N641AE

Part: FUEL — LEAKING (ZONE 600)

SEVERE TURBULENCE ON APPROACH. C/W SEVERE TURBULANCE INSPECTION IAW AMM 05-50-27. DURNING SEVERE TURBELANCE INSPECTION FOUND FUEL SEEPAGE ON RT WING,RIB 9,CREV 1 AND MULTIPLE SCREWS ON LWR LEADING EDGE. INSPECTED INTERNAL FUEL TANK RH LEADING EDGE AT RIB7. INSPECTED FUEL SEEP BY TH WING,RIB 9 SPAR 1 IRT AMM 28-11-00-700-801-A CLASSIFIED AS A TYPE III AREA AND STAIN

Part: WINDSHIELD — NO DISCREPANCY (ZONE 200) · airframe 55,388 hrs · 53,040 cycles

BIRDSTRIKE TO CAPTAIN`S WINDSHIELD. COMPLIED WITH BIRDSTRIKE INSPECTION IRW AMM 05-50-08 CLEANED WIND SCREEN AS REQUIRED. ACFT OKAY FOR SERVICE AT THIS TIME.

Part: RELAY — FAILED (TAT) · airframe 55,158 hrs · 52,763 cycles

ON TAKE OFF ROLL TAT 2 HEAT INOP, E1-2 IDLE STOP FAIL AND NO TAKE OFF CONFIG MSGS DISPLAYED ON EICAS. NO AURAL MSG DENOTED WITH NO TAKE OFF CONFIG MSG. TAT 2 HEAT INOP AND E 1-2 IDLE STOP FAIL MSGS INTERMITTENT ON TAXI BACK TO GATE. FACT 10AUG25 04:02 PHL R/R RELAY K0212 ASREQUIRED. NO FIX FURTHER T/S REQUIRED. R/R TAT CURRENT SENSOR IRW AMM 30-33-01 HIGH POWER RUN UP AND TAXI PERFORMED WITH NO DEFECTS OR INTERMITTENT DEFECTS NOTED. A/C OK FOR SERVICE.

Part: ENGINE — MAKING METAL (NR 2) · airframe 54,192 hrs · 51,697 cycles

E-2 ENGINE SHUT DOWN DURING CLIMB OUT AT ABOUT 5300' EICAS E-2 OUT DISPLAYED. (CAPT SAID OIL QTY STILL FULL AND NO ABNORMAL NOISES HEARD.) FACT 24FEB25 15:08 RDU REMOVED AND REPLACED #200 ENGINE IAW W/C 71-00-00. OPS AND LEAK CHECK GOOD.

Part: PRESSURE SWITCH — FAILED (RUDDER) · airframe 54,025 hrs · 51,518 cycles

RUDDER SYSTEM 1 INOP MESSAGE DISPLAYED DURING TAKE OFF ROLL. FACT 17JAN25 21:34 CAE R&R'D RUDDER SYS 1 PRESSURE SWITCH IAW AMM 27-23-04. OPS & LEAK CHECK GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 53,930 hrs · 51,409 cycles

ON DESCENT FROM FL230 FA REPORTED ELECTRICAL FUMES. CREW OBSERVED FUMES IN COCKPIT. FUMES CLEARED AFTER 3 MINS. (NO EICAS MSGS OR DEFECTS NOTED WITH A/C SYSTEMS) FACT 27DEC24 19:15 JAN: PERFORMED GVI FOR LIGHTNING STRIKE, NO DAMAGE NOTED. INSPECTED CABIN LIGHTING, NO DEFECTS NOTED. OPERATED BOTH PACKS FOR 15MINS, NO SMELLS OBSERVED. AIRCRAFT OK FOR SERVICE AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN) · airframe 52,682 hrs · 50,009 cycles

UNUSUAL ODOR NOTICED IN FLT DECK AFTER LANDING TRANSITIONING TO TAXIWAY. FACT 17MAY24 14:26 CLT INSP COCKPIT FWD AVIONICS BAY BATTERY COMPT RAN APU BLD WITH PACKS ON. UNABLE TO DUPLECATE ODOR SUSPECT ODOR FROM #1 TIRE AND BRAKE RECENTLY REPLACED NO DEFECTS FOUND AT THIS TIME OK FOR SERVICE

Part: BLEED VALVE — WARNING MESSAGE (NR 1 ENGINE) · airframe 52,338 hrs · 49,607 cycles

BLEED 1 VLV CLOSED EICAS MESSAGE DISPLAYED FOR APROX 20 MINS. SELF CLEARED AND DID NOT REAPPEAR. R&R E1 BLEED VALVE. NO FIX. DONE IAW AMM 36-11-05. R&R BLEED 1 PUSH BUTTON IAW AMM 20-13-04-04. OPS CHECK GOOD. A/C OK FOR SERVICE

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 52,235 hrs · 49,497 cycles

BAG SMOKE EICAS MESSAGE DISPLAYED WITH BAGGEXTG BUTTON ILLUMINATED IN FLT. BAG BAY SHOWS NO SIGN OF FIRE. EXTG BUTTON WAS PUSHED. MEL 21FEB24 11:27 SDF C05205 26-8 BAGGAGE COMPARTMENT FIRE EXTINGUISHER. FACT 21FEB24 18:15 PHL R+R BOTH BAGGAGE HIGH RATE AND METERING BOTTLES IAW AMM 26-23-01. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME. CLEAR MEL 26-8. MDIS 641 26-15 3048091 22FEB24 PHL CLOSE PREF LP 304808-1. PER MOCC INSPECT FORE AND AFT BAGGAGE SMOKE DETECTORS FOR OBVIOUS DEFECTS/DAMAGE. REPAIR.REPLACE AS NEEDED FACT 22FEB24 16:14 PHL INSPECTED BOTH SMOKE DETECTORS, NO OBVIOUS DEFECTS NOTED. REMOVED AND REPLACED AFT SMOKE DETECTOR AS A MAINTENANCE PRECAUTION IN REF TO AMM 26-15-01, OPS CHECK GOOD IN REF TO AMM 26-15-00. AIRCRAFT OK FOR SERVICE.

Part: PUMP — FAILED (NR 2 HYD SYS) · airframe 52,180 hrs · 49,439 cycles

HYD SYS #2 LOW QTY FOLLOWED BY HYD SYS #2 FAIL. R&R #2 ENGINE DRIVEN HYD PUMP IAW AMM 29-10-03 HYD SYS #2 REQUIRES AIR BLEED OPS AND LEAK CHECK PERFORMED LEAK CHECK OPS CHECK LEAK CHECK OPS CHECK GOOD.

Part: TRUNNION — CRACKED (RT MLG) · airframe 52,166 hrs · 49,427 cycles

E016631 RH MLG AFT UPPER TRUNION CRACKED OUTBD AREA. REMOVED AND REPLACED RH MLG AFT UPPER TRUNION IAW AERNNOVA TI-145-14-018 RH, ETD2024-145-001082, AND EO1-57-24-0029.

Part: DOUBLER — IMPROPER PART (LT ELEVATOR) · airframe 52,166 hrs · 49,427 cycles

E016433 NO REPAIR INFO FOUND FOR LH ELEVATOR SERVO TAB FAIL SAFE ROD CUTOUT LE UPPER SKIN DOUBLER. REACCOMPLISHED REPAIR OF THE LH ELEVATOR SERVO TAB FAIL SAFE ROD CUTOUT LEADING EDGE UPPER SKIN IAW EMB ETD2024-145-000771 AND EO1-55-24-0027.

Part: DOUBLER — IMPROPER PART (LT ELEVATOR) · airframe 52,166 hrs · 49,427 cycles

E016434 : NO REPAIR INFO FOUND FOR LH ELEVATOR SERVO TAB FAIL SAFE ROD CUTOUT LE LOWER SKIN DOUBLER. REACCOMPLISHED REPAIR OF THE LH ELEVATOR SERVO TAB FAIL SAFE ROD CUTOUT LEADING EDGE LOWER SKIN IAW EMB145 SRM 55-20-01-RE, ITEM 3, FIGURE 230 AND EO1-55-24-0028

Part: SEAT TRACK — CORRODED (FRM 46) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016403 LH UPPER SEAT TRACK SUPPORT CORRODED AT FR 46. : ACCOMPLISHED REPAIR ON LH UPPER SEAT TRACK SUPPORT AT FR 46 IAW EMB 145 SRM 53-00-11, ITEM 5 REPAIR TYPE C.FIGURE 207 AND PIEDMONT EO1-05-024-0055.

Part: UNKNOWN — CORRODED (UNKNOWN) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016291 FWD DIGITAL HAS CORROSION AROUND NUTPLATE HOLE AT L/H OUTBD EDGE. FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED DOUBLER ON THE FWD DIGITAL AROUND NUTPLATE LH OUTBD EDGE IAW EMB SRM 51-40-02, ETD2024-145-000476 AND PIEDMONT EO1-05-24-0055.

Part: UNKNOWN — CORRODED (UNKNOWN) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016292 FWD DIGITAL HAS CORROSION AROUND NUTPLATE HOLE JUST AFT OF L/H DISTRO BOX. FABRICATED REPAIR DOUBLER, INSTALLED REPAIR DOUBLER IAW EMB 145 SRM 51-40-02, ETD2024-145-000474 AND PIEDMONT EO1-05-24-0055.

Part: UNKNOWN — CORRODED (FRAME 18) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016288 AFT DIGITAL HAS CORROSION AROUND NUTPLATE HOLE AT FR18 JUST INBD OF SEAT TRACK. PERFORMED CUTOUT, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED REPAIR DOUBLER AND FILLER IAW ETD2024-145-00479 AND PIEDMONT MINOR EO1-05-24-0055.

