N725AE

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,714 hrs · 23,835 cycles

DURING B INSPECTION FOUND ROW 5/6 FLOOR STRIP LIGHTING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR LIGHTING STRIP AT ROW 5/6 IAW EMB AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — DIRTY (PAX DOOR) · airframe 26,612 hrs · 23,729 cycles

FLIGHT 3357, CREW REPORTED SQUEAL COMING FROM MAIN DOOR SEAL. AIRCRAFT REMOVE FROM SERVICE. REMOVED SAFETY STICKERS AND CLEANED MAIN DOOR SEAL AREA, PRESSURIZED ACFT PER AMM 21-31-00. NO SQUEAL NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,340 hrs · 23,440 cycles

DURING MAINTENANCE INSPECTION FOUND THE EXTERIOR WING LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 POWER SUPPL. ALSO REMOVED AND REPLACED NR 4 BATTERY IAW W/CD 33-700-19. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 26,196 hrs · 23,287 cycles

DURING B INSPECTION, FOUND LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW AMM 33-50-04. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 26,163 hrs · 23,249 cycles

DURING MAINTENANCE INSPECTION, FOUND WIRE W192-8833-22 BROKE AT CONNECTOR, WHILE REMOVING NR 6 EMERGENCY LIGHT STRIP. AIRCRAFT REMOVED FROM SERVICE. INSTALLED NEW CONNECTOR TERMINAL TO WIRE. OPS CHECKED GOOD IAW AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,741 hrs · 22,789 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY FLOOR PROXIMITY STRIP INOPERABLE BETWEEN ROWS 7 AND 8. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY POWER SUPPLY NR 3 BATTERY PACK IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HANDLE — LOOSE (CABIN DOOR) · airframe 25,703 hrs · 22,754 cycles

ON FLIGHT 4281 THE CREW REPORTED THE CABIN DOOR WOULD NOT OPEN FROM INSIDE OF AIRCRAFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MAIN CABIN DOOR INTERNAL ACTUATING HANDLE LOOSE AND UNABLE TO ACTIVATE UNLOCKING CAM MECHANISM. RE-INSTALLED INTERNAL ACTUATING HANDLE IAW ERJ 135 AMM 52-18-05. MAIN DOOR FUNCTIONAL CHECK WAS GOOD EAW ERJ 135 AMM 52-18-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,698 hrs · 22,748 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT LATERAL SEAT TRACK SUPPORT CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EO EM-53MR-1939. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,698 hrs · 22,748 cycles

DURING MAINTENANCE BASE INSPECTION FOUND LEFT OMEGA BEAM HAS CORROSION ON PREVIUOS REPAIR AT FRAME 20. REPAIRED LT OMEGA BEAM AT FRAME 20 IAW SRM 53-00-10 FIGURE 201 SHEET 1. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 25,698 hrs · 22,748 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE LEFT COCKPIT FRAME 10 IS CRACKED BENEATH THE DV WINDOW. REMOVED AND REPLACED FRAME 10 O/B SEGMENT IAW SRM 51-40-02. THE AIRCRAFT WAS RETUERNED TO SERVICE.

Part: LIGHT — DAMAGED (CABIN) · airframe 25,719 hrs · 22,769 cycles

DURING B-INSPECTION FOUND THE NR 2, 3, 4, & 6 EMERGENCY LIGHT STRIP TO BE CRACKED AND HAVE BROKEN WIRES. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW NR 2, 3, 4, & 6 EMERGENCY LIGHT STRIP IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SUPPORT — CORRODED (SEAT TRACK) · corrosion level 2 · airframe 25,855 hrs · 22,934 cycles

DURING HEAVY CHECK FOUND RT UPPER SEAT TRACK SUPPORT AT FRAMES 46,47 AND 50 HAVE CORROSION AROUND RIVET HEADS. REPAIRED SUPPORT IAW EO-EM-53MR-1939.

