N832AE

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 28,312 hrs · 23,528 cycles

DURING APPROACH ON FLIGHT 3632 CREW REPORTED LANDING BAGG SMOKE ON EICAS & BAGGAGE EXTINGUISHER BUTTON ILLUMINATED. BAGG SMOKE MESSAGE CLEARED MINUTES AFTER PRESSING BAGG EXTINGUISHER BUTTON. THE ACFT WAS REMOVED FROM SERVICE. R & R CARGO BAGGAGE COMPARTMENT FIRE BOTTLES IAW AMM 26-23-01. PERFORMED FIM TAKS 26-15-00-810-805-A PRIOR TO FIRE BOTTLE R & R. NO DEFECTS NOTED WITH SMOKE DETECTOR SYS. NO ACTUAL SIGNS OF SMOKE OR FIRE NOTED.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 27,972 hrs · 23,222 cycles

CABIN DOOR HARD TO OPEN IAW F/A. LUBED MAIN DOOR FRAME ROLLERS IAW MM 53-21-02. OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (MAIN CABIN DOOR) · airframe 27,823 hrs · 23,083 cycles

F/A REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN. PERFORMED MAIN DOOR INTERNAL ACTUATING HANDLE TEST IAW TASK 52-18-00-820-801. A MAX PUSH FORCE FROM DYNOMOMETER WAS 20 LBS WITHIN LIMITS OF 50 LBS. LUBED MAIN DOOR FRAME ROLLERS IAW MM 53-21-02. OPS CHECKED GOOD.

Part: SWITCH — LOOSE (A/C PACK) · airframe 27,804 hrs · 23,066 cycles

SWITCH FOR PAC 1 FELL OUT, AND SMOKE WAS COMING OUT OF OPENING. PAC 1 SWITCH REINSTALLED IAW AMM 20-13-04. INTERNAL INSPECTION FOR OVERHEAT CARRIED OUT. NO FAULT NOTED.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 27,674 hrs · 22,935 cycles

F/A REPORTS MAIN CABIN DOOR IS HARD TO OPEN. LUBED MAIN DOOR EXTERNAL HANDLE MECHANISM & FUSELAGE ROLLERS. OPS CHECKED OK IAW AMM 52 18 00.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 27,631 hrs · 22,899 cycles

MAIN CABIN DOOR HARD TO OPEN. ADJUSTED AND LUBED MAIN CABIN DOOR ROLLERS IAW MM 52-10-01. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN · airframe 27,143 hrs · 22,500 cycles

CREW REPORTED THAT AFTER ENTERING ICING CONDITIONS ON DESCENT, THE WING BUTTON ON THE OVERHEAD PANEL DID NOT DISPLAY OPEN INSCRIPTION AND RECEIVED AN EICAS ANTI-ICE FAIL MESSAGE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. PERFORMED ANTI-ICE OPS CHECK IAW AMM 30-00-00-700-802-A. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (LT WING) · airframe 27,030 hrs · 22,414 cycles

DURING B INSPECTION, FOUND THE LT EMERGENCY LIGHT ABOVE WING INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LT EMERGENCY LIGHT IAW AMM 33-50-10. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: SCREW — DEFECTIVE (CABIN DOOR) · airframe 26,886 hrs · 22,311 cycles

DURING MX INSP, FOUND THE CABIN DOOR HANDLE HARD TO MOVE TO THE OPEN AND CLOSED POSITION. THE ACFT WAS REMOVED FROM SERVICE. R & R THE AFT LOWER GUIDE SCREW IAW AMM 53-21-06. THE OPS CHECK WAS GOOD AT THIS TIME. THE ACFT WAS RETURNED TO SERVICE.

Part: ESCAPE HATCH — LACK OF LUBE (COCKPIT) · airframe 26,125 hrs · 21,698 cycles

ON FLIGHT 3321 THE CREW REPORTED THEY COULD NOT OPEN THE LANDING GEAR EMERGENCY HATCH. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED EMERGENCY LANDING GEAR HATCH DOOR AS REQ PER STANDARD PRACTICE. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SENSOR — FAILED (SPOILER) · airframe 26,006 hrs · 21,579 cycles

ON FLIGHT 4097 THE CREW REPORTED THAT ON CLIMB THROUGH 7000FT THEY RECEIVED A SPOILER FAIL INDICATION ON EICAS AS WELL AS OPEN INDICATION SPOILERS NEVER OPENED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED RIGHT I/B SPOILER PROX SWITCH IAW 27-63-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,723 hrs · 21,318 cycles

ON FLIGHT 4187 THE CREW REPORTED THE FORWARD CABIN FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE FLASHLIGHT IAW EMB-140 AMM 33-50-16. THE OPERATIONAL TEST WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 25,660 hrs · 21,262 cycles

ON FLIGHT 4085 THE FLIGHT ATTENDANT REPORTED THE MAIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. LUBRICATED THE MAIN DOOR FRAME ROLLERS PER AMM 53-21-02. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,498 hrs · 20,190 cycles

