N851AE

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 32,052 hrs · 28,909 cycles

FOUND FWD EMERGENCY BATT #2 LIGHTS INOP-C/A-REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY AND CRADLE ASSY IAW WC 33-700-19 AND W/C 33-700-17 OPS CHECK GOOD. EMERGENCY LIGHTING BATTERY P/N 2013-1A S/N 104519

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,871 hrs · 28,737 cycles

FLOOR EMERGENCY STRIP LIGHTING INOP. ROWS 1-4-C/A-REMOVED AND REPLACED #2 BATTERY PACK IAW AMM 33-50-04. OPS CHK GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,715 hrs · 28,569 cycles

SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED SERVICE DOOR EVTERNAL EMERGENCY LIGHT IAW AMM TASK 33-50-10-000-801-A AND 33-50-10-400-801-A OPC GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,557 hrs · 28,432 cycles

EMERGENCY LIGHTS OVER R/H WING AND AT R/H EMERGENCY EXIT LIGHT AFT GALLEY ARE INOP-C/A-RAR # 2 BATTERY POWER SUPPLY IAW AMM 33-50-04. OPC GOOD FOR EMERGENCY LIGHT OVER R/H WING AND R/H EMERGENCY EXIT LIGHT AFT GALLEY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,430 hrs · 28,312 cycles

DURING THE PS-2 CHECK FOUND EMERGENCY LIGHTS RELATED TO EMERGENCY BATTERY #2 INOP. C/A-REMOVED AND REPLACED EMERGENCY BATTERY #2 IAW AMM 33-50-04. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,430 hrs · 28,312 cycles

RT FORWARD LOWER FAIRING EMERGENCY LIGHT INOP. C/A-REMOVED AND REPLACED RT FORWARD LOWER FAIRING EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.

Part: RELAY — FAILED · airframe 31,190 hrs · 28,112 cycles

ODOR OF SOMETHING BURNING AFTER LANDING ON TAXI AND FA REPORTED SEEING HAZE IN CABIN-C/A-PERFORMED ENG ODOR EVENT TROUBLESHOOTING IAW ETN-EM-72-034. REF FIM TASK 21-20-00. NO ODOR NOTED. PERFORMED GVI OF RH AND LH RELAY SUPPORT PANELS IAW AMM 6-41-03. NO ODOR NOTED. DISCREPENCY REMAINS OPEN.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 30,930 hrs · 27,891 cycles

AFTER DECENDING FROM FL 370 TO SEA LEVEL IN A VERY HUMID ENVIRONMENT BAGG SMOKE LIGHT FLASHED ON AND SELF EXTINGUISHED-VERIFIED NO SMOKE OR FIRE VISUALLY AFTER LIGHT EXTINGUISHED. C/A-PERFORMED CARGO SMOKE DECTECTOR INSPECTION CHECK IAW 26-15-01. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: PROXIMITY SWITCH — OUT OF ADJUST (NLG) · airframe 30,538 hrs · 27,500 cycles

LG AIR/GND FAIL MESSAGE "TRANSFERRED TO NRWC 851-DFW-02449"-C/A-PERFORMED NOSE LANDING GEAR AIR/GROUND PROXIMITY SWITCH CLEARANCE ADJUSTMENT IAW EMB 140 AMM 32-63-05. PROXIMITY SWITCH OPC CHECK GOOD IAW EMB 140 AMM 32-63-00. REMOVED AND REPLACED NLG WOW PROX SW PER EMB AMM 32-63-02 OPC GOOD. REMOVED AND REPLACED RT MLG FWD WOW PROX SW PER EMB AMM 32-63-01, OPC GOOD. PROXIMITY SENSOR P/N 80-057-01 S/N 24484

Part: SIGN — INOPERATIVE (CABIN) · airframe 30,196 hrs · 27,111 cycles

COCKPIT DOOR STEP EXIT MARKER EMERGENCY LIGHT INOP "TRANSFERRED TO NRWC 851-DFW-02325"-C/A-REF NRWC 851-DFW-02335 RAR FORWARD EXIT IDENTIFIER SIGN IAW EMB 140 AMM 33-50-13, OP CK GOOD.

