N807AE

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 32,810 hrs · 30,282 cycles

AFT CABIN FLASHLIGHT NOT WORKING-C/A-REMOVED AND REPLACED AFT CABIN FLASHLIGHT IAW EMB 140 AMM 3--50-16 OPC CHECK GOOD NO DEFECTS NOTED AT THIS TIME.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,787 hrs · 30,263 cycles

EXTERNAL EMERGENCY LIGHT ON PAX DOOR INOP-C/A-REMOVED AND REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT ON PAX DOOR IAW AMM 33-50-10. OPS CHECK GOOD.

Part: FLASHLIGHT ASSY — SHORTED (CABIN) · airframe 32,773 hrs · 30,253 cycles

FWD FA FLASHLIGHT HOLDER INOP/SHORTED-C/A-DEFERRED FWD FA FLASHLIGHT HOLDER. MEL# 25-53 AUTH# 120247-C. PERFORMED OPC IAW AMM 33-51-01 WITH OTHER FLASHLIGHTS ONBOARD. OPC GOOD. SUSPECTED POSSIBLE INTERMITTENCY WITH FLASHLIGHT HOLDER. RAR FLASHLIGHT AND HOLDER IAW AMM 33-50-16. OPC GOOD. MEL RESTORED.

Part: POWER SUPPLY — NOT REPORTED (EMERGENCY LIGHTS) · airframe 31,613 hrs · 29,180 cycles

REMOVED AND REPLACED THE POWER SUPPLY IAW AMM 33-50-04. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,348 hrs · 28,936 cycles

FLASHLIGHT IN THE COCKPIT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD.

Part: CONTROL PANEL — HOT (FLT ATTENDANT) · airframe 31,051 hrs · 28,650 cycles

FA REPORTED THAT THE FA CONTROL PANEL WAS GETTING HOT AND STARTED TO SMELL LIKE AN ELECTRICAL FIRE. PERFROMED ETN-EM-72-034, NO UNSUAL ODORS OF ANY KIND NOTED.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 30,765 hrs · 28,300 cycles

AFTER GEAR EXTENSION UNUSUAL AMOUNT OF ELEVATOR FLUTTER/VIBRATION ALL THE WAY TO LANDING. LH (ON UPPER SKIN) ELEVATOR INNER LEADING EDGE II SECTION HAS A BENT AND A CRACK ABOUT 1/4" LONG, 1/2" WIDE AND 5/8" HEIGHT. PERFORMED GVI OF ELEVATOR CONTROL CABLES AND PULLYS THRU ACCESS PANELS 123BL (FWD AVIONICS), AFT TAIL CONE 312AR COMPARTMENT AND FLOOR PANEL 251BF AS PER EMB 140 32-10-00. DOORS SECURED. RE-SECURED LH RECIRCULATION SYSTEM MUFFLER IAW AMM 21-24-02. OPS CHECKED GOOD. PERFORMED AUTO PILOT TEST IAW AMM 22-11-00. CHECKED GOOD

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 30,742 hrs · 28,265 cycles

#4 EMERGENCY BATTERY PACK IS DEAD.-C/A-REMOVED AND REPLACED #4 EMERGENCY BATTERY PACK IAW EMB-140 AMM 33-50-04, OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,723 hrs · 28,233 cycles

AT 80 KTS GOT SPS FAIL MESSAGE ABORTED TAKEOFF. PERFORMED TROUBLE SHOOTING PER FIM 27-36-00 FOUND TO BE A TRANSITORY CONDITION. OPC GOOD PER AMM 27-36-00. NO MESSAGES RECORDED ON CMC OR EICAS.

Part: FRAME — CRACKED (FRM 23) · airframe 30,588 hrs · 28,065 cycles

FRAME 23 CRACKED AT RT OTBD FLOOR SUPPORT. ACCOMPLISHED INSTALLATION OF SERVICEABLE FRAME SECTION IAW EO-EM-53MR-1808.

Part: DOOR SILL — CORRODED · airframe 30,588 hrs · 28,065 cycles

CENTER SERVICE DOOR SILL CORRODED IN MULTIPLE AREAS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,588 hrs · 28,065 cycles

LEFT LAVATORY BEAM, UNDER THE LT BEAM GUSSET FOUND CORRODED AROUND FORWARD NUTPLATE HOLE. ACCOMPLISHED A PERMANENT REPAIR IAW ERS-EM-53MR-2953.

