N621AE

Part: UNKNOWN — ODOR (CABIN) · airframe 47,221 hrs · 44,624 cycles

LEVELING AT CRUISE FLIGHT SMELLED BURNING ODOR EXPERIENCED BY ALL CREW MEMBERS, RAN QRH AND AFTER TURNING OFF GASPER SMELL WENT AWAY. FOLLOWED FIM 21-20-00-810-801-A FOUND SLIGHT ELECTRICAL SMELL ON BOTH FLIGHT DECK FLASHLIGHTS. REM AND INSP FLASHLIGHT ASSY WITH NO DEFECTS NOTED. REINSTALLED IAW AMM33-50-16. COMPL FIM WITH NO DEFECTS NOTED. INSP INSIDE BOTH PKS NLS WITH NO DEFECTS NOTED. RAN APU BLD, BOTH PKS,RECIRC AND GASPER FANS FOR APP 30 MIN WITH NO DEFECTS OR SMELLS NOTED . AC OK 4 SERVICE

Part: NONE — NONE · airframe 47,075 hrs · 44,457 cycles

SUPPLEMENTAL INFORMATION - ERROR - UNIQUE CONTROL NUMBER CHANGE FROM HNAAA20211004733 TO HNAA2021100400473 PDIS 621 52-71 2482261 02OCT21 OAJ CLOSE BAG DOOR INDICATION ON TAKE OFF MEL 02OCT21 13:17 OAJ C27509 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING FACT 03OCT21 01:28 SBY OPERATED BAG BAY DOOR NUMEROUS TIMES WITHOUT FAULTS. OPERATED MICRO SWITCHES BY HAND, WITHOUT NOTICEABLE DEFECTS. OPS CHECK GOOD. CLEAR MEL 52-3-2.

Part: NONE — NONE · airframe 47,075 hrs · 44,457 cycles

PDIS 621 52-71 2482261 02OCT21 OAJ CLOSE BAG DOOR INDICATION ON TAKE OFF MEL 02OCT21 13:17 OAJ C27509 52-3-2 BAGGAGE DOOR WARNING / POSITION WARNING FACT 03OCT21 01:28 SBY OPERATED BAG BAY DOOR NUMEROUS TIMES WITHOUT FAULTS. OPERATED MICRO SWITCHES BY HAND, WITHOUT NOTICEABLE DEFECTS. OPS CHECK GOOD. CLEAR MEL 52-3-2.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 46,553 hrs · 43,867 cycles

COCKPIT THRESHOLD STEP, EMERGENCY LIGHT SIGN IS INOP. REMOVED COCKPIT THRESHOLD PANEL, FOUND WIRE BROKEN AT QUICK DISCONNECT CONNECTOR, INSTALLED NEW CONTACT PIN AND MALE CONNECTOR ONTO WIRE, CONNECTED QUICK DISCONNECT CONNECTORS, OPS CHECKED LIGHTS, OPS CHECKED GOOD, INSTALLED COCKPIT THRESHOLD PANEL.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 45,810 hrs · 43,064 cycles

WINDSHIELD HEAT 1 FAIL MESSAGE ON EICAS. C/W FLT CREW PROCEDURES. REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER, REFERENCE AMM 30-42-01-000-801-A AND 30-42-01-400-801-A. OPERATIONS CHECK GOOD. OK FOR SERVICE.

Part: BATTERY — NOT SEATED (EMERGENCY LIGHTS) · airframe 45,784 hrs · 43,028 cycles

CABIN CEILING EMERGENCY EXIT AFT SIGN LIGHT DOES NOT TURN ON. RESET C/B NO FIX. REMOVED LT CABIN FLOOR PANEL 251JF TO ACCESS EMERGENCY BATTERY RESEATED NR 3 EMERGENCY BATTERY CANNON PLUG. OPERATIONS CHECK GOOD INSTALLED FLOOR PANEL 251JF USING RETAINED HARDWARE OK FOR SERVICE AT THIS TIME PERFORMED. OPERATIONS CHECK, IAW W/C 33-70-17.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,784 hrs · 43,028 cycles

EMERGENCY LIGHT ABOVE FA SEAT DOES NOT TURN ON THE EXIT SIGN. R & R NR 100 EMERGENCY LIGHT SYSTEM BATTERY PACK, IAW AMM 33-50-04.

Part: SKIN — DEFORMED (FRAMES 12A-13) · airframe 45,698 hrs · 42,926 cycles

FUSELAGE EXTERNAL SKIN DEFORMED BETWEEN FR 12A/13 STR 6R/7R. ACCOMPLISHED REPAIR OF FUSELAGE EXTERNAL SKIN AT UPPER AFT CORNER OF RT DV WINDOW BETWEEN FR 12A-13 STGR 6R-7R, IAW PIEDMONT EO1--53-20-0422.

Part: SKIN — CRACKED (FRAME 77) · airframe 45,698 hrs · 42,926 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 77. ONE BETWEEN STRINGERS 3L-4L, AND ONE BETWEEN STRINGERS 4L-5L, AND ONE BETWEEN STRINGERS 6L-7L. FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 77. ONE BETWEEN STRINGERS 3L-4L, AND ONE BETWEEN STRINGERS 4L-5L AND ONE BETWEEN STRINGERS 6L-7L.

Part: TRUNNION — CRACKED (LT MLG) · airframe 45,698 hrs · 42,926 cycles

LT MLG AFT UPPER TRUNNION HAS POSSIBLE CRACK IN RADIUS ABOVE FASTENER. PERFORMED HFEC INSPECTION ON AFT UPPER TRUNNION AND FOUND TO BE CRACKED, IAW EASI NDT MANUAL NR 6581 (400 KHZ H 60.6 V72.6 ANGLE 127 DEGREES). REMOVED AND INSTALLED SERVICEABLE LT AFT TRUNNION, IAW AERNNOVA TI NR TI-145-14-018 LT REV F, ETD2020-145-032819 AND EO1-57-20--0421. SEE NRTC'S E827994, E828197, E828328,AND E828329 FOR STRUT REMOVAL, DOORS REMOVAL AND INSTALL SPOILER HYD LINESRAR AND CLAMPS AND CLAMP BLOCKS RAR.

Part: STRINGER — CRACKED (FRAME 13) · airframe 45,698 hrs · 42,926 cycles

STRINGER 6R CRACKED AT FR 13. REMOVED AND INSTALLED SERVICEABLE STRINGER 6R AT FR 13, IAW EMB145 SRM 51-40-02 AND SRM 51-20-01.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 45,698 hrs · 42,926 cycles

SSI 53-30-48 CARGO DOOR LOWER SILL HAS CORROSION AND BARE METAL, MARKED. REMOVED CORROSION BY BLENDING, IAW EMB 145 SRM 51-10-03. PERFORMED HFEC INSPECTION AND UT THICKNESS, IAW EASI NDTM. NO RELEVANT INDICATION NOTED, .055"-.074" MATERIAL REMAINING ET EASI 8958 UT EASI 8389. REMOVED AND REPLACED CARGO DOOR LOWER SILL, IAW EMB145SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-17) · airframe 45,698 hrs · 42,926 cycles

FWD DIGITAL IS CORRODED AROUND SCREW HOLE ON CENTEROMEGA BEAM BETWEEN FR 16-17. FABRICATED REPAIR DOUBLERS AND SHIMS, IAW EMB 145 SRM 53-21-10. INSTALLED REPLACEMENT DIGITAL SECTION REPAIR DOUBLER AND SHIM, IAW EMB 145 SRM 53--21-10 AND PIEDMONT EO1-05-20-0420.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 45,698 hrs · 42,926 cycles

SSI 53-30-48 CARGO DOOR LOWER SILL HAS CORROSION AND BARE METAL, MARKED. REMOVED CORROSION BY BLENDING, IAW EMB 145 SRM 51-10-03. PERFORMED HFEC INSPECTION AND UT THICKNESS, IAW EASI NDTM. NO RELEVANT INDICATION NOTED .055"-.074" MATERIAL REMAINING ET EASI 8958 UT EASI 8389. REMOVED AND REPLACED CARGO DOOR LOWER SILL, IAW EMB145SRM 51-40-02. USED INCORRECT UNIQUE CONTROL NUMBER HNAA202000346 SHOULD BE HNAA2020121100346.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 45,698 hrs · 42,926 cycles

SSI 53-20-10 SERVICE DOOR CENTER SILL IS CORRODED AROUND 3 SCREW HOLES. BLENDED CORROSION ON SERVICE DOOR CENTER SILL AROUND 3 SCREW HOLES, IAW EMB 145 SRM51-10-03. REMAINING THICKNESS AT CENTER AND AFT BLENDED AREAS ON SERVICE DOOR CENTER SILL FOUND TO BE WITH ALLOWABLE LIMITS, IAW EMB145 SRM 53-21--02. REPAIRED SERVICE DOOR CENTER SILL, IAW PDT EO-1-53-20-0413.

