N15948

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 27,645 hrs · 26,733 cycles

DURING MX INSPECTION, LT WING EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. REPAIRED A BROKEN ELECTRICAL CONNECTOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 27,645 hrs · 26,733 cycles

DURING MX INSPECTION, THE RT WING EMERGENCY EXIT DOOR SIGN WAS FOUND TO BE INOPERATIVE. RESECURRED THE EXIT SIGN INVERTER ELECTRICAL CONNECTOR, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DIMMER — DEFECTIVE (COCKPIT) · airframe 26,095 hrs · 25,199 cycles

IAH - FLIGHT 2060, DURING TAXI THE CREW REPORTED A RELAY CLICKING ON THE CAPTAINS SIDE WITH LOTS OF FUMES. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REMOVED AND REPLACED SWITCH S0019 (DIMMER SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BLADE — BROKEN (NR 2 ENGINE) · airframe 25,728 hrs · 24,819 cycles

FLIGHT 2031, CREW REPORTED NR 2 ENG LP VIBRATIONS EXCEEDED LIMITS. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND R & R THE NR 2 ENGINE, OPS AND LEAK CHECK WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL HANDLE — INOPERATIVE (COCKPIT) · airframe 25,555 hrs · 24,643 cycles

IAH - FLIGHT 2544, THE CREW REPORTED THAT THE GEAR WAS SLOW TO RETRACT ON DEPARTURE FROM DAL WITH THE ASSOCIATED WARNINGS. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR HANDLE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,135 hrs · 24,206 cycles

IAH - DURING MAINTENANCE INSPECTION THE LEFT EMERGENCY EXIT LIGHT AT THE WING EXIT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 24,923 hrs · 23,993 cycles

IAH - 500 FEET ABOVE THE GROUND THE CREW REPORTED A LANDING GEAR AIR/ GRND FAIL MESSAAGE ON EICAS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE RESET THE LANDING GEAR AIR GROUND CIRCUIT BREAKER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (NLG) · airframe 24,900 hrs · 23,966 cycles

IAH - FLIGHT 2876, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON LANDING. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE BETWEEN FR 49-50 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

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

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV-DURING C-CHECK LT OMEGA BEAM LOWER SUPPORT FLANGE AT FR 54-59 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM LOWER SUPPORT FLANGE AT FRAME 54-59 IAW EMB-145 EC5310-01466. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE AT FRAME 44 TO CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FR 44 IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: YOKE — CRACKED (NR 1 ENGINE) · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK NR 1 ENGINE FWD LWR ENGINE YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED NR1 ENGINE FWD LWR ENGINE YOKE IAW EC5450-01028 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK (FR 33) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM FR 33 IAW EMB-145 SRM 53-00-10 FIG 202 STEP 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK (FR 29) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER BEAM CROSSBEAM SUPPORT AT FR 29 AND RESTORED TO ORIGINAL FINISH IAW EMB-145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK SKIN CRACKS AROUND RIVET HEAD FR 78 RT SIDE. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN FR 78 RT SIDE IAW EC5330-02260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (AILERON) · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) MISSING. MAINTENANCE REMOVED AND REPLACED RT AILERON CONTROL ROD ATTACHMENT BRACKET (I/B) ATTACHMENT POINT (I/B) BUSHING (HAT) IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK (FR 33) CTR OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK (FR 29) LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT CARBON FIBER CROSSBEAM. MAINTENANCE PERFORMED REPAIR FOR LT OMEGA BEAM L-FLANGE AT FRAME 29 IAW EMB-145 SRM 53-00-10 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK LT OMEGA BEAM L-FLANGE HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 58 CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM L-FLANGE AT FRAME 58 CARBON CROSS MEMBER IAW SRM 53-00-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK SKIN CRACKS AROUND RIVET AT RT SIDE FR 77. MAINTENANCE PERFORMED REPAIR TO AFT FUSELAGE SKIN RT SIDE FR 77 IAW EC5330-02260. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK (FR 38) CTR OMEGA BEAM L-FLANGE AT CARBON FIBER CROSSBEAM HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CTR OMEGA BEAM L-FLANGE 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 24,863 hrs · 23,930 cycles

SHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 49-50 AT CARBON CROSS MEMBER HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM "L" FLANGE AT 49-50 AT CARBON CROSS MEMBER IAW EMB-145 SRM 51-40-02, 53-00-10 AND RESTORED TO ORIGINAL FINISH TO THE REWORKED AREA IAW CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK CARGO DOOR CUTOUT LWR STRUCTURE CORRODED (LEVEL 2 LOCAL) IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER STRUCTURE IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV - DURING C-CHECK LT OMEGA BEAM AT FRAME 20 FLANGE HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE PERFORMED REPAIR ON LT OMEGA BEAM AT FRAME 19-20 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,863 hrs · 23,930 cycles

SHV-DURING C-CHECK CENTER OMEGA BEAM L-FLANGE AT FR 44 HAS CORROSION (LEVEL 2 LOCAL) TO CARBON CROSS MEMBER. MAINTENANCE PERFORMED REPAIR ON CENTER OMEGA BEAM L-FLANGE AT FRM 44 IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — DIRTY (LANDING GEAR) · airframe 26,683 hrs · 25,910 cycles

IAH - FLIGHT 2541, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND THE THRUST REVERSERS WOULD NOT DEPLOY ON LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY TESTED THE THRUST REVERSERS WITH NO DEFECTS. CLEANED THE LANDING GEAR PROX SENSORS, OPERATIONALLY TESTED THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (RUDDER) · airframe 24,784 hrs · 23,848 cycles

IAH - FLIGHT 2149, DURING POST FLIGHT INSPECTION THE CREW REPORTED A HOLE IN THE RIGHT LOWER SIDE OF RUDDER II. MAINTENANCE REPLACED THE DAMAGED SECTION OF SKIN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MODULE — INOPERATIVE (CABIN PRESSURE) · airframe 24,522 hrs · 23,581 cycles

IAH - FLIGHT 2547, DURING CLIMB THE CREW REPORTED THAT THE AUTO PRESSURIZATION WAS NOT WORKING AND THAT THE EICAS INDICATIONS WERE INTERMITTENT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CPAM MODULE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INDICATOR — DEFECTIVE (COCKPIT) · airframe 24,163 hrs · 23,220 cycles

CRP - FLIGHT 2894, DURING CLIMB THE CREW REPORTED THAT THE NUMBER ONE FUEL QUANTITY INDICATOR DASHED OUT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL QUANTITY REPEATER OPERATIONALLY TESTED THE FUEL QUANTITY WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — OUT OF ADJUST (CABIN) · airframe 24,033 hrs · 23,080 cycles

LRD - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE OVERHEAD EMERGENCY EXIT LIGHT AT ROW TWELVE TO BE INOPERATIVE. MAINTENANCE ADJUSTED THE EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,016 hrs · 23,061 cycles

IAH - DURING MAINTENANCE INSPECTION THE CEILING EMERGENCY LIGHT AT ROW 3 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT BULB, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — SHORTED (COCKPIT) · airframe 23,700 hrs · 22,733 cycles

IAH - FLIGHT 2720, THE CREW REPORTED, SMELLED ELECTRICAL SMOKE AND CB11 FOR THE COCKPIT READING LIGHTS POPPED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE F/O'S READING LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,556 hrs · 22,589 cycles

IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT LIGHT AT ROW 12CB WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 23,494 hrs · 22,529 cycles

IAH - FLIGHT 2372, THE FLIGHT ATTENDANT REPORTED A SMELL OF FUEL IN THE CABIN DURING DESCENT WITH THE SMELL COMING FROM THE WING AREA AND AFT. THE SMELL DISSIPATED AFTER THE RECIRC FAN WAS TURNED OF, AND RETURNED ON APPROACH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT RAN BOTH PACKS WITH NO DEFECTS OR SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — FUMES (CARGO BAY) · airframe 22,430 hrs · 21,365 cycles

THERE WERE SUFFOCATING FUMES AND ODOR REPORTED BY THE GROUND WORKERS COMING FROM THE CARGO BIN. THE CARGO BIN WAS INSPECTED AND FOUND ODOR TO BE RESIDUAL FROM A PASSENGER TRANSPORTING FISH, THERE WAS NO FLUIDS FOUND IN CARGO AND NO MX OR DISCREPANCIES FOUND. REL TO SERVICE.

