N823AE

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,625 hrs · 30,859 cycles

AFT F/A FLASHLIGHT INOP. C/A-FLIGHT CREW PLACARED PER MEL 25-53 AUTH#050500-C MOC#696734. REMOVED AND REPLACED THE FA'S FLASHLIGHT IN THE AFT CABIN IAW AMM 33-50-16. OPC GOOD. MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 35,625 hrs · 30,859 cycles

CAPT FLASHLIGHT AND AFT F/A FLASHLIGHT INOP. C/A-FLIGHT CREW PLACARED PER MEL 25-53 AUTH#050499-C MOC#696734. M PROCEDURES C/W. REMOVED AND REPLACED CA FLASHLIGHT AS PER AMM 33-50-16, OPS CHECK GOOD MEL ITEM RESTORED. REMOVED AND REPLACED THE FA'S FLASHLIGHT IN THE AFT CABIN IAW AMM 33-50-16. OPC GOOD. MEL RESTORED.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 35,613 hrs · 30,846 cycles

AFT PASSENGER CABIN EMERGENCY FLASHLIGHT INOP. C/A-REMOVED AND REPLACED AFT PASSENGER CABIN EMERGENCY FLASHLIGHT IAW AMM 33-50-16 STEPS 2.I.(1) AND 3.H.(4). OPC GOOD.

Part: HANDLE — DEFECTIVE (BRAKE SYSTEM) · airframe 35,217 hrs · 30,437 cycles

PARKING BRAKE DIFFICULT TO SET. C/A-REMOVED AND REPLACED PARKING BRAKE HANDLE ASSY IAW AMM 32-44-11 OPT CHK GOOD.

Part: TIRE — DAMAGED (MLG) · airframe 34,169 hrs · 29,459 cycles

DURING LANDDING. UPON APPLYING STEADY BRAKES. THE AIRCRAFT VIBRATES SIGNIFICANTY UNTIL REACHING LOW SPEED IF DOES NOT OCCURS DURING LOW SPEED OR TAXIING SPEED. FOUND TIRE NR 2 HAS FLAT SPOT. R&R NR 2 MAIN LANDING GEAR WHEEL ASSEMBLY IAW W/C 32-700-11.

Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 32,270 hrs · 27,701 cycles

LAVATORY SMOKE MSG IN FLIGHT, RAN PROCEDURE, FLIGHT ATTENDANT NOTES NO SMOKE OR HEAT SOURCE IN LAVATORY WHEN INSPECTED, PAX WAS IN LAVATORY AT TIME. PERFORMED OPERATIONS CHECK OF LAVATORY SMOKE DETECTION SYS. OPERATIONS CHECK GOOD, BREAKERS RESET & OK FOR SERVICE IAW AMM 26-14-00.

Part: WIRE — BROKEN (CABIN) · airframe 32,039 hrs · 27,433 cycles

EMERGENCY LIGHT STRIP WIRE BROKEN UNDER FLOOR PANEL 251GF. REPAIRED EMER LIGHT STRIP WIRE UNDER FLOOR PANEL 251GF IAW SWPM 20-21-00 & 20-50-01. SEE NRTC BOW 216053 FOR OPERATIONS CHECK. SEE TASK & WIP ENTRIES FOR DETAILS.

Part: CONTROL PANEL — MALFUNCTIONED (ENGINE FUEL) · airframe 30,956 hrs · 26,518 cycles