Part: FRAME — CRACKED (FRM 25) · airframe 45,698 hrs · 42,926 cycles

SSI 53-20-43, FRAME 25 IS CRACKED BETWEEN STRINGERS 15R AND 16R, MARKED. FABRICATED, PREPPED AND INSTALLED SERVICEABLE FR 25 LOWER RT FRAME SECTION INTERNAL SPLICE DOUBLER, IAW EMB 145 SRM 53-00-04, ITEM 4, FIGURE 201 AND EMB 145 SRM 51-20-03 AND 51--40-02 AND EO1-53-20-0414.

Part: BRACKET — CRACKED (PAX DOOR HANDLE) · airframe 45,698 hrs · 42,926 cycles

MAIN DOOR INTERNAL ACTUATING HANDLE BRACKET CRACKED, MARKED. REMOVED AND REPLACED MAIN DOOR INTERNAL ACTUATING HANDLE BRACKET, IAW EMB 145 SRM 51-40-02.

Part: STRUCTURE — CORRODED (MAIN DOOR) · airframe 45,698 hrs · 42,926 cycles

MAIN DOOR LOWER EDGE HAS CORROSION AROUND FOUR NUT PLATE HOLES, MARKED. ACCOMPLISHED REPAIR AT FWD NUTPLATE HOLE, IAW EMB 145 SRM 52-10-04 ITEM 3 FIGURE 201 SHEET 3 AND EO1-52-20-0426.

Part: BRACKET — CRACKED (DOOR HANDLE) · airframe 45,698 hrs · 42,926 cycles

MAIN DOOR INTERNAL ACTUATING HANDLE BRACKET CRACKED, MARKED. REMOVED AND REPLACED MAIN DOOR INTERNAL ACTUATING HANDLE BRACKET, IAW EMB 145 SRM 51-40-02. USED INCORRECT UNIQUE CONTROL NUMBER HNAA2020003444 SHOULD BE HNAA2020121100344.

Part: SPAR — CRACKED (RT WING) · airframe 45,698 hrs · 42,926 cycles

RT WING SPAR 1 CRACKED ON LOWER FLANGE AT SCREW HOLE JUST OUTBOARD OF RIB 9. CRACK IS APPROXIMATELY 1/4 INCH, END IS MARKED. ACCOMPLISHED REPAIR OF RT WING SPAR I AT RIB 9, IAW EMB 145 SRM 57-20-05 ITEM 2 AND EO-1-57-20-0412.

Part: SKIN — CHAFED (CARGO DOOR) · airframe 45,698 hrs · 42,926 cycles

CARGO DOOR INTERNAL LOWER SKIN CHAFFED FWD OF ROD CLIP HOLDER, MARKED. REMOVED AND INSTALLED NEW CARGO DOOR INTERNAL SKIN, IAW EMB 145 SRM 51-40-02.

Part: PROFILE — CORRODED (EMERGENCY EXIT) · airframe 45,698 hrs · 42,926 cycles

LT EMERGENCY EXIT LOWER PROFILE L CORRODED UNDER TEFLON GUIDES. REMOVED AND INSTALLED SERVICEABLE LT EMERGENCY EXIT LOWER PROFILE LUNDER TEFLON GUIDES, IAW EMB 145 SRM 51--40-02 AND SRM 51-20-03.

Part: ACCESS DOOR — CRACKED · airframe 45,698 hrs · 42,926 cycles

ACCESS HATCH 272DR UPPER BEAM CRACKED, MARKED. REMOVED AND REPLACED ACCESS HATCH 272DR UPPER BEAM, IAW EMB 145 SRM 51-40-02.

Part: SPAR — CRACKED (LT WING) · airframe 45,698 hrs · 42,926 cycles

LT WING SPAR 1 CRACKED AT SECOND SCREW HOLE OUTBOARD OF RIB 9, CRACK IS APPROXIMATELY 3/8" LONG, FROM FWD FLANGE EDGE TO SCREW HOLE. EASI NR 6581 USED, FREQ=400KHZ, V-GAIN=77.0, H-GAIN=64.0, LPF=100. ACCOMPLISHED REPAIR OF LT WING SPAR I AT RIB 9, IAW EMB 145 SRM 57-20-05 ITEM 2 AND EO-1-57-20-0419 REV A, ETD2020-145-033221 AND TI-145-16-051LT.

Part: PROFILE — CORRODED (RT EMER EXIT) · airframe 45,698 hrs · 42,926 cycles

RT EMERGENCY EXIT LOWER PROFILE L CORRODED UNDER TEFLON GUIDES. REMOVED AND REPLACED RT EMERGENCY EXIT LOWER L-PROFILE, IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 77) · airframe 45,698 hrs · 42,926 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 77 BETWEEN STRINGERS 6R-7R. REPAIRED FUSELAGE EXTERNAL SKIN AT FRAME77 BETWEEN STRINGERS 6R-7R, IAW EMB 145 SRM53-32-01 AND EO1-53-20-0423.

Part: SKIN — CRACKED (FRAME 79) · airframe 45,698 hrs · 42,926 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 79 BETWEEN STRINGERS 6R-7R. FABRICATED AND INSTALLED SKIN BUSHING REPAIR AT FRAME 79 BETWEEN STRINGERS 6R-7R, IAW EMB 145 SRM 53-32-01-RE AND EO1-53-20-0423.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 45,698 hrs · 42,926 cycles

RT DRAG ANGLE BETWEEN VERTICAL STAB AND FUSELAGE IS CRACKED AT FRAME 76 STRINGER 3R. REMOVED AND REPLACED VERTICAL STAB DRAG ANGLE TO FUSELAGE AT FR 76 STRG 3R AND REINSTALLED PREVIOUS REPAIR, IAW EMB 145 SRM 51-40-02.

Part: SKIN — CRACKED (FRAME 79) · airframe 45,698 hrs · 42,926 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 79 BETWEEN STRINGERS 3L-4L. FABRICATED AND INSTALLED BUSHING RE-PAIR AT FRAME 79 BETWEEN STRINGERS 3L-4L, IAW EMB145 SRM 53-32-01-RE AND EO1-53-20-0424.

Part: SKIN — CRACKED (FRAME 78) · airframe 45,698 hrs · 42,926 cycles

FUSELAGE EXTERNAL SKIN IS CRACKED AT FRAME 78. ONE BETWEEN STRINGERS 4L-5L, AND ONE BETWEEN STRINGERS 6L-7L. FABRICATE AND INSTALLED SKIN BUSHING REPAIR AT FRAME 78 BETWEEN STRINGERS 6L-7L, IAW EMB 145 SRM 53-32-01-RE AND EO1-53-20-0424, NO RELEVANT INDICATION BETWEEN 4L-5L.

