N909AE

Part: PROXIMITY SWITCH — FAULTED (SPOILER SYS) · airframe 45,869 hrs · 42,380 cycles

EICAS SPOILER FAIL WITH SPOILER INDICATING OPEN IN CRUISE. APPLIED QRH, CLEARED AFTER 40 MINUTES. FOUND ONE OCCURANCE OF SPOILER IB FAIL ON CMC, T/S PER FIM 27-63-00-810-806-A. SUSPECT INTERMITTENT FAIL OF INBD PROXIMITY SWITCH. R & R THE LT & RT INBD PROXIMITY SWITCHES IAW AMM 27-63-01. OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 44,141 hrs · 40,384 cycles

RUDDER OVERBOOST EICAS MSG DURING CLIMB AT 400FT. C/W QRH RUDDER OVERBOOST & RUDDER 2 SYS INOP CHECKLIST (OVERBOOST MSG 400FT, 150-160 KNOTS. RUDDER 2 SYS INOP MSG AFTER SELECTING RUDDER 2 SYS SHUTOFF P/B) FACT 04FEB25 23:56 PHL T/S IAW FIM 27-22-00-810-803-A SUB TASK 817-001-A, OPS CHECK IAW AMM 34-13-00/400. COULD NOT DUPLICATE DISCRAPANCY. OPS CHECK GOOD, A/C OK FOR SERVICE AT THIS TIME.

Part: ENGINE — FAULTED (NR 1) · airframe 43,911 hrs · 40,136 cycles

LOUD BANG ENG 1 OUT MESSAGE. NO N2 ROTATION. R & R #100 ENG IAW W/C 71-00-0. OPS CHECK GOOD.

Part: DUCT — PUNCTURED (ZONE 200)

SMOKE IN AIRCRAFT AT FL300. EMERGENCY DECLARED. AIRBORNE SMOKE WAS IN CABIN AND FLT DECK UNKNOWN SOURCE. MEL 14AUG24 01:39 SYR C22718 21-15-2 AIR CONDITIONING PACKS C/W FLT CREW PROCEDURES. TROUBLESHOOT SMOKE IN CABIN AND PACK 1 SHUTDOWN.FOUND Y-DUCT AT DUAL HEAT EXCHANGER WITH HOLE AND SMOKE RESIDUIE IN PACK 1 PANEL WITH BLOW DUCT AT CONDENSER.REMOVED AND REPLACED PACK 2Y-DUCT IRW AMM 21-60-01. REMOVED AND REPLACED DUCT IN PACK 1 IRW AMM 21-51-04 RUN PACKS 10MINS NO SMOKE OR SHUTDOWN.OPS CHECK GOOD OK FOR SERVICE AT THIS TIME,CLEAR MEL 21-15-02.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2264 CORROSION ON CARGO DOOR ENTY TEE LOWER AT FR68. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2251 CORROSION ON T PROFILE AT FR65. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,990 hrs · 37,940 cycles

49-2186 CRACK ON APU RH AUXILIARY LINK UPPER ATTACHMENT DOUBLER. R&R'D IAW SRM 51-40-02 MANUFACTURED REPLACEMENT DOUBLER IAW SRM53-23-13

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2165 CRACK ON CF4 LH SHEAR CLIP AT FR61, STR6-7L. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2166 CRACK ON CF4 RH SHEAR CLIP AT FR61, STR6-7R. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2154 CRACKED FWD FUSELAGE 2, RH OVERHEADE SIDE FRAME ABOVE FLT DECK. R&R'D FRAME IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2163 CRACK ON CF4 LH SHEAR CLIP AT FR58, STR15-16L. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2164 CRACK ON CF4 LH SHEAR CLIP AT FR60, STR15-16L. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2137 CORROSION ON LOWER SKIN AND BUSHING AT FR75, 1" BELOW STR20L. REPAIRED IAW EO1-53-23-0421

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2080 CRACK ON SHEAR CLIP AT FR68, STR6-10R. REEPAIRED IAW EO1-53-23-0438

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2099 CRACK ON CF2 LH SHEAR CLIP ATFR25, STR15-16L. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2082 CRACK ON SHEAR CLIP AT FR68 STR6-9L. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2111 CRACK ON CF1 RH SHEAR CLIP AT FR16, STR15-16R. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2087 CRACK ON SHEAR CLIP AT FR73, STR16-17L

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2100 CRACK AT CF2 LH SHEAR CLIP AT FR28, STR15-16L. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2077 CORROSION ON BAG DOOR LOWER CUT-OUT LOWER BEAM

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2074 CORROSION ON CF2 SILL #2 BETWEEN FR30-35. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2088 CORROSION ON L-SHAPE AT FR65. REPAIRED IAW EO1-53-23-0434

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2091 CORROSION ON RH SILL AT BETWEEN FR71-73. REPLACED IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2081 CRACK ON SHEAR CLIP AT FR67 UPPER FLOOR FR67, STR6-7L . REPALACE IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

CRACK ON CF2 CENTER OMEGA BEAM NR 1 VERTICAL FLANGE AT FRM 28. REPAIRED IAW EO1-53-23-0418.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2095 CRACK ON CF2 RH SHEAR CLIP AT FR24. STR15-16R. R&R'D IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2108 CORROSION ON RH SERVICE DOOR FWD SILL AT FR18-20. RAPAIRED IAW EO1-53-23-0416

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2098 CRACK ON CF2 RH SHEAR CLIP AT FR25, STR15-16R. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2096 CRACK ON CF2 RH SHEAR CLIP AT FR24, STR16-17R. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2092 COSSION ON RH SILL AT BETWEEN FR68-71. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2113 3 CRACKS ON CF1 LH OMEGA BEAM #1 FLOOR STRUCTURE AT FR18-24. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2097 CRACK ON CF2 LH SHEAR CLIP AT FR24, STR15-16L. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2085 CRACK ON SHEAR CLIP AT FR71, STR17-18L. R&R'D IAW SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2094 CRACK ON BAG DOOR MECHANISM BRACKET AT FR61. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2089 COSSION ON L-SHAPE AT FR68. REPASIRED IAW EO1-53-23-0434

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2086 CRACK ON SHEAR CLIP AT FR72, STR16-17L. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2110 3 CRACKS ON CF1 AFT DIGITAL FLOOR STRUCTURE AT FR17-18. R&R'D IAW SRM51-40-20

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2073 CORROSION ON CF2 RH SILL #1 BETWEEN DR24-29. R&R'D IAW SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 41,991 hrs · 37,940 cycles

53-2054 CORROSION ON RH OMEGA BEAM TOP GUSSET AT FR59-61. REPAIRED IAW EMB145 AMM 20-10-01 AND SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2060 CRACK ON CF3 LH OMEGA BEAM AT WING BOX. REPLACE IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2061 CRACK ON LH OMEGA BEAM AFT OB ANGLE AT WING BOX.R&R'D IAW EMB 145 SRM 53-23-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2064 CRACKS ON CF2 LH OMEGA BEAM #3 VERTICAL FLANGE AT FR31,32, AND 33. R&R'D IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2067 CRACKS ON CF3 LH OMEGA BEAM AT FR36,37,AND 38. R&R'D IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2062 CRACKS ON CF2 OMEGA BEAM #2 VERTICAL FLANGE AT FR24,25,26,27, AND 28. REMOVED AND REPLACED IAW EMB145 SRM 51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2059 CRACK ON CF3 RH OMEGA BEAM , AFT IB ANGLE AT CENTER BOX. REMOVED AND REPLACED IAW EWMB145 SRM 53-23-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2020 CRACKS ON FUSELAGE SKIN AT FR77-79, STR5-9L. REPAIRED IAW EO1-53-23-0432

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2021 CRACKS ON FUSELAGE SKIN AT FR78-80, STR4-9R. REPAIRED IAW EO1-53-23-0432

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,991 hrs · 37,940 cycles

53-2052 CRACK ON FLOOR STRUCTURE AT RH OMEGA BEAM TOP DOUBLER FR57. REPLACED IAW EMB145 SRM51-40-02

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,257 hrs · 37,084 cycles

BLEED 1 LEAK INDICATION ON CLIMB AT 2500FT RAN QRH MSG WENT AWAY. T/S #1 BLEED LEAK FOUND #1 ENG PYLON Y-PIPE LEAKING. INSPECTED Y-PIPE AND CLAMPS WITH NO DEFECTS NOTED. RE-INSTALLED PIPE AND CLAMPS AS REQ. OPS AND LEAK CHECK GOOD. A/C OK FOR SERVICE AT THIS TIME

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 41,225 hrs · 37,053 cycles

4C ESCUTION CRACKED.-C/A-RAR 4C ESCUTION IN REFERENCE WITH CMM 25-20-63. END.

