N953UW

Part: AUTOTHROTTLE SYS — MALFUNCTIONED · airframe 25,488 hrs · 21,159 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS NO GREEN ATTCS ON TAKEOFF ROLL, REJECTED TAKE OFF 40 KNOTS. MAINTENANCE ACCOMPLISHED FIM TASK 22-31-00. AUTO THROTTLE TEST OK IAW AMM 22-31-00. OK FOR SERVICE. TESTS OK.

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 25,446 hrs · 21,119 cycles

AIRCRAFT NOT GROUNDED: DURING CLIMB PASSING 10'000 FEET CABIN PRESSURE INDICATED - 300SWITCHED TO MANUAL MODE AND WAS ABLE TO MAINTAIN CABIN PRESSUREBETWEEN 1000 FEET TO 1200 FEET. REMOVED AND REPLACED CPCS CONTROLLER IAW AMM 21-31-01.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 25,357 hrs · 21,043 cycles

AIRCRAFT NOT GROUNDED: PILOT REPORTS A/T FAIL, A/P FAIL, A/T FAULT, A/P FAULT, TAILSTRIKE AVOIDANCE FAULT, CHECK IRS 2 POSITION MESSAGES. MAINTENANCE REPORTS IAW FIM 22-31-00-810-815-A (FAULT 22310017TA1), ACCOMPLISHED AIOP A1 MODULE RESET. TESTS GOOD. FOUND TO BE TRANSITORY CONDITION.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 23,647 hrs · 19,586 cycles

DURING A PREFLIGHT TEST, WHEN SELECTING EMERGENCY LIGHTS ON, THE EMERGENCY LIGHT BATTERY FAULT EICAS MESSAGE DISPLAYED. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED POWER SUPPLY IAW AMM 33-50-01, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: SWITCH — OUT OF ADJUST (EMERGENCY LIGHTS) · airframe 22,261 hrs · 18,501 cycles

OVERHEAD EMERGENCY LIGHTS ABOVE 1R AND 1L AND FLIGHT DECK STEP LIGHT ILLUMINATED WITH WEIGHT ON WHEELS. MAINTENANCE FOUND FOWARD DOOR SWITCH OUT OF ADJUSTMENT AND ADJUSTED DOOR SWITCH AND PERFORMED SATISFACTORY OPERATIONAL CHECK IAW AMM 33-26-00/400.

Part: SLIDE — DEFECTIVE (L2 DOOR) · airframe 21,985 hrs · 18,286 cycles

L2 SERVICE DOOR DISARM VISUAL INDICATION NOT FULLY IN WINDOW WITH HANDLE IN DISARM POSITION. RIGGED L2 DOOR IAW AMM 52-12-52-820-801-A. OPS CHECKED NORMAL. REMOVED AND REPLACED THE SLIDE IAW J/C 43L00025001.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 21,541 hrs · 17,938 cycles

FLIGHT DECK EMERGENCY LIGHT INOPERATIVE. REPLACED POWER UNIT. AIRCRAFT WAS GROUNDED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 21,138 hrs · 17,625 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-03. AIRCRAFT WAS GROUNDED.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 20,756 hrs · 17,328 cycles

FLIGHT DECK EMERGENCY LIGHT NOT WORKING. REPLACED EMERGENCY LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 20,693 hrs · 17,276 cycles

AIRCRAFT WAS NOT GROUNDED. COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE DURING TEST. REPLACED LIGHT ASSEMBLY.

Part: WARNING MESSAGE — FALSE ACTIVATION (AUTOBRAKE) · airframe 20,514 hrs · 17,112 cycles

WHEN LOWERING THE LANDING GEAR, AUTOBRAKE DISENGAGED AND EICAS MESSAGES BRK RH FAULT AND BRAKE LT FAULT ILLUMINATED. DECLARED EMERGENCY. PERFORMED FIM TASK. NO FAULTS FOUND.

Part: HEAT EXCHANGER — DIRTY (AC BAY) · airframe 20,497 hrs · 17,095 cycles

AIRCRAFT WAS GROUNDED. AT 1,000 FT. AFT FA CALLED AND REPORTED A STRONG BURNING ODOR. DECLARED EMERGENCY AND RETURNED TO BOS. ACCOMPLISHED DUAL HEAT EXCHANGER CLEANING.