Part: ROLLER — SEIZED (NLG UPLOCK) · airframe 45,694 hrs · 42,924 cycles

ON TAKEOFF, EICAS SHOWED LG AIR GROUND FAIL. COUPLED WITH LOUD BANG ON NLG EXTENSION: MAINTENANCE: TESTED ALL WOW PROX SWITCHES, IAW AMM 32 63 05. ALL TESTED GOOD. FOUND NOSE UP LOCK ROLLER SEIZED DUE TO PRC. REMOVED PART OF THE PRC AS REQ. NO OTHER DEFECTS NOTED. OK FOR SERVICE. SEE SEQ 3 FOR GEAR OPERATIONS CHECK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,694 hrs · 43 cycles

NDIS 621 33-50 0025060 07OCT20 RIC CLOSE. EMERGENCY LIGHTS AT 13A THRU 18A, LT EXTERNAL EMERGENCY LIGHTS, MAIN SERVICE DOOR EMERGENCY LIGHTS AND CABIN CEILING EMERGENCY EXIT MARKER WILL NOT ILLUMINATE. 37208 00 NGR FACT 07OCT20 07:47 RIC. R & R BATTERY POWER SUPPLY 400, IN REF TO AMM 33-50-04-000/400-801-A. OPERATIONS CHECK GOOD. P/N ON BATTERY CHARGER ASSEMBLYY BAS-0933-901 S/N C02581, EMERGENCY LIGHT BATTERY PACK 2013-1A S/N 104879 P/N OFF BATTERY CHARGER ASSEMBLY S/N 12568, EMERGENCY LIGHT BATTERY PACK S/N 71051.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,694 hrs · 42,924 cycles

CABIN FLOOR EMERGENCY STRIPS INOPERABLE REAR OF CABIN. R & R NR 6 EMERGENCY LIGHT DC/AC/INVERTER IN REF TO AMM 33-50-11-000/400-801-A. OPT CHECK GOOD, OK FOR SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 44,460 hrs · 41,514 cycles

EMERGENCY EXIT LIGHT ABOVE FAS SEAT INOPERATIVE. R&RD EXIT SIGN.

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHT) · airframe 43,502 hrs · 40,446 cycles

NDIS 621 33-51 0012890 21APR19 RIC CLOSE EMERGENCY LIGHT ABOVE F/A SEAT INOP 28805 00 BSH FACT 21APR19 09:11 RIC RESEATED EMERGENCY LIGHT ABOVE F/A SEAT

Part: UNKNOWN — MALFUNCTIONED (NLG)

AFTER SELECTING GEAR UP. NOSE GEAR MADE THUMPING NOISE AND NOSE GEAR INDICATION ALTERNATED AMBER TO UP FOR FOR 8 MINS. CREW PERFORMED ALTERNATE EXTENSION, GEAR EXTENDED NORMALLY. INSPECTED NOSE LANDING GEAR FOR OBVIOUS DEFECTS NONE NOTED ON RELAY MSG ON CMC CHECKED NLG IP LOCK SENSOR IAW 32-36-05 NO DEFECTS NOTED.

Part: RIVET — MISSING (FUSELAGE) · airframe 43,066 hrs · 39,923 cycles

NDIS 621 53-30 0009060 03JAN19 SBY CLOSE FOUND 1 RIVET MISSING & 1 RIVET POPPED AT F24 XSTR 19R. FACT 03JAN19 12:34 SBY REMOVED ATTACDHMENT RIVETS FROM STRINGER 19R AND REMOVED FRAME LEGS OF FR 24 & 25 AT STR 19R. INSTALLED FRAME LEGS FOR FR24 & 25 AND SKIN RIVETS TO STR 19R AND INSTALLED FWD SPLICE FWD OF FR24 & 25 IAW 0106145-20280. REPAIR IAW EO1-53-19-0001.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,066 hrs · 39,923 cycles

EMERGENCY EXIT SIGN ABOVE FWD FA'S SEAT INOP. RESET EMERGENCY LIGHT C/B, OPS CHECK FOR EMERGENCY SIGN ABOVE FWD F/A'S SEAT IS GOOD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,066 hrs · 39,923 cycles

NDIS 621 53-30 0009070 03JAN19 SBY CLOSE FOUND CORROSION AT F24 & STR. 194. DOESNOT EXTEND OUT OF CHEM MILLED AREA. (SEE SEQ. 4 FOR DETAILS) FACT 03JAN19 12:46 SBY REMOVED ATTACHMETN RIVETS FROM STRINGER 19R AND REMOVED FRAME LEGS OF FR24 & 25 AT STR 19R. INSTALLED FRAME LEGS FOR FR24 & 25 AND SKIN RIVETS TO STR 19R AND INSTALLED FWD SPLICE FWD OF FR24 IAW DWG 145-20280 REPAIR CORROSION IAW E01-53-19-0001.

Part: AUTOPILOT SYS — MALFUNCTIONED · airframe 42,745 hrs · 39,517 cycles

ACFT DID A UNCOMMANDED HARD RIGHT TURN WITH AUTOPILOT ENGAGED. PILOT COMPLIED WITH AN IMMEDIATE EMERGENCY ACTION ITEMS WITH AUTO PILOT FAIL ON EICAS AND AUTO RED AP ON FLIGHT MODE ANNUNCIATOR ON PFD. COMPLIED WITH MX PROCEDURE. COULD NOT DUPLICATE THE DISCREPANCY. SIMULATED FLIGHT FOR 15 MINUTES, NO FAULTS NOTED. NO EVENT CODES NOTED. AUTOPILOT OPS CHECKS GOOD IAW 22-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 42,655 hrs · 39,400 cycles

CABIN ALTITUDE ALERT MSG AT 14,000. REACTIVATED PRESSURIZATION SYS OUTFLOW VALVES IAW MM 21-31-03-440-801-A AND 21-31-04-440-801-A. OPS CHECKED PRESSURIZATION WITH BOTH PACKS IAW MM 21-31-00-700-801-A, NO DEFFECTS NOTED.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 42,287 hrs · 38,961 cycles

CARGO DOOR LOWER SILL IS CORRODED. R & R THE CARGO DOOR LOWER SILL.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 42,287 hrs · 38,961 cycles

FRAME 65, SHEAR TIE IS CORRODED. R & R THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 42,287 hrs · 38,961 cycles

FRAME 68, SHEAR TIE WAS FOUND CORRODED. REPAIRED THE SHEAR TIE.

Part: DOOR FRAME — DENTED (CARGO BAY) · airframe 42,287 hrs · 38,961 cycles

CARGO DOOR LOWER FRAME PROFILE IS DENTED. R & R CARGO DOOR LOWER FRAME PROFILE.

Part: SKIN — DENTED (PAX DOOR) · airframe 42,287 hrs · 38,961 cycles

PAX DOOR LOWER CENTER EXTERIOR SKIN, 6 INCHES FROM BOTTOM HAS 2 DENTS. REPAIRED THE DOOR SKIN.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 42,247 hrs · 38,933 cycles

MAIN PAX DOOR EXTERNAL HANDLE BROKEN. REPLACED THE HANDLE. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN LIGHTS) · airframe 42,247 hrs · 38,933 cycles

INTERIOR LIGHTS FLICKERING WITH ASSOCIATED BURNING ODOR. PERFORMED INSPECTION AND OPS CHECK OF CABIN LIGHTS. VERIFIED ALL CABIN LIGHTS OPERATIONAL. NO BURNING ODOR NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,422 hrs · 37,323 cycles

FWD CABIN EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,327 hrs · 37,245 cycles

EMERGENCY LIGHT ABOVE FA SEAT INOPERATIVE. R & R THE BULB. OPS CHECKED GOOD.

Part: O-RING — WORN (BLEED DUCT) · airframe 39,747 hrs · 36,775 cycles

AT 10 FT, RECEIVED A BLEED 1 LEAK IN FLT AND WOULD NOT GO AWAY. REPLACED THE O-RINGS AT COUPLINGS 5, 9, 13, 15, 21 IAW AMM 36-11-10. TOURQED CLAMPS AT PRE-COOLER IAW AMM 36-11-04. LEAK CHECKED GOOD IAW AMM 36-00-00.

