N676AE

Part: VALVE — LEAKING (NR 1 ACM) · airframe 40,695 hrs · 36,574 cycles

LOUD NOISE AFTER STARTING ENGINE NR 2 FOLLOWED BY A VERY STRONG FISHY SMELL. PERFORMED GVI OF BOTH PACK DUCTS IAW EMB 145 AMM 21-51-14-200-801-A WHILE RUNNING PACKS ON APU THEN ENG BLEEDS W/ CREW. NO LOUD NOISE OR SMELL PRESENT, BUT SLIGHT LEAK OF NR 1 DUAL TEMP VALVE. DEFERRED PACK 1.

Part: NONE — NONE · airframe 40,475 hrs · 36,318 cycles

AFT EMERGENCY FLASHLIGHT HOLDER BROKEN.-C/A-RAR CABIN AFT EMERGENCY FLASHLIGHT AND BASE. OPS CHECKED GOOD IAW AMM 33-50-16.

Part: FLASHLIGHT ASSY — INOPERATIVE (FWD CABIN) · airframe 39,970 hrs · 35,728 cycles

FWD CABIN EMERGENCY FLASHLIGHT WILL NOT CHARGE REF: LOGPAGE 4702705 ITEM 1 MEL 2532 - AUTH# 070310M-C-C/A-RAR FWD CABIN EMEREGENCY FLASHLIGHT ASSY IAW EMB 145 AMM 33-50-16 MEL RESTORED

Part: FLASHLIGHT — INOPERATIVE (FWD CABIN) · airframe 39,924 hrs · 35,677 cycles

CABIN FORWARD FLASHLIGHT INOP-C/A-DEFERRED FWD CAB FLASHLIGHT. M PROCEDURE C/W

Part: WARNING LIGHT — FALSE INDICATION · airframe 39,458 hrs · 35,147 cycles

BLEED 2 FAIL ON TAKE-OFF ROLL AT 70 KNTS , TO-1 WAS SELECTED DUE TO PERFORMANCE MESSAGE WENT AWAY REJECTED TAKE-OFF.-C/A-DEFERRED ENGINE 2 BLEED SYSTEM, M PROCEDURES COMPLIED WITH. MEL# 36-03 AUTH# 040364DM-C

Part: WARNING MESSAGE — FALSE ACTIVATION (STAB TRIM) · airframe 39,049 hrs · 34,702 cycles

ABORTED TAKEOFF AT 40 KTS DUE TO WARNING MASTER LIGHT AND THEN 'TRIM' AURAL MESSAGE. THE TRIM WAS SET TO 8 UP. C/A: PERFORMED OPERATIONAL CHECK OF THE HORIZ STAB TAKE OFF TRIM AURAL WARNING, IAW EMB 145 AMM 27-40-00-700-805-A, NO DEFECT NOTED. AIRCRAFT OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION · airframe 38,389 hrs · 34,034 cycles

DURING FCF AURAL WARNING OF TOO LOW TERRAIN, STARTED AT 10,000 FT AND STOPPED AT 22,000 FT. NO AURAL WARNINGS AT 20,000 FT. DURING DESCENT, WARNING OCCURED AT 29000 FT FOR TOO LOW TERRAIN. SINK RATE AND PULL UP. EVENT OCCURED AGAIN AT 19500 FT AND 5000 FT. AT 2000 FT THE RA CALLED OUT 500 FT. AT 500 FT IT CALLED OUT MINIMUMS EVEN THOUGH RA WAS SET TO 200 FT. C/W WORK SCOPE REVISION 1. NO DEFECTS NOTED AT THIS TIME. REFERENCE NRWC 676-ORD-0433 FOR EGPWS COMPUTER CANNED FROM N684JW. OPS CHECK GOOD.

Part: SKIN — GOUGED (FRAMES 6-7) · airframe 37,774 hrs · 33,444 cycles

FUSELAGE SKIN IS GOUGED JUST BELOW PANEL 113EL AT FRAMES 6-7 BETWEEN STRINGERS 13L-15L-C/A-ACCOMPLISHED PERMANENT REPAIR ON FUSELAGE SKIN GOUGE JUST BELOW PANEL 113EL AT FRAMES 6-7 BETWEEN STRINGERS 13L-15L IAW ERS-EM-53MR-4019

Part: BEAM — CORRODED (FRAME 29) · airframe 37,774 hrs · 33,444 cycles

CENTER OMEGA BEAM IS CORRODED AT FRAME 29-C/A-ACCOMPLISHED REPAIR TO CENTER OMEGA BEAM CORROSION AT FRAME 29 IAW ERS-EM-53MR-4017 PT. A REV: ORIGINAL

Part: CROSSBEAM — CORRODED (FRAME 49) · airframe 37,774 hrs · 33,444 cycles

CENTER OMEGA BEAM CORRODED AT CROSS BEAM FRAME 49-C/A-ACCOMPLISHED REPAIR OF CENTER OMEGA BEAM CROSS BEAM FRAME 49 IAW EMB 145 SRM 53-00-10 FIG 203 AND ERS-EM-5300-4002 FOR USE OF ALTERNATE FASTENERS

Part: FLOORBEAM — CORRODED (FRAME 29) · airframe 37,774 hrs · 33,444 cycles

LH OMEGA BEAM IS CORRODED AT FRAME 29-C/A-ACCOMPLISHED REPAIR TO LH OMEGA BEAM CORROSION AT FRAME 29 IAW ERS-EM-53MR-4020 PT. A REV: ORIGINAL

Part: BEAM — CORRODED (FRAME 29) · airframe 37,774 hrs · 33,444 cycles

LH OMEGA BEAM IS CORRODED AT FRAME 29-C/A-ACCOMPLISHED REPAIR TO LH OMEGA BEAM CORROSION AT FRAME 29 IAW ERS-EM-53MR-4020 PT. A REV: ORIGINAL.

