N683AE

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,415 hrs · 42,965 cycles

F068535 CORROSION ON LH OTBD #2 FLOOR SILL. REMOVED AND REPLACED FLOOR SILL ON LH OTBD #2 FLOOR SILL IAW EMB145 SRM 51-40-02.

Part: SKIN — BUCKLED (ZONE 100) · airframe 45,415 hrs · 41,965 cycles

F069494 RH WHEEL WELL INTERNAL SKIN IS BUCKLED AT FR3. REPAIRED BUCKLED RH WHEEL WELL INTERNAL SKIN AT FR 3 IAW PIEDMONT EO1-53-25-0329 AND ETD2025-145-928107.

Part: CROSSBEAM — DAMAGED (ZONE 200) · airframe 45,415 hrs · 41,965 cycles

CROSSMEMBER AT FRAME 5 HAS ELONGATED FASTENER HOLES NEAR STGR 15R. REPAIRED CROSSMEMBER AT FR 5 ELONGATED FASTENER HOLES NEAR STR 15R IAW EO1-53-25-0326 AND ETD2025-145-927858.

Part: FRAME — DAMAGED (ZONE 100) · airframe 45,415 hrs · 41,965 cycles

FRAME 5 HAS ELONGATED FASTENER HOLES NEAR STGR 15R. REPAIRED FR 5 ELONGATED FASTENER HOLES NEAR STR 15R IAW EO1-53-25-0330 AND ETD2025-145-927849.

Part: FRAME — DAMAGED (ZONE 200) · airframe 45,415 hrs · 41,965 cycles

FRAME 4 IS DAMAGED AT STGR 15R. REPAIRED FR 4 DAMAGE AT STR 15R IAW PIEDMONT EO1-53-25-0327 AND ETD2025-145-927854.

Part: FRAME — DAMAGED (ZONE 100) · airframe 45,415 hrs · 41,965 cycles

FRAME 3 BETWEEN STR 14R AND 17R IS DENTED AND BENT AT SKIN ATTACHMENT FLANGE. RAR FR3 BETWEEN STGR 11R-19R IAW EMB 145 SRM 51-40-02

Part: STRINGER — DAMAGED (ZONE 200) · airframe 45,415 hrs · 41,965 cycles

STRINGER 14R HAS AN OVERSIZED HOLE AT FR2. RAR STRINGER 14R BTW FR 1A-6 IAW EMB 145 SRM 51-40-02. DURING REPLACEMENT FOUND 13 HOLES BETWEEN FR 2-3 TO ONLY HAVE 1.5D EDGE DISTANCE. 13 HOLES ARE ACCEPTED AS A PERMANENT REPAIR IAW ETD2025-145-928801 AND EO1-53-25-0345.

Part: SHEAR TIE — DAMAGED (ZONE 100) · airframe 45,415 hrs · 41,965 cycles

FRAME 3 BETWEEN STR 14R AND 17R IS DENTED AND BENT AT SKIN ATTACHMENT FLANGE. RAR FR3 BETWEEN STGR 11R-19R IAW EMB 145 SRM 51-40-02

Part: FRAME — DAMAGED (ZONE 100) · airframe 45,415 hrs · 41,965 cycles

FRAME 4 IS DAMAGED AT STGR 15R. REPAIRED FR 4 DAMAGE AT STR 15R IAW EO1-53-25-0327 AND ETD2025-145--927854.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,415 hrs · 42,965 cycles

F068625 GALLEY FLOOR SUPPORT BRACKET AT FR-23 AND STGR-16 HAS CORROSION. RAR GALLEY FLOOR SUPPORT BRACKET AT FR-23 AND R/H STGR 16 IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,415 hrs · 42,965 cycles

F068549 CORROSION ON RH CROSS FLOORBOARD SUPPORT AT FRAME 28. R & R RH CROSS FLOORBOARD SUPPORT AT FRAME 28 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · corrosion level 2 · airframe 45,415 hrs · 42,965 cycles

F068523 CABIN CENTER OMEGA BEAM GUSSET BETWEEN FR-39/42 HAVE CORROSION. REMOVED AND REPLACED CABIN CENTER OMEGA BEAM GUSSET BTW FR 39-42 (NO.4) IAW EMB 145 SRM 51-40-02

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,415 hrs · 41,965 cycles

F068508 CORROSION ON LH #3 FLOOR BEAM GUSSET. REMOVED AND REPLACED LH #3 FLOOR BEAM GUSSET IAW EMB 145 SRM 51-40-02

Part: SHEAR TIE — CRACKED (ZONE 100) · airframe 45,415 hrs · 41,965 cycles

F068552 SHEAR CLIP IS CRACKED AT FRAME 26 BETWEEN STRINGERS 16R-17R. REMOVED AND REPLACED SHEAR CLIP AT FRAME 26 BETWEEN STRINGERS 16R-17R IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,415 hrs · 41,965 cycles

F068510 CABIN L/H OMEGA BEAM GUSSET BETWEEN FR-35/38 HAVE CORROSION. REMOVED AND REPLACED CABIN L/H OMEGA BEAM GUSSET #4 IAW EMB 145 SRM 51-40-02

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 45,415 hrs · 42,965 cycles

F068545 CABIN L/H OMEGA BEAM GUSSET BETWEEN FR-51/53 HAVE CORROSION. REMOVED AND REPLACED L/H OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02.

Part: SKIN — DAMAGED (ZONE 200) · airframe 45,415 hrs · 41,965 cycles

F068464 FWD FUSELAGE I SKIN PANEL FROM FR 1A-3 STR 14R TO THE NLG CUTOUT REQUIRES REPLACEMENT DUE TO MULTIPLE TOOL MARKS. REMOVED MULTIPLE TOOLING MARKED FWD FUSELAGE I SKIN PANEL FROM FR 1A-3 STR 14R TO THE NLG CUTOUT, PREPPED AND INSTALLED SERVICEABLE SKIN PANEL FROM FR 1A-3 STR 14R TO THE NLG CUTOUT IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (ZONE 100) · airframe 45,415 hrs · 41,965 cycles

F066756 REAR FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT FR 77 BETWEEN STGR 6R / 7R. ACCOMPLISHED BUSHING REPAIR ON REAR FUSELAGE EXTERNAL SKIN AT FR 77 BETWEEN STGR 6R /7R IAW EO1-53-25-0351 AND EMB-145 SRM 53-32-01 RE, ITEM 9, FIGURE 213, SHEETS 1-3.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,292 hrs · 39,451 cycles

AUTO FAIL WITH AUTO TRIM FAIL. OPS CHECK AUTOPILOT AND AUTO PILOT TRIM IAW 22-11-00. OPS CHECK GOOD CLEAR MEL 22-1-1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,362 hrs · 38,380 cycles

PACK 2 OVERHEAT DISPLAYED ON EICAS DURING TAKE OFF, AIR COND PACK N650 AND ABOVE AMENDED. R & R PACK 2 OVERTEMP SWITCH, TEMP SENSOR, AND CONDENSOR MIXER. RAN ENGINES AT POWER WITH BLEEDS AND PACKS ON. NO PACK 2 OVHT MESSAGE DISPLAYED AT THIS TIME. R/R #2 PACK VALVE IAW AMM 21-51-01-000/400-801-A. PERFORMED OPS CHECK AT HIGH POWER IAW AMM TASK 21-51-00-700-801-A. NO OVERHEAT MESSAGE SHOWN AT THIS TIME.

