N14188

Part: SKIN — DENTED (ZONE 100) · airframe 44,150 hrs · 29,861 cycles

APU COWLING LOWER SKIN FOUND WITH TWO PROTRUSIONS. DENTS 1 AND 2 WERE REPAIRED. DENT 3 IS FREE OF SHARP EDGES AND THERE ARE NO SIGNS OF MISSING OR PULLED FASTENERS. DETAILED VISUAL INSPECTION WAS PERFORMED AND NO DAMAGED WERE FOUND.

Part: THRUST REVERSER — DAMAGED (LEFT) · airframe 44,150 hrs · 29,861 cycles

LEFT ENGINE THRUST REVERSER FWD OUTBOARD EDGE DAMAGED AND TORN. THE REPAIR HAS BEEN COMPLETED.

Part: SKIN — DAMAGED (ZONE 100) · airframe 44,150 hrs · 29,861 cycles

APU COWLING WITH SKIN DAMAGED ON REAR EDGE LH AREA. APU COWLING SKIN ON FR06 FOUND WITH SEVERAL CRACKS ON EDGE. WORK WAS PERFORMED ON THE APU COWLING ACCOMPLISHING TYPE B BLEND OUTS. ADDITIONALLY, CRACK 3 AND 4 WERE REPAIRED.

Part: DOOR FRAME — DAMAGED (ZONE 100) · airframe 44,150 hrs · 29,861 cycles

AFT TOP CORNER OF BAGGAGE DOOR AIRFRAME SIDE MISSING A SECTION OF MATERIAL WHERE BAGGAGE DOOR MATES COMPLY WITH PERMANENT REPAIR. PERMANENT REPAIR WAS PERFORMED.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 44,150 hrs · 29,861 cycles

CRACKS ON FLOOR PANELS 262AF AND 262BF. REPAIR WAS PERFORMED.

Part: NUT — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,150 hrs · 29,861 cycles

ALL FOUR APU COWLING ATTACH SPHERICAL NUTS RUSTED AND BOLTS ALSO. REMOVAL OF RUST WAS PERFORMED.

Part: PLATE — SCRATCHED (ZONE 100) · airframe 44,150 hrs · 29,861 cycles

NOSE LANDING GEAR WELL WALL RH FOUND WITH SCRATCHES ON PLATE. DIGITAL PLATE WAS REPLACED.

Part: PLATE — CRACKED (ZONE 600 AILERON) · airframe 43,966 hrs · 29,677 cycles

RH AILERON DAMPER MOUNT PLATE CRACKED. FULLY REMOVED RH AILERON ASSY AND INSTALLED NEW AILERON.

Part: LIGHT — MISINSTALLED (ZONE 200) · airframe 43,304 hrs · 29,028 cycles

RH OVERWING EXTERNAL EMERGENCY LIGHT INSTALLED UPSIDE DOWN. REMOVED AND REINSTALLED RH OVERWING EXTERNAL EMERGENCY LIGHT IN CORRECT POSITION.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 43,213 hrs · 28,946 cycles

EMERGENCY LIGHTS ON INTERIOR FAILED OPS CHECK. CHARGED BATTERIES. PERFORMED CHECK OF EMERGENCY LIGHTING SYSTEM. OPS CHECK SAT

Part: WIRE — DAMAGED (ZONE 200) · airframe 42,153 hrs · 27,932 cycles

MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. FOUND INCOMPLETE / DIRTY GROUND. CLEANED AND REINSTALLED GROUND WIRE TERMINAL. OPS CHECK SAT

Part: LAMP — INOPERATIVE (ZONE 800) · airframe 42,147 hrs · 27,926 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MAIN DOOR EMERGENCY EXIT LAMP. OPS CHECK SAT

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 42,147 hrs · 27,926 cycles

EMERGENCY EXIT AISLE CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT CEILING LAMP. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 39,886 hrs · 25,785 cycles

#1 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT

Part: FRAME — CRACKED (FRM 59 S15-16L) · airframe 39,663 hrs · 25,577 cycles

CF 4, FRAME 59, LH FRAME SECTION FOUND CRACKED BTW STR 15L-16L. CF4, FR59, LH FRAME SECTION SPLICE BTW STR 14L-16L REMOVED FOR ACCESS. CF4, FR59, LH FRAME SECTION BTW STR 15L-16L CRACK REMOVED AND FRAME REPAIRED

