N839AE

Part: CONTROL UNIT — MALFUNCTIONED (HSCU) · airframe 26,868 hrs · 23,681 cycles

AT 1200 FT "PTRIM MAIN INOP" ON EICAS PITCH WAS AT 2 UP SPEED AT 250 RTS IAS A/P OFF. PERFORMED AOM 1 PROCEDURE, DIVERTED. CMC MSG HSCU FAILURE C/W FIM TASK 27-43-00-810-801-A AND FOUND TRANSITORY CONDITION, R & R HSCU AS PRECAUTIONARY METHOD. OPS CK GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 26,776 hrs · 23,596 cycles

F/O FLASHLIGHT CLIP BROKEN. R & R F/O'S FLASHLIGHT HOLDER ASSY IAW AMM 33-50-16-000-801-A AND 33-50-16-400-801-A. OPS CHECK GOOD.

Part: FLASHLIGHT — OUT OF POSITION (CABIN) · airframe 25,263 hrs · 22,263 cycles

DURING MAINTENANCE INSPECTION FOUND THE FLIGHT ATTENDANT`S FORWARD FLASHLIGHT NOT CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND FORWARD FLASHLIGHT OUT OF POSITION, RE-SECURED IN THE PROPER CHARGING POSITION, CHARGING NORMAL IAW AMM 25-60-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 25,034 hrs · 22,025 cycles

ON FLIGHT 4348 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT DID NOT WORK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IN THE COCKPIT IAW EMB AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MOUNT — BROKEN (COCKPIT) · airframe 25,031 hrs · 22,023 cycles

ON FLIGHT 4016 THE CREW REPORTED THE FLASHLIGHT MOUNT IN COCKPIT BROKEN THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT IN COCKPIT IAW EMB 140 MM 25-60-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,009 hrs · 22,000 cycles

DURING B INSPECTION FOUND THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AND RIGHT LAMPS LIGHT IAW EMB AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. PART NUMBER 1317. NO FIX. REMOVED AND REPLACED THE EMERGENCY LIGHTING SYSTEM POWER SUPPLY AND BATTERY AT NR 4 POSITION IAW WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,878 hrs · 21,874 cycles

DURING PS-2 INSPECTION FOUND BOTH EXTERNAL OVERWING EMERGENCY EXIT LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY CHARGER AND BATTERY ASSEMBLY IAW MTX W/C # 33-700-19. THE OPERATIONAL CHECK WAS GOOD IAW MTX W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — LOOSE (EXTERIOR) · airframe 24,841 hrs · 21,841 cycles

DURING B INSPECTION FOUND THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY LOOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. TIGHTENED THE LEFT EXTERIOR OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-10-400-801-A. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,810 hrs · 21,815 cycles

DURING B INSPECTION FOUND THE LEFT AND RIGHT EXTERNAL OVERWING EMERGENCY LIGHTS FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER ASSEMBLY POWER SUPPLY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,601 hrs · 24,601 cycles

DURING MAINTENANCE CHECK FOUND THE EMERGENCY LIGHTS INOPERABLE. PLACED ON MEL 33-29. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW 33-50-07. THE OPERATIONAL CHECK WAS GOOD. MEL RESTORED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 24,597 hrs · 21,604 cycles

DURING PS-2 CHECK FOUND THE LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERABLE. ALSO FOUND THE RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHT INOPERABLE. LIGHT EMERGENCY LEFT PART NUMBER 30-2510-3. WHILE TROUBLESHOOTING, FOUND BLOWN FUSES ON NR 4 BATTERY CHARGER ASSEMBLY. REMOVED AND REPLACED THE NR 4 BATTERY AND POWER SUPPLY IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,560 hrs · 21,571 cycles

DURING B INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. PART NUMBER 1317. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER IAW WC 33-700-19.OPC IAW WC 33-700-17. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,517 hrs · 21,529 cycles

