N800AE

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,783 hrs · 30,786 cycles

DURING PS-1 CHECK, FOUND OVERWING EMER EXIT LOCATING SIGN FWD INOP-C/A-REMOVED AND REPLACED OVERWING FWD EMER EXIT LOCATING SIGN IAW EMB140 AMM 33-50-15, OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,644 hrs · 30,647 cycles

FA REPORTS THAT CLOSING THE DOOR MAKES FRONT FLASHLIGHT STOP CHARGING - POSSIBLY BAD CONTACTS. C/A-REMOVED AND REPLACED FLIGHT ATTENDENT FLASHLIGHT ASSEMBLY IAW AMM 33-50-16.

Part: IGNITION UNIT — MALFUNCTIONED (NR 1 ENGINE) · airframe 33,578 hrs · 30,571 cycles

SUPPLEMENTAL HUNG START ENGINE #1 N2 HUNG AT 33%, HAD FUEL FLOW BUT NOT ITT RISE. RAMPER SIGNALED THAT HE SAW LOTS OF SMOKE OUT THE BACK AND SMALL FLAMES IN FRONT OF ENGINE. "TRANSFERRED TO NRWC 800-ABI-02432"-C/A-INSPECTED #1 ENGINE INLET AND EXHAUST FOUND NO INDICATION OF FIRE OR SOOT, ENGINE ITT WAS AT 140 C JUST AFTER EVENT, PERFORMED 2 ENGINE STARTS ONCE ON CHANNEL B AND ONCE ON CHANNEL A. FOUND IGN CHANNEL A TO BE INOP. REMOVED AND REPLACED A CHANNEL IGNITOR NO FIX SEE NRWC 800-ABI-02432 FOR FURTHER DETAILS. DEFERRED MEL 74-1 AUTH #070001-B. ENGINE FOUND OK FOR SERVICE. REMOVED AND REPLACED #1 IGNITION CH "A" IAW MM 74-13-10 OPS CHECK GOOD. MEL RESTORED.

Part: ENGINE — FIRE (NR 1) · airframe 33,503 hrs · 30,495 cycles

GROUND PERSONNEL OBSERVED FLAMES OUT OF BACK OF ENGINE #1 AND WHITE SMOKE COMING OUT OF FRONT AT SHUTDOWN. NO EICAS MESSAGES PRESENT. "TRANSFERRED TO NRWC 800-ABI-02406"-C/A-REMOVED AND REPLACED #1 ENGINE IAW WORK CARD 71-000-00 LEAK CHECK GOOD OPS CHECK GOOD

Part: SKIN — DENTED (PAX DOOR) · airframe 33,476 hrs · 30,466 cycles

PASSENGER DOOR OUTER SKIN DENTED. REPAIRED PASSENGER DOOR OUTER SKIN IAW SRM 52-10-01

Part: SKIN — DENTED (PAX DOOR) · airframe 33,472 hrs · 30,461 cycles

FOUND DENT ON AFT SECTION OF PAX DOOR EDGE 14.5 INCHES FROM BOTTOM OF DOOR, ABOUT .75 INCHES WIDE, 1.0 INCHES LONG AND ABOUT .120 INCHES DEEP. "MAJOR REPAIR" "TRANSFERRED TO NRWC 800-ABI-02384"-C/A-PERFORMED DOUBLER AND FILLER REPAIR ON AFT SECTION OF PAX DOOR EDGE 14.5 INCHES FROM BOTTOM OF DOOR IAW EMB 140 SRM 52-10-01 FIGURE 204

Part: PIN — BACKED OUT (CONNECTOR) · airframe 33,298 hrs · 30,288 cycles

SUPPLEMENTAL SERVICE DOOR OPEN/NO PRESS ISSUES. C/A-FLIGHT CREW PLACARDED SERVICE DOOR WARNING SYSTEM. AUTH # 050195-B MEL 52-04 MOC # 607040. T/S SERVICE DOOR OPEN INDICATED FOUND PIN K NO CONNECTOR P7198 PUSH OUT RESET PIN K ON CONNECTOR P7198 IAW GENERAL MAINTENANCE PRACTICES OPS CHECK GOOD MEL RESTORED.

