N950UW

Part: CONTROL LEVER — FAULTY (MLG) · airframe 23,925 hrs · 19,934 cycles

AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AND THERE WAS NO EICAS MESSAGES. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT, THE AIRCRAFT WAS GROUNDED. REPLACED LANDING GEAR CONTROL LEVER ASSEMBLY IAW AMM 32-33-01. OPS CHECKED GOOD, CYCLED GEAR TWICE, NO FAULTS NOTED IAW 32-33-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,534 hrs · 19,634 cycles

TWO SECTIONS OF THE EMERGENCY LIGHT WOULD NOT ILLUMINATE IN THE FIRST CLASS SECTION. MAINTENANCE REPLACED BOTH SECTIONS OF THE DAMAGED EMERGENCY LIGHT STRIP IAW AMM 33-50-21, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: LEVER — LACK OF LUBE (R2 DOOR) · airframe 23,425 hrs · 19,536 cycles

R2 SERVICE DOOR ARMING LEVER WOULD NOT MOVE WHEN ATTEMPTING TO ARM DOOR. CHECKED RIGGING, AIRCRAFT WAS GROUNDED. LUBED AND ADJUSTED AFT RIGHT SERVICE DOOR EMERGENCY EVACUATION SLIDE MECHANISM IAW AMM 52-42-40-820. AFT RIGHT SERVICE DOOR OPERATES NORMAL.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 22,953 hrs · 19,153 cycles

AFT RIGHT FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT INDICATOR NOT FLASHING. REPLACED THE BATTERY IAW J/C 43C20025001.

Part: SIGN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 22,751 hrs · 18,988 cycles

RIGHT FORWARD SERVICE DOOR, EMERGENCY EXIT SIGN NOT WORKING PROPERLY. REPLACED THE SIGN. THE AIRCRAFT WAS GROUNDED.

Part: SKIN — CRACKED (RT WING) · airframe 21,049 hrs · 17,651 cycles

TWO CRACKS ON THE RIGHT WING LOWER SKIN PANEL DRAIN HOLE. REPAIRED THE SKIN PANEL IAW EA 257882A.

Part: NUT — DAMAGED (DOOR SLIDE) · airframe 5,796 hrs · 4,747 cycles

FORWARD PASSENGER DOOR EMERGENCY EVACUATION SLIDE FORWARD INSULATOR NUT IS DAMAGED. REPLACED FORWARD PASSENGER DOOR EMERGENCY EVACUATION SLIDE FORWARD INSULATOR NUT. AIRCRAFT WAS GROUNDED.

Part: SCREW — DAMAGED (DOOR SLIDE) · airframe 5,796 hrs · 4,747 cycles

AFT SERVICE DOOR SLIDE PACKBOARD ATTACH SERVICE SCREW IS DAMAGED. REPLACED AFT SERVICE DOOR SLIDE PACKBOARD SCREW. AIRCRAFT WAS GROUNDED.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 5,796 hrs · 4,747 cycles

MAIN CABIN R2 DOOR SURROUND PANEL EXIT LIGHT LENS IS BROKEN. REPLACED THE LENS. AIRCRAFT WAS GROUNDED.

Part: FITTING — GOUGED (DOOR SLIDE) · airframe 5,796 hrs · 4,747 cycles

AFT PASSENGER DOOR FORWARD EVACUATION SLIDE FITTING IS GOUGED. BLENDED THE FITTING. AIRCRAFT WAS GROUNDED.

Part: FLAP — CRACKED (RT WING) · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND WING TRAILING EDGE INBOARD AFT FLAP BETWEEN RIB 10A AND 12A. REPAIRED RIGHT FLAP ASSEMBLY PER EA 269993.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 5,796 hrs · 4,747 cycles

MAIN CABIN L2 DOOR SURROUND PANEL EXIT LIGHT LENS IS BROKEN. REPLACED THE LENS. AIRCRAFT WAS GROUNDED.

Part: SEAT TRACK — CORRODED (FRAMES 43-50) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON RIGHT MAIN CABIN INBOARD SEAT TRACK AT Y270 BETWEEN FRAMES 43 AND 50, UPPER SECTION OF TRACK. REPLACED THE SEAT TRACK IAW SRM 53-00-10, REPAIR 51, AND DRAWING 190-22607-475.

Part: NUT — DAMAGED (SERVICE DOOR) · airframe 5,796 hrs · 4,747 cycles

FORWARD SERVICE DOOR EMERGENCY EVACUATION SLIDE FORWARD INSULATOR NUT IS DAMAGED. REPLACED THE FORWARD INSULATOR NUT ON THE FORWARD SERVICE DOOR EMERGENCY EVACUATION SLIDE.

Part: NUT — DAMAGED (DOOR SLIDE) · airframe 21,049 hrs · 17,651 cycles

AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE RAFT INSULATOR NUT DAMAGED. REPLACED 1EA ISOLATOR ON AFT SERVICE DOOR EMERGENCY EVACUATION SLIDE RAFT. AIRCRAFT WAS GROUNDED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y292 BETWEEN FR 83.5 AND FR 85. REPAIRED SEAT TRACK PER SRM 53-23-10, 53-00-10 REPAIR 51, AND DRAWING 170-65600-441.

Part: DAMPER — CORRODED (SERVICE DOOR) · airframe 21,049 hrs · 17,651 cycles

FORWARD SERVICE DOOR DAMPER HAS CORROSION. REPLACED FORWARD SERVICE DOOR DAMPER. AIRCRAFT WAS GROUNDED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR SEAT TRACK AT Y292 BETWEEN FR 78 AND FR 81. REPAIRED SEAT TRACK PER SRM 53-23-10, REPAIR 51 AND DRAWING 170-65600-441.

