N848AE

Part: ACM — FAILED (NR 1) · airframe 32,568 hrs · 30,135 cycles

PACK 1 OVERLOAD WITH BURNING SMELL. SMELL WENT AWAY AFTER TURNING PACK 1 OFFPERFORM FIM 21-20-00 FOR BURNING SMELL IN COCKPITREF: LOGPAGE 4528695 ITEM 1-C/A-PERFORMED FIM TASK 21-20-00. FOUND PACK 1 TO BE THE CAUSE OF ODOR EVENT IN COCKPIT. PACK 1 MEL ISSUED / AIRCRAFT OK FOR SERVICE. INSTALLED ACM IAW EO #EM-2100-048 UP TO & INCLUDING STEP 35. COMPLETED INSTALLATION OF ACM IAW ENVOY E0 # EM-2100-048 FROM STEP 36 TO COMPLETION. OPC OF PACK 1 GOOD. NO DEFECTS NOTED. MEL RESTORED.

Part: DOOR — DENTED (CABIN) · airframe 31,089 hrs · 28,786 cycles

PAX SERVICES REPORT DENT ON MAIN CABIN DOOR AFT OF EXTERNAL HANDLE NEAR TRAILING EDGE. C/A-INSPECTED IAW SRM 52-10-01 AND FOUND DENT TO BE IN AREA B AND OUT OF LIMITS. C/W PART A OF ERS-EM-52DF-987 DAMAGE ACCEPTABLE AS IS.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 30,251 hrs · 27,934 cycles

BOTH LH AND RH AFT OVERWING EXIT LIGHTS ARE INOP.-C/A-REMOVED AND REPLACED #4 EMERGENCY LIGHT POWER SUPPLY CHARGER ASSY AND BATTERY HOLDER ASSY IAW AMM 33-50-04. OPS CHECK GOOD. BATTERY CHARGER ASSY P/N 11-0049 S/N 15612

Part: DAU — MALFUNCTIONED (NR 2) · airframe 30,138 hrs · 27,831 cycles

ABORTED TAKEOFF 90 KNOTS DUE TO MASTER WARNING," TAKE OFF TRIM". ALL TRIMS WERE INDICATING GREEN-C/A-REMOVED AND REPLACED DAU#2 IAW EMB 140 AMM 31-41-01. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 29,890 hrs · 27,608 cycles

FWD F/A FLASHLIGHT HOLDER BOTTOM PART OF BRACKET IS BROKEN. R&R F/A FLASHLIGHT ASSY IAW AMM 33-50-16.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,383 hrs · 27,151 cycles

PAX DOOR EXTERNAL EMERGENCY LIGHT FAILS TO ILLUNINATE. R&R PAX DOOR EXTERNAL EMERGENCY LIGHT ASSY IAW AMM'S 33-50-10 AND 33-30-02. OPC GOOD IAW AMM 30-50-00-700-801.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 29,277 hrs · 27,041 cycles

BURNING SMELL IN COCKPIT ON POWER UP. FOUND CIRCUIT BREAKER O/C RELAY 1, O/C RELAY 2 POPPED. PERFORMED FIM TASKS 20-21-00-810-801 UP TO STEP 5 BLOCKS 1, 26-29, 33. FIM 34-22-00-810-835 COMPLETED. NO DEFECTS NOTED. RESET CB'S. OPC GOOD. ALL WORK DONE IAW AMM 20-40-01, 23-51-00, 33-51-00, 34-22-00. AIRCRAFT OK FOR SERVICE. PULLED OUT OR DROPPED DOWN FOLLOWING PANELS TO SMELL/INSPECT WIRES: DASH, OVERHEAD, GLARESHIELD, CENTER PEDESTAL, LT/RT KICK. INSPECTED PRINTER, EGPWS COMPUTER, CAPT/FO/OBSERVER READING LIGHTS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,232 hrs · 26,984 cycles

PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-06. OPS CHECKED GOOD.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 29,126 hrs · 26,861 cycles

DURING TAXI, UNDER BRAKING ONE OR MORE BRAKE WOULD RELEASE, RE-ENGAGE THEN RELEASE, EVEN UNDER LIGHT BRAKING AT ALL SPEEDS WHILE TAXIING. RAN BRAKE ANALYZER IAW AMM 32-41-00, TESTED GOOD, ACFT RETURN TO SERVICE

Part: SEAL — LEAKING (PAX DOOR) · airframe 29,100 hrs · 26,833 cycles

LOUD SQUEAL FROM THE MAIN CABIN DOOR, GOT LOUDER THROUGH FL 230. COMPLIED WITH A MAIN DOOR RUBBER TRIM SEAL FILLER STRIP REPAIR IAW AMM 52-00-01. DOOR OPS CHECKED GOOD IAW AMM 21-31-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,099 hrs · 26,832 cycles

SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW MM 33-50-00. OPS CHECKED GOOD.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 29,072 hrs · 26,803 cycles

FWD SHEAR TIE AT FRAME 65 WAS FOUND CORRODED. THE SHEAR WAS REPAIRED IAW SRM 53-31-04.

