIDE DOUBLER IAW EC5320-017018. INSTALLED AND TOP COATED UPPER AND LOWER PIN GUIDES IAW EC5320-01708. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEARING CAP — CORRODED (NLG) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK CORROSION FOUND ON LT AND RT NLG BEARING CAPS. MAINTENANCE REPLACED LT AND RT NLG BEARING CAPS AND SHIMMED IAW AMM 32-20-01, FOR INSTALLATION SEE W04249, TASK 7021. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,890 hrs · 24,356 cycles

DURING C-CHECK, CARGO UNDERFLOOR SUPPORT 65-68 LT SIDE UNDER FLOORBOARD 271FF HAS CORROSION. MAINTENANCE R & R FLOOR SUPPORT IAW SRM 51-40-02 AND 53-31-10. ACFT APPROVED FOR RETURN TO SERVICE.

Part: CHECK VALVE — LEAKING (LEFT WING) · airframe 30,625 hrs · 23,420 cycles

THE CREW REPORTED FUEL LEAK ON TAKOFF FOR FIRST FIVE MINUTES THEN WHEN AT 10,000 FT AND REDUCED PITCH NO LEAK WAS NOTICED. MAINTENANCE INSPECTED AND REPLACED THE LEFT WING FUEL CHECK VALVE AT RIB 19. OPS CHECKED GOOD. NO LEAKS NOTED.

Part: YOKE — CRACKED (LT ENGINE) · airframe 29,514 hrs · 22,537 cycles

ACFT WAS IN FOR A 5A CHECK, WHEN INSPECTION FOUND NTHE LT FWD LWR ENGINE YOKE CRACKED. MX R & R THE ENGINE YOKE IAW EC 5450-01013. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: CONTROL MODULE — ODOR (CABIN LIGHTS) · airframe 28,742 hrs · 21,939 cycles

ELECTRICAL BURNING ODOR REPORTED COMING FROM FRONT OF CABIN. R & R THE PASSENGER CABIN LIGHTS CONTROL MODULE ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APRROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 28,697 hrs · 21,907 cycles

THE CREW REPORTED A ELECTRICAL BURN ODOR COMING FROM SEAT 1A AREA. MX INSPECTED AND FOUND LIGHT SOCKET SHORTED OUT AT LOCATION SIDEWALL PANEL ABOVE SEAT 1A. THE POWER SUPPLY BALLAST WAS DISCONNECTED. THE LT SIDEWALL LIGHT HARNESS ASSY WAS REPLACED AT SEAT 1A. OPS CHECKS WERE GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 24,426 hrs · 18,510 cycles

DURING CRUISE THE CREW REPORTED THAT THE AUTO-PRESSURIZATION FAILED AND DECLARED AN EMERGENCY. DIVERTING TO AEX WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OUTFLOW VALVE, PERFORMED OPERATIONAL CHECKS AND CLEARED THE DISCREPANCY.

Part: OUTFLOW VALVE — INTERMITTENT (CABIN PRESSURE) · airframe 24,426 hrs · 18,510 cycles

DURING CRUISE THE CREW REPORTED THAT THE AUTO-PRESSURIZATION FAILED AND DECLARED AN EMERGENCY DIVERTING TO AEX WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PNEUMATIC OUTFLOW VALVE, PERFORMED OPERATIONAL CHECKS AND CLEARED THE DISCREPANCY.

Part: KEY — SHORTED (FIRE TEST PANEL) · airframe 23,859 hrs · 18,081 cycles

CLE FLT 2043 - THE CREW REPORTED A NR 1 ENGINE FIRE INDICATION ON LANDING. THE CREW FOLLOWED MEMORY ITEMS THEN QRH. MESSAGE REMAINED AND EVSC PROCEDURE WAS FOLLOWED. THE ENGINE FIRE BOTTLES WERE BLOWN. MAINTENANCE INSPECTED AND NO ENGINE FIRE WAS DETECTED. INSPECTED AND FOUND THE FIRE DETECT PUSH TO TEST SWITCH WAS BAD. THE SWITCH WAS REPLACED. BOTH NR 1 AND NR 2 ENGINE FIRE BOTTLES WERE REPLACED. OPERATIONAL CHECKS OF THE ENGINE FIRE DETECT SYSTEM WAS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 23,794 hrs · 18,031 cycles