Part: SEAT TRACK — CORRODED (NR 1) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016008 RH UPPER #1 SEAT TRACK HAS SOME CORROSION. REMOVED AND REPLACED RH UPPER # 1 SEAT TRACK IAW EMB 145 AMM 53-01-- 06.

Part: SEAT TRACK — CORRODED (FRM 37) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016018 L/H LOWER SEAT TRACK SUPPORT IS CORRODED BETWEEN FR 37. REMOVED AND REPLACED LH LOWER SEAT TRACK SUPPORT BETWEEN FR 37 IAW EMB 145 SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FRM 28) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016017 RH FLOOR CROSS BEAM AT FRAME 28 CORRODED. RAR RH FLOOR CROSS BEAM AT FRAME 28 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FRMS 32-35) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016030 R/H LOWER SEAT TRACK SUPPORT IS CORRODED BETWEEN FR. 32-35. RAR R/H LOWER SEAT TRACK SUPPORT BETWEEN FR. 32-35 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016033 R/H #1 CABIN FLOOR SILL IS CORRODED. REMOVED AND REPLACED RH #1 CABIN FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: SEAT TRACK — CORRODED (NR 2) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016077 RH #2 OTBD SEAT TRACK HAVE SOME CORROSION. REMOVED AND REPLACED RH #2 OTBD SEAT TRACK IAW EMB 170 AMM 53-01-06.

Part: SEAT TRACK — CORRODED (NR 5) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016059 LH #5 UPPER SEAT TRACK CORRODED AROUND SCREWS. RAR LH #5 OTBD SEAT TRACK IAW EMB 145 AMM 53-01-06. EASI #7414

Part: SEAT TRACK — CORRODED (FRMS 32-35) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016029 L/H LOWER SEAT TRACK SUPPORT IS CORRODED BETWEEN FR. 32-35. REMOVED AND REPLACED WITH SERVICEABLE L/H LOWER SEAT TRACK SUPPORT BETWEEN FR32-35 IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (NR 6) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E015961 CENTER OMEGA BEAM GUSSET #6 IS CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE CENTER OMEGA BEAM GUSSET #6 IAW EMB 145 SRM 51-40-02.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E016250 SERVICE DOOR CENTER SILL IS CORRODED. FABRICATED 2 EACH DOUBLER AND INSTALLED AND APPLIED HYSOL TO PRIMERED AREAS ON SERVICE DOOR CENTER SILL IAW EMB-145 SRM 53-21-02 RE, ITEM 2, FIGURE 201 AND EO1-53-24-0051

Part: FRAME — CRACKED (FRM 66 S18L) · airframe 52,166 hrs · 49,427 cycles

E015857 FR 66 CRACKED AT STR18L. : REMOVED AND REPLACED FR66 AT STR18L IAW EMB 145 SRM 51-40-02.

Part: FRAME — CRACKED (FRM 73 S16-17R) · airframe 52,166 hrs · 49,427 cycles

E015863 FR 73 CRACKED BETWEEN STRGS 17R-16R. DRILLED SERVICEABLE LOWER FRAME 73 SECTION ,AND FABRICATED AND DRILLED U” SHAPED SPLICED AND INSTALLED IAW EMB 145 SRM 53-00-04 RE ITEM 4 FIGURE 201 AND EO1-53-24-0032

Part: FLOOR SUPPORT — CORRODED (NR 6) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E015898 R/H #6 OTBD FLOOR SILL IS CORRODED. REMOVED AND REPLACED R/H #6 OTBD FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: DOOR FRAME — CORRODED (CARGO) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E015858 CARGO DOOR AIRFRAME CUTOUT LWR SILL CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE CARGO DOOR AIRFRAME CUTOUT LWR SILL IAW EMB145 SRM 51-40-02.

Part: GUSSET — CORRODED (NR 7) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E015901 L/H OMEGA BEAM GUSSET #7 IS CORRODED. REMOVED AND REPLACED L/H OMEGA BEAM GUSSET #7 IAW EMB 145 SRM 51-40-02.

Part: GUSSET — CORRODED (FRMS 60-61) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E015908 CENTER BEAM GUSSET IS CORRODED BETWEEN FRAMES 60-61. REMOVED CORRODED AND REPLACED WITH NEW, SERVICEABLE CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E015860 RH CARGO FLOOR SILL #3 CORRODED. RAR RH CARGO #3 FLOOR SILL IAW EMB 145 SRM 51-40-02

Part: GUSSET — CORRODED (FRMS 60-61) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E015909 R/H FLOOR BEAM GUSSET IS CORRODED BETWEEN FRAMES 60-61. RAR R/H FLOOR BEAM GUSSET BETWEEN FR 60-61 IAW EMB 145 SRM 51-40-02

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 52,166 hrs · 49,427 cycles

E015648 RH EMERGENCY ESCAPE HATCH LWR FRAME UNDER RUB STRIP HAS CORROSION. RAR R/H EMERGANCY ESCAPE HATCH LWR PROFILE IAW EMB 145 SRM 51-40-02.

Part: STRINGER SPLICE — CHAFED (FRM 52 S19R) · airframe 52,166 hrs · 49,427 cycles

E015296 STRINGER 19R PREVIOUS REPAIR IS CHAFED AT SKIN SPLICE AFT FRAME 52. FABRICATED AND DRILLED SHIMS, ALODINED AND PRIMED REPAIR PIECES AND INSTALLED REINFORCING ANGLE IAW EMB 145 SRM 53-24-02RE, FIGURE 201 AND EO1-53-24-0033

Part: DOUBLER — IMPROPER PART (FRM 73) · airframe 52,166 hrs · 49,427 cycles

E015153 FLUSH DOUBLER REPAIR AT FR 73 STGR 18L HAS NO DTI INFORMATION. REMOVED DOUBLER AND FILLER, FABRICATED SERVICEBLE DOUBLER AND FILLER AND INSTALLED REPAIR AT FR 73 AND STGR 18L IAW EMB 145 ETD2024-145-000911 AND EO1-53-24-0046.

Part: DOUBLER — IMPROPER PART (PAX DOOR) · airframe 52,166 hrs · 49,427 cycles

E015038 NO REPAIR INFO FOUND FOR EXT DOUBLER ON PAX DOOR AT FWD UPPER CORNER. RE-ACCOMPLISHED REPAIR AT THE PAX DOOR UPPER FWD CORNER IAW EMB ETD2024-145-001181 AND EO1-52-24-0031

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,161 hrs · 49,422 cycles

PRONOUNCED SMOKE ODOR DURING DESCENT. RAN BOTH PACKS WITH ENG AND APU BLEEDS AND OPERATED W/S HEATING SYSTEM, NO SMOKE SMELLS NOTED. INSPECTED BOTH PACKS FOR DEFECTS, SEE NEXT SEQ FOR DISCR. NO OTHER OBVIOUS DEFECTS NOTED. OK FOR SERVICE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,716 hrs · 48,907 cycles

PACK 2 OVERHEAT IN FLIGHT. MOMENTARY FUMES FROM PACK 1 IN FLIGHT. PACK 1 OVERHEAT DURING TAXI. FACT 31AUG23 23:37 BUF SEE THIS LP SEQ 2 FOR MEL OF PACK 1 AND 2 ASSGN BOTH PACK 1 AND 2 OVERHEAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,664 hrs · 48,850 cycles

BAG SMOKE INDICATION ON CLIMBOUT-FOLLOWED QRH WITH BLOWN FIRE BOTTLE. BAGGAGE COMPARTMENT FIRE EXTINGUISHER. FIRE DEPT INSPECTED BAG BAY AND NO SIGN OF FIRE OR SMOKE PRESENT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,341 hrs · 48,522 cycles

DURING CLIMBOUT BLEED 2 LEAK WARNING MESSAGE. CREW FOLLOWED QRH AND MESSAGE EXTINGUISHED. FACT 23JUN23 17:44 PHL R+R DUCT SLEEVE ON #2 PACK HEAT EXCHANGER IN REF TO AMM 21-51-02. AIR BLEED SYSTEM OPS CHECK GOOD IN REF TO AMM 36-00-00. OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,339 hrs · 48,519 cycles

SPS 2 INOP AND SPS ADVANCE DISPLAYED IN FLT FACT 22JUN23 13:03 CLT T/S IRT FIM 27-36-00-810-807-A STEPS 1-3 R/R STALL PROTECTION COMPUTER IAW AMM 27-36-02 OPS CHECK GOOD OK FOR SERVICE. AFTER PUSH BACK SPS2 INOP PRESENTED FOLLOWED BY SPS ADVANCED DFRL 22JUN23 20:01 CLT T/S IRT FIM TASK 27-36-00-810-802-A STEPS 1-4. T/S IRT FIM 27-36-00-810-807-A. SLAVED IN SPC, NO FIX. REINSTALLED ORIGINAL SPC. PERFORMED ELECTRICAL TEST ON FIM 27-36-00-810-807-A. ELECTRICAL TEST PASS. INSPECTED AND FOUND STALL PROTECT. PANEL BUTOUT 2PB STICKING. CORRECTIVE ACTION CONTINUED ON SEQ 3 FACT 22JUN23 20:03 CLT R+R STALL PROTECTION PANEL IAW AMM 27-36-05. PERFORMED STALL PROTECTION SYS OPS CHECK IAW AMM 27-36-00 MULTIPLE TIMES. OPS CHECK GOOD. COULD NOT DUPLICATE MESSAGES AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 50,938 hrs · 48,094 cycles

NO.2 HYD PRESSURE SPIKED TO 3200 PSI FOR A SHORT TIME IN FLIGHT FACT 11APR23 12:36 MDT REMOVED AND REPLACED NO.2 ENGINE HYD PUMP REF 29-10-03 LEAK AND OPS CHECK GOOD OK FOR SERVICE

Part: UNKNOWN — UNKNOWN · airframe 50,396 hrs · 47,338 cycles

TAT 2 HEAT INOP MSG DURING CRUISE AND REMAINED ON ENTIRE FLIGHT. FACT 11MAR23 16:09 R&R TAT CURRENT SENSOR K0494 IAW FIM 30-33-00-810-802-A. PERFORMED OPS CHECK IAW AMM 30-33-00. OPS CHECK GOOD. OK FOR SERVICE AT THIS TIME.

