N14974

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,503 hrs · 25,307 cycles

DURING MX THE GALLEY OVERHEAD AND COCKPIT STEP EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 31,365 hrs · 23,556 cycles

DURING C-CHECK, TWO MIGRATED HAT BUSHINGS ON RT AILERON PCA FITTING. MX R & R PCA FITTING IAW EC5750-01177. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (ZONE 100) · airframe 31,365 hrs · 23,556 cycles

DURING C-CHECK, FRAME 48 HAS 2 MISDRILLED HOLES AT STR 15R. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (ZONE 100) · airframe 31,365 hrs · 23,556 cycles

DURING C-CHECK, STRUCTURE AT FRM 48, STR 15R HAS 2 MISDRILLED HOLES. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 31,365 hrs · 23,556 cycles

DURING C-CHECK, LT UPPER SEAT TRACK SUPPORT FRM 50, LWR ATTACH FASTENERS CORRODED. MX PERFORMED REPAIR IAW SRM 51-40-02 AND EC5320-01522, REV A. WET INSTALLED FASTENERS, EDGE SEALED, ALODINE, PRIMERED AND RESTORED ORIGINAL FINISH IAW CPM 51-21-06. ACFT APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,365 hrs · 23,556 cycles

DURING C-CHECK, BAGGAGE DOOR LOWER CUTOUT BEAM HAS CORROSION. MX R & R BAGGAGE DOOR LOWER CUTOUT BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — DAMAGED (ZONE 100) · airframe 31,365 hrs · 23,556 cycles

DURING C-CHECK, STRUCTURE AT FRM 50, STR 15R HAS 1 MISDRILLED HOLE. MX PERFORMED REPAIR IAW EC5320-01678. ACFT APPROVED FOR RETURN TO SERVICE.

Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 29,612 hrs · 22,169 cycles

THE CREW REPORTED THE AFT CABIN EMERGENCY LIGHT STAYS ILLUMINATED WHEN ACFT POWER WAS TURNED OFF. MX INSPECTED AND RESECURED WIRE W776-8515-20 ON CONNECTOR P8104. OPS CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 28,525 hrs · 21,341 cycles

BHM - FLIGHT 2824 THE CREW REPORTED A POSSIBLE LIGHTNING STRIKE, AND SMELLED ELECTRICAL TYPE SMOKE. THE AIRCRAFT LANDED AT BHM WITHOUT INCIDENT WHERE CONTRACT MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION WITH NO DEFECTS NOTED, FOUND NO EVIDENCE OF SMOKE OR BURN SMELL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — INOPERATIVE (ZONE 100) · airframe 28,457 hrs · 21,293 cycles

AFTER TAKE OFF FROM DFW CREW REPORTED SMOKE IN COCKPIT. FLIGHT AIR RETURNED BACK TO DFW. LANDING WAS UNEVENTFUL. MAINTENANCE COMPLIED WITH FIM 21-20-00-810-801-A AND DETERMINED SMOKE IN COCKPIT WAS DUE TO PACK NR 1 FAILURE. AIRCRAFT RELEASED IAW MEL 21-51-00-3, CATEGORY "C". AIRCRAFT RETURNED TO SERVICE. THE AIRCRAFT LANDED, MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE RECIRCULATION FAN, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED OFR RETURN TO SERVICE.

Part: CONTROL VALVE — DRAGGING (BRAKE SYSTEM) · airframe 28,485 hrs · 21,315 cycles

TYS - A/C WAS TAXIING FROM IAH GATE WHEN CREW FELT THE BRAKES DRAGGING. UPON FURTHER INSPECTION FOUND THE RT INBOARD BRAKE DRAGGING. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL VALVE AND OPS CHECK GOOD LP(2818684). ACFT WAS RELEASED TO SERVICE.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 27,900 hrs · 20,859 cycles

