N14977

Part: WIRE — BROKEN (CABIN) · airframe 44,915 hrs · 34,057 cycles

FLOOR PROXIMITY STRIP HAS BROKEN WIRES AT FRAME 46. REPAIRED FLOOR PROXIMITY STRIP WIRES AT FRAME 46 IN ACCORDANCE WITH SWPM 20-21-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,787 hrs · 34,207 cycles

DENT AT FRAME 22A AND STRINGER 11R AREA. CUTOUT DAMAGE AREA, FABRICATED FILLER AND DOUBLER. INSTALLED, SEALED AND REFINISHED. AIRCRAFT STILL IN C CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAME 23) · corrosion level 2 · airframe 41,096 hrs · 31,035 cycles

DURING C-CHECK, THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,096 hrs · 31,035 cycles

DURING C-CK, RT OMEGA BEAM CORRODED AT FR 25. REPAIRED RT OMEGA BEAM AT FR 25 IAW SRM 53-21-10. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: FAN — INOPERATIVE (RECIRCULATION) · airframe 38,887 hrs · 29,250 cycles

THE CREW REPORTED THAT A POP WAS HEARD AT THE TOP OF CLIMB, MILD SMOKE ODOR IN COCKPIT AND CABIN, WITH THE ODOR GETTING WORSE AT HIGH POWER SETTINGS, AND WENT COMPLETELY AWAY AT LOW POWER. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE ACFT AND FOUND THE CABIN RECIRCULATING FAN TO BE INOPERATIVE. R & R THE RECIRCURLATING FAN, OPERATIONALLY TESTED WITH NO DEFECTS NOTED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,811 hrs · 29,187 cycles

EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE AT ROW 3 THRU 7. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD.

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 36,510 hrs · 27,331 cycles

CREW REPORTED A STRONG ELECTRICAL ODOR FROM THE GALLEY AREA. LANDED WITHOUT INCIDENT AND MAINTENANCE R & R THE LIGHT CONTROL MODULE, AND CABIN LIGHT BALLAST, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL MODULE — INOPERATIVE (CABIN LIGHTS) · airframe 36,510 hrs · 27,331 cycles

THER CREW REPORTED A STRONG ELECTRICAL ODOR FROM THE GALLEY AREA. LANDED WITHOUT INCIDENT AND MAINTENANCE R & R THE LIGHT CONTROL MODULE, AND CABIN LIGHT BALLAST, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 36,255 hrs · 27,140 cycles

DURING C-CHECK, THE APU FIREWALL WAS FOUND TO BE CRACKED AT THE RT UPPER AND LOWER MOUNTS. MAINTENANCE PERFORMED DOUBLER REPAIRS TO THE CRACKS IAW SRM 53-32-13, FIGURE 205. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ATTACH BRACKET — WORN (VERTICAL STAB) · airframe 36,255 hrs · 27,140 cycles

DURING C-CHECK, THE TOP RUDDER ATTACH BRACKET ON THE VERTICAL STABILIZER WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (RT AILERON) · airframe 36,255 hrs · 27,140 cycles

DURING C-CHECK, THE RT AILERON PCA BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW EC5760-01044, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,420 hrs · 23,423 cycles

DURING C CHECK, R & R OMEGA BEAM AT FRAME 18 HAS CORROSION (LOCAL LEVEL 2). MX PERFORMED REPAIR ON RT OMEGA BEAM AT FRAME 18 IAW EC5310-01631. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 31,420 hrs · 23,423 cycles

DURING C CHECK, CARGO LOWER BEAM FRAME 65-68 IS CORRODED. MX R & R CARGO LOWER BEAM BETWEEN FRAME 65-68 IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,511 hrs · 21,913 cycles

DURING SCHEDULED MX INSPECTION, THE AFT EMERGENCY EXIT GALLEY SIGN WAS FOUND TO BE INOPERATIVE. MX R & R THE AFT EMERGENCY EXIT GALLEY SIGN IAW AMM 33-50-14 WITH OPS CHECKED SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SLEEVE — LEAKING (ANTI-ICE SYS) · airframe 28,509 hrs · 21,157 cycles

ORD FLT 5817 THE CREW REPORTED WING ANTI ICE FAIL DURING CLIMBOUT WHILE ENCOUNTERING ICING CONDITIONS. MESSAGE CLEARED AFTER EXITING ICING. MAINTENANCE INSPECTED AND FOUND LEAK COMING FROM SLEEVE ON DUAL TEMP CONTRL VALVE AND FROM DUAL HEAT EXCHANGER EXHAUST DUCT. THE SLEEVE AND NR 2 HEAT EXCHANGER EXHAUST DUCT WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,119 hrs · 20,849 cycles

DURING ROUTINE MAINTENANCE THE 1ST AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD.