Part: FLOOR SUPPORT — CORRODED (FRMS 47-53) · corrosion level 2 · airframe 39,663 hrs · 25,577 cycles

CF 3, LH OMEGA BEAM #6 INBD FLANGE BTWN FRAME 47-53 FOUND CORRODED. CF3, LH OMEGA BEAM #6 INBD FLANGE BLENDED OUT OF LIMITS. CF3, LH OMEGA BEAM TRIM REMOVED FOR ACCESS. AT CF3, LH OMEGA BEAM #6 INBD FLANGE BTW FR 47-53 REPAIR COMPLETE AND OMEGA BEAM TRIM REINSTALLED

Part: FLOOR SUPPORT — CRACKED (FRMS 33-37) · airframe 39,663 hrs · 25,577 cycles

CF2, LH OMEGA BEAM #3 CRACKS SUSPECTED FOUND AT FRAME 33-34 ON FLOOR STRUCTURE. AFTER NDT INSPECTION, TWO CRACKS CONFIRMED ON LH OMEGA BEAM #3 AT FR33 AND FR 34 NEED TO BE REPAIRED. CF2, LH OMEGA BEAM CRACK AT FR 33,34 REPAIRED

Part: SKIN — DAMAGED (FRM 9-10 S13-15L) · airframe 39,663 hrs · 25,577 cycles

FWD FUSELAGE EXT, DAMAGE FOUND ON LH SIDE SKIN BTW FR 9-10 AND BTW STR 13L-15L. FWD FUSELAGE EXT, L SIDE SKIN BTW FR 9-10 AND BTW STR 13L-15L, DAMAGE BLENDED FOUND OUT OF LIMITS. REMAINING THICKNESS 0.053" ON NOMINAL 0.063. FWD FUSELAGE EXT, LH SIDE SKIN BTW FR 9-10 AND BTW STR 13L-15L, DAMAGE REPAIRED.

Part: NONE — SEIZED · airframe 38,787 hrs · 24,799 cycles

SMOKE AND FUMES IN THE COCKPIT AND CABIN. FOUND PACK 1 ACM TO BE SEIZED. REMOVED AND REPLACED LH ACM/ OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,496 hrs · 23,626 cycles

RH EMERGENCY LIGHT INOPERATIVE. R&R LIGHT BULB. OPS CHECK NOT SAT. REMOVED AND REPLACED #2 BATTERY POWER SUPPLY, OPS CHECK SAT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND #1 INVERTER FOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED #1 EMERGENCY LIGHT INVERTER, OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND EMERGENCY EXIT SIGN ABOVE FORWARD F/A SEAT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-23) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND FLOORBOARD SILL CORRODED AT FRAME 18-23 LEFT SIDE. MAINTENANCE REPLACED FLOORBOARD SILL AT FRAME 18-23.

Part: GUSSET — CORRODED (LAVATORY) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND LAV LEFT GUSSET CORRODED AROUND FORWARD SCREW HOLE. MAINTENANCE REPLACED LAV LEFT HAND GUSSET.

Part: SKIN — DENTED (MAIN DOOR) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND MAIN CABIN DOOR EDGE SKIN DENTED AT LOWER AFT CORNER. MAINTENANCE REPAIRED I/A/W ETD2019-145-156108 AND SRM 52-10-01

Part: PIN — CORRODED (H/S HINGE) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND RIGHT SIDE HORIZONTAL STABILIZER HINGE PIN CORRODED. MAINTENANCE REPLACED RIGHT HORIZONTAL STABILIZER HINGE PIN.

Part: HINGE PIN — CORRODED (HORIZONTAL STAB) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND LEFT HAND HORIZONTAL STABILIZER HINGE PIN CORRODED. MAINTENANCE REPLACED LEFT HAND HORIZONTAL STABILIZER HINGE PIN.

Part: FLOORBEAM — CORRODED (FRAME 62) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND FLOORBEAM AT FRAME 62 /STRINGER 16R TO BE CORRODED. MAINTENANCE REPLACED CORRODED FLOORBEAM AT FRAME 62/ STRINGER 16

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND LEFT HAND FLOOR SILL CORRODED @ AFT SCREW HOLE FRAME 59. MAINTNENACE REPLACED LEFT FLOOR SILL @FRAME 53-59,

Part: GUSSET — CORRODED (LAVATORY) · airframe 36,416 hrs · 22,744 cycles

DURING C CHECK INSPECTION FOUND CENTER LAV GUSSET CORRODED @AFT SCREW HOLE. MAINTNENACE REPLACED THE LAV CENTER GUSSET.