Part: RIB — CRACKED (LT WING) · airframe 20,422 hrs · 17,037 cycles

CRACK ON LEFT LEADING EDGE RIB 17 AT -YA8551. REPLACED THE RIB IAW DRAWING 190-31005-49.

Part: RIB — CRACKED (RT WING) · airframe 20,422 hrs · 17,037 cycles

CRACK ON RIGHT WING LEADING EDGE RIB 17 AT YA8551. REPLACED THE RIB IAW DRAWING 190-31005-409.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 20,422 hrs · 17,037 cycles

CRACKED MAIN CABIN FORWARD LOWER CEILING PANEL 228 ARC EXIT LIGHT LENS COVER. REPLACED EXIT MARKING SIGN LENS COVER PER E190 AMM 33-50-17.

Part: SEAT TRACK — CORRODED (FRAMES 20-23) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SEAT TRACK AT Y279, AND GOUGED BETWEEN FRAMES 20 AND 23. REPAIRED THE SEAT TRACK IAW SRM 53-00-10, REPAIR 51, EA 270315, AND DRAWING 170-67120-439.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON AFT MAIN CABIN RIGHT SEAT TRACK AT Y304 AND FRAME 84. REPLACED THE SEAT TRACK IAW DRAWING 170-65606-443.

Part: SKIN — CRACKED (LT WING) · airframe 20,422 hrs · 17,037 cycles

CRACK ON LEFT WING SPAR 2 TRAILING EDGE UPPER SKIN, FORWARD OF THE NR 4 SPOILER. REPAIRED THE SKIN IAW SRM 57-50-01, REPAIR 51, AND 57-10-01, REPAIR 1.

Part: PLATE — CORRODED (FRAME 24) · airframe 20,422 hrs · 17,037 cycles

CORROSION ON MAIN CABIN FLOOR STRUCTURE PLATE AT Y609.6 AND FR 24. REPLACED FLOOR PLATE PER DRAWINGS 170-67030-441, AND 170-67142-001.

Part: ISOLATOR — DAMAGED (L2 DOOR SLIDE) · airframe 20,422 hrs · 17,037 cycles

L2 AFT PASSENGER DOOR SLIDE AFT ISOLATOR DAMAGED. REPLACED THE ISOLATOR. AIRCRAFT WAS GROUNDED.

Part: DOUBLER — CORRODED (FRAMES 15-16) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FORWARD FLOOR DOUBLER BETWEEN -Y304 AND -Y355, BETWEEN FRAMES 15 AND 16. REPLACED FLOOR DOUBLER PER E190 SRM 51-41-02 AND AARD 53-00-00-3 REPAIR 3.

Part: FLOOR SUPPORT — ELONGATED (FRAME 32) · airframe 20,422 hrs · 17,037 cycles

ELONGATED HOLE ON MAIN CABIN FLOOR SUPPORT AT -Y330 AND FRAME 32. REPLACED THE FLOOR SUPPORT IAW DRAWING 190-67250-807.

Part: ISOLATOR — DAMAGED (R2 DOOR) · airframe 20,422 hrs · 17,037 cycles

R2 SERVICE DOOR SLIDE FORWARD ISOLATOR DAMAGED. REPLACED THE ISOLATOR. AIRCRAFT WAS GROUNDED.

Part: ISOLATOR — DAMAGED (R1 DOOR SLIDE) · airframe 20,422 hrs · 17,037 cycles

R1 SERVICE DOOR EVACUATION SLIDE ISOLATOR DAMAGED. REPLACED THE ISOLATOR. AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (RT WING) · airframe 20,422 hrs · 17,037 cycles

RIGHT WING LOWER SKIN DRAIN HOLE AT RIB 10 CRACKED. REPAIRED IAW EA 506657A.

Part: STRUCTURE — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON AFT MAIN CABIN RIGHT REINFORCEMENT STRUCTURE AT Y1168, FRAME 84. REPLACED REINFORCEMENT STRUCTURE IAW DRAWING 190-65140-801.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y368 BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW DWG 190-05555-805.

Part: DOUBLER — CORRODED (FRAME 11) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON COCKPIT FLOOR SUPPORT FORWARD DOUBLER AT FRAME 11. REPLACED THE FWD DOUBLER IAW DRAWING 170-00825-411.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y342 BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-505.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FLOOR SUPPORT BETWEEN -Y1066 AND -Y1244, FRAMES 12 AND 16. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN LEFT FLOOR SUPPORT -Y1104 AND FRAME 16. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-21768-407.

Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT -Y736 AND FRAME 17. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-415.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON AFT MAIN CABIN RIGHT SHEAR PANEL AT Y588 TO Y889, BETWEEN FRAMES 87 AND 88 REPLACED SHEAR PANEL IAW 53-00-00-3, REPAIR 3.

Part: SEAT TRACK — CORRODED (FRAMES 12-19) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN SEAT TRACK BETWEEN Y279 BETWEEM FRAMES 12 AND 19. REPLACED THE SEAT TRACK IAW 53-00-00-3, REPAIR 3.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON AFT MAIN CABIN LEFT SHEAR PANEL AT -Y1008 BETWEEN FRAMES 87 AND 88. REPLACED SHEAR PANEL IAW 53-00-00, REPAIR 3.

Part: SEAT TRACK — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND SEAT TRACK AT -Y279 AND FR 84. REPAIRED SEAT TRACK PER E190 SRM 53-00-10 AND DRAWING 170-65600-441.

Part: SEAT TRACK — CORRODED (FRAMES 31-34) · airframe 20,422 hrs · 17,037 cycles

CORROSION ON LEFT LATERAL SEAT TRACK BETWEEN FRAMES 31 AND 34. REPLACED THE SEAT TRACK IAW DRAWING 170-67030-441, AND 170-17900-803.

Part: SUPPORT — CORRODED (FRAME 89) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON AFT MAIN CABIN RIGHT PANEL SUPPORT AT Y889 AND FR 89. REPLACED PANEL SUPPORT IAW DRAWING 170-66000-457.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT -Y1092 AND FRAME 19. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-00822-505.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON AFT MAIN CABIN LEFT FLOOR SUPPORT AT -Y342 AND FRAME 84. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-65600-443.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON AFT MAIN CABIN LEFT FLOOR SUPPORT AT -Y965 AND FRAME 84. REPLACED THE FLOOR SUPPORT IAW DRAWING 170-65600-443.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FLOOR SUPPORT, FRAMES 12 AND 14, BETWEEN Y940 AND Y1016. REPLACED FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3.

Part: SUPPORT — CRACKED (FRAME 86) · airframe 20,422 hrs · 17,037 cycles

CRACK ON AFT MAIN CABIN LEFT PANEL SUPPORT AT -Y711 AND FRAME 86. REPLACED PANEL SUPPORT IAW DRAWING 170-65660-447.

Part: SUPPORT — CRACKED (FRAME 86) · airframe 20,422 hrs · 17,037 cycles

CRACK ON AFT MAIN CABIN RIGHT PANEL SUPPORT AT Y711 AND FRAME 86. REPLACE PANEL SUPPORT PER DWG 170-65660-447.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 20,422 hrs · 17,037 cycles

CORROSION ON AFT MAIN CABIN RIGHT HAND GUSSET AT Y584 AND FRAME 90. REPLACED GUSSET IAW DRAWING 170-60001-823.

Part: WINDOW — CRAZED (CABIN) · airframe 20,422 hrs · 17,037 cycles

CRAZED LEFT NR 1 WINDOW BETWEEN FRAMES 23 AND 24. REPLACED THE WINDOW IAW AMM 56-20-00.

Part: ROLLER — LACK OF LUBE (L1 DOOR) · airframe 19,506 hrs · 16,353 cycles

AIRCRAFT WAS NOT GROUNDED. 1L DOOR HARD TO OPEN AND CLOSE. MAINTENANCE PERFORMED LUBRICATION OF COMMAND RAMP AND ROLLERS PER AMM 53-10-21.

Part: ENGINE — VIBRATION (NR 1) · airframe 19,429 hrs · 16,302 cycles

AIRCRAFT WAS GROUNDED. FUMES AFTER TAKEOFF WITH SLIGHT ENGINE VIBRATION, SUSPECT NR 1 ENGINE. DIVERTED TO PHL DUE TO ODOR IN CABIN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. ACCOMPLISHED CABIN AIR QUALITY JOB CARD 43L00021001 AND CF34-10E6 ENGINE RELATED CABIN ODOR JOB CARD 43L00072001. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. MAINTENANCE COULD NOT DUPLICATE ISSUE.