Part: DUCT — DETACHED (RECIRC FAN)

AT APPROXIMATELY 4000 FT, LOUD BANG HEARD FOLLOWED BY CALL FROM F/A REPORTING SMOKE IN CABIN AT ROW 9. INSPECTED AREA UNDER FLOORBOARDS IN CABIN AT ROW 9 AND FOUND RECIRC FAN MUFFLER NOT ATTACHED. RESECURED DUCT IAW AMM 21-20-01. NO SMOKE DETECTED, ONLY WATER VAPER FROM PACK SYSTEM.

Part: FLASHLIGHT — INOPERATIVE (COCKCPIT) · airframe 38,962 hrs · 36,155 cycles

CAPTAIN`S EMERGENCY FLASHLIGHT WILL NOT TURN ON. R & R CAPTAIN`S FLASHLIGHT, OPS CHECK GOOD.

Part: THERMOSTAT — FAILED (BLEED OVERTEMP) · airframe 38,784 hrs · 36,031 cycles

BLEED 2 OVERTEMP IN ICING ON CLIMBOUT. RETURNED TO DEPARTING AIRPORT. REPLACED FAN AIR VALVE CONTROL THERMOSTAT. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,651 hrs · 35,924 cycles

SERVICE DOOR EXTERIOR FLOOD LIGHT IS INOPERATIVE. R & R BULB. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,462 hrs · 35,776 cycles

RIGHT FWD WING TO FUSELAGE EMERGENCY FLOOD LIGHT NR 4 INOPERATIVE. R & R LIGHT BULB IN RT FWD WING TO FUSELAGE EMERGENCY LIGHT. OPS CHECK GOOD.

Part: FLASHLIGHT — INTERMITTENT (AFT CABIN) · airframe 38,316 hrs · 35,655 cycles

AFT CABIN FLASHLIGHT INTERMITTENT. R & R AFT CABIN FLASHLIGHT. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,314 hrs · 35,654 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FLIGHT ATTENDANT FLASHLIGHT IAW GHC.

Part: BATTERY — DISCHARGED (MAIN) · airframe 38,314 hrs · 35,653 cycles

BACK UP BATTERY SUPPLY HAS LOW VOLTAGE. R & R BACK UP BATTERY IAW AMM 24-35-01. OPERATIONALLY CHECKED GOOD.

Part: REINFORCEMENT — CRACKED (FUSELAGE) · airframe 38,314 hrs · 35,653 cycles

REINFORCEMENT FRAME ABOVE LT WINDSHIELD LATERAL POST CRACKED. R & R REINFORCEMENT ABOVE LATERAL POST IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,314 hrs · 35,653 cycles

RIGHT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2R. PERFORMED PERMANENT REPAIR IAW ERS-EM-53MR-1664.

Part: STRUCTURE — CORRODED (LAVATORY) · airframe 38,314 hrs · 35,653 cycles

LAVATORY WASTE BUCKET HAS CORROSION ON AFT SIDE OF FLAPPER VLV. PERFORMED PERMANENT REPAIR, INSTALLED DOUBLE IAW SRM 53-31-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,314 hrs · 35,653 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-1662.

Part: WIRE — BROKEN (CABIN) · airframe 38,314 hrs · 35,653 cycles

AFT EMER LIGHT STRIP HAS BROKEN WIRE. REPAIRED AFT EMER LIGHT STRIP BROKEN WIRE IAW SWPM 20-00-03.

Part: WEB — CHAFED (CARGO DOOR) · airframe 38,314 hrs · 35,653 cycles

BAGGAGE DOOR INNER WEB HAS MULTIPLE CHAFES. REPAIRED BAGGAGE DOOR INNER WEB CHAFES IAW ERS-EM-52MR-432.

Part: LIGHT — DAMAGED (CABIN) · airframe 38,314 hrs · 35,653 cycles

NUMBER 1 EMER LIGHT STRIP EXTRUSION DAMAGED. R & R EMER LIGHT STRIP NR 1 EXTRUSION IAW AMM 33-50-12. SEE NRWC BOW 201288 FOR INSTALLATION & OPERATIONS CHECK.

Part: WIRE — BROKEN (CABIN) · airframe 38,314 hrs · 35,653 cycles

LEFT NR 2 EMER FLOOR STRIP LIGHT WIRES ARE BROKE OFF. R & R LT NR 2 FLOOR EMER LIGHT STRIP IAW AMM 33-50-12. SEE NRWC BOW 201288 FOR OPERATIONS CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,314 hrs · 35,653 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AT FIRST FASTENER BELOW STRINGER 2L ON FRAME 75. CRACK IS APPROX 1/4" LONG. REPAIRED IAW ERS-EM-53MR-1662.

Part: SKIN — CRACKED (FUSELAGE) · airframe 38,314 hrs · 35,653 cycles

FUSELAGE EXTERNAL SKIN HAS POSSIBLE CRACK AT FRAME 75, STRINGER 2L. SEE NRTC E470588 FOR DOUBLER REPAIR OF FUSELAGE EXTERNAL SKIN CRACK AT FRAME 75, STRINGER 2L.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 38,073 hrs · 35,452 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R AFT CABIN FLASHLIGHT IN REFERENCE WITH AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: ECU — FAILED (TE FLAP) · airframe 37,918 hrs · 35,301 cycles

FLAP INDICATION ON EICAS TURNED AMBER & DASH AT THE SAME TIME AT FL 230. NO BACKUP INDICATION ON RMU. R & R FLAP ELEC CONTROL UNIT IAW AMM 27-53-02. OPERATIONS CHECKED GOOD, MEL 27-9 RESTORED. PARTS INTERCHANGEABLE IAW IPC & ETN EM-27-122.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 37,669 hrs · 35,082 cycles

CAPTAIN'S EMER FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S EMER FLASHLIGHT BULB IAW CMM 25-60-11.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 37,294 hrs · 34,733 cycles

GOT THE BAG SMOKE EICAS INDICATION WITH THE AURAL WARNING & THE BAG EXTING BUTTON ILLUMINATED. PRESSED THE BAG EXTING BUTTON IAW EPC & GOT A BAG EXTING LIGHT INOPERATIVE EICAS MSG. PERFORMED OPERATIONAL CHECK BAGGAGE SMOKE DETECTION SYS IAW AMM 26-15-00. OPERATIONS CHECKED GOOD. MELED BAGGAGE COMP EXT SYS PLACARD IAW MEL 26-09. R & R NR 1 & 2 SMOKE DETECTORS FOR BAGGAGE COMPARTMENT IAW MM 26-15-01. OPERATIONS CHECKED GOOD. R & R BAGGAGE COMPARTMENT FIRE EXT BOTTLES, HIGH RATE & METERING IAW MM 26-23-01. REF ITEM 1 LOG PAGE 3794321 FOR R & R OF SMOKE DETECTORS. MEL ITEM IS RESTORED. END CARGO AREA SMOKE DETECTOR PN 473597-13, SN 2911. FIRE BOTTLE 224 CU IN PN 337000271, SN 41965D1. FIRE BOTTLE 630 CU IN PN 346000731, SN 15691F1. CARTRIDGE PN M30903870.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,156 hrs · 34,589 cycles

FLIGHT ATTENDANT'S AFT CABIN FLASHLIGHT INOPERATIVE. R & R AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,084 hrs · 34,512 cycles

LEFT AFT WING TO FUSELAGE FAIRING EMER LIGHT IS INOPERATIVE. R & R LT AFT WING TO FUSELAGE FAIRING EMER LIGHT LAMP. OPERATIONS CHECKED GOOD IAW AMM 33-50-10.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,084 hrs · 34,512 cycles

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

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WING) · airframe 37,064 hrs · 34,491 cycles

WING ANTI-ICE FAIL CAUTION MSG WHEN TESTING SYS. FLIGHT CREW PLACARDED IAW MEL 30-01. REF ITEM NR 2, CLEARED PAC MEL & RETESTED SYS IN STANDARD BLEED CONFIGURATION. SURFACE ANTI-ICE OPERATIONS CHECKED OK IAW AMM 30-00-00-700-802A. MEL RESTORED.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 36,870 hrs · 34,310 cycles

PRESSURIZATION FAILED. MASKS DEPLOYED, EXCEPT SEATS 15 B & C. R & R PRESSURE REGULATOR & PNEUMATIC OUTFLOW VALVE IAW AMM 21-31-02 &21-31-04. PRESSURE SYS OPS CHECKED GOOD IN MANUAL & AUTO MODES IAW AMM 21-31-00.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 36,771 hrs · 34,227 cycles

COCKPIT FLASHLIGHT HOLDER BEHIND CAPTAIN`S SEAT BROKEN. FLASHLIGHT VERY LOOSE & FALLS OUT. R & R FLASH LIGHT HOLDER BEHIND CAPTAIN`S SEAT IAW AMM 33-50-16.