Part: RIB — CRACKED (LT WING) · airframe 37,774 hrs · 33,444 cycles

LH WING RIB 21 FOUND CRACKED INSIDE PANEL 551CB-C/A-ACCOMPLISHED DOUBLER REPAIR OF LH WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4.

Part: SKIN — DAMAGED (FRAMES 27-28) · airframe 37,774 hrs · 33,444 cycles

THREE SHARP PROTRUSIONS WERE FOUND IN THE FUSELAGE SKIN BETWEEN FRAMES 27-28 AND STRINGERS 18L-19L-C/A-FORWARD PROTRUSION FOUND TO BE OUT OF LIMITS IAW EMB 145 SRM 53-22-10. ACCOMPLISHED SMALL SKIN DOUBLER AND FILLER REPAIR IAW EMB 145 SRM 53-22-01. CENTER PROTRUSION FOUND TO BE WITHIN ALLOWABLE LIMITS IAW EMB 145 SRM 51-10-02 AND SRM 53-00-00. AFT PROTRUSION RE-CONTOURED AND INSTALLED FASTENER REPAIR IAW EMB 145 SRM 51-10-08.

Part: FRAME — CRACKED (FRM 66) · airframe 37,774 hrs · 33,444 cycles

DURING HMBV INSPECTION, QA FOUND FRAME 66 IS CRACKED AT STRINGER 16R. -C/A-REMOVED AND REPLACED FRAME 66 IAW EMB 145 SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 37,774 hrs · 33,444 cycles

DURING HMBV INSPECTION, QA FOUND THE LH OMEGA BEAM CORRODED AT CROSS MEMBER FR-59-C/A-ACCOMPLISHED A PERMANENT REPAIR ON THE LH OMEGA BEAM AT CROSS MEMBER FR-59 IAW EO-EM-53MR-1518 PT.A

Part: BEAM — CORRODED (FRAME 54) · airframe 37,774 hrs · 33,444 cycles

HMBV INSPECTION, QA FOUND THE LH OMEGA BEAM CORRODED DURING UNDER CROSS MEMBER AT FR 54-C/A-ACCOMPLISHED A PERMANENT REPAIR ON THE LH OMEGA BEAM UNDER CROSS MEMBER FR54 IAW EMB 145 SRM 53-00-10 FIG 202 SHEET 2.REPAIR MATERIALS: FILLER; ALCLAD 2024T3 0.SHIM; ALCLAD 2024T3 0.039EXTERNAL ANGLE; ALCLAD 2024T3 0.050

Part: DOOR SILL — CORRODED (FRAMES 65-68) · airframe 37,774 hrs · 33,444 cycles

DURING HMBV INSPECTION, QA FOUND THE CARGO DOOR SILL CORRODED-C/A-REMOVED AND REPLACED THE CARGO DOOR SILL IAW EMB 145 SRM 51-40-02. REPLACEMENT SILL P/N 145-25480-603SD

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 37,774 hrs · 33,444 cycles

DURING HMBV INSPECTION, QA FOUND THE CARGO DOOR CUTOUT FR 65 SHEAR CLIP CORRODED-C/A-PERFORMED A PERMANENT REPAIR ON THE CARGO DOOR CUTOUT FR 65 SHEAR CLIP IAW EMB 145 SRM 53-31-04 ITEM 4. SHEAR CLIP REPAIR P/N 145-25175-001

Part: SHUNT — CORRODED (FRAME 80) · airframe 37,774 hrs · 33,444 cycles

DURING ACCOMPLISHMENT OF EO-2400-018 (APU SHUNT GROUND IMPROVEMENT), FOUND THE APU SHUNT AREA ON FR 80 TO BE CORRODED-C/A-ACCOMPLISHED APU SHUNT REPAIR ON FR 80 IAW EMB 145 SRM 53-32-04 STEP 3 AND DET. E, SECTION A-A PAGE 208. REPAIR MATERIALS;DOUBLER: AL CLAD 2024 T3 ? 0.063?FILLER: AL CLAD 2024 T3 ? 0.040

Part: SKIN — DENTED (FRAMES 15-16) · airframe 37,774 hrs · 33,444 cycles

AIRCRAFT ARRIVED WITH TDMI 676T5345 TO REPAIR A DENT TO THE RH CENTER FUSELAGE BETWEEN FR 15-16 AND STGR 12R-13R-C/A-PERFORMED PERMANENT REPAIR ON DENT ON RH CENTER FUSELAGE BETWEEN FR 15-16 AND STGR 12R-13R IAW EMB 145 SRM 53-21-01 FIGURE 202. REPAIR MATERIALS: FILLER 2024-T3 0.032 DOUBLER 2024-T3 0.050

Part: WIRE — BROKEN (FLASHLIGHT ASSY) · airframe 37,774 hrs · 33,444 cycles

AFT EMERGRNCY FLASHLIGHT BASE (SP3558)WIRE SPLICE BROKEN-C/A-COMPLETE:REPAIRED WIRE W775-0006-24BK/SP3558 ON AFT EMERGENCY FLASHLIGHT BASE IAW EMB 145 SWPM 20-21-00 AND WM 33-51-50