Part: LAMP — INOPERATIVE (AFT) · airframe 41,186 hrs · 37,023 cycles

AFT CEILING EMERGENCY LIGHT INOP-C/A-RAR AFT CEILING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. OPC GOOD. END.

Part: LAMP — INOPERATIVE (SD) · airframe 41,186 hrs · 37,023 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPC GOOD. END.

Part: FILTER — DIRTY (NR 1 FAN AIR VLV) · airframe 40,871 hrs · 36,707 cycles

CREW DECLARED EMERGENCY FOR BLEED1 TEMP AND ANTI ICE FAIL REMOVED AND CLEANED #1 FAN AIR VALVE FILTER AND RE INSTALLED FILTER IAW EMB-145 AMM 36-11-07. PERFORMED OPS CHECKS WITH CREW IAW AMM 30-00-00 OPS CHECKS GOOD NO MESSAGE NOTED AT THIS TIME A/C OK FOR SERVICE

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 40,848 hrs · 36,686 cycles

DURING PS-2 CHECK FOUND RH SERVICE DOOR EMERGENCY LIGHT INOP.-C/A-FOUND LAMP BLOWN. RAR IAW EMB-145 AMM 33-50-10. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: NONE — NONE · airframe 40,511 hrs · 36,329 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-RAR SERVICE DOOR EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECK GOOD. END.

Part: BLEED AIR SYS — CRACKED · airframe 40,192 hrs · 35,922 cycles

BLEED 1 TEMP IN RED IN ICING CONDITIONS EXITED ICING BEFORE WARNING MSG APPEARED.#2 E2 BLEED AIR PRE-COOLER CRACKED.-C/A-RAR E1 FAN AIR VALVE THERMOSTAT OUTLET HOSE IAW EMB 145 AMM 36-11-06. OP CHECK GOOD IAW EMB-145 AMM 36-00-00 REF NRWC 909-ORD-06439 AND RAR E2 PRECOOLER IAW EMB 145 AMM 36-11-04. OPS TEST GOOD IAW EMB 145 AMM 36-00-00 REF NRWC # 909-ORD-06442 FOR WORK ACOMPLISHED

Part: NONE — BROKEN (AFT) · airframe 39,585 hrs · 35,232 cycles

AFT CABIN EMERGENCY FLASHLIGHT BRACKET BROKEN-C/A-RAR CABIN EMERGENCY FLASHLIGHT BRACKET ASSY IAW EMB 145 AMM 33-50-16.

Part: NONE — NONE · airframe 39,286 hrs · 34,898 cycles

BOTH OVERWING EMERGENCY EXIT SIGNS AND FLOOR STRIP INOP-C/A-RAR #5 EMERGENCY LIGHT DC/AC INVERTER IAW EMB 145 AMM 33-50-11. OPC GOOD

Part: NONE — NONE · airframe 38,638 hrs · 34,137 cycles

FORWARD FA FLASHLIGHT INOP-C/A-RAR FWD FA FLASHLIGHT IAW ETN-EM-33-059, OPC GOOD NO DEFECTS NOTED AT THIS TIME

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,077 hrs · 33,456 cycles

RH EXTERIOR OVERWING EMERGENCY LIGHT IS INOP-C/A-RAR RH EXTERIOR OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-07. OPC GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,052 hrs · 33,432 cycles

RH AFT OVER WING EMERGENCY LIGHT INOP-C/A-RAR RH AFT OVER WING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10. OPC GOOD.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 38,001 hrs · 33,375 cycles

RH OVERWING EMERGENCY LIGHT IS INOP.-C/A-RAR RH OVERWING EMERGENCY LIGHT IAW EMB145 AMM 33-50-10. OPC GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,966 hrs · 33,342 cycles

DURING PS-1 CHECK FOUND RH CENTER FAIRING EXTERIOR EMERGENCY LIGHT INOP-C/A-RAR EMERGENCY EXTERIOR LIGHT PER AMM 33-50-10

Part: FITTING — CRACKED (RT NACELLE) · airframe 37,692 hrs · 33,068 cycles

RH ENGINE FORWARD LOWER YOKE-PYLON FORWARD LINKAGE FITTING IS CRACKED. -C/A-IN REFERENCE TO WIP #15. C/W REPAIR OF RH FWD LOWER PYLON YOKE LINKAGE FITTING IAW ERS-EM-54MR-698-2 AND ERS-EM-5400-873.

Part: LINKAGE — CRACKED (LT ENG YOKE) · airframe 37,692 hrs · 33,068 cycles

LEFT ENGINE FORWARD LOWER YOKE-PYLON FORWARD LINKAGE IS CRACKED.-C/A-COMPLETE: REPAIRED LH ENGINE FORWARD LOWER YOKE PYLON LINKAGE FITTING IAW ERS- EM-54MR-698 AND ERS-EM-5400-874

Part: FITTING — CRACKED (PYLON LINKAGE) · airframe 37,692 hrs · 33,068 cycles

RIGHT ENGINE FORWARD LOWER YOKE-PYLON FORWARD LINKAGE FITTING IS CRACKED-C/A-REPAIRED IAW ERS-EM54MR-698.

Part: NUT PLATE — DAMAGED (FRAME 65) · airframe 37,692 hrs · 33,068 cycles

FRAME 65 HAS AN ELONGATED NUTPLATE HOLE ON RH SIDE.-C/A-REPAIRED IAW ERS-EM-53MR-4299.

Part: FRAME — CHAFED (FRM 65 S11-12R) · airframe 37,692 hrs · 33,068 cycles

FRAME 65 IS CHAFED ON INBOARD SIDE BETWEEN STRINGERS 11R AND 12R. REPAIRED FRAME 65 BETWEEN STR 11R AND 12R IAW ERS-EM-53MR-4295.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 37,692 hrs · 33,068 cycles

LEFT SIDE VERT STAB DRAG ANGLE APPEARS TO HAVE 1 CRACK APPROX. 1' LONG.-C/A-RAR DRAG ANGLE SECTION IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FRAMES 47-48) · airframe 37,692 hrs · 33,068 cycles

R/H HAT BEAM ANGLE SUPPORT IS CRACKED BETWEEN FRAMES 47-48.-C/A-REPLACED RH HAT BEAM ANGLE SUPPORT IAW SRM 53-23-02.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 37,692 hrs · 33,068 cycles

RIGHT SIDE VERT STAB DRAG ANGLE APPEARS TO HAVE 2 CRACKS APPROX. 1/2" LONG.-C/A-RAR DRAG ANGLE AND REINSTALLED REPAIR DOUBLER IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FRAMES 19-20) · airframe 37,692 hrs · 33,068 cycles

SSI , LT OMEGA BEAM SUPPORT ANGLE IS CRACKED BETWEEN FR 19A AND FR 20 AT FLOOR LEVEL -C/A-RAR LH OMEGA BEAM SUPPORT ANGLE BETWEEN FR 19A AND FR 20 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 15-18) · airframe 37,692 hrs · 33,068 cycles

CPCP ITEM , 2 EA FLOOR PNL SUPPORT ANGLES ARE CORRODED AT PAX DOOR CUTOUT BETWEEN FR 15 AND FR 18 AT STR 15 LT -C/A-REMOVED AND REPLACED 2 EA PAX DOOR FLOOR SUPPORT ANGLES BETWEEN FR15 AND FR18 STR 15L IAW SRM 51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,692 hrs · 33,068 cycles

R/H #1 AND #8 EMERGENCY LIGHT EXTRUSION DAMAGED.-C/A-COMPLETE:INSTALLED NEW R/H #1 AND #8 EMERGENCY LIGHT EXTRUSION IAW EMB 145 AMM 33-50-12.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 37,611 hrs · 32,988 cycles

PRESSURIZATION FAILURE ON DEPARTURE -AIR RETURN CABIN P. CLIMBED TO 10,000+ PUT ON OX MASKS (BOTH OF US) DESCENDED TO 10,00, CABIN KEPT CLIMBING, WAS IN RED. THEN DESCENDED SLOWLY BACK DOWN TO NORMAL LEVELS. C/A-R & R PNEUMATIC AND ELECTRO PNEUMATIC OUTFLOW VALVES IAW EMB-145 MM 21-31-04 AND EMB-145 MM 21-31-03. OPC GOOD. REF NRWC 909-ORD-05388.