AC N29917 FERRIED INTO SHV BECAUSE OF GROUND DAMAGE BY LAVATORY TRUCK. SKIN PANEL AT FRAME 61-66 STRINGER 16R TO 19L HAS DAMAGE. FERRY FLIGHT CONDITIONS WERE TO "SECURE BOTH OUTFLOW VALVES, TRIM JAGGED MATERIAL FROM AROUND PUNCTURED AREAS, RE-CONTOUR PUNCTURE AREAS WITHOUT CAUSING FURTHER DAMAGE TO ADJACENT STRUCTURE, AND APPLY THREE LAYERS OF SPEED TAPE TO THE AFFECTED PUNCTURES FOR PURPOSE OF FERRY FLIGHT." UPON ARRIVING IN SHV, MAINTENANCE PERFORMED REPAIR ON SKIN PANEL AT FRAME 61-66 STRINGER 16R TO 19L IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: AHRS — INOPERATIVE (NR 1) · airframe 23,110 hrs · 17,511 cycles

IAH - FLIGHT 2945, THE CREW REPORTED A AHRS NR 1 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 AHRS UNIT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SELECTOR — OUT OF POSITION (COCKPIT) · airframe 22,255 hrs · 16,858 cycles

MTY - FLIGHT 2151DURING CLIMB THE CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT DIVERTED TO NTY WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE FREE FALL SELECTOR TO BE MOVED OUT OF THE DETENT POSITION. THE SWITCH WAS MOVED TO THE PROPER POSITION, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,245 hrs · 16,850 cycles

SHV - DURING C CHECK THE RT AFT SKIN WAS FOUND TO BE CRACKED AROUND FASTENERS (4 EACH) BETWEEN FRAMES 78-79 AND STRINGERS 3L-5L. MAINTENANCE REMOVED THE CRACKS AND PERFORMED BUSHING REPAIRS IAW EC5330-02162. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 22,245 hrs · 16,850 cycles

SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM 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: RELAY — FAILED (ANTI-ICE SYSTEM) · airframe 22,200 hrs · 16,819 cycles

AIRCRAFT 29917 - FLT 2056 IAH-MCI DIVERT TO SHV - WING ANTI-ICE FAIL MSG DURING TEST. FLIGHT DIVERTED DURING CRUISE. SHV MAINTENANCE REMOVED AND REPLACED RELAY K0528 IAW EMB-145 AMM 20-13-12, PERFORMED ANTI-ICE OPERATIONAL CHECK IAW EMB-145 AMM 30-00-00, OPERATIONAL CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOSE — LEAKING (AC BAY) · airframe 22,092 hrs · 16,739 cycles

FLIGHT 2038 - EWR - FLIGHT CREW REPORTED PACK NR 2 FAIL IN CLIMB. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED PACK HOSE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (MAIN) · airframe 21,349 hrs · 16,204 cycles

IAH - FLIGHT 2705, DURING TAKEOFF THE CREW REPORTED A BATTERY ONE OVERTEMP INDICATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE MAIN BATTERY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUT — LOW (NLG) · airframe 21,073 hrs · 16,004 cycles

IAH - FLIGHT 2573, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND A ENG 1-2 REV DISAGREE MESSAGE ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR TO REQUIRE SERVICING. MAINTENANCE SERVICED THE LANDING GEAR, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PIN — LOOSE (EMERGENCY LIGHT) · airframe 20,712 hrs · 15,749 cycles

IAH - DURING MAINTENANCE INSPECTION THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW 12 WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE-SECURED THE PIN AT SPLICE SP9208, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — CORRODED (SPOILER) · airframe 19,638 hrs · 14,934 cycles

FLIGHT NR 2941, THE CREW REPORTED HALFWAY DOWN TAKEOFF ROLL THEY RECEIVED A T/O CONFIG WARNING ON THE EICAS WITH SPOILER BOX ON THE EICAS RED. A SPOILER FAIL MESSAGE APPEARED AFTER PULLING OFF RUNWAY. THE ACFT TAXIED BACK TO THE GATE. MX INSPECTED AND REPLACED THE RT INBD SPOILER PROXIMITY SWITCH AND THE PROXIMITY SWITCH CONNECTOR. OPC CHECKS WERE GOOD.

