N955UW

Part: PNEUMATIC SYSTEM — LOW PRESSURE (CABIN DOOR) · airframe 25,521 hrs · 21,388 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING CHECK OF CABIN DOOR EMERGENCY PNEUMATIC ASSEMBLY, FOUND L1 DOOR UNDER DISPATCH LIMITS. MAINTENANCE SERVICED PNEUMATIC ASSEMBLY TO PROPER PRESSURE PER AMM 52-41-51-614-801-A AND 52-12-51-614-802-A.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (L2 DOOR) · airframe 25,521 hrs · 21,388 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING CHECK OF CABIN DOOR EMERGENCY PNEUMATIC ASSEMBLY, FOUND L2 DOOR UNDER DISPATCH LIMITS. MAINTENANCE SERVICED PNEUMATIC ASSEMBLY TO PROPER PRESSURE PER AMM 52-41-51-614-801-A AND 52-12-51-614-802-A.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (R2 DOOR) · airframe 25,521 hrs · 21,388 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING CHECK OF CABIN DOOR EMERGENCY PNEUMATIC ASSEMBLY, FOUND R2 DOOR UNDER DISPATCH LIMITS. MAINTENANCE SERVICED PNEUMATIC ASSEMBLY TO PROPER PRESSURE PER AMM 52-41-51-614-801-A AND 52-12-51-614-802-A.

Part: WARNING LIGHT — FALSE ACTIVATION (SMOKE DETECTOR) · airframe 25,521 hrs · 21,388 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS CABIN SMOKE DETECTOR LIGHT ILLUMINATED. RESET IAW FIM 26-14-00. CHECKS OK.

Part: FIRE BOTTLE — LOW PRESSURE (APU) · airframe 25,477 hrs · 21,350 cycles

AIRCRAFT WAS GROUNDED: APU FIRE BTL DISCH MSG DISPLAYED. ACCOMPLISHED FIM 26-22-00-810-804-A. REMOVED & REPLACED APU FIRE BOTTLE IAW AMM 26-22-01. OPS CHECK GOOD. NO EVIDENCE OF BOTTLE AGENT DISCHARGE PRESENT.

Part: BLEED VALVE — UNRELIABLE (NR 1 ENGINE) · airframe 25,384 hrs · 21,279 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS WITH ICING CONDITIONS AND APPARENT WEAK BLD ON #1 WE DIVERTED TO CLT AFTER DECLARING EMERGENCY PRIOR TO DESCENT. MAINTENANCE REMOVED AND REPLACED #1 ENG PRSOV IAW AMM 36-11-01 & NAPR SHUTOFF VALVE IAW AMM 36-11-03. ALL OPS NORMAL.

Part: WIRE HARNESS — FAULTY (DOOR WARNING) · airframe 25,379 hrs · 21,275 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DOOR POS IND ON MFD - LEFT AFT DOOR WENT RED ON T/O ROLL. REJECTED T/O AT 65KTS. MAINTENANCE REMOVED & REPLACED AFT PASSENGER DOOR WARNING HARNESS IAW AMM 52-72-21. OPS CHECK GOOD.

Part: HEAT EXCHANGER — CONTAMINATED (NR 2 A/C PACK) · airframe 24,513 hrs · 20,452 cycles

AIRCRAFT WAS GROUDNED: PILOT REPORTS STRONG SMELL ON ENTIRE CABIN AND COCKPIT, FLIGHT ATTENDANT SAID ODOR SMELLED LIKE BURNED FOOD. DEPRESSURIZED AIRCRAFT AS QRH PROCEDURE AND SMELL WENT AWAY. AFTER LANDING TURNED PACKS AND BLEEDS ON AND STRONG SMELL CAME BACK AFTER 2 MINUTES. MAINTENANCE ACCOMPLISHED JOBCARD 43L00051001 AND FOUND #2 PACK EXCHANGER CONTAMINATED WITH COFFEE. : MAINTENANCE ACCOMPLISHED CARD 43L19121001 AS REQUESTED, RAN PACKS FOR 2 HOURS AFTER CLEANING WITH NO ODORS NOTED.

Part: CIRCUIT BREAKER — TRIPPED (COCKPIT) · airframe 24,335 hrs · 20,288 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS AVNX MAU 1A FAIL, 9 OTHER CAUTION MSGS, 19 OTHER ADVISOFT MSGS. MAINTENANCE REPORTS C/B B7 ON CAPT'S SIDE WAS POPPED. RESET C/B EVERY THING BACK TO NORMAL IAW FIN 31-42-00-810-808-A.

Part: SIGN — INOPERATIVE (CABIN) · airframe 23,155 hrs · 19,327 cycles

BOS - R1 LOWER EMERGENCY LIGHT INOP. MAINTENANCE REPLACED R1 LOWER EXIT IDENTIFIER SIGN IAW AMM 33-50-15 OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAULTY (ZONE 700) · airframe 22,843 hrs · 19,062 cycles

THE AIRCRAFT WAS GROUNDED. INFLIGHT: EICAS MESSAGE PARKING BRAKE NOT RELEASED DURING CRUISE. COMPLIED WITH QRC + QRH PROCEDURES, HOWEVER, MESSAGE DID NOT EXTINGUISHED FLAPS FULL LANDING GEAR AT 75,000 NO ISSUES. REPLACED E BRAKE VALVE PER AMM 32-44-01 AND REPLACED E BRAKE PRESSURE SWITCH PER AMM 32-44-09. A SUPPLEMENTAL REPORT HAS BEEN ISSUED UPON RECEIPT OF FINAL CORRECTIVE ACTION. (PLEASE SEE SDR AALA201809069022) (***CLOSED)

Part: VALVE — FAULTY (EMERGENCY BRAKE) · airframe 22,843 hrs · 19,062 cycles

INFLIGHT, AN EICAS MESSAGE FOR PARKING BRAKE NOT RELEASED DURING CRUISE. COMPLIED WITH QRC & QRH PROCEDURES, MESSAGE DID NOT EXTINGUISH. FLAPS FULL, LANDING GEAR AT 75,000 NO ISSUES. THE AIRCRAFT WAS GROUNDED. REPLACED THE EMERGENCY BRAKE VALVE IAW AMM 32-44-01 AND REPLACED EMERGENCY BRAKE PRESSURE SWITCH IAW AMM 32-44-09.