Part: FAN — INOPERATIVE (LT RECIRCULATION) · airframe 29,514 hrs · 26,435 cycles

STRONG ELECTRICAL BURNING ODOR ON THE FLIGHT DECK & FRONT CABIN, DURING FLIGHT. IAW FIM 21-20-00-810-801-A, AC DIST - SMK/ABNORMAL ODOR IN CABIN AND COCKPIT INSPECTED THE LT + RT POWER DIST PANELS, NO DEFECTS. LT & RT RELAY SUPPORTS, NO DEFECTS. UNDER COCKPIT FLOOR, BEHIND INSTRUMENT PANEL, NO DEFECTS NOTED. EXAMINED ALL FLASHLIGHTS, NO DEFECTS OR UNUSUAL ODORS. VERIFIED ALL CABIN PSUS & SIGNS AND LIGHTING NORMAL. IN THE GALLEY, FOUND AN ELECTRICAL CONNECTOR ON THE COFFEE POT TO HAVE A MODERATE ELECTRICAL BURNED ODOR, INSPECTED UNDER CABIN FLOOR, AT RECIRCULATION FANS, NO ABNORMAL ODORS BUT FOUND THE NR 2 RECIRCULATION FAN INOPERATIVE. CIRCUIT BREAKER J-21 PULLED AND SECURED. OPERATED BOTH BACKS FOR ONE HOUR, NO ABNORMAL ODORS. FCF FOUND SATISFACTORY. SWAPPED OUT THE COFFEE MAKER. REMOVED AND REPLACED THE NR 2 CABIN RECIRCULATION FAN IAW AMM 21-24-01. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,992 hrs · 25,935 cycles

NR 6 FLOOR EMERGENCY LIGHT WAS INOPERATIVE. R & R THE EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,990 hrs · 25,933 cycles

NR 6 FLOOR EMERGENCY LIGHT INOPERATIVE.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 28,974 hrs · 25,914 cycles

AFT SHEAR TIE FRAME 68 CORRODED. THE SHEAR WAS REPAIRED IAW SRM 53-31-04.

Part: SHEAR TIE — CORRODED (FRAME 65) · airframe 28,974 hrs · 25,914 cycles

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

Part: STRUCTURE — CORRODED (FRAME 65) · airframe 28,974 hrs · 25,914 cycles

IN RFI AT FR 65 BTW STR 15L-18L, FWD L-SHAPE FOUND CORRODED-C/A-IN RFI @ FR 65 BTW STR 15L AND 18L DAMAGED SEGMENT OF FWD L SHAPE BLENDED OUT OF LIMITS IAW ETN EM 53-272 AND DISCARDED IAW SRM 53-31-04 RE IN RFI @ FR 65 BTW STR 15L-18L FWD L-SHAPE REPAIRED IAW ETN EM-53-272 AND SRM 52-31-043

Part: STRUCTURE — CORRODED (FRAMES 68-69) · airframe 28,974 hrs · 25,914 cycles

IN RFI FR 68 BTW STR 15L-18L AFT L SHAPE FOUND CORRODED IN LH RFI BWN FR 68-69 BLEED AIR POST DUCT NEEDS TO PARTIALL REMOVED FOR SHEET METAL ACCESS IN L/H RFI BTW FR 68-69 BLEED AIR POST DUCT NEEDS TO BE REINSTALLED-C/A-IN RFI @ FR 68 BTW STR 15L AND 186 DAMAGED SEGMENT OF AFT L SHAPE LENDED OUT OF LIMIT SIAW ETN EM 53-272 AND DISCARDED IAW SRM 53-31-04IN RFI @ FR 68 BTW STR 15L-186 AFT L-SHAPE REAPIRED IAW ETN EM-53-272 AND SRM 53-31-04IN L/H RFI BTW FR 68-69 BLEED AIR AFT POST DUCT REMOVED FOR ACCESS IAW AMM 36-11-09 IN L/H RFI BTW FR 68-69 BLEED AIR AFT POST DUCT RE-INSTALLED IAW AMM 36-11-09