DURING B INSPECTION FOUND THE EXTERNAL OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT EXTERNAL AFT EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. PART NUMBER 1317. DID NOT FIX. REMOVED AND REPLACED THE NR 4 BATTERY ASSEMBLY AND CHARGER IAW WC 33-700-19. THE OPERATIONAL CHECK WAS NORMAL IAW WC 33-700-17. NO FURTHER DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 24,496 hrs · 21,510 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT EXTERIOR EMERGENCY LIGHTS ON THE LEFT AND RIGHT SIDES INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-LAMPED THE LEFT AND RIGHT EXTERIOR EMERGENCY AFT LIGHTS. PART NUMBER 1317. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND BATTERY POWER SUPPLY IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HINGE — LACK OF LUBE (CABIN DOOR) · airframe 24,167 hrs · 21,196 cycles

ON FLIGHT 3327 THE FLIGHT ATTENDANT REPORTED THE MAIN CABIN DOOR HANDLE WAS DIFFICULT TO OPERATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED INSPECTION AND LUBRICATED HINGES AND THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 23,939 hrs · 21,019 cycles

ON FLIGHT 2805 THE FLIGHT ATTENDANT REPORTED THE CABIN ENTRY DOOR WAS VERY HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED MAIN DOOR ROLLERS. THE OPERATIONAL CHECK WAS GOOD IAW EMB ETN EM 52-029. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 23,850 hrs · 20,955 cycles

DURING B INSPECTION, FOUND THE EMERGENCY FLOOR STRIP NR 4 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. RECONNECTED REMOVABLE SPLICE AT EMERGENCY FLOOR STRIP NR 4 IAW AMM 33-50-12. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (LAVATORY BEAM) · airframe 23,783 hrs · 20,909 cycles

DURING B INSPECTION, FOUND THE LAVATORY RIGHT BEAM GUSSET CORRODED FORWARD AND AFT ENDS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NEW SERVICEABLE LAVATORY RIGHT BEAM GUSSET IAW EMB SRM 51-40-02, 51-20-03,AND 51-40-06. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISINSTALLED (EMERGENCY LIGHT) · airframe 23,785 hrs · 20,910 cycles

DURING B INSPECTION, FOUND THE NR 1 FLOOR EMERGENCY LIGHT WOULD NOT WORK. AIRCRAFT REMOVED FROM SERVICE. DISCONNECTED AND RECONNECTED PROPERLY SP9019 AND SP9020 IAW SWPM 20-21-00. OPS CHECKED GOOD IAW AMM 33-50-00.

Part: FRAME — CRACKED (FUSELAGE) · airframe 23,783 hrs · 20,909 cycles

DURING B INSPECTION, FOUND FRAME 23 CRACKED BELOW STRINGER 15R. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE DAMAGED SECTION OF FRAME 23 IAW SRM 53-00-04 AND, 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 23,785 hrs · 20,910 cycles

DURING B INSPECTION, FOUND THE NR 4 CABIN FLOOR EMERGENCY LIGHT HAS BROKEN WIRES. AIRCRAFT REMOVED FROM SERVICE. INSTALLED SERVICEABLE NR 4 CABIN EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SHEAR TIE — CORRODED (CARGO DOORWAY) · airframe 23,779 hrs · 20,905 cycles

CARGO DOOR CUTOUT FWD LOWER CORNER FRAME 65 SHEAR TIE CORRODED. REPAIRED SHEAR TIE AT FR65 IAW EO EM-53MR-1129.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,771 hrs · 20,897 cycles

DURING B INSPECTION, FOUND THE RIGHT AND LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY PACK AND POWER SUPPLY IAW AE W/C 33-700-19. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,747 hrs · 20,875 cycles

DURING B INSPECTION, FOUND THE LEFT AND RIGHT AFT EXT EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 23,458 hrs · 20,638 cycles