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 49,146 hrs · 46,162 cycles

AUTO MODE SELECTED CABIN ALT CLIMBED WOULD NOT REGULATE PRESSURIZATION. MANUAL MODE WAS NOT SELECTED. C/W TASK 21-31-03-040-800-A. ROA REACTIVATED EOV IAW AMM TASK 21-31-03-440-801-A. R/R'D PRESS DIGITAL CONTROLLER IAW AMM 21-31-01-04. OPS CK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME CLEAR MEL.

Part: ENTERTAIN SYS — ODOR (CD PLAYER) · airframe 48,708 hrs · 45,646 cycles

C/B J15 POPPED.UPON RESETTING J15 FUMES WERE NOTED FROM CD PLAYER._P/C J15 MX RAN PACKS NO FUME NOTED. FOUND THE POWER WIRE WAS SWITCHED WITH THE GROUND WIRE FOR THE CD PLAYER ON THE DC TO DC CONVERTER. CORRECTED THE POWER WIRE AND GROUD WIRE INSTALLATION IN REF TO AMM 23-32-05-000/400-801-A. CD PLAYER OPERATES AS REQUIRED. OK FOR SERVICE CLEAR MEL.

Part: NONE — NONE · airframe 48,453 hrs · 45,368 cycles

PDIS 641 32-10 2392501 05DEC21 PHL CLOSE AFTER LANDING GND REPORTED BLACK SMOKE FROM R/H MLG CA REPORTS BRAKE PERFORMANCE AND TEMPS WERE NORMAL. CA INSP GEAR AND HEARD AND FELT STEADY CLICKING COMG WHEEL WELL. FACT 05DEC21 22:29 PHL PERFORM GVI OF RH MLG AREA. NO LEAKS OR DAMAGE NOTED BRAKE PERFORMANCE GOOD OK FOR SERVICE AT THIS TIME

Part: DAU — FAULTED (NR 1) · airframe 47,913 hrs · 44,743 cycles

LOSS OF 115VAC BUSS IN FLIGHT WITH LOSS OF FMS1, PFD1, MFD2. R & R NR 1 DAU IAW AMM 34-41-01.OPS CHECK GOOD AT THIS TIME.INSPECTED ELECTRICAL CONNECTIONS GOING TO AVIONICS MASTER 1 NO DEFECTS NOTED AT THIS TIME.PERFORMED OPS CHECK OF AVIONICS MASTER SYSTEM IAW AMM 24-26-00 OPS CHECK GOOD AT THIS TIME OK FOR SERVICE.

Part: SKIN — DAMAGED (FRM 24 S17-18R) · airframe 47,637 hrs · 44,426 cycles

SMALL PROTRUSION ON EXTERNAL SKIN JUST FWD OF FRAME 24 BETWEEN STR 17R-18R. REPAIRED SMALL PROTRUSION ON EXTERNAL SKIN JUST FWD OF FRAME 24 BETWEEN STR 17R-18R IAW PIEDMONT EO1-05--21-0146, AND EMB145 SRM 53-22-01.

Part: SEAT TRACK — CORRODED (FRMS 54-55) · airframe 47,637 hrs · 44,426 cycles

RH OUTBD AFT SEAT TRACK RAIL IS CORRODED AT FR. 54 AND FR. 55. REMOVED CORROSION ON RH OUTBOARD AFT SEAT TRACK RAIL AT FR 54 AND FR 55 IAW EMB 145SRM 51-10-03 AND FOUND BLENDED AREAS TO BE WITH-IN ALLOWABLE LIMITS IAW EMB 145 SRM 53-00-11.

Part: FLOOR SUPPORT — CORRODED · airframe 47,637 hrs · 44,426 cycles

LH OUTBD #3 FLOOR SILL IS PITTED. REMOVED AND REPLACED LH OUTBD #3 FLOOR SILL IAW EMB 145 SRM 51-20-03 & SRM 51-40-02.

Part: PLATE — DAMAGED (BULKHEAD) · airframe 47,637 hrs · 44,426 cycles

PILOT'S BULKHEAD ATTACHMENT UPPER BOLT HOLE ELONGATED. REMOVED AND REPLACED PILOTS BULKHEAD PLATE IAW EMB145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · airframe 47,637 hrs · 44,426 cycles

RH OUTBD #3 FLOOR SILL IS PITTED. REMOVED AND REPLACED RH OUTBD #3 FLOOR SILL IAW EMB 145 SRM 51-20-03,51-40-02. RESTORED TO ORIGINAL FINISH IAW EMB 145 CPM 51-21-06,P-IEDMONT BULLETIN #51-02.

Part: FLOOR SUPPORT — CORRODED · airframe 47,637 hrs · 44,426 cycles

RH OUTBD #2 FLOOR SILL IS PITTED. REMOVED AND REPLACED RH OUT BOARD #2 FLOOR SILL IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · airframe 47,637 hrs · 44,426 cycles

RH OUTBD FLOOR SILL #5 IS PITTED. REMOVED AND REPLACED RH OUT-BD FLOOR SILL #5 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED · airframe 47,637 hrs · 44,426 cycles

RH OUTBD FLOOR SILL #4 IS PITTED. REMOVED AND REPLACED RH OUTBD FLOOR SILL #4 IAW EMB 145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED · airframe 47,637 hrs · 44,426 cycles

RH OUTBD AFT SEAT TRACK IS CORRODED AT NUMEROUS AREAS. REMOVED, AND REPLACED THE RH OUTBD AFT SEAT TRACK IAW EMB 145 AMM53-01-06.

Part: FLOOR SUPPORT — CORRODED · airframe 47,637 hrs · 44,426 cycles

LH OUTBD FLOOR SILL #4 IS PITTED. REMOVED AND REPLACED LH OUTBD FLOOR SILL #4 IAWEMB 145 SRM 51-40-02 & SRM 51-20-03.

Part: FLOOR SUPPORT — CORRODED · airframe 47,637 hrs · 44,426 cycles

LH OUTBD #7 FLOOR SILL IS PITTED. REMOVED AND REPLACED LH OUTBD #7 FLOOR SILL IAW EMB 145 SRM 51-20-03 & SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FRMS 39-40) · airframe 47,637 hrs · 44,426 cycles

LH CENTER SEAT TRACK IS CORRODED BETWEEN FR 39-40. REMOVED AND REPLACED LH CENTER SEAT TRACK BETWEEN FR 39-40 IAW EMB145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 47,637 hrs · 44,426 cycles

RH #4 CARGO FLOOR SILL CORRODED. REMOVED AND REPLACED RH #4 CARGO FLOOR SILL IAW EMB--145 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FRMS 51-52) · airframe 47,637 hrs · 44,426 cycles

RH OUTBD SEAT TRACK IS CORRODED BETWEEN FR 51-52. REMOVED AND REPLACED R/H OUT-BD SEAT TRACK BETWEEN FR 51-52 IAW EMB145 AMM 53-01-06.

Part: FLOOR SUPPORT — CORRODED · airframe 47,637 hrs · 44,426 cycles

LH OUTBD FLOOR SILL #6 IS PITTED. REMOVED AND REPLACED LH OUTBD # 6 FLOOR SILL IAW EMB 145 SRM 51-20-03 & SRM 51-40-02.

Part: SKIN — PUNCTURED (RUDDER) · airframe 47,637 hrs · 44,426 cycles

RUDDER II HAS HOLE RH SIDE BOTTOM ON TRAILING EDGE (MARKED). REPAIRED RUDDER II HOLE ON RH SIDE BOTTOM ON TRAILING EDGE IAW PIEDMONT EO1-55-21--0134 AND ETD2021--145-016785.

Part: SKIN — CRACKED (FRM 77 S6-7R) · airframe 47,637 hrs · 44,426 cycles

EXTERIOR FUSELAGE AT FR 77 BETWEEN STR6R-7R HAS POSSIBLE CRACKS AROUND 2 RIVETS. REPAIRED EXTERIOR FUSELAGE AT FR 77 BETWEEN STR 6R-7R CRACKS AROUND 1 RIVET IAW PIEDMONT EO1-53-21-0140. ONE RIVET FOUND NOT TO HAVE CRACKS AROUND IT.

Part: SKIN — CRACKED (FRM 79 S3-4R) · airframe 47,637 hrs · 44,426 cycles

EXTERIOR FUSELAGE AT FR 79 BETWEEN STR 3R-4R HAS POSSIBLE CRACKS AROUND 1 RIVET (MARKED). REPAIRED EXTERIOR FUSELAGE AT FR 79 BETWEEN STR 3R-4R CRACKS AROUND1 RIVET IAW PIEDMONT EO1-53-21-0140.

Part: SKIN — CRACKED (FRM 78 S4-7L) · airframe 47,637 hrs · 44,426 cycles

EXTERIOR FUSELAGE AT FR 78 BETWEEN STR 4L-7L HAS POSSIBLE CRACKS AROUND 5 RIVETS. REPAIRED EXTERIOR FUSELAGE AT FR 78 BETWEEN STR 4L-7L CRACKS AROUND3 RIVETS IAW PIEDMONT EO1-53-21-0141. TWO RIVETS FOUND NOT TO HAVE CRACKS AROUND THEM.

Part: STRINGER — CHAFED (FRMS 52-53 S19R) · airframe 47,637 hrs · 44,426 cycles

RH FUSELAGE STRINGER 19R BETWEEN FR 52-53 IS CHAFED. RE-ACCOMPLISHED ANGLE REPAIR ON RH FUSELAGE STRINGER 19R BETWEEN FR 52-53 IAW EMB 145 SRM 53-24-02 AND EO1--53-21-0138.