Part: DOOR — MALFUNCTIONED (CABIN) · airframe 22,428 hrs · 18,711 cycles

AIRCRAFT WAS GROUNDED. CREW REPORTED L1 DOOR HARD TO CLOSE. UPON ARRIVAL AT AIRCRAFT FOUND DOOR 90% CLOSED. WHILE ATTEMPTING TO CYCLE DOOR, DOOR ASSIST BOTTLE DEPLOYED. REPLACED SHEAR PIN, DIAPHRAGM AND SERVICED DOOR ASSIST BOTTLE PER AMM 52-11-51 AND 52-11-53. ALSO OPERATED DOOR PER AMM 52-11-00. THIS SDR IS FOR SERVICING DOOR ASSIST BOTTLE. (SEE CONTROL #AALA201806139019 AND #AALA201806139020)

Part: PIN — LACK OF LUBE (CAPTAIN'S SEAT) · airframe 22,312 hrs · 18,624 cycles

CAPTAIN`S SEAT WOULD SLIDE FULL AFT PASSING 100 KNOTS DURING TAKEOFF ROLL. CLEANED AND LUBRICATED THE LOCKING PINS AND TRACKS. OPS CHECKED NORMAL.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,888 hrs · 17,509 cycles

MAIN CABIN R2 DOOR EMERGENCY EXIT SIGN INOPERATIVE AND CASE IS CRACKED. REPLACED EXIT SIGN IAW AMM 33-50-15-000-801, AMM 33-50-400-801, AND AMM 33-50-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 20,888 hrs · 17,509 cycles

LEFT FORWARD EMERGENCY LIGHT BATTERY PACK FAILED A FUNCTIONAL CHECK. REPLACED BATTERY PACK IAW AMM 33-50-01-000-801-A, 33-50-01-400-801-A, 33-50-01, AND 33-50-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 20,888 hrs · 17,509 cycles

RIGHT FORWARD EMERGENCY LIGHT BATTERY PACK FAILED A FUNCTIONAL CHECK. REPLACED THE BATTERY PACK IAW AMM 33-50-01-000-801-A, 33-50-01-400-801-A, 33-50-01, AND 33-50-00.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 20,888 hrs · 17,509 cycles

DURING A WIRE EWIS CLEANING AND INSPECTION, FOUND EMERGENCY LIGHTING SYSTEM WIRES W101-01942-24 AND W101-22693-20 EXTERNAL INSULATION BROKEN AND WIRES EXPOSED AT FORWARD MAIN CABIN LEFT FUSELAGE AT STRINGER 3 AND FRAME 19. REPAIRED THE WIRES, PERFORMED SATISFACTORY OPS CHECK OF EMERGENCY EXIT LIGHTS IAW SWPM 20-41-20 AND AMM 33-50-00.

Part: WINDOW — DAMAGED (PAX CABIN) · airframe 20,888 hrs · 17,509 cycles

CRAZING & SCRATCHES ON L1 PASSENGER WINDOW BETWEEN STRINGER 9 AND 10, FRAMES 23 AND 24. REPLACED THE WINDOW IAW AMM 56-20-00. ACCOMPLISHED SATISFACTORY LEAK CHECK.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 20,888 hrs · 17,509 cycles

DELAMINATION ON FIRST OFFICER`S FORWARD HEATED WINDSHIELD UPPER EDGE. REPLACED THE WINDSHIELD IAW 5313P233-001.

Part: SHEAR TIE — DAMAGED (FRAME 24) · airframe 20,888 hrs · 17,509 cycles

ELONGATED HOLE ON THE FRAME 24 SHEAR TIE AT STRINGER 28R. REPLACED THE SHEAR TIE IAW DRAWING 170-67065-461.

Part: RIB — CRACKED (HORIZ STAB) · airframe 20,888 hrs · 17,509 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LEFT HAND HORIZONTAL STABILIZER LEADING EDGE MOST INBOARD RIB. REPLACED RIB PER DRAWING 170-62333-001.

Part: SKIN — CRACKED (LT WING) · airframe 20,888 hrs · 17,509 cycles

CRACK ON LEFT WING LOWER SKIN AFT OF SPAR 2 AND OUTBOARD OF RIB 9A. REPAIRED WING SKIN IAW SRM 57-10-01, REPAIR 54, SRM 57-10-01, SRM 51-43-02, AND EA 272998.

Part: SEAT TRACK — CORRODED (FRAMES 54-55) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON MAIN CABIN SEAT TRACK AT Y1300 BETWEEN FRAMES 54 AND 55. REPLACED THE SEAT TRACK IAW DRAWING 190-22606-453.

Part: PROFILE — DAMAGED (FRAME 24) · airframe 20,888 hrs · 17,509 cycles

ELONGATED HOLE ON L-PROFILE AT STRINGER 28R AND FR 24. REPLACED L-PROFILE IAW SRM 51-41-01 AND DRAWING 170-67065-461.

Part: BOLT — WORN (L1 DOOR SLIDE) · airframe 20,888 hrs · 17,509 cycles

L1 DOOR EMERGENCY SLIDE ATTACHMENT BOLT WORN.. REPLACED THE BOLT. AIRCRAFT WAS GROUNDED.

Part: BOLT — WORN (R2 DOOR SLIDE) · airframe 20,888 hrs · 17,509 cycles

R2 DOOR EMERGENCY SLIDE ATTACHMENT BOLT IS WORN. REPLACED THE BOLT. AIRCRAFT WAS GROUNDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN PASSENGER DOOR CUTOUT, FLOOR STRUCTURE AREA, FLOORBEAM AT -Y1308.1, BETWEEN FR 16 AND FR 17. REPLACED FLOORBEAM PER DRAWING 170-01330-507, SRM 51-40-02 AND SRM 51-43-02.