Part: SKIN — CRACKED (FRAME 75) · airframe 29,072 hrs · 26,803 cycles

LEFT REAR FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. THE SKIN WAS REPAIRED IAW SRM 53-31-01.

Part: SKIN — PUNCTURED (RUDDER) · airframe 29,072 hrs · 26,803 cycles

RUDDER, RT SKIN PUNCTURED BETWEEN RIBS ZV2938.0, AND 3229. THE RUDDER SKIN WAS REPAIRED IAW SRM 55-40-01.

Part: SKIN — DAMAGED (FRAME 23) · airframe 29,072 hrs · 26,803 cycles

DAMAGE ON THE RT SKIN, 2 INCHES FWD OF FRAME 23 AND 1.5 INCHES BELOW STRINGER 19R. REPAIRED IAW 53-21-01.

Part: WIRE — DAMAGED (EXIT SIGN) · airframe 29,072 hrs · 26,803 cycles

DURING LT SIDE WALL INSTALLATION FOUND LT O/WING EXIT SIGN WIRES DAMAGED. LT O/WING EXIT SIGN WIRES REPAIRED IAW SPWN 20-21-00.

Part: BEAM — CORRODED (FUSELAGE) · airframe 29,072 hrs · 26,803 cycles

BAGGAGE DOOR LOWER BEAM CORRODED. -C/A-LOWER BEAM REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,072 hrs · 26,803 cycles

LT REAR FUSELAGE SKIN CRACKED AT FRAME 75 AT STR 2L-C/A-LT REAR FUSELAGE SKIN AT FRAME 75 STR 2L REPAIRED IAW SRM 53-31-01 FIG 219 SHEET 2

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 29,072 hrs · 26,803 cycles

BAGGAGE DOOR FWD L-SHAPE CORRODED AT FR 65-C/A-IN RF1 AT FR65, FWD L-SHAPE BLENDED, OUT OF LIMITS IAW ETN EM-53-272 AND OLD SEGMENT REMOVED IAW SRM 53-31-04. IN RF1 ATFR65, FWD L-SHAPE REPAIRED IAW SRM 53-31-04

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 29,072 hrs · 26,803 cycles

RT SILL NUMBER 4 CORRODED AT SEVERAL PLACES. RT SILL NUMBER 4 FOUND BEYOND LIMITS CORRODED AT SEVERAL PLACES IAW SRM 53-23-10 RT SILL NUMBER 4 REPLACED WITH NEW PART IAW SRM 51-40-02.

Part: DOOR — DAMAGED (CABIN) · airframe 29,072 hrs · 26,803 cycles

DAMAGE ON MAIN DOOR LOWER EDGE. 7.000" FROM AFT EDGE. -C/A-ON MAIN DOOR LOWER EDGE, 7" FROM AFT ADGE DAMAGE BLENDED AND REPROTECTED IAW SRM 51-10-05 ITEM 4 TYPE 6.

Part: TRIM PANEL — DAMAGED (CABIN) · airframe 29,072 hrs · 26,803 cycles

CABIN FLOOR PROXIMITY EMERGENCY LIGHT TRIM DAMAGED. -C/A-FLOOR PROXIMITY STRIP LIGHT REPLACED IAW AMM 33-50-12 INSTALLATION COVERED BY TASK PAI715-2.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,072 hrs · 26,803 cycles

OMEGA BEAM LOWER FLANGE, BOTH SIDE OF WALKWAY, FOUND CORRODED BTW FR-43 TO FRM 52. -C/A-OMEGA BEAM LOWER FLANGE, BOTH SIDE OF WALKWAY CORROSION BTW FR 43 TO FR 52 BLENEDED AND REPROTECTED IAW SRM 53-23-10 REMAINING THICKNESS .044 OR .050 & .066 OF .071 SEE NDT RE[PRT MP FAI;T FPIMD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 29,072 hrs · 26,803 cycles

LT SILL NUMBER 6 CORRODED AT SEVERALS PLACES. -C/A-LT SILL NR 6 CORRODED OUT OF LIMIT IAW SRM 53-23-10 LT SILL NR 6 REPLACED WITH NEW PART AND INSTALLED IAW SRM 51-40-02.