Part: BATTERY — DISCHARGED (CABIN) · airframe 36,616 hrs · 34,113 cycles

EMERGENCY LIGHT ON RT FWD FUSELAGE FAIRING INOPERATIVE. R & R NR 2 EMER BATTERY & CHARGER ASSEMBLY IAW WC 33-700-19. OPERATIONS CHECKED GOOD IAW WC 33-700-17. BATTERY CHARGER ASSEMBLY PN 11-0049, SN 20146.

Part: ENGINE — FAILED (RIGHT) · airframe 36,581 hrs · 34,089 cycles

NUMBER 2 PACK HAS OIL SMELL WHEN OPERATING. R & R RT ENG IAW WC 71-000-00. OPERATIONS CHECKED GOOD. NO LEAKS DETECTED.

Part: FLAPPER VALVE — FAULTY (WING) · airframe 36,152 hrs · 33,738 cycles

CAPTAIN DECLARED AN EMER & DIVERTED DUE TO A POSSIBLE FUEL LEAK. EMER OVERWEIGHT LANDING WAS ACCOMPLISHED. LANDING TOUCHDOWN WAS 45,000 LBS LESS THAN A 200 FT MIN DESCENT. TOUCHDOWN WAS ACCOMPLISHED SOFT LANDING. R & R LOWER RIB 19 FLAPPER VLV IAW AMM 28-11-04. LEAK CHECKED GOOD.

Part: FADEC — MALFUNCTIONED (NR 1 ENGINE) · airframe 34,980 hrs · 32,725 cycles

N1 DROP OFF 20% 86.7 TO 67 OCCURRED TWICE AT 37,000 WITH AUTO RELIGHT TWICE. R & R NR 1 ENG 1 A FADEC IAW MM 73-25-10-400-801. PERFORMED ENG POWER RUN UP IAW 72-00-00-700-801. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,860 hrs · 32,637 cycles

LEFT WING FWD EMERGENCY LIGHT INOPERATIVE. R & R LT WING FWD EMERGENCY LIGHT IAW AMM 33-50-10, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,785 hrs · 32,571 cycles

RIGHT FWD FUSELAGE EMERGENCY LAMP INOPERATIVE. R & R RT FWD FUSELAGE EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A & 33-50-10-000-801-A, OPERATIONS CHECKED GOOD.

Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 34,411 hrs · 32,274 cycles

DURING STICK PUSHER TEST WE RECEIVED SPS 1 - 2 INOPERATIVE WARNINGS & STICK PUSHER FAIL CAUTION. TRIED 4 UNSUCCESSFUL ATTEMPTS. TROUBLESHOOT IAW FIM TASK 27-36-00-810-808-A & FOUND TO BE A TRANSITORY CONDITION. SYS OPERATIONS CHECKED GOOD IAW AMM 27-36-00.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 34,382 hrs · 32,251 cycles

CAPTAIN`S FLASHLIGHT NOT SECURE IN HOLDER & NOT CHARGING. R & R CAPTAIN`S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD MEL IS RESTORED.

Part: UNKNOWN — SMOKE (NR 1 ENGINE) · airframe 34,309 hrs · 32,203 cycles

ON FLIGHT 3639 FIRST OFFICER NOTICE GREY SMOKE COMING FROM ENG NR 1 INLET. GVI OF THE INLET & OUTLET AREA OF THE NR 1 ENG, NO EVIDENCE OF ANY LEAK NOTED AREA WAS FOUND CLEAN & DRY AMM 71-00-00, RRMM 05-50-00.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 34,227 hrs · 32,141 cycles

DURING PS 2 CHECK FOUND FWD FLIGHT ATTENDANT`S FLASHLIGHT TO BE MISSING. INSTALLED NEW FLASHLIGHT ASSEMBLY IAW AE EMB-145 AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,009 hrs · 31,974 cycles

FLOOR PROXIMITY STRIP LIGHT AT 17A INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: RIB — CRACKED (RT WING) · airframe 33,915 hrs · 31,905 cycles

RT WING RIB 5 CRACKED. REPLACED RIB IAW EO EM-57MR-595.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 33,915 hrs · 31,905 cycles

CARGO DOOR FWD FRAME CORRODED AT FOUR NUTPLATES. REPAIRED IAW EO-EM-52MR-379.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 33,915 hrs · 31,905 cycles

LEFT ELEVATOR TOP SURFACE DENTED. REPAIRED IAW EO-EM-55MR-441.

Part: SKIN — DAMAGED (RUDDER) · airframe 33,915 hrs · 31,905 cycles

RUDDER SKIN DAMAGED. REPAIRED IAW EO-EM-55MR-439.

Part: LIGHT — BROKEN (CABIN) · airframe 33,900 hrs · 31,891 cycles

RIGHT NR 3 EMERGENCY LIGHT STRIP BROKEN. REMOVED AND INSTALLED SERVICABLE EMERGENCY LIGHT IAW AMM 33-50-12.

Part: PROFILE — CORRODED (DOOR FRAME) · airframe 33,900 hrs · 31,891 cycles

FRAME 65 LT PROFILE CORRODED AROUND CARGO DOOR SILL AREA. REPAIRED IAW EO EM-53MR-1129.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 33,900 hrs · 31,891 cycles

EMERGENCY LIGHT STRIP WIRING EXTENDING FROM UNDERFLOOR AT POSITIONS 2,3,4,AND 6 DAMAGED. REPAIRED WIRING IAW SWPM 20-50-01.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 33,900 hrs · 31,891 cycles

FWD EMERGENCY LIGHT WIRING CUT. REPAIRED WIRE IAW SWPM 20-50-01. OPS CHECKED.

Part: LIGHT — BROKEN (CABIN) · airframe 33,900 hrs · 31,891 cycles

RIGHT NR 1 EMERGENCY LIGHT STRIP BROKEN. R & R RT LIGHT STRIP IAW AMM 33-50-12.

Part: FLASHLIGHT ASSY — INTERMITTENT (COCKPIT) · airframe 33,885 hrs · 31,881 cycles

F/O'S FLASHLIGHT IS INTERMITTENT DURING USE. CONNECTED F/O'S FLASHLIGHT BATTERY OPS CHECKED GOOD IAW AMM 33-51-01

Part: PUMP — INOPERATIVE (NR 2 ENGINE FUEL) · airframe 33,622 hrs · 31,663 cycles

THE CREW REPORTED THE NR 2 ENGINE DURING ARE DECENT SURGED POWER AND IGNITIONS SWITCH BETWEEN A AND B ALL OTHER ENG IND WERE NORMAL. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 2 ENGINE FUEL PUMP METERING UNIT IAW MM 73-21-10-000-801. THE OPS CHECK WAS GOOD. NO FAULTS FOUND. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 33,104 hrs · 31,218 cycles

THE CREW REPORTED AN ABNORMAL ODOR STARTING AT ROW 11 AND STRONGER IN THE AFT AERA. THE ACFT WAS REMOVED FROM SERVICE. RAN BOTH A/C PACKS IN HOT & COLD MODES USING APU. ILLUMINATED ALL CABIN LIGHTS FOR TEST. UNABLE TO DISCERN ANY OFFENSIVE ODORS. OK FOR CONTINUED SERVICE. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,915 hrs · 31,053 cycles