Part: TURBINE WHEEL — CRACKED (NR 1 ENGINE) · airframe 22,298 hrs · 21,230 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 ON THE NR 1 ENGINE A CRACK INDICATION OF THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL WAS FOUND DURING THE ULTRASOUND INSPECTION. THE NR 1 ENGINE WAS REPLACED.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 22,178 hrs · 21,109 cycles

SEAT 12BC SIDEWALL AFT EMERGENCY LIGHT INOP. FOUND CONNECTOR LOOSE. TIGHTENED CONNECTOR AND OPS CHECKED GOOD. IAW EMB 145 AMM 33-50-14

Part: SKIN — CRACKED (RT WING) · airframe 19,890 hrs · 18,793 cycles

IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE GROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE AT EVER 50FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 05/01/08 TYS MAINTENANCE INSTALLED A TRIPLER REPAIR IN ACCORDANCE WITH EXPRESSJET ENGINEERING CHANGE AND REPAIR AUTHORIZATION 5740-01146, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE HARNESS — DISCONNECTED (EXIT SIGN) · airframe 16,566 hrs · 15,119 cycles

OKC - FLIGHT 2637, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE THE F/A SEAT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE SIGN TO BE DISCONNECTED. MAINTENANCE RECONNECTED THE SIGN, OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 15,884 hrs · 14,329 cycles

EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSY IAW EMB 145 AMM 33-50-10. OPS CK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 15,884 hrs · 14,329 cycles

GALLEY AREA RT OMEGA BEAM CORRODED. BLENDED OUT CORROSION, APPLIED HYSOL, FABRICATED REPAIR DOUBLER, DRILLED COUNTERSANK, ALODINED, PRIMED. INSTALLED PAINT. ALL WORK C/W IAW EMB135/145 SRM 51-10-03, 51-20-03, 51-40-06, 51-40-02 AND 53-21-10 AND CPM 51-21-04, 51-21-05 AND 51-21-06.

Part: CASTING — CRACKED (DOOR FRAME) · airframe 15,884 hrs · 14,329 cycles

MAIN DOOR FRAME STRUCTURE UPPER FWD STOP HOLE IS CRACKED (TOP INBOARD HOLE). REMOVED AND REPLACED CASTING FOR UPPER FWD PAX DOOR STOP IAW EMB 145 SRM 51-40-02.

Part: HOUSING — GOUGED (HORIZONTAL STAB) · airframe 15,884 hrs · 14,329 cycles

RT HORIZ STAB SPHERICAL BEARING HOUSING GOUGED. REWORKED HOUSING TO 1ST OVERSIZE W/ ENGINEERING APPROVAL. ALL WORK C/W IAW EC5510-01130, EC551-01080, EMB-145 AMM 55-37-00.

Part: HOUSING — GOUGED (ZONE 300) · airframe 15,884 hrs · 14,329 cycles

LT HORIZ STAB SPERICAL BEARING HOUSING GOUGED. REWORKED HOUSING TO 1ST OVERSIZE W/ENGINEERING APPROVAL. ALL WORK C/W IAW EC5510-01130, EC5510-01080, EMB145-AMM55-37-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,636 hrs · 14,059 cycles

IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,771 hrs · 13,026 cycles

CLE - DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT LOCATED ON THE PAX DOOR DID NOT ILLUMINATE DURING THE TEST. MAINTENANCE REPLACED THE LIGHT BULB AND THE OPERATIONAL TEST WAS GOOD.

Part: WIRE — LOOSE (EMERGENCY LIGHT)

IAH - DURING AIRCRAFT MODIFICATION SEVERAL EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND GROUND WIRE GS85008DC TO BE LOOSE. MAINTENANCE RESECURED THE GROUND WIRE, OPERATIONALLY CHECKED THE EMERGENCY LIGHTING SYSTEM WITH NO DEFICIENCIES NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (COCKPIT) · airframe 12,153 hrs · 10,282 cycles

CREW REPORTED (STRONG FUEL ODOR UPON APU START.) MAINTENANCE INSPECTED AND OPERATIONALLY CHECKED THE APU GOOD. NO DEFECTS NOTED (SUSPECT POSSIBLE TAILWIND DURING START PROCESS) AIRCRAFT RETURNED TO SERVICE.

