N957UW

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,785 hrs · 21,273 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY LIGHT BATTERY FAULT EICAS MSG DISPLAYED WHEN LIGHTS TESTED DURING PREFLIGHT 2 OVERHEAD CABIN EMERG LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERG LT BATTERY AT PANEL 243 OVERHEAD. OPS CHECK NORMAL.

Part: DUCTED FAN — FAILED (RECIRCULATION) · airframe 25,737 hrs · 21,236 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ELECT SMELL IN COCKPIT THRUOUT A/C CABIN, VERY STRONG IN FIRST CLASS SMELL REPORTED BY FA 1. RETURN TO THE GATE. MAINTENANCE ACCOMPLISHED JOB CARD 43L00021001. FOUND LEFT RECIRCU FAN BAD. REMOVE & REPLACED LEFT RECIRCULATION FAN IAW AMM 21-24-01. REMOVED & REPLCAED RECIRCULATION DUCT IAW AMM 21-24-03. REMOVED & REPLACED RECIRCULATION FILTERS IAW AMM 21-24-02. OPS CHECK GOOD. NO SMELL IN COCKPIT OR CABIN NOTED.

Part: SLIDE — PARTIAL DEPLOY (R1 DOOR) · airframe 25,441 hrs · 20,951 cycles

AIRCRAFT NOT GROUNDED: MAINTENANCE REPORTS R1 SLIDE PARTIALLY DEPLOYED, ASSIST BOTTLE DEPLETED. REPLACED DIAPHRAGM AND SLIDE ASSEMBLY IAW JOB CARD 43L00025001.

Part: POSITION SENSOR — FAULTY (LEFT) · airframe 24,177 hrs · 19,826 cycles

THE PILOT DECLARED AN EMERGENCY DUE TO A FLAPS FAILED EICAS MESSAGE. FLAPS FAILED TO RETRACT PROPERLY FROM 1 TO 0 AFTER TAKE OFF, AND AT EXTENSION FOR LANDING THE FLAPS FAILED AGAIN AND STAYED AT FLAPS 3 WITH FULL FLAPS SELECTED. MAINTNENANCE REMOVED AND REPLACED THE LT FLAP POSITION SENSOR UNIT IAW AMM 27-53-04. OPS CHECKED GOOD, NO FAULTS NOTED.

Part: SENSOR — FAULTY · airframe 24,101 hrs · 19,775 cycles

DURING APPROACH, IN ICING CONDITIONS AT 2500 FEET, THE AIRCRAFT EXPERIENCED VIOLENT ROLL. AP & AT DISCONNECTED AND EICAS MESSAGES WERE DISPLAYED AT FAIL, WIND SHEAR FAIL, STALL PROT FAIL, AND THE AOA LIMIT FAIL. AFTER LANDING, ADS PROBE 3+1 FAIL, DISPLAYED. REPLACED SMART PROBE IAW AMM 34-13-01.

Part: PIN — BROKEN (DOOR SLIDE) · airframe 21,271 hrs · 17,584 cycles

AFT PASSENGER DOOR EMERGENCY SLIDE RELEASE PIN THREAD IS BROKEN OFF. REPLACED AFT PASSENGER DOOR EMERGENCY SLIDE. AIRCRAFT WAS GROUNDED.

Part: FLAP TRACK — WORN (TE FLAP) · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IS IN BASE, WEAR ON LEFT WING INBOARD FLAP TRACK 2A INBOARD. REPLACED LEFT WING INBOARD FLAP TRACK 2A INBOARD PER AMM 57-54-25.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND COCKPIT FLOOR DOUBLER BETWEEN LBL 0 AND -Y1016, BETWEEN FR 7 AND FR12. REPAIRED COCKPIT FLOOR DOUBLER PER AARD 53-10-10-1 REPAIR 1 AND EA 274427.

Part: SLIDE — BROKEN (ZONE 800) · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT WAS GROUNDED. AFT SERVICE DOOR EMERGENCY SLIDE, RELEASE PIN THREAD IS BROKEN OFF. REPLACED AFT DOOR EMERGENCY SLIDE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON COCKPIT FLOOR DOUBLER AT -Y640 BETWEEN FR 19 AND FR 20. REPLACED FLOOR DOUBLER PER AARD 53-00-00-3 REPAIR 3 AND DRAWING 170-00822-413.

