N36915

Part: RIB — CRACKED (LT WING) · airframe 41,367 hrs · 31,802 cycles

LEFT WING RIB 5 CRACKED.

Part: RIB — NOT REPORTED (NOT REPORTED) · airframe 41,367 hrs · 31,802 cycles

REPAIRED RIB 5 IAW ETD 2019-145-095616.

Part: RIB — CRACKED (NOT REPORTED) · airframe 41,367 hrs · 31,802 cycles

RH RIB 5 CRACKED. REPAIRED RIB 5 IAW ETD 2019-145-095615

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 41,194 hrs · 31,671 cycles

DURING MX INSPECTION THE EMERGENCY LIGHTS WERE FOUND INOP. MX REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK WITH OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 39,099 hrs · 29,985 cycles

THE CREW REPORTED THAT THE EMERGENCY EXIT SIGN ABOVE THE FA SEAT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EXIT SIGN, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,000 hrs · 26,678 cycles

THE CREW REPORTED EMERGENCY LIGHTS BETWEEN ROW 2 AND 3 WERE NOT WORKING. MAINTENANCE INSPECTED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY PACK. OPS CHECKED GOOD.

Part: SKIN — CORRODED (ZONE 100) · airframe 34,855 hrs · 26,562 cycles

MAINTENANCE DISCOVERED THE NR 2 AFT RA ANTENNA HAD 4 NUTPLATES CORRODED ALSO FOUND ANTENNA SUPPORT PLATE TO BE CORRODED AND CRACKS AROUND FASTENER HOLES. MAINTENANCE REPAIRED DAMAGED SKIN LOCATION BY REMOVING DAMAGED SKIN AND FABRICATING AND INSTALLING REPAIR DOUBLER IAW ETD 2015-145-063091A AND EA 3440-01052.

Part: UNKNOWN — ODOR (COFFEEMAKER) · airframe 34,275 hrs · 26,113 cycles

CREW REPORTED A LIGHT ELECTRICAL BURNING ODOR FROM THE RT COFFEEMAKER AND ODOR CLEARED WHEN COFFEEMAKER WAS TURNED OFF. MAINTENANCE PERFORMED OPS CHECK FOR NR 1 COFFEEMAKER WITH NO ODORS NOTED. AC WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 32,790 hrs · 24,977 cycles

DURING C-CHECK, CARGO DOOR LOWER BEAM BETWEEN FRAMES 65-68. R & R CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 32,680 hrs · 24,883 cycles

THE CREW REPORTED UNUSUAL ODOR, BURNING OR ELECTRICAL, LIGHTS IN ROW 7 ARE HOT. MAINTENANCE INSPECTED AND REPLACED ROW 7A READING LIGHT. OPS CHECKED GOOD.

Part: SKIN — NICKED (ZONE 200) · airframe 31,257 hrs · 23,786 cycles

DURING A-CHECK INSPECTION, A NICK WAS DISCOVERED IN THE FUSELAGE SKIN UNDER THE GPU ACCESS DOOR. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A DOUBLER REPAIR AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: RELAY — INOPERATIVE · airframe 29,677 hrs · 22,610 cycles

BAGGAGE EXTINGUSHING BUTTON NOT ILLUMINATING DURING FIRE DETECTION TEST. R & R RELAY. OPS CHECK GOOD ACFT RELEASED AND RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,039 hrs · 22,111 cycles

THE ACFT SUSTAINED LIGHTNING STRIKE DAMAGE ON THE FUSELAGE SKIN BETWEEN STR 1R & 2R FR 16/17. MX PERFORMED A MAJOR REPAIR IAW SRM 53-00-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,039 hrs · 22,111 cycles

THE AFT SUSTAINED LIGHTNING STRIKE DAMAGE ON THE FUSELAGE SKIN BETWEEN STR 20R & 19R FR 29 & 30 MX PERFORMED A MAJOR REPAIR IAW SRM 53-00-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,039 hrs · 22,111 cycles

THE ACFT SUSTAINED LIGHTNING STRIKE DAMAGE ON THE FUSELAGE SKIN BETWEEN STR 20R & 19R FR 27 & 28 MX PERFORMED A MAJOR REPAIR IAW SRM 53-00-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,039 hrs · 22,111 cycles

THE ACFT SUSTAINED LIGHTNING STRIKE DAMAGE ON THE FUSELAGE SKIN BETWEEN STR 11R & 9R FR 1 & 2 MX PERFORMED A MAJOR REPAIR IAW SRM 53-00-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,039 hrs · 22,111 cycles

THE ACFT SUSTAINED LIGHTNING STRIKE DAMAGE ON THE FUSELAGE SKIN BETWEEN STR 2R & 4R FR FORWARD OF FR 13 MX PERFORMED A MAJOR REPAIR IAW SRM 53-00-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 27,918 hrs · 21,226 cycles