Part: LENS — UNSECURE (CABIN) · airframe 18,865 hrs · 15,822 cycles

AIRCRAFT WAS NOT GROUNDED: AFT CENTER ISLE EMERGENCY EXIT LIGHT LENS UNSECURED. REPLACED EMERGENCY EXIT LIGHT LENS ON AFT CENTER ISLE AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 20-00-00.

Part: HANDLE — LACK OF LUBE (L2 DOOR) · airframe 18,824 hrs · 15,772 cycles

L2 DOOR HARD TO ARM & DISARM. LUBRICATED THE L2 DOOR ARM HANDLE AND ROD. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPIISHED.

Part: BRAKE — DIRTY (LT MLG) · airframe 18,445 hrs · 15,424 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT MAIN GEAR SMOKE. CLEANED NR 1 & NR 2 BRAKE ASSEMBLY AND INSPECTED PER AMM 32-49-11-210-801A WITH NO DEFECTS BEING NOTED.

Part: WINDOW — NOISY (COCKPIT) · airframe 18,272 hrs · 15,277 cycles

AIRCRAFT WAS GNDED. UNUSUALLY LOUD NOISE FROM CAPTAIN'S NR 1 WINDOW ON INITIAL CLIMB OUT. R & R WINDOW IAW TASK 56-11-00.

Part: LIGHT — CONTAMINATED (WING TO BODY)

LEFT AFT EMERGENCY LIGHT IN WING TO BODY FAIRING IS FULL OF MOISTURE. REMOVED LENS COVER, DRIED MOISTURE & REPLACED LENS IAW AMM 33-60-00.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

EXTERNAL MIDDLE EMER LIGHT ON THE LT FUSELAGE IS INOPERATIVE. REPLACED THE EMER LIGHT POWER UNIT NR 5.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

RIGHT EXTERNAL EMER LIGHTS ARE INOPERATIVE. REPLACED THE MID, RT POWER SUPPLY UNIT NR 3.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 16,217 hrs · 13,496 cycles

C3 CHECK, CORROSION ON FWD CARGO COMPARTMENT DOOR CUT OUT LOWER CTR SEAL REST. REPLACED SEAL REST IAW SRM 51-40-03 & 51-41-01.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 16,217 hrs · 13,496 cycles

C3 CHECK, RT WING LOWER SKIN PANEL CRACKED AT DRAIN HOLE AT RIB 10. REPAIRED RT WING LOWER SKIN PANEL CRACKED AT DRAIN HOLE AT RIB 10 IAW EA 506657.

Part: SPLICE — CORRODED (FRAMES 87-88) · airframe 16,217 hrs · 13,496 cycles

C3 CHECK, FOUND CORROSION ON SHEAR PANEL SPLICE BETWEEN FRAME 87 & 88 AT RBL 990.6. R & R SHEAR PANEL SPLICE IAW SRM 51-42-02 & 53-23-10.

Part: GUSSET — CORRODED (ZONE 200) · corrosion level 2 · airframe 16,217 hrs · 13,496 cycles

C3 CHECK, CORROSION ON AFT CABIN FLOOR STRUCTURE GUSSET AT FRAME 90 & +Y584.2. REPLACED GUSSET IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 90) · airframe 16,217 hrs · 13,496 cycles

C3 CHECK, CORROSION FOUND ON AFT MAIN CABIN FLOOR PANEL SUPPORT AT FRAME 90 LBL 838.2. R & R FLOOR PANEL SUPPORT IAW SRM 51-41-02 & 51-42-01.

Part: SHEAR PLATE — CORRODED (FRAMES 87-88) · airframe 16,217 hrs · 13,496 cycles

C3 CHECK, CORROSION FOUND ON SHEAR PLATE AT AFT ENTRY DOOR. R & R SHEAR PANEL IAW SRM 51-43-01 & TR 190-5300-11-056315.

Part: SHEAR PLATE — CORRODED (ZONE 200) · airframe 16,217 hrs · 13,496 cycles

C3 CHECK, CORROSION ON AFT ENTRY DOOR FLOOR SHEAR PANEL BETWEEN FRAME 86 & 87, BETWEEN +Y275MM & -Y275MM. REPLACED SHEAR PANEL IAW SRM 51-42-01.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,217 hrs · 13,496 cycles

C3 CHECK, FWD FLIGHT ATTENDANT FLASHLIGHT BATTERY INOPERATIVE. REPLACED BATTERY IAW AMM 33-51-01. ACCOMPLISHED A SUCCESSFUL OPERATIONAL CHECK IAW AMM 33-51-00.