Part: RIB — CRACKED (LT WING) · airframe 47,637 hrs · 44,426 cycles

LH WING RIB 21 IS CRACKED. PERFORMED REPAIR AT L/H WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4 FIG.203 AND EO1-57-21-0139.

Part: RIB — CRACKED (RT WING) · airframe 47,637 hrs · 44,426 cycles

RH WING RIB 21 IS CRACKED. PERFORMED REPAIR AT R/H WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4 FIGURE 203 AND EO1-57-21-0139.

Part: BRACKET — CRACKED (NLG WW) · airframe 47,637 hrs · 44,426 cycles

NLG UP-LOCK BOX FWD HORIZONTAL ATTACHMENT BRACKET IS CRACKED. REMOVED AND REPLACED NLG UP LOCKBOX FWD HORIZONTAL ATTACHMENT BRACKET / SUPPORT IAW EMB 145 SRM 51-40-02.

Part: BRACKET — CRACKED (NLG UPLOCK) · airframe 47,637 hrs · 44,426 cycles

NLG UP-LOCK BOX BRACKET IS CRACKED (MARKED). REMOVED AND REPLACED NLG UP LOCK BOX BRACKET IAW EMB145 SRM 51-40-02.

Part: ANTI-ICE VALVE — INOPERATIVE (WING) · airframe 47,481 hrs · 44,275 cycles

BLEED VALVE 1 CLOSED ON EICAS WITH ICE CONT- A/I INOP + WING A/I FAIL TROUBLE SHOOTING. R+R PNEUMATIC OVERHEAD PANEL AS REQ. OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (BLEED VALVE) · airframe 47,481 hrs · 44,275 cycles

PDIS 641 36-11 2387341 14APR21 RIC ASSGN BLEED 1 VLV CLOSED MSG DISPLAYED ON EICAS IN FLIGHT WITH WITH ICE COND A/I INOP AND WING A/I FAIL. IN WORK AT RIC

Part: STALL WARNING — INOPERATIVE · airframe 47,223 hrs · 43,993 cycles

SPS 1 INOP MASTER WARNING ON TAKE OFF ROLL REJECTED TAKE OFF. T/S SPS 1 INOP REF FIM 27-36-00-810-801-A FOUND TRAN SITORY CONDITION PERFORMED STALL PROTECTION SYS OPS CHECK IAW AMM 27-36-00 OPS CHECK GOOD A/C OK FOR SERVICE.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 47,193 hrs · 43,952 cycles

CABIN PRESSURIZATION IN AUTO WOULD NOT PRESSURIZE, IN MANUAL MODE IT WAS UNCONTROLLABLE. MAINTENANCE PERFORMED: FOUND CABIN PRESSURE CONTROLLER TO BE FAULTING. R & R CABIN PRESSURE DIGITAL CONTROLLER, IAW AMM 21-31-01. OPERATIONS CHECK GOOD, IAW AMM 21-31-00-700. CLEAR MEL 21-10-3. OUTFLOW VALVE INHIBITORS RE-STOWED IN PROPER POSITIONS. AC OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,998 hrs · 43,739 cycles

FLOOR EMERGENCY LIGHTS ON ROWS 1-3 GO OUT AFTER YOU TURN THEM ON. REMOVED AND REPLACED NUMBER 2 EMERGENCY LIGHT BATTERY SUPPLY, IAW AMM 33-50-04.

Part: CABIN PRESSURE — FAULTED · airframe 46,898 hrs · 43,623 cycles

PDIS 641 21-31 2379721 19OCT20 ROA CLOSE. CABIN AUTO PRESS FAIL IN FLIGHT WITH NO ASSOCIATED MESSAGES. MANUAL PRESS FUNCTION OK. FACT 19OCT20 13:32 ROA. T/S USING FIM 21-31-00-810-809-A STEPS 1 AND 2. OPERATIONS CHECKED, IAW AMM 21-31-00-700-802-A, NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (BATTERY OVERTEMP) · airframe 45,580 hrs · 42,153 cycles

PDIS 641 24-36 2204481 18OCT19 MGM CLOSE BATTERY 1 OVERTEMP MESSAGE ON EICAS IN FLIGHT FACT 19OCT19 16:22 MGM R&R CANNON PLUG ON WIRE P1007 TO BATTERY #1 TEMP SEN SOR. PERFORMED OPS CHECK OF BATTERY & TEMP ON MFD. O PS CHECK GOOD, NO DISCREPANCIES NOTED. OK FOR SERVICE.

Part: CONNECTOR — DAMAGED (BATTERY TEMP) · airframe 5,575 hrs · 42,147 cycles

PDIS 641 24-36 2204471 18OCT19 CLT CLOSE BATT 1 OVRTEMP MESSAGE DISPLAYED AND BATT CONTINUES TO CLIMB ON GROUND. FACT 18OCT19 15:34 CLT CLEANED AND RESEATED ALL 4 PINS IN BATTERY 1 TEMP SE NSOR CONNECTOR (P1007) BATTERY TEMP IS NORMAL WITH NO EICAS MESSAGES. OK FOR SERVICE. NOTE: ALSO DURING TROUBLE SHOOTING R&R'D BATTERY, TEMP INSTALLED BOTH DAU'S (NO FIX), AND R&R'D CANNON PLUG ON WIRE P1007 TO BATT #1 TEMP SENSOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,678 hrs · 41,145 cycles

641 33-51 0022950 15MAY19 RIC CLOSE CEILING EMERGENCY LIGHT ABOVE MAIN DOOR DOES NOT ILLUMINATE. 28916 00 NGR FACT 15MAY19 11:29 RIC R/R MAIN DOOR EMERGENCY LIGHT IN REF TO AMM 33-50-06-000/400-801-A. P/N ON LIGHT 1317 P/N OFF LIGHT 1317.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 43,873 hrs · 40,202 cycles

NDIS 641 33-51 0020380 15DEC18 SBY CLOSE EMERGENCY LIGHT UNDER MAIN DOOR HINGE IS INOP 34166 00 CRH FACT 15DEC18 09:34 SBY FOUND WIRES FOR THE EMERGENCY LIGHT DICONNECTED AT T HE QUICK CONNECTS. RECONNECTED WIRES TO EMERGENCY LI GHT. OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 43,828 hrs · 40,152 cycles

PDIS 641 52-30 1723121 06DEC18 FWA ASSGN BAGG DOOR OPEN DURING TAKEOFF ROLL. AND ABORTED TAKE OFF. HISTORY: NOV 28 MEL 06DEC18 16:00 FWA C34017 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 43,757 hrs · 40,077 cycles

PDIS 641 52-30 1691001 25NOV18 AVP ASSGN ON TAKEOFF ROLL BAGGAGE DOOR OPEN INDICATION EICAS M ESSAGE DISPLAYED. VERIFIED DOOR CLOSED AND LATCHED W ITH GROUND PERSONNEL. MATTHEW HISTORY: NONE MEL 25NOV18 06:27 AVP C32902 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING

Part: RELAY — UNKNOWN (PARK BRAKE) · airframe 43,740 hrs · 40,057 cycles

PDIS 641 32-44 1690951 20NOV18 PHL CLOSE PARKING BRAKE ON LIGHT FOUND TO BE ILLUMINATED SHORTLY AFTER TAKEOFF. T/O CONFIG CHECK OK. BRAKES OPS NORMAL. FACT 20NOV18 10:43 PHL RR PARK BRAKE RELAY K0212 AS REQUIRED. RR PARK BRAKE PRESS SW IAW 32-44-07. LEAK CHECK GOOD. SLAVED IN AWU AS REQ. NO FIX. REINSTALLED AWU. RR PARKING BRAKE SWITCH INDICATOR AS REQUIRED. OPS CHECK PARKING BRAKE GOOD AT THIS TIME. OK FOR SERVICE.

Part: CUP — CRACKED (CARGO DOOR) · airframe 43,436 hrs · 39,714 cycles

DISCREPANCY: IN HEAVY MAINTENANCE CHECK AT ABI POSSIBLE CRACK ON CARGO DOOR HANDLE RECESS CUP NOTED. CORRECTIVE ACTION: VERIFIED CRACK THROUGH NDT AND REPAIRED CRACK IAW EDT2018-145-099950.

Part: WEB — CHAFED (CARGO DOOR) · airframe 43,436 hrs · 39,714 cycles

DISCREPANCY: IN HEAVY MAINTENANCE CHECK AT ABI CARGO DOOR INTERIOR WEB IS FOUND TO HAVE MULTIPLE CHAFES. CORRECTIVE ACTION: PERFORMED NDT TESTING, MECHANICALLY MEASURED CHAFES AND FOUND MULTIPLE TO BE OUT OF LIMITS, VERIFIED INTERCHANGEABILITY OF INTERIOR WEB, AND RAR NEW CARGO DOOR INTERIOR WEB IAW SRM 51-40-02

Part: SKIN — CRACKED (CARGO DOOR) · airframe 43,436 hrs · 39,714 cycles

DISCREPANCY: IN HEAVY MAINTENANCE CHECK AT ABI BAGGAGE DOOR SKIN IS FOUND TO BE CRACKED AFT OF THE OPEN CLOSE HANDLE. CORRECTIVE ACTION: CRACK VERIFIED THROUGH NTD TESTING AND REPAIRED IAW ETD2018-145-091736

Part: OIL SYSTEM — LOW (NR 1 ENGINE) · airframe 43,045 hrs · 39,249 cycles

NR 1 ENGINE AT MIN DISPATCH. SERVICED THE NR 1 ENGINE WITH 2 QTS OF OIL IAW AMM 12-12-01-03.