Part: ACM — SEIZED · airframe 11,463 hrs · 9,576 cycles

DURING FLIGHT CREW DETECTED SMOKE IN CABIN AND COCKPIT. CREW INITIATED EMERGENCY PROCEDURES AND PERFORMED EMERGENCY DESCENT. AIRCRAFT MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND NUMBER ONE AIRCYCLE MACHINE SEIZED. MAINTENANCE REMOVED AND REPLACED NUMBER ONE AIRCYCLE MACHINE. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,505 hrs · 9,616 cycles

SHV- DURING C CHECK EMEREGENCY LIGHT ON PANEL 243 ALC FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED BULB. RETESTED AFFECTED EMERGENCY LIGHT AND OPERATED GOOD IAW EMB 145 AMM 33-50-08. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,505 hrs · 9,616 cycles

SHV- DURING C CHECK EMEREGENCY LIGHT ON PANEL 243 ALC FAILED OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED BULB. RETESTED AFFECTED EMERGENCY LIGHT AND OPERATED GOOD IAW EMB 145 AMM 33-50-08. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-22-10 FIGURE 201 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE LEFT HAND BUTTSTRAP BETWEEN FRAMES 19 AND 24 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: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 19 AND 23 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EC 5320-01099. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE LEFT HAND OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10 FIGURE 202 SHEET 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

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

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AFFECTED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CHAFED (RT COWLING) · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK NR 1 LOWER COWLING, OUTBOARD STRINGER WAS FOUND TO CHAFFED NEAR AFT RIB. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE RIGHT HAND OMEGA BEAM BUTT STRAP BETWEEN FR 59-60 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND OMEGA BEAM BUTT STRAP IAW EMB 145 SRM 53-24-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RIB — CHAFED (RT COWLING) · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE AFT RIB ON THE UPPER RIGHT COWLING WAS FOUND TO BE CHAFFED AT THE CENTER LINE. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 54-10-07. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STIFFENER — CHAFED (RT COWLING) · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE RIGHT HAND LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE LEFT HAND SILL BETWEEN FR 18-20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND SILL BETWEEN FR 18-20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE FORWARD DIGITAL BUTTSTRAP WAS FOUND TO BE CORRODED AT FR 15-17. MAINTENANCE REMOVED DAMAGED SECTION AND REPLACED FORWARD DIGITAL BUTTSTRAP AND PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH EMB SRM 53-21-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE CENTER RAMP ANGLE BETWEEN FRAMES 18 AND 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE CENTER BUTTSTRAP BETWEEN FRAMES 18 AND 23 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: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

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

Part: BUTTSTRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE CENTER 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: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,505 hrs · 9,616 cycles

SHV-DURING C CHECK THE CENTER OMEGA BEAM BETWEEN FRAMES 20 AND 22 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: UPLOCK — FAILED (MLG) · airframe 11,297 hrs · 9,414 cycles

AIRCRAFT DIVERTED INTO TYS (FLIGHT WAS SCHEDULED FROM ALANTA TO CLEVLAND) BECAUSE NOSE GEAR WOULD NOT COME UP. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR UPLOCK BOX IAW EMB-145-MM-32-33-07, OPERATIONAL CHECKED GOOD. AIRCRAFT WAS RELEASED TO SERVICE WITH NO FURTHER FAULTS.

Part: MODULE — INOPERATIVE (SMOKE DETECTOR) · airframe 10,903 hrs · 9,021 cycles

BAGGAGE SMOKE WARNING LIGHT ON OVERHEAD DOES NOT LIGHT UP DURING TEST. REMOVED AND REPLACED RELAY K0629 PLUS APU MODULE ASSY IAW EMB MM 26-13-10. OPS CHECK GOOD. RELAY IAW WMB MM CHAP 20. OPS CHECK GOOD.

Part: PROXIMITY SWITCH — FAULTY (LEFT GEAR)

CLE FLIGHT# 2052 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE ECIAS IMMEDIATELY AFTER GEAR EXTENSION BEFORE LANDING.THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.MAINTENANCE REPLACED THE LEFT MAIN GEAR AFT WOW PROXIMITY SENSOR.OPERATIONAL CHECKS WERE GOOD.

Part: HANDLE — LOOSE (MAIN DOOR)

SYR FLIGHT#2886 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE.MAINTENANCE INSPECTED AND RESECURED THE INSIDE HANDLE ON THE MAIN CABIN DOOR.OPERATIONAL CHECKS WERE GOOD.

