N14938

Part: SOCKET — SHORTED (CABIN LIGHTS) · airframe 32,273 hrs · 31,599 cycles

THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN FRONT CABIN. MAINTENANCE INSPECTED AND FOUND THE OVERHEAD LIGHT SOCKET SHORTED AND MELTED. R & R AFFECTED HARNESS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 31,321 hrs · 30,664 cycles

DURING 2A INSPECTION, THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77, BELOW STRINGER 4. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 30,365 hrs · 29,727 cycles

DURING A-CHECK INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO HAVE A .2" (5MM) CRACK AT FRAME 75 BETWEEN STR 2R & 3R. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 29,662 hrs · 29,022 cycles

DURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 17-19 AND STRINGERS 21L-21R. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-02633. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,662 hrs · 29,022 cycles

DURING C-CHECK, THE SERVICE DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. MX R & R THE SILL IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 29,662 hrs · 29,022 cycles

DURING C-CHECK THE CENTERLINE SHEAR TIE AT FRAME 42, 6:00 POSITION IN THE WING BOX WAS FOUND TO BE CRACKED. MX R & R THE SHEAR TIE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 29,662 hrs · 29,022 cycles

DURING C-CHECK, THE CARGO DOOR LOWER INTERNAL SKIN WAS FOUND TO BE CORRODED AROUND THE BOTTOM NUT PLATES. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5230-01208. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CRACKED (VERTICAL STAB) · airframe 29,662 hrs · 29,022 cycles

DURING C-CHECK THE VERTICAL STAB DOUBLER BETWEEN FRAMES 80-81 AND STRINGERS 1L-1R WAS FOUND TO BE CRACKED. MX R & R THE DOUBLER IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,662 hrs · 29,022 cycles

DURING C-CHECK THE SHEAR TIE AT FRAME 19 BETWEEN STRINGERS 21L AND 21R WAS FOUND TO BE CORRODED. MX R & R THE SHEAR CLIP IAW EC5320-01713. ACFT APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — WORN (RUDDER) · airframe 29,662 hrs · 29,022 cycles

DURING C-CHECK, THE RUDDER LOWER CENTER HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX OVERSIZED THE HOLES AND REPLACED THE HAT BUSHINGS IAW EC5540-01178. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — CHAFED (CABIN LIGHTS) · airframe 29,611 hrs · 28,972 cycles

DURING POST FLIGHT INSPECTION, CREW REPORTED A STRONG ELECTRIC BURNING ODOR IN CABIN. NARROWED DOWN TO CEILING LIGHTS 14A-18A. MX REPAIRED A CHAFED WIRE ON THE CEILING LIGHT AT 18A, OPS CHECKED WITH NO DEFECTS. ACFT APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 29,611 hrs · 28,972 cycles

DURING POST FLIGHT INSPECTION, CREW REPORTED A STRONG ELECTRIC BURNING ODOR IN CABIN. FOUND TO BE CEILING LIGHTS 14A-18A. OPEN

Part: LIGHT — OVERHEATED (ZONE 200) · airframe 29,453 hrs · 28,807 cycles

THE CREW REPORTED A STRING ELECTRICAL BURNING ODOR AROUND ROW 14. MX INSPECTED THE ACFT AND R & R THE SIDEWALL LIGHT ASSY AT ROW 15 RT, OPS TESTED WITH NO DFECTS, AND THE ACFT WAS APPROVED OFR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 28,754 hrs · 28,123 cycles

THE CREW REPORTED THAT AFTER LANDING THERE WAS AN ELECTRICAL BURNING ODOR IN THE CABIN AND COCKPIT THAT WENT AWAY AFTER 3 MINUTES, AND SEEMED TO BE COMING FROM BEHIND THE CAPTAINS SEAT. MX INSPECTED THE ACFT C/W FIM21-20-00-810-801A, AND R & R RELAY K0094 FROM THE RELAY BOX BEHIND THE CAPTAINS SEAT. OPS CHECKS WERE COMPLETED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TIRE — FAILED (RT MLG) · airframe 28,457 hrs · 27,824 cycles

VIBRATION FROM WHEELS ON ACFT ROTATION. TOWER FLY-BY REVEALED RT MAIN TIRE BLOWN. UPON LANDING, RT MAIN INBD WAS BLOWN. R & R NR 3 & NR 4 MWA.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,277 hrs · 27,656 cycles