Part: WEB — CORRODED (FRAMES 26-27) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD CARGO DOOR FRAME BOTTOM WEB BETWEEN FRAMES 26 AND 27, BETWEEN STRINGERS 26R AND 27R. REPLACED THE WEB IAW DRAWING 170-67080-461 AND SRM 51-43-02.

Part: SEAT TRACK — CORRODED (FRAMES 37-43) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSIION ON MAIN CABIN LEFT INBOARD SEAT TRACK, -Y1041, BETWEEN FRAMES 37 AND 42. REPLACED THE SEAT TRACK IAW DRAWING 190-23017-405, SRM 51-41-02, SRM 51-43-03, AND SRM 51-43-04.

Part: SEAT TRACK — CORRODED (FRAMES 49-53) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

GOUGED AND CORRODED LEFT MAIN CABIN SEAT TRACK AT -Y1346, BETWEEN FRAMES 49 AND 53. REPLACED THE SEAT TRACK IAW SRM 51-41-01, 51-43-03, AND DRAWING 190-22606-453.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR STRUCTURE, AFT PASSENGER DOOR CUTOUT LOWER SILL BEAM AT -Y1200 AND FR 85. REPLACED LOWER SILL FLOORBEAM PER DRAWING 170-65480-445 AND SRM 51-41-01, SRM 51-43-03 AND SRM 51-43-04.

Part: STRUCTURE — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON RIGHT AFT MAIN CABIN FLOOR REINFORCEMENT STRUCTURE AT FRAME 84, BETWEEN Y300 AND Y1160. REPLACED REINFORCEMENT STRUCTURE IAW DRAWING 190-65140-801.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOOR STRUCTURE, FLOORBEAM AT Y342.9 BETWEEN FR 17 AND FR 18. REPLACED FLOORBEAM PER DRAWING 170-00822-503.

Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y711.2 AND FR 17. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-503.

Part: SHEAR PANEL — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON AFT MAIN CABIN RIGHT SHEAR PANEL AT Y1200, BETWEEN FRAMES 84 AND 85. REPLACED THE SHEAR PANEL IAW DRAWING 190-65293-001.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON MAIN CABIN RIGHT HAND INBOARD SEAT TRACK AT Y273 BETWEEN FR 37 AND FR 42. REPLACED SEAT TRACK PER DRAWING 190-23017-407.

Part: DOUBLER — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION FORWARD MAIN CABIN FLOOR SUPPORT DOUBLER AT -Y635, BETWEEN FRAMES 19 AND 20. REPLACED THE DOUBLER IAW DWG 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 19-20) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT -Y1219.2, BETWEEN FRAMES 19 AND 20. REPLACED THE FLOOR SUPPORT IAW DWG 53-00-00-3, REPAIR 3.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR STRUCTURE, CENTER SHEAR PANEL BETWEEN Y0 AND -Y150, BETWEEN FR 87 AND FR 88. REPLACED CENTER SHEAR PANEL PER AARD 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON TH EFORWARD MAIN CABIN FLOOR SUPPORT AT -Y1092.2 AND FR 19. REPLACED FLOOR SUPPORT IAW DRAWING 170-29712-805.

Part: SEAT TRACK — CORRODED (FRAMES 78-84) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON MAIN CABIN RIGHT INBD SEAT TRACK AT Y260, BETWEEN FRAMES 78 AND 84. REPLACED THE SEAT TRACK IAW DRAWING 170-65600-443.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE FORWARD MAIN CABIN FLOOR SUPPORT Y406 BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW DRAWING 190-05555-805, SRM 51-41-01, AND SRM 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT -Y355.3 BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-413.

Part: SEAT TRACK — CORRODED (FRAMES 13-19) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN SEAT TRACK AT -Y279.4, BETWEEN FRAMES 13 AND 19. REPLACED THE SEAT TRACK IAW DWG 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE AFT MAIN CABIN FLOOR SUPPORT AT -Y1160, FRAME 84. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-66000-463.

Part: FLOORBEAM — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON AFT MAIN CABIN FLOORBEAM AT FR 84 BETWEEN Y120 AND Y230. REPLACED THE FLOORBEAM IAW SRM 53-23-10, REPAIR 55.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y965 BETWEEN FRAMES 12, AND 14. REPLACED FLOOR SUPPORT DWG 53-00-00-3, REPAIR 3.

Part: DOUBLER — CORRODED (FRAMES 15-16) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT DOUBLER AT -Y368.3, BETWEEN FRAMES 15 AND 16. REPLACED FLOOR SUPPORT DOUBLER IAW DWG 53-00-00-3, REPAIR 3.

Part: FLOORBEAM — CORRODED (FRAME 17) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOORBEAM AT FRAME 17, BETWEEN Y330.2 AND Y1066. REPAIRED THE FLOORBEAM IAW SRM 53-00-10, REPAIR 53.

Part: SEAT TRACK — CORRODED (FRAMES 12-18) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN SEAT TRACK AT Y279.4 BETWEEN FRAMES 12 AND 18. REPLACED THE SEAT TRACK IAW DWG 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT -Y 1117.6 AND FRAME 16. REPLACED THE FLOOR SUPPORT IAW DWG 170-00822-413.

Part: FLOORBEAM — CORRODED (FRAME 87) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE FLOORBEAM AT -Y278 AND FRAME 87. REPAIRED THE FLOORBEAM IAW SRM 52-23-10, REPAIR 53.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT -Y1168.4, BETWEEN FRAMES 12 AND 16. REPLACED THE FLOOR SUPPORT IAW DRAWING 53-00-00-3, REPAIR 3.

Part: FLOORBEAM — CORRODED (FRAME 90) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE AFT MAIN CABIN FLOORBEAM SPLICE AT FRAME 90, BETWEEN Y0 AND -Y160. REPLACED THE FLOORBEAM SPLICE IAW DRAWING 170-65660-447.