Part: LANDING GEAR — MALFUNCTIONED (NLG) · airframe 16,216 hrs · 13,495 cycles

FLIGHT CREW REPORTED THAT NLG WOULD NOT EXTEND ON APPROACH. DECLARED AN EMER & ACFT LANDED WITH NLG IN UP POSITION. MLG LT & RT WAS EXTENDED. NO SIGNIFICANT INJURIES WITH PAXS OR CREW. MX ACTION PENDING.

Part: MECHANISM — INOPERATIVE (EVAC SLIDE) · airframe 15,274 hrs · 12,662 cycles

CREW REPORTS UNABLE TO DISARM R2 DOOR. R & R R2 DOOR EVACUATION SLIDE MECHANISM, REMOVED & INSTALLED SLIDE.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,832 hrs · 12,275 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: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,725 hrs · 12,178 cycles

RON FIRST OFFICER`S FIXED WINDSHIELD HAS MULTIPLE CRACKS & DELAMINATION ALONG THE UPPER EDGE 15 INCHES OTBD OF INNER CORNER. R & R WINDSHIELD IAW AMM 56-11-00400-801-A.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 13,673 hrs · 11,383 cycles

AFT RT FLASHLIGHT NEEDS TO BE REPLACED. REPLACED BATTERY & RESEALED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,505 hrs · 11,246 cycles

RT OVERWING EXIT IDENTIFIER LIGHT INOPERATIVE. R & R NR 3 ELPU.

Part: POWER UNIT — DEFECTIVE (CABIN) · airframe 10,921 hrs · 9,308 cycles

IFE MODIFICATION. RIGHT FORWARD EMERGENCY EXIT LIGHT BATTERY PACK (ABOVE R1 DOOR) WILL NOT HOLD A CHARGE. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT IAW E190 AMM 33-50-01-000-801-A & 33-50-01-400-801-A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK. MAIN CABIN FLOORBEAM CORRODED BETWEEN FR 12 & FR 17 AT Y 273 & Z -490. REMOVED AND REPLACED FLOORBEAM IAW STR 190-5300-11-0563A AND E190 SRM 51-43-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR87 TO FR88, Z490 & BETWEEN Y273 TO -Y273. REPLACED SHEAR PLATE BETWEEN FR87 TO FR88, Z480 & BETWEEN Y273 TO -Y273 IAW TYPICAL REPAIR TR-190-5300-11-0563A, EMBRAER SRM 51-42-01.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR87 TO FR88, Z490 & BETWEEN -Y1175 TO -Y273. REPLACED SHEAR PLATE BETWEEN FR87 TO FR88, Z480 & BETWEEN -Y1175 TO -Y273 IAW TYPICAL REPAIR TR-190-5300-11-0563A, EMBRAER SRM 51-42-02.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR WEB BETWEEN FR87 TO FR88, Z490 & BETWEEN -Y273 TO -Y1175. REPLACED SHEAR WEB BETWEEN FR87 TO FR88, Z480 & BETWEEN Y273 TO Y1310 IAW TYPICAL REPAIR TR-190-5300-11-0563A, EMBRAER SRM 51-43-01 & 51-42-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL FLOORBEAM BETWEEN FR85 TO FR87, Z490, -Y273. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR85 TO FR87, Z490, -Y273 IAW TYPICAL REPAIR TR-190-5300-11-0563A.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88, Z480 & BETWEEN Y273 TO Y1310. REPLACED SHEAR PANEL BETWEEN FR87 TO FR88, Z480 & BETWEEN Y273 TO Y1310 IAW TYPICAL REPAIR TR-190-5300-11-0563A, EMBRAER SRM 51-40-02 & 51-42-01.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON LEFT HAND FLOOR DOUBLER SILL PLATE BETWEEN FR13 TO FR16, Z-490 & BETWEEN Y269 TO Y338. REPLACED LEFT SILL PLATE BETWEEN FR13 TO FR16, Z-490 & BETWEEN Y269 TO Y338 IAW EMBRAER SRM 51-23-05, 51-23-06 & TYPICAL REPAIR TR190-5300-11-0563A.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD DOOR SILL BETWEEN FR12 TO FR14, Z490 & BETWEEN Y912 TO Y1380. REPLACED FORWARD DOOR SILL BETWEEN FR12 TO FR14, Z490 & BETWEEN Y912 TO Y1380 IAW EMBRAER SRM CHAPTER 51 STANDARD PRACTICES & TYPICAL REPAIR TR190-5300-11-0563.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD DOOR SILL AT FR16, Z490, Y1200. REPLACED FORWARD DOOR SILL AT FR16, Z490, Y1200 IAW TYPICAL REPAIR TR-190-5300-11-0563A.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,835 hrs · 9,227 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BEAM BETWEEN FR12 TO FR21, Z-490, -Y273. REPLACED SEAT TRACK BEAM BETWEEN FR12 TO FR21, Z-490, -Y273 IAW EMBRAER SRM 51-40-00 & TYPICAL REPAIR TR190-5300-11-0563A.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 10,231 hrs · 8,672 cycles

