N829AE

Part: FLASHLIGHT ASSY — UNSERVICEABLE (CABIN) · airframe 27,347 hrs · 24,835 cycles

CABIN FLASHLIGHT BEHIND 16B IS LOOSE IN CRADLE AND IS NOT SECURE ENOUGH TO CHARGE. R & R CABIN FLASHLIGHT BEHIND SEAT 16B IAW AMM 33-50-16-4. OPS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,315 hrs · 24,803 cycles

RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-10, OPS CHECKED GOOD.

Part: ROLLER — BINDING (PAX DOOR) · airframe 27,018 hrs · 24,485 cycles

F/A REPORTS MAIN CABIN DOOR HARD TO OPEN. SERVICED MAIN DOOR ROLLERS IAW AMM 53-21-02, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,748 hrs · 24,265 cycles

SOME EMERGENCY LIGHTS FOUND ON BY GROUND PERSONNEL. PERFORMED CHARGING OF EMERGENCY LIGHT BATTERIES IAW CMM 25-60-03. PERFORMED EMERGENCY OPS CHECKED IAW AMM 33-50-00. OPS CHECKED FAILED.

Part: FLASHLIGHT — DEFECTIVE (COCKPIT) · airframe 26,458 hrs · 24,026 cycles

THE CAPTAIN’S FLASHLIGHT WAS NOT ACCEPTING A CHARGE. THE ACFT WAS REMOVED FROM SERVICE. R & R FLASHLIGHT IAW AMM 25-60-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 26,309 hrs · 23,813 cycles

DURING MX INSPECTION, FOUND A FEW AFT FLOOR EMERGENCY LIGHTS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR4 BATTERY POWER SUPPLY IAW-AMM-33-50-04. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,054 hrs · 23,505 cycles

DURING B INSPECTION FOUND THE AFT AISLE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT AISLE EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,054 hrs · 23,505 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT ABOVE SEAT 11C INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP AT SEAT 11C IAW EMB 140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,000 hrs · 23,457 cycles

DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S COCKPIT FLASHLIGHT IAW EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACM — DAMAGED (AC BAY) · airframe 25,848 hrs · 23,311 cycles

ON FLIGHT 4007 THE CREW REPORTED THEY NOTICED AN ELECTRICAL SMOKE SMELL WHEN NR 1 PACK WAS SELECTED. PACK 1 DEFFERED PER MEL 21-29 AUTH # 030322D-C. FOUND AIR CYCLE MACHINE BLADES TO BE DAMAGED. REMOVED AND REPLACED THE IAW AMM 21-51-03. OPS CHECK GOOD. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: VALVE — INOPERATIVE (AC BAY) · airframe 25,850 hrs · 23,313 cycles

ON FLIGHT 4371 THE CREW REPORTED THAT DURING TEST OF RECIRC FAN PER MEL 21-29, THEY HEARD A LOUD GRINDING NOISE AND EXPERIENCED SMELL OF HEAVY SMOKE/ FUMES. THIS OCCURED WITH APU BLEED OPEN, X BLEED OPEN AND BOTH PACKS SELECTED OFF. OPERATED APU, NR 2 PACK AND RECIRC FAN. NO GRINDING SOUNDS OR ODOR FOUND. SUSPECT POSSIBLE INADVERTANT USE OF DEFERRED NR 1 PACK REF EMB 140 AMM 21-60-00. REMOVED AND REPLACED NR 2 PACK VALVE AND THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 21-51-01. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 25,826 hrs · 23,284 cycles