DURING B INSPECTIONS FOUND THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT EXTERNAL OVERWING EMERGENCY LIGHT IAW EMB 140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — BROKEN (CABIN) · airframe 24,498 hrs · 20,190 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGECNY FLOOR PROXIMITY STRIP LIGHTS ON FLOOR PANEL 241DF HAS A BROKEN CONNECTOR. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CONNECTOR ON THE EMERGENCY FLOOR PROXIMITY STRIP LIGHTS 241DF IAW EMB 140 WM 20-21-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,916 hrs · 19,750 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AFT FUSELAGE EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FUSELAGE EXIT EMERGENCY LIGHT IAW EMB AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,838 hrs · 19,688 cycles

DURING B-INSPECTION FOUND THE AFT OVERWING EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,778 hrs · 19,639 cycles

DURING B-INSPECTION FOUND THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY BATTERY AND BATTERY CHARGER IAW EMB 140 AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 23,127 hrs · 19,152 cycles

ON FLIGHT 2866 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN DOOR FRAME ROLLERS. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD AMM 53-10-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — ODOR (HYDRAULIC BAY) · airframe 23,124 hrs · 19,148 cycles

FOR FLIGHT 3281 DURING PREFLIGHT OF AIRCRAFT A VERY STRONG ODOR OF METAL OVERHEATING IN THE NR 1 (LEFT) HYDRAULIC COMPARTMENT. THE ODOR BECAME MUCH WORSE WHEN SELECT HYDRAULIC PUMP WAS ON. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF NR 1 & NR 2 HYDRAULIC PUMPS. NO DEFECTS NOTED AT THIS TIME. REF EMB 140 AMM 29-14-00. NO PARTS REMOVED OR REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — MALFUNCTIONED (EXTERIOR) · airframe 23,111 hrs · 19,139 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT OVERWING E EXTERIOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERIVCE. AFTER FURTHER INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT OPERATIVE. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS PERFORMED IAW EMB 140 AMM 33-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,925 hrs · 19,016 cycles

OVERWING EMERGENCY LIGHT INOP RT. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT LAMP RT IAW EMB 140-AMM 33-50-10 OPS CHECK GOOD IAW EMB 140 AMM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,925 hrs · 19,016 cycles

DURING INSPECTION FOR FLIGHT 2844 THE OVER WING RIGHT EMERGENCY LIGHT WAS FOUND TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OVERWING EMERGENCY LIGHT LAMP RIGHT IAW EMB-140 AMM 33-50-10. THE OPERATIONAL CHECK WAS GOOD IAW EMB-140 AMM 33-50-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,688 hrs · 18,851 cycles

DURING MAINTENANCE INSPECTION FOUND THE OBSERVER SEAT LIFE VEST BAG TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE OBSERVER SEAT LIFE VEST IAW EMB 140 EEL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 22,260 hrs · 18,522 cycles

ON FLIGHT 2821 THE CREW REPORTED THE MAIN CABIN DOOR UPPER FLAPPER MECHANISM IS DIFFICULT TO CYCLE SEAL CLOSED WHEN CLOSING DOOR HANDLE FULL DOWN. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBED MAIN CABIN DOOR ROLLER IAW EMB 140 AMM 52-18-00. NO PARTS REMOVED OR REPLACED. THE OPERATIONAL CHECK WAS GOOD, NO DEFECT NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 20,459 hrs · 17,045 cycles

FOR FLIGHT 2712 THE EMERGENCY LIGHT STRIP AT ROW 7-8 WAS DISCOVERED TO HAVE A BROKEN WIRE. THE AICRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLOOR LIGHT STRIP. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 19,486 hrs · 16,289 cycles

DURING THE MAINTENANCE BASE VISIT FOUND FRAME 23 BETWEEN STRINGER 15 RIGHT AND 16 RIGHT TO BE CRACKED AROUND RIVET WHERE AFT SERVICE DOOR SILL IS ATTACHED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH INSTALLATION OF FRAME SECTION IAW SRM 51-40-02 AND EO EM 53MR-1608. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 19,486 hrs · 16,289 cycles

DURING HEAVY MAINTENANCE BASE VISIT INSPECTION FOUND THE RIGHT OMEGA BEAM CRACKED AT THE NUT PLATE HOLES JUST AFT OF FRAME 59 AND 60. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACE THE RIGHT OMEGA BEAM FROM FRAME 57 TO FRAME 62 IAW EMBRAER SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 18,947 hrs · 15,851 cycles

ON FLIGHT 3910 DURING THE APPROACH THE CREW REPORTED, RECEIVED A BRAKE INBOARD INOPERABLE MESSAGE ON EICAS WHEN THE LANDING GEAR WAS EXTENDED. THE CREW DECLARED AN EMERGENCY DIVERTING TO CMH AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT IAW FIM TASK 32-41-00-810-809A FOUND SYSTEM NR 2 BRAKE CONTROL VALVE BAD. REMOVED AND REPLACED THE NR 2 BRAKE CONTROL VALVE IAW EMB AMM 32-41-06. NO LEAKS NOTED AND THE OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TRIM SWITCH — STUCK (COCKPIT) · airframe 18,517 hrs · 15,448 cycles