Part: BEAM — CORRODED (FRAMES 65-68) · airframe 28,974 hrs · 25,914 cycles

IN L/H RFI FR 65-68 BAGGAGE DOOR LOWER BEAM FOUND CORRODED AFTER FURTHER INVESTIGATION ANGLE PN 145-25681-001 AND 145-2568/1-007 BOTH FOUND CRACKED AND REMOVED FOR REPLACEMENT AFTER FURTHER INVESTIGATION FWD D TEE FITTING P/N 145-25893-001 FOUND CORRODED OUT OF LIMITS AND REMOVED FOR REPLACEMENTIN RFI BTW FR 65-68 TEE FITTING PN 145-25892-001 PLATES P/N 145-2542-007 AND 145-25421005 AND PROFILE T P/N 145-25523-001 AND 145-25523-003 ALL REMOVED FOR ACCESS-C/A-IN RFI BTW FR 65-68 BAGGAGE DOOR LOWER BEAM FOUND CORRODED OUT OFLIMITS AND REMOVED FOR REPLACEMENT IAW SRM 51-40-02 AND ETN-EM-53-23 IN RFI BTW FR 65-68 NEW BALLGED DOOR LOWER BEAM INSTALLED IAW SRM 51-40-02 ANGLES P.N 145-25681-011 AND 145-25681-607 BOTH INSTALLED IAW SRM 51-40-02FWD TEE FITTING PN 144-25893-001 INSTALLED IAW SRM 51-40-02 IN RFI BTW FR 65-68 TEE FITTING PN 145-25892-001 PLATES P/N 145-25421-007 AND 145-25421-005 AND PROFILE T P./N 145-25523-001 AND 145-25523-003 ALL REINSALLED IAW SRM 51-40-02

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 28,729 hrs · 25,671 cycles

COCKPIT FLASHLIGHT HOLDER BROKEN FLASHLIGHT WILL NOT STAY IN ENOUGH TO CHARGE. R & R CAPTAINS FLASHLIGHT CRADLE IAW CMM 25-60-02.

Part: PRESSURE SWITCH — FAULTY (RUDDER SYS) · airframe 28,579 hrs · 25,553 cycles

INFLIGHT AT 250 KIAS EICAS MSG AUTOPILOT FAIL, YAW DAMP FAIL & RUDDER SYS 1 - 2 INOPERATIVE. RAN CHECKLIST DID NOT RESOLVE. R & R SYS NR 2 PRESS SWITCH USING AMM 27-23-04. OPERATIONS CHECKED GOOD AT THIS TIME. NO FURTHER DEFECTS NOTED.

Part: SEAT — MALFUNCTIONED (COCKPIT) · airframe 28,508 hrs · 25,491 cycles

CAPTAIN SEAT UNCOMMANDED RECLINED REPEAT WRITE UP. R & R CAPTAINS SEAT IAW AMM 25-11-01. OPERATIONS CHECKED OK.

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,266 hrs · 25,286 cycles

EMERGENCY PATH FLOOR LIGHTING STRIP AT SEAT 10A HAS BROKEN CONNECTOR WIRE NEEDS STRIP. INSTALLED NEW FLOOR LIGHTING STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (CABIN) · airframe 28,266 hrs · 25,286 cycles

FLOOR PROX LIGHT STRIP NR 8 INOPERATIVE, WIRE BROKEN AT SPLICE. REPAIRED BROKEN WIRE IAW SWPM.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 27,888 hrs · 24,981 cycles

FOUND BRAKE ON INDICATOR LIGHT INOPERATIVE IAW PS 1 INSPECTION. R & R BRAKE ON INDICATOR LIGHT LAMP IAW AMM 20-13-04-04. OPERATIONS CHECKED GOOD.