Part: UNKNOWN — SMOKE (NOT REPORTED) · airframe 42,947 hrs · 39,132 cycles

DURING START, AND TAXI, CREW SAW PUFFS OF WHITE SMOKE. INSPECTED THE NOSE E/E BAY, NO OBVIOUS DEFECTS NOTED. INSPECTED THE NOSE HYD SERVICE AREA, NO OBVIOUS DEFECTS NOTED. CREW GROUND RAN THE ACFT FOR 5 MINS NO EVIDENCE OF WHITE SMOKE. OK FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 42,523 hrs · 38,652 cycles

NR 2 ENGINE ANTI ICE FAILED MESSAGE WITH OPEN INSCRIPTION NOT ILLUMINATED, FOLLOWED BY ICE CONDITION ANTI ICE MESSAGES. FOLLOWED FIM TASK 30-21-00-810-A. ANTI ICE VALVE FAILED CMC MESSAGE STEPS 1, 7, 15. R & R THE NR 2 ENGINE ANTI ICE VALVE IAW 30-21-00. PERFORMED OPS CHECK IAW 30-21-00. OPS CHECKED GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS) · airframe 41,366 hrs · 37,461 cycles

CEILING EXIT SIGN BETWEEN ROWS 11 & 12 IS NOT ILLUMINATING ON THE AFT SIDE. UPON FURTHER INSPECTION, FOUND LOOSE ELECTRICAL CONNECTORS ON EXIT SIGN. CLEANED AND CONNECTORS. OPS CHECKED GOOD, OK FOR SERVICE.

Part: ANTI-ICE VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 41,245 hrs · 37,339 cycles

NR 2 ENGINE ANTI-ICE MESSAGE APPEARED ON EICAS, CREW RAN THROUGH QRH PROCEDURE MESSAGE STAYED AND DIDN`T GO OUT. VALVE SECURED OPEN IAW AMM 30-21-01-040-801-A.. OPERATIONAL PROCEDURE IAW AMM TASK 30-21-01-040-801-A.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 40,645 hrs · 36,675 cycles

SPOILER FAIL EICAS CAUTION MESSAGE DURING TAXI OUT. SPOILER INDICATED CLOSED. MAINTENANCE REPORTS GROUND SPOILER ENG CHT FAULT MESSAGE ON CMC.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (NR 2 ENGINE) · airframe 40,571 hrs · 36,597 cycles

NR 2 ENGINE ANTI ICE FAILED AT 18,000 FEET. WOULD NOT CLEAR WITH ABNORMAL PROCEDURES. ENGINE ANTI-ICE VALVE DEACTIVATED. ANTI-ICE VALVE OPS CHECKED.

Part: INDICATION SYS — MALFUNCTIONED (ANTI ICE SYS) · airframe 40,551 hrs · 36,573 cycles

DURING FLIGHT, THE NR 2 ENGINE ANTI ICE INLET OPEN ENSCRIPTION EXTINGUISHED. COMPLIED WITH TASK 30-21-00-700804-A. OPS CHECKED GOOD. VALVE CONFIRMED OPEN WITH TEST. FLIGHT DECK INDICATION ONLY.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,009 hrs · 36,014 cycles

RIGHT EXTERNAL OVER-WING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB IAW MM 33-50-10. OPS CHECKED GOOD.

Part: HYDRAULIC SYSTEM — LOW (NR 1) · airframe 39,555 hrs · 35,518 cycles

IN FLIGHT, HYD 1 LOW QTY MESSAGE APPEARED ON EICAS. CREW FOLLOWED QRH PROCEDURE 10-7. CREW NOTICED QTY DROPPING AND SUSPECTED NR 1 HYD SYSTEM FAILURE. CREW THEN FOLLOWED QRH 10-5 QTY INDICATION JUST ABOVE AMBER, GREEN IN FLT DECK WITH ENGINES SHUTDOWN. NR 1 HYD SYS SERVICED, SEQ 2. QTY DID NOT CHANGE WHEN ARRIVED. JACKED ACFT, DID RETRACTION & EXTENSION TEST IN REF TO MM 32-30-00. OPS CHECK GOOD AT THIS TIME. LOWERED ACFT. SERVICED NR 2 HYD QTY IN REF TO MM 12-13-01. OK FOR SERVICE.

Part: CIRCUIT BREAKER — PULLED · airframe 39,371 hrs · 35,287 cycles

DURING TAKEOFF ROLL, NO CONFIGURATION WARNING. CREW ABORTED TAKEOFF. REF ETD2016-145-049640, THE NO TAKEOFF CONFIG WARNING WAS INDUCED DUE TO SPOILER IND CB PULLED IAW DDPM AND IND FAILS TO SHOW "OPEN". SPOILER IND CB CLOSED AND MAINTENANCE ACTION C/W IAW ETD.

Part: RELAY — FAILED (PITOT HEAT) · airframe 39,355 hrs · 35,261 cycles

WHILE ON DESCENT NR 3 PITOT INOPERATIVE. EICAS CAUTION MESSAGE APPEARED. STARTED SMELLING ODOR THAN MOMENTS LATER F/A REPORTED SMOKE IN CABIN. DECLARED EMERGENCY LANDING AND EVACUATED ACFT ON GROUND. NO HISTORY CX DAMAGE INSPECTION OVERHEAT BURN DAMAGE FOUND ON LOWER CENTER RT RELAY SUPPORT ACCESS PANEL 224ERW, STEMMING FROM RELAY K0057. R & R RELAY REPLACE ALL ASSOCIATED BURNED WIRING STILL IN PROGRESS.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 39,321 hrs · 35,214 cycles

BAGGAGE DOOR OPEN INDICATION ON T/O ROLL. ABORTED T/O, RETURN TO GATE AND CONFIRMED DOOR CLOSED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,240 hrs · 35,108 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AT FRAME 75, THE FIRST FASTENER BELOW STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1930.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,240 hrs · 35,108 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2L. REPAIRED LT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1930.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,239 hrs · 35,107 cycles

STRINGER 20R IS CORRODED, BETWEEN FRAME 13 - 14. CORROSION IS ACCEPTED AS IS IAW ERS-EM-5300-1920.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 39,239 hrs · 35,107 cycles

TOILET WASTE VLV SUPPORT CORRODED. FABRICATED & PREPPED REPAIR DOUBLER IAW SRM 53-31-02.

Part: YOKE — CRACKED (RT PYLON) · airframe 39,239 hrs · 35,107 cycles

RIGHT FWD PYLON LOWER YOKE CRACKED ON THE FWD FLANGE. REMOVED & INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,239 hrs · 35,107 cycles

RIGHT OTBD AFT CARGO FLOORBEAM HAS CORROSION AROUND SCREW HOLE. REMOVED & INSTALLED RT OTBD AFT CARGO FLOORBEAM, FLOORBOARD SUPPORT, IAW SRM 51-40-02.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 39,239 hrs · 35,107 cycles

CROSSBEAM AT FRAME 20 IS CORRODED. REMOVED & REPLACED CROSSBEAM AT FRAME 20 IAW SRM 51-40-02 & ETN-EM-53-139.

Part: STRIP — BROKEN (CABIN) · airframe 39,239 hrs · 35,107 cycles

EMERGENCY LIGHT STRIPS 5 & 8 ARE BROKEN. R & R EMER LIGHT STRIPS 5 & 8 IAW AMM 33-50-12. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: SPAR — CRACKED (LT WING) · airframe 39,239 hrs · 35,107 cycles

LEFT WING SPAR I LOWER FLANGE CRACKED AT NUTPLATE HOLE AT RIB 9, VERIFIED BY HFEC. REPAIRED LT WING SPAR I LOWER FLANGE CRACK AT NUTPLATE HOLE AT RIB 9 IAW ERS-EM-57MR-583. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.

Part: LIGHT — DIRTY (CABIN) · airframe 39,239 hrs · 35,107 cycles

PASSENGER DOOR EMER LIGHT INOPERATIVE. CLEANED PAX DOOR EMER LIGHT IAW CPM 51-14-00. OPERATIONS CHECKED GOOD.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 39,239 hrs · 35,107 cycles

SERVICE DOOR LOWER BEAM CRACKED AT AFT END. SEE NRTC E491285 FOR CORRECTIVE ACTION. ENTIRE BEAM IS BEING REPLACED UNDER THAT NRTC.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 39,239 hrs · 35,107 cycles

EMERGENCY LIGHT FLOOR STRIPS 3 & 4 INOPERATIVE. RECONNECTED PLUG P8031 J8031 AT NR 3 BATTERY IAW SWPM 20-21-00 & AMM 20-50-00. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: WIRE — BROKEN (CABIN) · airframe 39,239 hrs · 35,107 cycles

SERVICE DOOR HINGE COVER EMER LIGHT HAS A BROKEN WIRE. REPAIRED WIRES ON SERVICE DOOR HINGE COVER EMER LIGHT IAW SWPM 20-21-00.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 39,239 hrs · 35,107 cycles

LEFT OMEGA BEAM OTBD SUPPORT IS CRACKED, BETWEEN FRAME 47 - 48. REMOVED CRACKED, BETWEEN FRAME 47 - 48. LEFT OMEGA BEAM OTBD SUPPORT & INSTALLED SERVICEABLE BEAM SUPPORTS IAW SRM 53-23-02.

Part: CHECK VALVE — FAILED (BRAKE SYSTEM) · airframe 39,239 hrs · 35,107 cycles

RETURN LINE CHECK VLV OF THE EMER & PARKING BRAKE SYS FAILED OPERATIONAL CHECK. R & R EMER & PARKING BRAKE SYS RETURN LINE CHECK VLV IAW AMM 32-44-08. LEAK CHECKED GOOD.

Part: FIREWALL — CRACKED (APU BAY) · airframe 39,239 hrs · 35,107 cycles

INTERNAL APU FIREWALL SKIN CRACKED ABOVE RT VERTICAL SUPPORT UPPERMOST RIVET. REPAIRED INTERNAL APU FIREWALL SKIN ABOVE RT VERTICAL SUPPORT UPPERMOST RIVET IAW EO EM-53AD-1883R5.