Part: LIGHT — DAMAGED (CABIN) · airframe 25,719 hrs · 22,769 cycles

DURING B-INSPECTION FOUND THE LEFT STRIP ASSEMBLY CRACKED AND WIRES BROKEN FOR LIGHT STRIP. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSTALLED NEW NR 1 LEFT LIGHT STRIP ASSEMBLY IAW EMB AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,698 hrs · 22,748 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLOOR EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BATTERY. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,719 hrs · 22,769 cycles

DURING B-INSPECTION FOUND THE AFT NR 2 FLOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW EMB AMM 33-50-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: TAPE — OUT OF POSITION (RECIRC FAN) · airframe 25,550 hrs · 22,631 cycles

ON FLIGHT 4573 THE CREW REPORTED A STRONG BURNING SMELL IN COCKPIT DURING FLIGHT. THE CREW DECLARED AN EMERGECNY AND DIVERTED. THE AIRCRAFT LANDED WITHOUT INICIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED GENERAL VISUAL INSPECTION OF INTERNAL AIR RECIRCULATION FAN AND FOUND INSULATIOIN TAPE OBSTRUCTING INTAKE OF FAN. REMOVED TAPE FROM FORWARD RIGHT HAND FAN. FAN OPERATES NORMAL PER EMB 135 AMM 21-26-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,522 hrs · 22,616 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,494 hrs · 22,593 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY LIGHT BY THE PASSENGER DOOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN ENTRANCE DOOR EMERGENGY LIGHT IAW EMB 33-50-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: HOLDER — BROKEN (CABIN) · airframe 25,483 hrs · 22,585 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE FLASHLIGHT HOLDER ABOVE THE FLIGHT ATTENDANT SEAT BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED FLASHLIGHT ASSEMBLY IAW EMB 135 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,461 hrs · 22,567 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AFT WING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT WING EMERGENCY LIGHT BULB IAW EMB AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD IAW AMM 52-00-00. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUARD — BROKEN (COCKPIT) · airframe 25,194 hrs · 22,372 cycles

FOR FLIGHT 4573 DURING THE PRE FLIGHT INSPECTION FOUND THE GUARD FOR APU FIRE EXTIN BUTTON HAS BROKEN SPRING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE APU FIRE SW GUARD IAW AMM 20-13-04. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,082 hrs · 22,289 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE AISLE OVERWING EMERGENCY EXIT FORWARD SIGN DOES NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-15. REMOVED AND REPLACED THE NR 6 INVERTER IAW AMM 33-50-11. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,082 hrs · 22,289 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE AISLE AFT EMERGENCY DOME LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE BULB IAW AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 25,070 hrs · 22,279 cycles

EMERGENCY FLOOR LIGHT STRIP FROM ROW 9 BACK TO ROW 13 INOP. REMOVED AND REPLACED NR 4 BATTERY PACK AND CHARGER IAW WC 33-700-19 DID NOT FIX PROBLEM. FOUND NUMBER 6 EMERGENCY LIGHT DC/AC INVERTER CONNECTOR P8532 LOOSE. RECONNECTED CONNECTOR IAW EMB MM 33-50-11 SECTION I (5) OPS CHECK GOOD IAW EMB MM 33-50-00.

Part: DETECTION SYS — MALFUNCTIONED (COCKPIT) · airframe 24,903 hrs · 22,124 cycles

ON FLIGHT 3360 THE CREW REPORTED THAT ON APPROACH WITH THE ICE DETECTOR KNOB IN AUTO, THE AIRCRAFT WAS INDICATING AN ICE CONDITION EVENT THOUGH THEY WERE IN THE CLEAR AND TAT WAS 10C AND HIGHER. DID NOT TURN OFF UNTIL FINAL APPROACH AT DFW. THE CREW DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL TEST OF ICE DETECTION SYSTEM IAW EMB 135 AMM 30-80-00. NO DEFECTS NOTED AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (BLEED AIR SYS) · airframe 24,905 hrs · 22,126 cycles

ON FLIGHT 2871 THE CREW REPORTED A WING ANTI ICE FAIL WITH BLEED 2 LOW TEMPERATURES IN ICING CONDITION. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT AT DFW. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE ENGINE 2 PUSH-BUTTON IAW AMM 20-13-04. THE OPERATIONAL CHECK WAS GOOD IAW AMM 36-11-02. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LENS — MISSING (CABIN) · airframe 23,777 hrs · 21,163 cycles

FOR FLIGHT 4525 DURING PREFLIGHT INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT LENS MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVERWING EMERGENCY LIGHT ASSEMBLY IAW EMB-135 AMM 33-50-07. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PROXIMITY SWITCH — FAULTY (SPOILER) · airframe 22,679 hrs · 20,246 cycles

ON FLIGHT 4542 THE CREW REPORTED AN INADVERTENT SPOILER OPENING IN FLIGHT. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED SAFELY WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE LEFT OUTBOARD PROXIMITY SWITCH. REPLACED THE ELECTRONIC PLUG CONNECTOR TO THE LEFT OUTERMOST PROXIMITY SENSOR P/N 038999/26FA98SN. ALL OPERATIONAL CHECKS WERE GOOD IAW EMB AMM 27-63-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — GOUGED (RT AILERON) · airframe 20,713 hrs · 18,518 cycles