Part: ANTI-ICE VALVE — CORRODED (LT WING) · airframe 29,072 hrs · 26,803 cycles

ENGINE BLEED AIR AND ANTI-ICING SYSTEMS, LT WING ANTI-ICING VALVE FOUND WITH CORROSION BEYOND ACCEPTABLE LIMITS (FILTER CAP THREADS INTO VALVE THREADS PORTIONS MISSING AND DAMAGED. LT WING ANTI ICING VALVE REPLACED IAW AMM 30-11-01.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 29,072 hrs · 26,803 cycles

RT SILL NUMBER 3 CORRODED AT SEVERAL PLACES. RT SILL NR 3 CORRODED OUT OF LIMIT IAW SRM 53-23-10. RT SILL REPLACED WITH NEW PART AND INSTALLED IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 29,072 hrs · 26,803 cycles

LT OMEGA BEAM OUTBD LOWER FLANGE CRACK 6 INCH AFTER FRM-41. -C/A-LT OMEGA BEAM LOWER ANGLES REPAIRED AS PER SRM 53-23-02.

Part: WIRE — DAMAGED (CABIN) · airframe 28,845 hrs · 26,597 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. SEE IPC 33-50-10-40 FOR LOCATION. REPAIRED WIRE W716-0008-20 IAW WM 20-21-00. OPERATIONS CHECKED GOOD.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 28,794 hrs · 26,540 cycles

CAPTAINS FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT HOLDER IAW AMM 33-50-16. OPERATIONS CHECKED GOOD. NO FURTHER DEFECT NOTED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,775 hrs · 26,523 cycles

FLIGHT ATTENDANT EMER FLASHLIGHT RED LED INDICATOR INOPERATIVE. R & R FLIGHT ATTENDANT EMER FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: DUCT — CRACKED (BLEED AIR SYS) · airframe 28,598 hrs · 26,378 cycles

NUMBER 2 ENG 14TH STAGE DUCT FROM CUSTOMER SERVICE PANEL CRACKED AT ANTI-ICE VLV END. R & R 14TH STAGE DUCT AT NR 2 ENG CUSTOMER SERVICE PANEL TO ANTI-ICE VLV IAW AMM 36-11-09. LEAK CHECKED GOOD.

Part: ENGINE — FAILED (NR 2) · airframe 28,494 hrs · 26,287 cycles

LAVATORY SMOKE AFTER TAKEOFF, AOM 1 PROCEDURE COMPLIED WITH. FLIGHT ATTENDANT REPORTS SMOKE & FUMES IN CABIN. R & R NR 2 ENGINE IAW WC 71-000-00. OPERATIONS CHECKED GOOD. LEAK CHECKED GOOD. PERFORMED ETN-EM-72-034 FOR NEW ENG. NO SMOKE OR ODOR PRESENT.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 28,486 hrs · 26,278 cycles

THE CAPTAIN'S SIDE COCKPIT FLASHLIGHT HAS NO CHARGE. R & R CAPTAIN`S FLASHLIGHT IAW AMM 33-50-16. FOUND GOOD AT THIS TIME.

Part: DRAIN LINE — CRACKED (PITOT/STATIC SYS) · airframe 28,445 hrs · 26,242 cycles

LOW SPEED ABORT APPROX 60 KTS. MX NOT REQUIRED, CONDITIONS NOT MET FOR HIGH ENERGY STOP INSPECTION 05-50-16-200-801-A. REFERENCE NRWC 848-CMI-01730 ERRONEOUS AIRSPEED INDICATION TROUBLESHOOTING, RT PITOT DRAIN HOSE CLEAR, CRACKED. R & R PITOT STATIC SYS 2 DRAIN TUBE IAW 34-13-05-000-801-A & 34-13-05-400-801-A. OPERATIONS & LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,445 hrs · 26,242 cycles

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

Part: PITOT SYSTEM — CONTAMINATED · airframe 28,265 hrs · 26,117 cycles

FLASHING IAS AMBER LIGHT ON PFD A/S ON STBY & FIRST OFFICER SIDE SAME ADC 2 SELCETED. PROBLEM CORRECTED, A/S WAS INCREASING ON CA SIDE. DRAINED WATER FROM PITOT SYS. PERFORMED OPERATIONS CHECK LEAK CHECKED IAW AMM 34-13-00. OPERATIONS CHECKED GOOD. ACFT IS COMPLIANT FOR CONTINUED CAT II OPERATION.