ON FLIGHT 4161 DURING THE CLIMB AT APPROXIMATELY 4000 FEET THE FIRST OFFICER REPORTED THAT THE PITCH TRIM SWITCH WAS STUCK IN THE UP POSITION. THE CAPTAIN’S SWITCH WAS WORKING OK AND OVERRODE THE FIRST OFFICERS SWITCH. THE CREW ELECTED TO RETURN TO ORD. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE HORIZONTAL STABILIZER PITCH TRIM SWITCH IAW EMB AMM 27-40-03. THE OPERATIONAL CHECK WAS GOOD. NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (BRAKE SYSTEM) · airframe 18,459 hrs · 15,383 cycles

ON LANDING FOR FLIGHT 4395 THE CREW REPORTED A BRAKE OUTBOARD MESSAGE ON EICAS. THE INBOARD BRAKE TEMPERATURE WAS MUCH HIGHER THAN THE OUTBOARD. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BRAKE CONTROL UNIT IAW 140 AMM 32-41-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,441 hrs · 11,615 cycles

ON MBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO HAVE CORROSION AT CROSS MEMBER FRAME 25. REPAIRED OMEGA BEAM IAW SRM 53-00-10 FIG 202. AIRCRAFT RETURN TO SERVICE.

Part: CONTROL UNIT — FAILED (COCKPIT) · airframe 12,305 hrs · 10,018 cycles

ON TAKEOFF RECEIVED LANDING GEAR/GROUND FAIL MESSAGE WITH ASSOCIATED AURAL WARNINGS REGARDING CONFIGURATION. PERFORM PROCEDURES IN AOM1 - RETURNED TO CMH. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS 1 AND 2 TARGETS. REMOVED AND REPLACED LANDING ELECTRONIC GEAR CONTROL UNIT IAW EMB AMM 32-32-01. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS IAW AMERICAN EAGLE WORK CARD 32-700-16. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 12,244 hrs · 9,965 cycles

NO CABIN PRESSURIZATION IN CLIMB. REMOVED AND REPLACED DIGITAL PRESSURIZATION CONTROLLER IAW EMB AMM 21-21-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND CENTER HAT BEAM FLOOR RAMP IS CORRODED AT FRAME 20. INSTALLED NEW SUPPORT IAW EMB AMM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 AND 36. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND LEFT INBOARD OMEGA BEAM CORRODED AT FRAME 20. REMOVED CORROSION AND MADE A DOUBLER REPAIR TO OMEGA BEAM. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 AND 36. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 36 AND 47. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND LEFT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 28 AND 36. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND RIGHT INBOARD SEAT TRACK CORRODED BETWEEN FRAMES 20 AND 28. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND LEFT INBOARD FLOOR SUPPORT FOR LAVATORY UNIT CORRODED. REMOVED AND REPLACED DIGITAL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: DOUBLER — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND RIGHT OUTBOARD HAT BEAM DOUBLER PLATE AT FRAME 22 CORRODED. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING IMBV INSPECTION, FOUND LEFT INBOARD SEAT TRACK BETWEEN FRAMES 22-28 IS CORRODED. REMOVED AND INSTALLED TRACK IAW AMM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND FLOOR SUPPORT FOR POTABLE WATER OVERFLOW HOOK-UP CORRODED. INSTALLED NEW FLOOR SUPPORT FOR POTABLE WATER OVERFLOW DRAIN AT FRAME 60 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING IMBV INSPECTION, FOUND AFT RIGHT UPPER SEAT TRACK CORRODED BETWEEN FRAMES 47-53. REMOVED AND INSTALLED SEAT TRACK IAW EMB SRM 53-01-06. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING IMBV INSPECTION, FOUND AFT RIGHT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAMES 47 AND 53. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND FORWARD CENTER DIGITAL AT FRAME 13 CORRODED. REMOVED AND REPLACED DIGITAL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND RIGHT INBOARD FLOOR SUPPORT FOR LAVATORY CORRODED. REMOVED AND REPLACED DIGITAL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

DURING MBV INSPECTION, FOUND SERVICE DOOR CENTER SILL CORRODED. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (FUSELAGE)

THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 135 SRM, SRM EMB-145/1142 REV 30, CHAPTERS 51-40-02 AND 51-20-03. (M)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)

EMERGENCY FLOOR LIGHTING STRIP INOPERATIVE AT SEAT 16A, ISSUED MEL 33-27. FOUND CONNECTION OF STRIP LIGHTING LOOSE. RE-SECURED AS REQUIRED IAW EMB AMM, MEL RESTORED. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — DIRTY (COCKPIT)

ORD - WHILE TAXIING AIRCRAFT, CAPTAINS SEAT INTERMITTENTLY WOULD SLIDE BACK FROM A LOCKED POSITION. MAINTENANCE CLEANED DEBRIS FROM SLIDE TRACK. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)