Part: SKIN PANEL — CRACKED (RT WING) · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED RIGHT WING TRAILING EDGE SKIN AT EDGE PAST FASTENER ON OUTBOARD SIDE OF RIB 10. REPAIRED LOWER SKIN PER SRM 57-10-01 REPAIR 54.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT ANGEL FOR DRAIN MAST, AFT OF FR 86, BETWEEN STRINGER 27R AND 28R. REPLACED INTERCOSTAL PER DRAWING 170-65180-445.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT ANGLE FOR DRAIN MAST, AFT OF FR 86, BETWEEN STRINGER 27R AND 28R. REPLACED ANGLE PER DRAWING 170-87561-001.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERCOSTAL AT FR 87 BETWEEN STRINGER 27R AND 28R. REPLACED INTERCOSTAL PER E190 SRM 51-41-01, 51-42-01, DWG 170-65180-445.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND FORWARD MAIN CABIN FLOORBEAM AT Y320, BETWEEN FR 17 AND FR 18. REPLACED FLOORBEAM PER DRAWINGS 170-00822-505 AND 170-07304-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN FLOORBEAM AT Y360, BETWEEN FR 12 AND FR 13. REPLACED FLOORBEAM PER SRM 51-41-01, SRM 51-43-03, AND DRAWING 190-05555-805.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR SUPPORT AT -Y1150 AND FR 16. REPLACED FLOOR SUPPORT PER DRAWING 170-00816-415.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN LEFT HAND SEAT TRACK AT -Y280 AND FR84. REPAIRED SEAT TRACK PER SRM 53-00-10 REPAIR 51.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR SUPPORT AT -Y770 AND FR 17. REPLACED FLOOR SUPPORT PER DRAWING 170-00822-503.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN CROSSBEAM AT Y720 AND FR 14. REPAIRED CROSSBEAM PER SRM53-00-10 REPAIR 53.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT AFT MAIN CABIN FLOOR STRAP SUPPORT AT Y1160, BETWEEN FR 85 AND FR 86. REPLACED FLOOR STRAP SUPPORT PER DRAWING 170-66000-445.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN RIGHT HAND FLOOR SILL AT Y970, BETWEEN FR 12 AND FR 14. REPLACED FLOOR SILL PER 53-00-00-3 REPAIR 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORRODED FORWARD MAIN CABIN FLOORBEAM AT -Y340 AND Y360, BETWEEN FR12 AND FR13. REPLACED FLOORBEAM PER 53-00-00-3 AND SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR PANEL SUPPORT AT -Y1180 AND FR 84. REPLACED FLOOR SUPPORT PER DRAWING 170-66000-445.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON LEFT HAND LOWER REAR SKIN PANEL AROUND FASTENER, NEXT TO DRAIN HOLE, AT SPAR 2 AND RIB 10. REPAIRED SKIN PANEL PER EA 254412.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND SEAT TRACK AT -Y280, BETWEEN FR 16 AND FR20. REPLACED SEAT TRACK PER 53-00-00-3 REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN RIGHT HAND SEAT TRACK AT Y250 AND FR 17. REPLACED SEAT TRACK PER 53-00-00-3 REPAIR 3.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN RIGHT HAND FLOORBEAM FASTENER AT Y280 AND FR 87. REPLACED FLOORBEAM PER AARD 53-00-00-3 REPAIR 3 AND SRM 51-43-03.

Part: DOOR SILL — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

CORROSION ON FORWARD MAIN CABIN RIGHT FLOOR SUPPORT AT Y1100, BETWEEN FRAMES 17 AND 18. REPLACED THE FLOOR SUPPORT IAW 53-00-00-3 AND DRAWING 170-00822-413.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR STRAP SUPPORT AT -Y1180 AND FR 85. REPLACED FLOOR STRAP SUPPORT DRAWING 170-66000-445.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN RIGHT HAND REINFORCEMENT STRUCTURE AT FR 84, BETWEEN Y280 AND Y1150. REPLACED FLOOR SUPPORT.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR SILL AT -Y1180, BETWEEN FR 12 AND FR 13. REPLACED FLOOR SILL PER 53-00-00-3 REPAIR 3 FIGURE 1 SHEET 11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD MAIN CABIN LEFT HAND FLOOR SUPPORT AT -Y770 AND FR 18. REPLACED FLOOR SUPPORT PER DRAWING 170-00822-413 AND SRM 51-41-01.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT MAIN CABIN FLOOR PANEL SUPPORT AT Y920, BETWEEN FR 89 AND FR 90. REPLACED PANEL SUPPORT PER AARD 53-00-00-3 REPAIR 3.

