N14174

Part: BUTTON — STUCK (ZONE 200) · airframe 42,184 hrs · 29,659 cycles

UNABLE TO OPEN EMERGENCY GEAR PANEL 222EF BY NORMAL MEANS. SUSPECT CLOSURE LATCH BUTTON STUCK. CLEANED DEBRIS AROUND DOOR AND LUBRICATED. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 41,812 hrs · 29,301 cycles

COCKPIT EMERGENCY LIGHT OUT. REMOVED AND REPLACED LAMP. OPS CHECK SAT

Part: BATTERY PACK — DISCONNECTED (ZONE 200) · airframe 41,364 hrs · 28,885 cycles

FOUND 6 EMERGENCY LIGHTS INOPERATIVE. SUSPECT BATTERY PACK #3. FOUND #3 BATTERY PACK DISCONNECTED. INSTALLED BATTERY. OPS CHECK SAT.

Part: INVERTER — INOPERATIVE (ZONE 200) · airframe 41,257 hrs · 28,788 cycles

AFT OVERWING EMERGENCY EXIT CEILING LIGHT INOPERATIVE. SWAPPED BATTERY NUMBER 3. OPS CHECK FAILED. REINSTALLED ORIGINAL BATTERY. REMOVED AND REPLACED #4 INVERTER. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,353 hrs · 27,928 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,231 hrs · 27,814 cycles

MAIN CABIN DOOR NOT CLOSING PROPERLY. FOUND AFT MICRO-SWITCH TO BE GETTING CAUGHT AND NOT FULLY RELEASING, PREVENTING THE FULL CLOSURE OF THE MCD. FOUND INTERNAL DOOR HANDLE ROTATED CLOCKWISE AND INTERNAL HANDLE BOLT, WASHER, AND NUT MISSING. REINSTALLED HANDLE TO CORRECT POSITION AND REPLACED BOLT, WASHER, AND NUT. OPS CHECK SAT. NO OTHER FAULTS FOUND AT THIS TIME.

Part: CONTROL UNIT — INOPERATIVE (UNKNOWN) · airframe 39,465 hrs · 27,100 cycles

STRONG FUEL SMELL THROUGHOUT CABIN AND FLIGHT DECK ON GROUND AND IN AIR. REMOVED AND REPLACED APU FUEL CONTROL UNIT. OPS CHECK SAT ALSO PACK 1 AND 2 RUNNING NO FUEL SMELL NOTED.

Part: STOP — INOPERATIVE (UNKNOWN) · airframe 39,459 hrs · 27,093 cycles

MAIN CABIN DOOR STUCK IN CLOSED POSITION. REMOVED AND REPLACED DOOR STOPPER ASSEMBLY. OPS CHECK SAT. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 38,858 hrs · 26,543 cycles

FUEL SMELL IN CABIN. LEAK FOUND AT LEFT WING INBOARD AFT LOWER CORNER. LEAK CHECK GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (HYD QTY) · airframe 38,798 hrs · 26,490 cycles

E1 HYD LO QTY IN FLIGHT. FOUND HYD SYSTEM #2 AT MAX CAPACITY. GVI OF HYD BAYS, NO LEAKS NOTED. TRANSFERRED FLUID FROM SYS 2 TO 1, RAN BOTH ENGINES. NO LEAKS NOTED AND NO INDICATION OF AIR IN SYSTEM. SERVICED BOTH HYD SYSTEMS. TAXI, STEERING AND BRAKE SYSTEM CHECKS GOOD. NO LEAKS NOTED. OPS CHECK GOOD.

Part: DOUBLER — CORRODED (FRM 68-70) · airframe 38,567 hrs · 26,285 cycles

AT REAR FUSE 1 EXT, RADIO ALT ANTENNA NO 2 AFT LOWER DOUBLER CORRODED ON BELLY SKIN BTW FR 68-70. SKIN IS REPAIRED WITH A DOUBLER

Part: SHEAR TIE — CRACKED (FRM 712 S6-10L) · airframe 38,567 hrs · 26,285 cycles

RF 1 , FRAME 71, SHEAR CLIP BTWN STR 6L-10L CRACKED. SHEAR CAP FR 71 BTW STR 6L-10L REMOVED FOR REPLACEMENT. NEW SHEAR FABRICATED. SHEAR CLIP FR 71 BTW STR 6L-10L REPROTECTED. FR 71 BTW STR 6L-10L, NEW SHEAR CLIP INSTALLED.