FLIGHT 3512. CREW REPORTED RIGHT AFTER APPLYING TAKEOFF POWER RECEIVED NR 1 PACK OVERLOAD FOR ONE SECOND, THEN WENT AWAY. AFTER CLIMBIMG THROUGH APPROX 500FT, DETECTED A FAINT ELECTRICAL BURNING ODOR, RECEIVED NR 1 PACK CLOSED MESSAGE. TURNED OFF NR 1 PACK AND ODOR WENT AWAY. DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. PERFORMED ENGINE RUNS AFTER RECIRCULATION FANS & GASPER FAN INSPECTION, NR 1 ACM AND NR 1 HEAT EXCHANGER REPLACED. STILL RECEIVED AN ELECTRICAL BURN ODOR ON FIRST POWER RUN FOR NR 1 ENGINE WITH NR 1 PACK ON, BLEED NR 1 ON, AND CROSSBLEED VALVE AUTO WITH BOTH ENGINE RUNNING. PERFORMED NR 1 HEAT EXCHANGER OPS CHECKED & LEAK CHECKED GOOD IAW AMM 21-51-02. PERFORMED NR 1 ACM OPS & LEAK CHECKED FOUND GOOD IAW AMM 21-51-00. R & R LT ENGINE CARBON SEAL IAW MM 72-25-25. R & R RT ENGINE CARBON SEAL IAW MM 72-25-25. PASSED FUNCTIONAL CHECK FLIGHT. FLEW AT 3000-10000 FT, NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 25,467 hrs · 22,935 cycles

DURING MAINTENANCE INSPECTION FOUND THE PANEL 251BF EMERGENCY LIGHT STRIP WIRES BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PANEL 251BF EMERGENCY LIGHT STRIP IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,895 hrs · 22,342 cycles

ON FLIGHT 3058 THE CREW REPORTED THE CAPTAIN FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN FLASHLIGHT ASSEMBLY IAW EMB 140 MM 33-50-16 AND PERFORMED OPERATIONAL CHECK IAW EMB 140 MM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BRACKET — BROKEN (COCKPIT) · airframe 24,321 hrs · 21,674 cycles

DURING MAINTENANCE INSPECTION FOUND THE COPILOT CONSOLE EMERGENCY FLASHLIGHT BRACKET BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COPILOT CONSOLE EMERGENCY FLASHLIGHT BRACKET IAW EMB 140 AMM 33-50-16. THE FLASHLIGHT OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,889 hrs · 21,167 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY NR 2 WILL NOT HOLD A CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY POWER SUPPLY NR 2 AND CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 23,898 hrs · 21,179 cycles

DURING B-INSPECTION FOUND THE CABIN EMERGENCY LIGHT STRIP CONNECTOR BROKEN OFF AT CABIN FLOOR PANEL 251GF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE CABIN EMERGENCY LIGHT STRIP AT CABIN FLOOR PANEL 251GF IAW EMB 140 WM 20-21-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — WRONG PART (CABIN) · airframe 23,898 hrs · 21,179 cycles

DURING B-INSPECTION FOUND THE GALLEY AREA FLOOR PROXIMITY EMERGENCY LIGHT STRIP WAS THE WRONG PART NUMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE GALLEY AREA PROXIMITY EMERGENCY LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: STRINGER — GOUGED (FUSELAGE) · airframe 23,888 hrs · 21,166 cycles

DURING MAINTENANCE INSPECTION FOUND THE STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 IAW AEA EO EM-52MR-1434. THE AIRCRAFT WAS RETURNED TO SERVCE.

Part: HOLDER — BROKEN (CABIN) · airframe 23,898 hrs · 21,179 cycles

DURING B-INSPECTION FOUND THE NR 6 AND NR 2 PROXIMITY LIGHT HOLDER BROKEN. THE NR 6 PROX LIGHT HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 AND NR 2 PROX LIGHT HOLDER IAW EMB 140 AMM 33-50-12, AND REMOVED AND REPLACED THE NR 6 PROX LIGHT IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,641 hrs · 20,978 cycles

DURING B-INSPECTION FOUND THE OVERWING EMERGENCY-LIGHT AT 11A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY OVERHEAD LIGHT BULB AT 11A IAW EMB-140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM PANEL — DAMAGED (MAIN DOOR) · airframe 23,273 hrs · 23,273 cycles

ON FLIGHT 4258 THE CREW REPORTED THE MAIN CABIN DOOR DOES NOT OPEN FULLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MAIN DOOR HINGE COVER TRIM DAMAGED. REMOVED DAMAGED PORTION OF TRIM. DOOR OPENS AND CHECK GOOD. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,396 hrs · 19,928 cycles