Part: WIRE — DAMAGED (CABIN) · airframe 39,239 hrs · 35,107 cycles

SERVICE DOOR EMER LIGHT WIRE IS DAMAGED. REPAIRED SERVICE DOOR EMER EXIT LIGHT WIRE IAW SWPM 20-21-00.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,239 hrs · 35,107 cycles

EXTERNAL FUSELAGE SKIN ONE POSSIBLE CRACK AT RIVET ON FRAME 78, BETWEEN STRINGER 5L & 6L. UPON FURTHER INVESTIGATION ALSO FOUND CRACK ON FRAME 78, BETWEEN STRINGER 3L - 4L. PERFORMED REPAIR ON FUSELAGE SKIN IAW ERS-EM-5300-1919.

Part: MOUNT BRACKET — BROKEN (FLASHLIGHT) · airframe 38,794 hrs · 34,699 cycles

REAR CABIN FLASHLIGHT MOUNTING BRACKET BROKEN. R & R REAR CABIN FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: BLEED VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 38,251 hrs · 34,199 cycles

ABORTED TAKEOFF, DUE TO BLD 2 VALVE FAIL EICAS MSG, AFTER THRUST SET ON TAKEOFF. 1 TAKEOFF IAW MEL GOT MSG SPEED WDS 30-40 KTS. R & R ENG 2 BLEED VALVE IAW AMM 36-11-05. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 37,694 hrs · 33,708 cycles

EICAS MSG, SPOILER FAIL IN FLIGHT SPOILERS INDICATED CLOSED. CB PULLED IAW AOM 1 CHECKLIST. POST FLIGHT INSPECTION FOUND LT INBD SPOILER PANEL FLOATING SLIGHTLY. PERFORMED OPERATIONAL TEST OF SPOILER SYS IAW AMM 27-63-01. SYS OPERATIONS CHECKED NORMAL AT THIS TIME. NO FURTHER MSGS NOTED OR CMC FAULTS.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 37,686 hrs · 33,698 cycles

CAPTAIN'S EMER FLASHLIGHT CRADLE BROKEN. R & R CAPTAIN`S EMER FLASHLIGHT CRADLE IAW EMB TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 37,660 hrs · 33,663 cycles

AFTER LANDING NOSE WHEEL STEERING NOT WORKING. TOWED TO THE GATE. R & R NLG WOW PROXIMITY SWITCH IAW AMM 32-63-02. OPERATIONS CHECKED GOOD IAW ETN-EM-32-176 & FIM TASK 32-50-00-810-803-REF ITEM 2 LG 3673600.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 37,445 hrs · 33,452 cycles

REAR FLASHLIGHT CRADLE BROKEN. DEFERRED IAW MEL 25-53. M PROCEDURES COMPLIED WITH. R & R AFT EMER FLASHLIGHT BRACKET IAW AMM 33-50-16. OPERATIONAL CHECK GOOD, MEL RESTORED.

Part: SENSOR — CONTAMINATED (SPOILER) · airframe 37,386 hrs · 33,383 cycles

DURING LEVEL CRUISE FLIGHT AT 17,000 FEET & 310 KIAS, SPOILER FAIL, PRESENTED & MAINTAINED ON EICAS. COMPLIED WITH ABNORMAL PROCEDURE & CFR MET US ON LANDING. FOUND LT & RT OTBD SPOILER SENSORS CONTAMINATED & NOT PROPERLY WRAPPED. CLEANED & REWRAPPED BOTH SPOILER OTBD SENSORS IAW AMM 27-63-04. OPERATIONS CHECK OF SPOILERS SYS GOOD IAW AMM 27-63-01.

Part: ANTI-ICE VALVE — FAILED (NR 2 ENGINE) · airframe 37,340 hrs · 33,331 cycles

NR 2 ENGINE ANTI-ICE FAILED INFLIGHT AFTER AOM 1 PROCEDURE. R & R ANTI-ICE VALVE IAW AMM 30-21-01. OPS CHECKED GOOD IAW AMM 30-00-00-700-802-A & 30-00-00-700-803-A.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,502 hrs · 32,559 cycles

MAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 36,080 hrs · 32,195 cycles

AFTER 15 MIN IN CRUISE COCKPIT STARTED FILLING WITH FUMES. EMER PROC COMPLIED WITH, CONTINUED TO LANDING & EMER DECLARED COMPLIED WITH ETN-EM-72-034. COULD NOT DETECT FUMES IN COCKPIT OR CABIN THROUGHOUT PROCEDURE. REMOVED PACK ACCESS PANEL 191EL & INSPECTED LINES & PACK IAW SMP, NO DEFECT NOTED. CHECKED ACARS FOR THERMAL RUNAWAY IAW SMP, NO DEFECTS NOTED. REMOVED GLARE SHIELD IAW AMM 25-12-07 & INSPECTED WINDSHIELD HEATING SENSORS IAW SMP, NO DEFECTS NOTED. CHECKED COCKPIT EMER FLASHLIGHTS IAW SMP, NO DEFECTS NOTED. BAGGED DRAIN LINES ON ENG 1 & RAN ENG AT HIGH POWER & INSPECTED ENG FOR OIL MULTIPLE TIMES IAW MM 72-00-00, NO LEAKS NOTED & NO FUMES NOTED. PERFORMED BLACK LIGHT TEST FOR VISIBLE OIL & OIL LEAKS IAW SMP, NO LEAKS NOTED.

Part: WIRE HARNESS — DEFECTIVE (COCKPIT) · airframe 36,047 hrs · 32,159 cycles

EMERGENCY EXIT LIGHT UNDER FLIGHT DECK DOOR INOPERATIVE. R & R STEP LIGHT HARNESS IAW MM 33-26-06. OPERATIONS TEST OF EMER LIGHT GOOD IAW MM 33-50-00 & OPERATIONS TEST OF STEP LIGHT GOOD IAW MM 33-26-00.

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 35,720 hrs · 31,882 cycles

EMER LIGHTS NOT ARMED EICAS MSG, MOMENTARILY ILLUMINATED IN FLIGHT. CREW IS NOT SURE IF EMER LIGHTS ILLUMINATED. PERFORMED OPERATIONAL CHECK OF EMER LIGHTING SYS, NO DEFECTS NOTED AT THIS TIME IAW WORK CARD 33-700-17.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 35,561 hrs · 31,750 cycles

DURING CLIMB OUT ON FLIGHT 3362 CREW REPORTED A LOUD SQUEAL HEARD IN COCKPIT. AT FLT 20,000, CABIN ALT 2600, CABIN RATE AT 0, CAB DELTA P AT 6.6 CABIN RATE DID NOT CHANGE. DECLARED EMERGENCY FOR CABIN PRESS THE ACFT WAS REMOVED FROM SERVICE. BONDED LOWER SECTION OF DV SEAL IAW ETN-EM-56-034, AMM 56-11-00 & R & R DIGITAL CONTROLLER IAW AMM 21-31-01 OPERATIONS CHECKED GOOD. THE ACFT RETURN SERVICE.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 35,171 hrs · 31,443 cycles

APU FAIL MSG AFTER APU WAS RUNNING. STRONG ODOR OF FUEL AFTER APU STARTED. DEFERRED IAW MEL 49-1 & COMPLIED WITH MX PROCEDURE. EXAMINED THE FUEL LINE & CONNECTION FOR LEAKS, PERFORM OPERATION CHECK ON APU. OPERATIONS CHECKED GOOD, NO LEAKS IAW AMM 49-13-00 MEL RESTORED.

Part: ACM — SEIZED (AC BAY) · airframe 34,925 hrs · 31,248 cycles

A LITTLE SMOKE IN COCKPIT AFTER ENG NR 1 WAS STARTED 30 SEC LATER PACK NR 1 OVERHEAT MSG. FOUND NR 1 ACM SEIZED. R & R NR 1 ACM IAW AMM 21-51-03, OPERATIONS CHECKED GOOD AT THIS TIME. PERFORMED ETN EM 72-034 ENG ODOR EVENT SUPPLEMENT, NO DEFECTS NOTED AT THIS TIME.

Part: BRAKE — FAILED (TE FLAP) · airframe 34,904 hrs · 31,233 cycles

FLAP FAIL MSG WHEN FLAP LEVER MOVED TO 9. INDICATION REMAINED AT 0 ON EICAS. ACFT HAD VERY SLIGHT TENDENCY TO ROLL RIGHT. R & R RT FLAP TRANSMISSION BRAKE IAW AMM 27-51-01, OPERATIONS CHECKED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,874 hrs · 31,213 cycles

WHEN SETTING FLAPS FROM FULL UP, O DEGREES TO 9 DEGREES ON FINAL APPROACH FOR LANDING WE GOT, FLAP FAIL, MSG ON EICAS. PERFORMED FIM TASK 27-51-00-810-816-A. MSG CHANGED TO FLAP LOW SPEED.

Part: ACTUATOR — FAULTY (THRUST REVERSER) · airframe 34,723 hrs · 31,096 cycles

WHEN THRUST REVERSER WERE STOWED AFTER LANDING EICAS ENG 2 REVERSER DISAGREE MSG WAS PRESENTED & REMAINED ON AFTER SHUT DOWN. R & R E2 TERTIARY LOCK ACTUATOR IAW AMM 78-32-05. OPERATIONS CHECK & LEAK CHECKED GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 34,713 hrs · 31,088 cycles

INTERNAL FUSELAGE SKIN CORRODED BETWEEN FRAME 13 - 14, STRINGER 18R - 20R. PERFORMED REPAIR IAW AEA ERS-EM-53MR-210.