Part: DETECTOR — MALFUNCTIONED (ANTI-ICE) · airframe 37,611 hrs · 32,988 cycles

ICE COND- A/I INOP EICAS MESSAGE APPEARED 3 TIMES WITHIN 30 MINUTES ON THE GROUND AND AS WE TOOK THE RUNWAY- ABORTED TAKEOFF-C/A-RAR L/H ICE DETECTOR IAW EMB AMM 30-80-01 OPC GOOD NO FURTHER DEFECTS NOTED AT THIS TIME

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,542 hrs · 32,918 cycles

DURING PS-2 WALKAROUND, FOUND RT WING TO FUSELAGE FAIRING EXTERNAL EMERGENCY LIGHT TO BE INOPERABLE. C/A: R & R RT WING TO FUSELAGE FAIRING EXTERNAL EMERGENY LIGHT, IAW EMB 145 AMM 33-50-10. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: INVERTER — FAILED (CABIN) · airframe 36,367 hrs · 31,757 cycles

DURING PS-2 CHECK FOUND EMERGENCY LIGHT STRIP #1 AND SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED EMERGENY INVERTER #2 IAW 145 AMM 33-50-11 OPS-CHECK NO FURTHER DEFECTS NOTED AT THIS TIME

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,314 hrs · 31,701 cycles

FWD FLOOR PROXIMITY STRIP INOP TRANSFER TO NRWC # 909-MIA-04782-C/A-REPLACED FWD FLOOR PROXIMITY STRIP (EMERGENCY LIGHT) IAW AMM 33-50-12. OPS CK OK.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 36,199 hrs · 31,595 cycles

LEFT FWD EXT EMERGENCY LIGHT INOP-C/A-REPLACED THE LEFT FWD EXTERIOR EMERGENCY LIGHT ASSY IAW AMM 33-50-07. NO FIX. REMOVED AND REPLACED #1 EPSU AND BATTERY IAW AMM 33-50-04 OPC GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 80809

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,163 hrs · 31,563 cycles

LH FWD WING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH FWD WING EMERGENCY LIGHT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. END.

Part: BATTERY PACK — INOPERATIVE (EXTERNAL LIGHT) · airframe 35,736 hrs · 31,127 cycles

LH FWD EXTERNAL EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH EXTERNAL EMERGENCY LIGHT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A NO FIX T/S WITH WM 33-50-50 FOUND BATTERY #1 AND CHARGER INOPERATIVE REMOVED AND REPLACED BATTERY #1 AND CHARGER IAW W/C 33-700-19 OPC GOOD END. CHARGER ASSY BATTERY P/N BA5-0933-901 S/N C03023

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,169 hrs · 30,590 cycles

RT AFT EXTERIOR EMERGENCY LIGHT BAD. C/A-R&R RT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,994 hrs · 30,410 cycles

R/H UPPER EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECKED.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 34,622 hrs · 30,076 cycles

LAVATORY SMOKE WHILE AT GATE AND PAX INSIDE. QRH PROCEDURE C/W. BREAKERS PULLED. ELECTRICAL ODOR INSIDE. REMOVED AND REINSTALLED FLOOR PANEL 272AF IAW AMM 53-01-03 TO INSPECT FOR REPORTED ELECTRICAL SMELL UNDER LAV. REF NRWC 909-ORD-04222 AND NRWC 909-ORD-04223 FOR INSPECTION AND OPS CHECKS OF LAV AND SURROUNDING AREAS. COULD NOT DUPLICATE NO DEFECTS NOTED

Part: UNKNOWN — ODOR (COCKPIT) · airframe 34,570 hrs · 30,027 cycles

OIL SMELL IN FLIGHT DECK FROM TOP OF DESCENT TO THE GROUND. C/W ETN-EM-72-034. PERFORMED VISUAL INSPECTION FOR PRESENCE OF OIL AFT OF FAN BLADES ON STRUTS AND LOWER INSIDE OF INNER BYPASS AND OPENED WASH PORT NO EVIDENCE OF OIL FOUND. C/W WORK SCOPE FROM TECH SUPPORT, PERFORMED ETN-EM-72-034, NO OIL LEAKS,ODORS OR OTHER DEFECTS NOTED.

Part: BRAKE — LEAKING (MLG) · airframe 34,504 hrs · 29,957 cycles

3767 DFW-SGF N909 SMOKING BRAKES WHILE LANDING NUMBER 2 BRAKE LEAKING FLUID HE DID NOT DECLARE EMERGENCY BUT CFR FOLLOWED HIM INTO GATE. C/A-RAR #2 BRAKE IAW W/C 32-600-14 OPC AND LEAK CHECK GOOD.

Part: LEVER — BINDING (PARKING BRAKE) · airframe 34,276 hrs · 29,735 cycles

PARKING BRAKE LEVER GETS HUNG UP AND IS HARD TO SET-C/A-CLEANED AND LUBED PARKING BRAKE LEVER PEREMB 145 MM12-12-00. NO DEFECTS NOTED

Part: STRUT — LOW (NLG) · airframe 34,071 hrs · 29,523 cycles

LG AIR/GND ON TAKE OFF COULDNT RETRACT LANDING GEAR. C/A-FOUND NOSE LG STRUT TO BE BELOW LIMITS. SERVICED NOSE LG STRUT IAW WC 32-600-06. PERFORMED OPS CHECK OF LG IAW AMM 32-34-00 OPS CHECK GOOD. T/S IAW FIM 32-63-00. PERFORMED OPC GOOD OF LANDING GEAR IAW AMM 32-34-00. LANDING GEAR PROX SWITCHES FUNCTIONAL CHECK GOOG IAW WC 32-700-12. NO DEFECTS NOTED.

Part: PANEL — DAMAGED (MAIN DOOR) · airframe 34,071 hrs · 29,522 cycles

EMERGENCY LIGHT PANEL ON MAIN DOOR DAMAGED. C/A-REMOVED AND REPLACED EMERGENCY LIGHT PANEL ON MAIN DOOR, OPC GOOD, IAW AMM 25-23-04.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,734 hrs · 29,223 cycles

DURING PS-1 CHECK, FOUND AFT EXTERIOR EMERGENCY LIGHTS INOP. C/A- REMOVED AND REPLACED BATTERY HOLDER ASSEMBLY AND BATTERY CHARGER ASSEMBLY IAW AMM 33-50-04. OPS CHECK FAIL. NO FIX. DEFERRED PER MEL. FOUND NR 1 FUSE ON POWER SUPPLY BLOWN. REMOVED AMD REPLACED FUSE IAW CMM 25-60-03. REMOVED AND REPLACED LT CENTER FAIRING EMERGNCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 33,683 hrs · 29,164 cycles

LT AND RT OVER WING EXTERIOR EMERGENCY LIGHTS INOP. C/A-TROUBLE SHOT LT AND RT OVER WING EXTERIOR EMERGENCY LIGHTS IAW WM 33-50-50. FOUND NR 4 EMERGENCY BATTERY TO BE BAD. REMOVED AND REPLACED NR 4 EMERGENCY BATTER AND NR 4 EMERGENCY BATTERY CHARGER IAW W/C 33-700-19. OP CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. END. BATTERY CHARGER ASSY P/N 11-0049 S/N 12811.