Part: A/C PACK — DEFECTIVE (NR 2) · airframe 28,076 hrs · 20,820 cycles

FLIGHT 2250 - PVD - FLIGHT CREW REPORTED PACK 2 OVERLOAD AND PACK OVERHEAT ON EICAS WITH SMOKE IN CABIN AND A LOUD GRINDING NOISE FROM THE MID CABIN. CLE MX REMOVED AND REPLACED PACK NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 27,719 hrs · 20,551 cycles

CREW REPORTED A LAV SMOKE DETECT INOP MESSAGE ON THE EICAS. MX INSPECTED AND REPLACED THE LAV SMOKE DETECTOR SENSOR. OPS CHECKS WERE GOOD.

Part: MODULE — INTERMITTENT (CABIN PRESSURE) · airframe 27,455 hrs · 20,352 cycles

CLE FLT 2760 THE CREW REPORTED DURING CLIMBOUT THE CABIN DIFFERENTIAL PRESSURE BEGAN TO FLUCTUATE ERRATICALLY BETWEEN 0 AND 9.0 PSI. CABIN PRESSURE AND CABIN RATE NORMAL. CONTINUED FLIGHT TO CLE WITH NO PRESSURE PROBLEMS. CABIN DIFFERENTIAL PRESSURE CHANGED BETWEEN DASHES AND 0 PSI FOR ENTIRE FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE CABIN PRESSURE ACQUISITION MODULE.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK EXTERNAL FUSELAGE HAS DENT AT FRAMES 19-20 STRINGERS 12L-13L. MAINTENANCE PERFORMED REPAIR OF EXTERNAL FUSELAGE DENT AT FRAMES 19-20 STRINGER 12L-13L IAW EC5330-02250. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK EXT FUSELAGE SKIN HAS CREASE FRAMES 19-20 STRINGER 11L. MAINTENANCE PERFORMED SKIN REPAIR AT FRAME 19-20 STRINGER 11L IAW EC5330-02250. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK SUSPECTED CRACKS AT RIVET HOLES ON RT FUSELAGE AT FRAMES 78 AND 79. MAINTENANCE PERFORMED REPAIR ON RT FUSELAGE FRAME 78 AND 79 IAW EC5330-02253 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,476 hrs · 19,618 cycles