Part: FRAME — GOUGED (CARGO DOOR) · airframe 30,588 hrs · 28,065 cycles

CARGO DOOR LOWER OTBD EDGE FRAME IS GOUGED. REMOVED AND REPLACED LOWER OTBD EDGE FRAME IAW SRM 51-20-01, 51-40-02, AND 51-20-03, 51-40-06.

Part: TERMINAL — MISSING (EMERGENCY LIGHT) · airframe 30,588 hrs · 28,065 cycles

LEFT FUSELAGE NR 1 EMERGENCY LIGHT TERMINAL END MISSING. INSTALLED A SERVICEABLE EMERGENCY LIGHT TERMINAL IAW SWPM 20-21-00.

Part: DOOR SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 30,588 hrs · 28,065 cycles

CARGO DOOR SILL IS CORRODED. R & R THE DOOR SILL IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (CARGO DOOR) · airframe 30,588 hrs · 28,065 cycles

CARGO DOOR LATERAL L-SHAPE IS CORRODED ON LOWER FWD AND AFT END. R & R FRAME 65 L-SHAPE IAW SRM 53-31-04

Part: PROFILE — GOUGED (CARGO DOOR FRAME) · airframe 30,588 hrs · 28,065 cycles

CARGO DOOR UPPER OTBD EDGE OF FRAME IS GOUGED. R & R THE PROFILE IAW SRM 51-40-02.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 30,209 hrs · 27,704 cycles

LEFT AFT OVERWING EMER LIGHT INOPERATIVE. R & R LT EMER LIGHT ASSEMBLY IAW AMM 33-50-10, OPERATIONS CHECKED GOOD. EMER LIGHTING BATTERY PN 2013-1A, SN 73049 & BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 12787.

Part: COMPUTER — FAILED (NR 1) · airframe 30,150 hrs · 27,652 cycles

HEADING FAIL. DURING CRUISE THE CAPTAIN'S PFD, MFD & EICAS WENT BLACK. CREW DECLARED AN EMER & RETURNED WITHOUT INCIDENT. R & R NR 1 IC-600 IAW AMM 31-42-01. OPERATIONS GOOD IAW AMM 31-42-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,239 hrs · 26,828 cycles

FORWARD FUSELAGE 1 RT UPPER SKIN DAMAGED BETWEEN STRINGER 4R & STRINGER 14R. REMOVED DAMAGED FWD FUSELAGE 1 UPPER SKIN FROM STRINGER 1 TO STRINGER 14R & INSTALLED NEW SKIN PANEL IAW SRM 51-40-02, 51-20-01, 51-20-03 & 51-40-06.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 29,239 hrs · 26,828 cycles

FORWARD FUSELAGE 1 RT LOWER SKIN DAMAGED BETWEEN STRINGER 14R & STRINGER 15R. REMOVED DAMAGED FWD FUSELAGE 1 LOWER SKIN FROM STRINGER 14R TO STRINGER 18R & INSTALLED NEW SKIN IAW SRM 51-40-02, 51-40-03 & 51-40-06.

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 29,230 hrs · 26,819 cycles

DECLARED EMERGENCY LEFT ACCT BIRD STRIKE FOLLOWED BY ENG 1 FAILURE. FLT LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED LEFT ENGINE IAW WC 71-000-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 29,200 hrs · 26,789 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY IAW AMM 33-50-04, OPERATIONS CHECKED GOOD.

Part: BULB — INOPERATIVE (FLASHLIGHT) · airframe 28,638 hrs · 26,290 cycles

F/O'S COCKPIT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT BULB IAW CMM 33-50-16. OPS TESTED GOOD, NO FURTHER DEFECT NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,207 hrs · 25,844 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM TASK 33-50-08-000-801-A AND 33-50-08-400-801-A.