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 33,431 hrs · 28,896 cycles

LH AND RH OVERWING EMERGENCY LIGHTS INOP-C/A-REMOVED AND REPLACED #4 EPSU BATTERY PACK AND CHARGER, OPS CHECK GOOD IAW EMB AMM 33-50-04. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 101787

Part: BATTERY PACK — INOPERATIVE (EMEGENCY LIGHT) · airframe 33,424 hrs · 28,890 cycles

LH OVERWING EMERGENCY LIGHT INOP-C/A-REMOVED AND REPLACED LH OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A. NO FIX. TROUBLE SHOT IN REFERANCE WITH WM 33-50-50 FOUND #4 POWER SUPPLY AND BATTERY TO BE BAD. RAR #4 POWER SUPPLY AND BATTERY IN REFERANCE WITH W/C 33-700-19. CHARGER ASSY BATTERY P/N BA5-0933-901 S/N C02264

Part: PRESSURE SWITCH — FAILED (RUDDER SYSTEM) · airframe 33,384 hrs · 28,849 cycles

RUDDER SYS 1-2 INOP OVER 180 KNOTS. DID NOT HAVE AN OVERWEIGHT LANDING.-C/A-REF FIM 27-22-00-810-804-A, RPL'D SYS 2 RUDDER PERSSURE SW IN REF TO AMM 27-23-04 & OPS CHKED RUDDER SYS OK IN REF TO AMM 27-23-00. NO FAULT & LEAK FOUND.

Part: SKIN — DAMAGED (RUDDER) · airframe 33,380 hrs · 28,846 cycles

RUDDER 1 TOP SKIN SURFACE HAS AREAS OF DAMAGE. R&R RUDDER I TOP SKIN/RIB IAW SRM 51-40-02.

Part: DOOR FRAME — CORRODED (FRAMES 65-68) · airframe 33,380 hrs · 28,846 cycles

FWD LOWER CORNER OF AFT CARGO DOOR CUTOUT HAS CORROSION.-C/A-REMOVED AND REPLACE D CARGO DOOR SILL IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FRAMES 67-68) · airframe 33,380 hrs · 28,846 cycles

SUPPORT BRACKET FOR CARGO DOOR TORSION BAR/CABLE DRUM BETWEEN FRAMES 67-68 HAS 1/4 " CRACK -C/A-REMOVED AND REPLACED SUPPORT BRACKET FOR CARGO DOOR TORSION BAR/CABLE DRUM BETWEEN FRAMES 67-68 IAW SRM 51-40-02.

Part: LIGHT — CRACKED (CABIN) · airframe 33,380 hrs · 28,846 cycles

NR 6 FLOOR LIGHTING STRIP IS CRACKED AT THE HOLES. C/A-COMPLETE:INSTALLED NEW NR 6 FLOOR LIGHT STRIP IAW AMM 33-50-12.

Part: APU — FIRE (APU BAY) · airframe 33,380 hrs · 28,846 cycles

TRANSFERRED FROM AML PAGE 4399798/1 - REF TDMI 909T4951. APU FIRE COWL LEAVING RIVET HEAD MARKS ON APU FIREWALL AND FRAME BOTTOM. SEE NRTC E520460. E WESTFALL 437731. REF LOG PAGE 4030028 ITEM 3. C/A-COMPLETE:C/W PERM REPAIR APU FIREWALL IAW ERS-EM-49MR-074. TDMI RESTORED, SEE AIRCRAFT LOG PAGE 4399798 ITEM 1 FOR BAL. ENTRY.

Part: LIGHT — CRACKED (CABIN) · airframe 33,380 hrs · 28,846 cycles

1 EACH EMERGENCY LIGHT STRIP CRACKED. C/A-COMPLETE:INSTALLED 2 EACH NEW FLOOR PROXIMITY LIGHT STRIPS ON LIGHT STRIP EXTRUSION IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 33,380 hrs · 28,846 cycles

NR 8 FLOOR LIGHT STRIP HAS A BROKEN WIRE. C/A-COMPLETE:INSTALLED NEW FLOOR PROXIMITY LIGHT STRIP ON AIRCRAFT IAW AMM 33-50-12.

Part: LIGHT — CRACKED (CABIN) · airframe 33,380 hrs · 28,846 cycles

NR 4 FLOOR LIGHT STRIP IS CRACKS BY THE HOLES. C/A-COMPLETE:INSTALLED NEW NR 4 FLOOR LIGHT STRIP IAW AMM 33-50-12.

Part: LIGHT — CRACKED (CABIN) · airframe 33,380 hrs · 28,846 cycles

NR 5 FLOOR LIGHT STRIP IS CRACKS BY THE HOLES. C/A-COMPLETE: INSTALLED NEW EMERGENCY LIGHT STRIP FOR NR 5 POSITION IAW 33-50-12.

Part: ACM — FAILED (AC BAY) · airframe 33,165 hrs · 28,641 cycles

NR 1 PACK PRODUCED A METALIC ODOR IN FLT. PACK THEN FAILED TO PRODUCE COLD AIR. CABIN 27 DEGREES C, COCKPIT 28 DEGREES C. R&R LT AIR CYCLE MACHINE IAW AMM 21-51-03 OPERATIONAL AND LEAK CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 32,643 hrs · 28,118 cycles

FA FLASHLIGHT INOPERATIVE. R & R THE FA FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 31,841 hrs · 27,382 cycles

CABIN ALTITUDE WARNING AT FL 250. TROUBLESHOT AND FOUND THE AUTO PRESSURIZATION DIGITAL CONTROLLER DISPLAY ELEVATION SWITCH TO BE STICKING. SUSPECT DIGITAL CONTROLLER IS BAD. REPLACED DIGITAL CONTROLLER IAW AMM 21-31-01-000-801-A, & 21-31-01-400-801-A. PERFORMED FNC OF PRESSURIZATION CONTROL IN AUTO IAW 21-31-00-700-802-A. OPS CHECKED NORMAL.

Part: STATIC INVERTER — INOPERATIVE · airframe 31,590 hrs · 27,130 cycles

115 BUS OFF EICAS TWICE IN FLT, DIVERTED. INVERTER INOPERATIVE. REMOVED AND REPLACED AC STATIC INVERTER IAW AMM 24-20-01 OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,574 hrs · 27,116 cycles

L/H OVERWING EMERGENCY LT INOP-C/A-REMOVED AND REPLACED L/H OVERWING EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A..OPC GOOD AT THIS TIME.END.

Part: MODULE — FAILED · airframe 31,266 hrs · 26,821 cycles

DURING TAXI, SHUTDOWN THE NR 2 ENGINE, GEN 1, GEN 3, GENERATORS OVERLOADED, APU GEN NEVER CAME ONLINE AFTER START, EICAS SHOWED ELEC EMER ABNORMAL, COULD NOT SHUT DOWN BATTERIES MANUALLY. WAS TOWED TO THE GATE. REMOVED AND REPLACED OVERHEAD PANEL ELECTRICAL, PERFORMED AN OPS CHECK AND FOUND WORKING PROPERLY IAW AMM 24-00-01 AND 24-00-00

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 30,818 hrs · 26,361 cycles

NR 2 ENGINE ANTI-ICE FAILED IN FLIGHT. REMOVED AND REPLACED THE ENGINE ANTI-ICE VALVE IAW AMM 30-21-01 AND R & R THE ENGINE ANTI-ICE PRESSURE TRANSDUCER IAW AMM-30-21-06.

Part: CLAMP — FAILED (ANTI-ICE VALVE) · airframe 30,817 hrs · 26,360 cycles

NR 2 ENGINE ANTI-ICE VALVE CYCLING OPEN AND CLOSE. SHOULD BE OPEN. FOUND THE TUBE ASSY DOWN STREAM OF NR 2 ENGINE ANTI-ICE VALVE LOOSE. SECURED THE TUBE ASSY WITH A NEW CLAMP UNLOCKED VALVE AND OPS CHECKED IAW AMM 30-21-00.

Part: VALVE — LEAKING (NR 1 A/C PACK) · airframe 30,587 hrs · 26,100 cycles

NR 1 BLEED LEAK AT 6000 FT MESSAGE ACTIVATED. DISAPEARED AFTER 5 MINUTES. REPLACED AND REMOVED THE NR 1 PACK VALVE TO HEAT EXCHANGER DUCT SLEEVE AND CLAMPS IAW ETN-EM-21-056. PERFORMED OPS CHECK OF THE NR 1 BLEED SYSTEM FOUND WORKING PROPERLY. NO LEAKS NOTED IAW AMM 36-00-00.