TYS - A/C WAS EN ROUTE TO BNA FROM EWR WHEN LIGHTNING STRUCK THE A/C. THE A/C LANDING AT BNA WITHOUT ANY INCIDENT. MAINTENANCE COMPLIED WITH TASKCARD 6232012, WHICH IS THE LIGHTNING STRIKE TASKCARD. THE A/C WAS THEN FERRIED TO TYS WHERE MAINTENANCE REMOVED AND REPLACED THE LT WING TIP (PN-145-73550-404) IAW EMB 145AMM 57-30-00. ALSO REPLACED THE RT NOSE GEAR DOOR (PN-145-31700-404) IAW32-20-05). REMOVED AND REPLACED THE APU SILENCER (PN-4503825-SN-1148) IAW 53-32-00). ALSO REPLACED THE LT ELEVATOR TIP IAW EMB 145 AMM 55-20-01 (PN 145-22634-403). COMPLIED WITH THE LIGHTNING STRIKE INSPECTION IAW EMB 145 AMM 5-50-01. PERFORMED LEAK CHECKS, GEAR CHECKS AND PRESSURIZATION CHECKS. A/C WAS THEN RELEASED BACK TO SERVICE.

Part: SUPPORT FITTING — CRACKED (PYLON) · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK ANGLE SUPPORT CLIP CRACKED IN PYLON FRAME 73 STRINGER 8L. MAINTENANCE REMOVED AND FABRICATED NEW ANGLE SUPPORT CLIP IN PYLON AT FRAME 72-73 STRINGER 8L. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 900) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT RADIUS AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM BETWEEN FRAMES 18-23 IAW EMB-145 SRM 51-40-02 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK STRINGER 5R DAMAGED FRAMES 65-66. MAINTENANCE PERFORMED REPAIR OF STRINGER 5R AT FRAME 65 IAW ETD 2010-145/07996. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — WORN (AILERON) · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK ON RT AILERON 2ND FROM I/B HINGE BRACKET O/B SIDE HAT BUSHING MISSING. MAINTENANCE REMOVED AND REPLACED I/B HINGE BRACKET O/B SIDE FOR RT AILERON IAW EMB-145 SRM 51-40-02 AND CPM 51-21-05/06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 33 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM CARBON CROSSBEAM ATTACHMENT AREA AT FRAME 33 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (ZONE 200) · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK SKIN DENTED BETWEEN FRAMES 65-66 STRINGER 4R-5R ON EXTERNAL FUSELAGE. MAINTENANCE PERFORMED REPAIR ON FUSELAGE SKIN AT FRAME 65-66 STRINGER 4R-5R IAW ETD 2010-145/07996. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK BAGGAGE DOOR LOWER CUTOUT FRAMES 65 TO 68 INTERIOR AND EXTERIOR HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED THE CARGO LOWER BEAM IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 29 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM CARBON CROSSBEAM ATTACHMENT AREA AT FRAME 29 IAW EMB-145 SRM 53-00-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT FITTING — CRACKED (PYLON) · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK ANGLE SUPPORT CLIP CRACKED IN PYLON AT FRAME 73 STRINGER 8R. MAINTENANCE REMOVED AND INSTALLED NEW FABRICATED ANGLE SUPPORT CLIP IN PYLON AT FRAME 72-74 STRINGER 8R IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — GOUGED (LT WING) · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK LT SPEED BRAKE CENTER HINGE I/B ATTACHMENT BRACKET (ON WING) HAS GOUGES INSIDE & AROUND BOLT HOLE. MAINTENANCE REMOVED AND REPLACED LT SPEED BRAKE CENTER HINGE ATTACHMENT BRACKET IAW EMB-145 AMM 20-10-01 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — WORN (AILERON) · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK RT AILERON PCA O/B ROD FITTING O/B HAT BUSHING ON AILERON MIGRATED. MAINTENANCE REMOVED AND REPLACED RT AILERON PCA BRACKET FITTING IAW EC5750-01177 REV C. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CORRODED (LEVEL 2 LOCAL) AT FRAMES 59-61. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 59-61 IAW EC5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 38 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR TO CENTER OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 38 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 33 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CARBON CROSSBEAM AT FRAME 33 IAW EMB-145 SRM 51-40-02, SRM 53-00-10 AND CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 26,748 hrs · 19,965 cycles

SHV - DURING C-CHECK LT OMEGA BEAM CARBON CROSSBEAM AREA AT FRAME 54 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM CARBON CROSSBEAM AT FRAME 54 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (MAIN) · airframe 26,322 hrs · 19,636 cycles