Part: FLOOR SUPPORT — CORRODED (FRAME 90) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE AFT MAIN CABIN FLOOR SUPPORT, -Y750, FRAME 90. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-66000-457, SRM 51-42-01, AND SRM 51-41-01.

Part: SUPPORT FITTING — CORRODED (FRAME 90) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSIION ON AFT MAIN CABIN GALLEY SUPPORT FITTING AT -Y750 AND FRAME 90. REPLACED SUPPORT FITTING IAW DWG 170-66000-457, & 170-65660-447.

Part: FLOOR SUPPORT — CORRODED (FRAME 14) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT FRAME 14, Y711. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-503..

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE AFT MAIN CABIN FLOOR SUPPORT AT -Y1000 AND FRAME 84. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-65600-443.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y1092.2, BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW DWG 53-00-00-3, REPAIR 3.

Part: FLOORBEAM — CORRODED (FRAME 89) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE AFT MAIN CABIN FLOORBEAM AT Y900, FRAME 89. REPLACED IAW DWG 53-00-00-3, REPAIR.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE AFT MAIN CABIN FLOOR SHEAR PANEL AT Y920, BETWEEN FRAMES 87 AND 88. REPLACED THE SHEAR PANEL DWG 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE FORWARD MAIN CABIN FLOOR SUPPORT AT Y711.2, FRAME 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01 AND DRAWING 170-21768-407.

Part: FLOOR SUPPORT — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON THE AFT MAIN CABIN FLOOR SUPPORT UPPER SHEET AT -Y278, BETWEEN FRAMES 85 AND 86. REPLACED THE FLOOR SUPPORT IAW DWG 53-00-00-3, REPAIR 3.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON AFT MAIN CABIN FLOOR SHEAR PANEL -Y920, BETWEEN FRAMES 87 AND 88. REPLACED THE SHEAR PANEL IAW DWG 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAMES 85-86) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT UPPER SHEET AT Y278, BETWEEN FRAMES 85 AND 86. REPLACED THE FLOOR SUPPORT IAW DWG 53-00-00-3, REPAIR 3.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 20,888 hrs · 17,509 cycles

CORROSION ON AFT MAIN CABIN FLOOR LEFT GUSSET AT -Y278 AND FRAME 90. REPLACED THE GUSSET IAW DRAWING 170-60001-823.

Part: GIRT BAR — OBSTRUCTED (L2 DOOR SLIDE) · airframe 19,767 hrs · 16,655 cycles

L2 DOOR ARMING LEVER IS DIFFICULT TO MOVE. MAINTENANCE REMOVED DEBRIS GIRT BAR FLOOR FITTINGS AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW FIM TASK 52-12-00-810-808A.

Part: LEVER — LACK OF LUBE (L2 DOOR) · airframe 19,764 hrs · 16,652 cycles

L2 DOOR ARMING LEVER IS DIFFICULT TO MOVE. MAINTENANCE LUBED THE DOOR ARMING LEVER AS REQUIRED AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: MODULE — DEFECTIVE (ZONE 100) · airframe 19,675 hrs · 16,584 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THE FOLLOWING: AOA LIMIT FAILURE, SPOILER FAULT, SLAT FAIL AND SHAKER ANTICIPATED EICAS MESSAGES. AN EMERGENCY WAS DECLARED INTO PHL WHERE THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLIGHT CONTROL PANEL (AALA201702149019), THE MAU2 POWER MODULE (AALA201702149020) AND NIC PROC3. (AALA201702149021)

Part: MODULE — DEFECTIVE (SPOILER) · airframe 19,675 hrs · 16,584 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THE FOLLOWING: AOA LIMIT FAILURE, SPOILER FAULT, SLAT FAIL AND SHAKER ANTICIPATED EICAS MESSAGES. AN EMERGENCY WAS DECLARED INTO PHL WHERE THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLIGHT CONTROL PANEL (AALA201702149019), THE MAU2 POWER MODULE (AALA201702149020) AND NIC PROC3. (AALA201702149021)

Part: MODULE — DEFECTIVE (ZONE 100) · airframe 19,675 hrs · 16,584 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THE FOLLOWING: AOA LIMIT FAILURE, SPOILER FAULT, SLAT FAIL AND SHAKER ANTICIPATED EICAS MESSAGES. AN EMERGENCY WAS DECLARED INTO PHL WHERE THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLIGHT CONTROL PANEL (AALA201702149019), THE MAU2 POWER MODULE (AALA201702149020) AND NIC PROC3. (AALA201702149021)

Part: LEVER — INOPERATIVE (MLG) · airframe 18,896 hrs · 15,953 cycles

FLIGHT CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT WHERE IT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE FOUND LANDING GEAR CONTROL LEVER AT FAULT AND REPLACED IT PER AMM 32-33-01. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 17,452 hrs · 14,745 cycles

AIRCRAFT WAS GNDED. CREW REPORTED SLAT LOCK OUT MSG ON DESCENT. DECLARED AN EMER & LANDED WITHOUT INCIDENT. PERFORMED FIM TASK 27-81-00-810-802-A. NO FAULTS FOUND, TRANSITORY CONDITION. PERFORMED FLIGHT CONTROL RETURN TO SERVICE TEST IAW AMM 27-00-00-070-801A. ACFT OK FOR CONTINUED SERVICE.

Part: STRUT — LOW (NLG) · airframe 16,702 hrs · 14,033 cycles

O TAKEOFF RECEIVED EICAS WOW SENSOR FAIL & LG WOULD NOT RETRACT. CREW RETUNED TO FIELD. ACCOMPLISHED NLG SHOCK STRUT SERVICING IAW CARD 43C70032003. ACCOMPLISHED A SUCCESSFUL LG EXTENSION & RETRACTION TEST IAW AMM 32-33-00. NO FAULTS NOTED.