Part: LIGHT — MISINSTALLED (CABIN) · airframe 27,374 hrs · 25,086 cycles

ON FLIGHT 3402 THE CREW REPORTED THE FLOOR EMERGENCY LIGHTING STRIPS WERE INSTALLED INCORRECTLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. SWAPPED FLOOR STRIPS 1 & 5 IAW AMM 33-50-12, FLOOR STRIP NR 1 AND THE OPERATIONAL CHECK WAS OK IAW AMM 33-50-12. HOWEVER STRIP NR 5 FAILED. REMOVED AND REPLACED STRIP NR 5 IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (CARGO DOORWAY) · airframe 26,373 hrs · 24,234 cycles

DURING MAINTENANCE INSPECTION, FOUND CARGO DOOR CUTOUT SILL CORRODED BEYOND LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE CARGO DOOR CUTOUT SILL IAW SRM 53-32-01. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 26,362 hrs · 24,223 cycles

DURING MAINTENANCE INSPECTION FOUND CRACK ON LEFT FRAME 10 -- CHANNEL IS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CHANNEL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,362 hrs · 24,223 cycles

DURING MAINTENANCE INSPECTION FOUND CORROSION AT DIGITAL 0.0 AT FRAME 58 AROUND SCREW HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND RELACED DIGITAL 0.0 AT FRAME 58 AROUND SCREW HOLES IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 26,362 hrs · 24,223 cycles

DURING MAINTENANCE INSPECTION FOUND CORROSION AT GUSSET 479.0 FRAME 20 AROUND SCREW HOLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DAMAGED GUSSET AT 479.0 FR 20. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,362 hrs · 24,223 cycles

DURING MAINTENANCE INSPECTION FOUND CORROSION AT SERVICE DOOR FORWARD SILL AROUND THE SCREW HOLES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR FORWARD SILL IAW EMB SRM 51-40-20. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,362 hrs · 24,223 cycles

DURING MAINTENANCE INSPECTION FOUND CORROSION AT DIGITAL 479.0 FRAME 61 UNDER COMPOSITE BEAM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DIGITAL 479.0 FRAME 61 UNDER COMPOSITE BEAM IAW EMB SRM 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,362 hrs · 24,223 cycles

DURING MAINTENANCE INSPECTION FOUND CORROSION AT THE RIGHT WALL SILL AT FRAME 61. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT WALL SILL AT FRAME 61. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,362 hrs · 24,223 cycles

DURING MAINTENANCE INSPECTION FOUND CORROSION AT DIGITAL 479.0 FROM FRAME 22 TO FRAME 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED DIGITAL 479.0 FROM FRAME 22 TO FRAME 25 IAW SRM EMB SRM 51-20-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 26,972 hrs · 24,724 cycles

DURING B INSPECTION FOUND CORROSION AT CARGO DOOR SILL FRAME 65. THE AIRCRAFT WAS REMOVED FROM SERVICE. LOCKED AND DRILLED NEW CARGO SILL SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 26,866 hrs · 24,624 cycles

DURING B INSPECTION FOUND 5 EACH FLOOR EMERGENCY LIGHT STRIP DAMAGED AT THE BASE ONLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP BASES AS INDICATED REF EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 26,970 hrs · 24,723 cycles

DURING B INSPECTION FOUND THE NR 1 EMERGENCY LIGHT STRIP HAS BROKEN CONNECTOR (AIRCRAFT SIDE). THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED WIRES TO THE NR 1 LIGHT STRIP AND AIRCRAFT SIDE WIRING REF EMB 140 SWPM 20-00-03. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 26,972 hrs · 24,724 cycles

DURING B INSPECTION FOUND THE EMERGENCY STRIP LIGHTING ONE EACH HAS BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED RACK EMERGENCY STRIP LIGHTING WIRE REF EMB 140 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 25,946 hrs · 23,773 cycles

FLIGHT 3067, THE CREW REPORTED THAT ON APPROACH AT 6000 FT AND 243 KNOTS, RECEIVED A FLAP FAIL EICAS MESSAGE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESET SYSTEM AND COMPLIED WITH OPS CHECK IAW 27-51-00-710-801-A00. NO CMC MESSAGES DISPLAYED AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — DAMAGED (CABIN) · airframe 25,328 hrs · 23,097 cycles