BATTERY NR 2 OVERTEMP UP TO 64C. REMOVED AND REPLACED BATTERY IAW EMB 145AMM 24-36-01, OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 26,024 hrs · 19,400 cycles

MCI - DURING POST FLIGHT INSPECTION THE CREW REPORTED THE RIGHT EMERGENCY DOOR EXIT LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: O-RING — DETERIORATED (BLEED AIR SYS) · airframe 25,678 hrs · 19,145 cycles

CLE FLT 2556 THE CREW REPORTED A BLEED 1 LEAK MESSAGE IN CLIMB. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED LINE GAMMA JOINT O-RINGS AT LEFT UPPER DUCT IN CARGO BAY. OPERATIONAL CHECKS WERE GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,630 hrs · 19,103 cycles

EXTERIOR EXIT MARKER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP INVERTER AND OPERATIONAL CHECKED GOOD.

Part: CONTROL UNIT — FAULTY (BRAKE SYSTEM) · airframe 25,002 hrs · 18,631 cycles

CLE FLT 2841 THE CREW REPORTED A INBOARD BRAKE INOP MESSAGE WHEN THE GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — MALFUNCTIONED (COCKPIT) · airframe 24,607 hrs · 18,336 cycles

IAH - FLIGHT 2117, THE CREW REPORTED AN ELECTRIC SMELL IN THE COCKPIT ON DESCENT INTO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CENTER PROJECTOR LAMP UNDER THE GLARE SHIELD, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (SPOILER) · airframe 24,184 hrs · 18,017 cycles

OMA - FLIGHT 2593, ON DESCENT THE CREW REPORTED THAT THE SPOILER FAILED TO CLOSE SYMMETRICALLY, AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT OMA WITHOUT INCIDENT. MCI MX REMOVED AND REPLACED THE RIGHT SPEED BRAKE ACTUATOR, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MAGNETIC SEAL — LEAKING (NR 2 ENIGINE) · airframe 23,532 hrs · 17,491 cycles

IAH - FLIGHT 3108, THE CREW REPORTED THAT APPROXIMATELY ONE HOUR INTO FLIGHT THEY STARTED LOSING OIL PRESSURE AND QTY ON THE NUMBER TWO ENGINE. THE CREW SHUT DOWN THE NUMBER TWO ENGINE AS A PRECAUTION, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NUMBER TWO ENGINE FPMU MAGNETIC CARBON SEAL, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT)

CLE FLIGHT 2522, THE CREW REPORTED THE CAPTAIN` S EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE INSPECTED AND REPLACED THE CAPTAIN`S FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SHV - DURING C-CHECK IT WAS FOUND THAT THE LT OMEGA SHAPE WAS CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: SKIN — DENTED (FUSELAGE)

SHV - DURING C-CHECK IT WAS FOUND THAT THE LT REAR FUSELAGE SKIN WAS DENTED AT FRAME 65/STRINGER 16L, DIRECTLY BELOW THE FORWARD LOWER CORNER OF THE CARGO DOOR CUTOUT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SHV - DURING C-CHECK IT WAS FOUND THAT THE RT OMEGA BEAM HAT SECTION WAS CORRODED AROUND NUT PLATE HOLES AT FRAME 18. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC532001411. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,662 hrs · 14,722 cycles

EWR - DURING ROUTINE MAINTENANCE, MX FOUND FIRST EMERGENCY LIGHT STRIP INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL SUCCESFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,625 hrs · 14,699 cycles

EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT FLOOR STRIPS 6, 7 AND 8 INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,827 hrs · 14,116 cycles

DURING SCHEDULED MAINTENANCE THE LEFT AFT FLOOR PROXIMITY LIGHT WAS FOUND TO BE INOPERATIVE. THE EMERGENCY LIGHT STRIP WAS REMOVED AND REPLACED, OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,870 hrs · 13,387 cycles

BTV FLT 2414 - DURING 5A CHECK FOUND RT OVERWING EMERGENCY LIGHT DOES NOT COME ON. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT BULB IAW EMB145 AMM 33-50-10. OPS CHECK GOOD.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 17,552 hrs · 13,129 cycles