PRIOR TO DECENT, NR 1 FUEL LOW PRESSURE ANNUNCIATION ILLUMINATED FOLLOWED BY CLICKING RELAYS. ABOUT THE SAME TIME RECEIVED AN ELECTRICAL BURNING ODOR BOTH IN THE COCKPIT & CABIN. RAN FUEL LOW PRESSURE, CABIN & COCKPIT FUMES CHECKLISTS. FUEL PUMP WAS ON 1A THEN SWITCHED TO PUMP 1B. THE FUEL LOW PRESSURE CAUTION MESSAGE EXTINGUISHED & CLICKING RELAYS STOPPED. DURING DECENT AT ABOUT 15,000 FT THE ELECTRICAL BURNING ODOR DISSIPATED. AN EMERGENCY WAS DECLARED & ACFT LANDED SAFELY. PERFORMED GVI OF FUEL PUMP CONNECTORS K0119 1A K0122, 1B K0123 & 1C FOUND NO DAMAGE. PERFORMED GVI OF RELAYS K0301 & K371, APU FUEL & ENG FUEL, FOUND NO DAMAGE. CONFIRMED FUEL PMP 1A CHATTERING WHEN SELECTED, ALL OTHER FUEL PMPS WORKING CORRECTLY IAW AMM 28-21-14, 20-13-03 & AWM 28-21-50. R & R FUEL CONTROL PANEL IAW AMM 28-20-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,121 hrs · 25,818 cycles

AFT EMER LIGHT ON CEILING INOPERATIVE. R & R AISLE EMER LIGHT LAMP IAW AMM 33-50-08. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: ELT — INOPERATIVE · airframe 29,634 hrs · 25,410 cycles

ELT INOPERATIVE. CURRENT MEL 25-59 CHANGED IAW MEL MAN REVISION 29 FROM AUTH 03061D-D TO TO 030612D-A DATE OF DISCOVERY IS 3-14-14 EXP 6-12-14 MEL REMAINS OPEN.

Part: HOLDER — BROKEN (FLASHLIGHT) · airframe 29,618 hrs · 25,392 cycles

FLIGHT ATTENDANT FLASHLIGHT HOLDER HAS BROKEN RETAINING CLIP. R & R FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY IAW AMM 25-60-11, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,234 hrs · 25,035 cycles

REAR EMERGENCY FLOOR LIGHTING STRIP INOPERATIVE. R & R REAR EMERGENCY FLOOR LIGHTING STRIP IAW AMM 33-50-12.

Part: VENT — SMOKE (ROWS 5 AND 7) · airframe 28,568 hrs · 24,241 cycles

AT TOUCH DOWN DURING LANDING, F/A REPORTED A WHITE LIKE SMOKE SUBSTANCE COMING OUT OF LOWER "B" SIDE VENTS BETWEEN ROWS 5 AND 7 AFTER LANDING IT DISAPPEARED UPON FURTHER INVESTIGATION NO OTHER ANOMOLIES WERE NOTED. THERE WAS NO SMOKE SMELL AT ALL TO NEVER REOCCUR. PERFORMED OPS CHECK OF ACFT SYS IAW (DISTRUBITION) IAW 21-20-00 AND FIM 21-20-00- 810-801A. FOUND NO ABNORMAL ODOR OR SMOKE IN CABIN.

Part: FLASHLIGHT ASSY — INOPERATIVE (CABIN) · airframe 27,900 hrs · 23,592 cycles

DURING B INSPECTION, FOUND THE F/A FLASHLIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R FLASHLIGHT IAW AMM 33-50-16. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 27,093 hrs · 22,962 cycles

DURING MAINTENANCE INSPECTION FOUND THE AFT FLIGHT ATTENDANT FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT AS REQUIRED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 27,093 hrs · 22,961 cycles

FRAME 23 AT STRINGER 15R IS CRACKED. REPAIRED IAW EO EM-53MR-1797.

Part: TRIM PANEL — BROKEN (CABIN) · airframe 27,114 hrs · 22,975 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 6 RIGHT AISLE BROWN EXTRUSION BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 6 RIGHT AISLE BROWN EXTRUSION IAW EMB-140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (CABIN) · airframe 27,114 hrs · 22,975 cycles

DURING MAINTENANCE INSPECTION FOUND THE NR 1 EMERGENCY LIGHT STRIP 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: LIGHT — BROKEN (CABIN) · airframe 27,114 hrs · 22,975 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIPS NR 3 & NR 4 BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIPS NR 3 & NR 4 IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,114 hrs · 22,975 cycles

DURING B INSPECTION FOUND THE LAV AREA LEFT GUSSET HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV AREA LEFT BEAM GUSSET IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR SEAL — TORN (MAIN DOOR) · airframe 27,114 hrs · 22,975 cycles