ON FLIGHT 4172 THE CREW REPORTED THE COCKPIT HAS STRONG ODOR COMING FROM THE GASPER. THE SMELL MAY BE FROM LAVATORY FLUID. THE AIRCRAFT WAS REMOVED FROM SERVICE. SERVICED THE LAV, THE SMELL DISSIPATED FROM THE COCKPIT, NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 32,456 hrs · 30,692 cycles

DURING B INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 32,312 hrs · 30,588 cycles

ON FLIGHT 3247 THE CREW REPORTED AFTER LANDING DURING TAXI THEY RECEIVED AN EICAS MESSAGE "BAGG SMOKE" ILLUMINATED. CREW FOLLOWED AOM 1 PROCDURES AND DECLARED AN EMERGENCY REQUESTING CFR. DISCHARGED BOTTLE BAGGAGE SMOKE INDICATION WENT OUT AFTER ABOUT 5 MINUTES. THE FLIGHT ATTENDANT REPORTED NO FIRE OR SMOKE AFTER BEING ASKED TO INVESTIGATE. CFR FOUND NO EVIDENCE OF SMOKE OR FIRE. THE AIRCRAFT TAXIED TO THE GATE AND WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FWD CARGO COMPARTMENT SMOKE DETECTOR IAW EMB AMM 26-15-01. PART 473597-13. S/N 0064. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR AS PER EMB MM 26-15-01. OPS CHECK GOOD AT THIS TIME. PART 473597-13. S/N 3071. THE AIRCRAFT WAS RETURNED TO SE

Part: INVERTER — INOPERATIVE (CABIN) · airframe 32,281 hrs · 30,565 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT ABOVE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM TASK 33-50-00-700-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 32,272 hrs · 30,558 cycles

ON FLIGHT 3302 THE CREW REPORTED THAT ON SHORT FINAL FOR LANDING AT DFW THEY RECEIVED A FIRE INDICATION. THE CREW PERFORMED THE MEMORY ACTION ITEM TO EXTINGUISH A FIRE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE TOWER WAS NOTIFIED AND CFR WAS REQUESTED. THE CREW PERFORMED THE REMAINING CHECKLIST PER AOM VOL 1. CFR INSPECTED THE AIRCRAFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF BAGGAGE COMPARTMENT FIRE EXTINGUISHING SYSTEM AND LININGS IAW EMB 145 AMM 25-51-01 NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — DIRTY (CABIN) · airframe 32,242 hrs · 30,535 cycles

FOR FLIGHT 3325 THE CREW REPORTED THE AIRCRAFT CABIN HAD A STRONG ODOR OF FISH. THE CREW RECEIVED MANY COMPLAINTS FROM THE PASSENGERS. THE AIRCRAFT WAS REMOVED FROM SERVICE. INTERIOR CLEANING AND DISINFECTING OF FISH ODOR IAW STANDARD PRACTICES. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 32,217 hrs · 30,516 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY EXIT LIGHT ABOVE SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY AND BATTERY HOLDER ASSEMBLY IAW EMB145 AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL MODULE — DEFECTIVE (CABIN) · airframe 32,204 hrs · 30,507 cycles

DURING B INSPECTION FOUND THE EMERGENCY EXIT LIGHT SWITCH ON THE FLIGHT ATTENDANTS PANEL INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER CABIN LIGHTS CONTROL MODULE ASSEMBLY IAW AMM 33-21-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 32,074 hrs · 30,402 cycles

DURING B INSPECTION FOUND THE EMERGENCY EXIT SIGN ABOVE THE EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED SERVICE DOOR EMERGENCY LIGHT INVERTER CONNECTOR IAW EMB AMM TASK 33-50-11-400-801. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM TASK 33-50-00-700-801. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 31,446 hrs · 29,913 cycles

ON FLIGHT 3575 THE CREW REPORTED THAT AFTER LANDING WHILE TAXIING TO THE GATE THE BAGGAGE SMOKE WARNING CAME ON. THE AIRCRAFT WAS STOPPED AND THE AOM VOLUME 1 CHECKLIST WAS COMPLETED. AN EMERGENCY WAS DECLARED AND REQUESTED CRASH, FIRE AND RESCUE. THE CREW SENT AN ACARS MESSAGE TO MAINTENANCE TO ADVISE THE FIRE BOTTLES HAD BEEN USED. CRASH, FIRE AND RESCUE FOUND NO INDICATION OF HEAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO COMP FWD SMOKE DETECTOR IAW EMB145 26-15-01. THE SMOKE INDICATION MAY HAVE RESULTED FROM EXTREME HUMIDITY IN MIA. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,863 hrs · 29,467 cycles

DURING B INSPECTION, FOUND THE OVERHEAD EMERGENCY LIGHT IN GALLEY INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IAW AMM 33-50-09-000-801-A AND 33-50-09-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,618 hrs · 29,274 cycles

DURING B INSPECTION FOUND THE LAST TWO CEILING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED TWO EACH EMERGENCY CEILING LIGHTS IAW EMB145 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,495 hrs · 29,171 cycles

DURING MAINTENANCE INSPECTION, FOUND THE CENTER AISLE EMERGENCY CEILING LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CENTER AISLE EMERGENCY CEILING LIGHTS IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,214 hrs · 28,932 cycles

DURING B-INSPECTION FOUND THE EMERGENCY AISLE LIGHT INOPERABLE AT ROW 12. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AISLE EMERGENCY LAMP AT ROW 12 IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-00-700-801A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 30,146 hrs · 28,878 cycles

DURING B-INSPECTION FOUND THE EMERGENCY EXIT SIGN IN FRONT OF SEAT 3B INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT PER WM 33-50-50. REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER. THE OPERATIONAL CHECK WAS GOOD PER WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,146 hrs · 28,878 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT IN PSU ABOVE SEAT 12A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ROW 12A PSU EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD IAW AE WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,008 hrs · 28,767 cycles

DURING B-INSPECTION, FOUND THE OVERHEAD EMERGENCY LIGHT AT EMERGENCY EXIT DOOR-ON PSU PANEL -LT SIDE- INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 30,008 hrs · 28,767 cycles

DURING B-INSPECTION, FOUND THE AFT OVERHEAD AISLE EMERGENCY LIGHT NEAR LAVATORY INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED AFT OVERHEAD AISLE EMERGENCY LIGHT BULB IAW AMM 33-50-08. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,924 hrs · 28,692 cycles

DURING B-INSPECTION FOUND THE FURTHEST AFT CABIN CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IN AFT CABIN EMERGENCY CEILING LIGHT IAW EMB AMM TASKS 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: LIGHT — INOPERATIVE (CABIN) · airframe 29,822 hrs · 28,612 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT THE LAVATORY ENTRANCE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP AT LAV ENTRANCE IAW 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 29,774 hrs · 28,573 cycles

ON FLIGHT 3548 THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT CYCLE ON OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET SYSTEM AND THE OPERATIONAL CHECK WAS GOOD REF AMM 33-51-00 AND AMM 24-00-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (CABIN) · airframe 29,757 hrs · 28,561 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FORWARD SECTION OF THE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM IAW WORK CARD 33-700-17. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,657 hrs · 28,492 cycles

DURING B-INSPECTION FOUND THE EMERGENCY EXIT SIGN OVER SERVICE DOOR WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11. OPERATIONAL CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 27,503 hrs · 26,834 cycles

ON FLIGHT 3616 DESCENDING THROUGH FLIGHT LEVEL 240 THE CREW REPORTED A STRONG ELECTRIC ODOR IN THE COCKPIT AND CABIN. THE ODOR STARTED TO GO AWAY AROUND 13000 FEET. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. C/W ETN NO: EMB-72-034R4. NO ELECTRIC ODOR NOTED IN COCKPIT AND IN CABIN. NO PARTS REMOVED OR REPLACED. PASSED FUNCTIONAL CHECK FLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CABLE — OUT OF ADJUST (PAX DOOR) · airframe 27,436 hrs · 26,784 cycles

FOR FLIGHT 4005 DURING PRE FLIGHT INSPECTION FOUND THE MAIN PASSENGER DOOR LEVER STUCK HALFWAY THRU UNLOCKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. ADJUSTED CABLE D FOR THE MAIN DOOR IAW EMB 145 AMM 52-18-00-820-804. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRANSDUCER — WORN (NR 2 BRAKE) · airframe 27,266 hrs · 26,667 cycles

ON FLIGHT 4243 THE CREW REPORTED THE ANTISKID RELEASED BRAKES ON LANDING. THE BRAKING AIRCRAFT DID NOT DE-CELERATE NORMALLY. THE OUTBOARD BRAKE TEMPERATURE WENT UP AND INBOARD BRAKE TEMPERATURE DID NOT MOVE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 BRAKE WHEEL SPEED TRANSDUCER IAW EMB 145 AMM 324103. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 26,946 hrs · 26,440 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CENTER AISLE AFT EMERGENCY LIGHT MISSING LENSE AND BULB. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED BULB IN CENTER AISLE AFT EMERGENCY LIGHT IAW EMB 145 AMM 33-50-08-400-801-A. THE LENS WAS FOUND IN THE OVERHEAD BIN AND INSTALLED IAW EMBTASK 33-5008-400-802.