IAH - FLIGHT 2890, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE CAPTAINS PFD (PRIMARY FLIGHT DISPLAY), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,517 hrs · 13,102 cycles

IAH - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHTING AT 15ABC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 16,398 hrs · 12,211 cycles

SHV - DURING C-CHECK, LEFT OMEGA BEAM AT FR 29 IS CORRODED. MAINTENANCE REPAIRED LEFT OMEGA BEAM AT FR 29 IAW EMB 145 SRM 53-00-10 FIG 202. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SKIN PANEL — CORRODED (HORIZ STAB) · airframe 16,398 hrs · 12,211 cycles

SHV - DURING C-CHECK LT AND RT HORIZONTAL STAB LEADING HAVE RIVETS WITH CORROSION. MAINTENANCE REMOVED CORROSION AND REPLACED RIVETS IAW EC5530-01101. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 16,398 hrs · 12,211 cycles

SHV - DURING C-CHECK THE MAIN AND SERVICE DOOR ATTACHMENT REWORK CRACKS WERE DISCOVERED ON THE FORWARD LOWER MAIN DOOR STOP AT BOTTOM INBOARD HOLE (2 O'CLOCK POSITION) AND TOP OUTBOARD HOLE (8 O'CLOCK POSITION. MAINTENANCE REPAIRED CRACK ON THE FORWARD LOWER MAIN DOOR STOP AT BOTTOM INBOARD HOLE (2 O'CLOCK POSITION) AND TOP OUTBOARD HOLE (8 O'CLOCK POSITION) IAW EC5310-01386. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: SELECTOR — INOPERATIVE (MLG) · airframe 15,725 hrs · 11,687 cycles

MCI- FLIGHT 2488, DURING T/O, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOORS WOULD NOT RETRACT. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR LEVER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,866 hrs · 10,992 cycles

STL - FLIGHT 3221, DURING PREFLIGHT INSPECTION, THE AISLE PATH LIGHTING STRIP BETWEEN SEATS 6A AND 7A WAS FOUND TO BE INOPERATIVE. MAINTENANCE PLACED THE AIRCRAFT ON MEL 33-50-00/2 CAT C CONTROL NUMBER 061034, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 13,781 hrs · 10,150 cycles

IAH - DURING MAINTENANCE INSPECTION, THE PAX DOOR THRESHOLD ATTACHMENT ANGLE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAULTY (EMERGENCY LIGHT) · airframe 12,697 hrs · 9,297 cycles

CREW REPORTED EMERGENCY EXIT SIGN ABOVE GALLEY DOOR WILL NOT LIGHT UP. MAINTENANCE REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,762 hrs · 9,280 cycles

EWR - FLIGHT 3424, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE GALLEY DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED THE NR 2 AND 3 EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED THE EMERGENCY LIGHT INVERTED. OPERATIONAL CHECK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,309 hrs · 8,990 cycles

SHV - DURING SERVICE/ROUTINE CHECK THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LAMP IAW EMB 145AMM 33-50-09. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,277 hrs · 8,964 cycles

OKC - FLIGHT 2964, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE AISLE PATH EMERGENCY LIGHTS BETWEEN ROWS THREE AND SEVEN DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER. OPS CHECKED WITH NO DEFECTS ALL IAW EMB-145 MM 33-50-11, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,262 hrs · 8,948 cycles

IAH- FLIGHT 2606, DURING PREFLIGHT INSPECTION THE EMERGENCY EXIT SIGN ON THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,102 hrs · 8,824 cycles

CREW REPORTED TWO LOWER EMERGENCY LIGHT PANELS ARE INOPERATIVE. MAINTENANCE RECHARGED AND OPS CHECKED EMERGENCY LIGHT STRIPS IAW 33-50-00 CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 11,965 hrs · 8,711 cycles

EWR LOG SQUAWK HALF OF AISLE PATH LIGHTS OUT. REMOVED AND REPLACED NR 2 BATTERY PACK IAW EMB145 AMM 33-50-04. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)

CREW REPORTED THAT THE GALLEY EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RESECURED THE CANNON PLUG ON THE GALLEY EMERGENCY LIGHT, OPS CHECKED LIGHT GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,624 hrs · 8,439 cycles