SHV-DURING C-CHECK SUSPECTED CRACKS AT RIVET HOLES ON RH FUSELAGE AT FRAMES 76 AND 77. MAINTENANCE PERFORMED REPAIR ON RH FUSELAGE FRAME 76 & 77 IAW EC5330-02253 REV ORIG. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK SUSPECTED CRACKS AT RIVET HOLES ON LT FUSELAGE AT FRAMES 78 AND 79. MAINTENANCE PERFORMED REPAIR ON LT FUSELAGE AT FRAMES 78-79. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (HORIZ STAB) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK HORIZONTAL STABILIZER HINGE PIN RT I/B HOUSING BUSHING MIGRATED. MAINTENANCE PERFORMED REPAIR AND INSTALLED 1ST OVERSIZE BUSHING TO RT HORIZONTAL STABILIZER HINGE PIN I/B AND O/B HOUSINGS IAW EMB-145 SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK STRINGER 18L CORRODED (LEVEL 2 LOCAL) RIVETS FRAME 50-54. MAINTENANCE REMOVED AND REPLACED STRINGER 18L BETWEEN FRAMES 50-54 IAW EMB-145 SRM 51-40-02 AND SRM 53-00-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — CRACKED (ELEVATOR) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK PANEL 335FB CUTOUT IS CRACKED O/B EDGE. MAINTENANCE PERFORMED REPAIR ON PANEL 335FB CUTOUT IAW EC5520-01268. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK APU FIREWALL CRACKED AT 11 O'CLOCK POSITION VIEWING FROM AFT RIGGING BAY ACCESS. MAINTENANCE REPAIRED APU FIREWALL CRACK AT 11 O'CLOCK POSITION VIEWING FROM AFT RIGGING BAY IAW EMB-145 SRM 53-32-13 SECTION 5 FIGURE 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK APU FIREWALL CRACKED AT 9 O'CLOCK POSITION FACING AFT ON INSIDE. MAINTENANCE REPAIRED APU FIREWALL CRACK AT 9 O'CLOCK POSITION FACING AFT ON INSIDE IAW EMB-145 SRM 53-32-13 SECTION 5 FIGURE 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HINGE BRACKET — WORN (SPOILER) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING CHECK RT GROUND SPOILER I/B HINGE ATTACHMENT BRACKET I/B 1ND O/B HAT BUSHINGS MIGRATED. MAINTENANCE REMOVED AND REPLACED RT GROUND SPOILER I/B HINGE BRACKET IAW EMB-145 AMM 57-51-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BUSHING — MIGRATED (HORIZ STAB) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK HORIZONTAL STABILIZER HINGE PIN LT O/B HOUSING IS GOUGED. MAINTENANCE PERFORMED REPAIR AND INSTALLED 2ND OVERSIZE BUSHING TO LT HORIZONTAL STABILIZER HINGE PIN O/B HOUSING IAW EMB-145 SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HOUSING — GOUGED (HORIZ STAB) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK HORIZONTAL STABILIZER HINGE PIN LEFT I/B HOUSING GOUGED. MAINTENANCE PERFORMED REPAIR AND INSTALLED 2ND OVERSIZE BUSHING TO LEFT HORIZONTAL STABILIZER HINGE PIN I/B HOUSING IAW EMB-145 SRM 55-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU) · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK APU FIREWALL CRACKED AT 8 O'CLOCK POSITION FACING AFT ON INSIDE. MAINTENANCE REPAIRED APU FIREWALL CRACK AT 8 O'CLOCK POSITION FACING AFT ON INSIDE IAW EMB-145 SRM 53-32-13 SECTION 5 FIGURE 204. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK CROSSOVER BEAM AT FRAME 19 CENTER OMEGA BEAM TO RT FLOOR SILL HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REMOVED AND REPLACED CROSSOVER BEAM AT FRAME 19 CENTER OMEGA BEAM TO RT FLOOR SILL IAW EMB-145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 26,476 hrs · 19,618 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION (LEVEL 2 LOCAL) AT FRAME 23. MAINTENANCE PERFORMED REPAIR FOR LT OMEGA BEAM AT FRAME 23 IAW EC5320-01568. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTACTOR — DEFECTIVE (NR 1 BATTERY) · airframe 26,386 hrs · 19,551 cycles

IAH - FLIGHT 2937, DURING CRUISE THE CREW REPORTED AN ELECTRICAL EMERGENCY ABNORMAL MESSAGE. THE CREW PERFORMED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE BATTERY CONTACTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RECOVERY UNIT — OUT OF ADJUST (AILERON) · airframe 26,119 hrs · 19,350 cycles

CLE FLT 2578 THE CREW REPORTED THE AIRCRAFT REQUIRED A SIGNIFICANT AMOUNT OF LEFT TRIM TO COUNTER A DISTINCT RIGHT ROLL. MAINTENANCE INSPECTED AND ADJUSTED THE LEFT AND RIGHT AILERON NEUTRAL RECOVERY UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: WINDSHIELD — FAULTY (COCKPIT) · airframe 24,864 hrs · 18,404 cycles

FLIGHT 2968 - EWR - DURING PREFLIGHT, FLIGHT CREW REPORTED F/O SIDE WINDSHIELD GLOWING. EWR MX REMOVED AND REPLACED WINDSHIELD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: DOOR — DENTED (SERVICE DOOR) · airframe 24,174 hrs · 17,891 cycles

SHV - SERVICE DOOR JAMMED AND HAS MULTIPLE DENTS. REPAIRED SERVICE DOOR IAW 5240-01046. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — MALFUNCTIONED (CABIN) · airframe 23,489 hrs · 17,368 cycles