Part: DOOR — NOISY (EMERGENCY EXIT) · airframe 27,790 hrs · 24,879 cycles

PASSENGER REPORTED LOUD SQUEALING SOUND COMING FROM THE EMER EXIT AT ROW 11 ON RT SIDE OF ACFT. REMOVED RT WING EMER EXIT DOOR, INSPECTED NO DEFECTS NOTED, INSTALLED DOOR IAW AMM 52-21-00. PRESSURIZED ACFT IAW AMM 21-31-00, NO DEFECTS NOTED, RETURN TO SERVICE.

Part: STRUCTURE — DENTED (EMERGENCY EXIT) · airframe 27,591 hrs · 24,719 cycles

UPON INSPECTION FOUND RT SIDE OVERWING TE DENTED OUTWARD APPROX 1.45 INCHES LONG & 1/32 DEEP. COMPLIED IAW ERS-EM--5200-213 ACCEPT DENT AS IS. NO FURTHER ACTION REQUIRED.

Part: RELAY — FAULTY (EMERGENCY LIGHT) · airframe 27,468 hrs · 24,618 cycles

EMERGENCY LIGHT NOT ARMED MSG APPEARS ON EICAS WITH COCKPIT CONTROL IN ARM POSITION & FLIGHT ATTENDANT CONTROL IN NORM POSITION. MSG COMES ON FOR APPROX 15 - 20 SECONDS, GOES AWAY & THEN APPEARS AFTER 45 SECONDS. R & R EMER LIGHTS RELAY K0275 IAW AMM 20-13-02. EMER LIGHTING OPERATIONS CHECKED GOOD IAW AMM 33-50--00. R & R CONTROL MODULE OF EMER LIGHT & PASS SYS IAW 33-21-01. OPERATIONS CHECKED GOOD.

Part: WIRE — DAMAGED (FLASHLIGHT) · airframe 27,073 hrs · 24,308 cycles

FIRST OFFICER EF 2C RECHARGEABLE FLASHLIGHT RED LED LIGHT WIRE TORN. R & R FIRST OFFICER EF 2C RECHARGEABLE FLASH LIGHT ASSEMBLY IAW WC 33-700-20. OPERATIONAL CHECKED GOOD AT THIS TIME.

Part: FLASHLIGHT — DEGRADED (CABIN) · airframe 27,073 hrs · 24,308 cycles

FORWARD PAX CABIN EF 2C RECHARGEABLE FLASHLIGHT DEGRADED INSULATION, SIGN OF RUSTY. R & R FWD PAX CABIN EF 2C RECHARGEABLE FLASHLIGHT ASSEMBLY IAW WC 33-700-20. OPERATIONAL CHECKED GOOD AT THIS TIME.

Part: INDICATION SYS — CONTAMINATED (AIRSPEED) · airframe 26,742 hrs · 24,000 cycles

AT FL 370 IN IMC WE RECEIVED IAS COMPARE TO CAUTIONS. IT WAS DETERMINED THAT THE FIRST OFFICER`S SIDE WAS GIVING INCORRECT INFO, THEN CAPTAINS & FIRST OFFICER`S AIRSPEED INDICATIONS BECAME ERRATIC & DECREASED RAPIDLY, PLI APPEARED AFTER DESCENDING THROUGH FL240 INDICATIONS SEEMED TO BE NORMAL. FOUND WATER IN SYS, DRAINED WATER, OPERATIONS TEST OF SYS IAW AMM 34-15-00. OPERATIONS CHECKED GOOD & NO DEFECTS NOTED.