ON FLIGHT 2866 THE CREW REPORTED THAT ON THE TAKEOFF ROLL AT ABOUT 80 KTS RECEIVED A MASTER WARNING TRIPLE CHIME "TRIM" MESSAGE. AT THAT TIME A ROLL TRIM BOX ON EICAS APPEARED. WHEN THE NUMBERS ON TRIM BLOCK RE-APPEARED THE TRIM WENT FROM 8 TO 6. TRIM SWITCH WAS NOT TOUCHED DURING TAKEOFF ROLL. LOW SPEED ABORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HORIZONTIAL STAB CONTROL UNIT IAW EMB 140 AMM 27-40-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 23,449 hrs · 20,628 cycles

ON FLIGHT 2709 THE CREW REPORTED THE FLIGHT ATTENDANT’S FLASHLIGHT WAS MISSING. DEFERRED PER MEL 25-53 AUTH #060497-C SPARE PROVIDED ENTER ON MIC. REPLACED FLASHLIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-16 MEL RESTORED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 23,396 hrs · 20,588 cycles

DURING B INSPECTION, FOUND THE EMERGENCY CEILING LIGHT AT ROW 6 IS INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LAMP IN EMERGENCY CEILING LIGHT ROW 6 PER EMB 140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD PER EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 23,133 hrs · 20,349 cycles

DURING B-INSPECTION FOUND THE FIRST OFFICER’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRST OFFICER’S FLASHLIGHT BULB & BATTERY PACK IAW EMB AMM 33-51-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,033 hrs · 20,245 cycles

DURING MAINTENANCE INSPECTION FOUND THE CABIN EMERGENCY CEILING LAMP ROW 6 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED LAMP EMERGENCY CABIN CEILING LAMP ROW 6 IAW STANDARD AIRCRAFT MAINTENANCE PRACTICE TEST IAW EMB AMM 33-50-00 TEST OK. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,746 hrs · 19,967 cycles

DURING B INSPECTION FOUND EMERGENCY LIGHT AT MAIN DOOR CEILING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BULB CEILING MAIN ENTRANCE EMERGENCY LIGHT IAW EMB AMM 33-50-00 OPERATIONAL CHECKS GOOD. THE AIRCRAFT RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,598 hrs · 19,844 cycles

DURING B-INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF THE EMERGENCY LIGHTS AND THE CHECK WAS GOOD IAW EMB AMM 33-50-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 21,453 hrs · 18,880 cycles

FOR FLIGHT 3318 DURING FIRE TEST THE BAGGAGE SMOKE EXTINGUISHER BUTTON DID NOT ILLUMINATE NOR PRESENT ON EICAS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD BAGGAGE SMOKE DETECTOR IAW AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,912 hrs · 16,756 cycles

ON FLIGHT 4287 DURING THE INSPECTION FOUND THE EMERGENCY FLOOR LIGHTING PROXIMITY STRIP AT 7 AND 8 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR LIGHT EMERGENCY STRIP AT ROW 8A IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 18,881 hrs · 16,727 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT FRAME 23 CRACKED IN 2 LOCATIONS BETWEEN STRINGERS 15 RIGHT AND 14 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CRACK LENGTHS ARE .25 AND .75 INCH. REPAIRED FRAME 23R IAW EO EM-53MR-1634. THE ACFT WAS RETURNED TO SERVICE.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 18,881 hrs · 16,727 cycles

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

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,881 hrs · 16,727 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CENTER OMEGA BEAM CORRODED NEAR FRAME 27 CROSS MEMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED OMEGA BEAM IAW EO EM-53MR-1632. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (ZONE 200) · airframe 15,368 hrs · 12,571 cycles

ON FLIGHT 4663 ON TAKE OFF CREW RECEIVED A BRAKE DEGRADE ON EICAS. CREW ABORTED TAKEOFF AND RETURNED TO BLOCK. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT IAW FIM TASK 32-41-00-810-805A. REMOVED AND REPLACED ACU IAW AMM 32-41-02. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE)

DURING MBV INSPECTION THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED DAMAGED SILL, TREATED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (A)