Part: FLOORBEAM — CORRODED (FRAME 11) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON COCKPIT FLOORBEAM, FRAME 11 BETWEEN LBL 12 AND RBL 9. REPAIRED THE FLOORBEAM IAW EA 269659, 506660A, AND 269655.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 21,049 hrs · 17,651 cycles

CRACK ON LT WING LOWER SKIN PANEL DRAIN HOLE. REPAIRED THE SKIN PANEL IAW EA 257829.

Part: DOUBLER — CORRODED (FRM 11 FLOOR) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON COCKPIT FLOOR STRUCTURE DOUBLER CONNECTOR AT FR 11. REPLACED DOUBLER IAW SRM 51-40-02, 51-40-03, 51-41-02, AND DWG 170-00825-503.

Part: LENS — DAMAGED (EXIT SIGN) · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. MAIN CABIN LOWER CEILING PANEL EXIT SIGN COVER DAMAGED. REPLACED MAIN CABIN LOWER CEILING PANEL 253CLG EXIT SIGN LENS.

Part: SEAT TRACK — CORRODED (FRAMES 65-66) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT MAIN CABIN LEFT INBOARD SEAT TRACK, -Y260, FRAMES 65 & 66. REPLACED THE SEAT TRACK IAW SRM 51-43-01/-02, 51-41-01, 51-40-02-03, AND DWG 25441-005.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT, Y340 BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW SRM 51-75-16, 51-41-02, 51-43-03, 51-43-04, 51-10-10, 51-31-00, AND DWG 170-07304-002.

Part: SEAT TRACK — CORRODED (FRAMES 17-20) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

FOUND CORROSION ON THE FORWARD MAIN CABIN LEFT SEAT TRACK, -Y260 BETWEEN FRAMES 17 & 20. REPLACED THE SEAT TRACK IAW 53-00-00-3, REPAIR 3, SRM 51-41-01, AND 51-41-03.

Part: ANGLE — CORRODED (FRM 17 FLOORBEAM) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOORBEAM ANGLE AT Y340 AND FR 17. REPAIRED THE FLOORBEAM ANGLE IAW SRM 51-75-16, 51-31-00, 51-40-03, 51-41-02, 51-43-03, 51-43-04, AND DWG 170-00822-505.

Part: DOUBLER — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR DOUBLER AT -Y345 BETWEEN FRAMES 15 AND 16. REPLACED THE DOUBLER IAW 53-00-00, REPAIR 3, SRM 51-12-01, 51-10-03, 51-41-02, AND 51-40-02.

Part: SEAT TRACK — CORRODED (FRAMES 20-33) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON RIGHT FORWARD MAIN CABIN SEAT TRACK AT Y280 BETWEEN FRAMES 20 AND 33. REPLACED THE SEAT TRACK IAW SRM 51-43-03, SRM 51-43-02, AND DWG 170-67120-437.

Part: SPLICE PLATE — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT SERVICE DOOR SPLICE PLATE ATTACHED TO MACHINED HORIZONTAL BEAM AT Y1143 BETWEEN FRAMES 84 & 85. REPLACED THE SPLICE PLATE IAW SRM 51-42-02, AND DRAWING 190-65293-001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT FR 84 BETWEEN Y317 AND Y1143. REPLACED FLOOR SUPPORT PER DRAWING 190-65140-801, SRM 51-41-01, 51-41-02 AND 51-43-02.

Part: SEAT TRACK — CORRODED (FRAMES 81-84) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON LEFT, AFT MAIN CABIN FLOOR SEAT TRACK AT -Y292 BETWEEN FRAMES 81.5 & 84. REPAIRED THE SEAT TRACK IAW SRM 53-00-10, AND SRM 53-23-10.

Part: ROLLER — FROZEN (EMEGENCY EXIT) · airframe 21,049 hrs · 17,651 cycles

LEFT WING EMERGENCY DOOR CUTOUT, FORWARD UPPER ROLLER IS FROZEN. CLEANED EXIT DOOR CUTOUT FORWARD UPPER ROLLER IAW AMM 12-22-01.

Part: FLOORBEAM — CORRODED (FRAME 19) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOORBEAM FITTING AT FRAME 19, Y-1140, Z-490. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-03, SRM 51-43-03, AND DRAWING 170-00822-413.

Part: ROLLER — FROZEN (EMERGENCY DOOR) · airframe 21,049 hrs · 17,651 cycles

RIGHT WING EMERGENCY EXIT DOOR CUT OUT, TOP FORWARD ROLLER IS FROZEN. CLEANED EXIT DOOR CUTOUT FORWARD ROLLER IAW AMM 12-22-01.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR SPLICE AT -Y101 AND FR 90. REPLACED FLOOR SPLICE PER SRM 51-10-03, 51-12-01, 51-43-03, 51-40-02, 51-40-03 AND DRAWING 170-65660-447.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND FORWARD MAIN CABIN FLOOR SILL AT -Y1110 BETWEEN FR 12 AND FR 13. REPLACED SILL PER SRM 51-43-04, SRM 51-41-02 AND 53-00-00-3 REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CABIN RIGHT HAND FLOOR TRACK AT Y280 BETWEEN FR12 AND FR 18. REPLACED SEAT TRACK PER AARD 53-00-00-3 REPAIR 3, SRM 51-41-01, 51-41-02, 51-43-03 AND 51-43-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON CENTER MAIN CABIN UPPER SECTION OF SEAT TRACK AT Y271 AND FR 39. REPLACED SEAT TRACK PER SRM 51-43-03,51-43-04,51-40-02 AND DRAWING 190-23017-405.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOOR BEAM AT -Y345 BETWEEN FR 12 AND FR 13. REPLACED FLOOR BEAM PER DRAWING 170-00822-503, SRM 51-41-01, 51-41-02 AND 51-41-03.