Part: WARNING SYSTEM — FALSE ACTIVATION (BRAKE SYS) · airframe 26,812 hrs · 26,344 cycles

ON FLIGHT 3696 DURING TAKEOFF ROLL THE CREW HEARD MASTER WARNING TAKEOFF FOR THE BRAKES ON THE AURAL WARNING UNIT. THE CREW OBSERVED THE BRAKE LIGHTS NOT ON AND THE PARKING BRAKE FULLY DOWN. THE CREW ELECTED TO DO A LOW SPEED ABORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESET ELECTRICAL POWER PERFORMED FIM TASK 31-51-00 NO DEFECTS NOTED AT THIS TIME. THE OPERATIONAL CHECK WAS GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 26,764 hrs · 26,310 cycles

ON FLIGHT 4108 - THE CREW REPORTED ON/AFTER TOUCHDOWN NO BRAKING AVAILABLE USING NORMAL BRAKING WITH EITHER CAPTAINS OR FIRST OFFICERS BRAKE PEDALS. NORMAL BRAKING RESUMED AT SLOW TAXI SPEED AND OPERATION AT GATE ARRIVAL. BRAKE DEGRADED MESSAGE ON EICAS ILLUMINATED BRIEFLY THEN WENT OUT WITH NO CREW ACTION. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TAXI CHECKS WITH FLIGHT CREW FOR OPERATION OF MAIN BRAKES. PERFORMED VISUAL INSPECTION OF MAIN BRAKES IAW EMB 145 AMM 32-41-00. ALL OPERATIONAL CHECKS WERE GOOD. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,134 hrs · 25,014 cycles

F/O'S FLASHLIGHT INOP.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,134 hrs · 25,014 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FIRST OFFICERS FLASHLIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS FLASHLIGHT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 24,658 hrs · 24,605 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING EXIT AFT EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED INVERTER NR 5 IAW AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 24,601 hrs · 24,548 cycles

DURING THE PRE-FLIGHT CHECK FOR FLIGHT 2754 THE CREW FOUND THAT THE EMERGENCY LIGHT ABOVE THE GALLEY SERVICE DOOR WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RESEATED THE EXIT SIGN CONNECTOR IAW AMM 33-50-14. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — PUNCTURED (LT WING) · airframe 24,454 hrs · 24,431 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THAT THE LEFT WING LOWER MAIN LANDING GEAR SKIN WAS DAMAGED DURING JACKING PROCEDURES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE LEFT WING LOWER MAIN LANDING GEAR SKIN IAW EO EM-57MR-460. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,454 hrs · 24,431 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM CORRODED FORWARD OF FRAME 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED CUT OUT, FABRICATED DOUBLER AND SHIMS AND INSTALLED REPAIR PIECES IAW EMB SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 24,454 hrs · 24,431 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CARGO DOOR LOWER CENTER SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. FABRICATED DOUBLER FOR THE DAMAGED AREA AND INSTALLED IAW EO EM-53MR-1452. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,454 hrs · 24,431 cycles

DURING MAINTENANCE BASE INSPECTION FOUND CORROSION UNDER CROSS BEAM AT FRAME 29 LEFT SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. ACCOMPLISHED REPAIR AT LEFT FRAME 29 OMEGA IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 24,107 hrs · 24,103 cycles

DURING PS1 CHECK THE RIGHT AFT EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT EMERGENCY EXIT SIGN. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-14-00-801-A AND AMM 33-50-14-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: AUDIO PANEL — MALFUNCTIONED (COCKPIT) · airframe 23,645 hrs · 23,635 cycles

ON FLIGHT 4003 THE CREW REPORTED EXCESSIVE STATIC OVER THE SPEAKERS WITH THE GPU AND WITH THE BATTERY ALONE. THE CREW STARTED THE APU AND NOTICED SMOKE COMING FROM THE FIRST OFFICERS PANEL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE DIGITAL AUTO PANEL AND THE AUDIO CONTROL PANEL IAW EMB-145 ACFT MM 23-51-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SKIN — DENTED (FUSELAGE)

DENT ON LT FUSELAGE BETWEEN FRAMES 66 AND 67L AND BETWEEN STRINGERS 19 AND 20L. PERFORMED CUT OUT OF THE SKIN TO REMOVE THE DAMAGE. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM. (K)

Part: SKIN — DAMAGED (FUSELAGE)

DENT ON THE LT FUSELAGE SKIN FWD OF FRAME 20 STRINGERS 15L AND 16L. PERFORMED CUTOUT TO REMOVE THE DAMAGE; FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (CARGO DOOR)

CARGO DOOR CUT OUT LOWER SILL CORRODED. REMOVED EXISTING LOWER SILL AND CLEANED THE AREA. POSTIONED NEW SILL AND ATTACHED. REPAIR DONE IAW SRM. (K)

Part: ACTUATOR — INOPERATIVE (HORIZONTAL STAB)

FLT 4241 - ORD - RETURN TO FIELD FOR BACK UP PITCH TRIM FAIL. REPLACED HORIZONTAL STABILIZER ACTUATOR IAW EMB 145 AMM 27-40-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: MECHANISM — DIRTY (COCKPIT) · airframe 12,368 hrs · 13,071 cycles

ON TAKEOFF THE FO SEAT SLID BACK UNCOMMANDED. INSPECTED CLEANED AND LUBED SEAT LOCKING MECHANISM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (SW21200502003) (K)

Part: CLAMP — SEPARATED (RT ENGINE) · airframe 12,076 hrs · 12,776 cycles

DURING CLIMB FROM ORD ENTERED ICING CONDITIONS. HEARD A LOUD (POP) NOISE FROM BACK. BLD (2) LK ON EICAS. NOISE WAS LOUDEST OVER WING AND PASSENGERS SEAT AT WING REPORTED FEELING VERY HOT RUSH OF AIR FROM ABOVE. INSPECTED AND FOUND BAD BLEED LINE CLAMP AND SLEEVE. REPLACED BOTH CLAMP AND SLEEVE AS WELL AS PANEL DAMAGED WHEN CLAMP SEPARATED. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (K)

Part: TUBE — SEPARATED (BLEED TUBE) · airframe 12,073 hrs · 12,773 cycles

AFTER TAKEOFF, CREW REPORTED LOUD BANG FOLLOWED BY A BLEED 1 LEAK MESSAGE, CREW FOLLOWED AOM PROCEDURE AND MESSAGE DID NOT EXTINGUISH FOLLOWED AOM FOR A PRECAUTIONARY ENGINE SHUTDOWN. FA REPORTED VIBRATION IN THE CABIN NOT FELT BY THE CREW. INSPECTED AND FOUND BLEED TUBE ASSY JOINT BLOWN OPEN AND SEPARATED REMOVED AND REPLACED BLEED TUBE IAW AMM. OPS CHECK AND LEAK CHECKS WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB)