Part: YOKE — CRACKED (LT PYLON) · airframe 34,713 hrs · 31,088 cycles

LEFT PYLON FWD LOWER YOKE I CRACKED BY ENG MOUNT. R & R LT PYLON FWD LOWER YOKE I IAW EO EM-54MR-386.

Part: SILL — CORRODED (FUSELAGE) · airframe 34,713 hrs · 31,088 cycles

SERVICE DOOR CTR SILL CORRODED. R & R SERVICE DOOR CTR SILL IAW SRM 51-40-02.

Part: BEAM — CRACKED (FUSELAGE) · airframe 34,713 hrs · 31,088 cycles

RIGHT BEAM CRACKED AT INBD SUPPORT BETWEEN FRAME 47 & 48. R & R RT BEAM AT INBD SUPPORT BETWEEN FRAME 47 & 48 IAW SRM 53-23-02.

Part: WIRE — DAMAGED (FLASHLIGHT) · airframe 34,713 hrs · 31,088 cycles

LAVATORY FLASHLIGHT WIRE ON LAVATORY CEILING IS MISSING ON CONTACT & ITS RUBBER QUICK DISCONNECT. INSTALLED NEW SPLICE AT SP 3557 FOR LAVATORY FLASHLIGHT IAW WM 91-10-02 & SWPM 20-00-03.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 34,713 hrs · 31,088 cycles

STRINGER 21L IS CORRODED AT FRAME 13. INSTALLED NEW STRINGER 21L & INSTALLED STRINGER SPLICE IAW SRM 51-40-02.

Part: FIREWALL — CRACKED (RT MLG WW) · airframe 34,713 hrs · 31,088 cycles

THE RT MLG WW AFT FIREWALL IS CRACKED AT TWO POSITIONS. R & R SERVICEABLE AFT FIREWALL ON THE RT MLG WW IAW SRM 51-40-02.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 34,577 hrs · 30,988 cycles

ON FLIGHT 3757 AFTER TAKEOFF LAVATORY SMOKE WARNING. FLIGHT ATTENDANT REPORTED LIGHT BLUE SMOKE IN CABIN. SMOKE DISSIPATED AFTER CABIN SMOKE PROCEDURE & AN EMERGENCY LANDING. THE ACFT WAS REMOVED FROM SERVICE. GND RAN ENGS AT TAKEOFF POWER & THE NR 2 PACK TEMP SET AT MIDWAY. DETERMINED NR 2 ENG PRODUCING BURNING SMOKE & SMELL IN CABIN. ENG ODOR EVENT. R & R NR 2 ENG IAW WC 71-00-00, OPERATIONS CHECKED GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 33,865 hrs · 30,421 cycles

CEILING EMERGENCY EXIT ROW LIGHT BACK HALF INOPERATIVE. RESET POWER OPS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — MISINSTALLED (EMERGENCY EXIT) · airframe 33,832 hrs · 30,398 cycles

RT OVERWING EMERGENCY LIGHT INSTALLED UPSIDE DOWN. REPOSITIONED RT OVERWING EMERGENCY LIGHT IAW MM 33-50-10. OPS CHECKED GOOD, OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,569 hrs · 29,394 cycles

DURING B INSPECTION FOUND THE 12A EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE 12A EMERGENCY LIGHT BULB IAW EMB AMM 33-50-07-000-801-A AND 33-50-07-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,249 hrs · 29,148 cycles

A DURING B INSPECTION FOUND THE AFT OVERHEAD EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 31,855 hrs · 28,833 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING AFT EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 31,745 hrs · 28,748 cycles

DURING MAINTENANCE INSPECTION FOUND EXTERIOR OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY CHARGER NR 4 IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,711 hrs · 28,722 cycles

DURING B INSPECTION FOUND THE RIGHT UPPER WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPLY UNIT IAW W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,685 hrs · 28,697 cycles

DURING PS-2 INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AND BATTERY IAW AMM TASK 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 31,652 hrs · 28,673 cycles

DURING B INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY POWER SUPPY IAW EMB 145 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,285 hrs · 28,390 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLOOR LIGHT STRIP AT ROW 1 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 FLOOR STRIP IAW EMB 145 AMM 36-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 31,281 hrs · 28,387 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR EMERGENCY REFLECTANT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. NO FIX DEFERRED PER MEL 33-29 AUTH 091072D-C ALL MAINTENANCE ITEMS COMPLIED WITH. REPAIRED WIRING AT SPLICE (SP7377) IAW EMB SWPM 20-00-03 OPS/CHECK GOOD IAW EMB AMM 33-50-00 MEL ITEM RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,124 hrs · 28,277 cycles

DURING B INSPECTION FOUND THE FORWARD EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY POWER SUPPLY AND BATTERY IAW AE W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 30,327 hrs · 27,652 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RECHARGEABLE FLASHLIGHT SYSTEM NEEDS A BATTERY. AIRCRAFT REMOVED FROM SERVICE. REPLACED BATTERY. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 30,282 hrs · 27,619 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT CABIN EMERGENCY FLASHLIGHT HAS BROKEN FINGER IN CRADLE TO SUPPORT FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (NLG) · airframe 29,548 hrs · 27,076 cycles

ON FLIGHT 4344 THE CREW REPORTED THAT ON APPROACH AFTER GEAR EXTENDED A NOISE WAS HEARD FROM FORWARD OF THE RUDDER PEDALS. SOUNDED LIKE BUMPING ON THE INSIDE OF THE PLANE. THE CREW DECLARED AN EMERGENCY AND PERFORMED A FLY-BY SO THE TOWER COULD INSPECT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NOISE WAS NOT CONTINUOUS AND HEARD ONCE DURING TAXI WHEN WE WENT OVER A POT HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR DOWN LOCK PROXIMITY SWITCHES IAE EMB 145 AMM 32-61-02. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,169 hrs · 26,803 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS FAIL TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AND RIGHT LAMPS IAW AMM 33-50-10 AND REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHTS POWER SUPPLY IAW 33-50.04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,170 hrs · 26,803 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CENTER CABIN EMERGENCY LIGHTS FLICKERING WHEN ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHTS BATTERY AND BATTERY PACK IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,170 hrs · 27,803 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED AFT RIGHT OVERWING EXTERNAL EMERGENCY LIGHT. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING) · airframe 30,919 hrs · 28,115 cycles

DURING B INSPECTION, FOUND THE LEFT AND RIGHT OVERWING EXTERNAL EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,919 hrs · 28,115 cycles

DURING B INSPECTION, FOUND THE CENTER CABIN EMERGENCY LIGHTS FLICKERING WHEN ON. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,016 hrs · 26,680 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT REAR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LEFT SIDE REAR IAW AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 28,996 hrs · 26,663 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CABIN OVERWING FORWARD EMERGENCY EXIT LOCATOR SIGN INOPERATIVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,844 hrs · 26,547 cycles

FOR FLIGHT 3541 THE CREW REPORTED THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 28,521 hrs · 26,288 cycles

FOR FLIGHT 5252 DURING THE PREFLIGHT CHECK THE CREW FOUND THE EMERGENCY EXIT LIGHTS SWITCH WAS IN THE ON POSITION. THE FLIGHT ATTENDANT REPORTED THAT THE EMERGENCY LIGHTS WERE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ALL EMERGENCY BATTERY PACKS IAW AMM 33-50-04. SERIAL NUMBERS: 104897, 72744, 103849 AND 62032. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COVER — LOOSE (CABIN DOOR) · airframe 28,489 hrs · 26,266 cycles

ON FLIGHT 3560 THE FLIGHT ATTENDANT REPORTED MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESECURED MAIN CABIN DOOR COVER IAW AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (NR 1 ENGINE) · airframe 2,819 hrs · 26,211 cycles

FOR FLIGHT 3545 ON POST FLIGHT SMOKE HAD BEEN COMING OUT OF THE NR 1 ENGINE FOR OVER 20 MINUTES. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED NR 1 ENGINE EXHAUST AREA FOUND NO OIL LEAKS. PERFORMED TAKEOFF POWER ENGINE RUN BN IAW EMB AMM 71-00-01 NO SMOKE NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (NR 1 ENGINE) · airframe 28,178 hrs · 26,049 cycles

ON FLIGHT 3906 THE CREW REPORTED AN ENGINE NR 1 FIRE DETECTOR FAIL MESSAGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF THE ENGINE FIRE DETECTOR SYSTEM IAW EMB 145 AMM 26-10-00 AND GENERAL VISUAL INSPECTION OF E1 FIRE DETECTOR IAW STANDARD MAINTENANCE PRACTICES AND ONE ENGINE START/STOP SEQUENCE. THE OPERATIONAL CHECK WAS GOOD NO DEFECTS NOTED. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 27,501 hrs · 25,531 cycles

ON FLIGHT 2897 THE CREW REPORTED THAT DURING THE CLIMB, RECEIVED A MAIN PITCH TRIM INOPERABLE MESSAGE ON ECAS. THE CAPTAIN ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND FIRST OFFICER’S PITCH TRIM SWITCH. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 27,074 hrs · 25,230 cycles

ON FLIGHT 3468 MAINTENANCE REPORTED THE CREW RECEIVED A SPOILER FAIL EICAS MESSAGE IN FLIGHT. MAI MAINTENANCE REPORTED THE CAPTAIN DECLARED AN EMERGENCY BUT THE CREW DID NOT CALL MOC TO REPORT THIS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF SPOILER SYSTEM IAW EMB 145 AMM 27-63-01-700-801-A THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CRACKED (LT PYLON) · airframe 30,533 hrs · 25,864 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT ENGINE FORWARD LOWER YOKE FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ENGINE FORWARD YOKE FITTING IAW AEA EO-EM-54MR-382. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIRE BOTTLE — DISCHARGED (LAVATORY) · airframe 26,635 hrs · 24,933 cycles