Part: CROSSBEAM — DAMAGED (FUSELAGE) · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. ELONGATED HOLES ON FORWARD MAIN CABIN CROSSBEAM AT FR 14 BETWEEN -Y790 AND -Y915. REPAIRED CROSSBEAM PER SRM 53-00-10.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR PANEL SUPPORT AT Y914 AND FR 89. REPLACED FLOOR SUPPORT PER AARD 53-00-00-3 REPAIR 3, SRM 51-41-02 AND 51-43-03.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT MAIN CABIN GALLEY FLOOR SUPPORT AT -Y355 AND FRAME 84. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-03, AND DWG 170-65600-445.

Part: FLOOR SUPPORT — CORRODED (FRAME 86) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT Y723 AND FRAME 86. REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, AND DWG 170-65660-441.

Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y730 AND FRAME 17. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, 51-40-03, 51-41-01 AND DWG 170-00822-505.

Part: FLOOR SUPPORT — CORRODED (FRAME 14) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT AT Y730 AND FRAME 14. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, 51-40-03, 51-41-01, AND DWG 170-00822-505.

Part: FLOOR SUPPORT — CORRODED (FRAME 88) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT -Y711 AND FRAME 88. REPLACED PANEL SUPPORT IAW SRM 51-41-01, AND DWG 170-65660-441.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN GALLEY FLOOR SUPPORT AT -Y977 AND FRAME 84. REPLACED THE FLOOR SUPPORT IAW SRM 51-43-03, AND DWG 170-65660-441.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT -Y1143 AND FRAME 84. REPLACED FLOOR PANEL SUPPORT IAW SRM 51-41-01, SRM 51-41-02, AND DRAWING 170-66000-445.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT Y365 BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT SRM 51-41-01, AND DRAWING 190-05555-805.

Part: FLOOR SUPPORT — CORRODED (FRAME 90) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT MAIN CABIN FLOOR SUPPORT AT -Y800 AND FRAME 90. REPLACED FLOOR SUPPORT IAW SRM 51-41-01, 51-41-02, 51-43-03, 51-42-01, AND DWG 170-66000-457.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-13) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT BETWEEN FRAMES 12 AND 13. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3, SRM 51-41-02, AND SRM 51-43-04.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT MAIN CABIN FLOOR STRUCTURE SHEAR PANEL AT -Y88 BETWEEN FRAMES 87 AND 88. REPLACED THE SHEAR PANEL IAW 53-00-00-3, REPAIR 3, SRM 51-42-02, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON RIGHT FORWARD MAIN CABIN FLOOR SUPPORT AT Y1090 BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3, REPAIR 3, SRM 51-41-02, 51-43-03, AND 51-40-02.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON AFT MAIN CABIN SHEAR PANEL BETWEEN FRAMES 87 AND 88. REPLACED THE SHEAR PANEL IAW 53-00-00-3 REPAIR 3, SRM 51-42-02, AND SRM 51-40-02.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR SPLICE AT -Y1016 BETWEEN FR 87 AND FR 88. REPLACED SPLICE PER AARD 53-00-00-3 REPAIR 3, SRM 51-42-02, 51-40-02 AND 51-40-04.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR GUSSET Y291 AND FR 90. REPLACED GUSSET PER SRM 51-41-02, 51-40-03, AND DRAWING 170-60001-823.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR GUSSET AT Y546 AND FR 90. REPLACE GUSSET PER SRM 51-40-02, 51-40-03, 51-41-02 AND DRAWING 170-60001-823.

Part: MOUNT — CORRODED (FRAME 16) · corrosion level 2 · airframe 21,049 hrs · 17,651 cycles

CORROSION ON FORWARD MAIN CABIN FLOOR SUPPORT MOUNT AT Y1141 AND FRAME 16. REPLACED FLOOR SUPPORT IAW SRM 51-43-03, AND DRAWING 170-21768-407.

Part: LIGHT — DETACHED (SEAT 1D) · airframe 20,733 hrs · 17,413 cycles

DETACHED EMERGENCY LIGHT STRIP AT SEAT 1D. MAINTENANCE SECURED THE LIGHT STRIP IAW AMM 33-50-21.

Part: CONTROL MODULE — FAULTY (BRAKE SYSTEM) · airframe 20,726 hrs · 17,407 cycles

AIRCRAFT WAS GROUNDED. DURING FLIGHT, LEFT HAND AND RIGHT HAND BRAKE FAULT ADVISORY EICAS MESSAGE ILLUMINATED AND CLEARED WITHOUT PILOT INPUT. MAINTENANCE REPLACED NR 1 BRAKE CONTROL MODULE PER AMM 32-41-07 AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK PER AMM 32-41-00.

Part: LIGHT — MISSING (CABIN) · airframe 20,624 hrs · 17,329 cycles

MISSING SEGMENT OF THE EMERGENCY LIGHT STRIP IN FORWARD CABIN AT SEAT 1D. MAINTENANCE REPLACED THE LIGHT IAW AMM 30-50-21.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 20,150 hrs · 16,980 cycles

R2 DOOR ASSIST BOTTLE LOW PSI. ACCOMPLISHED R2 DOOR ASSIST BOTTLE SERVICING IAW AMM 52-4251-200-802-A GOOD TO CONTINUE SERVICE. NO LEAKS FOUND. THE AIRCRAFT WAS NOT GROUNDED.