SHV-DURINC CHECK THE NR 6 AISLE PROXIMITY STRIP WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP IAW EMB 145 AMM 33-50-08, THE ENSUING OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,624 hrs · 8,439 cycles

SHV - DURING C-CHECK THE CENTER FLOORBEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25 WHERE THE CARBON FIBER CROSSMEMBER ATTACHES. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 11,624 hrs · 8,439 cycles

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

Part: BUTTSTRAP — GOUGED (FUSELAGE) · airframe 11,624 hrs · 8,439 cycles

SHV - DURING C-CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 22 AND 23 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PLATE — CORRODED (FUSELAGE) · airframe 11,624 hrs · 8,439 cycles

DURING C-CHECK THE SHELL PLATE ON THE CENTER FLOORBEAM AT FRAME 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SHELL PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,624 hrs · 8,439 cycles

DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EC 5320-01124. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 11,624 hrs · 8,439 cycles

SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT 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: ANGLE — CORRODED (CABIN) · airframe 11,624 hrs · 8,439 cycles

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

Part: FLOORBEAM — CORRODED (CABIN) · airframe 11,625 hrs · 8,439 cycles

DURING C-CHECK THE LEFT CROSSBEAM AT FRAME 19 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: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,624 hrs · 8,439 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 11,624 hrs · 8,439 cycles

DURING C-CHECK THE LEFT FLOORBEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-21-10 FIG 202, SHEET 1. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 11,624 hrs · 8,439 cycles

DURING C-CHECK THE EXTERNAL FUSELAGE SKIN WAS FOUND TO BE DENTED BETWEEN FRAMES 20 AND 21, AND BETWEEN STRINGERS 12L AND 13L. MAINTENANCE PERFORMED A PATCH REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSLEAGE) · airframe 11,624 hrs · 8,439 cycles

SHV - DURING C-CHECK THE CENTER FORWARD FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 11,624 hrs · 8,439 cycles

DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE UPPER RIGHT HAND MOUNTING BRACKET. MAINTENANCE PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145 SRM 53-32-13 FIGURE 203. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN)

CLE FLIGHT 2114 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT GO OUT AFTER TESTING. MAINTENANCE PERFORMED A RESET OF THE SYSTEM AND OPERATIONAL CHECKS WERE GOOD.

Part: SERVO VALVE — FAULTY (APU)

IAH FLIGHT 2627 THE CREW REPORTED A STRONG FUEL SMELL IN THE COCKPIT AND CABIN WHEN THE APU WAS STARTED. MAINTENANCE REPLACED THE APU BLEED SERVO CONTROL VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

IAH- FLIGHT 2085, DURING FINAL ARRIVAL AND APPROACH BEGINNING, EICAS WARNING FOR BAGGAGE SMOKE ILLIMINATED WITH OVERHEAD EXTG BUTTON. EICAS MESSAGE CAME ON/WENT OUT/ CAME ON/ WENT OUT A TOTAL OF THREE (3) TIMES IN ONE MINUTE AND STAYED OUT. IAH- MAINTENANCE REMOVED AND REPLACED FORWARD BAGGAGE SMOKE DETECTOR. PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO EVIDENCE OF FIRE OR SMOKE IN THE BAGGAGE COMPAPTMENT.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

BAN- FLIGHT 2631, THE CREW NOTED THE BAGGAGE SMOKE INDICATIONS ILLUMINATED. THE CREW DISCHARGED BOTH FIRE BOTTLES IN THE BAGGAGE COMPARTMENT, RETURNED TO BNA AND LANDED WITHOUT INCIDENT. BNA- MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE BAGGAGE COMPARTMENT, NO INDICATIONS OF FIRE OR RESIDUAL SMOKE. PERFORMED BAGGAGE COMPARTMENT FIRE DETECTION TEST, OPS CHECK GOOD. MAINTENANCE REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT FIRE BOTTLES, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — FAULTY (CABIN)

DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ABOVE ROW 17 WOULD NOT ILLUMINATE.MAINTENANCE INSPECTED AND REPLACED THE #4 EMERGENCY BATTERY CHARGER ASSEMBLY.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — INOPERATIVE (MLG)