PHOTOLUMINESENT STRIP NEXT TO SEAT 1D DOES NOT ADHERE TO THE FLOOR. MAINTENANCE REMOVED AND REPLACED THE PHOTOLUMINESENT STRIP.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 9,848 hrs · 8,334 cycles

EMERGENCY LIGHT AT ROW 21 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LOWER EMERGENCY POWER UNIT. OPERATIONAL CHECK IS GOOD.

Part: PIN — UNSECURE (EVAC SLIDE) · airframe 9,319 hrs · 7,819 cycles

RDU - CORD HANGING FROM SLIDE PACK DOOR 1-L. RESTOWED MTC SAFETY PIN AS REQUIRED.

Part: BATTERY — DISCHARGED (CABIN)

BOS - RT EMERGENCY ESCAPE HATCH EXIT MARKER SIGN LIGHT OUT. MAINTENANCE REMOVED AND REPLACED ESCAPE HATCH EXIT MARKER SIGN EMERGENCY BATTERY IAW AMM 33-50-01.

Part: ROLL PIN — WORN (ENTRY DOOR) · airframe 9,101 hrs · 7,672 cycles

PHL - FWD ENTRY DOOR DOES NOT CLOSE PROPERLY. REPLACED ROLL PIN AT HOISTING MECHANISM ON FWD ENTRY DOOR.

Part: STRAP — BROKEN (DOOR) · airframe 8,867 hrs · 7,511 cycles

LGA - COCKPIT DOOR LOWER EMERGENCY STRAP BROKE. MAINTENANCE REPLACED COCKPIT LOWER STRAP, CHECKED OK.

Part: ENGINE — DIRTY (RIGHT) · airframe 8,000 hrs · 6,720 cycles

FLIGHT 1268, DFW - PHL - NOXIOUS FOUL ODOR IN AFT CABIN SHORTLY AFTER TAKEOFF RETURNED TO DFW AFTER LANDING AND DEPLANING THE ODOR PERSISTED IN THE AFT CABIN. MAINTENANCE ACCOMPLISHED RIGHT ENGINE CHANGE PER JC 43L40071001. NO ODORS NOTED ON ENGINE RUNS.

Part: AIR FILTER — DIRTY (CABIN)

PHL - FLT 1980 ATL TO PHL. SHORTLY AFTER TAKEOFF, FLIGHT ATTENDANT CALLED ABOUT STRONG ODOR, LIKE BURNING OIL SMELL, PRIMARILY IN AFT CABIN. NO ODOR NOTED IN COCKPIT. TURNED OFF NR 2 PACK AND SMELL DISSIPATED. MAINTENANCE REMOVED AND REPLACED THE RECIRCULATING AIR FILTERS.

Part: CABLE — BROKEN (L2 DOOR)

BOS - FLIGHT 2140 LANDED IN BOS AND CATERING WENT ON TO CLEAN THE AIRCRAFT THRU THE L2 DOOR. THE ARM/DISARM TELEFLEX CABLE WAS BROKEN AND THE L2 DOOR SLIDE PARTIALLY DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE TELEFLEX CABLE AND THE L2 SLIDE.

Part: WASHER — MISSING (R2 DOOR)

PHL - THE R2 DOOR SLIDE INDICATOR ON DOOR IS NOT SHOWING DISARMED ON GROUND, NEEDS TO BE ADJUSTED. MAINTENANCE FOUND A MISSING WASHER ON R2 DOOR FLAG LINKAGE, INSTALLED MISSING WASHER.