Part: SENSOR — OUT OF ADJUST (ZONE 700) · airframe 16,639 hrs · 13,987 cycles

EMERGENCY LANDING, EICAS WOW SENSOR FAIL, GEAR LOCKED DOWN AFTER TAKEOFF. CREW RETUNED TO FIELD & AS A PRECAUTIONARY MEASURE DECLARED AN EMER. THE ACFT LANDED WITHOUT INCIDENT. ACCOMPLISHED AN ADJUSTMENT OF THE WOW SENSOR & A SATISFACTORY OPERATIONAL CHECK IAW FIM 32-61-00-810-840-A.

Part: STRUT — CORRODED (NLG) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, DISCOVERED CORROSION & PROTECTIVE COATING PEELING ON LT & RT SIDE OF NLG SHOCK STRUT & AXLE. R & R WITH SERVICEABLE NLG IAW TASK CARD 43L71132001.

Part: LENS — CRACKED (EXTERIOR LIGHT)

LEFT SIDE BEHIND INBD FLAP EXTERIOR EMER LIGHT LENS IS CRACKED. R & R LT EXTERIOR EMER LIGHT LENS BEHIND INBD FLAP IAW AMM 33-50-25.

Part: LENS — CRACKED (EXTERIOR LIGHT)

LOWER RT WING TO BODY FAIRING EMER LIGHT LENS IS CRACKED. R & R LOWER RT WING TO BODY FAIRING EMER LIGHT LENS ASSEMBLY & PERFORMED OPERATIONS CHECK. OPERATIONS CHECKED GOOD. APPLIED SEALANT & TORQUES SCREWS TO SPEC IAW AMM 33-50-400-802, 33-50-25-710-801 & 33-50-25-00-802.

Part: LENS — CRACKED (EXIT SIGN)

R2 DOOR LOWER EMER EXIT SIGN LENS CRACKED. R & R R2 DOOR LOWER EMER EXIT SIGN LENS IAW AMM 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, RT AFT EMER LIGHT INOPERATIVE. REMOVED & INSTALLED SERVICEABLE EMER LIGHT POWER UNIT FOR POSITION NR 6. OPERATIONS CHECKED GOOD AT RT AFT EXTERIOR EMER LIGHT IAW AMM 33-50-01-000-801-A, 33-5-01-400-801-A & 33-50-00-710-801-A.

Part: STRUT — CORRODED (NLG) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, AFTER REMOVAL OF NLG INNER STRUT, FOUND CORROSION ON THE LOWER SEAL WORKING SURFACE INSIDE MAIN STRUT. R & R WITH SERVICEABLE NLG IAW TASK CARD 43L71132001.

Part: TORQUE LINK — WORN (NLG) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, NLG TORSION LINKS HAVE PLAY WHERE THE UPPER & LOWER LINKS CONNECT. NLG WAS REPLACED IAW TASK CARD 43L71132001.

Part: LENS — CRACKED (EXIT SIGN)

R2 DOOR UPPER EMER EXIT SIGN LENS CRACKED. R & R R2 DOOR UPPER EMER EXIT SIGN LENS IAW AMM 33-50-17. OPERATIONS CHECKED GOOD IAW AMM 33-50-00-710-801-A.

Part: LENS — CRACKED (EXIT SIGN)

R1 DOOR UPPER EMER EXIT SIGN LENS CRACKED. R & R R1 DOOR UPPER EMER EXIT SIGN LENS IAW AMM 33-50-17. OPERATIONS CHECKED GOOD IAW AMM 33-50-17.

Part: LENS — CRACKED (EXIT SIGN)

R1 DOOR LOWER EMER EXIT SIGN LENS CRACKED. R & R R1 DOOR LOWER EMER EXIT SIGN LENS IAW AMM 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LENS — CRACKED (EXIT SIGN)

L2 DOOR LOWER EMER EXIT SIGN LENS CRACKED. R & R L2 DOOR LOWER EMER EXIT SIGN LENS IAW AMM 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: GLOWSTRIP — DAMAGED (CABIN)

MAIN CABIN PHOTO LUMINESCENT INDICATOR STRIP LIGHT IS DAMAGED MORE THAN 10%. R & R AT MAIN CABIN PHOTO LUMINESCENT INDICATOR STRIP LIGHT IAW AMM 33-50-21.

Part: LENS — CRACKED (EXIT SIGN)

L1 DOOR EMER EXIT SIGN LENS CRACKED. R & R L1 DOOR EMER EXIT SIGN LENS IAW 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00. REFER TO INDIVIDUAL SIGN OFF ENTRIES FOR WORK STEPS PERFORMED.

Part: LENS — CRACKED (EXIT SIGN)

FORWARD LT CLOSET EMER EXIT SIGN LENS CRACKED. R & R FWD LT CLOSET EMER EXIT SIGN LENS IAW AMM 33-50-17. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

MAIN CABIN FWD & AFT FLIGHT ATTENDANT SEAT FLASHLIGHT BATTERIES ARE LOW, 3 EACH. R & R FLASHLIGHT BATTERIES AT MAIN CABIN IAW DWG 43P25D0742 IAW J & AMM 33-51-01 E190. OPERATIONAL CHECKED GOOD.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT, LOWER FWD CORNER SEAL REST. REPLACED SEAL REST IAW AMM 20-10-01 200 & EO 5313P247.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, CORROSION ON FWD CARGO DOOR CUT OUT, LOWER AFT CORNER SEAL REST. REPLACED SEAL REST IAW AMM 20-20-13 & AARD 53-00-00-3.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, CORROSION ON AFT CARGO DOOR CUT OUT, LOWER AFT CORNER SEAL REST. REPLACED IAW AMM 20-10-01 & AARD 53-00-00-3.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, CORROSION ON FWD CARGO DOOR CUT OUT, LOWER FWD CORNER SEAL REST. REPLACED SEAL REST IAW AMM 20-20-13 & AARD 53-00-00-3.

Part: BEARING — CORRODED (PAX DOOR)

C3 CHECK, AFT PAX DOOR ARM MECHANISM ROLLER BEARING HAS CORROSION, RP-93. R & R AFT PAX DOOR ARM MECHANISM ROLLER BEARING, DAMPER DOOR STOP ROLLER, IAW CMM 52-12-30-020-006-A01 STEP 8 D & CMM 52-12-30-420-023-A01 STEP 29 A. NO ADJUSTMENT DISTURBED.