Part: UNKNOWN — UNKNOWN · airframe 40,985 hrs · 37,965 cycles

VERTICAL STABILIZER LH AND RH SPHERICAL BEARING HOUSINGS ARE OUT OF DIMENSIONAL TOLERANCE. REPAIRED IAW EO1-55-23-0044

Part: UNKNOWN — UNKNOWN · airframe 40,985 hrs · 37,965 cycles

COCKPIT LH LATERAL BRACKET, LH OF OVERHEAD PANEL, BETWEEN FR 12 AND 13 CRACKED. REPAIRED IAW 145 SRM51-40-02

Part: NONE — NONE · airframe 40,985 hrs · 37,965 cycles

PILOT'S BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED. REPAIRED IAW EO1-53-23-0046

Part: UNKNOWN — UNKNOWN · airframe 40,985 hrs · 37,965 cycles

AFT UPPER L/H SIDE OF FUSELAGE FR78 HAS ONE (1) FASTNER WITH POSSIBLE CRACKED SKIN. REPAIRED IAW EO1-53-23-0042

Part: UNKNOWN — UNKNOWN · airframe 40,985 hrs · 37,965 cycles

RH FWD VERTICAL STAB TO FUSELAGE ANGLE HAS POSSIBLE CRACK AT MARKED LOCATIONS. REPAIRED IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LH WING TIP UPPER ATTACHMENT FLANGE IS SCRATCHED. REPAIRED IAW EMB145 SRM 51-10-03 AND 57-20-07AD

Part: UNKNOWN — UNKNOWN · airframe 40,985 hrs · 37,965 cycles

AFT UPPER L/H SIDE OF FUSELAGE FR78 HAS ONE (1) FASTNER WITH POSSIBLE CRACKED SKIN. REPAIRED IAW EO1-53-23-0042

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

FRAME 65 IS CHAFED BETWEEN STRINGERS 2L-3L. REPAIRED IAW ETD 2023-145-004197

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSION ON CARGO DOOR SILL. REPAIRED IAW SRM 51-40-02, 51-20-03, AND 51-40-06

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSION ON CROSS BEAM BRACKET BETWEEN LH FLOOR GUSSET AND LH FLOOR SIL IN LAV AREA BETWEEN FRAMES 60-61. REPAIRED IAW EMB145 SRM 51-20-03 AND 51-40-02.

Part: NONE — NONE · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSOIN IN LAV FLOOR GUSSET BETWEEN FRAMES59-61. REPAIRED IAW EMB145 SRM 51-10-03, 53-24-10AD, 51-40-02, AND 51-20-03.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSION IN LAV FLOOR GUSSET BETWEEN FRAMES 59-61. REPAIRED IAW EMB145 SRM 51-10-03, 51-40-02, 51-20-03, AND 53-24-10AD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSION IN GALLEY FLOOR LH CROSSBEAM AT FRAME 18. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-01, AND 51-21-06.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSION ON SPLICE BRACKET ON LH FLOOR SILL IN LAV BETWEEN FRAMES 60-61. REPAIRED IAW EMB145 SRM 51-20-03, AND 51-40-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSION ON LH #3 FLOOR SILL. REPAIRED IAW EMB145 SRM 51-40-02, 51-20-03, AND 51-40-09

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSOIN ON INTERNAL FUSELAGE REINFORCEMENT SKIN PLATE BETWEEN FRAMES 61-62 STRINGERS 20L-21L. REPAIRED IAW EMB145 SRM 51-40-02 AND SB145-53-0068 FIG 7 DETAIL A2

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 40,985 hrs · 37,965 cycles

LEVEL 2 CORROSION ON INTERNAL FUSELAGE SKIN PLATE BETWEEN FRAMES 62-63 STRINGERS 20L-21L. REPAIRED IAW EMB145 SRM 51-40-02 AND SB145-53-0068

Part: CLAMP — LOOSE (NR 1 HEAT EXCH) · airframe 40,827 hrs · 37,793 cycles

ON DESENT, ACFT THROUGH RAIN & TURBULENCE. A SUDDEN ELECTRICAL ODOR IN FLT DECK & GALLEY FOR APPROX 5 MINS. ODOR DISSIPATED ON ITS OWN WITHOUT CREW INPUT. AT GATE UNDER APU POWER NO ODOR NOTED. PERFORMED GVI UNDER INSTRUMENT PANEL IN COCKPIT, INSP CIRCUIT BREAKERS & OPS LIGHTS (INTERIOR). NO DEFECTS NOTED. OPS CHECK WITH CREW OF ANTI-ICE SYS IAW AMM 30-00-00. NO DEFECTS. PERFORMED GVI & OPS CHECK OF BOTH PACKS. NOTED NR 1 PACK MAKES LOUDER WHINING NOISE. FOUND NR 1 HEAT EXCHANGER EXHAUST DUCT SLEEVE CLAMP LOOSE. SECURED THE CLAMP. OPS CHECKED GOOD.

Part: LOCALIZER — FAULTED · airframe 40,596 hrs · 37,523 cycles

BOTH LOCALIZER SIGNALS UNRELIABLE ON APPROACH TO FWA. DIVERTED TO DAY. PERFORMED VOR/ILS SYSTEM OPERATIONAL TEST IAW AMM 34-32-00-700-801-A. VOR/ILS SYSTEMS #1 AND #2 OPERATIONAL TESTS PASSED. AIRCRAFT OK FOR SERVICE

Part: NONE — NONE · airframe 39,922 hrs · 36,761 cycles

PDIS 683 28-41 2646932 22JUN22 CLT CLOSE AFTER TAKE OFF #1 FUEL QTY READ 0 AND TOTAL FUEL QTY READ 0 FACT 22JUN22 18:39 CLT UPON ARRIVAL TO A/C FOUND FUEL QTY TO BE OPERATING NORMALLY. AS POSITIVE MX R&R FUEL CONDITIONING UNIT IN REF WITH AMM 28-41-01. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE

Part: CONTROL UNIT — FAULTED (TE FLAPS) · airframe 38,772 hrs · 35,446 cycles

FLAP FAILURE ON APPROACH, FLAP FAIL STUCK ON 14 DEGREES. R+R FLAP ELECTRONIC CONTROL UNIT IAW AMM 27-53-02-000/400-801-A. OPS CHECK GOOD OK FOR SERVICE.