Part: LINKAGE — OUT OF ADJUST (R2 DOOR)

FLIGHT 1280, DFW-PHL - THE R2 DOOR ESCAPE SLIDE INDICATOR NOT SHOWING FULLY ARMED (RED) IN FLIGHT. AIRCRAFT RELEASED ON MEL. MAINTENANCE ADJUSTED LINKAGE THAT CONTROLS THE SLIDE INDICATOR, AC OKAY FOR SERVICE. MEL CLEARED.

Part: ACM — MALFUNCTIONED (AC BAY)

FLIGHT 867, PHL-PUJ - WHILE EN ROUTE TO PUJ, THE FLIGHT EXPERIENCED A STRONG AND PUNGENT BURNING ODOR IN THE CABIN AND THE COCKPIT. NO SMOKE WAS EVIDENT. O2 MASKS WERE DONNED AND QRH PROCEDURES WERE ACCOMPLISHED. THE ODOR DIMINISHED AFTER TURNING THE BLEED OFF. MAINTENANCE FOUND WATER IN SENSE LINE OF NR 2 PACK, PERFORMED OPERATIONAL CHECK AND FERRIED TO PHL. PHL MAINTENANCE TROUBLESHOT AND REPLACED THE LEFT AIR CYCLE MACHINE.

Part: PIN — DAMAGED (EVAC SLIDE)

PHL - THE AGENT HAD TROUBLE CLOSING THE MAIN CABIN DOOR, FOUND THE DOOR SLIDE DEACTIVATION PIN JAMMING THE DOOR AT FLOOR LEVEL. MAINTENANCE REMOVED THE PIN AND INSPECTED THE DOOR AREA. THE AIRCRAFT WAS RELEASED PER EA 115452 WITH PIN MISSING FROM L1 DOOR, INSTALLED PLACARD STATING PIN IS MISSING AND TO USE A PIN FROM ANOTHER LOCATION IF NECESSARY. PIN IS TO BE INSTALLED IN DOOR AND PLACARD REMOVED.

Part: SLIDE — DEFECTIVE (R2 DOOR) · airframe 5,763 hrs · 4,732 cycles

PIT - C1 - EES - DURING FUNCTIONAL CHECK PER JOB CARD 43T20025001, EMERGENCY LIGHTS FAILED TO ILLUMINATE ON SLIDE ASSEMBLY AT R-2 DOOR. ALL OTHER PARAMETERS OF FUNCTIONAL CHECK WERE SATISFACTORY. REPLACED R-2 DOOR SLIDE IAW EMBRAER AMM 25-65-01.

Part: COMPUTER — MALFUNCTIONED

FLIGHT 1833, PHL-MSP - ANTI ICE WING 2 WARNING, FUEL FEED 2 FAULT, SPDA FAIL, CARGO VENT FAIL ANNUNCIATED AT 8000 FT. THE CREW FOLLOWED QRH PROCEDURES, AN EMERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED FIM TASK 30-11-00-810-824-A, FAULT CODE DUE TO TRANSITORY CONDITION OF SPDA. FOUND FAULT CODE 24610015SP2 AND 24610043SP2. PERFORMED FIM TASK 24-61-00-810-882-A FAULT REMOVED "SPDA FAIL". FOUND FAULT CODE 28201252 FUEL FEED 2 FAULT, PERFORMED FIM TASK 28-21-00-810-815-A. FUEL FEED FAULT DID NOT RETURN, OK FOR CONTINUED SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

ATL - RIGHT AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY.

Part: MODULE — BURNED (EXTERNAL POWER)

FLIGHT 1146, RDU-PHL - THE CREW RECEIVED IDG 2 BUS EICAS MESSAGE DURING FLIGHT. THE MESSAGE WAS CLEARED BY FOLLOWING THE QRH PROCEDURES. AFTER PARKING AT THE GATE THE CREW NOTICED A STRONG ELECTRICAL ODOR AND SLIGHT HAZE. MAINTENANCE PERSONNEL FOUND THE EXTERNAL POWER MODULE BURNT. THE EXTERNAL POWER MODULE WAS REPLACED AND THE RIGHT ENGINE INTEGRATED DRIVE GENERATOR.