Part: HOLDER — DEFECTIVE (FLASHLIGHT) · airframe 26,598 hrs · 23,860 cycles

AFT FLASHLIGHT HOLDER LOOSE, FLASHLIGHT NOT STAYING IN HOLDER CLIP ASSEMBLY. R & R AFT FLASHLIGHT HOLDER IAW AMM 33-50-16, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,585 hrs · 23,845 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R CAPTAIN`S FLASHLIGHT IAW EEL.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 26,518 hrs · 23,791 cycles

CAPTAIN`S REPORTS PTRIM MAIN INOPERATIVE, MSG IN CRUISE. MAIN SYS CUT OUT SELECTED. COMPLIED WITH FIM TASK 27-43-00-810-801-A. PERFORMED OPERATIONS TEST IAW AMM TASK 27-40-00-700-802-A, & 27-40-00-700-803-A, OPERATIONS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 25,690 hrs · 23,028 cycles

COPILOT FLASHLIGHT HOLDER BROKEN. R & R COPILOT FLASHLIGHT HOLDER IAW AMM 33-50-16. OPS CHECK GOOD.

Part: UNKNOWN — SMOKE (RT MLG) · airframe 24,177 hrs · 21,735 cycles

ON FLIGHT 2998 THE CREW REPORTED THEY NOTICED A BURNING ODOR AND SMOKE FROM INBOARD BRAKE ON RIGHT MAIN GEAR. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED TAXI CHECK WITH CREW NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR FRAME — CRACKED (ACCESS PANEL) · airframe 24,120 hrs · 21,688 cycles

DURING MBV INSPECTION FOUND REAR ELECTRONICS ACCESS PANEL (272DR) INNER DOOR FRAME WITH 1 CRACK APPROXIMATELY 1.5 INCHES LONG UNDER ATTACHMENT PIN BRACKET. THE AIRCRAFT WAS REMOVED FROM SERVICE. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER AT CRACKED AERA IAW EO EM-52MR-353. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,120 hrs · 21,688 cycles

DURING MAINTENANCE INSPECTION PERFORMED PERMANENT REPAIR IAW PART C OF THIS EO AT OR PRIOR TO THE NEXT SCHEDULED MBV AIRCRAFT ARRIVED FOR MBV INSPECTION WITH TDMI FOR DAMAGE TO REAR FUSELAGE L THAT REQUIRED A PERMANENT REPAIR. THE AIRCRAFT WAS REMOVED FROM SERVICE. FABRICATED AND INSTALLED DOUBLER OVER DAMAGED AREA IAW EO EM-53MR-2017. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 24,120 hrs · 21,688 cycles

DURING MBV INSPECTION, QC FOUND FRAME 23 CRACKED BETWEEN STRINGERS 15R AND 16R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CRACKED SECTION OF THE FRAME, FABRICATED AND INSTALLED NEW REPAIR PARTS IAW EO EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 24,120 hrs · 21,688 cycles

DURING MBV INSPECTION FOUND THE CENTER LAV OMEGA BEAM CORRODED AROUND THE FORWARD NUT PLATE HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EO EM-53MR-2120. CORROSION LEVEL NOT SPECIFIED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 24,138 hrs · 21,703 cycles

DURING B INSPECTION FOUND THE RIGHT LAV GUSSET CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT LAV GUSSET IAW EMB SRM 51-40-02. LEVEL OF CORROSION NOT SPECIFIED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — EXPOSED (CABIN) · airframe 24,138 hrs · 21,703 cycles

DURING B INSPECTION FOUND THE NR 1, 2, 4, 5, 7 & 8 EMERGENCY FLOOR PROXIMITY LIGHT STRIPS WIRES EXPOSED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1, 2, 4, 5, 7 & 8 EMERGENCY FLOOR PROXIMITY LIGHT STRIPS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,992 hrs · 21,572 cycles

ON FLIGHT 3956 THE CREW REPORTED THE FLIGHT ATTENDANT FLASHLIGHT IN THE FORWARD CABIN WOULD NOT CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE FORWARD FLIGHT ATTENDANT FLASHLIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,981 hrs · 21,563 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT ASSEMBLY IAW EMB AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,536 hrs · 21,167 cycles