Part: ENGINE — ODOR (NR 1) · airframe 18,817 hrs · 15,777 cycles

RETURNED, ACFT WAS GNDED. RT AFTER ROTATION, THE CREW NOTED A STRONG SMELL OF BURNING OIL & HAD SMOKE IN THE COCKPIT. THE CREW OXYGEN MASKS WERE USED IN THE COCKPIT ONLY SINCE THERE WAS NO SMOKE & ONLY AN ODOR IN THE CABIN. DECLARED AN EMER & THE ACT RETURNED WHERE IT LANDED SAFELY WITH NO FURTHER INCIDENTS. PERFORMED CABIN AIR QUALITY TROUBLESHOOTING IAW JC 43L00021001 & NR 1 ENG DETERMINED TO BE THE SOURCE OF ODOR. ENG WATER WASH PREVIOUSLY ACCOMPLISHED PRIOR TO FLIGHT & PERFORMED AMS SYS DRY OUT IAW EMM 72-00-00-100-801. NO FURTHER SMELLS NOTED, OK FOR SERVICE.

Part: CYLINDER — LOW PRESSURE (L2 DOOR) · airframe 18,219 hrs · 15,265 cycles

AIRCRAFT WAS NOT GNDED. DOOR 2L CHECK DOOR PRESS ILLUMINATED ON CIDS PANEL. SERVICED 2L DOOR CYLINDER IAW AMM 52-10-00.

Part: LINER — SEPARATED (EMERGENCY EXIT) · airframe 17,775 hrs · 14,840 cycles

FLIGHT 1775 RT OVERWING EXIT DOOR LINER IS SEPARATED. REPAIRED RT OVERWING EXIT DOOR LINER IAW DWG DATA 190-90061-401 FOR 3 SEPARATED BRACKETS. R & R RT OVERWING EXIT DOOR IAW AMM 52-21-00.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, RT EXTERNAL FWD FUSELAGE REPAIR DOUBLER FASTENERS PULLING THROUGH FASTENERS. REMOVED DOUBLERS, INSPECTED & ACCOMPLISHED INTERIM REPAIR INSTRUCTIONS IAW EA 506663.

Part: LENS — CRACKED (EXIT SIGN) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, RT LOWER OVERWING EMER LIGHT EXIT SIGN LENS CRACKED. R & R RT LOWER OVERWING EMER LIGHT. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00-710-801-A.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, MAIN CABIN PHOTO LUMINESCENT STRIPS HAS MORE THAN 10% DAMAGED. R & R AT MAIN CABIN PHOTO LUMINESCENT STRIPS IAW AMM 33-50-21.

Part: INDICATOR — BROKEN (EVAC SLIDE) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, L2 AFT PAX DOOR SLIDE MECHANISM BELL CRANK VISUAL INDICATOR IS BROKEN. REPLACED BELL CRANK VISUAL INDICATOR.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, COCKPIT FLOOR CROSSBEAM HAS CORROSION AT FRAME 11 & RBL 3 - RBL 10. REMOVED BY BLENDING & DRILLING, PLUGGING 2 HOLES AT DEEPEST AREA IAW EA 506660.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, RT CABIN FLOOR SHEAR PANEL FOUND WITH CORROSION. R & R SHEAR PANEL IAW SRM 51-42-01 & SRM 51-42-02.

Part: BEAM — CORRODED (FUSELAGE) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, FWD CARGO DOOR SURROUND STRUCTURE LOWER BEAM HAS CORROSION ON OTBD FACE AT FWD LATCH FITTING. R & R LOWER BEAM IAW SRM 51-43-04 PAGE 1 - 6.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, AFT CARGO COMPARTMENT SHEAR CLIP HAS CORROSION. R & R SHEAR CLIP IAW SRM 51-41-01 PAGES 1 - 6.

Part: MECHANISM — DIRTY (EMERGENCY EXIT) · airframe 16,613 hrs · 13,733 cycles

RIGHT EMER ESCAPE HATCH LATCH MECHANISM HAS NO RESISTANCE WHEN OPENING OR CLOSING DOOR. CLEANED RT OVERWING ESCAPE HATCH DOOR LATCH MECHANISM. FOUND NO DISCREPANCY & NO FURTHER ACTION REQUIRED IAW AMM 12-22-00 & 51-21-20.

Part: LIGHT — CONTAMINATED (EXTERIOR) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, LOWER EMER LIGHT ASSEMBLY HAS WATER INTRUSION AT WING TO BODY FAIRING PANEL 199ML. REMOVED, CLEANED & REINSTALLED LOWER EMER LIGHT ASSEMBLY AT FAIRING PANEL 199ML IAW AMM 33-50-25-400-802-A 400.

Part: LENS — DIRTY (EXTERIOR LIGHT) · airframe 16,613 hrs · 13,733 cycles

UPPER EMER LIGHT LENS FOGGED AT WING TO BODY FAIRING PANEL 198NR. REMOVED, CLEANED & REINSTALLED UPPER EMER LIGHT LENS AT FAIRING PANEL 198NR IAW AMM 33-50-25-400-802-A400.

Part: MECHANISM — DIRTY (EMERGENCY EXIT) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, LT EMER ESCAPE HATCH LATCH MECHANISM IS HARD TO CLOSE. CLEANED LT OVERWING ESCAPE HATCH DOOR LOCK MECHANISM. FOUND NO DISCREPANCY. NO FURTHER ACTION REQUIRED IAW AMM 12-22-00 & 51-21-20.