EMERGENCY EXIT SIGN INOP AT COCKPIT STEP. REMOVED AND REPLACED NR 1 DC/AC INVERTER IAW EMB 140 AMM 33-50-11. OPC GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,396 hrs · 19,928 cycles

EMERGENCY EXIT SIGN INOP AT COCKPIT STEP. REMOVED AND REPLACED NR 1 DC/AC INVERTER IAW EMB 140 AMM 33-50-11. OPC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,323 hrs · 15,608 cycles

DURING MAINTANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT IAW EMB AMM TASK 33-50-07-000-801-A AND 33-50-07-400-801-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ILS SYSTEM — ERRATIC (COCKPIT) · airframe 20,243 hrs · 18,077 cycles

ON FLIGHT 2930 THE CREW REPORTED VIA TELEPHONE UPON APPROACH TO SHV BOTH INSTRUMENT LANDING SYSTEMS AND LOCALIZER INDICATIONS WERE ERRATIC AND UNRELIABLE. THE CREW ABORTED THE APPROACH AND STARTED A SECOND APPROACH BUT THE WEATHER MINIMUMS WERE TOO LOW AND THE CREW ELECTED TO DIVERT TO GGG. THE AIRCRAFT HAD A VERY HIGH FREQUENCY OMNI DIRECTIONAL RANGE LANDING. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COULD NOT DUPLICATE PROBLEM. A GENERAL VISUAL INSPECTION OF BOTH INSTRUMENT LANDING SYSTEM ANTENNAS WAS DONE AND NO DEFECT NOTED. THE OPERATIONAL CHECKS WERE GOOD IAW AMM 34-32-00 USING NAV-402 TEST BOX S/N 1159. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,909 hrs · 17,806 cycles

DURING MAINTENANCE BASE PS-2 INSPECTION FOUND THE RIGHT WING TO FUESLAGE FARING AFT EMERGENCY LIGHT BULB OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 19,084 hrs · 17,187 cycles

DURING MAINTENANCE BASE VISIT FOUND DAMAGE TO FRAME 27 AND STRINGER 15L. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGE AND FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAE EO EM-53MR-155. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,084 hrs · 17,187 cycles

DURING MAINTENANCE BASE VISIT FOUND THE FORWARD DIGITAL "WEB" TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DAMAGE, FABRICATED AND INSTALLED SPLICE SECTION AND DOUBLER IAW ETA EM-5300-1222. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,084 hrs · 17,187 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EMB SRM 53-00-10 FIG 201 SHEET 2. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,084 hrs · 17,187 cycles

DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EMB SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 19,084 hrs · 17,187 cycles

DURING MAINTENANCE BASE VISIT FOUND THE AFT EMERGENCY LIGHT STRIP CONNECTOR TO BE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CONNECTOR IAW EMB 140 SWPM 20-50-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,084 hrs · 17,187 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT BEAM GUSSET AT FRAME 22 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORRODED GUSSET AND INSTALLED NEW GUSSET IAW EMB SRM 51-40-02, SRM 51-20-03, SRM 51-40-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRIORITY VALVE — FAILED (LANDING GEAR) · airframe 18,904 hrs · 17,037 cycles

ON FLIGHT 3469 ON TAKEOFF THE CREW REPORTED THAT AFTER GEAR RETRACTION IT SOUNDED LIKE NOSE GEAR DOORS WERE OPENED FOLLOWED BY LANDING GEAR AIR/GROUND FAIL MESSAGE, FOLLOWED BY VARIOUS FAILURES ON EICAS. THE CREW ELECTED TO RETURN TO FIELD AND LANDED WITHOUT INCIDENT. THE CREW RAN A CHECK LIST AFTER LANDING AND GOT IC 12 THEN GOT STICK SHAKER WHILE TAXIING IN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LANDING GEAR PRIORITY VALVE IAW AMM 32-33-02 AND REMOVED AND REPLACED LEGU IAW AMM 32-32-01. GEAR SWINGS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 18,838 hrs · 16,983 cycles