Part: LIGHT — NOT SEATED (CABIN) · airframe 27,447 hrs · 25,477 cycles

SERVICE DOOR EMER LIGHT INOPERATIVE. FOUND SERVICE DOOR EMER LIGHT BULB UNSEATED. RESEATED BULB IAW AMM 33-50-10 STEPS 3 J 1 - 3. OPERATIONS CHECKED GOOD.

Part: COMPUTER — FAILED (AHRS) · airframe 26,506 hrs · 24,687 cycles

SHORTLY AFTER TAKEOFF AHRS 1 FAIL. ASSOCIATED ATT & HDG FAIL. R & R AHRS IAW AMM 34--21 01, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE · airframe 26,388 hrs · 24,585 cycles

FLASHLIGHT DOESN'T HOLD CHARGE. R & R WHOLE ASSEMBLY IAW AMM 33-50-16, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 25,787 hrs · 24,063 cycles

FLIGHT 2848 AFTER SHUTDOWN, WITH BOTH ENGINES OFF APU ON, GPU OFF, SPS1 INOP, SPS ADVANCED ALERTS ON EICAS & AOA COMPARATOR LIGHT ON PFD1 APPEARED. MASTER WARNING & CATION LIGHTS ALSO ALERTED & COULD NOT CLEAR OR SILENCE. WITH GPU ON, APU OFF WE WERE ABLE TO CLEAR & SILENCE THOSE WARNING CATION LIGHTS, EICAS & PFD1. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED OPERATION TEST OF THE STALL PROTECTION SYS IAW 140 AMM 27-36-00. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED.

Part: FITTING — GOUGED (RT AILERON) · airframe 24,093 hrs · 22,566 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON BRACKET WHERE DAMPER ATTACHES GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMPER FITTING IAW EO EM-27MR-112. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,093 hrs · 22,566 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 25 AND 28. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR IAW EMBRAER STRUCTUAL REPAIR MANUAL 53-22-10 AND 53-00-10 FIGURE 202 SHEET 2. THE CORROSION LEVEL IS NOT SPECIFIFED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISSING (CABIN) · airframe 24,158 hrs · 22,616 cycles

DURING MAINTENANCE INSPECTION FOUND THE CABIN AFT FLOOR EMERGENCY LIGHT STRIP HAS A WIRE [FUSELAGE SIDE] WITH A MISSING CONNECTOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED MISSING CABIN AFT FLOOR EMERGENCY LIGHT STRIP CONNECTOR (FUSELAGE SIDE) IAW ERJ 140 SWPM CHAPTER 20-21-00. C/W OPS CHECK OF CABIN FLOOR EMERGENCY LIGHT STRIPS IAW EMB AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 24,158 hrs · 22,616 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 6 EMERGENCY LIGHT STRIP HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 24,158 hrs · 22,616 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD EMERGENCY FLOOR LIGHT STRIP DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOR LIGHT STRIP IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FASTENER — DAMAGED (CABIN) · airframe 24,158 hrs · 22,616 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER CABIN FLOOR PROXIMITY (EMERGENCY LIGHT) STRIPS (SCREWS AND WASHERS) HARDWARE HEADS STRIPPED, CORRODED OR MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR PROXIMITY STRIPS IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,158 hrs · 22,616 cycles

DURING B INSPECTION FOUND THE RIGHT GUSSETT CORRODED AT FRAME 20. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT GUSSETT AT FRAME 20 IAW SRM 51-40-02. LEVEL OF CORROSION UNKNOWN. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INTERMITTENT (CABIN) · airframe 24,158 hrs · 22,616 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLASHLIGHT IN ROW 16 ON THE AFT BULKHEAD WORKING INTERMITTENLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT IN ROW 16 ON THE AFT BULKHEAD IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,025 hrs · 22,502 cycles

DURING B INSPECTION FOUND THE MAIN DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IN CEILING EMERGENCY LIGHT AT MAIN DOOR IAW EMB 140 AMM 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: BATTERY — UNSERVICEABLE (CABIN) · airframe 23,906 hrs · 22,390 cycles