DURING C-CHECK THE LT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FRAME 79 BETWEEN STRINGERS 6L/7L. MX REAMED OUT THE SKIN CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02622. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 27,918 hrs · 21,226 cycles

DURING C-CHECK THE RT AFT FUSELAGE SKIN WAS FOUND TO BE CRACKED AROUND A RIVET AT FRAME 79 STRINGER 5R/6R. MX REAMED OUT THE SKIN CRACK AND PERFORMED A BUSHING REPAIR IAW EC5330-02622. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — WORN (RUDDER) · airframe 27,918 hrs · 21,226 cycles

DURING C-CHECK THE RUDDER II CENTER UPPER MOUNT FITTING FOR THE RUDDER I HINGE WAS FOUND TO BE MISALIGNED. MX REPAIRED THE WORN BOLT HOLES IN THE FITTING AND REINSTALLED IT IAW EC5540-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONNECTOR — DEFECTIVE (SPOILER SYS) · airframe 25,317 hrs · 19,180 cycles

THE CREW REPORTED SPOILER FAIL MESSAGE IN FLIGHT AND PERFORMED AN AIR RETURN BACK TO ORD. MX INSPECTED AND REMOVED AND REPLACED SPOILER PROX SENSOR CONNECTOR, CONNECTOR PIN P1166. OPERATIONAL CHECKS WERE GOOD.

Part: STRUT — LOW PRESSURE (NLG) · airframe 23,174 hrs · 17,466 cycles

MKE FLT 2866 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER T/O. ALSO REPORTED A THRUST REVERSER DISAGREE MESSAGE. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE NOSE GEAR STRUT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED BACK TO SERVICE.

Part: INLET — CORRODED (NR 1 ENGINE) · airframe 22,927 hrs · 17,279 cycles

NR 1 ENGINE AIR INLET HAS 36 BOLT HOLES THAT ARE CORRODED. REPAIRED FLANGE HOLES BY REMOVING PREVIOUS BUSHING REPAIRS, REAMED HOLES AND INSTALLED COUNTERSUNK BUSHINGS IAW EC5420-01158 REV C.

Part: DOOR — OUT OF ADJUST (CABIN) · airframe 22,823 hrs · 17,191 cycles

MAIN CABIN DOOR HARD TO OPEN. ADJUSTED MAIN CABIN DOOR IAW EMB 145 AMM 52-18-06. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: RELAY — MALFUNCTIONED (COCKPIT) · airframe 22,015 hrs · 16,582 cycles

IAH - FLIGHT 2520, THE CREW REPORTED ELECTRICAL RELAY CONTINUED TO CLICK, AFTER T/O IT SLOWED DOWN CLICKING BUT CONTINUED WHEN THE GEAR WAS LOWERED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAYS K0023 & K0455, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: RELAY — MALFUNCTIONED (COCKPIT) · airframe 22,015 hrs · 16,582 cycles

IAH - FLIGHT 2520, THE CREW REPORTED ELECTRICAL RELAY CONTINUED TO CLICK, AFTER T/O IT SLOWED DOWN CLICKING BUT CONTINUED WHEN THE GEAR WAS LOWERED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RELAYS K0023 & K0455, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TIP CAP — DAMAGED (LT WING) · airframe 22,012 hrs · 16,580 cycles

LIGHTNING STRIKE. AIRCRAFT FERRIED TO TYS FOR LIGHTNING STRIKE INSPECTION AND REPAIRS. REPLACED LT WING TIP AND REPLACED LT NLG DOOR. REPAIRED RT ELEVATOR TIP IAW SRM 51-70-06. PERFORMED RECTANGULAR DOUBLER REPAIR AT STR 21L-20L AND FRM 18-20 IAW SRM 53-21-01. BLENDED, PRIMED AND PAINTED SEVERAL MINOR BURN MARKS THAT ARE WITHIN LIMITS IAW EMB 145 SRM 53-00-01. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SCREW — LOOSE (COCKPIT) · airframe 20,590 hrs · 15,567 cycles

IAH - FLIGHT 3038, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL COMING FROM THE RIGHT RELAY SUPPORT / DISTRIBUTION AREA. MAINTENANCE INSPECTED THE AIRCRAFT AND TIGHTENED VERY LOOSE SCREW ON THE FH ESSENTIAL DC BUS 2 BUS BAR, VERIFIED REMAINING SCREWS TO BE TIGHT, AND REMOVED AND REPLACED TWO RELAYS THAT OVERHEATED DUE TO THE LOOSE CONNECTION. OPERATIONAL CHECKS WERE PERFORMED WITHOUT DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 19,628 hrs · 14,828 cycles

