N801AE

Part: CLAMP — LOOSE (LT ENGINE) · airframe 34,258 hrs · 30,083 cycles

NR 1 ENG POWER FLUCTUATED N1,N2 AND ITT RISE ASSOCIATED WITH POWER CHANGES. MOST NOTICABLE AT MD RANGE POWER SETTINGS. FOUND BOTH LH ENG CHECK VALVE CLAMPS LOOSE. INSTALLED NEW GASKETS AND RETORQUED CLAMPS IAW AMM 36-11-01. PERFORMED HIGH POWER RUN IAW RR MM 72-00-00. OPS CHECK GOOD.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 34,028 hrs · 29,842 cycles

COCKPIT STEP AND GALLEY AISLE CEILING PANEL EMERGENCY EXIT IDENTIFIER SIGNS INOP. C/A-REMOVED AND REPLACED #1 EMERGENCY LIGHT DC/AC INVERTER IAW AMM 33-50-11. OPC GOOD.

Part: DOOR SILL — CORRODED (AFT SERVICE DOOR) · airframe 31,738 hrs · 27,577 cycles

CORROSION ON THE SERVICE DOOR SILL. INSTALLED THREE DOUBLER REPAIRS IAW SRM 53-21-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

FRAME 66 IS CRACKED AT THE END AT CARGO DOOR SILL AREA. REPAIRED FRAME 66 IAW ERS-EM-53MR-3300.

Part: WIRE — BROKEN (EXTERIOR LIGHT) · airframe 31,732 hrs · 27,571 cycles

WIRES FOR THE RT EMERGENCY LIGHT ON FWD BELLY PANEL ARE BROKEN. REPAIRED WIRES FOR THE RT EMERGENCY LIGHT ON FWD BELLY PANEL IAW SWPM 20-21-00.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

53-20-11 LEFT OMEGA BEAM IS CORRODED AT CROSSBEAM BTW FR 58-59. REPAIRED LEFT OMEGA BEAM BTW FR 57-59 IAW EO-EM-53MR-1518 REV 3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

53-20-11 CENTER OMEGA BEAM IS CORRODED AT CROSSBEAM BTW FR 58-59. REPAIRED CENTER OMEGA BEAM AT FR 59 IAW EO-EM-53MR-1518 REV 3.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

CARGO DOOR LOWER SILL IS CORRODED. REMOVED AND REPLACED CARGO DOOR SILL IAW SRM 51-40-02.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

FR-10 CRACKED BELOW LT DV WINDOW. REMOVED AND REPLACED LT FRAME 10 IAW SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

FRAME 65 CARGO LATERAL L-SHAPE CORRODED AT LOWER END. REPAIRED FRAME 65 CARGO LATERAL L-SHAPE IAW SRM 53-31-04 ITEM 4.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

FR-10 CRACKED BELOW RT DV WINDOW. REMOVED AND REPLACED RT FRAME 10 IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

LT OMEGA BEAM IS CORRODED AT CROSSBEAM FR-38. REPAIRED LT OMEGA BEAM CORROSION AT FRAME 38 IAW SRM 53-00-10, FIGURE 202, SHEET 1.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

CENTER OMEGA BEAM IS CORRODED AT CROSSBEAM FR-38. REPAIRED LT OMEGA BEAM CORROSION AT FRAME 38 IAW SRM 53-00-10, FIGURE 203, SHEET 1.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 31,732 hrs · 27,571 cycles

RT OMEGA BEAM INBOARD SUPPORT IS CRACKED BETWEEN FRAMES 47-48. REMOVED AND INSTALLED NEW REPLACEMENT RT OMEGA BEAM INBOARD SUPPORT PARTS IAW SRM 53-23-02.

Part: SEAT TRACK — CORRODED (FRAME 50) · airframe 31,732 hrs · 27,571 cycles

CORROSION FOUND ON THE RT OTBD SEAT TRACK SUPPORT AT FRAME 50. R & R THE SEAT TRACK SUPPORT IAW SRM 51-40-02.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,732 hrs · 27,571 cycles

EMERGENCY LIGHT STRIP NR 5 HAD A BROKEN WIRE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,732 hrs · 27,571 cycles

LEFT CABIN FLOOR EMERGENCY LIGHT STRIP NR 3 WIRES WERE BROKEN. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP IAW AMM 33-50-12.