THE CREW REPORTED EMERGENCY AISLE PATH LIGHTING NR 6, 7, & 8 TO BE INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 59. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO BAY) · corrosion level 2 · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 54. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 33. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NACELLE) · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK THE RT ENGINE FORWARD LOWER YOKE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED YOKE IAW EC 5450-01028. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK THE LT FRAME 10 WAS FOUND TO BE CRACKED AT STRINGER 10L RIGHT BELOW THE LT DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK FRAME 10 AT STRINGER 10R WAS FOUND TO BE CRACKED RIGHT BELOW THE RT DV WINDOW FRAME. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FRAME IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK THE LT SKIN WAS FOUND TO BE CRACKED AROUND SEVERAL RIVETS BETWEEN FRAMES 77-79 AND STRINGERS 2L-7L. MAINTENANCE PERFORMED A BUSHING REPAIR TO THE AFFECTED FASTENERS IAW EC5330-02123. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK THE RT SKIN WAS FOUND TO BE CRACKED AROUND SEVERAL RIVETS BETWEEN FRAMES 77-79 AND STRINGERS 2R-7R. MAINTENANCE PERFORMED A BUSHING REPAIR TO THE AFFECTED HOLES IAW EC5330-02123. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK CRACKED SHEAR CLIP FRAME 61 STRINGER 6R-7R. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 BETWEEN STRINGERS 6R-7R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CRACKED (FUSELAGE) · airframe 24,746 hrs · 24,024 cycles

SHV - DURING C-CHECK CRACKED SHEAR CLIP FRAME 61 STRINGER 6L-7L. MAINTENANCE REMOVED AND REPLACED SHEAR CLIP AT FRAME 61 STRINGER 6L-7L IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE — MALFUNCTIONED (TE FLAP) · airframe 24,517 hrs · 23,784 cycles

IAH - FLIGHT 2102, THE CREW REPORTED THAT AFTER T/O, RECEIVED A FLAP FAIL MESSAGE ON EICAS WITH THE FLAP LEVER AT 0 DEGREES AND THE FLAPS AT 9 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLAP TRANSMISSION BRAKE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DAU — DEFECTIVE (NR 2) · airframe 24,364 hrs · 23,619 cycles

XNA - FLIGHT 2660, THE CREW REPORTED A BLEED 1 LEAK IN FLIGHT THAT DID NOT GO AWAY. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION AND RETURNED TO XNA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL AND LEAK CHECKS, AND SUBSEQUENTLY REMOVED AND REPLACED THE NUMBER TWO DATA ACQUISITION UNIT. OPERATIONAL TESTS WERE PERFORMED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — LEAKING (BLEED AIR SYS) · airframe 23,650 hrs · 22,849 cycles

IAH - FLIGHT 2264 - THE CREW REPORTED A BLEED ONE LEAK ON CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED O-RINGS AT POSITIONS 17, 19, 23, 25 & 30, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SELECTOR — INOPERATIVE (COCKPIT) · airframe 23,229 hrs · 22,375 cycles

IAH - FLIGHT 2967 - THE CREW REPORTED THAT THE FLAPS FAILED AT 9 DEGREES. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP SELECTOR LEVER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACCUMULATOR — FAULTY (HYDRAULIC SYS) · airframe 22,739 hrs · 21,866 cycles

SHV - LOUD BANGING NOISE IN WHEEL WELL FOR 30 SEC AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR HYD ACCUMULATOR IAW EMB 145 AMM 32-33-15. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

IAH - FLIGHT 2361, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE FRONT AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: STRUCTURE — OUT OF POSITION (EMERGENCY EXIT) · airframe 20,725 hrs · 19,809 cycles

IAH - DURING A-CHECK INSPECTION THE RIGHT HAND OVERWING EMERGENCY EXIT DOOR WOULD NOT OPEN. THE METAL TRIM AT THE TOP OF THE DOOR WAS FOUND TO BE CATCHING ON THE OPENING. MAINTENANCE RECONTOURED/TRIMMED THE AFFECTED MATERIAL, OPERATIONALLY CHECKED THE EXIT WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 17,738 hrs · 16,607 cycles

CREW REPORTED LAV SMOKE DETECTOR WARNING ON EICAS WITH APU ON ENGINES OFF. MAINTENANCE REMOVED AND REPLACED LAV SMOKE DETECTOR SENSOR IAW EMB145 AMM 26-14-02. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 16,642 hrs · 15,388 cycles

CLE FLIGHT NR 2235, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE PRECEEDED BY E1-2 REVERSER DISAGREE IN FLIGHT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR WOW PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,366 hrs · 15,072 cycles

