N735TS

Part: SWITCH — BROKEN (FLASHLIGHT)

COPILOT FLASHLIGHT SWITCH AND BASE BROKEN. REPLACED ASSY.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 25,078 hrs · 22,519 cycles

DURING B INSPECTION FOUND THE LEFT AFT EXTERIOR EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-50-04 AND THE LEFT AFT EXTERNIAL LIGHT ASSEMBLY IAW AMM 33-50-10. PART NUMBER FOR LIGHT: 30-2510-3. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTACTOR — DETACHED (CABIN) · airframe 24,824 hrs · 24,824 cycles

DURING B INSPECTION FOUND THE INTERIOR AISLE FORWARD OVER WING EMERGENCY EXIT SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-ATTACHED CONTACT PIN ON INTERIOR AISLE FORWARD OVER WING EMERGENCY EXIT SIGN IAW EMB AMM 33-50-15. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,700 hrs · 21,020 cycles

DURING B-INSPECTION FOUND THE PSU EMERGENCY LIGHT ON A ROW INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP ON ROW A EMERGENCY EXIT PSU IAW EMB 135 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 23,672 hrs · 20,981 cycles

ON FLIGHT 2846 THE CREW REPORTED THE EMERGENCY EXIT ROW FLOOR STRIP LIGHTING AT SEAT 6A AND NOT EXIT ROW SEAT 9A IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPOSITIONED EMERGENCY LIGHT FLOOR STRIPS TO THE CORRECT POSITION AT THE EXIT ROW IAW EMB-135 AMM 33-50-12. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 23,652 hrs · 20,961 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP NR 2 FROM THE FORWARD CONNECTOR ACFT SIDE BROKEN OFF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED EMERGENCY STRIP CONNECTOR ACFT SIDE IN REF TO STANDARD PRACTICES WIRING MANUAL 20-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,646 hrs · 20,953 cycles

DURING B-INSPECTION FOUND THE EMERGENCY LIGHT STRIP AT SEAT 8A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT STRIP IAW 33-50-12. THE OPERATIONAL CHECK WAS GOOD IAW 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — WRONG PART (CABIN) · airframe 23,161 hrs · 20,456 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY FLOOR LIGHT STRIP AT EMERGENCY EXIT DOOR REMOVED DUE TO BEING THE WRONG PART NUMBER INSTALLED. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED EMERGENCY LIGHT STRIP IAW AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 22,698 hrs · 20,015 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CARGO FLOOR SUPPORT ANGLE AT FRAME 66 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED ANGLE IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 22,698 hrs · 20,015 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE CARGO DOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SILL IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 22,698 hrs · 20,015 cycles

DURING MAINTENANCE INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT CROSSBEAM FRAME 20. AIRCRAFT REMOVED FROM SERVICE. REPAIRED IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: REPAIR — CORRODED (FUSELAGE) · corrosion level 2

DURING MAINTENANCE BASE INSPECTION FOUND THE CENTER OMEGA BEAM REPAIR DOUBLER AT FRAME 24 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATION IS PENDING.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 22,698 hrs · 20,015 cycles

DURING MAINTENANCE INSPECTION FOUND LEFT OMEGA BEAM REPAIR DOUBLER AT FRAME 24 CORRODED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 21,560 hrs · 19,046 cycles

ON FLIGHT 4437 THE CREW REPORTED A GALLEY SMOKE HORN ACTIVATED WHEN CLIMBING OUT AT 13,000 FEET. NO FIRE INDICATIONS WERE ON EICAS. THE CAPTAIN ELECTED TO RETURN TO LGA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW EMB 135 AMM 26-14-01. THE OPERATIONAL CHECK WAS GOOD. COMPLIED WITH FCD EM 25049R1. TEMPER PROOF SEALANT. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,128 hrs · 18,671 cycles

FOR FLIGHT 4394 DURING PREFLIGHT INSPECTION THE CREW NOTICED THE FORWARD SECTION FLOOR EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY NR 2 IAW 33-50-04. THE OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — CONTAMINATED (FUSELAGE) · airframe 20,480 hrs · 18,123 cycles

FOR FLIGHT 4458 WHILE AT THE GATE WITH PASSENGERS BOARDED THERE WAS A NOTICEABLE FUEL ODOR APPARENT TO PASSENGERS AND FLIGHT CREW WITH ENGINES AND APU NOT RUNNING. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED AND FOUND RESIDUAL FUEL UNDER FLOOR BOARDS BETWEEN STATION 9984.0 TO 15721.0. NO LEAKS FOUND AS PER "CONTRACT COMPANY" FFC SERVICES (REPAIR ORDER) 5100680, IAW EMB -28-11-00. FUEL CELL REPAIR CONTRACTOR PRESSURIZED TANK WITH NO LEAKS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 20,476 hrs · 18,120 cycles

DURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY FLOOR STRIP FOR SEATS 11 THROUGH 13 TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FLOOR STRIP LIGHTING FOR SEATS 11 THROUGH 13. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAULTY (CABIN) · airframe 20,338 hrs · 17,991 cycles

ON FLIGHT 4417 A PASSENGER REPORTED AN ELECTRICAL BURNING ODOR AT ROW 9A AT THE PASSENGER SERVICE UNIT AND READING LIGHT. THE AIRCRAFT WAS AT THE GATE READY FOR PUSHBACK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CIRCUIT BOARD AT SEAT 9A IAW EMB 135 AMM. THE OPERATIONAL CHECK WAS GOOD. NO ODOR OR OTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 18,958 hrs · 16,812 cycles

ON FLIGHT 4553 THE FLIGHT ATTENDANT INFORMED THE CREW OF A VERY NOTCABLE SMELL IN THE AFT SECTION OF THE AIRCRAFT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LIGHT ASSEMBLY FOR SEAT 9A AND 8A SIDEWALL IAE AMM 33-21-06. OPERATIONAL CHECK GOOD, NO FURTHER SMELL NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — WORN (AILERON) · airframe 18,272 hrs · 16,210 cycles

DURING THE MAIN BASE VISIT INSPECTION FOUND RIGHT AILERON TO POWER ACTUATOR CONTROL ATTACHED FITTING WORN AT OUTBOARD HAT BUSHING LUG. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE REMOVED POWER ACTUATOR CONTROL FITTING AND INSTALLED NEW RIGHT AILERON POWER ACTUATOR CONTROL FITTING IAW EO EM-27MR-112. AIRCRAFT RETURNED TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 15,540 hrs · 13,897 cycles

ON FLIGHT 3989, CREW REPORTED LAV SMOKE WARNING ON EICAS AFTER TAKEOFF. FLIGHT ATTENDANT DID NOT HAVE ANY INDICATIONS OF SMOKE. AIRCRAFT REMOVED FOR SERVICE. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW EMB 135 AMM 26-14-01. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 14,299 hrs · 12,843 cycles

LEFT AND RIGHT EMERGENCY DOOR, LOWER EXIT LIGHTS EMERGENCY EXIT FLOOR LIGHTING INOPERATIVE. REMOVED AND REPLACED NR 5 INVERTER IAW EMB AMM. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 13,727 hrs · 12,354 cycles

EMERGENCY PATH LIGHTS FROM ROW 6 FORWARD NO TEST. REMOVED AND REPLACED NUMBER 2 POWER SUPPLY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SILL — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 13,412 hrs · 12,107 cycles

FOUND SERVICE DOOR FRAME LOWER SILL FOUND CORRODED. REMOVED EXISTING SILL. CLEANED AND TREATED REPAIR AREA. INSTALLED NEW SILL IAW EMB SRM 51-40-02. RESTORE PROTECTIVE FINISH, RETURNED AIRCRAFT TO SERVICE.

Part: LINE — BROKEN (HYDRAULIC SYS) · airframe 13,360 hrs · 12,058 cycles

NUMBER ONE HYDRAULIC SYSTEM FAIL, EMERGENCY DECLARED. REMOVED AND REPLACED BROKEN HYDRAULIC LINE AND HYDRAULIC PUMP DUE TO FUILD STARVATION. ALL WOORK DONE IAW EMB AMM 29-10-30 AND 29-10-03. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: LIGHT — BURNED (ROW 6A)

SMOKE COMING FROM FLOURESCENT LAMP FIXTURE OVER ROW 6A. REPLACED LIGHT FIXTURE AT SEAT 6A IAW EMB WM SP CH 20-21. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

CREW REPORTED THE LT FUSELAGE EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200503029) (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN INSPECTION MAINTENANCE FOUND THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE ISW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN INSPECTION MAINTENANCE FOUND A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR PARTS. FABRICATED A DOUBLER, FILLER, PLATE AND TWO SHIMS. REPAIR DONE IAW SRM. (K)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING AN IMBV INSPECTION MAINTENANCE FOUND THE LT OMEGA BEAM TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (FUSELAGE) · airframe 8,464 hrs · 7,886 cycles

DURING AN IMBV INSPECTION, THE BAGGAGE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED BAGGAGE DOOR SILL. INSTALLED NEW SILL, REPAIR DONE IAW SRM. (SW21200502482) (K)