Part: INDICATOR — FAULTED (FUEL QTY) · airframe 37,946 hrs · 34,513 cycles

PDIS 683 28-41 2407312 21MAY21 GSP CLOSE ON DECENT FUEL 1 QTY DISPLAYED 0LBS. 10 MINUTES LATER FUEL QTY 2 DISPLAYED 0LBS. BOTH INDICATIONS CAME BACK AFTER 1 MINUTE. FACT 21MAY21 23:09 GSP PERF ELEC FUEL QTY IND OPS CHECK IN REF TO AMM 28 4100. OPS CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE

Part: UNKNOWN — ODOR (COCKPIT/CABIN) · airframe 37,549 hrs · 34,091 cycles

PDIS 683 21-01 2532571 08MAR21 FLO ASSGN PACK 2 OVERHEAT WITH BURNING SMELL IN COCKPIT AND TR OUBLE COOLING A/C. BURNING SMELL ALSO NOTICED WITH O NLY PACK 1 RUNNING (NOTE: CREW STATED IT TAKES RUN NING 3 MINS BEFORE SMELL OCCURRED AND HAPPEN WHILE DURING A/I TEST WITH N2 WAS ABOVE 83%) 31347 00 RS PERFORMED OPS CHECK ON PACK SYSTEMS #1 AND #2 IAW AMM 21-51-00-700-802-A. OPS CHECK GOOD. PLANE COOLS AS NORMAL. NO BURNING SMELLS DETECTED. NO OTHER DEFECTS NOTED

Part: UNKNOWN — ODOR (CABIN) · airframe 37,452 hrs · 33,971 cycles

PDIS 683 21-01 2343301 10FEB21 SDF CLOSE ON TAKEOFF AT APPROX 115KTS BURNING SMELL NOTICED IN FLIGHT DECK, FOLLOWED BY ICE COND A/ICE INOP MSG ON EICAS. FACT 10FEB21 20:17 SDF RAN AIRCRAFT WITH CREW, NO DEFECTS OR BURNING SMELL NOTED. PERFORMED ANTI ICING VALVE OPS CK IAW EMB AMM 30-00-00-700-803-A NO DEFECTS NOTED. FOUND DUCT 2 TEMP SENSOR FAIL MESSAGE ON CMC. AS A PERCAUTION SEE SEQ 3 OF LP 234330 FOR MEL OF #2 PACK.

Part: SWITCH — MALFUNCTIONED (A/C PACK) · airframe 37,298 hrs · 33,800 cycles

AFTER T/O SMOKE SMELL IN COCKPIT. SHORTLY AFTER PACK 1 OVERHEAT MESSAGE ON EICAS. PACK 1 SHUTDOWN AUTOMATICALLY AND SMELL DISAPPATED W/I 3-4 SECONDS. CW FIM TASK 21 51 00 810 803 A BLOCKS 1 AND 2. RAN WITH APU AND ENGINE NO EICAS MESSAGE/TRANSITORY COND. R & R OT SWITCH, IAW AMM 21 51 09 400 AS A PRECAUTION. NO SMELL IN COCKPIT OR CABIN NOTED. OK FOR SERVICE. CLEAR MEL.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER SYSTEM) · airframe 37,203 hrs · 33,714 cycles

PDIS 683 27-21 2302681 05DEC20 ALB CLOSE. ON CLIMB OUT RUD 1-2 FAIL EICAS MESSAGE PRESENTED. PERFORMED QRH RUD SYSTEM 1 CAME BACK ONLINE. FACT 05DEC20 12:34 ALB. FOLLOWED EMB 145 FIM 27-22-00-810-804 A TO BLOCK 19 FOUND TO BE TRANSITORY CONDITION OF THE RUDDER ELECTRICAL CIRCUIT. R & R RUDDER SYSTEM 2 PRESS SWITCH, IAW EMB 145 AMM 27-23-04 FOR PRECAUTIONARY MEASURES. OPERATIONS/LEAK CHECK GOOD.

Part: SENSOR — FAILED (TE FLAP) · airframe 36,867 hrs · 33,317 cycles

FLAP FAIL EICAS MESSAGE ON ARRIVAL TO HTS WHEN FLAPS SELECTED TO 9 DEGREES WITH NO FLAP MOVEMENT. R&R'D L/H FLAP VELOCITY SENSOR IAW AMM 27-51-12. RAN FLAPS UP AND DOWN A COUPLE TIMES OPS CHECK GOOD AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,832 hrs · 33,274 cycles

FLAP FAIL ON EICAS WHEN FLAPS SELECTED DOWN. TROUBLESHOT IAW FIM TASK 27-51-00-810-816-A, STEPS 1,2,3, OPS CHECK IAW 27-51-00-700-801-A. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 36,852 hrs · 33,296 cycles

ON APPROACH, SELECTED FLAPS TO 9, FLAP FAIL MSG INSTANTLY APPEARED ON EICAS. PERFORMED FLAP RESET AND FLAP CONTROL SYSTEM OPS CHECK MULTIPLE TIMES. OPS CHECK GOOD AND NO DEFECTS NOTED IAW AMM 27-31-00. OK FOR SERVICE AT THIS TIME.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,832 hrs · 33,274 cycles

DENT IN EXTERIOR FUSELAGE SKIN ON FR 67 BETWEEN STRINGERS 13R AND 14R...PERFORMED CUTOUT AS REQUIRED AND FABRICATED AND INSTALLED DOUBLER AND FILLER FOR REPAIR OF FUSELAGE EXTERNAL SKIN AT FR 67 BETWEEN STGR 13R AND 14R IAW EMB-145 SRM 53-31-01 RE ITEM 4 AND PIEDMONT EO1-53-20-0185.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 36,832 hrs · 33,274 cycles

SSI 53-30-48 SHEAR CLIP AT FRAME 68 BY CARGO DOOR SILL IS CORRODED...REPAIR ACCOMPLISHED IAW EMB 145 SRM 53-31-04 ITEM 4 FIGURE 212 AND PIEDMONT EO1-53-20-0171.FR 68 SHEAR CLIP PN: 145-25369-003.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 36,832 hrs · 33,274 cycles

SSI 53-30-48 SHEAR CLIP AT FRAME 65 BY CARGO DOOR SILL IS CORRODED...REMOVED AND INSTALLED NEW SECTION OF SHEAR CLIP AT FRAME 65 IAW EMB 145 SRM 53-- 31-04 EO1-53-20-0160

Part: RIB — CRACKED (RT WING) · airframe 36,832 hrs · 33,274 cycles

RH WING RIB 21 IS CRACKED...ACCOMPLISHED WITH REPAIR AT RH WING RIB 21 IAW EMB 145 SRM 57-20-07.

Part: WEB — GOUGED (CARGO DOOR) · airframe 36,832 hrs · 33,274 cycles

CARGO DOOR WEBBING IS GOUGED AT PREVIOUS REPAIR...INSTALLED SERVICEABLE REPAIR DOUBLER IAW EMB 145 SRM 52-30-01, ITEM 12, FIG. 213.

Part: RIB — CRACKED (LT WING) · airframe 36,832 hrs · 33,274 cycles

LH WING RIB 21 IS CRACKED......ACCOMPLISHED REPAIR ON L/H WING RIB 21 IAW EMB 145 SRM 57-20-07.