Part: CONTROL MODULE — FAULTY (CABIN) · airframe 18,828 hrs · 14,361 cycles

FLIGHT 2152 - EWR - FLIGHT CREW REPORTED SMOKE AND SMELL IN THE GALLEY AREA AND LIGHTS FLICKERING. EWR MX REMOVED AND REPLACED GALLEY LIGHT CONTROL MODULE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO FLIGHT.

Part: PRESSURE SWITCH — DEFECTIVE (RUDDER SYSTEM) · airframe 18,129 hrs · 13,845 cycles

FLIGHT 2316 EWR FLIGHT CREW REPORTED RUDDER SYSTEM 1/2 INOP MSG ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFUL. EWR MX R&R RT RUDDER PRESSURE SWITCH AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (RUDDER SYSTEM) · airframe 18,129 hrs · 13,845 cycles

FLIGHT 2316 EWR FLIGHT CREW REPORTED RUDDER SYSTEM 1/2 INOP MSG ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFUL. EWR MX R&R LT AND RT RUDDER PRESSURE SWITCH AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — PUNCTURED (SERVICE DOOR)

ACFT IS PRESENTLY IN A C-CHECK STATUS AND THE SERVICE DOOR WAS FOUND WITH A PUNCTURE TO THE UPPER FRAME. MX CUT OUT THE AFFECTED AREA AND FABRICATED A L-SHAPE DOUBLER AFTER CONTOURING THE AREA. ALODINED, PRIMED AND PAINTED. INSTALL IAW EC52-40-01040 AND THE SRM. ACFT WILL BE RELEASED UPON COMPLETION OF WORK. (S)

Part: ESCAPE HATCH — DIRTY (EMERGENCY EXIT) · airframe 16,798 hrs · 12,917 cycles

RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND LEFT EMERGENCY OVERWING EXIT HATCH HARD TO OPEN. MX CLEANED AND LEFT EMERGENCY OVERWING EXIT HATCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BEZEL — INOPERATIVE (NR 2) · airframe 16,715 hrs · 12,855 cycles

EWR FLIGHT 2396 - THE CREW REPORTED THE F/O'S ALTIMETER ADJUSTMENT WAS INOPERATIVE DURING DESCENT INTO DTW. UNABLE TO LAND CAT II IN DTW THE FLIGHT WAS DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PFD BEZEL. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: VALVE — FAULTY (LT BRAKE) · airframe 16,258 hrs · 12,516 cycles

IAH - FLIGHT 2081, THE CREW REPORTED THE LEFT OUTBOARD BREAK TO BE LOCKED WITH FULL AMBER TEMP. MAINTENANCE REMOVED AND REPLACED THE O/B BRAKE CONTROL VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — UNRELIABLE (MLG DOOR) · airframe 15,465 hrs · 11,925 cycles

FLT 2296 - EWR - CREW REPORTED THAT NOSE GEAR DOORS OPENED UN-COMMANDED AT 3000 FT AND 210 KNOTS. EWR MX REMOVED AND REPLACED LGEU IAW EMB145 AMM 32-32-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 12,331 hrs · 9,518 cycles

SHV DURING C-CHECK, RT OMEGA BEAM HAS AREA OF CORROSION AROUND NUTPLATE NEAR FS 23. MAINTENANCE REPAIRED RT OMEGA BEAM NEAR FS 23 IAW EC5320-01228. THE AIRCRAFT IS APPROVED TO RETURN FOR SERVICE.

Part: FLASHLIGHT — ODOR (COCKPIT)

CREW REPORTED, ALL CREW MEMBERS NOTICED AN INSULATION WIRE BURNING SMELL BEHIND CAPTAINS SEAT AND BEHIND THE FLIGHT ATTENDANTS SEAT. GATE RETURNED AIRCRAFT, DURING TAXI. MAINTENANCE INSPECTED NR 1 AND NR 2 RELAY COMPARTMENTS AND RIGHTHAND AND LEFTHAND POWER DISTRIBUTION BOX NO DAMAGE FOUND IAW EMB145 AMM 20-13-02. FOUND FLIGHT ATTENDANT AND CAPTAINS FLASHLIGHT BASE [HOLDER] MELTED. REMOVED AND REPLACED CAPTAINS AND FLIGHT ATTENDANTS FLASHLIGHT ASSEMBLY IAW EMB33-50-16, OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 4,818 hrs · 8,961 cycles