Part: LIGHT — CONTAMINATED (EXTERIOR) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, LOWER EMER LIGHT ASSEMBLY HAS WATER INTRUSION AT FAIRING 198NR. REMOVED, CLEANED & REINSTALLED LOWER EMER LIGHT ASSEMBLY IAW AMM 33-50-25-400-802-A 400.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, VERTICAL STAB REAR SPAR RIB 9 & 10 TE CRACKED. R & R RIB 9 & 10 IAW EA 106515 & DWG 170-63629-005.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, CTR CABIN FLOOR SHEAR PANEL WAS FOUND CORRODED. R & R SHEAR PANEL IAW REPAIR 190-5300-11-0563B FIGURE 2 & SRM 51-40-02.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 16,613 hrs · 13,733 cycles

C3 CHECK, FWD CARGO DOOR SURROUND STRUCTURE DOUBLER ON LOWER BEAM IS GOUGED & HAS CORROSION. R & R DOUBLER IAW SRM 51-43-04.

Part: LINK — LOOSE (RT PYLON) · airframe 15,205 hrs · 12,503 cycles

RT PYLON INBD LOWER LINK FITTING ASSEMBLY FOUND LOOSE. TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 15,205 hrs · 12,503 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 (LT PYLON) · airframe 15,205 hrs · 12,503 cycles

RON, DURING ACCOMPLISHMENT OF EO 5414P124 THE LT 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 15,205 hrs · 12,503 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: COVER — MISSING (EXIT SIGN) · airframe 15,018 hrs · 12,339 cycles

EXIT SIGN AT ROW 12 ON OVERHEAD MISSING EXIT SIGN LIGHT COVER. MX REPLACED LENS COVER ON EXIT SIGN NOW OK.

Part: PRESSURE SWITCH — FAULTY (BRAKE SYSTEM) · airframe 14,844 hrs · 12,196 cycles

FLIGHT 2161, BOS - LGA. CAPTAIN ADVISED DISPATCH HE WAS DIVERTING TO JFK DUE TO A PARKING BRAKE MSG. THE CAPTAIN DECLARED AN EMERGENCY & THE FLIGHT LANDED UNEVENTFULLY. REPLACED THE NR 2 HYD SYS EMERGENCY BRAKE PRESS SWITCH.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 14,243 hrs · 11,737 cycles

FOWARD FLIGHT ATTENDANT FLASHLIGHT DOES NOT INDICATE CHARGING. R & R FWD FLIGHT ATTENDANT FLASHLIGHT BATTERY.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 12,871 hrs · 10,710 cycles

SMALL STRIP APPROX 12 TO 14" OF PHOTOLUMINESENT EMERGENCY EXIT LIGHTING MISSING ON FLOOR IN FIRST CLASS SEATING AREA. MX R & R LUMINENESENT STRIP AT FIRST CLASS 1D, F.

Part: SENSOR — INOPERATIVE (LE SLAT) · airframe 12,179 hrs · 10,180 cycles

FLIGHT 1845, BOS-PHL - THE PILOT REPORTED "HAD SLAT FAIL MESSAGE IN CRUISE. ZERO SLATS AND 2 DEGREE FLAPS ON LANDING. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD SLAT SKEW SENSOR (S2/3). OPERATIONAL CHECK IS GOOD.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 11,712 hrs · 9,869 cycles

PIT - SAF-T-GLO STRIP LOOSE FROM FLOOR SEAT 1D. RE-ATTACHED TO FLOOR PHOTO LUMINESCENT STRIP LIGHT AT SEAT 1D.

Part: LIGHT — LOOSE (CABIN) · airframe 10,916 hrs · 9,272 cycles

ILLUMINATION STRIP LOOSE AT ROW 1. MAINTENANCE SECURED STRIP, OKAY FOR SERVICE.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SPLICE PLATE AT FR90, Z-490, -Y273. REPLACED SPLICE PLATE AT FR90, Z-490, -Y273 IAW EMBRAER SRM 51-41-02.

Part: SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON SPLICE AT FR89, -Z490, Y273. REPLACED SPLICE AT FR89, -Z490, Y273 IAW TYPICAL REPAIR 190-5300-11-0563A.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SPLICE PLATE AT FR90, Z-490, -Y507. REPLACED SPLICE PLATE AT FR90, Z-490, -Y507 IAW EMBRAER SRM 51-41-02.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - SURFACE CORROSION ON SHEAR PLATE AT FR84, -Z490, BETWEEN Y273 TO Y1310. REPLACED SHEAR PLATE AT FR84, -Z490 IAW E190 SRM 51-41-02, 51-43-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON WEB FR87, S17R, -X490, BETWEEN -Y1310 TO -Y273. REPLACED WEB FR87, S17R, -X490, BETWEEN -Y1310 TO -Y273 IAW TYPICAL REPAIR 190-5300-11-0563A.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON FLOOR SUPPORT BETWEEN FR85 TO FR87, -Z490, Y273. REPLACED FLOOR SUPPORT BETWEEN FR85 TO FR87, -Z490, Y273 IAW TYPICAL REPAIR 190-5300-11-0563A.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON GUSSET PLATE AT FR90, -Z490, Y273. REPLACED GUSSET PLATE AT FR90, -Z490, Y273 IAW E190 SRM 51-41-02.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON WEB AT FR87, S17L, -Z490,-Y1310. REPLACED WEB AT FR87, S17L, -Z490, Y1310 IAW TYPICAL REPAIR 190-5300-11-0563A.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR85 TO FR89, -Z495, -Y273. REPLACED SHEAR PANEL BETWEEN FR85 TO FR89, -Z495, -Y273 IAW E190 SRM 51-23-04 AND 51-23-05.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON SHEAR PANEL AT FR87, -Z490, BETWEEN Y273 TO -Y273. REPLACED SHEAR PANEL AT FR87, -Z490, BETWEEN Y273 TO -Y273 IAW TYPICAL REPAIR 190-5300-11-0563A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR12 TO FR20, -Z490, Y273. REPLACED FLOORBEAM BETWEEN FR12 TO FR20, -Z490, Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR12 TO FR20, -Z490, Y273. REPLACED FLOORBEAM BETWEEN FR12 TO FR20, -Z490, Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR18, Z-490, -Y273. REPLACED FLOORBEAM AT FR18, Z-490, -Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR12 TO FR16, -Z490, -Y1380. REPLACED SHEAR PLATE BETWEEN FR12 TO FR16, -Z490, -Y1380 IAW E190 SRM 51-41-02, 51-43-02.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - EXFOLIATION CORROSION ON DOUBLER AT FR16, -Z490, BETWEEN -Y275 TO -Y745. REPLACED DOUBLER AT FR16, -Z490, BETWEEN -Y275 TO -Y745 IAW TYPICAL REPAIR 190-5300-11-0563A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR12 TO FR20, Z-490, Y273. REPLACED FLOORBEAM BETWEEN FR12 TO FR20, Z-490, Y273 IAW TYPICAL REPAIR TR190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR17, Z-490, -Y273. REPLACED FLOORBEAM AT FR17, Z-490, -Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, Z-490, -Y273. REPLACED FLOORBEAM AT FR16, Z-490, -Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR12 TO FR20, -Z490, Y273. REPLACED FLOORBEAM BETWEEN FR12 TO FR20, -Z490, Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - SURFACE CORROSION ON SHEAR PLATE BETWEEN FR12 TO FR14, -Z490, Y1100. REPLACED SHEAR PLATE BETWEEN FR12 TO FR14, -Z490, Y1100 IAW TYPICAL REPAIR 190-5300-11-0563 AND E190 SRM 51-41-02, 51-43-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR19, Z-490, -Y273. REPLACED FLOORBEAM AT FR19, Z-490, -Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - CORROSION ON FLOORBEAM BETWEEN FR12 TO FR20, -Z490, Y273. REPLACED FLOORBEAM BETWEEN FR12 TO FR20, -Z490, Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,785 hrs · 9,164 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR15, Z-490, -Y273. REPLACED FLOORBEAM AT FR15, Z-490, -Y273 IAW TYPICAL REPAIR 190-5300-11-0563.