Part: SKIN — CRACKED (FUSELAGE) · airframe 36,832 hrs · 33,274 cycles

RH FR. 75 AREA HAS A SKIN CRACK ABOVE STR., 2R MARKED, SETTINGS: FREQ. 400KHZ, ANGLE: 291.1 DEG., H-61.3DB., V-77.6DB., FILTER: LO-PASS 500HZ., PROBE: 100-500KHZ....ACCOMPLISHED REPAIR OF FUSELAGE SKIN AT FR 75 STGR 2R IAW EMB 145 SRM 53-31-01 AND EO1-53-20-0157

Part: WARNING MESSAGE — FALSE ACTIVATION (STAB ANTI-ICE) · airframe 36,307 hrs · 32,675 cycles

STAB ANTI-ICE FAIL MESSAGE DISPLAYED....FIX:FOLLOWED FIM TASK 30-12-00-810-805-A.CHECKED CMC MESSAGE, HAD A/ICE LOW PRESSURE DISPLAYED.PER FIM OPS CHECKED A/ICE SYS IAW AMM 30-00-00/500 WITH OPS CHECK GOOD. DETERMINED TO BE TRANSITORY.

Part: TUBE — BROKEN (CONTROL VALVE) · airframe 35,493 hrs · 31,717 cycles

WING ANTI-ICE FAIL IN FLIGHT,CREW RAN QRH,MSG PERSISTED. DOWNLOADED CMC WITH MFD AND FOUND WING A/ICE LEAK MSG, REMOVED PANEL 191 FR AND FOUND Y DUCT BETWEEN PACK VALVE AND DUAL TEMP CONTROL VLV, P/N 145-2-27547-409 BROKEN, R & R TUBE ASSY AS REQUIRED,OPS CHECK GOOD IAW EMB 145 AMM 30-00-00, REINSTALLED PANEL,OK FOR SERVICE

Part: WIRE — BROKEN (CABIN) · airframe 35,424 hrs · 31,640 cycles

NDIS 683 33-51 0011610 26MAY19 RIC CLOSE SERVICE DOOR EMERGENCY LIGHT ON HONGE INOP FACT 26MAY19 11:23 RIC FOUND #2 BATT SUPPLY FAULTY AND GROUND WIRE BROKEN AFTER SPLICE SP7377. R/R #2 BATT SUPPLY IAW AMM TASK 33-50-04-000/400-801-A. REPAIRED WIRE W716-0008-20 ION REF TO SWPM 20-21-00 P/N ON BATT SUPPLY 1330408 S/N 15960 P/N OFF BATT SUPPLY 1330408 S/N 16118.

Part: TRACK — DIRTY (PAX DOOR) · airframe 35,014 hrs · 31,192 cycles

PDIS 683 52-10 1854172 20MAR19 PWM CLOSE MAIN PAX DOOR, UNABLE TO OPEN. HISTORY: NO FACT 20MAR19 21:26 PHL CLEANED AND LUBED PASSENGER DOOR TRACKS AND LATCHES AS REQUIRED. OPS CHECK GOOD. OKAY FOR SERVICE.

Part: CONNECTOR — SHORTED (SPOILER SYS) · airframe 34,953 hrs · 31,122 cycles

PDIS 683 27-60 1854021 06MAR19 PHL CLOSE CLIMBING THROUGH 18000FT SPOILER FAIL AND THEN NOTICED C/B F-22 WAS POPPED. SPOILER INDICATION WAS OPEN. HISTORY: YES FACT 06MAR19 04:08 PHL MX INSP FOUND RT OB SPOILER PLUG 1166 SHORTED TO GROUND AT PIN A RT IB SPOILER PLUG 1167 HAD CORRODED & SEIZED PIN A + BOTH LT IB+OB PROX SWITCH PLUGS P1166+P1167 SHOWED SIGNS OF PLUG DEGREDATION R&R ALL PROX SWITCHES LT IB+OB-RH IB+OB IAW AMM 27-63-04 R&R ALL CONNECTORS LT P1166-P1167&RT P1166&P1167 REF SWPM 20-50-00 OPS CK NO CD POP OK FOR SERVICE.

Part: DUCT — RUPTURED (WING ANTI ICE) · airframe 34,405 hrs · 30,500 cycles

PDIS 683 30-14 1692911 16NOV18 MDT CLOSE WING A/ICE FAIL MESSAGE DURING FLIGHT AFTER TWO A/I TESTS. FACT 16NOV18 18:41 MDT AFTER INVESTIGATION OF NEARBY DUCTS, FOUND R/H PACKEXHAUST DUCT RUPTURED CAUSING THE WING ANTIICE FAIL MESSAGE FROM WING ANTI ICE THERMOSTATIC SENSOR READING HIGH PACK EXHAUST AIR TEMP. R&R'D R/H PACK EXHAUST DUCT IAW AMM 21-51-02 REF FIM 30-11-00-810-807-A OPS CHECK GOOD REF AMM 30-00-00 MDIS 683 30-14 1692912 16NOV18 MDT CLOSE FOUND R/H PACK EXHAUST DUCT RUPTURED. FACT 16NOV18 18:51 MDT REMOVED AND REPLACED R/H PACK EXHAUST DUCT IN REFERENCE WITH AMM 21-51-02

Part: WIRE — BROKEN (CABIN) · airframe 33,840 hrs · 28,834 cycles

EMERGENCY LIGHT ON SERVICE DOOR INOP. REPAIRED BROKE WIRE W716-0007-20 IN SERVICE DOOR LINER, IAW AMM 20-00-03.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 32,786 hrs · 28,682 cycles

DURING TAKE OFF ROLL AT ABOUT 80 KNOTS, IN ICE CONDITIONS, THE ANTI-ICE INOPERATIVE WARNING MESSAGE DISPLAYED. TROUBLESHOT IAW FIM 30-80-00-810-801-A, AND PERFORMED AN OPS TEST IAW 30-00-00-700-803A, ANTI-ICE VALVE TESTED. NO DEFECTS OR MESSAGES. OK FOR SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 32,650 hrs · 28,551 cycles

NDIS 683 33-51 0001790 11DEC17 RIC CLOSE SERVICE DOOR EMERGENCY LIGHT WONT ILLUMINATE 28805 00 SJU FACT 11DEC17 08:17 RIC FOUND BROKEN WIRES W716-0007-20 AND W716-0008-20 REP LACED WIRES IAW SWPM 20-21-00 OPS CHECK GOOD OK FOR SERVICE

Part: BUSHING — MIGRATED (LT AILERON) · airframe 32,473 hrs · 28,371 cycles

LEFT AILERON, OTBD PCA FITTING HAS A MIGRATING BUSHING. REMOVED AND REPLACED THE LEFT AILERON PCA FITTING IAW EO EM-27MR-112.

Part: DOOR SILL — DAMAGED (CARGO) · airframe 32,473 hrs · 28,371 cycles

AFTER CORROSION REMOVAL OF CARGO DOOR SILL, FOUND THE DOOR SILL TO HAVE A DEFECT INDICATION DURING NDI INSPECTION. INSTALLED A NEW DOOR SILL IAW SRM 51-40-02.

Part: BUSHING — MIGRATED (RT AILERON) · airframe 32,473 hrs · 28,371 cycles

RIGHT AILERON DAMPER FITTING ON AILERON HAS MIGRATING BUSHING. INSTALLED A SERVICEABLE AILERON IAW AMM 27-10-00.