Part: SKIN — PEELING (FUSELAGE) · airframe 33,025 hrs · 30,033 cycles

TRANSFERED FROM AML PAGE 4191593 ITEM 3. FOUND POSSIBLE CRACK/SKIN PEELING AT FRAME 25 STRINGER 21L REF. ITEM 1 OF THIS LOG PAGE. C/A-COMPLIED WITH REPAIR OF DAMAGED AREA AT FRAME 25 STRINGER 21L AND 21R IAW SRM 53-22-01.

Part: CONTROL UNIT — FAILED (HOR STAB TRIM) · airframe 32,826 hrs · 29,857 cycles

PTRIM MAIN INOP WARNING MESSAGE DURING DECENT.-C/A-FOLLOWED FIM TASK 27-43-00-810-801-A. REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB 140 AMM 27-40-01. OPC FAILED, MESSAGE REMIANS ON EICAS. FURTHER T/S REQUIRED. PERFORMED CMC DOWNLOAD AND FOUND "CTRL WHEEL TRIM SW FAULT" MESSAGE. REMOVED AND REPLACED FO CONTROL YOKE PITCH TRIM SWITCH IAW EMB 140 AMM 27-40-03 OPC FAILED. FURTHER T/S REQUIRED. CLEANED AND INSPECTED CANNON PLUG P1085 AND P1086. RESECURED AND PERFORMED OPERATIONAL CHECK OF HORIZONTAL STABILIZER TRIM SYSTEM IAW EMB AMM 27-40-00. OPC GOOD NO FURTHER DEFECTS NOTED. HORIZONTAL STAB SWITCH ASSY P/N 145-63000-401

Part: SKIN — DAMAGED (FUSELAGE) · airframe 32,240 hrs · 29,278 cycles

GASH BELOW DOOR 312, APPLIED SPEED TAPE FOR FERRY FLIGHT. REPAIRED SKIN AND ACCESS DOOR RETAINER BETWEEN STR 18R AND 16R FR 78 AND 81 IAW EM-53MR-3479.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,083 hrs · 28,052 cycles

NR 4 AISLE EMERGENCY LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED THE LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD.

Part: FRAME — CORRODED (FRM 65) · corrosion level 2 · airframe 31,068 hrs · 28,035 cycles

FRAME 65 CORRODED BETWEEN STRINGERS 16 AND 17L. REPAIRED THE FRAME IAW ERS-EM-53MR-3200.

Part: TRIM SWITCH — FAILED (COCKPIT) · airframe 30,826 hrs · 27,830 cycles

MAIN PITCH TRIM SYS FAILED INFLIGHT DURING CRUISE WITH THE AUTO PILOT ON. WHILE SLOWING ON FINAL AT 180 KNOTS WE GOT A BACKUP PTRIM INOPERATIVE. R & R CAPTAINS & FIRST OFFICERS YOKE PITCH TRIM SWITCHES IAW AMM 27-40-03. OPERATIONS CHECKED GOOD. R & R CAPTAINS & FIRST OFFICERS AUTO PILOT DISC SWITCHES IAW AMM 22-11-07. FUNCTIONAL CHECK GOOD RVSM & CAT II ELIGIBLE.

Part: ACTUATOR — FAILED (AILERON) · airframe 30,623 hrs · 27,688 cycles

ON TAKEOFF FELT A SLIGHT UNCOMMANDED ROLL. R & R ROLL TRIM ACTUATOR IAW AMM 27-14-00. OPERATIONS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 30,357 hrs · 27,441 cycles

MAIN CABIN DOOR HANDLE STICKY & HARD TO OPERATE. LUBRICATED MAIN CABIN DOOR IAW SMP. OPERATIONS CHECKED GOOD, NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,259 hrs · 27,341 cycles

EMERGENCY LIGHT NR 7 CEILING PANEL INOPERATIVE. R & R EMERGENCY LIGHT IN NR 7 CEILING PANEL IAW AMM 33-50-08, OPERATIONS CHECKED GOOD.