IAH - FLIGHT 3030 - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT APPROXIMATELY 5 MINUTES AFTER CONNECTING GROUND POWER, SMOKE WAS WITNESSED COMING FROM THE TOP OF THE GALLEY. MAINTENANCE PLACED THE GALLEY LIGHTING ON NEF-GL-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. LATER THAT DAY THE AIRCRAFT RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LIGHTING BALLASTS ABOVE THE GALLEY CEILING, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BALLAST — INOPERATIVE (CABIN LIGHTS) · airframe 23,489 hrs · 17,368 cycles

DURING PREFLIGHT INSP, CREW REPORTED THAT APPROX 5 MINUTES AFTER CONNECTING GROUND POWER, SMOKE WAS WITNESSED COMING FROM THE TOP OF THE GALLEY. MX PLACED GALLEY LIGHTING ON NEF -GL-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. LATER THAT DAY AIRCRAFT RETURNED TO DEPARTURE WHERE MX REMOVED AND REPLACED THE LIGHTING BALLASTS ABOVE THE GALLEY CEILING, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 23,323 hrs · 17,242 cycles

IAH - FLIGHT 2145 - DURING CRUISE, THE CREW REPORTED A NR 1 BLEED INOP MESSAGE, AND THE SWITCH WOULD NOT LATCH IN THE "ON" POSITION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLEED PUSH BUTTON, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CASE — CRACKED (NR 2 ENGINE) · airframe 16,982 hrs · 22,986 cycles

DURING COMPLIANCE OF SB AE3007A-72-368 MAINTENANCE FOUND THE NR 2 ENGINE FAN CASE HAD MULTIPLE CRACKS AROUND THE CIRCUMFERENCE OF THE CASE. THE COMPOSITE CONTAINMENT RING WAS ALSO DELAMINATED. THE FAN CASE WAS REPLACED.

Part: CIRCUIT BREAKER — BURNED (COCKPIT) · airframe 22,189 hrs · 16,401 cycles

CLE FLT 2031 - THE CREW REPORTED A HOT ELECTRONICS’ SMELL COMING FROM THE CLOSET AREA. MAINTENANCE INSPECTED AND REPLACED CB0059. OPERATIONAL CHECKS WERE GOOD.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 21,659 hrs · 16,014 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS AREAS OF CORROSION. MX REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02 AND CPM 51-21-07. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: BUSHING — MIGRATED (SERVICE DOOR)

SHV - DURING C-CHECK SERVICE DOOR UPPER HINGE AT FUSELAGE HAS MIGRATED HAT BUSHING. MX REWORKED FITTING LOCATED AT SERVICE DOOR UPPER HINGE AT FUSELAGE AND INSTALLED OVERSIZED BUSHING IAW EC 5240-01036. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (MLG)

THE CREW REPORTED A LANDING GEAR LEVER DISAGREE ON EICAS AFTER TAKEOFF. THE AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED MULTIPLE GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS ALL WITH NO DEFECTS FOUND, AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K)

Part: LIGHT — INTERMITTENT (CABIN)

CLE - DURING MAINTENANCE CHECK MAINTENANCE FOUND THAT THE MAIN CABIN DOOR EMERGENCY LIGHT WORKED INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY. ALL OPERATIONAL CHECKS WERE GOOD. (S)

Part: BLEED VALVE — FAULTY (APU) · airframe 17,441 hrs · 13,040 cycles

CLE FLIGHT 2212 THE CREW REPORTED AFTER STARTING THE APU THERE WAS A STRONG FUEL SMELL. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: LEVER — LACK OF LUBE (COCKPIT) · airframe 16,931 hrs · 12,649 cycles

CLE FLIGHT 2023 - THE CREW REPORTED NR 1 THRUST LEVER STICKS IN THE DETENT. MAINTENANCE INSPECTED AND LUBED THE THRUST LEVER TRACKS. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 16,817 hrs · 12,561 cycles

IAH FLT 2919, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING ODOR IN THE CABIN WHILE USING PACK 1. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED DEBRIS FROM THE PACK DUCTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 16,700 hrs · 12,468 cycles

SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION ON FR 38. MAINTENANCE REPAIRED LT OMEGA BEAM AT FR 38 IAW EMB 145 SRM 53-00-10 AND EC5330-01137. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 16,700 hrs · 12,468 cycles

SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION AT VARIOUS AREAS ON LOWER FLANGE BETWEEN FR 45-53. MAINTENANCE BLENDED CORROSION FROM LT OMEGA BEAM LOWER FLANGE FR 45-53, OUT OF LIMITS AT CROSSBEAM, FR 49, ALL OTHER AREAS WITH IN LIMITS IAW EMB 145 SRM 53-23-10. REPAIRED LT OMEGA BEAM AT FR 49 IAW EMB 145 SRM 53-21-10 & EC5320-01341. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 16,700 hrs · 12,468 cycles

SHV - DURING C-CK CENTER OMEGA BEAM HAS CORROSION AT FR 38. MAINTENANCE REPAIRED CENTER OMEGA BEAM AT FR 38 IAW EMB 145 SRM 53-00-10 AND EC5330-01137. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,700 hrs · 12,468 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAMES 24 AND 28. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,700 hrs · 12,468 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 34. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A SHIM FILLER REPAIR IAW EMB 145 SRM 53-00-10, FIG 202. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — GOUGED (TE FLAPS) · airframe 16,700 hrs · 12,468 cycles

SHV - MAJOR - DURING C-CHECK THE RIGHT INBOARD FLAP, INBOARD FLAP ROLLER HOUSING WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGE AND AND INSTALLED A NEW MANUFACTURED BUSHING IAW EC 5710-01124. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — FAULTY (MLG)

CREW REPORTED, LANDING GEAR/LEVER DISAGREEMENT AFTER TAKEOFF, GEAR WOULD NOT RETRACT. AIR RETURNED BACK TO EWR. MAINTENANCE REMOVED AND REPLACED LGEU IAW EMB145 AMM 32-32-01; REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE IAW EMB AMM 32-33-04 P/N:2225-0100-003, S/N:020 MANUFACTURER: EMB/LEIBHERR INC. PERFORMED RETRACTION AND EXTENSION OF LANDING GEAR SYSTEM IAW EMB145 AMM 32-30-00. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. SDR REMAINS OPEN FOR FURTHER INFORMATION.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,105 hrs · 10,444 cycles

SDF - RIGHT AFT WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT AFT WING EMERGENCY LIGHT BULB, OPS CHECK GOOD IAW EMB 145 AMM 33-50-07, 33-50-00.

Part: VALVE — LEAKING (RT WING VENT) · airframe 13,926 hrs · 10,310 cycles

CLE FLIGHT NR 2293, THE CREW REPORTED A RIGHT WING FUEL LEAK IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT WING FUEL VENT VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: FRAME — DENTED (FUSELAGE) · airframe 11,909 hrs · 8,767 cycles

DURING C-CHECK FOUND FRAME 64 DENTED AT STRINGER 16L. RECONTOURED DENT PERFORMED NDI AND INSTALLED A DOUBLER REPAIR IAW EC5330-01229.

Part: SILL — CORRODED (FUSELAGE) · airframe 9,814 hrs · 7,429 cycles

DURING C CHECK, THE SERVICE DOOR FORWARD SILL WAS FOUND CORRODED. REPLACED SILL IAW EMB SRM 51-40-02.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS)

RIC - DURING ROUTINE INSPECTION, MAINTENANCE FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED BULB IAW EMB 145 AMM 33-50-09. OPERATIONAL CHECK WAS PERFORMED SUCCESSFULLY.

Part: SMOKE — DETECTED (COCKPIT)

THE CREW NOTED SMOKE IN THE COCKPIT. THE CREW DECLARED EMERGENCY AND DIVERTED TO MEM. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF SMOKE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE THE AISLE EMERGENCY LIGHT AT ROW 12 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT LAMP AT ROW 12.OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

SHV - DURING SERVICE CHECK INSPECTION, THE AFT AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — FAULTY (COCKPIT)

BOS- THE CREW NOTED THAT THE LAV SMOKE DETECTOR WAS INOP. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR PANEL, PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — DIRTY (LAVATORY)