Part: FITTING — DAMAGED (RT AILERON) · airframe 31,732 hrs · 27,571 cycles

RIGHT AILERON DAMPER FITTING DAMAGED. REMOVED AND REPLACED THE FITTING IAW EO EM-27MR-112.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 31,298 hrs · 27,198 cycles

COPILOTS FLASHLIGHT INOPERATIVE. R & R COPILOTS FLASHLIGHT IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,844 hrs · 26,685 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R & R MAIN DOOR EMERGENCY LIGHT LAMP IAW AMM 33-50-06, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 30,235 hrs · 26,109 cycles

AFT CABIN EMERGENCY FLASHLIGHT ASSEMBLY. R & R AFT CABIN EMERGENCY FLASHLIGHT ASSEMBLY IAW AMM 33-50-16-000-801-A & 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 29,718 hrs · 25,663 cycles

NR 2 EMERGENCY LIGHT BATTERY INOPERATIVE. R & R NR 2 EMERGENCY LIGHT BATTERY IAW W/C 33-700-19. OPS CHECKED GOOD.

Part: CRADLE — BROKEN (FLASHLIGHT) · airframe 29,002 hrs · 25,079 cycles

DURING MX INSPECTION, FOUND THE F/O RECHARGEABLE FLASHLIGHT CRADLE BROKEN. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT CRADLE IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: DOOR — BINDING (MAIN CABIN) · airframe 28,906 hrs · 24,995 cycles

THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED THE MAIN CABIN DOOR FRAME ROLLERS IAW AMM 53-21-02. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 28,514 hrs · 24,673 cycles

DURING B INSPECTION FOUND THE AFT CABIN EMERGENCY FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT IN REFERENCE WITH EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 27,837 hrs · 24,090 cycles

DURING B INSPECTION FOUND THE EMERGENCY LIGHT ON SERVICE DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CONNECTOR ON WIRE W716-0007-20 IAW EMB-140 SWPM 20-50-01. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 27,516 hrs · 23,842 cycles

NOTED SMOKE COMING FROM CAPTAINS WINDSHIELD HEAT ELEMENT IN FLT, TURNED OFF WINDSHIELD HEAT SMOKE DISSIPATED. FOUND CAPTAINS WINDSHIELD POWER CABLE BURNED AT TERMINAL BLOCK OF WINDSHIELD. CAPTAINS WINDSHIELD REPLACED. REMOVED AND REPLACED THE CAPTAIN WINDSHIELD TEMP CONTROLLER IAW EMB 140 AMM 30-42-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,388 hrs · 23,736 cycles

DURING B INSPECTION FOUND THE SERVICE DOOR CUTOUT LOWER CENTER SILL CORRDED AROUND THE NUT PLATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SERVICE DOOR CENTER SILL AROUND THE NUT PLATE IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 23,736 hrs · 23,736 cycles

DURING B INSPECTION FOUND THE NR 4 EMERGENCY LIGHT STRIP ELECTRICAL CONNECTORS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT STRIP IAW EMB-140 AMM 33-50-12 NR 4 EMERGENCY LIGHT STRIP IAW EMB-140 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,388 hrs · 23,736 cycles

RT OMEGA BEAM IN LAV CORRODED AT NUTPLATE HOLE. REPAIRED RT OMEGA BEAM IN LAV CORROSION AT NUTPLATE HOLE IAW EO EM-53MR-2038, PT. A.

Part: SILL — CORRODED (FUSELAGE) · airframe 27,388 hrs · 23,736 cycles

DURING B INSPECTION FOUND THE CARGO DOOR CUTOUT CENTER SILL CORRDED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR CUTOUT CENTER SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,363 hrs · 23,716 cycles

FRAME 23 CRACKED AT ABOVE STRINGER 15R. REPAIR ACCOMPLISHED IAW EO EM-53MR-1808.