Part: CONNECTOR — DAMAGED (FLASHLIGHT ASSY) · airframe 30,248 hrs · 27,330 cycles

AFT CABIN FLASHLIGHT INOPERATIVE. R & R CONNECTOR J8017 IAW SWPM 20-50-00. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,847 hrs · 26,984 cycles

RT & LT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EPSU IAW AMM 33-50-04, OPERATIONS CHECKED GOOD, SEE AML 3494619 2 FOR BATTERY R & R.

Part: BATTERY — FAILED (CABIN) · airframe 29,847 hrs · 26,984 cycles

NR 4 EPSU BATTERY R & R DUE TO CHARGER IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: HOLDER — DEFECTIVE (CABIN) · airframe 29,677 hrs · 26,836 cycles

DURING MX INSPECTION ON FLIGHT 3479 FOUND RT & LT WING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY HOLDER ASSEMBLY IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: VALVE — FAILED (BLEED AIR SYS)

ON FLIGHT 2744 DURING CLIMB OUT CREW REPORTED BLEED 1 OVER TEMPERATURE EICAS WARNING DURING CLIMB OUT & DECLARED EMERGENCY. RETURNED TO KORD. THE ACFT WAS REMOVED FROM SERVICE. R & R NR 1 FAN AIR VLV IAW EMB-145 AMM 36-11-03, OPERATIONS CHECKED GOOD IAW AMM 36-00-00. THE ACFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,444 hrs · 26,643 cycles

DURING MAINTENANCE INSPECTION FOUND MAIN DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R MAIN DOOR EXTERNAL EMERGENCY LIGHT IAW EMB-140 AMM 33-50-10 CHECKED GOOD.

Part: LENS — CRACKED (CABIN) · airframe 29,355 hrs · 26,579 cycles

PASSENGER ENTRY DOOR EMERGENCY LIGHT LENS CRACKED. R & R PASSENGER ENTRY DOOR EMERGENCY LIGHT LENS IAW 140 AMM 33-26-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,209 hrs · 26,453 cycles

MAIN CABIN DOOR GROUND ILLUMINATING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-50-06. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 28,160 hrs · 25,463 cycles

DURING B-INSPECTION, FOUND THE RT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE RT AFT OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-50-07, STEPS 4 AND 5. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 28,123 hrs · 25,429 cycles

A PASSENGER SITTING IN 15A NOTICED A STRONG ELECTRICAL ODOR DURING THE DESCENT. THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS REMOVED FROM SERVICE. COULD NOT FIND ANY ELECTRICAL BURNING ODOR. AS A PRECAUTIONARY ACTION THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS R & R. ALSO, THE 15A SEAT AREA CEILING AND SIDE WALL LAMPS WERE R & R IAW AMM 33-21-06. FLUORESCENT LAMP, PN: 5113WW. THE FUNCTIONAL CHECK FLIGHT WAS SATISFACTORY. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — FAULTY (CABIN) · airframe 27,604 hrs · 24,969 cycles

ON FLIGHT 2847 THE FLIGHT ATTENDANT REPORTED A STRONG CHEMICAL ODOR DURING FLIGHT IN THE FOWARD SECTION OF THE PASSENGER CABIN. ALSO THE COCKPIT CREW REPORTED THE CAPTAIN’S FLASHLIGHT SMELLED LIKE ELECTRICAL BURNING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANT FLASHLIGHT IAW EMB-140 AMM 33-50-16. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT PART NUMBER P2-07-0011-100 IAW EMB 140 AMM 25-60-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 27,607 hrs · 24,971 cycles

ON FLIGHT 2832 THE CREW REPORTED THAT AN ELECTRIC BURNING SMELL STILL EXISTS IN THE FRONT CABIN AREA. REFERENCE SDR SIMA20130403005 FOR PREVIOUS REPORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ENGINE RUNS IAW EMB. AMM 71-00-01. OPERATED PACKS IN HOT AND COLD FOR INDICATION OF SMELL IAW EMB 21-51-00. PERFORMED OPERATIONAL CHECK OF WINDSHIELD HEAT IAW EMB 30-42-00. CHECKED LIGHTS FOR INDICATION OF SMELLS NO ELECTRICAL ODORS NOTED AT THIS TIME. REF NRWC 800-DFW-01057. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — FAULTY (CABIN) · airframe 27,402 hrs · 24,805 cycles