Part: BEARING — CORRODED (SERVICE DOOR)

C3 CHECK, AFT SERVICE DOOR ARM MECHANISM ROLLER BEARING HAS CORROSION, RP-91. R & R AFT SERVICE DOOR ARM MECHANISM ROLLER BEARING, DAMPER DOOR STOP COLLAR, IAW CMM 52-42-30-020-006-A01 STEP 8 D & CMM 52-42-30-420-022-A01 STEP 28 A. NO ADJUSTMENT DISTURBED.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, CORROSION ON GUSSET AT FRAME 90 & +Y560. REPLACED GUSSET IAW SRM 51-410-02 & DWG 170-60001-823.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, CORROSION ON LT SHEAR PANEL BETWEEN FRAME 87 & 88, -Y304.8 & -Y1041.4. REPLACED SHEAR PANEL IAW DWG 170-66000-439.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, CORROSION ON SHEAR PANEL BETWEEN FRAME 87 & 88, -Y222.3 & +Y222.3. REPLACED SHEAR PANEL IAW AARD 53-00-00-3 REPAIR 3 & DWG 170-6600-439.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 16,611 hrs · 13,966 cycles

C3 CHECK, CORROSION ON RT SHEAR PLATE BETWEEN FRAME 87 & 88, +Y304.8 & +Y1041.4. REPLACED SHEAR PANEL IAW DWG 170-66000-439.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 16,369 hrs · 13,758 cycles

FLIGHT 2135 EN-ROUTE, DIRTY SOCK SMELL ON TAKEOFF. ONLY COULD BE SMELLED IN FLIGHT DECK. FLIGHT ATTENDANT DID NOT SMELL ANYTHING ON MAIN CABIN. PACKS 1 & 2 ON, ENG BLEED ON, APU WAS OFF. AT REDUCTION OF POWER 1000 FEET SMELL WENT AWAY. THE FLIGHT RETURNED TO FIELD & LANDED WITHOUT FURTHER INCIDENT. FOUND ENG NR 1 WETTED WITH OIL. SEE LP 1285192 FOR ENG CHANGE INFORMATION. AFTER ENG CHANGE COMPLIED WITH JC 43L00072001, 43L00021001, 43L00072001, 43L00021001, 43L00036002 & 43T40072004. ALSO REPLACED RECIRCULATION FILTERS IAW AMM 21-24-02 & CABIN SUPPLY DUCT ITEM 30 ON IPC 21-24-03 FIG 01.

Part: PROCESSOR — FAILED (ZONE 100) · airframe 16,252 hrs · 13,637 cycles

FLIGHT 1847 EN-ROUTE, THE FLIGHT EXPERIENCED AN ELEC MALFUNCTION IN CRUISE FLIGHT. THE CAPTAIN'S SIDE MAU1 WAS LOST, ALONG WITH ACARS, AUTOPILOT & AUTO BRAKE FUNCTIONS. THE FLIGHT DECLARED AN EMER & DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NIC 1 PROCESSOR.

Part: HEAT EXCHANGER — CONTAMINATED · airframe 16,175 hrs · 13,587 cycles

FLIGHT 2145, EN-ROUTE AT TAKEOFF THRUST, SMELL MUSTY ODOR THAT LASTED 5 MINUTES UNTIL AFTER TAKEOFF. THE ENG BLEEDS WERE ON & THE APU WAS OFF. DEACTIVATED PACK 2. CLEANED HEAT EXCHANGERS & REPLACED BOTH FWD & AFT TRIM AIR VALVE FILTERS, RT PACK BYPASS VALV EFILTER & HEPA FILTERS. ALSO PERFORMED TAKEOFF POWER RUN, NO ODORS NOTED.

Part: AIR FILTER — ODOR (ZONE 100) · airframe 16,128 hrs · 13,534 cycles

FLIGHT 2164 EN-ROUTE, CREW NOTED A DIRTY SOCK ODOR ONLY IN THE COCKPIT & WAS VERY STRONG AT TAKEOFF THRUST. THE BLEEDS WERE ON THE ENGS & THE APU WAS OFF. THE ODOR WAS VERY STRONG FOR 6 MINUTES. PLACED THE NR 2 PACK ON MEL. REPLACED BOTH RECIRCULATION AIR FILTERS IAW AMM 21-24-02-000. OPERATIONS CHECKED OK. RAN RT PACK WITH ENGS AT 70% N1 FOR 5 MINUTES IAW FIM 21-20-00-810-803A. NO SMELL NOTED. REMOVED MEL FROM NR 2 PACK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,932 hrs · 13,369 cycles

AFT & AFT GALLEY EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT POWER UNIT.

Part: MODULE — FAULTY (BRAKE SYSTEM) · airframe 15,709 hrs · 13,185 cycles

BOTH LT & RT BRK FAULT MSGS IN FLIGHT. THE FLIGHT DECLARED AN EMER & LANDED. THE ACFT WAS THEN TOWED TO THE GATE AS A PRECAUTION. R & R MAU 2 MAIN BRAKE CONTROL MODULE.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,177 hrs · 11,844 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON OTBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,177 hrs · 11,844 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON INBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,177 hrs · 11,844 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT PYLON OTBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (LT PYLON) · airframe 14,177 hrs · 11,844 cycles

LT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUTS LOOSE IN BOTH THE LT & RT ENGS, INBD & OTBD POSITIONS. RE-TORQUED THE LOCKNUTS & APPLIED THE APPROPRIATE SAFETIES.