THE CREW REPORTED THAT ON CLIMB THE LANDING GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE GEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 19,526 hrs · 14,749 cycles

IAH - FLIGHT 2012, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR — DIRTY (PAX DOOR) · airframe 19,196 hrs · 14,499 cycles

FLIGHT 2718 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR NOT OPENING. EWR MX CLEANED AND LUBED MAIN CABIN DOOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,307 hrs · 11,119 cycles

IAH - FLIGHT 2942, DURING PREFLIGHT INSPECTION THAT SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE AFFECTED EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIRE WARNING — MALFUNCTIONED (APU) · airframe 13,775 hrs · 10,677 cycles

FLIGHT 2600 - THE CREW REPORTED THAT AN APU FIRE WARNING INDICATION HAD ILLUMINATED WHILE THE AIRCRAFT WAS PARKED AT THE AIRPORT TERMINAL. THE APU FIRE BOTTLE WAS DISCHARGED AS A RESULT OF THE WARNING. MAINTENANCE INSPECTED THE APU AN FOUND NO EVIDENCE OF A FIRE OR SMOKE. THE FIRE BOTTLE WAS REPLACED AND OPERATIONAL CHECKS OF THE APU AND IT'S ASSOCIATED FIRE DETECTION SYSTEM WERE PERFORMED. THE OPERATIONAL CHECKS PROVED SATISFACTORY AND THE DISCREPANCY WAS CLEARED.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 13,560 hrs · 10,499 cycles

CARGO BAY SMOKE INDICATION AT 19000 FT IN DESCENT. NO EICAS MESSAGE. LOOKED AND SAW NO SMOKE IN CARGO BAY. REMOVED AND REPLACED NR 1 BAGGAGE SMOKE DETECTOR IAW EMB145 MM 26-15-01. OPS CHECK GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,932 hrs · 9,255 cycles

IAH - FLIGHT 2547, THE CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 12 WAS INOPERATIVE. MAINTENANCE INSPECTED THAT AIRCRAFT, OPERATIONALLY CHECKED THE EMERGENCY EXIT LIGHTS WITH NO DEFECTS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 11,627 hrs · 9,024 cycles

DURING ROUTINE MAINTENANCE THE EXIT ROW CEILING PANEL EXIT IDENTIFIER SIGN WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 6 INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,727 hrs · 6,773 cycles

SHV - DURING C-CHECK THE LEFT OMEGA BEAM HAS CORROSION BETWEEN FR 22 & 25. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED A DOUBLER REPAIR EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,727 hrs · 6,773 cycles

SHV - DURING C-CHECK CENTER OMEGA BEAM INNER SURFACE HAS CORROSION BETWEEN FR 24 & 25. MAINTENANCE REMOVED THE DAMAGE AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-23-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LAMP — FAULTY (EMERGENCY LIGHT)

DURING ROUTINE INSPECTION MAINTENANCE FOUND SEAT 12BC PSU EMERGENCY LIGHT TO BE INOPERATIVE. RELAMPED EMERGENCY LIGHT ASSEMBLY AT 12BC PSU IAW AMM 33-50-07. OPS CHECKED GOOD.

Part: FIREWALL — CRACKED (APU BAY) · airframe 4,108 hrs · 3,160 cycles

SHV-DURING C CHECK APU FIREWALL WAS FOUND TO HAVE A CRACK AT TOP 2 RIVETS OF R/H VERTICAL REINFORCEMENT. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FLOORBEAM — CORRODED (CABIN) · corrosion level 2 · airframe 4,108 hrs · 3,160 cycles

SHV-DURING C CHECK THE LEFT HAND OMEGA BEAM AT FRAME 20 INBOARD SIDE WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGED AREA AND PERFORMED A SPLICE REPAIR IAW EMB 145 SRM 53-21-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FIREWALL — CRACKED (APU BAY) · airframe 4,108 hrs · 3,160 cycles

SHV-DURING C CHECK APU FIREWALL WAS FOUND TO HAVE A CRACK AT FAR RIGHT FASTENER HOLE OF 2ND HORIZONTAL REINFORCEMENT FROM TOP. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC 5330-01202. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: ENGINE — SHUTDOWN · airframe 3,466 hrs · 2,619 cycles

CVG---CO3395, CREW REPORTED, "SMOKE IN COCKPIT AND CABIN ASSOCIATED WITH HIGH ITT ON #1 ENGINE AND COMPLETE LOSS OF OIL PRESSURE. NO FIRE WARNINGS OR INDICATIONS OTHER THAN SMOKE. SMOKE DISSAPATED WHEN # 1 ENGINE WAS SHUTDOWN." MAINTENANCE REMOVED AND REPLACED #1 ENGINE IAW EMB145 AMM #71-00-00. OPS. CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.