Part: UNKNOWN — UNKNOWN (FUSELAGE) · airframe 30,554 hrs · 26,063 cycles

THUMPING NOISE IN COCKPIT DURING CLIMB AND CRUISE. REPAIRED LEFT FWD FUSELAGE IAW SRM 53-10-01.

Part: BRAKE — LEAKING (NR 1) · airframe 30,465 hrs · 26,004 cycles

NR 1 BRAKE LEAKING. REMOVED AND REPLACED THE BRAKE IAW W/C 32-600-14. LEAK CHECKED GOOD.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,444 hrs · 25,991 cycles

AFT CEILING EXIT LOCATING SIGN LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,026 hrs · 25,585 cycles

MAIN ENTRY EMERGENCY LIGHT LAMP INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A, AND 33-50-10-400-801-A. OPS CHECKED GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 29,176 hrs · 24,852 cycles

HYD SYS NR 2 FAIL IN FLIGHT. REMOVED AND REPLACED THE NR 2 ELECTRIC HYD PUMP IAW AMM 29-10-04, OPS AND LEAK CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-25) · airframe 28,806 hrs · 24,516 cycles

CABIN CENTER OMEGA BEAM CORRODED AT NUTPLATE HOLE JUST FWD OF CENTER AISLE CROSSBEAM BETWEEN FRAMES 24-25. PERFORMED REPAIR OF CABIN CENTER OMEGA BEAM AT NUTPLATE HOLE JUST FWD OF CENTER AISLE CROSSBEAM IAW SRM 53-22-10.

Part: ANGLE — CRACKED (FRAMES 47-48) · airframe 28,806 hrs · 24,516 cycles

RIGHT OMEGA BEAM INBD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. REPAIRED IAW SRM 53-23-02, 51-20-03, AND 51-40-02.

Part: DOOR SILL — CORRODED (FRAMES 65 - 68) · airframe 28,806 hrs · 24,516 cycles

CARGO DOOR CUTOUT LOWER SILL CORRODED. REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL IAW SRM 51-40-02

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 28,806 hrs · 24,516 cycles

CARGO DOOR CUTOUT FRAME 65 SHEAR TIE CORRODED AT LOWER END. REPAIRED THE SHEAR TIE IAW SRM 53-31-04 AND ETN EM-53-272

Part: CROSSBEAM — CORRODED (FRAME 20) · airframe 28,806 hrs · 24,516 cycles

FRAME 20 AISLE CROSSBEAM CORRODED. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 53-21-10 AND ETN-EM-53-139 R4.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,620 hrs · 24,349 cycles

MEL 33-30, AUTH 060290-C SEAT 1A EMERGENCY FLOOR STRIP INOPERATIVE. EMERGENCY FLOOR STRIP AT SEAT 1A IAW AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. OPS CHECKS GOOD AT THIS TIME, MEL RESTORED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,583 hrs · 24,311 cycles

SEAT 1A EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. DEFERRED SEAT 1A EMERGENCY LIGHT FLOOR STRIP IAW MEL 33-30. R&R EMERGENCY FOOR STRIP AT SEAT 1A IAW EMB AMM 33-50-12-000-801-A AND 33-50-12-400-801-A. OPS CHECKS GOOD AT THIS TIME MEL RESTORED.

Part: AIR DUCT — DEFECTIVE (BLEED AIR SYS) · airframe 28,479 hrs · 24,229 cycles

IN CLIMB WING ANTI-ICE FAIL ON EICAS, NO OPEN INSCRIPTION, RAN CHECKLIST CYCLED SWITCH, NO EFFECT. FLIGHT ATTENDANT REPORTED ICE ON ENGS WITH NO INDICATION OF ICE CONDITIONS AFTER CLEARING INITIAL ICE CONDITIONS. R & R NR 2 HEAT EXCHANGER DUCT ASSEMBLY & GRATE ASSEMBLY & NR 2 BLEED AIR DUCT IAW AMM 53-04-01 & AMM 36-11-09. ALSO PERFORMED OPERATIONAL CHECK OF WING ANTI-ICE & ENG ANTI-ICE FOUND WORKING PROPERLY IAW AMM 30-11-00 & AMM 30-21-00.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,712 hrs · 21,730 cycles

FLASHLIGHT HOLDER AFT CABIN IS BROKEN. R & R AFT CABIN FLASHLIGHT CRADLE IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: THERMOSTAT — FAULTY (BLEED AIR SYS) · airframe 25,665 hrs · 21,688 cycles

BLEED 2 OVER TEMP DURING CLIMB THRU 10000 FT IN ICING CONDITIONS, REF FIM 36-11-00-810-804. PERFORMED INSPECTION GVI OF PRE COOLER REGION IAW AMM 36-11-04. CLEANED FAN AIR VLV FILTER AMM 36-11-03. R & R FAN AIR THERMOSTAT IAW AMM 36-11-06. OPERATIONS CHECKED IAW TASK 36-00-00-700-803, DID NOT FIX SEE ITEM BELOW.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,463 hrs · 21,525 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,417 hrs · 21,489 cycles

LEFT AFT EXT EMER EXIT LIGHT INOPERATIVE. R & R LT FUSELAGE AFT EXT EXIT LIGHT LAMP IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 25,136 hrs · 21,232 cycles

LAVATORY SMOKE ON EICAS, NO EVIDENCE OF FIRE OR SMOKE. LAVATORY SMOKE TEST WILL NOT TEST. PERFORMED LAVATORY SMOKE DETECTOR RESET FOLLOWED BY OPERATIONS CHECK & FOUND WORKING OK IAW AMM 26-14-00.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,987 hrs · 21,119 cycles

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

Part: SEAL — DAMAGED (SERVICE DOOR) · airframe 24,175 hrs · 20,396 cycles

FLIGHT ATTENDANT STATED THAT A LOUD SQUEAL WAS COMING FROM THE SERVICE DOOR & THAT SHE COULD SEE LIGHT ABOVE THE DIAMETER OF A NICKEL BETWEEN THE DOOR SEAL & THE DOOR FRAME AT THE UPPER RT CORNER OF THE DOOR. PRESSURIZATION INDICATION NORMAL AT 300 FEET MSL DOOR INDICATIONS NORMAL. REPAIR SERVICED DOOR UPPER RT CORNER SEAL IAW AMM 52-00-01. OPERATIONS PRESSURIZED CHECK NO LEAK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

RIGHT REAR FUSELAGE I SKIN CRACKS AT FRAME 75 BETWEEN STRINGERS 1R & 2R. PERFORMED PERMANENT REPAIR OF RT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1R & 2R IAW ERS-EM-53MR-595.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

LEFT REAR FUSELAGE I SKIN CRACKS AT FRAME 75 BETWEEN STRINGERS 1L & 3L. PERFORMED PERMANENT REPAIR OF LT REAR FUSELAGE I SKIN AT FRAME 75 BETWEEN STRINGERS 1L & 3L IAW ERS-EM-53MR-596.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

STRINGER 2L CHAFED BETWEEN FRAMES 20 & 21. BLENDED DAMAGE, INSTALLED DOUBLER & REINFORCEMENT IAW ERS-EM-53MR-573R1.

Part: SKIN — DAMAGED (RT ELEVATOR) · airframe 24,161 hrs · 20,385 cycles

RIGHT ELEVATOR HAS A BURN MARK ON THE TE APPROXIMATELY 19.5 INCHES OTBD OF THE RT SERVO TAB. REPAIRED RT ELEVATOR BURN MARK ON TE APPROXIMATELY 19.5 INCHES OTBD OF THE SERVO TAB IAW ERS-EM-5500-124. SEE TURNOVER FOR WORK ACCOMPLISHED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 AT FIRST FASTENER BELOW STRINGER 2L. CRACK IS APPROX 1/8 INCH IN LENGTH. REPAIRED LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 & ABOVE 2L IAW ERS-EM-53MR-596.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R. CRACK IS APPROX 3/8 INCH IN LENGTH. REPAIRED RT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 & ABOVE 2R IAW ERS-EM-53MR-595.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,161 hrs · 20,385 cycles

NUMBER 8 EMER LIGHT STRIP WIRING CONNECTORS ON PLANE SIDE BROKEN OFF. INSTALLED NR 8 EMER LIGHT CONNECTORS ON PLANE SIDE IAW SWPM 20-21-00. SEE BOW 159911 FOR OPERATIONS CHECK.