Part: SKIN — CRACKED (FRAMES 68-69) · airframe 35,350 hrs · 21,975 cycles

DURING SCHEDULED MAINTNENACE CHECKS FOUND SKIN DAMAGE AT THE #2 RADIO ALTIMETER BASE BETWEEN FRAMES 68-69 AND STRINGERS 21L-21R. THE DAMAGE IS IN THE FORM OF CRACKING AROUND THE FASTNER HOLES USED TO SECURE THE #2 RADIO ALTIMETER. MAINTENANCE REPAIRED I/A/W SRM 53-00-23 AND ETD 2019-145-018727

Part: SKIN — DENTED (FRAMES 19-20) · airframe 35,078 hrs · 21,786 cycles

IAH FLIGHT 4446, DURING GROUND INSPECTION A DENT WAS FOUND ON THE FUSELAGE SKIN AFT OF THE MAIN DOOR BETWEEN FRAME 19-20 AT STRINGER 4L-5L. MAINTENANCE REMOVED THE DAMAGE, AND INSTALLED A EPAIR DOUBLER ON THE AFFECTED AREA. LEAK CHECKS WERE PERFORMED SATISFACTORILLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 35,072 hrs · 21,781 cycles

IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY EXIT SIGN ON THE LEFT HAND COCKPIT PARTITION WA SFOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — DEFECTIVE (GALLEY) · airframe 29,959 hrs · 18,155 cycles

ACFT WAS FOUND TO HAVE THE EMERGENCY LIGHT STRIP DAMAGED AT THE AFT GALLEY. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT THE AFT GALLEY IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,620 hrs · 16,480 cycles

DURING ROUTINE MAINTENANCE THE RT EMERGENCY EXIT ROW DOOR LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE RT EXIT DOOR EMERGENCY LIGHT INVERTER. OPS CHECKED GOOD.

Part: INVERTER — FAULTY (EMERGENCY LIGHTS) · airframe 26,018 hrs · 15,358 cycles

DURING ROUTINE MAINTENANCE THE AFT AISLE CELING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 23,178 hrs · 13,553 cycles

DURING MX INSPECTION, THE NR 3 EMERGENCY LIGHT BATTERY FAILED OPS CHECK. MAINTENANCE R & R THE BATTERY PACK AND OPS CHECKED SUCCESSFUL. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 22,600 hrs · 13,171 cycles

AFTER DEPARTURE, RECEIVED A REPORT FROM THE TOWER THAT THEY WERE VENTING FUEL FROM THE RT WING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING FLAPPER VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 19,634 hrs · 11,257 cycles

THE CREW REPORTED SMOKE IN CABIN DURING CLIMBOUT WHEN ENGINE BLEED 1 SELECTED. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED NR 1 ENGINE, OPS CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 18,888 hrs · 10,776 cycles

GALLEY AREA FWD DIGITAL CORRODED IN SEVERAL AREAS BEYOND LIMITS. REMOVED CORROSION, FABRICATED FILLER AND DOUBLER, PRIMED AND PAINTED.

Part: ENGINE — LEAKING (NR 1) · airframe 13,879 hrs · 7,563 cycles

PHX - FLIGHT 2843 THE CREW REPORTED SMOKE IN THE CABIN AND COCKPIT ON SHORT FINAL FOLLOWED BY A LAV SMOKE WARNING ON EICAS. THE AIRCRAFT LANDED AT PHX WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT FOR A FERRY FLIGHT TO IAH. THE AIRCRAFT FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROBE — INOPERATIVE (PITOT HEAT) · airframe 13,693 hrs · 7,451 cycles

IAH - FLIGHT 3137, THE CREW REPORTED THAT THE PITOT 3 HEAT WAS INOPERATIVE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE PITOT STATIC PROBE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 12,356 hrs · 6,741 cycles

IAH - FLIGHT 2233, DURING CRUISE FLIGHT THE CREW REPORTED A PITCH TRIM FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT (HSCU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (FUEL SYSTEM) · airframe 12,199 hrs · 6,652 cycles