Part: ACM — LEAKING (AC BAY)

FLT 2140 EN ROUTE. OILY AIR DURING INITIAL CLIMB. MAINTENANCE REMOVED AND REPLACED NR 2 AIR CYCLE MACHINE.

Part: SLIDE — PARTIAL DEPLOY (L1 DOOR) · airframe 8,875 hrs · 7,506 cycles

FLIGHT 2041, BOS-DCA - AFTER GATE ARRIVAL-L1 SLIDE PARTIALLY DEPLOYED. MAINTENANCE ACCOMPLISHED REMOVAL AND INSTALLATION OF L-1 DOOR EVAC SLIDE AND ASSIST BOTTLE DIAPHRAGM PER AMM 25-65-01-400 08-1-A AND AMM 25-65-01-200-800-A/600.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 8,582 hrs · 7,285 cycles

BOS - AFT FLIGHT ATTENDANT BREAK AWAY FLASHLIGHT INOP. MAINTENANCE REPLACED EMERGENCY FLASHLIGHT BAT & STRAP. CHECKS OK.

Part: CONTROL VALVE — MALFUNCTIONED (BRAKE SYSTEM) · airframe 8,510 hrs · 7,215 cycles

FLIGHT 1759, PHL - RDU - ON APPROACH INTO RDU WHEN LANDING GEAR WAS EXTENDED A LEFT AND RIGHT BRAKE FAULT WAS RECEIVED. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAIN BRAKE CONTROL VALVE PER AMM 32-41-09-400. BRAKE SYSTEM BLED, OPERATIONAL CHECK IS SATISFACTORY PER AMM 32-41-00710-801.

Part: SEAT — LOOSE (COCKPIT) · airframe 8,430 hrs · 7,158 cycles

PIT - F/O'S SEAT SLIDES LEFT AND RIGHT REGARDLESS OF FWD AND AFT POSITION. ALSO FWD AND AFT TRACK HARD TO MOVE, NEEDS TO BE LUBRICATED. MAINTENANCE REMOVED AND REPLACED F/O SEAT PER AMM 25-11-01-*400-801A, CHECKS OK.

Part: ENGINE — ODOR (LEFT)

FLIGHT 2140, CABIN ODOR ON TAKEOFF. REMOVED AND REPLACED THE LEFT ENGINE. RAN THE ENGINE WITH NO ODORS IN FLIGHT DECK.

Part: SLIDE — PARTIAL DEPLOY (CABIN)

FLIGHT 9244, PIT - BOS, FERRY FLIGHT - ON ARRIVAL THE CAPTAIN NOTICED THE DOOR DID NOT FEEL CORRECTLY WHEN THEY TRIED TO OPEN IT, HE STOPPED AND CALLED MAINTENANCE WHO ENTERED THE AIRCRAFT FROM THE REAR DOOR. THE SLIDE WAS FOUND TO HAVE PARTIALLY DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE PER AMM 25-65-01-000-801A AND 25-65-01-400-801A.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT 1268, DFW - PHL - DURING TAKEOFF, CLIMB, AND DESCENT ODOR OF OVERHEATED PLASTIC DETECTED. ODOR NOTICED BY BOTH PILOTS, FLIGHT ATTENDANTS, AND A MAINTENANCE SUPERVISOR WHO WAS SEATED MID CABIN. THE PILOTS AND FLIGHT ATTENDANTS REPORTED EXPERIENCING MILD EYE IRRITATION. MAINTENANCE OPERATED BOTH PACKS OFF APU AIR WITH NO ODORS DETECTED. OPERATED ALL ELEC SYSTEMS WITH NO DEFECTS NOTED. TWO SUCCESSFUL TEST FLIGHTS HAVE BEEN PERFORMED WITH NO ODORS NOTICED.