ON FLIGHT 3426 THE CREW REPORTED A STRONG ELECTRICAL SMELL AROUND THE FLIGHT ATTENDANT SEAT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 27,114 hrs · 24,561 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO DOOR SKIN DENTED & GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED CARGO DOOR SKIN IAW EMB SRM 52-30-01 & EO 5202-332. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 27,114 hrs · 24,561 cycles

DURING MAINTENANCE INSPECTION FOUND CORRODED CIRCUMFERENTIAL SPLICE BENEATH AIR DUCT AT 415.5 STRINGERS 21 LEFT TO 21 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CIRCUMFERENTIAL SPLICE IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRAP — CORRODED (FUSELAGE) · airframe 27,267 hrs · 24,683 cycles

DURING MAINTENANCE INSPECTION FOUND RIGHT OMEGA BEAM GUSSET STRAP CORROSION AT SCREW HOLES AS MARKED, BETWEEN FRAMES 60 AND 61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORROSION AT RIGHT OMEGA BEAM BUSSET AT SCREW HOLES FOUND TO BE OUT OF LIMITS BETWEEN FR 60 AND 61 IAW EMB 140 SRM 51-10-03. LOCATED, DRILLED AND DEBURRED NEW GUSSET STRAP IAW EMB 140 SRM 51-20-03 AND 51-40-02 AND 61. REMOVED CORRODED GUSSET IAW EMB 140 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MISALIGNED (CABIN) · airframe 27,304 hrs · 24,717 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT NR 2 CABIN FLOOR LIGHT STRIP MISALIGNED IN PROXIMITY HOLDER. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ALIGNED LIGHT STRIP IN NR 2 LEFT CABIN FLOOR LIGHT STRIP HOLDER EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,267 hrs · 24,683 cycles

DURING MAINTENANCE INSPECTION FOUND CENTER OMEGA BEAM GUSSET STRAP HAS CORROSION AT SCREW HOLES AS MARKED, BETWEEN FRAMES 60 AND 61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVE CORROSION AT CENTER OMEGA BEAM GUSSET AT SCREW HOLE FOUND TO BE OUT OF LIMITS BETWEEN FR 60 AND 61 IAW EMB 140 SRM 51-10-03. REMOVED CENTER OMEGA BEAM GUSSET STRAP BETWEEN FRAMES 60 AND 61 REF EMB 145 SRM 51-40-02. LOCATED DRILLED AND DEBURR REF EMB 145 SRM 53-24-10 SRM 51-20-03. INSTALLED NEW CENTER OMEGA BEAM GUSSET PER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,322 hrs · 24,728 cycles

DURING MAINTENANCE INSPECTION FOUND CORROSION AT CARGO DOOR FRAME SILL AROUND NUT PLATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. BLENDED OUT CORROSION PER EMB 145 SRM 51-10-03 OUT OF LIMITS 100% MAT LOSS PER EMB 145 SRM 53-31-10. REMOVED FASTENERS AND DAMAGED AREA PER EMB SRM 51-40-02 AND 53-31-15 PARA(C). FABBED DOUBLER FROM MATERIAL 7475T761 .080 IAW EMB SRM 53-31-15 PARA E. LOCATED DRILLED AND COUNTERSUNK PER EMB SRM 51-20-03. PERFORMED HFEC INSP OF DAMAGE CUT OUT NO DEFECTS NOTED IAW NIM INTRO ITEM E. PREPPED AND PRIMED REPAIR AREA AND PARTS PER EMB SRM 51-21-04 51-21-05. INSTALLED REPAIR DOUBLER PER EMB SRM 53-31-15. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIP — TORN (CABIN) · airframe 27,343 hrs · 24,746 cycles

DURING MAINTENANCE INSPECTION FOUND LIGHTS STRIP HOLDER -2 BLACK SPLICE STRIPS FOR LIGHT STRIP TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED 2 BLACK SPLICE STRIPS FOR CABIN FLOOR LIGHT STRIP AS PER EMB 140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,018 hrs · 24,475 cycles