DURING MAINTENANCE INSPECTION FOUND THE PASSENGER DOOR EMERGENCY LIGHT PANEL HAS A HOLE IN LOWER CORNER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT PANEL IAW AMM 25-23-04. THE EMERGENCY LIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,003 hrs · 22,801 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,583 hrs · 22,512 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT ON PAX DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY IAW EMB-140 AMM 33-50-04. THE OPERATIONAL CHECK GOOD OF THE PASSENGER DOOR EMERGENCY LIGHT WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 24,583 hrs · 22,512 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT ON PASSENGER DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 BATTERY PACK BATTERY CHARGER ASSEMBLY IAW EMB-140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 24,369 hrs · 22,372 cycles

DURING MAINTENANCE INSPECTION FOUND THE FORWARD FLASHLIGHT CLIP BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLIGHT ATTENDANTS FORWARD FLASHLIGHT HOLDER AND FLASHLIGHT IAW EMB AMM 33-50-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DAU — FAILED (NR 1)

ON FLIGHT 2711 THE CREW REPORTED THE DATA ACQUISITION UNIT 1A FAILED. ALL ASSOCIATED EICAS FAILURES PRESENTED FAILURE LASTED APPROX 30 SECONDS. THE CREW ELECTED TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DATA ACQUISITION UNIT 1. THE OPERATIONAL CHECK WAS GOOD IAW AMM 31-41-00/01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 22,713 hrs · 21,018 cycles

FOR FLIGHT 2879 DURING THE PREFLIGHT INSPECTION MAINTENANCE FOUND THE NR 4 EMERGENCY LIGHT STRIP HAD A BROKEN CONNECTOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT STRIP IAW EMB AMM 33-50-12. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,691 hrs · 21,000 cycles

DURING MAINTENANCE BASE VISIT FOUND THE MAIN CABIN CEILING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ASSOCIATED INVERTER. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 22,249 hrs · 20,593 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY EXIT PLACARD AT FORWARD OVERHEAD AISLE WING EXIT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY EXIT PLACARD AT FORWARD OVERHEAD AISLE WING EXIT IAW EMB 140 AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,740 hrs · 20,166 cycles

DURING MAINTENANCE BASE VISIT FOUND FRAME 23 TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH REPAIR OF FRAME 23 RIGHT IAW EO-EM-53MR-1715. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — GOUGED (19 LEFT) · airframe 21,741 hrs · 20,166 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND STRINGER 19 LEFT TO BE GOUGED BETWEEN FRAMES 52-53. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED STRINGER 19 LEFT IAW EMB STRUCTRAL REPAIR MANUAL 53-24-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: RUDDER — MALFUNCTIONED (TAIL) · airframe 21,480 hrs · 19,928 cycles

ON FLIGHT 4499 DURING TAKEOFF THE CREW REPORTED THE RUDDER SYSTEM 2 INOPERABLE ON TAKEOFF. THE CAPTAIN ABORTED THE TAKEOFF. THE RUDDER PEDAL FELT NORMAL. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED ELECTRICAL RE-SET IAW AMM 24-31-00 AND OPERATIONAL CHECK OF THE RUDDER SYSTEM IAW AMM 27-20-00. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED AT THIS TIME. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,432 hrs · 20,755 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FLOOR EMERGENCY LIGHT PROXIMITY STRIP TO BE INOPERABLE AT 16A. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ADJUSTMENT TEST OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-50-00. ALL EMERGENCY LIGHTS OPERATIONAL. THE OPERATIONAL TEST WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,827 hrs · 18,421 cycles

DURING MAINTENANCE INSPECTION THE EMERGENCY FLOOR PROXIMITY STRIP AT SEAT 8A WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY FLOOR PROXIMITY STRIP IAW EMB-140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BACKED OUT (EMERGENCY LIGHTS) · airframe 17,739 hrs · 16,453 cycles

ON FLIGHT 4258, DURING PRE-FLIGHT CREW NOTED EMERGENCY LIGHTS OFF OF BATTERY 3 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REINSERTED PIN "D" AT CONNECTOR P8031, OPERATION CHECK GOOD IAW EMB-140 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: OIL SYSTEM — OVERSERVICED (LT ENGINE) · airframe 17,059 hrs · 15,850 cycles