Part: SKIN — GOUGED (PAX DOOR) · airframe 38,567 hrs · 26,285 cycles

GOUGE ON PAX DOOR EXTERNAL SKIN AFT EDGE LOWER AREA. REPAIR DOUBLER ON PAX DOOR EXTERNAL SKIN, ON AFT EDGE AND AT STR 14L

Part: SKIN — CORRODED · airframe 38,566 hrs · 26,285 cycles

RH PYLON, FUSELAGE SKIN WORN BY FRETTING FROM LANYARD BETWEEN FR67 AND FR68 AND STGR 07R. REPAIR DOUBLER ON RH REAR FUSE 1 SKIN, BTW FR 67-68 AND BTW STR 7R-8R

Part: FRAME — CORRODED · airframe 38,566 hrs · 26,285 cycles

FRAME 25 FOUND CRACKED BTW STR 15R-16R. FRAME IS REPAIRED WITH AN EXTENDED SPLICE REPAIR ON RH CENTER FUSE 2 FRAME 25, BTW STR 15R-16R

Part: BULKHEAD — NONE · airframe 38,566 hrs · 26,285 cycles

EXISTING REPAIR DOUBLER ON FWD PRESSURE BULKHEAD NEED TO BE REMOVED FOR INVESTIGATION. BULKHEAD REPAIRED WITH A DOUBLER

Part: BEAM — CRACKED · airframe 38,566 hrs · 26,285 cycles

CF2 U/FLOOR STRUCTURE LH OMEGA BEAM #3 BTW FR 29-36 CRACKS SUSPECTED AT FRAME 33-34-35. 3 REPAIR DOUBLERS ON LH CENTER FUSE 2 OMEGA BEAM, ON INBD FLANGE AT FR 33, 34, 35

Part: BEAM — CRACKED · airframe 38,566 hrs · 26,285 cycles

CF1, UNDERFLOOR, LH OMEGA BEAM CRACK SUSPECTED AT FRAME 21, 22, 23. 3 REPAIR DOUBLERS ON LH CENTER FUSE 1 OMEGA BEAM, ON INBD FLANGE AT FR 21, 22 AND 23

Part: BEAM — CRACKED · airframe 38,566 hrs · 26,285 cycles

CF2, UNDERFLOOR, LH OMEGA BEAM #2 BTW FR 23-30 CRACK SUSPECTED AT FRAME 24, 25, 27, 28. 4 REPAIR DOUBLERS ON LH CENTER FUSE 2 OMEGA BEAM, ON INBD FLANGE AT FR 24, 25, 27, AND 28

Part: ANGLE — CRACKED (RT MLG WW) · airframe 38,567 hrs · 26,285 cycles

RH MLG WHEEL WELL, AFT WEB, UPPER ANGLE CRACKED. DAMAGED AREA REMOVED BY CUT OUT ON R/H MLG WHEEL WELL AFT WEB UPPER ANGLE AT STA X 16783.5. R/H MLG WHEEL WELL AFT WEB UPPER ANGLE REPAIRED WITH ANGLE DOUBLE AND INSTALLED WITH SOLID RIVET AND HI-LOCK.

Part: FRAME — CRACKED · airframe 38,567 hrs · 26,285 cycles

CF 4, FRAME 59 CRACKED BTWEN STR 15L-16L FRAME IS REPAIRED WITH AN EXTENDED SPLICE ON L/H CENTER FUSE 4 FRAME 59, BTW STR 15L-16L.