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 37,774 hrs · 33,444 cycles

OVERWING CABIN CEILING PANEL FWD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE-C/A-COMPLETE:CONNECTED CABIN OVERWING CEILING PANEL FWD EMERGENCY LIGHT AS REQUIRED IAW EMB 145 AMM 33-50-15 AND WM 33-50-50. OPS CHECK GOOD

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,774 hrs · 33,444 cycles

1EA PROX LIGHT WITH OUT ARROWS HAVE BROKEN WIRES-C/A-COMPLETE:REMOVED AND REPLACED 1EA PROX LIGHT WITHOUT ARROWS IAW EMB 145 AMM 33-50-12. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 37,774 hrs · 33,444 cycles

LH NO. 3 EMERGENCY LIGHT STRIP DOES NOT ILLUMINATE-C/A-COMPLETE:SPLICED BROKEN WIRE W192-8679-22 AT LH FR 32/33 IAW EMB 145 SWPM 20-21-00, WM 33-50-50, AMM 33-50-00. OPS CHECK GOOD EASI # 7249

Part: FLOOR SUPPORT — CORRODED (FRAME 44) · airframe 37,774 hrs · 33,444 cycles

SSI #53-20-11 L/H OMEGA BEAM CORRODED AT CROSS BEAM FR-44-C/A-COMPLETE:ACCOMPLISHED PERMANENT REPAIR ON L/H OMEGA BEAM CORRODED AT CROSS BEAM AT FR-44 IAW ERS-EM-53MR-4018. SEE TURNOVER FOR DETAILS

Part: INVERTER — INOPERATIVE (CABIN) · airframe 37,162 hrs · 32,914 cycles

#1 FLOOR PROX EMERG LIGHT STRIP IS INOP. C/A-REMOVED AND REPLACED #2 DC/AC EMERGENCE EXIT LIGHTING INVERTER. OPS CHECKED GOOD IAW AMM 33-50-11.

Part: TANK UNIT — FAILED (NR 2 FUEL TANK) · airframe 36,576 hrs · 32,432 cycles

FUEL IND TANK NO 2 SHOWING DASHES. REMOVED AND REPLACED R/H TANK UNIT #4 IAW AMM 28-41-02. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,848 hrs · 31,662 cycles

EMERGENCY LIGHT OVER SERVICE DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT MARKING LIGHT. OPC GOOD IAW AMM 33-50-14.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,668 hrs · 31,456 cycles

STRONG BURNING / MILDEW MOLDY SMELL DURING VECTORS TO APPROACH AND LAND. OCCURRED AFTER MODERATE TURB DURING DESENT. WITH CONSTANT AND CONTINUOUS THRUST LEVER MOVEMENTS.AIRCRAFT REQUIRES INSPECTION FOR FERRYFLIGHT. REFERENCE LOG PAGE 4445943 ITEM-C/A-THIS AIRCRAFT HAS BEEN INSPECTED TO THE EXTENT NECESSARY FOR A FERRY FLIGHT AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT.

Part: HYDRAULIC SYSTEM — LEAKING · airframe 35,668 hrs · 31,456 cycles

INBND MIA DECLARED EMRGENCY FOR BURNING OIL SMELL. LNDD SAFELY.IN REFERENCE TO LG PG 4445943 ITEM 1 STRONG BURNING SMELL, FOUND EVIDENCE OF A POSSIBLE EXTERNAL HYDRAULIC LEAK DOWN THE BOTTOM OF THE FUSELAGE LEADING TO THE APU.CHECK GALLEY ARE FOR EVIDENCE OF SMELL . REFER TO TECH SUPPORT WORK SCOPE REV. 1.-C/A-INSPECTED GALLEY FOR SMEELS AND FOUND NO ABNORMAL SMELLS PRESENT, NO DEFECT NOTED

Part: UNKNOWN — ODOR (CABIN) · airframe 35,620 hrs · 31,424 cycles

ON DESCENT AT FLIGHT IDLE, MUSKY SMELL / ODOR FOR ABOUT A MINUTE, WENT AWAY WHEN TAKEN OUT OF IDLE. NO NOTICE OF SMELL AFTER LANDING / TAXI. TRANSFERED TO NRWC # 676-MIA-03291.-C/A-PERFORMED INSPECTION OF L/H AND R/H ENGINES IAW RRMM 72-00-00-200-802. PERFORMED ENGINE RUNS ON L/H AND R/H ENGINES IAW RRMM 72-00-00 AND USING ETN EM-72-034, ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT. REMOVED CABIN FLOOR PANELS AND INSPECTED AIR CONDITIONING DUCTS FOR DAMAGE. NO DEFECTS NOTED. PERFORMED INSPECTION OF L/H AND R/H ENGINES IAW RRMM 72-00-00-200-802. PERFORMED ENGINE RUNS ON L/H AND R/H ENGINES IAW RRMM 72-00-00 AND USING ETN EM-72-034, ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT. REMOVED CABIN FLOOR PANELS AND INSPECTED AIR CONDITIONING DUCTS FOR DAMAGE. NO DEFECTS NOTED. PERFORMED BORESCOPE OF L/H & R/H COOL FRONT SUMP AREA FOR OIL INDICATION I.A.W. RR MM 72-30-00-200-803. NO OIL INDICATIONS FOUND AT THIS TIME. REINSTALLED CABIN FLOOR PANEL 251BF IAW AMM 53-01-02.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,620 hrs · 31,424 cycles