FLIGHT 3115, DURING DESCENT CREW REPORTED BURNING ODOR AND SMOKE IN THE COCKPIT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED EMB 140 FIM 21-20-00-810-801-A AND FIM 21-20-00-810-803-A. FOUND OIL OVERSERVICED AT LT ENGINE. CLEANED COWLING AND ENGINE COMPONENTS. PERFORMED ENGINE RUN IAW EMB 140 AMM 71-00-00. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — SMOKE (LAVATORY LIGHTS) · airframe 14,860 hrs · 13,249 cycles

ABOUT 500' AFTER TAKEOFF 'LAV SMOKE' WARNING ILLUMINATED. WARNING LIGHT WENT OFF ON FINAL APPROACH, FA REPORTED SMOKE IN CABIN. TOUCHDOWN WAS SOFT. REMOVE AND REPLACED BOTH LAVATORY BALLAST IAW 140 AMM 33-28-02. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 14,860 hrs · 13,249 cycles

CREW FOLLOWED UP WITH CALL ABOUT 500' AFTER TAKEOFF 'LAV SMOKE' WARNING ILLUMINATED. WARNING LIGHT WENT OFF ON FINAL APPROACH. FA REPORTED SMOKE IN CABIN. OVERWEIGHT LANDING: LANDING WEIGHT 42320, SINK RATE 200 FT PER MIN TOUCHDOWN WAS SOFT.

Part: LANDING GEAR — DAMAGED (NOSE) · airframe 14,598 hrs · 12,964 cycles

AT ROTATION AND LIFT OFF GEAR WOULD NOT RETRACT AT THE SAME TIME GOT EICAS MESSAGE OF 'AIR GROUND FAILED'. RETURNED TO SFO AND MADE FLAPS 45 LANDING AT 0-50FPM SINC RATE AND 38270 POUND GROSS WEIGHT. SFP TO LAX. REMOVED AND REPLACED NOSE LANDING GEAR IAW EMB MM 32-20-01 OPS CHECK GOOD AIRCRAFT RETURNED TO SERVICE

Part: WIRE HARNESS — DAMAGED (MLG PROX SWITCH) · airframe 14,572 hrs · 12,934 cycles

LANDING GEAR FAILED TO RETRACT LOCKED IN DOWN POSITION (HANDLE). CREW ELECTED TO RETURN TO SJC. AIRCRAFT LANDED AND RETURNED SAFELY TO THE GATE. REMOVED AND REPLACED NOSE PROX SWITCH HARNESS AND LANDING GEAR ELECTRONIC CONTROL.

Part: LANDING GEAR — INOPERATIVE · airframe 14,551 hrs · 12,908 cycles

SOC REPORTED THE AIRCRAFT WAS RETURNING TO FIELD WITH GEAR THAT WOULD NOT RETRACT.

Part: RELAY — FAILED (ZONE 200) · airframe 14,454 hrs · 12,802 cycles

LG AIR/GND FAIL MESSAGE ON TAKEOFF, RETURNED TO SJC. SERVICED LEFT STRUT IAW EMB AMM 32-10-02. REMOVED AND REPLACED RELAY K0453 AND K0353 IAW WMM 32-23-10. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — SMOKE (COCKPIT) · airframe 14,370 hrs · 12,710 cycles

AFTER GPU CONNECTED ELECTRICAL SMOKE COMING FROM OVER HEAD PANEL, POST INSPECTION REVEALED ELECTRIC PUMP CIRCUIT BREAKER HAD BURNING ODOR. REMOVED AND REPLACED HYDRAULIC CONTROL PANEL IAW EMB AMM 20-13-10. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SWITCH — FAILED (ZONE 700) · airframe 14,198 hrs · 12,517 cycles

RECEIVED AIR TO GROUND WARNING MESSAGE AND GEAR FAILED TO RETRACT, RETURNED TO IND. REMOVED AND REPLACED NOSE LANDING GEAR WEIGHT ON WHEEL SWITCH IAW EMB AM 32-63-02 AND RIGHT MAIN LANDING GEAR NUMBER 2 PROXIMITY SWITCH IAW EMB AMM 32-63-01. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED · airframe 13,864 hrs · 12,152 cycles

LEFT FLOOR LIGHTS FLICKING WITH EMERGENCY LIGHTS IN ARM POSITION. PERFORMED ADJUSTMENT TEST IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT SERVICE.