Part: FRAME — CRACKED · airframe 38,567 hrs · 26,285 cycles

RF 1 FRAME 72, SHARE CLIP BTWN STR 7L-10L CRACKED SHARE CAP FR 72 BTR STR 7L-10L FORMED FOR REPLACEMENT. NEW SHEAR CLIP FABRICATED. SHEAR CLIP FR 72 BTW STR 7L-10L SEPARATED . NEW SHEAR CLIP INSTALLED.

Part: NONE — NONE · airframe 38,080 hrs · 25,847 cycles

MID-CABIN AFT EMERGENCY CEILING LIGHT INOPERATIVE. RE-SECURED CONNECTIONS FOR MID-CABIN AFT EMERGENCY CEILING LIGHT. OPS CHECK SAT

Part: NONE — NONE · airframe 37,994 hrs · 25,769 cycles

DAMAGE TO LH LOWER COWLING ON THE FWD LEADING EDGE. BLENDED DAMAGE, INVESTIGATED DAMAGE - NO CRACKS NOTED. PERFORMED HFEC ON BLENDED AREA. NO CRACKS NOTED.

Part: LAMP — INOPERATIVE · airframe 37,685 hrs · 25,507 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECK SAT

Part: COMPUTER — INOPERATIVE (EPGWS) · airframe 36,527 hrs · 24,498 cycles

TERRAIN INOPERATIVE, WINDSHEAR INOPERATIVE, GPWS INOPERATIVE IN CRUISE. R&R EPGWS COMPUTER. OPS CHECK SAT.

Part: SEAT TRACK — CRACKED (CABIN) · airframe 36,276 hrs · 24,285 cycles

AISLE SIDE FRAME CRACKED ON SEATS 3A AND 22A. RR SINGLE SEATS ASSEMBLY ON ROWS 3A AND 22A. OPS CHECK SAT.

Part: ACM — SEIZED (NR 2) · airframe 35,865 hrs · 23,907 cycles

BURNING SMELL IN COCKPIT AND SMOKE IN THE AFT CABIN (ENGINE 2 WAS RUNNING PACK 2 ON BEING SUPPLIED BY APU AND PACK 1 OFF DEICING WAS NOW REQUIRED FOR FLIGHT). NR 2 ACM SEIZED. R & R ACM. OPERATIONS CHECK SATISFACTORY. NO SMOKE NOTED WHEN RUNNING PACKS.

Part: SUPPORT — DAMAGED (CARGO DOOR) · airframe 35,627 hrs · 23,681 cycles

BAGGAGE DOOR HARD TO OPEN. REMOVED BAGGAGE DOOR SPRINGS AND BELL CRANK ASSEMBLY. REMOVED DAMAGED SUPPORTS AND INSTALLED NEW SUPPORTS. REPLACED SPRINGS AND BELL CRANK ASSEMBLY AND APPLIED TENSION TO BELL CRANK. OPS CHECK GOOD. DURING INSTALLATION FOUND MINOR CHAFE ON ROLLER FAIRING, BLENDED WITHIN LIMITS, ALODINED AND PRIMERED AND TOP COATED. ON BAGGAGE DOOR BELL CRANK ASSEMBLY INSPECTED THE NEW SUPPORT, SPRINGS, BELL CRANK AND TENSION TO BELL CRANK. OPS CHECK GOOD. INSPECTED MINOR CHAFE ON ROLLER FAIRING, FOUND NO CRACK INDICATION. INSTALLED CARGO SIDE PANELS AND TRIM. PERFORMED PRESSURIZATION INSPECTION, LEAK CHECK GOOD.

Part: WIRE — DAMAGED (EXTERNAL LIGHT) · airframe 35,606 hrs · 23,661 cycles

EXTERNAL EMERGENCY LIGHT ON THE SERVICE DOOR INOPERATIVE. REPLACED EXTERNAL EMERGENCY LIGHT HOUSING ASSEMBLY ON THE SERVICE DOOR. INSTALLED NEW WIRE & CRIMPED SPLICE SP7376 & SOCKET FOR CONNECTOR P7198 C PORT. R & R CONNECTOR P7198 AND REPLACED WIRES FROM OLD SOCKET CONNECTOR TO A NEW ONE. OPS CHECK SATISFACTORY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,520 hrs · 23,571 cycles

SIDE-HINGED SERVICE DOOR EMERGENCY LIGHT BULB INOP. R/R SIDE-HINGED SERVICE DOOR EMERGENCY LIGHT ASSY. OPS CHECK SAT.