ON FLIGHT 3500 DURING THE APPROACH THE CREW REPORTED THAT WITH THE LANDING GEAR DOWN INDICATIONS SHOWED 3 GREEN. RECEIVED A CONTINUOUS TRIPLE CHIME. THE CREW ELECTED TO FLY BY THE TOWER. THE CHIME LASTED 5-10 SECONDS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH CENTRAL MAINTENANCE COMPUTER DOWNLOAD WITH MULTI FUNCTION DISPLAY AND NO FAULTS WERE RECORDED AT THIS TIME, AND NO FURTHER ACTION REQUIRED IAW 45-45-00-970-801-A. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SELECTOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 18,127 hrs · 16,376 cycles

ON FLIGHT 4400 DURING THE CLIMBOUT THE CREW REPORTED, LOST FUEL QUANTITY INDICATIONS FOR TANK 2 AND RECEIVED A FUEL IMBALANCE MESSAGE ON EICAS. THE CREW ALSO RECEIVED ANOTHER MESSAGE ON EICAS WARNING FOR FUEL LOW FOR TANK 1. THE CREW DECLARED AN EMERGENCY AND RETURNED TO RDU. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FUEL QUANTITY INDICATOR SELECTOR IAW EMB140 AMM 28-23-08. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 17,381 hrs · 15,757 cycles

ON FLIGHT 4620 THE CREW DECLARED AN EMERGENCY INTO BOS DUE TO A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT LANDED SAFELY WITH NO INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS IAW EMB AMM 32-00-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,412 hrs · 12,703 cycles

DURING A MBV INSPECTION, FOUND CARGO DOOR SLLL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL, DRILLED AND ALODINED NEW PART. INSTALLED NEW SLLL IAW EMB SRM (SRM145/1142 REV. 39) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: DAU — MALFUNCTIONED (NR 1) · airframe 13,700 hrs · 12,145 cycles

ON FLIGHT 4548 CREW REPORTED AT GEAR EXTENSION. EICAS BREAK OUTBOARD INOP. CREW DECLARED AN EMERGENCY MESSAGE REMOVED AFTER LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 DAU IAW EMB 140 AMM 32-41-02. CHECKS GOOD, NO DEFECTS NOTED. PERFORMED LANDING EXTENSION AND RETRACTION , AMM 32-34-00. NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 13,001 hrs · 11,595 cycles

CREW ELECTED TO RETURN INTO CLT DUE TO RUDDER SYS 1/2 INOPERATIVE MESSAGE ON EICAS FOLLOWED BY AUTO PILOT AND YAW DAMPER FAIL ON EICAS AIRCRAFT RETURNED TO CLT WITH NO FURTHER INCIDENT DISC-YAW DAMPER AND AUTO PILOT FAIL IN FLIGHT, RUDDER SYSTEM 1 INOP INTERMITTENT, RUD SYS 2 INOP INTERMITTENT. REMOVED AND REPLACED RUDDER PRESSURE SWITCH FOR SYS 1 AND 2. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PROBE — MALFUNCTIONED (AOA) · airframe 12,993 hrs · 11,589 cycles

CREW REPORTED ON TAKE OFF ROLL AT APPROX 10 KIAS, "SPS ADVANCE" MESSAGE ILLUMINATED ON EICAS. CREW ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. AIRCRAFT RETURNED TO THE GATE SAFELY FOR MAINTENANCE. REMOVED AND REPLACED NUMBER 2 AOA IAW EMB140 MM 27-36-01. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: RELAY — BURNED (ELECTRICAL) · airframe 10,654 hrs · 9,926 cycles

STRONG ELECTRICAL FUMES, FUMES DISSAPATED AFTER FAN TURNED OFF. C/A - FOUND RELAY K0054 SOCKET BLOWN, K0454 AND K0035 DAMAGED. REMOVED AND REPLACED RELAYS. OPERATIONAL CHECKED GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 10,421 hrs · 9,732 cycles

AT 80 KNOTS RECEIVED RUDDER SYSTEM 1 INOP MESSAGE, ABORTED TAKEOFF. RUDDER SYSTEM 2 INOP MESSAGE. AOM CHECKLIST FOLLOWED AND BOTH SYSTEMS RESET. ACCOMPLISHED EMB FIM TASK 27-22-00-810-804-A WITH NO DEFECTS NOTED. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT BACK TO SERVICE.