THE CREW NOTED THAT THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO AGU, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED FROM AGU TO IAH FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE LGEU, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,872 hrs · 5,471 cycles

TYS DURING A SCHEDULED 2C INSPECTION THE AFT SERVICE DOOR SILL WAS FOUND CORRODED. MAINTENANCE REPAIRED CORRODED AREAS OF THE SEVICE DOOR SILL IAW EMB GST 1927/02A, EMB 135/145 CPM 51-21-04. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: SILL — CORRODED · airframe 7,872 hrs · 5,471 cycles

TYS, During a scheduled inspection the service door seal was found corroded. Maintenence repaired the damage by cleaning the corrosion and installing a lateral doubler. I/A/W-EMB-135/145-SRM-53-21-02, 51-40-02, CPM-51-21-04,05 & 06 and GST-2807/02. The repair was satisfactory and the aircraft will be released upon complection of inspection.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 7,872 hrs · 5,471 cycles

TYS, DURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE PROFILE Z AFT OF FRAME 23. MAINTENANCE REMOVED AND REPLACED THE PROFILE Z. IAW EMB 135/145 SRM-51-40-02, CPM-51-21-04,05. THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.

Part: SILL — CORRODED · airframe 7,872 hrs · 5,471 cycles

TYS DURING A SCHEDULED 2-C INSPECTION THE SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. MAINTENANCE R/R THE SERVICE FORWARD SEAL IAW EMB 145 SRM 52-10-02 AND EMB 145 CPM 51-21-05. ALL WORK WAS ACCOMPLISHED AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: PIN — CORRODED (RT & LT MLG) · airframe 7,872 hrs · 5,471 cycles

TYS DURING A SCHEDULED 2C INSPECTION, MAINTENANCE FOUND THE RT AND LT MLG BRACE PINS SHOWING EVIDENCE OF WEAR AND CORROSION. MAINT R&R BOTH LEFT AND RIGHT MLG BRACE PINS IAW EMB 145 AMM-32-10-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: FITTING — GOUGED (HORIZ STAB) · airframe 7,872 hrs · 5,471 cycles

TYS DURING A SCHEDULED 2-C INSPECTION, MAINTENANCE FOUND A GOUGE IN THE RT HORIZONTAL STAB HINGE PIN SAFETY PIN WHICH REQUIRED A GST, ALL WORK WAS ACCOMPLISHED IAW GST WHICH STATED BLEND, ALODINE, PRIME AND PAINT SRM 51-70-03, CPM 51-21-04, 05, 06. A/C WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: STRINGER — GOUGED · airframe 7,872 hrs · 5,471 cycles

TYS DURING A SCHEDULED 2-C INSPECTION MAINT. FOUND GOUGES ON STRINGER 19L AND 19R AT STA. 17727.0. MAINT. BLENDED AND NDI TESTED AREA,NO CRACKS WERE FOUND. FAB.ALLODINE,PRIME AND INSTALLED REPAIR PARTS AT STRINGER 19L. MEASURED,BLENDED PERFORM NDI ,FOUND NO DEFECTS,ALLODINED,PRIME AND PAINTED 19RIAW EMB 135/145 SRM 53-24-02,CPM 51-21-04,05,06. ALL WORK WAS ACCOMPLISH AND WILL BE REL. UPON COMPLETION OF ALL WORK.

Part: FITTING — GOUGED (HORIZ STAB) · airframe 7,872 hrs · 5,471 cycles

TYS DURING A SCHEDULED 2-C INSPECTION MAINTENANCE FOUND A GOUGED IN THE HORIZONTAL STAB LT HINGE PIN, A GST 2827/02 WAS ISSUED, WHICH STATED ALODINE, PRIME AND PAINT IAW WITH THE GST-2827-02, EMB 145 SRM 51-71-03, CPM 51-21-04-05 AND 51-21-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: LIGHT — INOPERATIVE (FUSELAGE)

EWR - During scheduled maintenance the right over wing emergency light was found to be inoperative. Maintenance removed and replaced the emergency light, performed an operational check and approved the aircraft for return to service.