Part: ENGINE — POWER LOSS (NR 2) · airframe 34,855 hrs · 22,959 cycles

#2 ENGINE IN FLIGHT CLIMBING THROUGH 5000 FEET LOUD BANG FOLLOWED BY ENGINE POWER ROLLING BACK. REMOVED AND REPLACED #2 ENGINE. OPS AND LEAK CHECK SAT.

Part: GENERATOR — LEAKING (NR 2 ENGINE) · airframe 34,649 hrs · 22,779 cycles

OIL LEAK ENGINE #2. R&R #2 ENGINE DRIVEN GENERATOR. OPS CHECK SAT. LEAK CHECK SAT. NO DEFECTS NOTED.

Part: PLACARD — MISSING (EMERGENCY EXIT) · airframe 34,100 hrs · 22,241 cycles

RT EMERGENCY EXIT MISSING PLACARD. INSTALLED RT EMERGENCY DOOR PLACARD. NO DEFECTS NOTED.

Part: HOUSING — DAMAGED (LAV SERVICE) · corrosion level 2 · airframe 34,015 hrs · 22,161 cycles

OPEN HOLE TO OUTSIDE AT FORWARD SIDE OF LAV DUMP HOUSING. REMOVED AND REPLACED LAV DUMP HOUSING.

Part: DOUBLER — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 34,015 hrs · 22,161 cycles

LAV DUMP HOUSING DOUBLER HAS ELONGATED FASTENER HOLES. REMOVED AND REPLACED LAV DUMP HOUSING DOUBLER.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,015 hrs · 22,161 cycles

SHEAR CLIP FROM PREVIOUS REPAIR HAS CORROSION AS MARKED FR 63 STGR 20R-21R AS MARKED. REMOVED AND REPLACED SHEAR CLIP AT FR 62 STGR 20R-21R.

Part: SHEAR TIE — CRACKED (FUSELAGE) · corrosion level 2 · airframe 34,015 hrs · 22,161 cycles

CRACK IN SHEAR CLIP FR26 BETWEEN STR 15-16R. REMOVED AND REPLACED SHEAR CLIP FR26 BETWEEN STR 15-16R.

Part: DOOR FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 34,015 hrs · 22,161 cycles

CORROSION AROUND NUT PLATES BOTTOM FRAME OF PASSENGER DOOR AS MARKED. COMPLIED WITH ETD2019-145-083615 REV A FOR PERMANENT REMOVAL AND REPAIR OF CORROSION AROUND NUT PLATES ON THE BOTTOM FRAME OF PAX DOOR.

Part: BRACKET — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 34,015 hrs · 22,161 cycles

BAGGAGE DOOR FWD LATERAL L-SHAPE LWR BRACKET CORRODED AS MARKED. REMOVED AND REPLACED BAGGAGE DOOR FWD LATERAL L-SHAPE BRACKET AT FR65.

Part: HANDLE — MISINSTALLED (EMERGENCY EXIT) · airframe 33,358 hrs · 21,574 cycles

EMERGENCY EXIT HANDLE OVER 18A INSTALLED UPSIDE DOWN. INSTALLED EMERGENCY EXIT HANDLE IN NORMAL POSITION. NO OTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,044 hrs · 21,286 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. R&R SERVICE DOOR EMERGENCY LIGHT. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,649 hrs · 20,940 cycles

EMERGENCY LIGHT ON ROW 18 ON CD SIDE INOP. R&R EMERGENCY LIGHT IN ROW 18 ON CD SIDE. OPS CK SAT NO DEFECTS NOTED.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 28,843 hrs · 18,230 cycles