Part: FITTING — DAMAGED (LT AILERON) · airframe 32,473 hrs · 28,371 cycles

LT AILERON DAMPER FITTING ON AILERON HAS MIGRATING HAT BUSHING. CHANGE DAMPER FITTING EO- EM-27MR-112.

Part: SUPPORT — CRACKED (NLG WW) · airframe 32,473 hrs · 28,371 cycles

AFT SUPPORT IN NOSE LANDING GEAR WHEEL WELL FOR UPLOCK BOX HAS A 1.5 INCH CRACK. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-02.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 32,473 hrs · 28,371 cycles

INBD AND OUTBD HINGE FITTINGS ON THE LEFT ELEVATOR SERVO TAB HAVE WORN HAT BUSHING BORES. REMOVED AND REPLACED THE FITTINGS IAW AMM 20-10-01.

Part: LIGHT — DAMAGED (CABIN) · airframe 32,473 hrs · 28,371 cycles

CABIN FLOOR EMERGENCY LIGHT STRIPS AT POSITIONS LT FORWARD MOST TRIM STRIP 1,3,4,5,7,8, AND RT 1,2, AND 8 ARE DAMAGED. REPLACED LIGHT STRIPS IAW AMM 33-50-12.

Part: WIRE SPLICE — FAILED (EMERGENCY LIGHT) · airframe 32,410 hrs · 28,299 cycles

AFT FLOOR EMERGENCY LIGHT INOPERATIVE. R & R THE EMERGENCY LIGHT SPLICE SP9213 IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 32,197 hrs · 28,085 cycles

DURING PS-1 CHECK, FOUND LAST EMERGENCY FLOOR PROXIMITY STRIP BY THE LAVATORY DOOR INOP. DEFERRED LAST EMERGENCY FLOOR PROXIMITY STRIP BY LAVATORY AS PER MEL 33-30. MTX PROCEDURES C/W. REPAIRED BROKEN AC SIDE CONNECTOR ON AFT EMERGENCY PROX STRIP IAW WM 20-21-00 PERFOMRED OPC EMERGENCY LIGHTING SYS IAW AMM 33-50-00-700-801-A NO FAULTS FOUND MEL RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,056 hrs · 27,954 cycles

MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT ASSY IAW AMM 25-23-04. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 31,639 hrs · 27,521 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN, OPEN DOOR IS CATCHING AND STICKING MID WAY. LUBRICATED AIRFRAME ROLLERS ON FWD MAIN CABIN DOOR IAW AMM 53-21-02. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 31,451 hrs · 27,394 cycles

F/A REPORTS AFT F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-51-01. CHECKED GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 29,993 hrs · 26,005 cycles

MAIN CABIN DOOR STICKS AND IS DIFICULT TO OPERATE. CLEANED AND LUBRICATED MAIN DOOR FRAME ROLLERS IAW EMB145 53-21-02 AMM OPS CHECK GOOD

Part: PUMP — FAILED (NR 1) · airframe 29,934 hrs · 25,960 cycles

DURING FLIGHT, RECIVED A HYD 1 LOW QTY ADVISORY ON THE EICAS. THE LOW QTY WAS CONFIRMED ON THE HYD PAGE OF THE MFD LATER RECEIVED AN E1 HYD PUMP FAIL ADVISORY ON EICAS AFTER PARKING. FOUND HYDRAULIC FLUID DRIPPING OUT OF NR 1 ENGINE COWLING. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYD PUMP IAW AMM 29-10-03 OPS AND LEAK CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 29,077 hrs · 25,189 cycles

CAPTAINS FLASHLIGHT INOPERATIVE. FLIGHT CREW PLACARDED CAPTAINS FLASHLIGHT INOPERATIVE, MEL 25-53. INSTALLED FLASHLIGHT IAW EMB 145 AMM 33-50-16. FLASHLIGHT OCK GOOD. MEL ITEM RESTORED.

Part: WIRE — BROKEN (CABIN) · airframe 28,589 hrs · 24,745 cycles

SERVICE DOOR EMER LIGHT IS INOPERATIVE. FOUND & REPAIRED BROKEN WIRE W716-0007-20 IN SERVICE DOOR HINGE AREA, BETWEEN SP7376 & PLUG P7198 IAW SWPM 20-21-00. SERVICE DOOR EMER LIGHT OPERATIONS TESTED OK IAW AMM 33-50-00.

Part: BLEED VALVE — FAILED (RT ENGINE) · airframe 28,351 hrs · 24,499 cycles

ABORTED TAKEOFF, MASTER WARNING BLEED 2 VLV FAIL. TRANSFERRED TO NRWC 683-MIA-02322. R & R RT ENG BLEED VLV. SEE REF NRWC 2770172 IAW AMM 36-11-05. PERFORMED OPERATIONAL TEST OF THE AIR BLEED SYS IAW 36-00-00-700-803-A.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,254 hrs · 24,415 cycles

FLASHLIGHT CRADLE BROKEN BEHIND CAPTAINS SEAT. R & R FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,255 hrs · 24,416 cycles

AFT FUSELAGE FRAME 75, SKIN CRACKED BETWEEN STRINGER 1L & 3L. REPAIRED FRAME 75 SKIN CRACK IAW ERS-EM-53MR-1747.

Part: FRAME — CORRODED (FUSELAGE) · airframe 28,255 hrs · 24,416 cycles

FRAME 65 AT FWD LOWER CARGO DOOR CUT OUT AREA IS CORRODED. REPAIRED FRAME 65 AT THE FWD LOWER CORNER OF THE CARGO DOOR CUT OUT AREA IAW SRM 53-31-04.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 28,255 hrs · 24,416 cycles

CARGO DOOR SILL CORRODED AT FRAME 65, 66 & 67, THREE AREAS MARKED. R & R CARGO DOOR SILL IAW SRM 51-40-02.

Part: SKIN — CHAFED (FUSELAGE) · airframe 28,231 hrs · 24,396 cycles

RIGHT FUSELAGE IS CHAFED INSIDE 424DB. REPAIRED RT FUSELAGE CHAFED INSIDE 424DB IAW ERS-EM-53MR-1729.

Part: FRAME — GOUGED (FUSELAGE) · airframe 28,231 hrs · 24,396 cycles

FRAME 65 GOUGED AT TOP, AROUND NUTPLATE HOLE. REPAIRED FRAME 65 GOUGED AT TOP, AROUND NUTPLATE HOLE IAW ERS-EM-53MR-1711.

Part: YOKE — CRACKED (LT PYLON) · airframe 28,231 hrs · 24,396 cycles

LEFT PYLON LOWER FWD YOKE IS CRACKED. REPAIRED LT PYLON LOWER FWD YOKE IAW EO EM-54MR-386.