DURING B INSPECTION FOUND THE LEFT WING EXIT INTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT LAMP IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (FLASHLIGHT) · airframe 26,708 hrs · 24,184 cycles

DURING B INSPECTION FOUND THE AFT EMERGENCY FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT LAMP IN REF TO DME CMM 25-60-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PITOT LINE — CRACKED (PITOT/STATIC SYS)

ON FLIGHT 3261 THE CREW REPORTED THAT DURING CRUISE AT FLIGHT LEVEL 370 IN VISABLE MOISTURE AT 200 KNOTS AND ENTERING A HOLD, THE FIRST OFFICER’S INDICATOR BECAME UNRELIABLE AND THEN DECREASED TO ZERO SHORTLY AFTER THE F/O'S ALTIMETER BECAME UNRELIABLE AND DIFFERED FROM THE CAPTAIN’S ALTIMETER BY APPROX 400 FT, THE EICAS DISPLAYED SPS ADVANCED FOLLWED BY THE CAPTAIN’S MESSAGE WHICH WHEN CHECKED DISPLAYED IC2 WOW INOP, THEN AP AND YD FAILED. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO ICT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLSHOT AND FOUND THE PITOT HOSE ASSEMBLY CRACKED. REMOVED AND REPLACED THE HOSE ASSEMBLY IAW EMB 140 AMM 34-13-05. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 34-15-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 26,346 hrs · 23,903 cycles

ON FLIGHT 2766 THE CREW REPORTED, RECEIVED A NR 1 PACK OVERLOAD EICAS MESSAGE. THE FLIGHT ATTENDANT REPORTED A POSSIBLE ELECTRICAL BURNING ODOR IN THE CABIN. THE CREW TURNED THE PACK OFF FOR 3 MINUTES. THEY TURNED IT BACK ON AND IT OPERATED NORMALLY AND THE ODOR DISSIPATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED CMC DOWNLOAD PER AMM 45-45-00, NO MESSAGES. PERFORMED OPERATIONAL CHECKS AND GENERAL VISUAL INSPECTION OF NR 1 PACK IAW AMM 21-51-00. NO FAULTS, LEAKS, OR DEFECTS NOTED. DURING ALL OPS AND LEAK CHECKS, NO ELECTRICAL SMELLS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (FLASHLIGHT) · airframe 25,301 hrs · 23,074 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN'S FLASHLIGHT HAS BROKEN ELECTRICAL CONNECTOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT AND CRADLE IAW WC 33-700-20. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 25,141 hrs · 22,911 cycles

DURING MAINTENANCE INSPECTION FOUND THE BAGGAGE FLOORBOARD 272BF HAS SOFT SPOT OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE BAGGAGE COMPARTMENT FLOORBOARD IAW AMM 53-01-03-000-801-A & 53-01-03-400-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,019 hrs · 22,801 cycles

DURING B-INSPECTION FOUND THE AFT CABIN AISLE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN AISLE EMERGENCY LIGHT LAMP IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,623 hrs · 22,442 cycles

ON FLIGHT 3912 THE CREW REPORTED THE FORWARD FLIGHT ATTENDANT’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDAN’TS FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INSULATION — DAMAGED (FIRE DETECTION) · airframe 24,551 hrs · 22,380 cycles

ON FLIGHT 4150 THE CREW REPORTED E2 FIRE DET FAIL ON INTERMITTENTLY INFLIGHT, CRUISE, DESCENT AND APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED INSULATION REPAIR ON W407-0014-20 & W407-0013-20 APPROX 3 FT FROM PO914 IAW EMB SWPM 20-21-00. FIRE DETECTION SYS OPS CHECK GOOD PER EMB 140 MM 26-10-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 24,530 hrs · 22,362 cycles

DURING MAINTENANCE INSPECTION FOUND THE CARGO BAGGAGE FIRE DETECTOR FAILED TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD SMOKE DETECTOR IN CARGO COMPARTMENT IAW EMB 140 AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 24,517 hrs · 22,351 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FORWARD CABIN FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN FLASHLIGHT IN REFERENCE WITH EMB AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,318 hrs · 22,176 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE AISLE CEILING LIGHT (EMERGENCY) AT ROW 15 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB AT ROW 15 AISLE CEILING POSITION IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 22,877 hrs · 20,976 cycles