ON DESCENT AT FLIGHT IDLE, MUSKY SMELL / ODOR FOR ABOUT A MINUTE, WENT AWAY WHEN TAKEN OUT OF IDLE. NO NOTICE OF SMELL AFTER LANDING / TAXI. TRANSFERED TO NRWC # 676-MIA-03291.-C/A-PERFORMED INSPECTION OF L/H AND R/H ENGINES IAW RRMM 72-00-00-200-802. PERFORMED ENGINE RUNS ON L/H AND R/H ENGINES IAW RRMM 72-00-00 AND USING ETN EM-72-034, ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT. REMOVED CABIN FLOOR PANELS AND INSPECTED AIR CONDITIONING DUCTS FOR DAMAGE. NO DEFECTS NOTED. PERFORMED INSPECTION OF L/H AND R/H ENGINES IAW RRMM 72-00-00-200-802. PERFORMED ENGINE RUNS ON L/H AND R/H ENGINES IAW RRMM 72-00-00 AND USING ETN EM-72-034, ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT. REMOVED CABIN FLOOR PANELS AND INSPECTED AIR CONDITIONING DUCTS FOR DAMAGE. NO DEFECTS NOTED. PERFORMED BORESCOPE OF L/H & R/H COOL FRONT SUMP AREA FOR OIL INDICATION I.A.W. RR MM 72-30-00-200-803. NO OIL INDICATIONS FOUND AT THIS TIME. REINSTALLED CABIN FLOOR PANEL 251BF IAW AMM 53-01-02.

Part: UNKNOWN — ODOR (CABIN) · airframe 35,613 hrs · 31,420 cycles

STRONG CHEMICAL ODOR IN COCKPIT AND CABIN ON DESCENT ENGINES WERE AT IDOL WHEN ODOR WAS FIRST SMELLED.-C/A-PERFORMED ENGINE RUNS AS PER ETN-EM-72-034. NO ODOR DETECTED AT ANY ENG. SETTING. AIRCRAFT O.K. FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,599 hrs · 31,409 cycles

SERVICE DOOR EMERGENCY LIGHT INOP-C/A-REMOVD AND REPLACED SERVICER DOOR EMERGENCY LIGHT IAW EMB 145 AMM 33-50-09-000-801 AND 33-50-09-400-801 OPS CHECK GOOD

Part: BONDING JUMPER — BROKEN (OUTFLOW VALVE) · airframe 35,242 hrs · 31,072 cycles

SUPPLEMENTAL AT 36000 CABIN ALTITUDE WENT TO 10000 GOT A MASTER WARNING. C/A-DEFERRED PRESSURIZATION CONTROL SYS AUTOMATIC MODE (M) CW. MEL 21-17 AUTH 100429DM-C. FOUND BONDING JUMPER TO BE BROKEN AND STUCK IN ELECTRO-PNEUMATIC OUTFLOW VALVE. R&R BONDING JUMPER IAW AMM 20-13-21. OPC GOOD IAW AMM 21-31-00. MEL ITEM RESTORED.

Part: ROLLER — DIRTY (MAIN DOOR) · airframe 34,729 hrs · 30,617 cycles

MAIN DOOR DIFFICULT TO CLOSE. CLEAN AND SERVICED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,666 hrs · 30,548 cycles

MAIN DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED MAIN DOOR EMERGENCY LIGHT IAW AMM 33-50-06-000-801-A AND 33-50-06-400-801-A. OPC OF LIGHT LAMP GOOD AT THIS TIME.

Part: DOOR SEAL — LACK OF LUBE (MAIN ENTRY DOOR) · airframe 34,590 hrs · 30,475 cycles

FA REPORTS MAIN ENTRY DOOR VERY HARD TO OPEN & CLOSE. MAIN ENTRY DOOR SEAL AND FOLDABLE DOOR LUBRICATED IAW AMM 52-11-00 OPENING AND CLOSING CHECK PASS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,461 hrs · 30,372 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-09-000-801-A, AND 33-50-09-400-801-A. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,161 hrs · 30,051 cycles

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

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT CARGO) · airframe 34,052 hrs · 29,962 cycles

CARGO SMOKE ILLUMINATED ON EICAS, BOTTLES BLOWN, WARNING ON BOTH EICAS AND CARGO EXTNGUISHING BUTTON. CARGO SMOKE DETECTOR AND RELAYS K0630, K0625, K0629 HAVE BEEN REMOVED AND REPLACED IAW AMM 26-23-01, AMM 26-15-01, AMM 26-15-50. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,982 hrs · 29,885 cycles

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

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 33,804 hrs · 29,728 cycles

AFT CABIN FLASHLIGHT INOP. REMOVED AND REPLACED AFT CABIN FLASHLIGHT BULB IAW AMM 33-50-16. OPS CK GOOD MEL RESTORED.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 33,514 hrs · 29,520 cycles

MAIN CABIN PAX ENTRY DOOR WONT OPEN ALL THE WAY, PLASTIC PIECE IN THE WAY. REMOVED THE DOOR TRIM AND REMOVED AND REPLACED MAIN DOOR HINGE PANEL IAW AMM 25-23-04.

Part: ACM — FAILED (NR 2) · airframe 33,442 hrs · 29,455 cycles

DURING TAXI, RECEIVED A BOTH ENGINES OFF, SMOKE IN THE COCKPIT AND CABIN. FOLLOWED EPC PROCEDURES FOR CABIN COCKPIT FIRE, SMOKE, FUMES, AND SMOKE SUBSIDED. RAN ENGINES AT IDLE AND HIGH POWER WITH NO ABNORMAL ODORS OR HAZE IN CABIN OR FLIGHT DECK IAW AMM 71-00-01. THE NR 2 PACK WAS MAKING A LOUD NOISE WITH THE NR 2 PACK FAILED MESSAGE. REMOVED AND REPLACED THE NR 2 AIR CYCLE MACHINE IAW AMM 21-51-03. OPS CHECKED GOOD.