Part: FRAME — CRACKED (FUSELAGE) · airframe 28,231 hrs · 24,396 cycles

CRACK AT RIVET ON FRAME 75, BETWEEN STRINGERS 2L-3L. REPAIRED AFT FUSELAGE FRAME 75, SKIN CRACKED ABOVE STRINGER 2L IAW ERS-EM-53MR-1747. SEE TASKS & WIPS FOR DETAILS.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 28,231 hrs · 24,396 cycles

GALLEY LT FLOORBEAM DIGITAL SUPPORT SPLICES, INBD & OTBD, CRACKED. R & R THE GALLEY LT FLOORBEAM DIGITAL SUPPORT SPLICES IAW SRM 51-40-02. SEE NRTC E475078 FOR TOPCOAT TOUCH UP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,231 hrs · 24,396 cycles

AFT FUSELAGE FRAME 75, SKIN CRACKED ABOVE STRINGER 2L. REPAIRED CRACKED IAW ERS-EM-53MR-1747. SEE TASKS & WIPS FOR DETAILS.

Part: FIREWALL — CRACKED (APU BAY) · airframe 28,231 hrs · 24,396 cycles

APU FIREWALL IS CRACKED AT RT OTBD RIVET ON UPPER CTR HORIZONTAL STIFFENER. PERFORMED REPAIR OF APU FIREWALL IAW SRM 53-32-13 & ETN-EM-53-244R2.

Part: CROSSMEMBER — CORRODED (FUSELAGE) · airframe 28,231 hrs · 24,396 cycles

GALLEY FLOOR CTR AISLE CROSS MEMBER CORRODED AT FRAME 20. R & R GALLEY FLOOR CTR AISLE CROSS MEMBER IAW SRM 51-40-02.

Part: GCU — INOPERATIVE (NR 2 ENGINE) · airframe 28,230 hrs · 24,395 cycles

GENERATORS 2 OFF BUSS, CAME ON ON EICAS AFTER SHUTTING DOWN ENG 1. DURING TAXI, RESET THE GEN BUTTON & AFTER FEW SECONDS IT COME BACK AGAIN, FOLLOWED BY ELECTRICAL ODOR. R & R NR 2 GCU IAW AMM 24-31-02. OPERATIONAL CHECKED GOOD.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 28,231 hrs · 24,396 cycles

CORROSION FOUND ON CARGO DOOR CUT OUT FRAME 65, ABOVE SILL. REPAIRED FRAME 65 AT THE FWD LOWER CORNER OF THE CARGO DOOR CUT OUT IAW SRM 53-31-04.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,890 hrs · 24,044 cycles

FLIGHT ATTENDANT REPORTED FLASHLIGHT HAS STOPPED CHARGING. IT WORKED FOR A WHILE BUT NOW IT HAS STOPPED CHARGING. R & R FLIGHT ATTENDANT FWD FLASHLIGHT ASSEMBLY AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 27,766 hrs · 23,915 cycles

FIRST OFFICERS FLASHLIGHT BROKEN. R & R FLASHLIGHT IAW SMP. OPERATIONS CHECKED GOOD.

Part: FAN — INOPERATIVE (CABIN) · airframe 27,759 hrs · 23,907 cycles

FLIGHT ATTENDANT REPORTED SMOKE FUMES IN CABINET BELOW CB PANEL IN GALLEY. PERFORMED GVI OF GALLEY AREA WITH NO DEFECTS NOTED. PERFORMED ENG ODOR EVENT IAW ETN-EM-72-034, NO DEFECTS NOTED. FOUND RECIRC FAN 2 INOPERATIVE, SEE LOG PAGE 3829649 ITEM 1. INSPECTED COFFEE POTS, GALLEY CB MODULE, EMER LIGHT BATTERY, LAV SMOKE DET PANEL, CD PLAYER & ALL LIGHTING & BALLAST IN GALLEY, NO ODOR NOTED. FUNCTIONAL TEST IS GOOD.

Part: GROUND WIRE — LOOSE (EXTERIOR LIGHT) · airframe 27,439 hrs · 23,638 cycles

SERVICE DOOR EXTERNAL EMER LIGHT INOPERATIVE. CLEANED & TORQUED GND CONNECTION WIRE ON SERVICE DOOR EXTERNAL EMER LIGHT ASSEMBLY IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 26,586 hrs · 22,863 cycles

COCKPIT EMER LIGHT INOPERATIVE. R & R COCKPIT EMER LIGHT BULB IAW AMM 33-50-05-000-801-A & 33-50-05-400-801-A. OPERATIONS CHECKED GOOD.

Part: WIRE — BROKEN (CABIN) · airframe 26,124 hrs · 22,474 cycles

DURING EMER LIGHT CHECK WORK CARD 33-700-17 ACCOMPLISHMENT FOUND SERVICE DOOR EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT LAMP IAW MM 30-50-10. LIGHT DID NOT ILLUMINATE DURING TEST. TROUBLE SHOT & FOUND BROKEN WIRE FROM CONNECTOR P7198 PIN D. REPAIRED WIRE IAW SPWM 20-21-00. LIGHT CHECKED GOOD IAW MM 33-50-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,080 hrs · 22,427 cycles

SERVICE DOOR FAIRING EMER LIGHT INOPERATIVE. R & R SERVICE DOOR EMER LIGHT LAMP IAW AMM 33-50-09-000-801-A & 33-50-09-400-801-A. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: TEAR STRAP — MECHANIC ERROR (FUSELAGE) · airframe 25,684 hrs · 22,100 cycles

HAIL DAMAGE EVENT. CTR FUSELAGE 1 TEAR STRAPS HOLE MISALIGNMENT. CUT OUT DAMAGED TEAR STRAPS & FABRICATED REPAIR PARTS IAW ERS-EM-53MR-694. TEAR STRAPS PN 145-20583-013.

Part: TEAR STRAP — MECHANIC ERROR (FUSELAGE) · airframe 25,684 hrs · 22,100 cycles

HAIL DAMAGE EVENT. CTR FUSELAGE 1 TEAR STRAPS HOLE MISALIGNMENT. CUT OUT DAMAGED TEAR STRAPS & FABRICATED REPAIR PARTS IAW ERS-EM-53MR-694. TEAR STRAP PN 145-20583-013.

Part: TEAR STRAP — MECHANIC ERROR (FUSELAGE) · airframe 25,684 hrs · 22,100 cycles

HAIL DAMAGE EVENT. CTR FUSELAGE 1 TEAR STRAPS HOLE MISALIGNMENT. CUT OUT DAMAGED TEAR STRAPS & FABRICATED REPAIR PARTS IAW ERS-EM-53MR-694.

Part: TEAR STRAP — MECHANIC ERROR (FUSELAGE) · airframe 25,684 hrs · 22,100 cycles

HAIL DAMAGE EVENT. CTR FUSELAGE 1 TEAR STRAPS HOLE MISALIGNMENT. CUT OUT DAMAGED TEAR STRAPS & FABRICATED REPAIR PARTS IAW ERS-EM-53MR-694. TEAR STRAP PN 145-20583-011.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

SHEAR CLIP AT FRAME 21 CRACKED AT STRINGER 10L. CUT OUT EFFECTED AREA & FABRICATED STRAP. PERFORMED REPAIR IAW ERS-EM-53MR-692.

Part: STRINGER — MECHANIC ERROR (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

MISS DRILLED HOLE ON STRINGER 4R BETWEEN FRAME 58 & 59. REPAIRED IAW ERS-EM-53MR-606.