CLE- FLIGHT 3040, THE CREW NOTED THAT THE LAV SMOKE INDICATION ILLUMINATED THROUGH APPROXIMATELY 18,000 ON CLIMBOUT FROM BNA. PERFORMED A VISUAL INSPECTION OF LAV AND A VISUAL INSPECTION OF THE LAV EXTINGUISHER. NOTHING ABNORMAL FOUND. WARNING CEASED AFTER TESTING FROM F/A GALLEY. PULLED CB E11 & E12 PER QRH. CLEANED DUST FROM SMOKE SCREEN, PERFORMED A OPERATIONAL CHECK OF THE LAV SMOKE DETECTION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DIRTY (LAVATORY)

ICT- FLIGHT 3796, THE CREW NOTED THAT THE LAV SMOKE DETECTOR LIGHT CAME ON INFLIGHT. MAINTENANCE CLEANED CONNECTORS P8201 AND P8100, PERFORMED A OPERATIONAL CHECK OF THE LAV SMOKE DETECTION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PANEL — FAULTY (COCKPIT)

IAH- FLIGHT 3969, EN ROUTE THE CREW NOTED THAT THE LAV SMOKE WARNING ILLUMINATED. NO INDICATION OF SMOKE OR FIRE FOUND, PULLED CB'S AS SPECIFIED IN QHR. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR PANEL, PERFORMED A OPERATIONAL CHECK OF THE SYSTEM AND NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT)

EWR- DURING FLIGHT 3440, THE CREW NOTED THAT A ERRONEOUS LAV SMOKE WARNING ILLUMINATED. THE CREW VERIFIED THAT THERE WAS NO SMOKE OR FIRE. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE LAV SMOKE DETECTION SYSTEM, NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: APU — LEAKING (TAIL)

CLE- AFTER STARTING THE APU AT THE GATE THE CREW NOTED A FUEL SMELL IN THE CABIN. CLE- MAINTENANCE INSPECTED THE APU, AND, THE AIRCRAFT WAS RELEASED IAW MEL. BNA- MAINTENANCE REMOVED AND REPLACED THE APU,PERFORMED A OPERATIONAL CHECK, NO DEFECTS NOTED,AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 4,430 hrs · 3,059 cycles

CLT FLIGHT 4258 CREW REPORTED THAT DURING THEIR PRE-FLIGHT CHECKS THE PITCH TRIM NR 2 WAS INOPERATIVE. THE AIRCRAFT WAS MAINTENANCE FERRIED TO RIC AND THE HORIZONTAL STAB CONTROL UNIT WAS REMOVED AND REPLACED IAW EMB-145 MM 27-40-01. THE OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 3,880 hrs · 2,683 cycles

YUL---DURING MODIFICATION WORK IN YUL MAINTENANCE FOUND FLOOR PROXIMITY STRIP (EMERGENCY LIGHT TRACK) THREE STRIP CONNECTORS DAMAGED. REMOVED AND REPLACED EMERGENCY LIGHT TRACK IAW AMM 33-50-12. CHECKED GOOD.

Part: TIRE — FAILED (RT MLG)

MKE - FLT 4186 - THE CREW REPORTED THAT THE NR 3 MAIN TIRE TREAD CAME OFF ON LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 3 MAIN WHEEL ASSY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: STRUCTURE — DAMAGED (RT WING TE FLAP)

MKE - FLT 4186 - THE CREW REPORTED THE NR 3 MAIN TIRE TREAD CAME OFF ON LANDING CAUSING DAMAGE TO RIGHT INBOARD FLAP ASSY. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD FLAP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: LINE — DAMAGED (RT MLG BRAKE)

MKE - FLT 4186 - THE CREW REPORTED THAT THE NR 3 MAIN TIRE TREAD CAME OFF ON LANDING CAUSING DAMAGE TO NR 3 BRAKE LINE. MAINTENANCE REMOVED AND REPLACED THE NR 3 BRAKE LINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)

Part: MODULE — SHORTED (CABIN)

CLE - FLT 4011 - ON TAXI FROM THE GATE, THE FLIGHT ATTENDANT NOTICED A BURNING SMELL IN THE FORWARD CABIN. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE INTERIOR LIGHT CONTROL MODULE (CABIN) IAW EMBRAER MM 33-21-01. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: SMOKE — DETECTED (COCKPIT)

CLE - FLT 4030 - THE CREW REPORTED SMOKE IN CABIN AND COCKPIT INFLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND RAN ENGINES WITH BLEEDS OPEN TO REMOVE RESIDUAL COMPRESSOR WASH FLUID. NO SMOKE IN AIRCRAFT WAS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: RIB — CRACKED (NR 2 PYLON)