DURING UNSCHEDULED MAINTENANCE FOUND THE NR 3 EMERGENCY LIGHTING BATTERY NEEDS TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY IAW EMB W/C 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 23,834 hrs · 22,325 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT CABIN FLASHLIGHT INOPERABLE. THE ITEM WAS PLACED ON MEL 25-23. REMOVED AND REPLACED FLASHLIGHT BATTERY. THE OPERATIONAL CHECK WAS GOOD IAW CMM 25-60-11 MEL 25-23 RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 23,811 hrs · 22,302 cycles

ON FLIGHT 4100 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT APPEARED TO BARELY HOLD A CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT ASSEMBLY IAW AMM 33-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (COCKPIT) · airframe 23,707 hrs · 22,203 cycles

DURING B INSPECTION FOUND THE FLASHLIGHT BEHIND CAPT'S SEAT MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED MISSING FLASHLIGHT BEHIND CAPT'S SEAT IN REFERENCE WITH EMB AMM 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 23,674 hrs · 22,177 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 BULB IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BALLAST — UNSERVICEABLE (CABIN) · airframe 23,457 hrs · 22,009 cycles

ON FLIGHT 3435 THE FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE GALLEY, THE GALLEY LIGHT WAS HOT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY LIGHT BALLASTS AND LIGHT BULBS IAW AMM 33-29-05. THE OPERATIONAL CHECK WAS GOOD. NO SMELL NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 23,176 hrs · 21,800 cycles

DURING MAINTENANCE INSPECTION FOUND BROKEN WIRE (AIRCRAFT SIDE) ON LAST EMERGENCY FLOOR LIGHTING STRIP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BROKEN TERMINAL END IAW WMM 20-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GASKET — DEFECTIVE (NR 1 ENGINE) · airframe 23,089 hrs · 21,729 cycles

ON FLIGHT 3241 THE CREW REPORTED, AFTER ONE HOUR INTO THE FLIGHT NOTICED THE NR 1 OIL QUANTITY HAD DECREASED TO 5 QUARTS. THE CREW REFERRED TO THE AOM PROCEDURES FOR OIL QTY LOW. ALL OTHER INDICATIONS REMAINED NORMAL. THE CREW CHOSE TO CONTINUE TO DFW AND MONITOR THE SITUATION. THE CREW NOTIFIED ATC AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED NR 1 ENGINE AFT SUMP COVER SEAL AS PER RR MM 72-59-10. THE LEAK CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — CONTAMINATED (LEFT) · airframe 21,781 hrs · 20,351 cycles

ON FLIGHT 3043 THE CREW ABORTED THE TAKEOFF ROLL AT ABOUT 70 KTS DUE TO SMOKEY BURNING ODOR IN THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED RR FIM 72-00-00-810-814 THRU STEP 10 ON LT ENGINE. PERFORMED BOROSCOPE OF LT ENGINE ZERO CARBON SEAL TO FIRST STAGE COMPRESSOR. FOUND ENGINE IGV AREA CONTAMINATED WITH TRI-FLOW FROM PREVIOUS MAINTENANCE. PERFORMED TWO 5 MINUTE T/O POWER RUNS WITHOUT BLEEDS ON WITH 5 MINUTES AT IDLE BETWEEN POWER RUNS IAW RR MM 72-00-00. THEN PERFORMED 3 TAKEOFF POWER RUNS WITH BLEEDS AND PACKS ON WITH 5 MINUTES IDLE BETWEEN RUNS IAW RR MM 72-00-00 AND EMB 140 AMM 21-20-00. NOTED SLIGHT ODOR ON FIRST RUN. NO ODOR NOTED ON LAST RUN. THE OPERATIONAL CHECK WAS GOOD.

Part: DOOR — UNSECURE (COCKPIT) · airframe 21,368 hrs · 19,885 cycles

ON FLIGHT 4374 CREW FOUND FIRST OFFICER ESCAPE ROPE COMPARTMENT DOOR KEEPS FALLING OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED F/O'S ESCAPE ROPE DOOR AS REQUIRED.

Part: DOOR — LACK OF LUBE (FIRE BOTTLE) · airframe 21,296 hrs · 19,808 cycles

FLIGHT 2754, CREW REPORTED THE LAVATORY FIRE BOTTLE INSPECTION DOOR IS EXTREMELY DIFFICULT TO OPEN AND NEEDS LUBE OR ADJUSTMENT. AIRCRAFT REMOVED FROM SERVICE. CLEANED AND LUBED LATCH, OPS CHECKED GOOD IAW AMM 25-40-00. AIRCRAFT RETURNED TO SERVICE.