IAH - DURING MAINTENANCE INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — LIGHTNING STRIKE (FWD FUSELAGE) · airframe 15,652 hrs · 14,175 cycles

DURING C-CHECK VARIOUS LIGHTNING STRIKE ON SKIN PNL 214. MAINTENANCE REPAIR SKIN PNL 214 ABOVE STR 13R AFT FR 1A IAW EC 5330-01465. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,652 hrs · 14,175 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION AROUND NUT PLATE BETWEEN FRAMES 22 AND 23. MAINTENANCE REPAIRED LT OMEGA BEAM NUT PLATE AT FRAME 22.5 AND RIVET HOLE CRACK AT FRAME 22 IAW SRM 51-30-01; 51-40-02 AND EC5320-01241. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,652 hrs · 14,175 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION ON I/B SIDE FROM FRAME 36 TO FRAME 38. REPAIRED LT OMEGA BEAM AT FRAME 38 IAW EMB 145 SRM 53-21-10, SECTION 2, FIGURE 201, SHEET 3 & EC 5320-01231 (ORIG).

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,652 hrs · 14,175 cycles

SHV - DURING C-CHECK THE RT OMEGA BEAM HAS CORROSION AROUND NUT PLATE AT FRAME 23. REPAIRED CORROSION ON RT OMEGA BEAM AROUND NUT PLATE AT FRAME 23 WITH INSTALLATION OF NEW OMEGA BEAM AT FRAME 23 IAW EMB 145 SRM 51-40-02 WITH NUT PLATE INSTALLATION PER EC 5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,652 hrs · 14,175 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FRAMES 23 & 24. REPAIRED CENTER OMEGA BEAM AT FRAME 24 IAW EMB 145 SRM 53-22-10 PARAGRAPH 2 FIGURE 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,652 hrs · 14,175 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM HAS CORROSION AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM FROM FR 17-24 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 15,652 hrs · 14,175 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION FROM FRM 46 TO FRM 52. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR LT OMEGA BEAM FRM 46 TO FRM 52 IAW EC 5320-01231. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 15,652 hrs · 14,175 cycles

SHV - DURING C-CHECK THE LT OMEGA BEAM HAS CORROSION FROM FRM 39 TO FRM 45. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR LT OMEGA BEAM AT FRM 44 IAW SRM 53-21-10, SECTION 2, FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,618 hrs · 14,139 cycles

RIC - DURING SCHEDULED MAINTENANCE, THE RIGHT FWD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECK GOOD. A/C RELEASED TO SERVICE.

Part: VALVE — FAILED (NR 2 ENGINE) · airframe 15,447 hrs · 13,960 cycles

RIC - FLIGHT CREW REPORTED BLEED NR 2 VALVE CLOSED MSG ON EICAS DURING ICE CONDITIONS. CREW PERFORMED AIR RETURN TO RIC. MX PERFORMED TROUBLESHOOTING AND REMOVED AND REPLACED ENGINE NR 2 ANTI-ICE VALVE, ENGINE NR 2 HIGH STAGE PRESS SW AND RELAY K1088. ALL OPERATIONAL CHECKS WERE PERFORMED SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,430 hrs · 12,797 cycles

IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED AISLE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHTS FROM ROW 8 TO 12 WERE DIM. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING)

DURING ROUTINE MAINTENANCE THE RIGHT OVERWING EMERGENCY LIGHT WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — FAULTY (FUSELAGE)

DURING ROUTINE INSPECTION MAINTENANCE FOUND THE LEFT AND THE RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY CHARGER IAW EMB145 AMM NR 33-50-04. OPS. CHECKED SYSTEM GOOD.

Part: UPLOCK — FAULTY (NLG)

CLE FLIGHT NR 2001 THE CREW REPORTED THE NOSE WHEEL DID NOT RETRACT AFTER TAKEOFF. THE GEAR WAS RECYCLED AND IT STILL DID NOT RETRACT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR UPLOCK BOX ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.

Part: SELECTOR — FAULTY (MLG)

MSP FLIGHT 2779 CREW REPORTED LANDING GEAR DISAGREE MESSAGE. RED NOSE INDICATION ON EICAS. COULD ALSO HEAR THAT NOSE GEAR WAS DOWN. GEAR RECYCLED OK. MAINTENANCE REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. OPERATIONAL CHECK WAS GOOD.

Part: UPLOCK — STICKING (RIGHT MLG)

CLE FLIGHT# 2225 THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE WITH A RED RIGHT MAIN INDICATION ON GEAR RETRACTION.THE GEAR WAS RECYCLED AND EXTENDED PROPERLY THEN RETRACTED WITH A DISAGREE MESSAGE AGAIN.THE CREW REPORTED BOTH MAIN GEAR WERE FELT TO BUMP UP AND LOCK.THE AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN GEAR UP LOCK BOX ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.