THE CREW REPORTED FO'S EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND OPERATIONAL CHECKS WERE GOOD

Part: DISPLAY — FAULTY (COCKPIT) · airframe 27,437 hrs · 17,166 cycles

THE CREW REPORTED PFD 1 BLACKED OUT AND CIRCUIT BREAKER POPPED. NOTED ELECTRICAL ODOR. MAINTENANCE INSPECTED AND REPLACED CAPTAINS PFD. OPS CHECKS WERE GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 60-61) · airframe 24,665 hrs · 15,273 cycles

CENTER OMEGA BEAM CORRODED BETWEEN FR 60-61. REPAIRED OMEGA BEAM IAW EC 5310-01473. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 24,665 hrs · 15,273 cycles

CARGO DOOR CUTOUT CENTER SILL HAS CORROSION. REPAIRED CARGO DOOR LOWER BEAM IAW SRM 51-40-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,413 hrs · 13,837 cycles

DURING ROUTINE MAINTENANCE, THE PASSENGER DOOR EMERGENCY EXIT IDENTIFIER SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 1 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: SKIN — DAMAGED (ZONE 200) · airframe 22,364 hrs · 13,805 cycles

DURING A LIGHTNING STRIKE INSPECTION, A PENCIL-TIP SIZED HOLE WAS FOUND BURNED IN THE FUSELAGE SKIN BETWEEN FRAMES 22 & 23 STRINGERS 5 & 6L. REPAIRED IAW SRM 53-21-01, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FRAME 77) · airframe 22,167 hrs · 13,682 cycles

DURING 4A INSPECTION, LEFT AFT FUSELAGE SKIN FOUND TO HAVE TWO CRACKS EMINATING FROM A RIVET ON FRAME 77 JUST ABOVE STRINGER 6L. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A FREEZE PLUG REPAIR IAW ETD2014-145-009276, AND ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLAPPER VALVE — LEAKING (LT WING FUEL) · airframe 21,968 hrs · 13,549 cycles

THE TOWER REPORTED A VAPOR TRAIL COMING FROM THE LT WING. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE LT OUTERMOST FLAPPER VALVE, OPERATIONALLY TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — DAMAGED (FLASHLIGHT ASSY) · airframe 19,398 hrs · 11,938 cycles

CREW REPORTED THE F/O'S FLASHLIGHT CRADLE TO NOT BE CHARGING THE FLASHLIGHT. REPAIRED THE F/O'S FLASHLIGHT ASSY WIRES WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,296 hrs · 11,878 cycles

DURING ROUTINE MX THE LT EMERGENCY EXIT ROW LOWER EMERGENCY LIGHT IDENTIFER WAS FOUND INOPERATIVE. MX REPLACED THE EMERGENCY EXIT ROW IDENTIFER SIGN. OPS CHECKED GOOD .

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,015 hrs · 11,698 cycles

DURING C-CHECK FRAME 50 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 18-19L. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01651. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · corrosion level 2 · airframe 19,015 hrs · 11,698 cycles

DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65-68 AND STRINGERS 15-16L. MX R & R THE LOWER BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 19,015 hrs · 11,698 cycles

DURING C-CHECK THE REINFORCEMENT SHEAR CLIP AT FRAME 65 (FWD CARGO DOOR FRAME) WAS FOUND TO BE CORRODED AT STRINGER 17L. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01494, REV A. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,097 hrs · 10,412 cycles

DURING ROUTINE MX THE FORWARD EMERGENCY LIGHTS FOUND INOPERATIVE. MX REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (NR 1 ENGINE) · airframe 14,941 hrs · 9,110 cycles

TYS - A/C WAS OBSERVED IN RIC UPON SHUTDOWN TO BE SMOKING FROM THE NR 1 ENGINE AND PUDDLES OF OIL. A/C WAS INSPECTED FOR PURPOSES OF A FERRY FLIGHT TO TYS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW EMB 145XR AMM 7100-00-00. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED AFTER THE ENGINE RUNS, LEAK CHECKS WERE C/W.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 14,158 hrs · 8,661 cycles