Part: LIGHT — SMOKE (CHART HOLDER) · airframe 33,412 hrs · 29,436 cycles

SMOKE FROM FIRST OFFICER`S CHART HOLDER LIGHT WHEN ON. REMOVED AND REPLACED THE CHART HOLDER IAW AMM 25-12-11. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,028 hrs · 29,103 cycles

MAIN DOOR ENTRY EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-06-000-801-A, AND 33-50-06-400-801-A.. OPS CHECKED GOOD.

Part: SHEAR TIE — CRACKED (FRAME 68) · airframe 32,777 hrs · 28,855 cycles

SHEAR TIE AT FRAME 68 HAS A HAIRLINE CRACK IN THE RADIUS BETWEEN STRINGERS 7L-8L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · airframe 32,777 hrs · 28,855 cycles

CORROSION ON CENTER OMEGA BEAM AT BL 0, FRAME 20. REMOVED AND REPLACED THE OMEGA BEAM BETWEEN FRAMES 17 - 24 IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (FRAME 59-60) · airframe 32,777 hrs · 28,855 cycles

CORROSION AROUND THE LAVATORY FLOOR NUTPALTE HOLE. REPAIRED THE DAMAGE.

Part: FRAME — DENTED (FRM 66) · airframe 32,777 hrs · 28,855 cycles

AFT CARGO FUSELAGE FRAME 66 HAS A DENT AT STRINGERS 13 - 14R. REPAIRED THE FRAME IAW ETD 2017-145-068563, AND NCR-EM-53-034.

Part: SEAL REST — CORRODED (SERVICED DOOR) · airframe 32,777 hrs · 28,855 cycles

SERVICE DOOR FWD SEAL REST CORRODED. REMOVED CORROSION IAW SRM 51-10-03

Part: STRUCTURE — CORRODED (FRAMES 59-60) · airframe 32,777 hrs · 28,855 cycles

CORROSION RT OMEGA BEAM. REPAIRED IAW SRM 53-24-10, FIGURE 202.

Part: FLANGE — CORRODED (FRAME 20) · airframe 32,777 hrs · 28,855 cycles

CORROSION ON LEFT OMEGA BEAM INBD FLANGE AT FRAME 20. REMOVED CORROSION IAW SRM 51-10-03.

Part: RIB — CORRODED (PAX DOOR) · airframe 32,777 hrs · 28,855 cycles

PAX DOOR CORRODED INSIDE BOTTOM INTERNAL AREAS OF DOOR FRAME AROUND FOUR NUTPLATES. INSTALLED A NEW INTERNAL RIB ON THE LOWER AFT SIDE OF PAX DOOR IAW SRM 51-40-02.

Part: FLOOR SUPPORT — DAMAGED (FRAME 64) · airframe 32,777 hrs · 28,855 cycles

ELONGATED NUTPLATE HOLE AT FRAME 64 ON THE LT OMEGA BEAM. INSTALLED A NEW OMEGA BEAM FROM FRAMES 61 - 65 IAW SRM 51-40-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,441 hrs · 28,540 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R SIDE HINGED MAIN DOOR EXTERNAL EMERGENCY LAMP IAW AMM 33-50-10-000-801-A/33-50-10-400-801-A, OPS CHECKED GOOD

Part: LIGHT — DIM (CABIN) · airframe 32,223 hrs · 28,315 cycles

FORWARD FLOOR EMERG LIGHT STRIP DIM. REMOVED AND REPLACED FORWARD FLOOR EMERG LIGHT STRIP IAW AMM 32-50-12; OPS CK GOOD.

Part: SKIN — DENTED (FUSELAGE) · airframe 27,921 hrs · 23,889 cycles

FORWARD FUSELAGE 1 EXTERNAL SKIN HAS A DENT BETWEEN FRAME 3 - 4, BETWEEN STRINGER 13L - 15L. REPAIRED FWD FUSELAGE 1 EXTERNAL SKIN DENT IAW ERS-EM-53MR-1231.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,921 hrs · 23,889 cycles

FRAME 25 CRACKED BETWEEN STRINGERS 15R & 16R. INSTALLED SERVICEABLE FRAME SPLICE & NEW SERVICEABLE L DOUBLERS ON FRAME 25 IAW SRM 53-00-04 & ERS EM-53MR-1232.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,921 hrs · 23,889 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75. REPAIRED CRACKED LT FUSELAGE SKIN AT FRAME 75 & STRINGER 2L IAW ERS EM-53MR-1235.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 27,921 hrs · 23,889 cycles

BAGGAGE DOOR 3 NUTPLATE HOLES CORRODED ON FWD FRAME. PERFORMED REPAIR ON BAGGAGE DOOR FWD FRAME IAW ERS-EM-52MR-325.

Part: LIGHT — BROKEN (CABIN) · airframe 27,921 hrs · 23,889 cycles

EMERGENCY LIGHT STRIP 4 BROKEN. R & R EMER LIGHT STRIP 4 IAW AMM 33-50-12.