Part: CONTROL HANDLE — INTERMITTENT (COCKPIT)

CLE FLIGHT 3226 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE EICAS MESSAGE UPON GEAR RETRACTION. MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: APU — FAILED (APU BAY) · airframe 5,790 hrs · 3,924 cycles

CREW REPORTED, APU AUTO SHUTDOWN ON TAXI TO GATE, FOLLOWED BY HEAVY SMOKE SMELL AND SMOKE HAZE IN REAR CABIN. YUL MAINTENANCE INSPECTED AND DEFERRED APU IAW MEL 49-00-00, PLACARD CONTROL NUMBER 017287. AIRCRAFT RETURNED TO SERVICE. 10/19/2001 RIC MAINTENANCE REMOVED AND REPLACED THE APU IAW EMB145 MM 49-10-00. OPS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 4,359 hrs · 2,927 cycles

CREW REPORTED AFTER RETRACT GOT BRAKE OVERHEAT MESSAGE. RE-EXTENDED LANDING GEAR TO COOL, GEAR WOULD NOT RETRACT. AIRCRAFT AIR RETURNED TO EWR. MAINTENANCE OPS CHECKED SYSTEM GOOD. GEAR WOULDN''T RETRACT IN FLIGHT BECAUSE AIRCRAFT WAS GOING OVER 200 KNOTS. GEAR CHECKED OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE.

Part: SEAL — BROKEN (EMER MEDICAL KIT)

CLE - FLT 3862 - CREW REPORTED MEDICAL KIT SEAL BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY MEDICAL KIT AND RETURNED THE AIRCRAFT TO SERVICE. (M)

Part: PLATE — CORRODED (FUSELAGE)

TYS - DURING A SCHEDULED 1C INSPECTION, FORWARD DIGITAL PLATE JUST AFT OF COCKPIT DOOR HAS CORROSION ON AND AROUND RIVET HEADS. MAINTENANCE REMOVED CORRODED AREA, MEASURED DAMAGED AREA, FOUND MAX DEPTH TO BE .008 INCH. NO FURTHER ACTION NEEDED. REF EMB REF GST-203/2001. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: STOP — GOUGED (CABIN DOOR)

TYS - DURING A SCHEDULED 1C INSPECTION, THE TOP AFT RADIAL STOP ON MAIN CABIN DOOR WAS GOUGED AT CORNER. MAINTENANCE BLENDED STOP IAW EMB REF GST-0244/01. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: STOP — GOUGED (DOOR FRAME)

TYS - DURING A SCHEDULED 1C INSPECTION, MAIN DOOR FRAME STOPS NR 1 AND 7 ARE WORN AND GOUGED, STOPS NR 4, 6, 9, 11 AND 12 ARE WORN. MAINTENANCE BLENDED STOPS IAW EMB 145MM 53-21-03 AND BLENDED UPPER FORWARD STOP IAW EMB REF GST 0244/01. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: DOOR FRAME — GOUGED (FUSELAGE)

TYS - DURING A SCHEDULED 1C INSPECTION, SERVICE DOOR INNER REINFORCEMENT FRAME HAS GOUGES IN UPPER FORWARD INNER REINFORCEMENT PLATE AND BELOW PLATE IN FRAME. MAINTENANCE BLENDED GOUGES AND INSTALLED A REINFORCEMENT PLATE ON SERVICE DOOR REINFORCEMENT FRAME IAW EMB 145 SRM 51-40-02 AND EMB REF GST 0203/2001. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: FRAME — NICKED (COCKPIT)

TYS - DURING A SCHEDULED 1C INSPECTION, SCRAPES AND NICKS WERE FOUND ON LEFT COCKPIT WINDSHIELD FRAME. MAINTENANCE BLENDED, DYE PENETRANT INSPECTED, ALODINED, PRIMED AND PAINTED THE AFFECTED AREA IAW EMB REF GST 0255/01. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

TYS - DURING A SCHEDULED 1C INSPECTION, THE LEFT OMEGA BEAM AFT RAMP ANGLE BETWEEN FRAME 19 AND 20 HAS CORROSION. REMOVED RAMP ANGLE, FABRICATED NEW RAMP ANGLE IAW EMB 145 SRM 51-30-01), ALODINED AND PRIMED IAW EMB 145 CPM 51-21-04 AND 05. REINSTALLED RAMP ANGLE IAW EMB 145 SRM 51-40-02. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BEAM — CORRODED (FUSELAGE)