Part: PROXIMITY SWITCH — FAULTY (MLG)

CLE FLIGHT#2268 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE ECIAS.MAINTENANCE INSPECTED AND REPLACED THE LEFT MAIN LANDING GEAR NR 2 PROXIMITY SWITCH AND THE LANDING GEAR ELECTRONIC UNIT.OPERATIONAL CHECKS WERE GOOD.PROXIMITY SWITCH P/N 8-527-01 S/N A27260

Part: SILL — CORRODED (CARGO DOOR) · airframe 11,555 hrs · 9,743 cycles

DURING A SCHEDULED 3C INSPECTION THERE WAS EVIDENCE OF CORROSION UNDER THE CARGO DOOR SILL PROTECTIVE PLATE. MAINTENANCE DRILL OUT THE RIVETS IN SILL, REMOVED CORRODED PARTS, FAB NEW BRACKETS AND INSTALL ALONG WITH A NEW CARGO SILL IAW EMB 135/145 SRM 51-40-02; SRM 51-30-01 AND EMB 135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: PROXIMITY SWITCH — FAULTY · airframe 11,523 hrs · 9,713 cycles

EWR---CO 2143, CREW REPORTED, " LANDING GEAR/ GROUND FAILURE MESSAGE ON EICAS WHEN GEAR DOWN IS SELECTED." MAINTENANCE REMOVED AND REPLACED LEFTHAND LANDING GEAR SHOCK ABSORBER PROXIMITY SWITCH, OPS. CHECKED GOOD IAW EMB145 MM #32-63-02. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING PREFLIGHT THE CREW NOTED THAT THE CABIN DOOR AND ROW TWELVE (12) WINDOW EXIT EMERGENCY LIGHTING FAILED TO ILLUMINATE.

Part: CHARGER — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE FOUND STRIPS 2 AND 3 OF THE EMERGENCY AISLE PATH LIGHTING, AND THE CABIN SERVICE DOOR EXTERIOR LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — FAILED (LT MLG)

EWR- DURING FLIGHT 3959 THE CREW NOTED THAT THE LANDING GEAR AIR/GROUND FAIL MESSAGE APPEARED APPROXIMATELY SEVEN MINUTES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. EWR- MAINTENANCE REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR PROXIMITY SENSORS (2 EA) AND OPERATIONAL CHECK CHECKED GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RECEPTACLE — BURNED (GALLEY)

IAH-FLIGHT ATTENDANT REPORTED BURNT SMELL IN CABIN DURING DESENT AND FOR REMAINDER OF THE FLIGHT. MAINTENANCE REMOVED AND REPLACED THE HOT JUG RECEPTACLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING A-CHECK INSPECTION, THE PASSENGER DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IN ACCORDANCE WITH EMB-145 M/M 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 7,645 hrs · 6,039 cycles

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FLOOR SUPPORT IN ACCORDANCE WITH EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — SMOKE (TAILCONE)

EWR-CREW REPORTED ON APU START CABIN FILLED UP WITH SMOKE. LAV SMOKE DETECTOR ILLUMINATED. MX TROUBLESHOT AND FOUND FAULTY APU..A/C RELEASED MEL 49-00-00 CAT C CONTROL NUMBER 001068. A/C RETURNED TO SERVICE. SDR OPEN.

Part: APU — LEAKING (AFT)

CREW REPORTED ON APU START CABIN FILLED UP WITH SMOKE. LAV SMOKE DETECTOR ILLUMINATED MX TROUBLESHOT AND FOUND FAULTY APU. A/C RELEASED IAW MEL 49-00-00 CAT. C CONTROL NUMBER 01068. A/C RETURNED TO SERVICE ON 10-02-00 IAH MX REMOVED/REPLACED THE APU AND CLEARED THE MEL ISSUED ON A/C/ A/C RETURNED TO SERVICE.CDR CLOSED REFERENCE SDR C2XAOOIA353 FOR CLOSING INFORMATION.