Part: BONDING STRAP — CORRODED (LT WING) · airframe 24,161 hrs · 20,385 cycles

LEFT WING TIP HAS CORRODED BONDING STRAP. REMOVED CORRODED BONDING STRAP, FABRICATED & INSTALLED SERVICEABLE BONDING STRAP WITH RIVETS ON LT WING TIP IAW ERS-EM-5700-184.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

AFT BELLY FAIRING RT FWD ATTACH L ANGLE IS CRACKED UNDER SPAR 3. REMOVED CRACKED AFT BELLY FAIRING RT FWD ATTACH L ANGLE & INSTALLED SERVICEABLE L ANGLE IAW SRM 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

AFT BELLY FAIRING LT FWD ATTACH L ANGLE IS CRACKED UNDER SPAR 3. REMOVED & INSTALLED SERVICEABLE L ANGLE IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED AT FRAME 75 AT FIRST FASTENER BELOW STRINGER 2R. CRACK IS APPROX 1/4 INCH IN LENGTH. REPAIRED RT UPPER FUSELAGE SKIN AT FRAME 75 AT FASTENER BELOW STRINGER 2R. SEE ERS-EM-53MR-595.

Part: SUPPORT BRACKET — CRACKED (LT ENGINE) · airframe 24,161 hrs · 20,385 cycles

LEFT ENG SCV TRIANGULAR SHAPED SUPPORT BRACKET IS CRACKED. R & R IAW PPBM 71-00-00 & CMM 80-11-93.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,161 hrs · 20,385 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 ABOVE STRINGER 2L. CRACK IS APPROX 3/8 INCHES IN LENGTH. REPAIRED LT UPPER FUSELAGE SKIN JUST AFT OF FRAME 75 ABOVE STRINGER 2L IAW ERS-EM-53MR-596.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,140 hrs · 20,368 cycles

CAPTAIN’S FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S FLASHLIGHT IAW AMM 25-60-00, OPERATIONS CHECKED GOOD.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 23,492 hrs · 19,819 cycles

PAX DOOR EMERGENCY LIGHT LENS CRACKED. R & R EMERGENCY LIGHT ASSEMBLY & SIDE HINGE DOOR LINER IAW MM 25-23-04, OPERATIONS CHECKED GOOD.

Part: DUCT — CRACKED (ANTI-ICE SYS) · airframe 23,385 hrs · 19,718 cycles

FOUND LT ENG INLET ANTI-ICE DUCT CRACKED DURING INSPECTION OF CUSTOMER SERVICE MANIFOLD. R & R LT ENG INLET ANTI-ICE DUCT IAW AMM 30-21-05. OPERATIONS CHECK & LEAK CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,436 hrs · 18,928 cycles

LEFT EXTERIOR FWD EMERGENCY LIGHT INOPERATIVE. NR 1 LIGHT BATTERY INOPERATIVE. R & R BATTERY IAW WC 33-700-19, OPS CHECKED GOOD, NO DEFECTS NOTED.

Part: CONTROL PANEL — ODOR (PCU) · airframe 22,368 hrs · 18,873 cycles

LIGHT OVER 8A BURNED OUT, ASSOCIATED WITH BURN ODOR. R & R PCU PANEL ASSY ON SEAT 8B-C IAW AMM 25-22-05. OPS GOOD, NO BURN ODOR NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,350 hrs · 18,859 cycles

NR 4 EMERGENCY LIGHT STRIP INOPERATIVE. R & R NR 4 EMERGENCY LIGHT STRIP, OPS CHECKED GOOD AMM 33-50-12.

Part: SLEEVE — INOPERATIVE · airframe 22,168 hrs · 18,702 cycles

THE CREW REPORTED PACK NR 1 VALVE CLOSED DURING CLIMB, RESET IAW AOM V1, STAYED OK FOR 5 MINUTES THEN CLOSED AGAIN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 210 AND NR 230 LT ACM SLEEVES IN REFR TO AMM 21-51-03, THE OPS CHECK WAS GOOD AT THIS TIME. ADJUSTED THE LINEAR ACTUATOR IAW AMM 21-25-03. PERFORMED OPS CHECK IAW AMM 21-25-01. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT ASSY — INOPERATIVE (COCKPIT) · airframe 21,553 hrs · 18,252 cycles

CREW REPORTED CAPTAIN’S FLASHLIGHT WAS NOT CHARGING. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT ASSY IAW MM SP 33-50-16. OPS CHECKED GOOD. THE WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,494 hrs · 18,200 cycles

CREW REPORTED CAPTAIN'S FLASHLIGHT WAS INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT IAW STAND MAINT PRACTICE. ACFT RETURNED TO SERVICE.

Part: DRAIN LINE — CONTAMINATED (PITOT/STATIC SYS) · airframe 21,286 hrs · 18,017 cycles

THE CREW REPORTED THAT IN ICING CONDITIONS THEY GOT AMBER IAS AND ALT INDICATIONS AT 37,000 FEET. THE PROBLEM PERSISTED UNTIL 20,000. AT ONE POINT FOS AIRSPEED INDICATED 60KTS AND FOS ALTIMETER WAY OFF. THE CAPTAIN'S ALTIMETER JUMPED TO DIFFERENT INDICATIONS STANDBY REMAINED SOMEWHAT STABLE. THE CREW DECLARED AN EMERGENY AND LANDED WITHOUT INCIDENT. NO DEFECTS WERER NOTED DURING POST FLIGHT AND THE ACFT WAS FOUND WITH NO ICE UPON LANDING. THE ACFT WAS REMOVED FROM SERVICE. DRAINED PITOT-STATIC DRAIN TUBES IAW AMM TASK 34-13+00-650-801-A. PERFORMED FUNCTIONAL CHECK OF ADC SYS. THE OPS CHECK WAS GOOD IAW AE W/C 34-700-03. PERFORM OPS CHECK OF PITOT AND ANEMOMETRIC STATIC PORT HEATING. THE OPS CHECK WAS GOOD IAW AMM 30-700-07. THE ACFT WAS RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 20,952 hrs · 17,746 cycles

DURING B INSPECTION FOUND THE COPILOT FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COPILOTS FLASHLIGHT ASSEMBLY IAW EMB AMM 33-51-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 20,802 hrs · 17,633 cycles

ON FLIGHT 3409 THE CREW REPORTED THAT AFTER TAKEOFF CLIMBING AT NORMAL CLIMB SPEED APROX 14,000 FT STICK SHAKER AVTIVATED NO LOSS OF AIRSPEED YAW DAMP FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETUNRED TO DRO. UPON LANDING SPOILERS FAILED TO DEPLOY. NORMAL LANDING EXECUTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. CMC CONTAINS NO MESSAGES FOER FLT 3409, FOUND MOISTURE CORROSION ON SPS COMPUTER ELECTRICAL CONNECTOR. CLEANED AIRFRAME CONNECTOR AND REPLACED SPS COMPUTER IAW AMM CH 27-36-02. SPS SYSTEM OPS CHECK OK IAW AMM CH 27-36-0. UNABLE TO DUPLICATE GROUND SPOILERS OPS CHECK OK IAW AMM II CH 27-63-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — IMPROPER PART (CABIN) · airframe 20,694 hrs · 17,554 cycles

ON FLIGHT 2985 THE CREW REPORTED THE INCORRECT FLOOR PROXIMITY STRIP LIGHT INSTALLED AT ROW 12. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE STRIP LIGHT AT ROW 12. THE OPERATIONAL CHECK WAS GOOD IAW EMB-145 AMM 33-50-12 AND 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BUTTON — DIRTY (HANDSET) · airframe 20,573 hrs · 17,451 cycles