Part: CONNECTOR — BROKEN (CABIN) · airframe 27,388 hrs · 23,736 cycles

DURING B INSPECTION FOUND THE NR 1 EMERGENCY LIGHT STRIP ELECTRICAL CONNECTORS BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT STRIP IAW EMB-140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 27,155 hrs · 23,535 cycles

ON FLIGHT 2898 THE CREW REPORTED THEY RECEIVED A FLAPS FAIL CAUTION MESSAGE ON EICAS. THE ABNORMAL/NORMAL CHECK LISTS WERE COMPLETED. AN EMERGENCY WAS DECLARED WITH A REQUEST FOR CRASH, FIRE AND RESCUE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE FECU IAW EMB 140 AMM 27-53-02. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM 27-53-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 26,827 hrs · 23,218 cycles

DURING MAINTENANCE INSPECTION, FOUND AFT CEILING EMERGENCY LIGHT INOPERATIVEE. THE AIRCRAFT WAS REMOVE FROM SERVICE. REMOVED AND REPLACED LIGHT BULB AT CEILING EMERGENCY LIGHT IAW AMM 33-50-08-000-801-A AND 33-50-08-400-801-A. THE AIRCRAFT RETURN TO SERVICE.

Part: FLASHLIGHT ASSY — FAILED (FWD CABIN) · airframe 26,746 hrs · 23,141 cycles

FLIGHT 4254, CREW REPORTED AN ELECTRICAL ODOR COMING FROM THE FRONT OF THE ACFT. DECLARED AN EMERGENCY AND LANDED. AIRCRAFT REMOVED FROM SERVICE. INSPECTED AND FOUND FLIGHT ATTENDANTS FLASHLIGHT AND CRADLE HAD ODOR CONSISTENT WITH ELECTRICAL ODOR. CAPTAIN VERIFIED ODOR. REMOVED AND REPLACED FWD CABIN FLASHLIGHT AND CHARGER ASSY IAW AMM 33-50-16. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,718 hrs · 23,112 cycles

DURING B INSPECTION, FOUND THE RIGHT AFT FUSELAGE EXTERIOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT EXTERIOR FUSELAGE EMERGENCY LIGHT LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (SPOILER) · airframe 26,468 hrs · 22,876 cycles

ON FLIGHT 4701 THE CREW REPORTED THAT WHILE ON DESCENT RECEIVED A SPOILER FAIL CAUTION MESSAGE ON EICAS, ALONG WITH A GREEN SPOILER OPEN INSCRIPTION ON EICAS, IN FLIGHT. THE CAUTION MESSAGE DISAPPEARED AND OPEN INSCRIPTION ON EICAS IN FLIGHT. CAUTION MESSAGE DISAPPEARED AND OPEN INSCRIPTION CHANGED BACK TO CLOSED WHEN DAU 1 EICAS REV BUTTON WAS PRESSED DUE TO ITEM 2. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SPOILER CONTROL UNIT IAW EMB 140 AMM 27-63-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CUSHION — MISSING (BATTERY PACK) · airframe 26,005 hrs · 22,436 cycles

DURING B-INSPECTION FOUND THE NR 1 EMERGENCY POWER SUPPLY BATTERY HAS MISSING SHOCK ABSORBING CUSHION PAD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED NR 1 EMERGENCY LIGHTING BATTERY IAW W/C 33-700-19. THE OPERATIONAL CHECK OF EMERGENCY LIGHTS WAS GOOD IAW W/C 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,921 hrs · 22,355 cycles

DURING B-INSPECTION FOUND THE RIGHT WING UPPER EMERGENCY LIGHT BULB INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT BULB IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SREVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,860 hrs · 22,297 cycles

DURING MAINTENANCE INSPECTION FOUND THE RIGHT SIDE CENTER FAIRING LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT CENTER FAIRING EXTERNAL EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,691 hrs · 22,178 cycles

DURING MAINTENANCE INSPECTION FOUND EMERGENCY AISLE LIGHT ABOVE LT EMERGENCY EXIT DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LIGHT BULB ON EMERGENCY AISLE LIGHT ABOVE LT EXIT DOOR IAW EMB140 AMM 33-50-08 OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,163 hrs · 21,801 cycles

RT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT LAMP IAW EMB 140 AMM 33-50-01. OPC GOOD.