FOR FLIGHT 2721 DURING THE PREFLIGHT INSPECTION FOUND THE RIGHT WING AFT EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WING AFT EMERGENCY LIGHT LAMP IAW EMB140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRIP — BROKEN (CABIN) · airframe 22,719 hrs · 20,847 cycles

ON FLIGHT 4060 THE CREW REPORTED THE EMERGENCY FLOOR LIGHT STRIP AT ROW 16 IS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIP AS REQUIRED IAW EMB140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 22,239 hrs · 20,402 cycles

DURING MAINTENANCE BASE VISIT FOUND RIVET HOLES FOR FAIRLEAD AT FRAME 55 ELONGATED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 55 IAW EO EM-53MR-1772. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — GOUGED (AILERON) · airframe 22,239 hrs · 20,402 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AILERON DAMPER FITTING GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AILERON DAMPER FITTING IAW ENGINEERING ORDER EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — DAMAGED (AILERON) · airframe 22,239 hrs · 20,402 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT AILERON DAMPER FITTING DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AILERON DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,239 hrs · 20,402 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 23 CRACKED IN 2 PLACES ON THE RIGHT SIDE AT FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 RIGHT SIDE IAW EO EM-53MR-1771. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,489 hrs · 18,865 cycles

INSPECTION FOR FLIGHT 4487 FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PANEL — CRACKED (PAX DOOR) · airframe 19,269 hrs · 17,706 cycles

DURING PHASE 3 INSPECTIONS FOUND THE COMPOSITE INTERIOR EMERGENCY LIGHT PANEL TO BE CRACKED. THE CRACK WAS APPROXIMATELY 1.5 INCHES LONG. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR INTERIOR COMPOSITE LINING AND THE EMERGENCY LIGHT ASSEMBLY IAW 25-23-04. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,090 hrs · 17,562 cycles

DURING MAINTENANCE INSPECTION, FOUND THAT THE AFT FLIGHT ATTENDANT’S FLASHLIGHT WOULD NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT'S FLASHLIGHT. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 13,645 hrs · 12,348 cycles

STRONG OIL ODOR IN BLEED SYSTEM FROM TAKEOFF TO 14,000 FEET. PERFORMED ENGINE RUNS WITH BLEEDS ON WITH NO DEFECTS. PERFORMED BOROSCOPE INSPECTION PER ROLLS ROYCE FAULT ISOLATION MANUAL 72-00-00 WITH NO DEFECTS. RETURNED AIRCRAFT TO SERVICE.

Part: ELECTRONIC UNIT — FAILED (ZONE 200) · airframe 13,609 hrs · 12,306 cycles

LANDING GEAR SELECTED TO UP POSITION WITH INDICATIONS SHOWING IN TRANSIT WITH NO GEAR MOVEMENT, CYCLED GEAR WITH NO CHANGE. PLACED GEAR LEVER IN DOWN POSITION FOLLOWED WITH THREE GREEN LIGHTS, RETURNED TO LAX. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT IAW EMB AMM 32-32-01. PERFORMED EXTENSION AND RETRACTION CHECKS WITH NO DEFECTS IAW EMB AMM 32-30-00. RETURNED AIRCRAFT TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,129 hrs · 11,787 cycles

CENTER BEAM FOUND CORRODED AT FRAME 20. PERFORMED CUTOUT OF CORRODED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-21-10, FIGURE 202. RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,129 hrs · 11,787 cycles

SERVICE DOOR SILL FOUND CORRODED. BLENDED AND TREATED AREA AND INSTALLED REPAIR DOUBLER BLEND AREA IAW EMB SRM 53-21-02. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,129 hrs · 11,787 cycles

CENTER OMEGA BEAM CORRODED AT FRAME 25. PERFORMED CUTOUT OF CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,129 hrs · 11,787 cycles

GALLEY FLOOR DIGITAL FOUND CORRODED. PERFORMED CUTOUT OF CORRODED AREA. REPLACED CORRODED AREA IAW EMB SRM 53-21-10, FIGURE 201. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,126 hrs · 11,787 cycles