ORD - FLT 4190 - CREW NOTED A DUAL PITCH TRIM FAIL IN FLIGHT. CREW RESET THE SYSTEM AND CONTINUED WITH NO OTHER FAULTS REPORTED. REPLACED HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — LOOSE (EMERGENCY SIGN)

ORD - FLT 4315 - CREW REPORTED THE RIGHT EMERGENCY EXIT SIGN ON EMERGENCY EXIT OVERWING DOOR TO BE INOPERATIVE. MAINTENANCE FOUND CONNECTOR FOR EMERGENCY SIGN LOOSE. RECONNECTED CONNECTOR AND COMPLIED WITH AN OPERATIONAL CHECK WITH NO DEFECTS NOTED. (M)

Part: LIGHT — INOPERATIVE (CABIN)

ORD - FLT 4348 - CREW REPORTED THE LAST ROW OF FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 7 FLOOR STRIP LIGHT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE (M)

Part: SKIN — DENTED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, A DENT WAS DISCOVERED BETWEEN FRAMES 68 AND 70 AND BETWEEN STRINGERS 19L AND 20L. AFTER RECONTOURING PER EMB GST-2624/02 FOUND SKIN TO BE OIL CANNED. PERFORMED EDDY CURRENT INSPECTION OF THE REWORKED AREA WITH NO DEFECTS NOTED. FABRICATED A REPAIR 'L' ANGLE. REPAIR DONE IAW EMB GST-2666/02 AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - FOUND CARGO DOOR CUT OUT LOWER SILL CORRODED. REPLACED SILL BEAM IAW EMB 145, SRM 145/1142, CHAPTER 51, REV 19, 51-40-02 AND STANDARD SRM PRACTICES. (M)

Part: CLIP — CORRODED (FUSELAGE)

ABI - FOUND FRAME 68 SHEAR CLIP CORRODED. INSTALLED NEW SECTION OF SHEAR CLIP IAW EMB GST 2686/02 PARA 2, AND EMB GST-2271/02A AND STANDARD SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE)

ABI - FOUND CORROSION WAS FOUND ON THE SERVICE DOOR CENTER SILL. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW AEAI ETN NR EM-53-036, AND STANDARD EMB 145 SRM PRACTICES. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, CARGO ENTRY WAY LOWER SILL CORRODED. REPLACED LOWER SILL BEAM IAW EMB 145 SRM 51-40-02. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, CROSSBEAM AND PROFILE AT FRAME 23 CORRODED. INSTALLED SERVICEABLE CROSSBEAM AND PROFILE IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

THIS IS A LEVEL 2 FINDING. AFT CARGO ENTRY GUSSET CORRODED. INSTALLED SERVICEABLE AFT CARGO ENTRY GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

LEVEL 2 FINDING, RIGHT AFT SILL HAS CORROSION. REPLACED RIGHT AFT SILL IAW EMB 145 SRM 51-40-02. (M)

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2

ABI - LEVEL 2 FINDING, GALLEY RAMP SUPPORT CORRODED. REPLACED GALLEY RAMP SUPPORT IAW EMB 145SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - LEVEL 2 FINDING, RIGHT FORWARD SILL HAS CORROSION. REPLACED RIGHT FORWARD SILL IAW EMB 145 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

LEVEL 2 FINDING, CENTER BEAM GUSSET HAS CORROSION. REPLACED CENTER BEAM GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

LEVEL 2 FINDING, AFT DIAMOND GUSSET HAS CORROSION. REPLACED AFT DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2

ABI - THIS IS A LEVEL 2 FINDING, RIGHT BEAM HAS CORROSION AT FRAME 23. INSTALLED REPAIR DOUBLER IAW EMB GST-2615/02. (M)

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2

LEVEL 2 FINDING, FORWARD DIAMOND GUSSET HAS CORROSION. REPLACED FORWARD DIAMOND GUSSET IAW EMB 145 SRM 51-40-02. (M)

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2

ABI - LEVEL 2 FINDING, LEFT SILL HAS CORROSION. REPLACED LEFT SILL IAW EMB145 SRM 51-40-02. (M)

Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2

ABI - FOUND CORROSION ON RIGHT HAT BEAM AT FRAME 22, LEVEL 2 FINDING. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT HAT BEAM AT FRAME 22 IAW EMB 145 SRM 53-21-10, 51-40-02 AND ETN EM 53-034. (M)

Part: WIRE — BROKEN (EMERGENCY LIGHTS)

CREW REPORTED THE LAST STRIP OF FLOOR PROXIMITY EMERGENCY LIGHTING TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE ON THE STRIP LIGHT. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CAP — CORRODED (LT MLG)

ABI - FOUND LEFT MAIN LANDING GEAR FORWARD LOWER BEARING CAP CORRODED. REMOVED AND REPLACED SERVICEABLE LEFT MLG FORWARD LOWER BEARING CAP IAW EMB 145 AMM. (M)

Part: CAP — CORRODED (RT MLG)

ABI - FOUND BOTH FORWARD AND AFT LOWER BEARING CAPS ON RIGHT MLG CORRODED. REMOVED AND REPLACED BOTH FORWARD AND AFT LOWER BEARING CAPS ON RIGHT MLG IAW EMB145 AMM. (M)

Part: SWITCH — FAILED (NR 2 T/R)

ORD - FLT 4211 - CREW REPORTED THE NR 2 THRUST REVERSER DISAGREE MESSAGE ON TAKEOFF ROLL. REMOVED AND REPLACED NR 2 ENGINE UPPER AND LOWER THRUST REVERSER STOW SWITCHES (S/N 1361 AND 1402) IAW AMM. OPS CHECK GOOD. (M)

Part: IFS — INOPERATIVE (NR 2)

MGM - FLT 3479 - EN ROUTE FROM DFW TO SAV, RECEIVED AHARS BASIC MODE MESSAGE AND FIRST OFFICERS INSTRUMENTS WENT BLACK. BOTH ALTIMETERS READING INACCURATE DATA DIVERTED TO MGM. NO CFR OR EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED AHARS UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY)

ORD - FLT 4232 - AFTER LANDING CREW HAD SMOKE WARNING INDICATION IN CARGO COMPARTMENT. THE CREW AT THAT TIME BLEW THE CARGO FIRE BOTTLES. MAINTENANCE INSPECTED AND FOUND NO FIRE IN THE AREA. MAINTENANCE REMOVED AND REPLACED FORWARD SMOKE SENSOR IAW EMB MM. OPERATIONAL CHECK WAS GOOD. FIRE BOTTLES WERE REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CHARGER — INOPERATIVE (CABIN)

ORD - FLT 4254 - CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 1 AND 2 BATTERY PACK ASSEMBLIES. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (CABIN)

ORD - FLT 4254 - CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NUMBER 1 AND 2 BATTERY PACK ASSEMBLIES. OPERATIONAL CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA1774. (M)

Part: BATTERY — FAILED (CABIN)

ORD - FLT 4254 - COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED NR ONE BATTERY AND FUSE. OPS CHECK GOOD. REF: OPER CONTROL NR 20000519SH002. (X)

Part: FUSE — FAILED (LIGHT)

ORD - FLT 4254 - COCKPIT OVERHEAD EMERGECY LIGHTS INOPERATIVE. REPLACED NR 1 BATTERY AND FUSE. OPS CHECK GOOD. REF: OPER CONTROL NR SIMA1242. (X)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

ORD - FLT 4327 - BAGGAGE SMOKE LIGHT CAME ON WHILE AT GATE. REMOVED AND REPLACED REAR SMOKE DETECTOR. OPS CHECK GOOD. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

STL - FLT 4123 - BAGGAGE SMOKE WARNING INDICATION ACTIVATED. FIRE EXTINGUISHER DISCHARGED. DIVERTED TO STL. INSPECTED AND FOUND NO EVIDENCE OF SMOKE OR FIRE. MEL'D SYSTEM AND FLIGHT CONTINUED TO XNA. ON 11-20-99, REMOVED AND REPLACED NR 1 BAGGAGE SMOKE DETECTOR. MEL RESTORED AND AIRCRAFT WAS AGAIN RETURNED TO SERVICE. (X)