Part: UPLOCK — FAULTY (RT MLG)

CLE FLIGHT 3214 THE CREW REPORTED A RIGHT MAIN LANDING GEAR/LEVER DISAGREE. THE RIGHT MAIN INDICATES DOWN WITH THE HANDLE UP. THE SYSTEM RESET AFTER CYCLING. MAINTENANCE INSPECTED AND REPLACED THE RIGHT MAIN GEAR UPLOCK BOX ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

CLE FLIGHT 3037, THE CREW REPORTED A RIGHT MAIN LANDING GEAR AND LEVER DISAGREE MESSAGE AFTER TAKEOFF. THE MESSAGE RESET AFTER 1ST CYCLE. MAINTENANCE PERFORMED AIR/GROUND OPERATIONAL CHECKS ON LANDING GEAR SYSTEMS. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BOLT — LOOSE (CABIN DOOR)

CLE FLIGHT#3157 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN.MAINTENANCE INSPECTED AND TIGHTENED THE INNER DOOR HANDLE ASSEMBLY BOLT.OPERATIONAL CHECKS WERE GOOD.THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BOLT — DEFECTIVE (DOOR HANDLE)

DURING ROUTINE MAINTENANCE THE MAIN ENTRY DOOR WAS DIFFICULT TO OPEN FROM OUTSIDE AND WILL NOT CLOSE FROM INSIDE. MAINTENANCE ADJUSTED THE EXTERNAL ACTUATING HANDLE AND REPLACED BOLTS TO THE INTERIOR HANDLE BRACKET.

Part: SCREW — LOOSE (CABIN)

CLE MAINTENANCE, DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE FOUND A LOOSE SCREW FOR THE INTERIOR TRIM PANEL STICKING OUT ENOUGH TO PREVENT THE DOOR FROM WORKING PROPERLY. THE SCREW WAS TIGHTENED AND OPERATIONAL CHECKS OF THE EMERGENCY EXIT WERE GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (LT MLG)

CLE FLIGHT 3750 THE CREW REPORTED THE LANDING GEAR DISAGREE MESSAGE DURING RETRACTION. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH LEFT MAIN GEAR UPLOCK PROXIMITY SENSORS. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR)

DURING A MAINTENANCE SERVICE CHECK THE EMERGENCY LIGHT OVER THE RIGHT WING WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB FOR THE EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: O-RING — LEAKING (NR 2 ENGINE)

EWR-CREW REPORTED AIR RETURN: NR 2 BLEED LEAK, LOUD NOISE AFTER TAKEOFF FROM NR 2 ENGINE. MX FOUND NR 2 BLEED LINE DISCONNECTED IN RADIO ALTIMETER ACCESS BAY, REMOVED AND REPLACED ORINGS, RECONNECTED BLEED LINE, RAN APU AND NR 2 PACK FOR ONE HOUR. NO BLEED LEAK ALERTS NOTED. NO FAULTS FOUND. A/C RETURNED TO SERVICE

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE 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. (M)

Part: SUPPORT — CORRODED (CABIN)

IAH - DURING C-CHECK INSPECTION, THE LEFT SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED NEAR FRAME 20. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A REPAIR DOUBLER ON THE AFFECTED SUPPORT IAW EMBRAER FAX SST 1274-99, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: ANGLE — CRACKED (FUSELAGE)

IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE 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. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

BTV - 3944 - DURING 2A INSPECTION MAINTENANCE, FOUND EMERGENCY LIGHTS OUT AT ROW 17 (OVERHEAD) AND SERVICE DOOR EXTERNAL. REMOVED AND REPLACED POWER SUPPLY. OPS CHECKED SYSTEM GOOD. (M)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE LEFT HAND OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE RIGHT HAND OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW EMB145 MM 33-50-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X)

Part: BATTERY CHARGER — INOPERATIVE (EMERGENCY EXIT)

EWR - FLT CO 4090 - CREW REPORTED LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 4 BATTERY CHARGER ASSY. OPS CHECKED, SYSTEM GOOD. ACFT TT: 2,213.2 HOURS. ACFT CYCLES: 1,817. (X)

Part: MLG — CONTAMINATED (MLG WW)

CLE - FLT 4115 - CREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED A LANDING GEAR DISAGREEMENT WARNING. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND LARGE QUANTITIES OF SNOW AND ICE IN THE WHEELWELLS. THE SNOW AND ICE WAS CLEANED OUT AND THE LANDING GEAR OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-145 MM 32-32-00. AIRCRAFT RELEASED FOR SERVICE. (X)