DURING B INSPECTION FOUND THE MAIN DOOR FOLDING FLAP SEAL TORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SIDE HINGED MAIN DOOR RUBBER TRIM SEAL IAW EM140 AMM 52-18-04. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 27,114 hrs · 22,975 cycles

DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY POWER SUPPLY UNIT NR 2 NEEDS TO BE REPLACED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EPSU NR 2 S/N 14911 EMERGENCY BATTERY POWER SUPPLY AND BATTERY HOLDER ASSEMBLY IAW AEA WC 33-700-19. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 27,114 hrs · 22,975 cycles

DURING B INSPECTION FOUND THE LAV AREA CENTER GUSSET HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAV AREA CENTER BEAM GUSSET IAW EMB SRM 51-40-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,880 hrs · 22,778 cycles

DURING B INSPECTION FOUND THE FORWARD CABIN EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT SEAT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT ASSEMBLY PER EMB 140 AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD PER EMB 140 AMM 33-51-01. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,750 hrs · 22,680 cycles

ON FLIGHT 3202 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW EMB CMM 25-60-02. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,945 hrs · 22,029 cycles

DURING MAINTENANCE INSPECTION FOUND THE LEFT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT AFT OVERWING EMERGENCY LIGHT BULB IAW EMB 140 AMM 33-50-07. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL VALVE — CONTAMINATED (AC BAY) · airframe 25,831 hrs · 21,933 cycles

ON FLIGHT 3381 - THE CREW REPORTED A FAINT BUT PERSISTANT UNUSUAL ODOR IN THE COCKPIT AND CABIN. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. ODOR IN THE COCKPIT AND CABIN DETERMINED TO BE P-80 RUBBER LUBRICANT USED ON SLEEVES OF NR 1 DUAL TEMP CONTROL VALVE. REMOVED AND REPLACED THE NR 1 DUAL TEMP CONTROL VALVE REF AML PG 3261494 ITEM 1. NO ODOR AT THIS TIME. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 25,504 hrs · 21,640 cycles

DURING MAINTENANCE, FOUND THE FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLASHLIGHT ASSEMBLY IAW AMM TASK 33-50-16-000-801-A AND 33-50-16-400-801-A. AIRCRAFT RETURNED TO SERVICE.

Part: HOLDER — BROKEN (COCKPIT) · airframe 24,887 hrs · 21,077 cycles

DURING B-INSPECTION FOUND THE FLASHLIGHT BASE BEHIND CAPTAIN’S SEAT BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT BASE BEHIND CAPTAIN’S SEAT. THE OPERATIONAL CHECK WAS GOOD IAW EMB 140 AMM CHAPTER 33-50-16. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,863 hrs · 21,055 cycles

DURING B-INSPECTION FOUND THE PASSENGER DOOR EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PASSENGER DOOR EMERGENCY LIGHT BULB IAW EMB AMM 33-50-06. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (CABIN DOOR) · airframe 24,443 hrs · 20,679 cycles

FOR FLIGHT 2886 FLIGHT ATTENDANT REPORTED MAIN CABIN DOOR HARD TO PUSH OPEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND STUCK ROLLER ON DOOR LUBED MECHANISIM AND PERFORMED OPS TEST IAW EMB 140 AMM 52-18-00 OPERATIONAL TEST NORMAL AT THIS TIME. NO PARTS REMOVED OR REPLACED THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 24,433 hrs · 20,673 cycles

FLIGHT 3221, CREW REPORTED RED LIGHT ON CAPTAIN`S FLASHLIGHT DID NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT, OPS CHECKED GOOD IAW 33-51-01. AIRCRAFT RETURNED TO SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,399 hrs · 20,646 cycles

DURING B-INSPECTION FOUND THE MAIN SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-06. THE OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: PCU — MALFUNCTIONED (RUDDER) · airframe 23,109 hrs · 19,640 cycles