DURING PREFLIGHT INSPECTION FOR FLIGHT 3650 THE FLIGHT ATTENDANT DISCOVERED THE LAVATORY FIRE EXTINGUISHER BOTTLE INDICATOR IN THE RED ARC. THE FIRE EXTINGUISHER BOTTLE APPEARED TO HAVE BEEN DISCHARGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRE EXTINGUISHER BOTTLE IAW AMM 26-29-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 25,813 hrs · 24,263 cycles

ON FLIGHT 2741 THE FLIGHT ATTENDANT NOTIFIED THE CREW OF SMOKE IN THE CABIN. THE CREW PERFORMED AN EMERGENCY DESCENT AND TURNED OFF PACK 2. PACK 1 ALREADY DEFERRED. THE SMOKE STARTED TO DISSIPATE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW FIM 21-20-00-810-801-A REFERENCE TO LOG PAGE 2830534 ITEM 1 FOR DISCREPANCY FOUND. GROUND MAINTENANCE RAN ENGINE 1 AND ENGINE 2 IAW AMM 71-00-01, NO FURTHER SMOKE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (COCKPIT) · airframe 21,049 hrs · 20,236 cycles

ON FLIGHT 3574 - CREW REPORTED EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT JUMP SEAT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB AMM 33-50-15 OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 20,052 hrs · 19,441 cycles

ON FLIGHT 4186, DURING TAXI CREW REPORTS EMERGENCY EXIT SIGN LIGHT ABOVE FLIGHT ATTENDANT JUMP SEAT IS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. RESECURED EXIT SIGN CONNECTOR IAW AMM 33-50-14. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING IAW AMM 33-50-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UPLOCK — INOPERATIVE (RT MLG) · airframe 19,504 hrs · 18,896 cycles

ON FLIGHT 4122, CREW REPORTED RIGHT MAIN GEAR DID NOT INDICATE DOWN. CREW DECLARED EMERGENCY AND FOLLOWED AOM PROCEDURES ALL THREE GEAR IN THE GREEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB 145 AMM 32-33-10. ALL SUBSEQUENT OPERATIONAL CHECKS SATISFACTORY AND NR 8194; AIRCRAFT RETURNED TO SERVICE AND NR 8194; AND NR 8194;AND NR 8194;

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 18,923 hrs · 18,316 cycles

ON TAKEOFF ROLL, GOT TAKEOFF CONFIG WARNING SPOILERS 60 KTS. TROUBLESHOOT IAW FIM REMOVED AND REPLACED THE AURAL WARNING UNIT IAW 31-51-01. OP CHECK GOOD. ALSO, PERFORMED HIGH SPEED TAXI TO CONFIRM PROPER OPERATION. OPS GOOD AIRCRAFT RETURNED TO SERVICE.

Part: O-RING — FAILED (BLEED AIR)

E1 BLEED LEAK ON EICAS CREW CALLED MOC AND AGREED TO RETURN TO ORD DID NOT LAND OVERWEIGHT. FOUND LEAK IN UPPER CLAMP BEHIND CARGO WALL NR 1 SIDE. REMOVED AND REPLACED O-RINGS IAW EMB 145MM 36-11-10, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BALLAST — BURNED (CABIN)

BURNING SMELL COMING FROM FRONT VENT OVER FLIGHT ATTENDANT LIGHT CONTROL. REPLACED CEILING LIGHT BALLAST AT SEAT 1A. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: MODULE — OVERHEATED (CABIN LIGHTS)

BURNING SMELL IN GALLEY AFTER LANDING. REPLACED CABIN LIGHTING CONTROL MODULE IAW AMM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)

Part: FLAP SYSTEM — FAILED (RT WING)

DFW - FLT 3719 - FLAP FAIL AT 9 DEGREES, WOULD NOT MOVE IN EITHER DIRECTION. REPLACED RIGHT FLAP BRAKE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PROFILE — CRACKED (APU COWL)

DURING MBV INSPECTION FOUND APU COWL PROFILE CRACKED. REMOVED, MANUFACTURED, AND INSTALLED NEW PROFILE IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200504818) (K)

Part: SKIN — CRACKED (ELEVATOR)

DURING MBV INSPECTION FOUND LT ELEVATOR LWR SKIN SURFACE CRACKED BETWEEN STA 99.9 AND 1280.0. REPLACED LT ELEVATOR IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200504818) (K)

Part: SILL — CORRODED (FUSELAGE)

DURING MBV INSPECTION FOUND FORWARD CABIN FLOOR SILL RT CORRODED AROUND UPPER AFT NUTPLATE BETWEEN FRAMES 19 AND 20. REPAIRED RT FLOOR SILL IAW SRM. AC RETURNED TO SERVICE. (SW21200504818) (K)

Part: DOUBLER — CORRODED (CABIN FLOOR)

DURING MBV INSPECTION FOUND FORWARD CABIN FLOOR DOUBLER AT FRAME 22 CORRODED AROUND NUTPLATE. INSTALLED NEW DOUBLER AT FRAME 22 IAW SRM. AC RETURNED TO SERVICE. (SW21200504818) (K)

Part: GUSSET — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND FORWARD CABIN GUSSET BETWEEN FRAMES 20 AND 23 CORRODED ON UPPER SURFACE. REMOVED AND INSTALLED CABIN GUSSET IAW SRM. AC RETURNED TO SERVICE. (SW21200504818) (K)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING MBV INSPECTION FOUND FORWARD CABIN LT FWD IB SEAT TRACK CORRODED AROUND FASTENERS. REMOVED AND REPLACED LT FWD IB SEAT TRACK IAW MM. AC RETURNED TO SERVICE. (K)

Part: DOUBLER — CORRODED (CABIN FLOOR)

DURING MBV INSPECTION, FOUND FWD CABIN FLOOR DOUBLER AT FRAME 20 CORRODED AROUND AFT NUTPLATE. INSTALLED NEW DOUBLER AT FRAME 20 IAW SRM 51-40-02. AC RETURNED TO SERVICE. (SW21200504818) (K)

Part: RAMP — CORRODED (FLOOR SUPPORT)

DURING MBV INSPECTION FOUND FORWARD CABIN FLOOR SUPPORT RAMP AT FRAME 19 AND 20 CORRODED ON UPPER AND AFT EDGE. REMOVED AND INSTALLED RAMP IAW SRM. AC RETURNED TO SERVICE. (SW21200504818) (K)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - DURING AN IMBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED BELOW SRM LIMITS. REMOVED EXISTING DAMAGE CENTER SILL AND INSTALL NEW SILL IAW EMBL 145 SRM 145/1142 REV 21, CHAPTERS 51-40-02, 51-40-06, AND 51-20-03. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19L WAS FOUND TO BE CHAFED BELOW SRM LIMITS BETWEEN FRAME 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED A NDT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A REPAIR ANGLE, SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 21, CHAPTERS 53-24-02 FIGURE 201. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND CORROSION ON THE LEFT FLOORBEAM BETWEEN FRAMES 24 AND 25. REMOVED CORROSION BY PERFORMING A 4.5 INCH CUTOUT. FABRICATED A DOUBLER ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM 145/1142 REV 20, 53-21-10, AND STANDARD SRM PRACTICES. (M)

Part: SUPPORT BRACKET — CORRODED (PAX DOORWAY)

THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION PASENGER DOOR CUTOUT CENTER SILL SUPPORT BRACKETS (P/N 145-24131-007 AND 145-24131-009) SERVICEABLE CENTER SILL IAW EMB 145 SRM 51-40-02. (M)

Part: BEAM — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, GALLEY CROSSBEAM (P/N 145-29150-001) AND PROFILE (P/N 145-29150-003) HAVE CORROSION. INSTALLED SERVICEABLE CROSSBEAM AND PROFILE IAW EMB 145 SRM 51-40-06, 51-20-03 AND 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, THE LEFT FLOORBOARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE FLOORBOARD SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (GALLEY)

ABI - THIS IS A LEVEL TWO FINDING FOUND DURING AN IMBV INSPECTION, FORWARD SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (SERVICE DOOR)

ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV INSPECTION, SERVICE DOOR AFT SILL CORRODED. REMOVED AFT SERVICE DOOR SILL AND INSTALLED SERVICEABLE AFT SILL IAW EMB 145 SRM 51-40-002. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE RIGHT OMEGA BEAM TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB REPAIR STATEMENT GST-2864/01, AND GST-2811/01, AND EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE LEFT OMEGA BEAM AT FRAME TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION, MAINTENANCE FOUND THE FORWARD DIGITAL TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB REPAIR STATEMENT GST-2811/01 AND EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING MBV INSPECTION MAINTENANCE, FOUND THE CENTER OMEGA BEAM TO BE CORRODED. CORROSION WAS REMOVED AND AREA WAS REPAIRED IAW EMB REPAIR STATEMENT GST 2811/01 AND EMB SRM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: SMOKE — DETECTED (CABIN)

ORD - FLT 4109 - APPROX 5000 FT, LAVATORY SMOKE ON EICAS, F/A VERIFIED SMOKE. CAPTAIN COULD SEE SMOKE. DECLARED EMERGENCY RETURN TO ORD, EVACUATED ON RUNWAY BEFORE CFR COULD ARRIVE. SMOKE CLEARED EICAS MESSAGE WENT OUT. NO SOURCE OF FIRE COULD BE FOUND BUT THERE WAS DEFINITELY SMOKE. FOUND NR 1 ENGINE HAD OIL LEAK AND BAD FUEL NOZZLES. REMOVED AND REPLACED NR 1 ENGINE IAW EMB MCM 055006-400-801-A. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - FLT 4109 - EMERGENCY FLOOR LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED FIRST STRIP IN FRONT OF LAVATORY. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DFW - FLT 3658 - REAR PORTION OF EMERGENCY LIGHTING CAME ON. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY NR 4. OPS CHECK GOOD. (M)