LEFT OMEGA BEAM CORRODED AT FRAME 25. PERFORMED CUTOUT TO REMOVE CORROSION, FABRICATE AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-01 AND 51-40-02. RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 7,302 hrs · 7,247 cycles

DURING PRE-FLIGHT, THE EMERGENCY LIGHTS DID NOT WORK DURING TEST FROM FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK AND POWER SUPPLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502113) (K)

Part: CHARGER — FAILED (CABIN)

EMERGENCY FLOOR LIGHTING ROWS 1-6 FAIL TO LIGHT DURING TEST. REPLACED BATTERY AND BATTERY CHARGER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY FLOOR LIGHT ON LT SIDE (FIRST 6 ROWS) DID NOT ILLUMINATE DURING TEST. REPLACED BATTERY POWER SUPPLY 2 IAW AMM. OPERATIONAL CHECK GOOD. (SW21200502112) (K)

Part: CHARGER — INOPERATIVE (CABIN)

MAINTENANCE REPORTED THE NR 2 AND 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK AND CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501204)

Part: CHARGER — INOPERATIVE (CABIN)

MAINTENANCE REPORTED THE NR 2 AND NR 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501204)

Part: CHARGER — INOPERATIVE (CABIN)

MAINTENANCE REPORTED THE NR 2 AND NR 3 EMERGENCY FLOOR PROXIMITY STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY CHARGER IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501204)

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB)

YHZ - FLT 4819 - ON SHORT FINAL WITH AP DISCONNECTED AT APPROX 135 KTS IN VMC CONDITIONS THE CREW RECEIVED EICAS MESSAGES PITCH TRIM 1 AND 2 INOPERATIVE. PERFORMED FAULT ISOLATION PROCEDURES IAW ETN EM 27-022R1 NO LATCHED EICAS OR CMC MESSAGES FOUND. AS A PRECAUTIONARY PROCEDURE REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT IAW EMB 140 AMM CH 27-4-01 OPERATIONAL CHECK SATISFACTORY AT THIS TIME NO FURTHER DEFECTS NOTED. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

DLH - FLT 4465 - OPERATIONS REPORTED THE EMERGENCY LGIHTS ON THE AIRCRAFT ARE IN THE ON POSITION AND COULD NOT ACCESS THE COCKPIT. EMERGENCY BATTERY PACKS ARE LOW. REPLACED 4 BATTERY PACKS P/N 2013-1A S/N 73055, P/N 2013-1A S/N 69967, P/N 2013-1A S/N 73159, P/N 2013-1A S/N 70931. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING A MBV INSPECTION, THE LEFT FLOORBEAM AT FRAME 20 CORRODD BELOW SRM LIMITS. CUT OUT DAMAGE SECTION OF LEFT FLOORBEAM, CLEANED AND TREATED THE REPAIR AREA. FABRICATED AN EXTERRNAL ANGLE, FILLER, PLATE AND SHIMS. REPAIR DONE IAW EMB SRM (SRM EMB 145.1142 REV 20) CHAPTERS 53-21-10 FIG 201. (M)

Part: WARNING LIGHT — ILLUMINATED (GUST LOCK)

LAX - FLT 3446 - DURING CRUISE FLIGHT, REPORTED THE GUST LOCK AMBER LIGHT CAME ON DURING LIGHT CHOP. CREW FOLLOWED PROCEDURES AND DECLARED AN EMERGENCY. AIRCRAFT WAS DIVERTED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK WAS SATISFACTORY IAW EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: PLUNGER — DIRTY (GUSTLOCK)

CMH - FLT 3882 - DURING FLIGHT CREW REPORTED THE GUST LOCK LIGHT ILLUMINATED. CREW FOLLOWED AOM PROCEDURES AND LANDED AT NEAREST AIRPORT. AIRCRAFT WAS LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE FOUND THE GUSTLOCK PLUNGER FOR MICROSWITCHES WAS DIRTY. PLUNGER WAS CLEANED AND AN OPERATIONAL CHECK WAS DONE. AIRCRAFT WAS RETURNED TO SERVICE. (M)