Part: STRUT — FAILED (RT MLG) · airframe 14,153 hrs · 11,812 cycles

RIGHT MLG SHOCK STRUT ASSEMBLY SEPARATOR PISTON FAILURE. INTERNAL DAMAGE. ACFT YAWED TO THE RT DURING TAKEOFF. REPLACED RT MLG SHOCK STRUT ASSEMBLY IAW JOB CARD 43L73132002.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 13,305 hrs · 11,121 cycles

CRACKS & DELAMINATION ON COPILOTS FIXED WINDSHIELD AROUND EDGES BETWEEN FRAME 8 TO FRAME 9 & BETWEEN STRINGER 2R TO STRINGER 1R. REPLACED COPILOTS FIXED WINDSHIELD IAW E190 MM 56-11-00.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - AFT PASSENGER DOOR EMERGENCY EXIT LIGHT INOP. REPLACED AFT EMERGENCY LIGHT POWER UNIT REF AMM 33-50-01.

Part: SHIELD — BROKEN (EMERGENCY LIGHT) · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - FORWARD LAV EMERGENCY LIGHT (EXIT) HAS SHIELD BROKEN. REPLACED EMERGENCY EXIT LIGHT IAW EMBRAER 190 AMM 33-50-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR TRACK BEAM BETWEEN FR17 TO FR19, Y10.75. REPAIRED FLOOR TRACK BEAM BETWEEN FR17 TO FR19, Y10.75 IAW EA 504628.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR84, Z-450, Y10. REPAIRED SEAT TRACK AT FR84, Z-450, Y10 IAW EMBRAER 190 SRM 53-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOOR TRACK BETWEEN FR17 TO FR19, Y10.75. REPAIRED FLOOR TRACK BETWEEN FR17 TO FR19, Y10.75 IAW EA 504628.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR85 TO FR87, Z-450, Y12. REPLACED FLOORBEAM BETWEEN FR85 TO FR87, Z-450, Y12 IAW EMBRAER 190 SRM 51-23-04.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SHEET PANEL AT FR85, -Z450, -Y10. REPLACED UPPER SHEET PANEL AT FR85, -Z450, -Y10 IAW EMBRAER 190 SRM 51-41-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SHEET PANEL AT FR85, -Z450, Y10. REPLACED UPPER SHEET PANEL AT FR85, -Z450, Y10 IAW EMBRAER 190 SRM 51-41-01.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD GALLEY FLOOR DOUBLER AT FR19 BETWEEN LBL 13 TO LBL 24. REPLACED FORWARD GALLEY FLOOR DOUBLER AT FR19 BETWEEN LBL 13 TO LBL 24 IAW EMBRAER 190 SRM 51-40-02.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN Y10 TO -Y10. REPLACED SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN Y10 TO -Y10 IAW EMBRAER 190 SRM 51-42-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR84, -Z450, -Y10. REPAIRED SEAT TRACK AT FR84, -Z450, -Y10 IAW EMBRAER 190 SRM 53-00-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM TRACK BETWEEN FR12 TO FR17, -Y10.75. REPLACED FLOORBEAM TRACK BETWEEN FR12 TO FR17, -Y10.75 IAW EMBRAER 190 SRM 51-41-01, 51-41-02, 51-43-03 & 51-43-04.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON GUSSET AT FR90, Z-450, Y10. REPLACED GUSSET AT FR90, Z-450, Y10 IAW EMBRAER 190 SRM 51-41-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FR17, -Z450, -Y10. REPLACED SEAT TRACK AT FR17, -Z450, -Y10 IAW EMBRAER 190 SRM 51-41-01, 51-41-02, 51-43-03 & 51-43-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,882 hrs · 9,344 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR87 TO FR88, Z-450, -Y12. REPLACED FLOORBEAM BETWEEN FR87 TO FR88, Z-450, -Y12 IAW EMBRAER 190 SRM 51-22-06.

Part: STRIP — DAMAGED (CABIN) · airframe 9,997 hrs · 8,589 cycles

PHL - EMERGENCY PATH STRIP DAMAGED IN FRONT OF 5C. REPLACED REFLECTIVE FLOOR STRIP AS NEEDED.

Part: DOOR — LACK OF LUBE (R1) · airframe 8,871 hrs · 7,610 cycles

R1 DOOR VERY STIFF WHEN ARMING AND UNARMING. MAINTENANCE LUBRICATED R1 DOOR, OPERATIONAL CHECK IS GOOD.

Part: MEGAPHONE — DEFECTIVE (CABIN) · airframe 8,740 hrs · 7,506 cycles

BOS - UNABLE TO REPLACE MEGAPHONE BATTERIES DUE TO STRIPPED COVER SCREWS. REPLACED MEGAPHONE AS REQUIRED. OPS NORMALLY.

Part: AIR DUCT — MISALIGNED (CABIN) · airframe 8,445 hrs · 7,254 cycles

FLIGHT 2141, BOS-LGA - DURING FLIGHT F/A SMELLED A TORCHED CLOTH BURNING SMELL IN FWD CABIN. CREW ALSO REPORTED NOISE FROM AC LEFT AFT OF FLIGHT CREW. AC RELEASED ON MEL. MAINTENANCE VERIFIED NOISE AND SMELL COMING FROM LEFT PACK SYSTEM. FOUND AIR DUCT NEAR FLOOR ON AC LEFT LOOSE, MISALIGNED. REALIGNED AIR DUCT AS REQUIRED. OPERATED PACKS, NO SMELL OR NOISE NOTED AT THIS TIME. REMOVED MEL.

Part: CONTROL MODULE — INOPERATIVE (BRAKE SYSTEM) · airframe 8,078 hrs · 6,975 cycles

FLIGHT 1776, PHL - BOS - BRAKE RIGHT FAULT ON EICAS. EMERGENCY DECLARED. MAINTENANCE REPLACE BRAKE CONTROL MODULE 1 IN MAU 1 SLOT 5 PER MM 32-41-07. OPERATIONAL CHECK IS GOOD PER MM 32-41-00.

Part: INDICATOR — MISALIGNED (R1 DOOR) · airframe 7,812 hrs · 6,772 cycles

PHL - INDICATOR FOR ARMED /DISARMED ON DOOR 1R IS MISALIGNED. ALSO HANDLES SEEM DIFFICULT TO OPERATE COMPARED TO NORMAL. MAINTENANCE ADJUSTED INDICATOR TO PROPER ALIGNMENT. SLIDE OPERATES NORMAL.