FOUND DENT ON RT SIDE OF AIRCRAFT BETWEEN FRAMES 29R AND 30R. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER, DRILLED, COUNTERSUNK, ALODINED AND PRIMED. DYE PEN'D AREA NO DEFECTS FOUND. INSTALLED FILLER AND DOUBLER. ALL WORK ACCOMPLISHED IAW EMB145 SRM 53-22-01 AND EMB145 AMM 21-31-00. PRESSURE CK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: STRUT — FAILED (NLG) · airframe 9,757 hrs · 7,489 cycles

CREW REPORTED LANDING GEAR AIR/GROUND FAIL MESSAGE AND ENG 1-2 REVERSER DISAGREE MESSAGE ON EICAS IN FLIGHT. MX INSP AND REPLACED NLG ASSEMBLY. OPS CHECKS GOOD.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 7,606 hrs · 5,817 cycles

SHV - DURING C-CHECK THE CROSSBEAM AT FRAME 23 FROM THE SERVICE DOOR AFT SILL TO THE RIGHT HAND OMEGA BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CROSSBEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — GROOVED (RUDDER) · airframe 7,606 hrs · 5,817 cycles

SHV - DURING C-CHECK THE RUDDER LOWER ACTUATOR FITTING WAS FOUND TO BE GROOVED. MAINTENANCE REMOVED THE UNDERSIZED BUSHING, OVERSIZED THE HOLE ON THE FITTING TO ACCEPT AN OVERSIZED BUSHING AND INSTALLED THE OVERSIZED BUSHING IAW EC5540-01029. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 7,606 hrs · 5,817 cycles

SHV - DURING C-CHECK THE T-REINFORCEMENT ON STRINGER 19L WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A REINFORCEMENT ANGLE IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 7,606 hrs · 5,817 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,606 hrs · 5,817 cycles

SHV - DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 53-21-10, STEP 2, FIG 201, SHEET 1. THE AIRCRAFT WILL BE APPROVED FOR RETURN TO SERVICE UPON COMPLETION OF C-CHECK.

Part: DAU — FALSE INDICATION (ENGINE) · airframe 6,122 hrs · 4,652 cycles

AT TAKEOFF PRIOR TO 80 KNOTS BOTH ENGINE PRESSURE IN AMBER AT 105 PSI AND RIGHT ENGINE IN THE RED. NO ALARMS. ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 DAU IAW EMB AMM 31-41-01. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (MLG)

STL- FLIGHT 2463, ON CLIMB THE CREW NOTED THAT THE LANDING GEAR WILL NOT RETRACT MESSAGE APPEARED ON THE EICAS. THE CREW RETURNED THE AIRCRAFT TO STL AND LANDED WITHOUT INCIDENT. STL- MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM, NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — GOUGED · airframe 3,726 hrs · 2,670 cycles

SHV- DURING C CHECK LEFT HAND LOWER COWLING WAS FOUND TO HAVE A GOUGE INSIDE INBOARD OF ACCESS TO AIR STARTER VALVE. MAINTENANCE REMOVED DAMAGE AND PERFORMED AN ANGLE REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ACTUATOR — INOPERATIVE (HORIZ STAB) · airframe 16 hrs · 8 cycles

ORF FLIGHT 3365. PILOT REPORTED THAT EN ROUTE TO ORF THE AUTO TRIM ALONG WITH THE PITCH TRIM NR 1 FAILED. FIFTEEN MINUTES LATER THE BACK-UP TRIM SYSTEM NR 2 FAILED AND THE SYSTEM STUCK AT +1. THE CREW ACCOMPLISHED A EMERGENCY LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE SYSTEM AND FOUND THE HORIZONTAL STABILIZER ACTUATOR INOPERATIVE. THE ACTUATOR WAS REMOVED AND REPLACED IAW EMB-145 MM 27-40-02, ALL OPERATIONAL AND LEAK CHECKS WERE SATISFCATORY. THE AIRCRAFT RELEASED FOR SERVICE.