TYS - DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON OMEGA BEAM AT CARBON FIBER CROSS BEAM ABOVE FRAMES 20 BETWEEN STRINGERS 18L AND 19L. MAINTENANCE REMOVED AND REPLACE OMEGA BEAM AND FABRICATED Z PROFILES IAW EMB 145 SRM 51-40-01 AND EMB REF GST-0272/01. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: FIRE DETECTOR — GOUGED (APU)

TYS - DURING A SCHEDULED 1C INSPECTION, THE APU FIRE LOOP WAS GOUGED. MAINTENANCE REMOVED AND REPLACED THE APU FIRE LOOP IAW EMB 145 MM 26-10-00. OPS CHECKED GOOD. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: STOP — WORN (SERVICE DOOR)

TYS - DURING A SCHEDULED 1C INSPECTION, SERVICE DOOR FRAME STOP NR 8 WAS FOUND TO BE WORN BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACD NR 8 DOORSTOP IAW EMB-145 MM 52-43-06. (M)

Part: ANGLE — CORRODED (FUSELAGE)

TYS - DURING A SCHEDULED 1C INSPECTION, RAMP ANGLE HAS CORROSION AT CARBON FIBER CROSS BEAM ABOVE FRAMES 19 AND 20, BETWEEN STRINGERS 21L AND 21R. MAINTENANCE REMOVED AND REPLACED CARBON FIBER BEAM AND RAMP ANGLE IAW EMB 145 SRM 51-40-02. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: SUPPORT BRACKET — DAMAGED (AFT FUSELAGE)

TYS - DURING A SCHEDULED 1C INSPECTION, THE APU BLEED AIR SUPPORT BRACKET WAS FOUND GOUGING INTO THE FIREWALL HEAT SHIELD. MAINTENANCE BLENDED APU BLEED AIR SUPPORT BRACKET IAW EMB REF GST 0247/01 AND REPLACED APU HEAT BLANKET. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BLANKET — GOUGED (AFT FUSELAGE)

TYS - DURING A SCHEDULED 1C INSPECTION, THE HEAT BLANKET ON THE APU FIREWALL HAS SEVERAL GOUGES. MAINTENANCE REMOVED APU HEAT BLANKET, CLEANED AND INSPECTED, AND FOUND 2 GOUGED OUT OF LIMITS. REPAIRED DAMAGE IAW EMB REF GST 024/01, THEN REINSTALLED BLANKET. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: STRAP — CORRODED (FUSELAGE)

TYS - DURING A SCHEDULED 1C INSPECTION, CORROSION WAS FOUND ON TOP CAP ABOVE OMEGA BEAM BETWEEN FRAMES 19 AND 23, STRINGERS 21L AND 21R. MAINTENANCE REMOVED AND REPLACED TOP CAP IAW EMB 145 SRM 51-40-02. REPAIRS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

IAH - FLT 4129 - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT A SECTION OF THE CABIN EMERGENCY PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPECTED AND OPERATIOALLY CHECKED THE EMERGENCY LIGHTING SYSTEM AND FOUND IT TO BE OPERATIONAL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (RIGHT)

TYS - THE RIGHT ENGINE WAS REMOVED AND REPLACED AFTER NUMEROUS ATTEMPTS TO TROUBLESHOOT AND CORRECT A HIGH OIL PRESSURE TREND. THE REMOVAL AND REPLACEMENT OF THE RIGHT ENGINE WAS ACCOMPLISHED IAW CONTINENTAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

IAH - DURING A-CHECK INSPECTION, THE FORWARD AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB145 MM 33-50-50, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CLE - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE FORWARD AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY PACK IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN)

EWR - DURING ROUTINE CHECK, FOUND NR 2 BATTERY PACK LOW CHARGE. REMOVED AND REPLACED BATTERY PACK WITH SERVICEABLE UNIT. OPS CHECKED, SYSTEM GOOD. (X)