FLIGHT 4116. FLIGHT ATTENDANT FORWARD HANDSET DOES NOT CALL FLIGHTDECK WHEN PILOT BUTTON IS PRESSED. TROUBLESHOT AND CLEANED DEBRIS FROM AFT HANDSET PTT IAW AMM. OPS CHECKED GOOD IAW AMM 23-31-00. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 19,770 hrs · 16,810 cycles

ON FLIGHT 2838, ADVANCED THE THRUST LEVERS TO THE DETENT FOR NORMAL CLIMB THRUST, E1 IMMEDIATELY BEGAN TO SPOOL DOWN UNCOMMANDED. EICAS MESSAGE E1 OUT APPEARED WITH NO OTHER ASSOCIATED MESSAGES. RAN THE APPROPRIATE EMERGENCY PROCEDURES. ADVISED ATC OF THE EMERGENCY AND WERE UNABLE TO CLIMB TO FL370. ATC ASSIGNED AN ALTITUDE OF FL210. ELECTED TO RESTART THE ENGINE. ABORTED THE RESTART ATTEMPT AND CONCLUDED THAT SOMETHING MECHANICAL MUST HAVE OCCURRED DUE TO NO N2 ROTATION. CONTINUED TO AMA AND A NORMAL VISUAL APPROACH WAS MADE. CFR WAS ON LOCATION AS REQUESTED. INSPECTION, NO VISUAL OR UNUSUAL INDICATIONS WERE NOTICEABLE ON OR INSIDE THE ENGINE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE IAW AEA WORKCARD 71-000-00. OPS AND LEAK CHECK GOOD NO DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,623 hrs · 16,681 cycles

DURING MAINTENEANCE INSPECTION FOUND THE LEFT SIDE FORWARD EMERGENCY LIGHT OVERWING FOUND NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT SIDE FORWARD EMERGENCY LIGHT OVERWING IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD IAW TASK 33-50-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,620 hrs · 16,678 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OMEGA BEAM CORRODED AT FRAME 23. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIR DAMAGE IAW EMBRAER STRUCTUAL REPAIR MANUAL 53-21-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 19,620 hrs · 16,678 cycles

DURING MAINTENANCE INSPECTION FOUND THE CENTER SERVICE DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICE DOOR LOWER SILL IAW EMBRAER STRUCTUAL REPAIR MANUAL 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — SCORED (RT AILERON) · airframe 19,620 hrs · 16,678 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVER AILERON BRACKET TO PCA HAS SCORING ON INSIDE DIAMETER TO WHICH HAT BUSHING IS INSTALLED INTO. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT AILERON PCA FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — CRACKED (CABIN) · airframe 19,660 hrs · 16,711 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT FLOOR PROXIMITY STRIPS NR 8, 6, 2 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT FLOOR PROXIMITY STRIPS NR 2, 5, 7 IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURN TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 19,660 hrs · 16,711 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 FLOOR EMERGENCY LIGHT PROXIMITY STRIP AND TRIM BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 FLOOR EMERGENCY LIGHT PROXIMITY STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,606 hrs · 16,664 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT AND THE COCKPIT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT & THE COCKPIT EMERGENCY LIGHT IAW EMB AMM TASK 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: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,353 hrs · 16,462 cycles

DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (12A CEILING) · airframe 19,332 hrs · 16,440 cycles

DURING B INSPECTION, FOUND THE CEILING EMERGENCY LIGHT INOPERATIVE AT 12A. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMEREGENCY LIGHT BULB AT SEAT 12A IAW AMM TASK: 33-50-08-000-801-A, AND 33-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,091 hrs · 16,263 cycles

DURING MAINTENANCE INSPECTION, FOUND THE FORWARD EMERGENCY LIGHT ON THE RIGHT FUSELAGE INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT BULB ON THE RIGHT FUSELAGE IAW AMM 33-50-07. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,927 hrs · 16,152 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY LIGHT IAW EMB AMM TASK: 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: FUSE — INOPERATIVE (DC BUSS) · airframe 18,716 hrs · 18,716 cycles

EMERGENCY ELECTRICAL ABNORMAL AND DC BUSS 2 FAIL. AIRCRAFT REMOVED FROM SERVICE. RESET ELECTRICAL SYSTEM IAW FIM 24-60-00. EMERGENCY ELECTRICAL ABNORMAL MESSAGE CLEARED, BUT DC BUSS 2 STILL REMAINS. FUSE F0006 CHECKED GOOD. 5 AMP CIRCUIT BREAKER ON RT PDU CHECKED GOOD, SWAP DAU'S, PROBLEM RETURNS, PLACED BACK INTO ORIGINAL POSITIONS. VERIFIED DC BUSS HAS 28V. REMOVED AND REPLACED FUSE F0006 IAW AMM II CH 20-13-08. OPS CHECKED GOOD IAW AMM II CH 24-60-00. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,919 hrs · 15,405 cycles

DURING B-INSPECTION FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT INTERMITTANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB IN RT AFT OVERWING EMERGENCY LT IAW EMB 145 AMM 33-50-10-000-801-A/33-50-10-400-801-A. OPERATIONAL CHECK GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (ELECTRICAL SYS) · airframe 17,719 hrs · 15,248 cycles

FOR FLIGHT 4196 THE CREW REPORTED THEY NOTICED THE EXTERNAL POWER CONNECTED AND ASKED TO HAVE IT DISCONNECTED. ONCE GROUND PERSONNEL DISCONNECTED, CABIN CEILING LIGHTS TURNED OFF FOLLOWED BY SLIGHT ELECTRICAL BURNING SMELL THE AIRCRAFT WAS REMOVED FROM SERVICE. ALL STATED ELECTRICAL PROBLEMS CAUSED BY USE OF EXTERNAL POWER WHILE MEL 24-9 IN EFFECT. RESET POWER, ALL NORMAL WITH APU POWER APPLIED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DIRTY (CABIN) · airframe 17,702 hrs · 15,237 cycles

DURING MAINTENANCE BASE VISIT FOUND THE MAIN DOOR MOUNTED EMERGENCY LIGHT WORKING INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED CONNECTOR FOR THE MAIN DOOR MOUNTED EMERGENCY LIGHT ASSEMBLY IAW EMB 145 WM CHAPTER 20-50-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 17,624 hrs · 15,179 cycles

DURING MAINTENANCE INSPECTION FOUND THE COCKPIT OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COCKPIT EMERGENCY LAMP IAW EMB AMM TASK 33-50-06-000-801A/33-50-06-400-801A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 17,433 hrs · 15,018 cycles

FOR FLIGHT 4112 THE CREW REPORTED THAT DURING THE PREFLIGHT INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT AS REQUIRED. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,324 hrs · 14,931 cycles

MAIN DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY EXIT LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,324 hrs · 14,931 cycles

DURING MAINTENANCE BASE VISIT FOUND THE MAIN DOOR EMERGENCY EXIT EXTERIOR LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN DOOR EMERGENCY EXIT LIGHT LAMP IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 15,778 hrs · 13,779 cycles

ON FLIGHT 3553 THE CREW REPORTED THAT IMMEDIATELY AFTER TAKEOFF RECEIVED A PITCH TRIM MAIN INOPERABLE EICAS WARNING MESSAGE AFTER ACTIVATING CAPTAIN’S YOKE TRIM NOSE DOWN. THE CAPTAIN’S PITCH TRIM NEVER HELD IN NOSE DOWN POSITION FOR MORE THAN 2 SECONDS. THE CREW NEVER HEARD A TRIM AURAL WARNING. THE CREW DETERMINED THE BACKUP PITCH TRIM SYSTEM WORKED AFTER AOM CHECKLIST. THE CAPTAIN ELECTED TO RETURN TO MIA. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB 145 AMM 27-40-01 AND TESTED IAW AMM 27-40-00 ALL TESTS OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,219 hrs · 13,356 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLOOR PROXIMITY STRIP AT ROW 8/9 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP AT ROWS 8/9 IAW EMB 145 AMM 33-50-12 . THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,096 hrs · 12,485 cycles

FOR FLIGHT 4165 DURING INSPECTION FOUND THE NR 3 AISLE EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,427 hrs · 11,938 cycles

DURING THE MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,302 hrs · 11,884 cycles