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 14,008 hrs · 11,416 cycles

ON FLIGHT 3882, DURING TAKEOFF CREW REPORTED THERE WAS A VERY PRONOUNCED EXCESSIVE VIBRATION DURING TAKEOFF ROLL AND DURING GEAR RETRACTION FROM NOSE GEAR. DURING TAKEOFF DEADHEAD EMJ CAPTAIN REPORTED 3 LOUD BANGS SIMILAR TO A COMPRESSOR STALL ON TAKEOFF. MOMENTARY LOSS OF NR 2 ENGINE INDICATIONS N1 N2 AND ITT INDICATED DASHED LINES ON LIFTOFF WITH APU RUNNING RELAYS BEHIND F/O SEAT KEPT CLICKING AND CABIN LIGHTS FLICKERED.

Part: CONTROL UNIT — MALFUNCTIONED (PITCH TRIM) · airframe 13,370 hrs · 10,928 cycles

ON FLIGHT 4393, CREW REPORTED AFTER TAKEOFF THAT MAIN PITCH TRIM INOP EICAS MESSAGE APPEARED ON EICAS. EMERGENCY WAS DECLARED AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HSCU PER EMB AMM 27-40-01 AND NR 8194; AIRCRAFT RETURNED TO SERVICE AND NR 8194; AND NR 8194; AND NR 8194; AND 8194.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 11,883 hrs · 9,793 cycles

ESCAPE PATH LIGHTING AT EXIT ROW WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: INVERTER — FAILED (ZONE 200) · airframe 11,784 hrs · 9,713 cycles

FOWARD OVERHEAD EXIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED INVERTER IAW EMB AMM. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,414 hrs · 9,417 cycles

ROWS 3 THROUGH 6 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FLOOR PROXIMITY STRIP AT ROW 5 AND 6 IAW EMB AMM 33-50-12. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: ODOR — DETECTED (CABIN)

AIRCRAFT RETURNED TO IND WITH LOSS OF PRESSURIZATION AND A BURNING ODOR. REPLACED COUPLER AND SEAL AT LEFT BLEED CUT JOINT NR 9 AND NR 11, IAW EMB 140, MM 36-11-09. NO DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND FORWARD CENTER OMEGA BEAM BETWEEN FRAMES 10-23 TOP SURFACE HAS CORROSION. REPAIRED GUSSET IAW IC 2006-145/6423 AND SRM 51-40-02 BY CUTTING OUT DAMAGE AND SPLICING IN A NEW PIECE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM BETWEEN FRAMES 18-20 CORRODED. RAI OMEGA BEAM IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND FLOOR SUPPORT RAMP CORRODED BETWEEN FRAMES 19-20. RAI RAMP IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND LEFT FORWARD SEAT TRACK CORRODED. RAI SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND CENTER HAT BEAM SECTION BETWEEN FRAMES 19-20 CORRODED OUT OF LIMITS. REPAIRED HAT BEAM BY INSTALLING AND EXTERNAL DOUBLER IAW I/C 2006-145/6494 AND SRM 53-21-10. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND FLOOR SUPPORT BETWEEN SERVICE DOOR AFT SILL AND CENTER OMEGA BEAM CORRODED. RAI PROFILE IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,948 hrs · 4,455 cycles

DURING MBV INSPECTION THE CENTER OMEGA BEAM BETWEEN FRAMES 23 AND 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, SHIMS AND FILLER. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 4,948 hrs · 4,455 cycles

DURING A MBV INSPECTION THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED A CUTOUT OF DAMAGED AREA. FABRICATED EXTERNAL ANGLE, FILLER, SHIMS. REPAIR DONE IAW SRM. (K)

Part: FCU — INOPERATIVE (AVIONIC BAY)

DURING APPROACH, TEH CREW REPORTED THE FLAPS BECAME STUCK IN THE DOWN POSITION. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS LANDED IN CMH WITH NO FURTHER PROBLEMS NOTED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)