Part: BEAM — CORRODED (FUSELAGE) · airframe 8,464 hrs · 7,886 cycles

DURING AN IMBV INSPECTION THE CENTER HAT BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORRODED CENTER HAT BEAM AND INSTALLED SERVICEABLE ONE. REPAIR DONE IAW SRM AND EA. (SW21200502482) (K)

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 8,464 hrs · 7,886 cycles

DURING AN IMBV INSPECTION, A PREVIOUS REPAIR ON FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE EXISTING DAMAGED REPAIR. FABRICATED 2 DOUBLERS, AND FILLER. REPAIR DONE IAW SRM. (SW21200502482) (K)

Part: SILL — CORRODED (SERVICE DOOR) · airframe 8,464 hrs · 7,886 cycles

DURING AN IMBV INSPECTION OF AIRCRAFT, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED AHT CORRODED SERVICE DOOR CENTER SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM. (SW21200502482) (K)

Part: STRINGER — CHAFED (FUSELAGE)

DURING AN IMBV MAINTENANCE FOUND A PREVIOUS REPAIR ON STRINGER 19R AT JUNCTION 5 BETWEEN FRAMES 52 AND 53 WAS FOUND CHAFED. REMOVED THE EXISTING DAMAGED REPAIR ANGLE AND SHIMS. FABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502482) (K)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DCA - FLT 4606 - EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT 9A. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY AND CHARGER IAW EMB 135 AMM CH 33-50-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

TOP AND LOWER LT EXIT LIGHTS ON SERVICE DOOR WILL NOT REMAIN ILLUMINATED. REPLACED NR 2 BATTERY POWER SUPPLY. AC RETURNED TO SERVICE. (SW21200407048)

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

CREW REPORTED THE FLOOR PROXIMITY EMERGENCY LIGHTS BY THE FIRST FOUR ROWS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY PACK IAW MFG MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200406977)

Part: POWER SUPPLY — INOPERATIVE (NR 2)

DURING PREFLIGHT, CREW REPORTED THE FORWARD EMERGENCY LIGHT WOULD STAY ON FOR ONLY 2 SECONDS. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY LIGHT BATTERY PACK IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLASHLIGHT — SHORTED (GALLEY)

BWI - FLT 4834 - CREW REPORTED A SMOKE ODOR COMING FROM THE EMERGENCY EXIT SIGN AT FLIGHT ATTENDANT STATION. CONTRACT MX INSPECTED AND FOUND THAT DE-ICE FLUID HAD SHORTED OUT THE FLIGHT ATTENDANT FLASH LIGHT CHARGER ASSEMBLY. THE CHARGER ASSEMBLY WAS PUT ON MEL AT THIS TIME. MX REMOVED AND REPLACED THE FLIGHT ATTENDANT FORWARD FLASHLIGHT ASSEMBLY IAW. THE EMB MM. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE CENTER SECTION OF THE FORWARD DIGITAL WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REMOVED DAMAGED 15.25 BY 21.25 SECTION OF THE FORWARD DIGITAL BY CUTOUT. FABRICATED A REPLACEMENT FORWARD DIGITAL CENTER SECTION. FABRICATED TWO DOUBLERS AND SHIMS AND REPAIRED IAW EMB 145 (SRM 145/1142, CHAPTER 53, REV 20) 53-21-10 PARA 4, AND STANDARD SRM PRACTICES. (M)

Part: BEAM — CORRODED (FUSELAGE)

DURING AN INSPECTION CORROSION WAS FOUND ON THE LEFT HAND BEAM AT FRAME 20. COMPLETELY REMOVED CORROSION BY CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM.

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED AT JUNCTION 05. BLENDED CHAFED AREA. PERFORMED EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED AND DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 19) AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, STRINGER 19R WAS FOUND TO BE CHAFED AT JUNCTION 05. BLENDED CHAFED AREA. PERFORMED EDDY CURRENT INSPECTION NO DEFECTS NOTED. FABRICATED A DOUBLER ANGLE, TWO SHIMS. REPAIR DONE IAW EMB 145 SRM (145/1142, CHAPTER 53, REV 19) 53-24-02, AND STANDARD SRM PRACTICES. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

ORD - FLT 4522 - ON CLIMB-OUT, CREW GOT EICAS MESSAGE OF ELECTRICAL EMERGENCY ABNORMAL AND EMERGENCY LIGHTS NOT ARMED, THEY RETURNED TO FIELD FOR MAINTENANCE. (M)