PHX - DURING B-CHECK, NR 2 ENGINE PYLON AFT FAIRING SUPPORT STRUCTURES INNER RIB CRACKED ENTIRE LENGTH OF THE RIB. REPAIRED PANEL RIB PER SRM 54-50-00 AND 51-30-2. (M)

Part: PANEL — CRACKED (NR 1 PYLON)

PHX - DURING C-CHECK, NR 1 PYLON HAS A CRACK AND MISSING MATERIAL FROM INTERNAL WEB ON LOWER AFT PANEL. MAINTENANCE REMOVED AND REPLACED DAMAGED AREA PER SRM 54-00-00. (M)

Part: INTERCOSTAL — CORRODED (CABIN)

PHX - DURING B-CHECK, FLOOR PANELS UNDER AFT LAVATORY AND GALLEY SPOTTED WITH CORROSION. REMOVED PANELS AND FOUND TWO FLOOR INTERCOSTAL BEAMS CORRODED AT STATION C72-C75, RBL 48-66. REPLACED FLOOR INTERCOSTAL BEAMS PER SRM 51-10-10 AND TREATED AREA AND PANELS PER SRM 53-10-10, 51-10-30. (M)

Part: INTERCOSTALS — CORRODED (BS 1163-1238)

PHX - DURING B-CHECK, INTERCOSTALS UNDER FORWARD LAVATORY AND GALLEY FROM STATION 1163 TO STATION 1238 (FRAME 14 AND FRAME 15A), BOTH 1 AND 2 LEFT AND RIGHT OF CENTER LINE, ARE CORRODED. RIGHT FRAME HAS 2.5 INCH DIAMETER WITH 15 PERCENT OF TOTAL THICKNESS AND LEFT FRAME HAS 2.5 INCH DIAMETER 10 PERCENT OF TOTAL THICKNESS. CORROSION CONDITIONS ON INTERCOSTALS BETWEEN FRAMES 14 AND 15A WAS DEFERRED BY AIRBUS INDUSTRIES LETTER DATED 12/9/95 UNITL AIRCRAFT NEXT C(2-8-96) FOR FINAL REPAIRS. PRESIDENTIAL AIR HAS ISSUED A MAINTENANCE CARRY OVER ITEM UNTIL FINAL REPAIRS COMPLETED. (M)

Part: TAILCONE — CRACKED (NR 1 ENGINE)

PHX - DURING B-CHECK, NR 1 ENGINE TAILCONE HAS CRACK ON AFT LOWER END OF TAILCONE. REPAIRED TAILCONE BY WELDING CRACK CONDITION PER AC 43-13-1A. (M)

Part: PANEL — BUCKLED (NR 1 ENG PYLON)

PHX - DURING B-CHECK, NR 1 ENGINE PYLON PANEL NR 474CR BUCKLED ON LOWER TRAILING EDGE. REPAIRED PANEL PER SRM 51-42-20. (M)

Part: PANEL — CRACKED (NR 1 PYLON)

PHX - DURNG B-CHECK, NR 1 ENGINE PYLON PANLE NR 475CL HAS LOOSE FASTENERS AND CRACK PROGRESSING TOWARD FASTENERS HOLE. REMOVED AND REPLACED LOOSE FASTENERS PER SRM 51-30-1. INSTALLED DOUBLER OVER CRACK CONDITION PER SRM 51-30-1. (M)

Part: PANEL — CRACKED (NR 1 PYLON)

PHX - DURING B-CHECK, NR 1 ENGINE PYLON PANEL NR 483DL WAS CRACKED AND BUCKLED. REPAIRED PANEL PER SRM 51-42-20. (M)

Part: PANEL — BUCKLED (NR 1 ENG PYLON)

PHX - DURING B-CHECK, NR 1 PYLON PANEL NR 474DR HAS LOWER LEADING EDGE AND TRAILING EDGE BUCKLED. REPAIRED PANEL PER SRM 51-42-20. (M)

Part: BATTERY PACK — DISCHARGED (L-4 DOOR)

L-4 DOOR OVERHEAD EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED 2 BATTERY PACKS PER MM 33-51-14. LIGHT OPS CHECK GOOD. (M)