Part: CONNECTOR — MISSING (CABIN) · airframe 27,920 hrs · 23,888 cycles

EMERGENCY LIGHT STRIP CONNECTOR ON ACFT SIDE MISSING AT PANEL 251BF. INSTALLED CONNECTOR ON NR 4 EMER LIGHT WIRE AT PANEL 251BF, SP 9103 IAW SWPM 20-50-01 STEP 2.

Part: WIRE — BROKEN (CABIN) · airframe 27,921 hrs · 23,889 cycles

EMERGENCY LIGHT STRIP 7 & 5 BROKEN WIRES. R & R EMER LIGHT STRIP 7 & 5 IAW AMM 33-50-12.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,920 hrs · 23,888 cycles

GALLEY FWD DIGITAL HAS CORROSION & CRACKS. REPAIRED GALLEY FWD DIGITAL IAW ERS-EM-53MR-1212.

Part: SKIN — CORRODED (FUSELAGE) · airframe 27,920 hrs · 23,888 cycles

FUSELAGE SKIN HAS CORROSION & DAMAGED PAINT FRAME 60, STRINGERS 20R - 21R. REPAIRED FUSELAGE SKIN IAW ERS-EM-53MR-1201.

Part: DOOR — CORRODED (CARGO BAY) · airframe 27,920 hrs · 23,888 cycles

BAGGAGE DOOR UPPER TRIM & LOWER TRIM SCREWS HOLES CORRODED. REMOVED CORROSION FROM BAGGAGE DOOR UPPER & LOWER TRIM SCREW HOLES IAW SRM 51-10-03 & ERS-EM-52MR-313.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 27,920 hrs · 23,888 cycles

CARGO DOOR FRAME CORRODED AROUND FOURTH HOLE FROM BOTTOM FWD NUTPLATE HOLE. PERFORMED REPAIR TO CARGO DOOR FRAME CORROSION IAW ERS-52MR-325.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,920 hrs · 23,888 cycles

FRAME 25 CRACKED BETWEEN STRINGERS 15R & 16R. REPAIRED FRAME 25 CRACK BETWEEN STRINGERS 15R & 16R IAW ERS-EM-53MR-1232.

Part: LIGHT — BROKEN (CABIN) · airframe 27,920 hrs · 23,888 cycles

EMERGENCY LIGHT STRIP NR 4 BROKEN. R & R EMER LIGHT STRIP NR 4 IAW AMM 33-50-12. SEE NRTC BOW184838 FOR OPERATIONAL CHECK.

Part: FIREWALL — CRACKED (FUSELAGE) · airframe 27,920 hrs · 23,888 cycles

APU FIRE WALL CRACKED BY RT LOWER MOUNT. REPAIRED CRACK IN APU FIREWALL BY RT LOWER MOUNT IAW SRM 53-32-13 & ETN-EM-53-244.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,920 hrs · 23,888 cycles

LEFT UPPER FUSELAGE SKIN CRACKED JUST AFT OF FRAME 75 & ABOVE STRINGER 2L. CRACK IS APPROX 3/8" LONG. EASI 8071 USED, FREQ=400 KHZ, LPF=100, V-GAIN=75, H-GAIN=64, 100-500KHZ PROBE USED. REPAIRED CRACKED LT FUSELAGE SKIN AT FRAME 75 & STRINGER 2L IAW ERS-EM-53MR-1235.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 27,920 hrs · 23,888 cycles

LEFT OVERWING EMER LIGHT NOT WORKING. R & R THE BULB TO THE LT OVERWING EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 27,920 hrs · 23,888 cycles

CARGO DOOR FRAME CORRODED AROUND FIFTH HOLE FROM BOTTOM FWD NUTPLATE HOLE. PERFORMED REPAIR TO CARGO DOOR FRAME CORROSION IAW ERS-52MR-325.

Part: WIRE — BROKEN (CABIN) · airframe 27,920 hrs · 23,888 cycles

EMERGENCY LIGHT STRIP NR 7 & 5 HAS BROKEN WIRES. R & R EMER LIGHT STRIP NR 7 & 5 IAW AMM 33-50-12. SEE NRTC BOW184838 FOR OPERATIONAL CHECK.

Part: SKIN — CRACKED (FUSELAGE) · airframe 27,920 hrs · 23,888 cycles

LEFT UPPER FUSELAGE SKIN CRACKED AT THE 1ST FASTENER BELOW STRINGER 2L ON FRAME 75. CRACK IS APPROX 1/4" LONG. EASI 8071 USED, FREQ=400 KHZ, LPF=100, V-GAIN=75, H-GAIN=64, 100-500KHZ PROBE USED. THIS REPAIR WILL BE INCORPORATED IN THE REPAIR FOR NRTC E443516. SEE PREVIOUSLY STATED NRTC FOR REPAIR DETAILS.

Part: DOOR FRAME — CORRODED (CARGO DOOR) · airframe 27,920 hrs · 23,888 cycles

CARGO DOOR FRAME CORRODED AROUND LOWER FWD NUTPLATE HOLE. PERFORMED REPAIR TO CARGO DOOR FRAME CORROSION IAW ERS-52MR-325.