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,140 hrs · 11,421 cycles

RIGHT HAT BEAM FOUND CORRODED AT FRAMES 22 AND 23. BLENEDED CORRODED AREA AND FILLED WITH EA934NA RESIN. FABRICATED AND INSTALLED DOUBLER IAW EMB IC2007-145/01376, DATED 02/26/07. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,140 hrs · 11,421 cycles

CENTER OMEGA BEAM FOUND CORRODED AT FRAME 25. PERFORMED CUT OUT TO REMOVE CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-01. RETURNED AIRCRAFT TO SERVICE.

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,140 hrs · 11,421 cycles

CENTER OMEGA BEAM FOUND CORRODED AT CENTER FUSELAGE III WING BOX AREA. PERFORMED CUT OUT OF CORROSION, FABRICATED REPAIR PARTS AND INSTALLED IAW EMB IC2007-145/1428, DATED 02-28-2007. RETURNED THE AIRCRAFT TO SERVICE.

Part: BEARING CAP — CORRODED (ZONE 700) · corrosion level 2 · airframe 13,140 hrs · 11,421 cycles

NOSE LANDING GEAR DRAG BRACE RIGHT LOWER BEARING CAP FOUND CORRODED. REMOVED AND REPLACED BEARING CAP IAW EMB AMM 32-20-02. PERFORMED RETRACTION/EXTENSION CHECK WITH NO DEFECTS, RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 13,140 hrs · 11,421 cycles

GALLEY FOWARD DIGITAL FOUND CORRODED. CUT OUT DAMAGE AREA, SPLICED IN REPAIR SECTION IAW EMB SRM 53-21-10. RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200505714) (K)

Part: SILL — CORRODED (FUSELAGE)

THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED LOWER DOOR SILL. INSTALLED SERVICEABLE SILL IAW SRM. (SW21200505714) (K)

Part: ENGINE — FIRE (NR 2)

ORD - FLT 4161 - NR 2 ENGINE FIRE REPORTED FROM RAMP. FLAMES SHOT OUT OF THE EXHAUST. NO INDICATION WAS PRESENT IN COCKPIT. CREW DISCHARGED BOTH FIRE BOTTLES. PERFORMED GENERAL VISUAL INSPECTION OF THE NR 2 ENGINE WITH NO DISCREPANCIES NOTED. PERFORMED GROUND RUN WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM)

MAINTENANCE REPORTED A DUAL PITCH TRIM FAIL ON LANDING AND TWICE ENROUTE PITCH TRIM 1 AND 2 INOPERATIVE. MESSAGE APPEARED FOR 5 SECONDS EACH TIME, THEN WENT OUT. REPLACED HSCU IAW MFG MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406973)

Part: ODOR — DETECTED (COCKPIT)

DURING CLIMB CREW REPORTED A BURNING ELECTRICAL ODOR. NO SMOKE WAS REPORTED. AN EMERGENCY WAS DECLARED AND FLIGHT LANDED WITH NO FURTHER INCIDENTS. THE ODOR DISSIPATED DURING DESCENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AN INSPECTION OF THE ELECTRICAL SYSTEM AND AN OPERATIONAL CHECK OF THE AVIONICS SYSTEM SHOWED NO DEFECTS. NO INDICATION OF SMOKE OR ODOR OF SMOKE WAS FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (GALLEY)

DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND TO BE CORRODED BELOW SRM LIMITS. BLENDED THE CORRODED AREA AND PERFORMED AN NDT INSPECTION AND FABRICATED AN INTERNAL DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT 1C2003-145/1485. (M)

Part: RAMP — CORRODED (GALLEY)

ABI - THIS IS A LEVEL 2 FINDING FOUND DURING AN IMBV NSPECTION GALLEY RAMP CORRODED AT FRAME 20. REMOVED AND INSTALLED NEW GALLEY RAMP IAW EMB 140 SRM 51-40-02, 51-20-07. (M)

Part: WINDSHIELD — FAILED (COCKPIT)

DFW - FLT 3813 - DURING CRUISE FLIGHT, THE FIRST OFFICERS WINDSHIELD SHATTERED. AIRCRAFT RETURNED TO DFW WITH NO FURTHER INCIDENT REPORTED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS WINDSHIELD IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)