DURING MAIN BASE VISIT INSPECTION FOUND THE RIGHT AILERON DAMPER FITTING TO BE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE RIGHT AILERON BY REPLACING DAMPER FITTING WITH NEW FITTING IAW EO-EM-27MR-122. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 20,614 hrs · 18,423 cycles

DURING MAINTENANCE BASE INSPECTION FOUND THE EMERGENCY LIGHT STRIPS 5 AND 6 AND LEFT OVERWING EMERGENCY LIGHT INOPERABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 4 BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BALLAST — ODOR (CABIN LIGHTS) · airframe 20,541 hrs · 18,359 cycles

DURING FLIGHT 4828 THE FLIGHT ATTENDANT REPORTED A STRONG BURNING ODOR AT SEAT 11A. THE CREW CLOSED THE GASPER ON THE PASSENGER SERVICE UNIT AND THE ODOR WAS LESS BUT STILL NOTICABLE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER LIGHTING BALLAST (LEFT SIDWALL) IAW EMB 135 AMM REF 33-21-03. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

ON FLIGHT 4661 - CREW REPORTED EMERGENCY LIGHTS OVER GALLEY INOPERATIVE. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY OVER GALLEY. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. (S)

Part: ALTIMETER — READS LOW (STANDBY) · airframe 16,044 hrs · 14,624 cycles

NOTIFIED BY DISPATCH CREW ELECTED TO DIVERT TO LGA DISC-DURING CLIMB AT APPROX 15,000 STANDBY AIRSPEED STARTED TOWARD 0' BY 20,000 STANDBY AI SHOWED 0 AND STANDBY ALTIMETER WAS APROX 6,000 FT LOW. REMOVED AND REPLACED STANDBY AIRSPEED INDICATOR AND STANDBY ALTIMETER. STANDBY AIRSPEED IND P/N OFF 64050-663-1 S/N OFF 5173. LEAK AND OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: BULB — ODOR (CABIN LIGHTS) · airframe 15,935 hrs · 14,534 cycles

ELECTRICAL BURNING SMELL AT ROWS 6 AND 7A. REMOVED AND REPLACED WINDOW SIDE LIGHT BULBS IAW AMM 33-20-00. OPS CHECK OK. AIRCRAFT RETURN TO SERVICE.

Part: BULB — ODOR (CABIN LIGHTS) · airframe 15,935 hrs · 14,534 cycles

ELECTRICAL BURNING ODOR AT ROWS 6 AND 7A. REMOVED AND REPLACED WINDOW SIDE LIGHT BULBS IAW AMM 33-20-00, OPS CHECK OK.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 34 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

LEFT INBOARD SEAT TRACK BETWEEN FRAMES 34 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: HINGE FITTING — CORRODED (ZONE 300) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

LEFT ELEVATOR SERVO TAB INBOARD HINGE FITTING CORRODED. REMOVED AND REPLACED HINGE FITTING IAW EMB 55-22-01. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 37 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

LEFT INBOARD SEAT TRACK BETWEEN FRAMES 23 AND 34 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

LEFT INBOARD SEAT TRACK BETWEEN FRAMES 18 AND 23 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

FLOOR SUPPORT BETWEEN FRAMES 22 AND 22A CORRODED. REMOVED AND REPLACED FLOOR SUPPORT IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 23 AND 34 CORRODED, NICKED AND GOUGED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 34 AND 47 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 23 AND 34 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

LEFT OUTBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 53 AND 55 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

RIGHT INBOARD SEAT TRACK BETWEEN FRAMES 23 AND 34 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

RIGHT OUTBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 15,794 hrs · 14,412 cycles

LEFT INBOARD SEAT TRACK BETWEEN FRAMES 47 AND 53 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW EMB AMM 53-01-06. AIRCRAFT RETURNED TO SERVICE.