Part: DUCT — DIRTY (CABIN AIR)

FLIGHT 1720, FLIGHT CREW REPORTED DIRTY, MUSTY ODOR ON TAKE OFF THRU CLIMB. MAINTENANCE ACCOMPLISHED RECIRCULATION DUCT CLEANING PER AMM 21-24-03-110-801-A. OPERATIONAL CHECK IS SATISFACTORY.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT 715, PHL-BOS - REPORTED ON JUNE 1; INTERMITTENT STRONG DIRTY SOCK ODOR FROM PACKS, MOST EVIDENT ON GROUND AND DEPARTURE. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT ON JUNE 3RD FOR LIGHTENING STRIKE MAINTENANCE AND CABIN AIR QUALITY CHECK. DURING CABIN AIR QUALITY CHECK ON JUNE 3 APU FOUND AS SOURCE OF CABIN ODOR AND PLACED ON MEL. CABIN AIR QUALITY TASK ACCOMPLISHED AND LEAK CHECK OF AIRPACKS, NO LEAKS NOTED. ACCOMPLISHED BAAT PROCEDURE, THE FILTERS SENT FOR ANALYSIS. THE RESULTS OF THE BAAT TEST WERE FOUND TO BE NEGATIVE. THE APU CAN BE RETURNED TO SERVICE AT THIS TIME.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT 2144, LGA - BOS - DIRTY SOCK SMELL IN CABIN. MAINTENANCE ACTION PENDING.

Part: ACM — CONTAMINATED (AC BAY)

FLIGHT 2144, LGA - BOS - DIRTY SOCK SMELL IN CABIN. MAINTENANCE INSPECTED THE LEFT ENGINE SPINNER FOR SIGNS OF OIL, HPC STAGES 3-5-9 WERE BORESCOPED FOR SIGNS OF OIL, AIR MIX DUCT BORESCOPED FOR SIGNS OF WATER, THE APU AIR DELIVERY DUCT WERE INSPECTED FOR OIL CONTAMINATION, BAAT TEST ACCOMPLISHED, ENGINE PRECOOLER INSPECTED. NO FAULTS WERE FOUND. THE NR 2 PACK AIR CYCLE MACHINE AND THE NR 2 DUAL HEAT EXCHANGER WERE REMOVED AND REPLACED DUE TO COFFEE RESIDUE CONTAMINATION.

Part: HEAT EXCHANGER — CONTAMINATED (AC BAY)

FLIGHT 2144, LGA - BOS - DIRTY SOCK SMELL IN CABIN. ADDITIONAL COMPONENT REMOVED IN ADDITION TO SDR 20110527EM027. MAINTENANCE INSPECTED THE LEFT ENGINE SPINNER FOR SIGNS OF OIL, HPC STAGES 3-5-9 WERE BORESCOPED FOR SIGNS OF OIL, AIR MIX DUCT BORESCOPED FOR SIGNS OF WATER, THE APU AIR DELIVERY DUCT WERE INSPECTED FOR OIL CONTAMINATION, BAAT TEST ACCOMPLISHED, ENGINE PRECOOLER INSPECTED. NO FAULTS WERE FOUND. THE NR 2 PACK AIR CYCLE MACHINE AND THE NR 2 DUAL HEAT EXCHANGER WERE REMOVED AND REPLACED DUE TO COFFEE RESIDUE CONTAMINATION.

Part: AIR FILTER — DIRTY (CABIN)

FLIGHT 2126, LGA-BOS - STRONG DIRTY SOCK SMELL ON TAKEOFF AND CLIMBOUT. THE CREW WAS LIGHT HEADED AND HAD AN ODD FEELING. MAINTENANCE TROUBLESHOT AIR QUALITY, NO ODORS WERE NOTED. ACCOMPLISHED INSPECTION AND CHECK OF LEFT PACK WATER SPRAY NOZZLE. ACCOMPLISHED CHECK OF PROPER SERVICING OF ENGINES 1 AND 2 AND APU. REPLACED RECIRCULATION AIR FILTERS.

Part: FAN — NOISY (E&E BAY)

FLIGHT 754, ATL-PHL - ACRID SMELL NOTED DURING TAKEOFF BY PILOTS AND FLIGHT ATTENDANTS. PUNGENT SMELL UNTIL WELL AFTER TAKEOFF THRUST. ODOR SUBSIDED TO APPROXIMATELY 1500FT. NO COCKPIT INDICATIONS THRU 8000FT. IN DESCENT ODOR OCCURRED AGAIN. MAINTENANCE FOUND THE LEFT FORWARD AVIONICS FAN MAKING LOUD RUMBLE NOISE. REMOVED AND REPLACED AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)

BOS - THE AFT RIGHT SERVICE DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED THE ASSIST BOTTLE PER AMM 52-12-51-03.

Part: FILTER — DIRTY (CABIN)

FLIGHT 1829, BOS-PHL - VERY SOUR SMELL REPORTED COMING INTO CABIN ON TAKEOFF AND CLIMBOUT. SEEMED TO DISSIPATE ON CLIMBOUT. MAINTENANCE CHECKED APU OIL LEVEL, FOUND GOOD. ACCOMPLISHED ENGINE RUN UP AT DIFFERENT SETTING, NO SMELL. ACCOMPLISHED TASK 21-20-00-810-A AND J/C FOR CABIN QUALITY CHECK, UNABLE TO DUPLICATE. REMOVED AND REPLACED RECIRCULATION AIR FILTER, AC IS GOOD FOR SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE)