Part: SMOKE DETECTOR — DEFECTIVE (CABIN) · airframe 25,113 hrs · 21,766 cycles

ON FLIGHT 3222 THE FLIGHT ATTENDANT REPORTED THE GALLEY FIRE DETECTION HAD NO GREEN LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR IAW EMB 140 MM 26-14-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 25,083 hrs · 21,744 cycles

ON FLIGHT 2717 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR FRAME ROLLERS IAW AMM 53-21-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,023 hrs · 21,699 cycles

DURING MAINTENANCE BASE VISIT FOUND ROW 16 CEILING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED ROW 16 CEILING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-08. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 24,983 hrs · 21,670 cycles

ON FLIGHT 2744 THE CREW REPORTED SMOKE EMINATING FROM THE TOP AFT EDGE OF THE LEFT ENGINE, UP UNTIL AT LEAST 15 MINUTES AFTER SHUTDOWN. THE CREW NOTED IT SEEMED LIKE OIL OR HYDRAULIC FLUID SMOKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT ENGINE IAW WC 71-000-00. THE OPERATIONAL AND LEAK CHECK WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT OVER THE RIGHT WING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT BULB OVER THE RIGHT WING IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,749 hrs · 21,465 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AFT EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EXTERNAL OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,472,754 hrs · 21,453 cycles

DURING MAINTENANCE BASE VIST FOUND THE MAIN PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCARFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10 AND EMB 140 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,727 hrs · 21,453 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE MAIN PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10 AND EMB 140 SWPM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — NOT SEATED (CABIN) · airframe 24,723 hrs · 21,448 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT TOP OVERWING EMERGENCY LIGHT IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND RIGHT TOP OVERWING EMERGENCY LIGHT BULB NOT SEATED PROPERLY RESEATED BULB IAW EMB 140 AMM SUBTASK 33-50-10-420-003-A00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,833 hrs · 19,008 cycles

FOR FLIGHT 4374 DURING THE INSPECTION FOUND THE RIGHT OVERHEAD WING EMERGENCY EXIT LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB 140 AMM 33-50-07-000-802-A AND 33-50-07-400-802-A. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 21,143 hrs · 18,465 cycles

FOR FLIGHT 3250 MAINTENANCE REPORTED THE AFT FLOOR EMERGENCY PROXIMITY LIGHT STRIP TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY AND CHARGER. COMPLIED WITH THE OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW MTX WC 33-700-17. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DAU — INOPERATIVE (NR 1) · airframe 20,531 hrs · 17,928 cycles

ON FLIGHT 4478 AFTER TAKING THE ACTIVE RUNWAY THE CREW REPORTED THAT ALL ENGINE AND TAKEOFF DATA WENT BLANK. DATA ACQUISITION UNIT 1 FAILS MESSAGE APPEARED ON EICAS. LOST ALL ENGINE INDICATIONS AND LANDING GEAR POSITION INDICATIONS. THE CREW ELECTED TO ABORT THE TAKEOFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 DATA ACQUISITION UNIT IAW 31-41-01 MM. PERFORMED ALL TEST AND SYSTEM CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 18,428 hrs · 16,207 cycles

ON FLIGHT 3321, CREW REPORTED SEVERAL EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ALL 4 BATTERY PACKS PER AMM 33-50-04. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. PARTS CHANGED WERE: BATT PACK NR 1 P/N- 20131A S/N- 104885 BATT PACK NR 2 P/N- 20131A S/N 103857, BATT PACK NR 3 P/N 20131A S/N - 103140 BATT PACK NR P/N-20131A, S/N- 101798.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,852 hrs · 15,672 cycles