Part: SENSOR — DEFECTIVE (FUEL SYSTEM) · airframe 15,304 hrs · 13,980 cycles

FUEL FLOW INDICATOR READS 0. LOW SPEED ABORTED TAKEOFF. REMOVED AND REPLACED ENGINE 2 FUEL FLOW SENSOR. OPERATIONAL AND LEAK CHECKS GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: GUST LOCK — FAILED (RUDDER) · airframe 14,716 hrs · 13,490 cycles

GUST LOCK LIGHT ILLUMINATED AT ROTATION - NOTICED CIRCUIT BREAKER 24 POPPED - RESET WITH NO EFFECT TO SYSTEM - DIVERTED TO IAD - EMERGENCY DECLARED. C/A - REMOVED AND REPLACED GUST LOCK ACTUATOR IAW EMB AMM 27-71-01 AND READJUSTED SPRING CARTRIDGE IAW EMB AMM 27-71-14. PERFORMED OPERATIONAL CHECK IAW EMB ACC 27-70-700-802-A. RETURNED AIRCRAFT TO SERVICE

Part: FLOORBEAM — CORRODED (GALLEY)

THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. BLENDED THE FORWARD DIGITAL TO REMOVED THE CORROSION. FABRICATED THE REPAIR DOUBLER, MARKED AND DRILLED FASTENER HOLES. REPAIR DONE IAW EMB. (K)

Part: BEAM — CORRODED (FUSELAGE)

THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. REMOVED THE CORROSION BY MAKING A CUT OUT. PREPARED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)

Part: SILL — CORRODED (SERVICE DOOR)

SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE CORRODED AREA. CLEANED AND TREATED THE BLENDED AREA. APPLIED EPOXY PRIMER AND TOP COAT OF PAINT. FILLED THE BLENDED AREA WITH EPOXY RESIN HYSOL EA934NA, SANDED THE RESIN TO MAKE IT FLAT AND APPLIED EPOXY PRIMER. FABRICATED 2 REPAIR DOUBLERS. REPAIR DONE IAW SRM. (K)

Part: BATTERY — UNKNOWN (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT FLOOR STRIP AT OVERWING EXIT DOES NOT ILLUMINATE ON TEST. REPLACED NR 3 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONNECTOR — FAILED (EMERGENCY LIGHT)

FOUND RT CABIN EMERGENCY EXIT SIGN LIGHTING INOPERATIVE. REPLACED CONNECTOR AND PIN AT SPLICE 9124. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: CONTROL UNIT — INOPERATIVE (HORIZONTAL STAB)

DURING LANDING, CREW RECEIVED PITCH TRIM BACKUP AND MAIN INOPERATIVE MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT IAW EMB MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

FOUND FORWARD FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED NR 1 AND NR 2 BATTERY PACKS IAW W/C 33-100-19. OPS CHECK GOOD. (M)

Part: FRAME — CHAFED (FUSELAGE)

ABI - DURING AN IMBV INSPECTION, FOUND FRAME 81 CHAFED BELOW SRM LIMITS. REMOVED LOWER SECTION OF FRAME. INSTALLED NEW FRAME IAW EMB 145 SRM, SRM EMB-145/1142 REV 24, CHAPTER 51-40-02. (M)

Part: SIGN — INOPERATIVE (CABIN)

RDU - FLT 4879 - CABIN AFT OVERHEAD EMERGENCY EXIT LOCATOR SIGN IS INOPERATIVE. RAI EMERGENCY EXIT LOCATION SIGN. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION OF AIRCRAFT, FOUND CORROSION ON GALLEY RIGHT BEAM AT FRAME 19. REMOVED CORROSION BY BLENDING. PERFORMED AN NDT INSPECTION OF THE AREA AND FOUND NO REJECTABLE INDICATIONS. REPAIRED IAW EMB GST-1348/02, AND STANDARD SRM PRACTICES. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON FORWARD DIGITAL. BLENDED CORROSION PERFORMED NDT, RESTORED SURFACE PROTECTION IAW EMB CPM 51-21-04, 51-21-05, 51-21-06. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CORROSION FOUND ON AFT DIGITAL. BLENDED, PERFORMED NDT, RESTORED SURFACE PROTECTION. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON CENTER BEAM AT FRAME 19. INSTALLED SERVICEABLE CENTER BEAM IAW EMB GST-1348/02. (M)

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

THIS IS A LEVEL 2 FINDING, CORROSION GALLEY CENTRAL BEAM GUSSET. BLENDED CORROSION, PERFORMED NDT, RESTORED SURFACE PROTECTION IAW EMB CPM 51-21-04, 51-21-05, 51-21-06. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CORROSION SERVICE DOOR CENTER SILL. REPAIRED CORRODED SERVICE DOOR SILL IAW EMB GST-1348/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON SERVICE DOOR FORWARD SILL. REPAIRED CORRODED FORWARD SILL IAW EMB GST 1348/02. (M)

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

ABI - THIS IS A LEVEL 2 FINDING, CORROSION ON DIAMOND GUSSET AT FRAME 20. BLENDED CORROSION, PERFORMED NDT, RESTORED SURFACE PROTECTION IAW EMB GST-1348/01. (M)