Part: FLASHLIGHT ASSY — DEFECTIVE (COCKPIT) · airframe 27,434 hrs · 23,473 cycles

CAPTAINS SIDE FLASHLIGHT CHARGING INTERMITTENTLY. FLASHLIGHT HOLDER HOLDING FLASHLIGHT LOOSELY & LIKELY THE CAUSE. R & R CAPTAINS FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: BUTTON — FAULTY (BLEED AIR SYS) · airframe 26,839 hrs · 22,975 cycles

ICE CONDITION, ANTI-ICE INOPERATIVE MASTER WARNING ON FINAL APPROACH. 72.4 N1 ON BOTH ENGS. R & R BLEED 1 PUSH BUTTON IAW MM 20-13-04. OPERATIONS CHECKED ANTI-ICE TEST IAW MM 30-00-00.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,468 hrs · 22,656 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FWD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 25,651 hrs · 21,959 cycles

AFTER SETTING TAKEOFF POWER INTENSE BURNING ODOR THROUGHOUT ENTIRE ACFT. NO VISIBLE SMOKE OR FUMES HIGHEST SPEED ABORT. ACCOMPLISHED ODOR DISSIPATED AT IDLE THRUST. A FLUSH OF INTERNAL SURFACE OF BOTH ENGS USING FOAM, COMP WASH, WAS PERFORMED LAST NIGHT. SUSPECT SMELL WAS FROM COMP WASH. PERFORMED GND ENG POWER RUNS IAW ETN-EM-72-034 & ODOR WAS DETECTED IN COCKPIT OR CABIN AT ALL DIFFERENT POWER SETTINGS.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,502 hrs · 21,857 cycles

FIRST OFFICER'S FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER'S FLASHLIGHT IAW AMM 33-50-00, OPERATIONS CHECKED GOOD.

Part: BRACKET — BROKEN (FLASHLIGHT) · airframe 25,161 hrs · 21,597 cycles

FLASHLIGHT BRACKET AT 18 BC BULKHEAD BROKEN. DEFERRED IAW MEL 25-53 AUTH 021155-C.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,070 hrs · 21,524 cycles

FIRST OFFICER'S EMERGENCY FLASHLIGHT INOPERATIVE. R & R FIRST OFFICER'S EMERGENCY FLASHLIGHT & BATTERY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 25,053 hrs · 21,513 cycles

FIRST OFFICER`S FLASHLIGHT HOLDER BROKEN. R & R FIRST OFFICER'S FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONAL CHECKED GOOD.

Part: ANTI-ICE VALVE — FAILED (NR 1 ENGINE) · airframe 24,816 hrs · 21,340 cycles

E1 ANTI-ICE FAIL ON CLIMB OUT DURING ICE PROTECTION TEST. R & R E1 ANTI-ICE VLV IAW AMM 30-21-01. OPERATIONS CHECKED GOOD IAW AMM 30-00-00-700-802-A. MEL ITEM RESTORED & DEFERRED IAW MEL 30-11 AUTHORIZATION 010559DM. PROCEDURE COMPLIED WITH.

Part: SHEAR TIE — CORRODED (FRAME) · airframe 24,330 hrs · 20,990 cycles

FRAME 65, SHEAR TIE CORRODED. REPAIRED IAW EO EM-53MR-1129.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 24,330 hrs · 20,990 cycles

SECOND FLOOR PROXIMITY STRIP COVER IS BROKEN ON FWD SIDE. R & R FLOOR PROXIMITY LIGHT STRIP COVER NR 2 IAW AMM 33-50-12.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 24,330 hrs · 20,990 cycles

LAST LT FLOOR PROXIMITY FLOOR STRIP HAS A BROKEN LEAD. R & R LAST LT FLOOR PROXIMITY FLOOR STRIP IAW AMM 33-50-12. BOW140807 FOR OPS CHECK.

Part: BATTERY — UNSERVICEABLE (CABIN) · airframe 23,349 hrs · 20,163 cycles

DURING MX INSPECTION, FOUND THE NR 2 EMERGENCY BATTERY NEEDS TO BE REPLACED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 2 EMERGENCY BATTERY IAW W/C 33-700-19. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: GUIDE — DIRTY (PAX DOOR) · airframe 22,797 hrs · 19,725 cycles

ON FLIGHT 2758 THE CREW REPORTED THE PASSENGER ENTRY DOOR HANDLE DID NOT ROTATE FULLY MAKING IT DIFFICULT TO OPEN DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED PASSENGER DOOR GUIDE/ROLLERS PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IAW EMB 145 AMM 52-10-01 AND FOUND TO BE WITHIN LIMITS NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (COMM SYSTEM) · airframe 22,260 hrs · 19,331 cycles

ON FLIGHT 3249 AIR TRAFFIC CONTROL DECLARED AN EMERGENCY ON BEHALF OF THE CREW DUE TO THEY WERE UNABLE TO TUNE COM 1 OR COM 2 THRU RMU OR TBCH OR UNILINK. TALKED TO ATC ON COM 3. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. CYCLED A/C POWER. COMM #1 AND COMM #2 OPC GOOD IAW AMM 23-12-00. PUT UNILINK BACK IN "DATA" MODE, IT OPC GOOD IAW AMM 23-22-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,184 hrs · 19,277 cycles

ON FLIGHT 3489 THE CREW REPORTED THE FIRST OFFICER’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT AS PER EMB 145 W/C. 33-700-20. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,867 hrs · 19,027 cycles

DURING MAINTENANCE INSPECTION FOUND CEILING EMERGENCY LIGHT OVER SEAT 2 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED EXTERIOR LEFT LOWER WING LIGHT; PART NUMBER30-2510-3 AND THE NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW WORK CARD 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,832 hrs · 18,998 cycles

DURING B INSPECTION FOUND THE LEFT FORWARD EMERGENCY OVER WING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY PACK AND CHARGER FOR NR 1 IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — DEFECTIVE (COCKPIT) · airframe 21,572 hrs · 18,794 cycles