DURING B INSPECTION FOUND THE RIGHT AFT OVERWING EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVERWING EXTERNAL EMERGENCY LIGHT IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,345 hrs · 21,016 cycles

DURING B INSPECTION FOUND THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,276 hrs · 20,959 cycles

DURING B INSPECTION FOUND THE GALLEY EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP PER EMB140 AMM 33-50-09. THE OPERATIONAL CHECK WAS GOOD PER EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — CRACKED (COCKPIT) · airframe 23,224 hrs · 20,920 cycles

DURING B INSPECTION FOUND THE EMERGENCY FLASHLIGHT HOLDER ABOVE CAPTAINS SEAT HAD A CRACKED LOWER ARM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT HOLDER ABOVE CAPTAIN'S SEAT. THE OPERATIONAL CHECK WAS GOOD IAW EMB140 AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 22,832 hrs · 20,536 cycles

DURING B INSPECTION FOUND THE FIRST OFFICER’S EMERGENCY FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S EMERGENCY FLASHLIGHT BULB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,478 hrs · 20,170 cycles

DURING MAINTENANCE INSPECTION, FOUND BOTH OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY HOLDER ASSY AND BATTERY POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,450 hrs · 20,138 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT AND RIGHT EXTERIOR OVERWING AFT EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND BATTERY CHARGER IAW AMM WC 33-700-19. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 22,448 hrs · 20,136 cycles

FLIGHT 3157, DURING PREFLIGHT INSPECTION, FLIGHT ATTENDANT REPORTED A STRONG ODOR IN AFT CABIN RESEMBLING FUEL OR ACETONE. AIRCRAFT REMOVED FROM SERVICE. AFTER INSPECTION OF SOURCE OF ODOR IT CAME FROM LAVATORY. RESERVICED LAVATORY SYSTEM. NO ODOR IS NOTICED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT OVERWING) · airframe 22,450 hrs · 20,138 cycles

DURING MAINTENANCE INSPECTION, FOUND THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT ASSEMBLY INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERWING EXTERIOR EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-10. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,424 hrs · 20,110 cycles

DURING B INSPECTION, FOUND BOTH AFT OVER THE WING EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY NR 4 IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,358 hrs · 20,036 cycles

DURING MAINTENANCE INSPECTION, FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY SUPPLY AND BATTERY HOLDER ASSEMBLY IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — MALFUNCTIONED (NR 1 ENGINE) · airframe 22,259 hrs · 19,918 cycles

ON FLIGHT 3018 THE CREW REPORTED THAT DURING CRUISE RECEIVED A HYDRAULIC SYSTEM 1 LOW QUANTITY THEN 20 MINUTES LATER HYDRAULIC SYSTEM 1 FAIL MESSAGE DISPLAYED ON EICAS. THE GEAR EXTENDED NORMALLY. THE CREW DECLARED AN EMERGENCY, COMPLETED THE EMERGENCY CHECKLIST AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW EMB 140 AMM 29-10-03. THE OPERATIONAL CHECK AND LEAK CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LOOSE (CABIN DOOR) · airframe 21,870 hrs · 19,493 cycles

ON FLIGHT 3190 THE CREW REPORTED THE MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND HANDLE LOOSE. RE-SECURED MAIN CABIN DOOR ACTUATING HANDLE IAW EMB 140 AMM 52-18-05. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MODULE — UNSERVICEABLE (COCKPIT) · airframe 21,469 hrs · 19,118 cycles

ON FLIGHT 4392 THE CREW REPORTED THE EMERGENCY LIGHT SWITCH IN THE COCKPIT WAS BROKEN THE LIGHTS TURNED ON IN ALL POSITIONS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MODULE ASSEMBLY IAW M/M 20-13-10 PER M/M 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 20,194 hrs · 18,077 cycles