Part: TEAR STRAP — DAMAGED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

TEAR STRAP DAMAGED AT FRAME 56 - 58 AT RT BUTT STRAP. PERFORMED REPAIR IAW ERS-EM-53MR-607. STRAP PN 145-29074-001.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R LT ELEVATOR TIP INBD SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R FWD FUSELAGE II SKIN IAW SRM 51-40-02 & ETN-EM-53-206.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGED EVENT. R & R CTR FUSELAGE II LT SKIN IAW SRM 51-40-02 & ETN EM-53-263.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R LT ELEVATOR ROOT SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R LT ELEVATOR TIP LE SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R RT ELEVATOR LE SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R FWD FUSELAGE II SKIN IAW SRM 51-40-02 & ETN EM-53-206.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. REPLACE CTR FUSELAGE II SKIN PANEL. R & R CTR FUSELAGE II SKIN IAW SRM 51-40-02 & ETN-EM-53-263.

Part: SKIN — DAMAGED (RT HORIZ STAB) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R RT STAB TOP SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R LT ELEVATOR LE SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R CTR FUSELAGE I RT SKIN IAW SRM 51-40-02 & ETN EM-53-262 R1.

Part: SKIN — DENTED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R FWD FUSELAGE I LT SKIN IAW SRM 51-40-02 & ETN-EM-53-206.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. REPLACE RT ELEVATOR TIP UPPER INBD SKIN. R & R RT ELEVATOR TIP UPPER INBD SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R RT ELEVATOR ROOT SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R RT ELEVATOR TIP LE SKIN IAW SRM 51-40-02, ETN EM-55-073 & ERS-EM-5500-137.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R REAR FUSELAGE I SKIN IAW SRM 51-40-02 & ERS-EM-5300-615.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. REPLACE REAR FUSELAGE SKIN PANEL. R & R REAR FUSELAGE I SKIN IAW SRM 51-40-02 & ERS EM-5300-615.

Part: SKIN — DAMAGED (LT HORIZ STAB) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R LT STAB TOP SKIN IAW SRM 51-40-02 & ETN EM-55-073.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 25,683 hrs · 22,099 cycles

HAIL DAMAGE EVENT. R & R CTR FUSELAGE IV TOP SKIN IAW SRM 51-40-02, 51-20-01 & ETN EM-53-265.

Part: LIGHT — INOPERATIVE (PAX DOOR) · airframe 25,683 hrs · 22,099 cycles

PAX DOOR EMER LIGHT IS INOPERATIVE. CORRECTION ACTION COMPLETE. PAX DOOR EMER LIGHT OPERATIONS CHECKED GOOD IAW 33-50-00.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,678 hrs · 22,095 cycles

LEFT OVERWING EMER LIGHT INOPERATIVE. R & R LT OVERWING EMER LIGHT LAMP IAW AMM 33-50-07-000-801-A & 33-50-07-400-801-A. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 25,553 hrs · 21,992 cycles

LEFT AFT OVERWING EMER LIGHT INOPERATIVE. R & R LT AFT OVERWING EMER LIGHT BULB IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,539 hrs · 21,978 cycles

RIGHT EXTERIOR OVERWING EMER LAMP INOPERATIVE. R & R RT EXTERNAL OVERWING EMER LIGHT BULB IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A OPERATIONS CHECKED GOOD.

Part: SEAL — FAILED (WINDSHIELD) · airframe 25,190 hrs · 21,615 cycles

CAPTAIN`S WINDSHIELD HUMP SEAL APPROXIMATELY 8 INCHES TOP RT CAME LOOSE IN FLIGHT & FINALLY BROKE OUT. REPAIRED SEAL IAW AMM 56-10-01. ITEM 2. NO OTHER DEFECTS NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,857 hrs · 21,333 cycles

AFT EMERGENCY FLASHLIGHT INOPERATIVE. R & R AFT EMERGENCY FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,546 hrs · 21,089 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE, BOTTOM. R & R LAMP ON SERVICE DOOR EMERGENCY LIGHT IAW AMM 33-50-10.

Part: BEAM — CORRODED (CARGO DOORWAY) · airframe 23,915 hrs · 20,594 cycles

DURING MBV INSPECTION, FOUND CARGO DOOR UPPER SILL CORRODED. ACFT WAS REMOVED FROM SERVICE FOR MBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW EO EM-53MR-2220R1. AIRCRAFT WILL BE RETURNED TO SERVICE AFTER MBV INSPECTION, MATERIAL USED 7475-T761, .080.

Part: LIGHT — DAMAGED (CABIN) · airframe 23,916 hrs · 20,594 cycles

NR 1, 3, & 4 EMERGENCY LIGHTS DAMAGED. R & R EMERGENCY LIGHTS IAW AMM 33-50-12.

Part: UNKNOWN — ODOR (CABIN/COCKPIT) · airframe 23,884 hrs · 20,567 cycles

ELECTRICAL FUMES ENTERED COCKPIT, CABIN, AND CARGO, AREA. APPLIED FULL ELECTRICAL LOAD IN DIFFERENT CONFIGURATIONS AND PERFORMED GVI OF COCKPIT,CABIN AND CARGO FOR ELECTTRICAL ODOR. UNABLE TO FIND ANY DISCREPANCY AFTER 3 HRS, CONTINUED FAULT. NO ELECTRICAL ISSUES NOTED.

Part: FLASHLIGHT — CRACKED · airframe 22,984 hrs · 19,843 cycles

DURING MX INSP, FOUND THE AFT EMERGENCY FLASHLIGHT HAS CRACKED TOP CAP. THE ACFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED AFT EMERGENCY FLASHLIGHT IAW AMM 33-50-16. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,860 hrs · 19,736 cycles

DURING B INSP, FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING OF SERVICE DOOR EXTERAL EMERGENCY LIGHT, FOUND BROKEN WIRE. PERFORMED REPAIR IAW WM 20-21-00. THE OPS CHECK WAS GOOD AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: CLAMP — UNDERTORQUED (BLEED AIR SYS) · airframe 20,454 hrs · 17,725 cycles

ON FLIGHT 3308 THE CREW REPORTED THAT THEY RECEIVED AN ENGINE 2 BLEEDC LEAK MESSAGE DURING CLIMBOUT. ELECTED TO RETURN TO CVG AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. REMOVED PANELS FOR ENTIRE BLEED 2 SYSTEM. TROUBLESHOT SYSTEM AND FOUND PRECOOLER V-BAND CLAMP UNDER TORQUED AND UPPER PORTION OF DUCT (P/N 816619-1) HAD BLOWN OFF OF NR 2 PACK. TORQUED PRECOOLER CLAMP AS NEEDED AND REMOVED AND REPLACED PACK FLEXIBLE DUCT COUPLER AND CLAMP. RAN SYSTEM. FOUND LEAK CHECK TO BE GOOD. INSTALLED ALL PANELS FOR BLEED 2 SYSTEM. RAN AIRCRAFT AND OPS CHECKED BLEED 2 SYSTEM FOR SEVERAL MINS AT TAKEOFF POWER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 20,347 hrs · 17,654 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD FLIGHT ATTENDANT’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT IAW AMM33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,143 hrs · 17,482 cycles