ON FLIGHT 3909 THE CREW REPORTED WHEN BATTERY POWER WAS ESTABLISHED ON AIRCRAFT THE FIRST OFFICERS YOKE CHART HOLDER STARTED SMOKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICERS YOKE CHART HOLDER IAW EMB 145 AMM 25-12-11. THE OPERATIONAL CHECK WAS GOOD IAW EMB 145 AMM 33-11-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,938 hrs · 18,328 cycles

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

Part: SENSOR — INOPERATIVE (TE FLAP) · airframe 20,369 hrs · 17,878 cycles

ON FLIGHT 3525 THE CREW REPORTED THAT AFTER SELECTING FLAPS TO "9" ON APPROACH "FLAP FAIL" APPEARED ON EICAS- FLAPS NEVER EXTENDED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FLAP VELOCITY SENSOR IAW EMB 145 AMM 27-51-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 20,354 hrs · 17,869 cycles

ON FLIGHT 4242 THE CREW REPORTED THAT ON APPROACH THEY HAD A FLAP FAIL. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF FLAP SYSTEM IAW EMB 145 AMM 27-50-00. THE OPERATIONAL CHECK WAS GOOD NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (PITCH TRIM) · airframe 20,077 hrs · 17,676 cycles

FLIGHT 4103, THE CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A PITCH TRIM MAIN AND PITCH TRIM BACK UP FAIL MESSAGE. THE CREW COMPLETED THE CHECKLIST AND DECLARED AN EMERGENCY AND RETURNED TO LIT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HORIZONTAL CONTROL UNIT STABLIZER IAW EMB 145 AMM 27-40-01. INSPECTED HSCU AND FOUND CONNECTOR LOOSE RECONNECTED IAW AMM 27-40-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CONTROL UNIT) · airframe 20,077 hrs · 17,676 cycles

FLIGHT 4103, CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A PITCH TRIM MAIN AND PITCH TRIM BACK UP FAIL MESSAGE. THE CREW COMPLETED THE CHECKLIST AND DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HORIZONTAL CONTROL UNIT STABLIZER IAW AMM 27-40-01. INSPECTED HSCU AND FOUND CONNECTOR LOOSE, RECONNECTED IAW AMM 27-40-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (COCKPIT) · airframe 19,789 hrs · 17,468 cycles

DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER FLASHLIGHT SWITCH BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FIRST OFFICER FLASHLIGHT AS PER AMM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — CHAFED (LT ENGINE) · airframe 19,553 hrs · 17,280 cycles

DURING MAINTENANCE BASE INSPECTION REMOVED THE LEFT ENGINE HARNESS PN 23077618 SN UM05033595 DUE TO IT BEING CHAFED AND OUT OF LIMITS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ENGINE HARNESS PN 23077618 SN UM05033595. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — BROKEN (COCKPIT) · airframe 19,350 hrs · 17,124 cycles

DURING MAINTENANCE VISIT FOUND THE PILOTS EMERGENCY FLASHLIGHT CHARGER BROKEN --IT WON'T HOLD THE FLASHLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PILOTS EMERGENCY FLASHLIGHT CHARGER IAW EMB 145 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STARTER — FAILED (ENGIEN) · airframe 18,456 hrs

MX ADVISES SMOKE IS COMING OUT OF ATS OUTLET ALONG WITH SPARKS R & R E2 ATS IAW AMM 80-10-01. ATS LEAK CHECK GOOD IAW AMM 71-00-01. ENG START GOOD. NO SMOKE OR SPARKS NOTED

Part: ELECTRONIC UNIT — MALFUNCTIONED (LANDING GEAR) · airframe 17,452 hrs · 15,630 cycles

ON FLIGHT 3202 DURING DESCENT THE GEAR EXTENSION LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS CAME ON THEN WENT OUT AFTER THE GEAR INDICATED DOWN. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPALCED THE LANDING GEAR ELECTRONIC UNIT IAW MM 32-32-01. 01. THE OPERATIONAL CHECK WAS GOOD. ALSO PERFORMED OPERATIONAL TEST OF THE PROXIMITY SWITCHES IAW MM 32-63-05 NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — FAILED (CABIN) · airframe 25,685 hrs · 25,227 cycles

DURING MAINTENANCE BASE VISIT FOUND THAT THE EMERGENCY LIGHT AT SEAT 3B FAILED TO COME ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 13,352 hrs · 12,302 cycles

DURING PHASE 3A INSPECTION FOUND LEFT EXTERIOR LOWER EMERGENCY LIGHT TO BE INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REPLACED BATTERY AND CHARGER IAW CMM 33-50-04. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 9,832 hrs · 9,239 cycles

ON FLIGHT 3528, CREW REPORTED EICAS BAGG SMOKE WARNING. PRESSED BAGGAGE EXTINGUISHER BUTTON AND COMPLETED BAGG SMOKE AOM-1 PROCEDURE. AFTER 2 MORE BAGG SMOKE INDICATIONS MESSAGE EXTINGUISHED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BAGGAGE SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE.

Part: ENGINE — SHUTDOWN

NR 1 ENGINE UNCOMMANDED SHUT DOWN IN FLIGHT. CREW LANDED AT JFK WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE. AIRCRAFT RETURNED TO SERVICE

Part: ENGINE — MALFUNCTIONED (NR 1)

FLT 4014 - CREW NOTED, SEEING THE OIL PRESSURE STARTING TO DROP AND THEN THE E1 SHUTDOWN. DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED NR 1 ENGINE IAW WC 72-000-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)