Part: TIRE — BLOWN (LT MLG) · airframe 21,106 hrs · 19,644 cycles

ON FLIGHT 3015 AFTER TAKEOFF THE TOWER NOTIFIED THE CREW OF A POSSIBLE BLOWN TIRE. THE CREW PERFORMED A FLY BY FOR THE LAX TOWER FOR INSPECTION. THE CREW DECLARED AN EMERGENCY AND LANDED AT LAX. THE LEFT INBOARD TIRE WAS BLOWN AND SHREDDED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT INBOARD WHEEL ASSY IAW WC 32-700-11. THE TIRE WAS FULLY INFLATED. THE TIRE TREAD SEPARATED FROM THE TIRE CASING. THE LEFT MAIN LANDING GEAR FORWARD PROXIMITY SWITCH HARNESS IS BROKEN AT BEND AT PROX SWITCH. REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR PROX HARNESS IAW ERJ-140 AMM 32-60-00. THE LEFT MAIN LANDING GEAR LOWER DOOR HAS BROKEN ANGLE BRACKET. REMOVED AND REPLACED LEFT MAIN LANDING GEAR LOWER DOOR IAW ERJ-140 AMM 32-10-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,090 hrs · 17,627 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FRAME 23 CRACKED AT RIGHT FLOOR SILL NEAR SERVICE DOOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 WITH DOUBLER IAW ETD2011-145/00044 AND SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — FAILED (NR 4) · airframe 15,743 hrs · 13,296 cycles

DURING A PREFLIGHT INSPECTION THE CREW NOTICED THE NUMBER 4 EMERGENCY LIGHT BATTERY FAILED TO HOLD A CHARGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 BATTERY AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CRADLE — BROKEN (FLASHLIGHT)

AFT EMERGENCY FLASHLIGHT CRADLE BROKEN. (K)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 12,470 hrs · 11,013 cycles

ON 3197, FLIGHT CREW REPORTED MAIN ENTRANCE EMERGENCY EXIT SIGN ABOVE FASTEN SEAT FAILS TO ILLUMINATE AND EXIT SIGN ABOVE FLIGHT ATTENDANT STATIONS FAILS TO ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY IAW EMB 140 AMM 33-50-04. OPERATIONAL CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: LINER — DAMAGED (COMBUST CHAMBER) · airframe 11,454 hrs · 9,909 cycles

CREW NOTED IN CLIMB-OUT AT 14000 NR 1 ENGINE ITT FLUCTUATED FROM 788-747 +/- 4*. PERFORMED BOROSCOPE OF LT ENGINE COMBUSTER LINER FOUND LINER TO HAVE OUT OF LIMITS DAMAGE. ENGINE REQUIRED REPLACEMENT. REMOVED AND REPLACED LT ENGINE IAW WC 71-000-00. FCF PASSED. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — FAILED (MLG) · airframe 10,943 hrs · 9,423 cycles

ON TAKEOFF WHEN GEAR HANDLE WAS MOVED UP DID NOT GET RIGHT MAIN GEAR IN TRANSIENT INDICATION. REMOVED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB AMM. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,680 hrs · 8,413 cycles

FOUND SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,680 hrs · 8,413 cycles

FOUND FLOOR SUPPORT ON RIGHT SIDE CORRODED BETWEEN FRAME 22 AND FRAME 23. REMOVED AND REPLACED PANEL SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 9,680 hrs · 8,413 cycles

FOUND ANGLE FROM FLOOR SUPPORT TO SERVICE DOOR SILL CORRODED. REMOVED AND REPLACED IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 9,369 hrs · 8,184 cycles

FOUND ALL EMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED NUMBER 1 AND 4 BATTERY PACKS IAW EMB AMM. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — ACTIVATED (CARGO BAY)

DFW - FLT 3853 - CARGO SMOKE DETECTOR MESSAGE IN FLIGHT, BLEW BOTH BOTTLES. REMOVED AND REPLACED FIRE DETECTOR SENSORS AND FIRE BOTTLES, P/N 337000271, S/N 3083601/3239381 AND P/N 3A6000731 S/N 846000731/16185E1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POTENTIOMETER — INOPERATIVE (COCKPIT LIGHTS)

DCA - FLT 4753 - ELECTRICAL SMELL IN COCKPIT WITH POPPED OVERHEAD LIGHT CIRCUIT BREAKER ISSUED MEL 33-1. REPLACED NR 1 COCKPIT OVERHEAD LIGHT DIMMER SWITCH, MEL CLOSED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)