ON FLIGHT 2734 THE CREW REPORTED THAT DURING CLIMBOUT RECEIVED A RUDDER OVER BOOST MESSAGE ON EICAS. THE CREW COMPILED WITH THE CHECKLIST AND NO FURTHER PROBLEMS WERE NOTED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RUDDER POWER CONTROL UNIT IAW EMB 140 AMM 27-22-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,108 hrs · 19,639 cycles

DURING MAINTENANCE BASE VISIT FOUND THE RIGHT AFT EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT 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 23,044 hrs · 19,591 cycles

FLOOR PROXIMITY STRIP 4TH FROM THE FRONT IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY STRIP LIGHT 4TH FROM THE FRONT IAW EMB 140 AMM 33-50-12. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,969 hrs · 19,537 cycles

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

Part: TIRE — SEPARATED (MLG) · airframe 22,882 hrs · 19,468 cycles

ON FLIGHT 3214 THE CREW REPORTED THE TREAD SEPARTED ON TAKEOFF. THE AIRCRAFT LANDED WITHOUT INCIDENT AT DFW. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 MAIN LANDING GEAR TIRE IAW MNTC W/C 32-700-11. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 22,566 hrs · 19,234 cycles

FOR FLIGHT 2773 DURING MAINTENANCE BASE INSPECTION FOUND SEAT 5A AND 6A EMERGENCY FLOOR LIGHT STRIP WIRE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED SEAT 5A AND 6A FLOOR LIGHT STRIP IAW EMB 140 AMM 33-50-12. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FITTING — CHAFED (AILERON) · airframe 22,095 hrs · 18,862 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT AILERON PCA FITTING TO HAVE CHAFE MARKS ON IT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AILERON PCA FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 22,095 hrs · 18,862 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND FRAME 23 TO HAVE A CRACK BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW EO EM-53MR-1797. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ATTACH FITTING — GOUGED (LT AILERON) · airframe 22,095 hrs · 18,862 cycles

DURING MAINTENANCE BASE VISIT INSPECTION FOUND THE LEFT AILERON DAMPER ATTACH FITTING GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AILERON DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 21,399 hrs · 18,066 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CEILING EMERGENCY LIGHT AT ROW 11 TO BE WORKING INTERMITTENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT ASSEMBLY IAW EMB AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,399 hrs · 18,066 cycles

DURING MAINTENANCE BASE VISIT FOUND THE CEILING EMERGENCY LIGHT AT PASSENGER DOOR TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT LAMP AT PASSENGER DOOR IAW ER 140 AMM 33-50-08. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: COUPLING — TORN (NR 2 PACK) · airframe 20,172 hrs · 17,046 cycles

ON FLIGHT 4523 THE CREW REPORTED, RECEIVED BLEED NR 2 LEAK WITH LOSS OF PRESSURIZATION. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO BDL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. DURING VISUAL INSPECTION OF THE NR 2 PACK FOUND A TORN COUPLING THAT ATTACHED THE PACK VALVE TUBE TO THE DUAL TEMPERATURE CONTROL VALVE. REMOVED AND REPLACED COUPLING IAW AMM 21-60-01 EMB 140. THE OPERATIONAL CHECK AND LEAK CHECK WERE GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

ON FLIGHT 3643 CREW REPORTED EMERGENCY LIGHTING INOPERATIVE ON PREFLIGHT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 AND 4 EMERGENCY BATTERY IAW AMM 33-50-04. OPS CHECKS GOOD. AFT RETURNED TO SERVICE. (S)

Part: SOLENOID — FAILED (ZONE 700) · airframe 12,992 hrs · 11,174 cycles

NOISE AND RUMBLE FROM NOSE LANDING GEAR AREA, EICAS INDICATED GEAR UP POSITIONS, RETURNED TO LGA. FOUND NOSE LANDING GEAR DOOR WOULD NOT CLOSE AFTER RETRACTION. REMOVED AND REPLACED NOSE GEAR DOOR SOLENOID VALVE IAW EMB AMM 32-33-02 AND EXTENSION AND RETRACTION CHECKS IAW EMB AMM 32-30-00 WITH NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.