FLIGHT 1290, DFW-PHL - ABOUT 25 MINUTES OUT FROM PHL THE CREW DECLARED AN EMERGENCY DUE TO RAPID DEPRESSURIZATION. FROM 37,000' THE FLIGHT INITIATED A RAPID DESCENT DOWN TO 8000'. THE OXYGEN MASKS DID DEPLOY IN THE MAIN CABIN. THE FLIGHT LANDED UNEVENTFULL, EMERGENCY EQUIPMENT WAS STANDING BY, AND THE AIRPLANE TAXIED TO THE GATE NORMALLY. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER AND THE OUTFLOW VALVE. AS A PRECAUTIONARY MEASURE THE AMS CONTROLLER 1 SPDA 2 SLOT 18 WAS REPLACED. MAINTENANCE ALSO REPLACED A DAMAGED AVIONICS COOLING AIR DUCT, MASKS, AND 02 GENERATORS.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE)

FLIGHT 1290, DFW-PHL - ABOUT 25 MINUTES OUT FROM PHL THE CREW DECLARED AN EMERGENCY DUE TO RAPID DEPRESSURIZATION. FROM 37,000' THE FLIGHT INITIATED A RAPID DESCENT DOWN TO 8000'. THE OXYGEN MASKS DID DEPLOY IN THE MAIN CABIN. THE FLIGHT LANDED UNEVENTFUL, EMERGENCY EQUIPMENT WAS STANDING BY, AND THE AIRPLANE TAXIED TO THE GATE NORMALLY. MAINTENANCE REPLACED THE CABIN PRESSURE CONTROLLER AND THE OUTFLOW VALVE. AS A PRECAUTIONARY MEASURE THE AMS CONTROLLER 1 SPDA 2 SLOT 18 WAS REPLACED. MAINTENANCE ALSO REPLACED A DAMAGED AVIONICS COOLING AIR DUCT, MASKS, AND 02 GENERATORS.

Part: ACM — ODOR (ZONE 100)

FLT 1410 ON TAKEOFF UP TO 10,000 FT, WITH APU OFF, A STRONG ODOR WAS PRESENT IN THE FLIGHT DECK. THE SMELL DISSIPATES AFTER 10,000 FT. NO SMELLS NOTED IN CABIN. MAINTENANCE BORESCOPED LEFT AND RIGHT ENGINE BOOSTER STAGES AND APU. FOUND NO EVIDENCE OF ANY OIL CONTAMINATION. REMOVED APU AIR DUCT, LEFT ENGINE STARTER DUCT, AND BORESCOPED LEFT RAM AIR INTAKE DUCT. FOUND ALL DUCTS CLEAN. RAN ENGINES WITH NO SMELL IN A/C OR COCKPIT. RELEASED AIRCRAFT FOR TEST FLIGHT. AIRCRAFT FAILED TEST HOP FOR "OIL SMELL" IN FLIGHT DECK AND CABIN. AIRCRAFT REMAINS OUT OF SERVICE FOR TROUBLESHOOTING. - MAINTENANCE COMPLETED INSTALLATION OF THE LEFT PACK SYSTEM, REPLACED THE AIR CYCLE MACHINE AND THE REFRIGERATION PACK.

Part: HEAT EXCHANGER — FAULTY (AC BAY)

BOS - CONTAMINATED AIR IN COCKPIT AND CABIN. THE ODOR SMELLS LIKE CONTAMINATED OIL; WITH PACK 2 OFF AND FRESH AIR THE ODOR IS GONE. MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK AIR CYCLE MACHINE AND THE RIGHT PACK HEAT EXCHANGER. ALL LEAK AND OPERATIONAL CHECKS ARE SATISFACTORY.

Part: ACM — MALFUNCTIONED (AC BAY)

BOS - CONTAMINATED AIR IN COCKPIT AND CABIN. THE ODOR SMELLS LIKE CONTAMINATED OIL; WITH PACK 2 OFF AND FRESH AIR THE ODOR IS GONE. MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK AIR CYCLE MACHINE AND THE RIGHT PACK HEAT EXCHANGER. ALL LEAK AND OPERATIONAL CHECKS ARE SATISFACTORY.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)

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

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)

ATL - AFT RIGHT SERVICE DOOR PNEUMATIC ASSIST BOTTLE CHARGE IS BELOW LIMITS. MAINTENANCE SERVICED THE AFT RIGHT SERVICE DOOR PNEUMATIC ASSIST BOTTLE PER AMM 52-12-51-614-801-A.

Part: ACTUATOR — BENT (SERVICE DOOR) · airframe 5,104 hrs · 4,157 cycles

PIT - C1 - MAJOR REPAIR - PNEUMATIC ACTUATOR ASSEMBLY STRIKER ASSEMBLY PUNCTURE PIN BENT AT FORWARD SERVICE DOOR. REPLACED FORWARD SERVICE DOOR ACTUATOR ASSEMBLY IAW E190 MM 52-41-51.

Part: POWER UNIT — INOPERATIVE (CABIN)

PHL - MID CABIN EMERGENCY LIGHT INOP. MAINTENANCE REPLACED NR 6 POWER UNIT.

Part: RESERVOIR — LOW PRESSURE (L1 DOOR)

BWI - THE L1 DOOR OPEN ASSIST RESERVOIR HAS LOW PRESSURE. MAINTENANCE SERVICED THE L1 DOOR OPEN ASSIST RESERVOIR.

Part: ACCUMULATOR — LOW PRESSURE (L1 DOOR)

ATL - THE L1 DOOR EMERGENCY ACCUMULATOR HAS LOW PRESSURE. MAINTENANCE SERVICED THE L1 DOOR EMERGENCY ACCUMULATOR.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR)

CLT - L1 DOOR SLIDE PARTIALLY DEPLOYED, LACING UNDONE. MAINTENANCE REPLACED THE L1 SLIDE.