DURING B INSPECTIONS, FOUND THE RIGHT FORWARD FUSELAGE EXTERNAL EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,940 hrs · 17,321 cycles

DURING B-INSPECTION FOUND THE FORWARD RIGHT EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD RIGHT EXTERNAL LIGHT LAMP IAW EMB 145 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 19,792 hrs · 17,221 cycles

DURING MAINTENANCE INSPECTION FOUND THE PROXIMITY EMERGENCY FLOOR LIGHT BROKEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD IAW AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,937 hrs · 16,591 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. THE OPERATIONAL CHECK OF THE LEFT OVER WING EMERGENCY LIGHT WAS GOOD IAW EMB-145-AMM-33-50-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 18,702 hrs · 16,420 cycles

DURING MAINTENANCE INSPECTION FOUND THE OBSERVER SEAT LIFE VEST BAG TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OBSERVER SEAT LIFE VEST IAW EMB 145 EEL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,702 hrs · 16,420 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT WING AFT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT WING AFT OVERWING EMERGENCY EXIT LIGHT IAW EMB 145 AMM 33-50-10 SUBTASK 33-50-10-020-003-A00 FOR REMOVAL AND SUBTASK 33-50-10-420-003-A00 FOR INSTALL. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — BROKEN (DIFIBRILLATOR) · airframe 18,673 hrs · 16,398 cycles

FOR FLIGHT 2821 THE FLIGHT ATTENDANT REPORTED THE SEAL ON DIFIBRILLATOR WAS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW SEAL ON DIFIBRILLATOR AS REQUIRED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,336 hrs · 15,391 cycles

ON FLIGHT 4268 ON APPROACH THE CREW REPORTED A STRONG ODOR COMING FROM PACK 1. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED EMB145 FIM 21-20-00 GROUND RAN A/C IAW RRMM 72-00-00 COULD NOT DUPLICATE. THE OPERATIONAL TEST WAS GOOD. C/W ETN EM-72-034-R4. NO ODOR NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MALFUNCTIONED (CABIN) · airframe 16,825 hrs · 15,012 cycles

ON FLIGHT 4373 THE CREW REPORTED A BURNING ODOR IN THE COCKPIT DURING TAKEOFF. THE ODOR WENT AWAY DURING THE CLIMB. THE CREW MADE THE DECISION TO CONTINUE TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FLASHLIGHT ASSEMBLY ABOVE FLIGHT ATTENDANTS JUMP SEAT IAW EMB-145 M/M 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 16,512 hrs · 14,773 cycles

SUPPLEMENTAL INFORMATION: ON FLIGHT 2918 DEPARTING DFW ON CLIMBOUT THE AIRCRAFT RECEIVED A STRONG LIGHTNING STRIKE. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO DFW WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAINS PRIMARY FLIGHT DISPLAY P/N 7014300901 S/N 01059205. REMOVED AND REPLACED THE FIRST OFFICER’S PRIMARY FLIGHT DISPLAY P/N 7014300901 S/N 0401D124. REMOVED AND REPLACED THE CAPTAIN’S MULTI-FUNCTION DISPLAY P/N 7014300901 S/N 98124081. REMOVED AND REPLACED THE FIRST OFFICER’S MULTI-FUNCTION DISPLAY P/N 7014300901 S/N 00056569. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOUSING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,328 hrs · 13,101 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LAVATORY EXTERNAL BUCKET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. FABRICATED REPAIR DOUBLER, LOCATED AND DRILLED FASTENER HOLES, COUNTERSUNK HOLES, ALODINED AND PRIMED REPAIR DOUBLER IAW EMB SRM 53-31-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DAU — FAILED (NR 1) · airframe 14,046 hrs · 12,882 cycles

ON FLIGHT 3950 THE CREW REPORTED 115 VAC BUS CYCLED ON THE EICAS 2 TIMES ON TAKEOFF AND AIRBORNE AND 3 TIMES ON APPROACH. THERE WAS A DATA ACQUISITION UNIT 1 FAIL MESSAGE ON EICAS 4 TIMES IN FLIGHT. EICAS WENT TO DASHES. THE BACKUP SHOWED MISCOMP. EACH TIME CYCLED OFF FOR A MATTER OF SECONDS. ALSO, LOST INDICATIONS FOR LANDING GEAR, FLAPS, AND SPOILERS. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CREW ELECTED TO RETURN TO ORD AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NUMBER 1 DATA ACQUISITION UNIT, IAW EMB 145 AMM 31-41-01. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,798 hrs · 9,937 cycles

ON FLIGHT CREW REPORTED ON POST FLIGHT, FLIGHT ATTENDANT FOUND ROW 1-7 FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. ***AWAITING FOLLOW UP***

Part: BRAKE — CRACKED (MLG)

ON WALK AROUND AFTER A PS-1 INSPECTOR NOTED THAT THE NUMBER ONE TIRE WAS WORN TO LIMITS. DURING REMOVAL OF TIRE MAINTENANCE NOTED THAT THE NUMBER 1 BRAKE BROKE APART DURING REMOVAL. REPLACED THE NUMBER ONE BRAKE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (A)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,364 hrs · 8,525 cycles

DURING A IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 29 WAS FOUND CORRODED. REPAIRED CORRODED AREA, REPAIR IAW SRM 53-00-10 FIG 202. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUELAGE) · airframe 9,364 hrs · 8,525 cycles

DURING A IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 29 WAS FOUND CORRODED. REPAIRED CORRODED AREA REPAIR IAW SRM 53-00-10 FIG 202. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (SERVICE DOORWAY) · airframe 9,364 hrs · 8,525 cycles

DURING A IMBV INSPECTION, THE SERVICE DOOR CUT OUT LOWER CENTER SILL WAS FOUND CORRODED. BLENDED CORRODED AREAS TREATED AND NDT. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,364 hrs · 8,525 cycles

DURING A IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED CORRODED AREA REPAIR IAW SRM 53-00-10 FIG 201. AIRCRAFT RETURNED TO SERVICE.

Part: PROFILE — CRACKED (CARGO DOORWAY) · airframe 9,364 hrs · 8,525 cycles

DURING A IMBV INSPECTION, THE CARGO FWD EDGE PROFILE LOWER CORNER WAS FOUND CRACKED. REMOVED PROFILE REPLACED WITH NEW PART IAW SRM 51-40-02, 51-40-04. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 9,364 hrs · 8,525 cycles

DURING A IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND CORRODED. REMOVED SILL REPLACED WITH NEW PART IAW SRM 51-40-02, 51-40-04, AND 51-40-06. AIRCRAFT RETURNED TO SERVICE.

Part: NONE — NONE (NONE)

FLIGHT CREW REPORTED SEVERE TURBULENCE ON FLIGHT FROM RST. FLIGHT LANDED AT ORD WITHOUT INCIDENT. COMPLIED WITH SEVERE TURBULENCE INSPECTION IAW AE WC 05=200-03, NO DAMAGE FOUND. AIRCRAFT RETURNED TO SERVICE. (M)