Part: LOCK — BROKEN (ZONE 200) · airframe 12,898 hrs · 11,102 cycles

LAVATORY DOOR LOCKS AND WILL NOT UNLOCK, TRAPPED PASSENGER INSIDE LAVATORY, EITHER NORMAL OR ALTERNATE RELEASE PROCEDURES WORK. REMOVED AND REPLACED LAVATORY DOOR LOCK IAW EMB AMM 25-40-02. OPERATIONAL CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 12,645 hrs · 10,897 cycles

MULTIPLE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 1 POWER SUPPLY IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

MCO - FLT 4498 - BAGG SMOKE INDICATION ON EICAS, FA REPORTED NO VISIBLE SMOKE FOLLOWED AOM PROCEDURES AND BLEW BOTTLES DECLARED EMERGENCY AND LANDED IN MCO WITHOUT INCIDENT. REPLACED BOTH CARGO FIRE BOTTLES AND BOTH CARGO SMOKE DETECTORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SILL — CORRODED (BAGGAGE DOOR)

THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE EXISTING LOWER SILL AND CLEANED THE AREA. INSTALLED SERVICEABLE SILL IAW SRM. (SW21200600333) (K)

Part: FLOORBEAM — CORRODED (GALLEY)

THE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF THE FORWARD DIGITAL TO REMOVE THE CORROSION. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (SW21200600333) (K)

Part: CLIP — CORRODED (BAGGAGE DOOR)

THE BAGGAGE DOOR FWD LATERIAL (SHEAR CLIP) LOWER SECTION AT FRAME 65 WAS FOUND CORRODED. REMOVED A SECTION OF THE SHEAR CLIP TO REMOVE THE CORROSION. PREPARED A SHEAR CLIP. FABRICATED A SHEAR CLIP SPLICE DOUBLER. REPAIR DONE IAW SRM. (SW21200600333) (K)

Part: CONTROLLER — BURNED (WINDSHIELD TEMP)

COCKPIT AND CABIN HAVE ELECTRIC SMOKE SMELL PERMEATING THROUGHOUT, VERY STRONG AND NOXIOUS. REPLACED NR 2 WINDSHIELD TEMP CONTROLLER AND NR 2 WINDSHIELD HEAT WIRES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — FAILED (NR 2) · airframe 6,400 hrs · 6,051 cycles

NR 2 ENGINE FAILED DURING TAKEOFF ACCOMPANIED BY A NOISE THAT SOUNDED LIKE A COMPRESSOR STALL. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE IAW MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502355) (K)

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED THE ROW 11 EMERGENCY EXIT ILGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT ASSEMBLY IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — GOUGED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, TWO GOUGES WERE FOUND IN FUSELAGE SKIN BETWEEN FRAMES 19 AND 20 AND STRINGERS 1L AND 2L, CENTER FUSELAGE 1. BLENDED THE GOUGED AREAS AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 ERV 22, CHAPTER 53-21-01, EMB REPAIR STATEMENT IC2003-145/3231 AND STANDARD SRM PRACTICES. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. REMOVED CORROSION CREATING A CUTOUT IN THE FLANGED AND WEB AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 22, 53-21-10 FIG 201 SHEET 2 AND CPM 51-21-06. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS BETWEEN FRAMES 24 AND 25. REMOVED CORROSION BY CREATING A CUTOUT IN THE FLANGED AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 22, 53-22-10, FIG 201 SHEET 2 AND CPM 51-21-06. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. REMOVED CORROSION BY CREATING A CUTOUT IN THE FLANGED AND WEB AREA. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 22, 53-21-10 FIG 201 SHEET 2 AND CPM 51-21-06. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 22, CHAPTER 53-24-02, EMB STATEMENT IC2003-145/3093A AND STANDARD SRM PRACTICES. (M)

Part: STRINGER — CHAFED (FUSELAGE)

ABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02, EMB STATEMENT IC2003-145/3098A AND STANDARD SRM PRACTICES. (M)

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

CREW REPORTED AN OVERHEAD EMERGENCY LIGHT IN THE CABIN TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 INVERTER IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)