DURING HMBV, THE CARGO DOOR SILL WAS FOUND CORRODED. REMOVED CORRODED CARGO DOOR SILL. POSITIONED NEW SILL AND DRILLED FOR FASTENERS. CLEANED, ANODIZED, PRIMED AND INSTALLED NEW CARGO DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 17,852 hrs · 15,672 cycles

DURING HMBV A CHAFE WAS DISCOVERED ON A PREVIOUS REPAIR REINFORCEMENT ANGLE ON STRINGER 19L. REMOVED DAMAGED REINFORCEMENT ANGLE AND CLEANED THE AREA. FABRICATED A 1.4 INCH BY 16.25 INCH REINFORCEMENT, TREATED AND INSTALLED REPLACEMENT REINFORCEMENT IAW EMB SRM 51-40-02 AND 53-24-02 FIG 201. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,533 hrs · 15,395 cycles

ON FLIGHT 4606 CREW REPORTED SEVERAL EMERGENCY LIGHTS NOT WORKING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY PACK IAW EMB AMM 33-50-04, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — DEFECTIVE (CABIN) · airframe 17,500 hrs · 15,367 cycles

CREW REPORTED ON PRE FLIGHT THAT THE EMERGENCY EXIT SIGN IN CABIN CEILING ONLY ILLUMINATING ON FWD FACE DURING TEST. AFT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 AC/DC POWER INVERTER IAW EMB AMM 33-50-11, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: COMPUTER — FAILED (WX RADAR SYS) · airframe 14,978 hrs · 13,455 cycles

NOTIFIED BY THE FLT CREW, RADAR FAILED CODE: 11 POC O MAGNETRON. CAPTAIN ELECTED TO DIVERT TO CMH DUE TO WEATHER CONDITIONS. REMOVED AND REPLACED RTU IAW EMB AMM 34-42-01 AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

LAX - FLT 3195 - CREW REPORTED A ROW OF EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY BATTERY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING INSPECTION AIRCRAFT, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVED THE CORROSION. FABRICATED A EXTERNAL DOUBLER, FILLER, SHIMS AND PLATE. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 28, CHAPTER 53-21-10 FIG 201 AND EMB. REPAIR STATEMENT IC2005-145/0983 PARA 1 DATED FEB 23, 2005. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUTOUT TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28 CHAPTERS 53-21-10 FIG 201. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAMES 23 AND 25 WERE FOUND CORRODED. BLENDED THE CORRODED AREAS TO REMOVED THE CORROSION AND PERFORMED NDT INSPECTION AND FABRICATED AN EXTERNAL DOUBLER FOR REPAIR. REPAIR DONE IAW EMB REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/0976, PARA 3 DATED FEB 24, 2005. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE CORROSION. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIRS DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 28, CHAPTER 53-22-10 FIG 201. (M)

Part: STRINGER — GOUGED (FUSELAGE)

ABI - DUIRNG A IMBV INSPECTION OF AIRCRAFT, STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 49 AND 50. BLENDED OUT THE GOUGE, PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-02. (M)

Part: STRINGER — GOUGED (FUSELAGE)

ABI - DURING INSPECTION OF AIRCRAFT, STRINGER 19L AS FOUND TO BE GOUGED BETWEEN FRAMES 49 AND 50. BLENDED OUT THE GOUGE. PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM-145/1142 REV 28 CHAPTER 53-24-02. (M)

Part: BEAM — CORRODED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, THE GALLEY AREA CENTER BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER BEAM. INSTALLED NEW BEAM IAW EMB SRM, SRM 145/1142 REV 28 CHAPTER 51-40-02. (M)

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

IND - FLT 4296 - IN FLIGHT DURING CLIMB PASSING 600 FT BAGGAGE SMOKE LIGHT ILLUMINATED. CREW DISCHARGED BOTTLES, DECLARED EMERGENCY LANDED WITHOUT INCIDENT. INSPECTED BAGGAGE SMOKE DETECTION SYSTEM WITH NO DEFECTS NOTED. RAI FIRE BOTTLES AND A/C RETURNED TO SERVICE. (M)