Part: FILTER — DIRTY (CABIN) · airframe 7,628 hrs · 6,612 cycles

BOS - FLIGHT ATTENDANTS AND PASSENGERS REPORT SMELL IN CABIN FROM ROW 15 - 23, SOMETHING LIKE KEROSENE OR BURNING ODOR. MAINTENANCE ACCOMPLISHED J/C 43L00021001 WITH NO FINDINGS, ACCOMPLISHED T/S OF MID E-BAY COMPARTMENT, DUCTING, AND AVIONICS COOLING BLOWERS, CHECK THE RT PACK DUCTING. ACCOMPLISHED BORESCOPES OF BOTH ENGINES, ACCOMPLISHED FIM TASK 49-10-00-810-813A. NO CONTAMINATION FOUND PER APU INSPECTION, ACCOMPLISHED BAAT TEST, CHECKED CABIN FURNISHINGS FOR ODOR. REPLACED THE RECIRC FAN FILTERS.

Part: AIR FILTER — DIRTY (CABIN AIR) · airframe 7,627 hrs · 6,611 cycles

FLIGHT 2139, THE FLIGHT ATTENDANTS REPORTED A BURNING RUBBER ODOR AROUND ROW 20 IN CABIN. THE ODOR DISSIPATED AFTER A FEW MINUTES. THE FLIGHT LANDED WITHOUT INCIDENT. ACCOMPLISHED CABIN AIR QUALITY JOB CARD, CHANGED LEFT AND RIGHT HEPA FILTERS, ACCOMPLISHED A HIGH POWER ENGINE RUN, EITHER BLEED AND APU BLEED FOR HOURS. NO ODORS NOTED, AC IS OKAY FOR SERVICE.

Part: VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 7,444 hrs · 6,412 cycles

FLIGHT 2025, BOS-DCA - ON TAKEOFF, HAD A STRONG SMELL OF WHAT SMELL LIKE HOT BLEED AIR. AIRCRAFT WAS CONFIGURED IN ACCORDANCE WITH PREVIOUS MEL. NO SMELL WAS NOTED IN CABIN, ONLY IN COCKPIT. MAINTENANCE ACCOMPLISHED JOB CARD FOR TROUBLESHOOTING CABIN AIR QUALITY. REPLACED THE NR 1 NASPROV VALVE PER AMM 36-112-03. RAN BOTH ENGINES AT TAKEOFF POWER. NO ODORS NOTED IN COCKPIT. AIRCRAFT OK FOR SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (LT MLG)

FLIGHT 1888, PHL - BOS - AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. LEVER WOULD NOT MOVE OUT OF THE DOWN POSITION. AT ROLL OUT THERE WERE THREE EICAS MESSAGES; ENGINE 1 AND 2 NO DISPATCH, AND FLIGHT CONTROL NO DISPATCH. ALL FUNCTIONS OF WEIGHT ON WHEELS SWITCH WORKED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR "A" SYSTEM SENSOR PER TASK 32-62-03.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

BOS - THE L1 ENTRY DOOR ASSIST BOTTLE IS BELOW WEEKLY CHECK PRESSURE LIMITS. MAINTENANCE SERVICED THE L1 ENTRY DOOR ASSIST BOTTLE PER WEEKLY CHECK CARD AND AMM 52-11-51-03.

Part: CYLINDER — LOW PRESSURE (SERVICE DOOR)

ATL - LEFT AFT SERVICE DOOR PNEUMATIC ASSIST CHARGE IS LOW. MAINTENANCE SERVICED THE LEFT AFT SERVICE DOOR PNEUMATIC ASSIST ASSEMBLY PER AMM 52-12-51-614-801A.

Part: CYLINDER — LOW PRESSURE (PAX DOOR)

ATL - LEFT FORWARD PASSENGER DOOR PNEUMATIC ASSIST CHARGE IS LOW. MAINTENANCE SERVICED THE LEFT FORWARD PASSENGER ENTRY DOOR PNEUMATIC ASSEMBLY PER AMM 52-11-51-614-801A.

Part: SEAT — OUT OF ADJUST (COCKPIT)

DCA - THE CAPTAIN'S SEAT FAILS TO LOCK IN SET POSITION ON THE FORWARD AND AFT SEAT RAIL. THE SEAT SLIDES AFT UNLESS THE HANDLE IS PUSHED FORCEFULLY INTO THE LOCKED POSITION. MAINTENANCE ADJUSTED THE FORWARD CAPTAIN MOVEMENT AND LOCK POSITIONS. OPERATIONAL CHECK IS GOOD AT THIS TIME.

Part: SEAT — MALFUNCTIONED (COCKPIT)

DCA - ON TAKEOFF THE FIRST OFFICER SEAT RECLINED AND WOULD NOT RETURN TO UPRIGHT POSITION. RELEASED ON MEL. OCTOBER 01 - PIT MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS SEAT. OPERATIONAL CHECK IS GOOD, REMOVED MEL 25-11-01, CN 3027C10.

Part: MECHANISM — OUT OF ADJUST (L1 DOOR)

FLIGHT 1821, CLT-MYR - THE 1L DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE INSPECTED THE 1L DOOR AND FOUND NO DAMAGE AND ADJUSTED THE DOOR MECHANISM. PRIOR HISTORY - ON AUGUST 6, 2009 THE L1 DOOR WAS HIT BY THE JETWAY. MAINTENANCE PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: STRUCTURE — BROKEN (COCKPIT SEAT)

CLT - THE CAPTAIN'S RIGHT ARMREST IS BROKEN AND BLOCKING SEAT ACCESS AND EGRESS FROM SEAT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S RIGHT ARMREST.

Part: SENSOR — INOPERATIVE (LE SLAT)

FLIGHT 1907 - PHL-DFW - THE FLIGHT CREW RECEIVED A SLAT FAIL EICAS MESSAGE EN ROUTE TO DFW. THE FLIGHT DIVERTED TO PIT FOR MAINTENANCE. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE LEFT SLAT 2/3 SKEW SENSOR.