FLIGHT 3150 - PBI - DURING CLIMB CREW REPORTED RT WING FUEL LEAK. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED FLAPPER VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR SYS) · airframe 10,447 hrs · 5,725 cycles

IAH - FLT 4918 - THE CREW REPORTED THAT THE WEATHER RADAR WAS INOPERATIVE AND GAVE CODES 16 & 24 IN TEST MODE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RADAR R/T/A, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — FAULTY (TE FLAP) · airframe 9,672 hrs · 5,309 cycles

DURING CLIMB THE CREW RECEIVED A FLAP FAIL MESSAGE AND ELECTED TO RETURN TO IAH. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT. THE AIRCRAFT WAS OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED.

Part: OIL COOLER — CONTAMINATED (APU) · airframe 9,451 hrs · 5,189 cycles

FLIGHT 2342 - EWR - FLIGHT CREW REPORTED LAV SMOKE ON EICAS ON T/O AND PAX DESCRIBED DISTINCT ODOR ON T/O AND LANDING. EWR MX CLEANED APU OIL COOLER AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 6,835 hrs · 3,669 cycles

FLT 1340 - TYS TO TYS - FLIGHT CREW REPORTED BLEED 1/2 LOW TEMP WITH WING 2 FAIL, IT WAS AN AIR RETURN AND DECLARED NO EMERGENCY AT THE TIME AND AIRCRAFT LANDED WITH NO INCIDENTS. MX PERSONNEL REMOVED AND REPLACED NR 2 ENG BLEED VLV AND OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 6,832 hrs · 3,667 cycles

BLEED 1 & 2 LOW TEMP WING ANTI ICE (2) FAIL WHILE IN ICING CONDITIONS. REMOVED AND REPLACED HIGH STAGE VALVE AND LOW PRESSURE SWITCH IAW EMB 145 XR AMM 36-11-02 & 30-11-11, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. SWITCH P/N APS7-1000, S/N 730-2-255.

Part: APU — CONTAMINATED · airframe 6,831 hrs · 3,666 cycles

TYS LAV SMOKE OCCURRED DURING CLIMBOUT IN THE LAV. CREW CHECKED LAV AREA, MESSAGE CLEARED AND RETURNED TO BLOCK. MAINTENANCE FOUND VERY HEAVY DEICING FLUID RUNNING DOWN THE APU INLET. MAINTENANCE RAN THE BLEEDS AND ENGINE BLEEDS. PERFORMED LAV SMOKE CHECKS AND OPS CHECKS GOOD. NO FURTHER MESSAGES, RELEASED BACK TO SERVICE IAW EMB 145XR AMM26-14-00.

Part: HOSE — BROKEN (E&E BAY) · airframe 6,767 hrs · 3,624 cycles

FLT 54 - MCI TO MCI - FLIGHT CREW REPORTED ADC 2 FAIL AND F/O ALT RED X'S. MX PERSONNEL REMOVED AND REPLACED THE TOTAL PRESSURE HOSE ON THE RIGHT ADC, OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,095 hrs · 2,742 cycles

SCHEDULE MX - 3A CHECK - ONT - RWD 724858 - DURING A/C PRELIM INSPECTION QC INSPECTOR FOUND EMERGENCY LIGHTS ON EXIT SIGNS AROUND SERVICE DOOR NOT OPERATING PROPERLY. MX PERSONAL PERFORMED GROUND FUNCIONAL CHECK OF SERVICE DOOR EMERGENCY LIGHT GOOD. A/C WAS APPROVED TO RETURN FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,095 hrs · 2,742 cycles

SCHEDULED MX - 3A CHECK - ONT - DURING PRELIM INSPECTION QC INSPECTOR FOUND EMERGENCY LIGHTS ON EXIT SIGNS AROUND OVERWING EXIT INOPERATIVE. MX PERSONAL PERFORMED GROUND FUNCTIONAL CHECK OF OVERWING EMERGENCY LIGHTS GOOD. A/C WAS APPROVED TO RETURN FOR SERVICE.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 4,217 hrs · 2,260 cycles

SDF - SMOKE IN THE COCKPIT. PERFORMED ENGINE RUNS AND BLEED CHECK, COULD NOT DUPLICATE PROBLEM AT THIS TIME.