FOR FLIGHT 3301 DURING MAINTENANCE CHECK THE NR 4 FROM THE PASSENGER DOOR FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 12,933 hrs · 11,603 cycles

FOR FLIGHT 2789 THE CREW REPORTED THE LEFT FORWARD OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 12,385 hrs · 11,185 cycles

ON FLIGHT 2738 THE CREW REPORTED THAT AT 37000 FEET THE CABIN ALTIMETER STARTED TO CLIMB AS CREW STARTED DESCENT AND THE CABIN ALTIMETER GOT TO APPROXIMATELY 9600 FEET. SWITCHED TO MANUAL MODE AND GOT THE CABIN ALTIMETER TO STABILIZE BUT IT WAS ERRATIC ALL THE WAY DOWN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PRESSURE DIGITAL CONTROLLER AND PERFORMED MANUAL/AUTO PRESSURE OPERATIONAL CHECK IAW AMM 21-31-01. ALSO CHECKED BOTH OUTFLOW VALVES, LINES, CONNECTIONS, ALL DOORS, WINDOWS, FOR ANY AIR LEAKS. PERFORMED AN OPERATIONAL CHECK OF THE MANUAL PRESSURIZATION. THE OPERATIONAL CHECK WAS GOOD IAW EMB145 AMM 21-31-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 10,295 hrs · 9,257 cycles

ON FLIGHT 3825, MTX REPORTED THE AIRCRAFT DID A AIR TURN BACK FOR A LAV SMOKE DETECTION ON CLIMB-OUT WITH NO VISIBLE SMOKE OR ODOR.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,789 hrs · 8,853 cycles

DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR. FABRICATED A FILLER AND TWO SHIMS. INSTALLED REPAIR PARTS AFTER CLEANING, ALODINING AND PRIMING. REPAIR DONE IAW EMB SRM (SRM EMB 145/1142 REV 40) CHAPTER 53-00-10. AIRCRAFT RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 9,789 hrs · 8,853 cycles

DURING A IMBV INSPECTION, THE CENTER FLOOR OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVE THE DAMAGE. FABRICATED A REPAIR DOUBLER. CLEANED AND TREATED THE DOUBLER. INSTALLED DOUBLER IAW EMB 145 SRM (SRM EMB-145/1142 REV 40) CHAPTER 53-21-10 FIGURE 202. AIRCRAFT RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,789 hrs · 8,853 cycles

DURING A IMBV INSPECTION THE BAGGAGE DOOR LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. POSITIONED NEW SILL AND DRILLED. CLEANED AND TREATED NEW SILL INSTALLED NEW SILL IAW EMB 145 SRM (SRM EMB - 145./1142 REV 40) CHAPTER 51-40-02, 51-40-04 AND 51-40-06. AIRCRAFT RETURN TO SERVICE.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 9,778 hrs · 8,842 cycles

ON FLIGHT 3458 MAINTENANCE REPORTED A ELECTRICAL BURNING ODOR IN THE GALLEY AREA. AIRCRAFT REMOVED FOR SERVICE. REMOVED AND REPLACED COFFEEMAKER IAW ETN EM-25-010R1. NO DEFECTS OR ODORS NOTED. REMOVED AND REPLACED BALLAST NR RT8439-234 IAW AMM 33-21-04. OPERATION CHECKS GOOD FOR GALLEY LIGHTS. NO DEFECTS OR ODORS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 9,636 hrs · 8,717 cycles

ON FLIGHT 3862, CREW REPORTED JUST AFTER TAKE OFF, AS THE LANDING GEAR RETRACTED, LAV SMOKE ALARM ON EICAS AND ALARM IN THE LAV SOUNDED. BOTH WENT AWAY WHEN LANDING GEAR WAS RETRACTED. ACFT REMOVED FROM SERVICE . PERFORMED OPS CHECK OF LAV SMOKE DETECTION SYS. IAW AMM 26-14-00 NO DEFECTS NOTED AT THIS TIME, NO OIL OR SMOKE SMELL DETECTED. ACFT RETURNED TO SERVICE.

Part: PRECOOLER — MALFUNCTIONED

ON FLIGHT 3992 DURING CRUISE CREW ADVISES THAT THERE IS A BURNING RUBBER OIL ODOR IN THE CABIN. WHEN ON THE GROUND THE TEMPERATURE STABILIZED. ACFT REMOVED FROM SERVICE. C/A R&R NR 2 ENGINE PRECOOLER. OPS CHECK GOOD. ACFT RETURNED TO SERVICE.

Part: PITOT LINE — CONTAMINATED · airframe 76,340 hrs · 6,959 cycles

ON FLIGHT 4125, CREW REPORTED DURING APPROACH THAT THEY COULD NOT TELL WHAT ATTITUDE THEY WERE AT. ALL THREE ALTIMETERS SHOWING DIFFERENT READINGS. CREW DECLARED EMERGENCY, FMS MESSAGE UNRELIABLE ALTIMETER DO NOT USE FOR NAV. AFTER LANDING CREW NOTICED THE STANDBY ALTIMETER WAS OFF 800 TO 900 FT. AFTER CREW SAT AT THE GATE FOR A WHILE ALL THREE INDICATIONS CAME BACK TO NORMAL. FOUND A LOT OF WATER IN THE RIGHT PITOT LINE. MINOR AMOUNT IN THE RIGHT LINE. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 5,458 hrs · 5,072 cycles

SEAT 16 A AISLE EMERGENCY LIGHT AND SEAT 19 LEFT OVERWING EMERGENCY LIGHT OUT. REPLACED NUMBER 1 EMERGENCY LIGHT POWER SUPPLY IAW EMB AMM. OPERATIONAL CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,803 hrs · 4,432 cycles

FOUND OMEGA BEAM CORRODED AT FRAME 20. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS. CLEANED, TREATED AND RESTORED PROTECTIVE FINISH IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: GROUND STUD — SHORTED (TE FLAPS) · airframe 4,425 hrs · 4,093 cycles

FLAP FAIL MESSAGE ON EICAS AT 230 KNOTS. FOUND INTERMITTENT RESISTANCE ON GS0352 DC GROUNDING POINT FOR LEFT TRANSMISSION BRAKE. CLEANED BONDING JUMPERS AT GROUND STUD. SWAPPED LEFT AND RIGHT FLAP MOTOR UNITS. OPERATIONAL CHECK GOOD IAW EMB AMM 27-50-00. PERFORMED FUNCTIONAL CHECK FLIGHT WITH NO DEFECTS NOTED, RETURNED AIRCRAFT TO SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 4,388 hrs · 4,065 cycles

FLAPS SELECTED TO 9 DEGREES AND RECEIVED FLAP FAIL MESSAGE, RESET FLAPS TO ZERO AND MESSAGE WENT AWAY. RESELECTED FLAPS TO 9 DEGREES AND FLAP FAIL MESSAGE RETURNED. MESSAGE CLEARED IT SELF AND FLAPS WENT 9 DEGREES. FLAPS RETRACTED NORMALLY UPON LANDING.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,375 hrs · 4,055 cycles

FLAPS DID NOT RETRACT AFTER TAKEOFF. CYCLED FLAPS REMAINED AT 9 DEGREES.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

ON APPROACH SELECTED 9 DEGREE FLAPS, A FLAP FAIL MESSAGE FOLLOWED. AIRCRAFT OPERATING MANUAL PROCEDURES. DECLARED EMERGENCY WITH AN UNEVENTFUL LANDING. MESSAGE REMAINED ILLUMINATED AFTER LANDING. (M)

Part: BRAKE — FAILED (T/E FLAP)

FLAP FAIL ON APPROACH. REMOVED AND REPLACED LEFT FLAP TRANSMISSION BRAKE, IAW EMB 145, AMM 27-51-01. OPS CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE. (M)

Part: CARBON SEAL — LEAKING (NR 2 ENGINE)

DFW - FLT 3749 - DURING TAKEOFF, RECEIVED LAVATORY SMOKE MASTER WARNING ON EICAS AND LAVATORY SMOKE DETECTOR ALARM WAS ACTIVATED. FOUND 0 CARBON LEAKING. REPLACED NR 2 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)