WIRE BROKEN ON EMERGENCY LIGHT FLOOR STRIP AT ROW 9-11. REMOVED AND REPLACED EMERGENCY LIGHT FLOOR STRIP IAW EMB AMM 33-50-12, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,840 hrs · 19,840 cycles

DURING MAINTENANCE BASE VISIT FOUND BOTH OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,233 hrs · 17,314 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OUTBOARD SEAT TRACK SUPPORT AT FRAME 50 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOR REPAIR COMPLIED WITH EO EM-53MR-1807. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — FAULTY (RT MLG) · airframe 18,367 hrs · 16,396 cycles

ON FLIGHT 3192 AT FLIGHT LEVEL 230 THE CREW REPORTED A RIGHT INBOARD 'BRAKE OVERHEAT' MESSAGE ON EICAS. THE CREW LOWERED THE LANDING GEAR PER THE AIRCRAFT OPERATIONS MANUAL FOR GEAR DOWN. THE CAPTAIN ELECTED TO DIVERT TO SBA DUE TO LACK OF FUEL. AS A PERCAUTION, CRASH, FIRE AND RESCUE WERE CALLED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT INBOARD BRAKE TEMPERATURE SENSOR IAW AMM CHAPT 32-47-01. THE OPERATIONAL CHECKS WERE GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,152 hrs · 15,048 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT EMERGENCY FLASHLIGHT NOT WORKING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRAKE — LEAKING (MLG) · airframe 14,186 hrs · 12,452 cycles

ON FLIGHT 4391 - CREW REPORTED AFTER LANDING RAMP REPORTED SMOKE COMING FROM NR 4 TIRE/BRAKE ASSY RAMP REQUESTED CFR. NO SMOKE VISIBLE WHEN CFR ARRIVED. CFR REPORTED TIRE/BRAKE ASSEMBLY TEMP AT 300 F VIA INFERRED TEMP METER. ACFT TAXIED TO THE GATE WITH OUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NR 4 BRAKE LEAKING. REMOVED AND REPLACED BRAKE AND NR 3 AND NR 4 AND WHEELS. AIRCRAFT RETURNED TO SERVICE.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 10,328 hrs · 9,656 cycles

CAPTAINS WINDSHIELD DELAMINATED AFTER TAKEOFF. REMOVED AND REPLACED WINDSHIELD IAW EMB AMM 56-10-01. OPERATIONAL CHECK GOOD - AIRCRAFT RETURNED TO SERVICE

Part: CONTACT — FAILED (EMERGENCY LIGHTS) · airframe 9,836 hrs · 9,332 cycles

RECEIVED EMERGENCY LIGHT NOT ARM MESSAGE, ABORTED TAKEOFF. REMOVED AND REPLACED ESSENTIAL BUS TIE CONTACTOR IAW EMB AMM 24-60-03. OPERATIONAL CHECKED GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

LAST 3 STRIPS OF EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED NR 4 POWER PACK IAW OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SKIN — SCRATCHED (MAIN DOOR)

DISC STRATCH ON THE MAIN ENTRANCE DOOR SKIN. PERFORMED A CUT OUT OF THE MAIN ENTRANCE DOOR SKIN. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW SRM AND EO. (SW21200600537) (K)

Part: SILL — CORRODED (SERVICE DOOR)

THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE CENTER SILL TO REMOVE THE CORROSION. PERFORMED EDDY CURRENT WITH NO REJECTABLE INDICATIONS. FABRICATED 2 DOUBLERS FOR REPAIR. REPAIR DONE IAW SRM. (K)

Part: SKIN — DAMAGED (FUSELAGE)

DURING AN MBV INSPECTION AND REPAIR OF DENT ON LEFT CENTER FUSELAGE 1 TDMI 851530243. PERFORMED CUT OUT OF THE SKIN PANEL BETWEEN FRAMES 22 AND 23 AND STRINGERS 13L AND 14. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 29, CHAPTERS 53-21-01 FIG 201. (M)