FLIGHT 5956 DEN TO DRO - AC N14174 FLAP 45 OVERSPEED AT 161 KTS. FERRIED TO SHV FROM DRO FOR INSPECTION. QC PERFORMED MAXIMUM FLAP EXTENDED SPEED INSP CHECK IAW EMB-145XR AMM 5-50-07. NO DAMAGE FOUND. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 14,020 hrs · 8,534 cycles

THE LOWER LT FUSELAGE I & II SUSTAINED DAMAGE FROM A TUG DURING GROUND OPERATIONS. THE DAMAGE AFFECTED THREE SKIN PANELS AND SOME UNDERLYING STRUCTURAL ELEMENTS. THE DAMAGE IS LOCATED BETWEEN FRAMES 12A AND 22. REMOVED AND REPLACED LOWER SKIN FROM FRAMES 13-24 STR 19L -18R. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER AT FRM 12A-13 BETWEEN STR 18L-19L AND AT FRM 20 BETWEEN STR 21R-19L. RE-CONTOURED REMAINING DENT BETWEEN FRM 15-16 AND STR 18L-19L. FRAME 20 DAMAGED BETWEEN STR 21R-19L REPAIRED AND RE-INSTALLED LOWER SECTION OF FRAME. PERFORMED RVSM MAPPING. REPAIR C/W IAW EC5330-02378.

Part: TRIM SWITCH — FAULTY (COCKPIT) · airframe 13,833 hrs · 8,384 cycles

ORD FLT 5871 - THE CREW REPORTED A MAIN PITCH TRIM FAIL MESSAGE IN FLIGHT. THE AIRCRAFT DIVERTED INTO CAK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S PITCH TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD.

Part: SENSOR — FAILED (NR 3 BRAKE) · airframe 13,723 hrs · 8,297 cycles

ORD FLT 6055 THE CREW REPORTED A BRAKE OVERHEAT MESSAGE ON TAKEOFF. THE AIRCRAFT ABORTED TAKEOFF AND TAXIED BACK TO GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 BRAKE OVERTEMP SENSOR. OPERATIONAL CHECKS WERE GOOD.

Part: STOWAGE BOX — LEAKING (COCKPIT) · airframe 13,572 hrs · 8,163 cycles

DURING ROUTINE MAINTENANCE THE OXYGEN LEVEL WAS FOUND LOW. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER'S CREW MASK STOWAGE BOX. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 9,494 hrs · 5,057 cycles

FLT 0001 - AUS - FLIGHT CREW REPORTED LAV SMOKE DETECTION NO TEST. MX PERSONNEL REMOVED AND REPLACED LAV SMOKE DETECTOR. OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,360 hrs · 4,983 cycles

SHV - DURING C-CHECK THE LT OMEGA SHAPE (BEAM) WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145XR SRM 53-00-10 DETAIL A FIG 201. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — LOOSE (EMERGENCY LIGHTS) · airframe 9,300 hrs · 4,928 cycles

MAIN DOOR EMERGENCY LIGHT FLICKERS ON/OFF. RESECURED BULB IAW EMB 145XR AMM 33-50-06. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,300 hrs · 4,928 cycles

RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145 AMM 33-50-07, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 9,300 hrs · 4,928 cycles

OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: DUCT CLAMP — DEFECTIVE (BLEED AIR SYS) · airframe 7,049 hrs · 3,738 cycles

FLT 2726 - EWR - CREW REPORTED ENGINE NR 1 ITT OVERTEMPERATURE ON CLIMBOUT AT FLIGHT LEVEL 180. CREW PERFORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX INSPECTED AND FOUND BAD 9TH STAG BLEED DUCT CLAMP. CLAMP WAS REMOVED AND REPLACED. EWR MX PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO FLIGHT.

Part: ENGINE — MALFUNCTIONED (NR 1)

DURING FLIGHT AFTER ENGINE BLEEDS WERE SELECTED THE LAV SMOKE ALARM CAME ON ALONG WITH THE LAV SMOKE INDICATION ON THE EICAS. REMOVED AND REPLACED THE NR 1 ENGINE. AIRCRAFT RETURNED TO SERVICE.