Part: APU — LEAKING (AFT)

EWR-DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT UPON APU START THE CABIN FILLED WITH SMOKE. MX PLACED THE APU ON MEL ATA49-00-00 CONTROL 001068, AND THE A/C WAS APPROVED FOR RETURN TO SERVICE ON 10/2/00. THE A/C LANDED AT IAH WHERE MX REMOVED/REPLACED THE AFFECTED APU, REMOVED THE MEL, AND A/C WAS APPROVED FOR RETURN TO SERVICE. REF SDR CONTROL #C2XAOOBT067 FOR OPEN SDR

Part: APU — LEAKING (AFT)

EWR-DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THAT UPON APU START THE CABIN FILLED WITH SMOKE. MAINTENANCE PLACED THE APU ON MEL ATA49-00-00 CONTROL 001068, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 10/02/00 THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED APU, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DUCT — LEAKING (NR 2 BLEED)

EWR - FLT 4395 - CREW REPORTED NR 2 BLEED LEAK LIGHT INFLIGHT, ACCOMPANIED BY SMOKE IN COCKPIT AND CABIN, ODOR DISSIPATED QUICKLY. MAINTENANCE RESEALED ENGINE BLEED DUCT NR 2 AT RADIO ALTIMETER ACCESS PANEL. OPS CHECKED AND LEAK CHECKED GOOD. (M)

Part: ENGINE — MALFUNCTIONED (FUSELAGE)

TYS - DURING A SCHEDULED INSPECTION, THE LEFT ENGINE OIL PRESSURE WAS FOUND TO BE EXCEEDING MANUFACTURES LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M)

Part: CONTROL UNIT — TRIPPED (HORIZ STAB)

FLT 3965 - PILOT REPORTED THEY GOT A TAKEOFF CONFIG WARNING WITH THE PITCH TRIM AT THE TOP OF THE GREEN ARC. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE HORIZONTAL STABILIZER CONTROL UNIT AND OPERATIONAL CHECKED THE SYSTEM GOOD IAW EMB145 MM 27-40-00. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: FLOORBEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT FLOORBEAM WAS FOUND CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION AND REPAIRED THE AFFECTED FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01109, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 3,914. 2 HOURS. CYCLES: 2,929. (X)

Part: DRAG ANGLE — CRACKED (RT VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILZIER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE AFT SECTION OF EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGTH BATTERY PACK IAW EMB145 MM 33-50-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: FLOORBEAM — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM WAS FOUND CORRODED FROM FRAME 15 TO FRAME 19. MAINTENANCE REMOVED THE CORROSION AND REPAIRED THE AFFECTED FLOORBEAM IAW EMBRAER FAX SST-1287/99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) ACFT TT: 3,914.2 HOURS. CYCLES: 2,929. (X)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

IAH - DURING C-CHECK INSPECTION, THE FORWARD SECTION OF EMERGENCY AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-01, AND THE AIRCRAFT WAS APPROVEDF FOR RETURN TO SERVICE. ACFT TT: 3,914.2 HOURS. CYCLES: 2,929. (X)

Part: DRAG ANGLE — CRACKED (LT VERT STAB)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5330-01101, AND THE AIRCRAFT WAS APPRROVED FOR RETURN TO SERVICE. ACFT TT: 3,914.2 HOURS. CYCLES: 2,929. (X)

Part: ENGINE — FAILED (NR 1)

IAH - FLT 4249 - THE CREW REPORTED SMOKE IN THE COCKPIT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND OPERATIONALLY CHECKED THE COOLING PACS IAW EMB145 MM 21-25-01 AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE DISCREPANCY RECURRED ON FLT 4252 FROM IAH/LBB WITH A LAV SMOKE WARNING. THE AIRCRAFT LANDED AT LBB WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: FRAME — DAMAGED (FUSELAGE)

FOUND DAMAGE CAUSED BY RAMP HANDLER BAG CART AFT OF CARGO DOOR BETWEEN FRAMES 27 AND 28. REPLACED FRAME AND REPAIRED WITH DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — DAMAGED (FUSELAGE)

FOUND DAMAGE CAUSED BY RAMP HANDLER BAG CART AFT OF CARGO DOOR BETWEEN FRAMES 27 AND 28. REPLACED FRAME AND REPAIRED WITH DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — FAILED (LEFT)

CLE - FLT 4014 - CREW REPORTED THE LEFT HAND ENGINE CONTROL A AND B SYSTEMS FAILED IN-FLIGHT. MAINTENANCE INSPECTED THE CONTROL SYSTEM AND THE ENGINE AND FOUND THE ENGINE'S I.T.T. HAD EXCEEDED MANUFACTURER'S LIMITS. THE LEFT HAND ENGINE WAS REMOVED AND REPLACED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. THE NR 1 AND NR 2 F.A.D.E.C.'S WERE REMOVED AND REPLACED FOR PRECAUTIONARY MEASURES. (X)