Part: UPPER SHEET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 21,270 hrs · 17,583 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION / SCRATCH ON AFT MAIN CABIN RIGHT HAND UPPER SHEET, UNDER SIDE AT Y280 BETWEEN FR 85 AND FR 86. REPLACED UPPER SHEET PER DRAWING 170-65-660-449.

Part: LENS — MISSING (CABIN) · airframe 20,880 hrs · 17,271 cycles

AIRCRAFT WAS NOT GROUNDED. CENTER AISLE FORWARD EXIT LOCATOR LENS COVER MISSING FOR OVERWING EXIT. REPLACED OVERWING EXIT LENS COVER.

Part: LINE — BROKEN (HYD SYSTEM 2) · airframe 20,501 hrs · 16,949 cycles

LOST HYDRAULIC SYS NR 2 QUANTITY AFTER TAKEOFF. FOUND BROKEN HYDRAULIC LINE AT NR 2 SYS CASE DRAIN FILTER MANIFOLD. REPLACED THE LINE. AIRCRAFT WAS GROUNDED.

Part: WINDSHIELD — LEAKING (COCKPIT) · airframe 20,309 hrs · 16,809 cycles

LOWER LEFT SIDE CAPTAIN`S WINDSHIELD IS LEAKING WATER FROM BETWEEN THE GLASS AND THE RUBBER SEAL, 15 TO 23 INCHES FROM RIGHT CORNER. REPLACED WINDSHIELD IAW AMM 56-11-00-400-801-A. AIRCRAFT WAS GROUNDED.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 19,807 hrs · 16,437 cycles

AIRCRAFT IN BASE MAINTENANCE, R1 SERVICE DOOR PNEUMATIC BOTTLE NEEDS SERVICING. SERVICED R1 SERVICE DOOR PNEUMATIC BOTTLE PER AMM 52-41-51-614-801.

Part: HANDLE — UNSECURE (OVERWING EXIT) · airframe 19,682 hrs · 16,347 cycles

RETURNED TO DEPARTURE DUE TO THE RIGHT OVERWING EMERGENCY DOOR EXIT INDICATED OPEN ON THE MASTER CAUTION. NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. DOORS INDICATE GREEN ON GROUND. MAINTENANCE FOUND RIGHT OVERWING ESCAPE HATCH HANDLE APPROX 10 DEGREE FROM FULL CLOSED POSITION. AT 10 DEGREES LATCH IS MOVED AND MICROSWITCH IS OFF, THIS WAS A GOOD INDICATION. LUBED LATCH HANDLE AND PINS TO ALLOW HANDLE TO MOVE TO 0 DEGREE (FULLY CLOSED) POSITION PER AMM 52-20-00 & AMM 52-21-00.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 19,565 hrs · 16,266 cycles

AIRCRAFT WAS NOT GROUNDED. ENTIRE SECTION OF FIRST PIECE OF PHOTO LUMINESCENT STRIP MISSING SIDE OF ISLE AT 1D. MAINTENANCE REPLACED PHOTO LUMINESCENT STRIP PER 33-50-00.

Part: ENGINE — ODOR (RIGHT) · airframe 18,522 hrs · 15,436 cycles

ACFT WAS GROUNDED, FLIGHT CREW REPORTED RECEIVING A LAV SMOKE EICAS ON TAKEOFF AT 500' AGL, EICAS WENT OUT WITH POWER REDUCTION AND A SMOKE ODOR IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED TC 43L00021001, TROUBLE SHOOT CABIN AIR QUALITY AND TC 43L00036002, PNEUMATIC BLEED AIR BLASTER AND COULD NOT DUPLICATE THE ODOR OR THE LAV SMOKE FAULTS. MAINTENANCE DETERMINED THAT THE ODOR IN THE CABIN WAS DUE TO PRESERVATIVE OIL RESIDUE FROM THE RT ENGINE CHANGE, ACCOMPLISHED PRIOR TO THIS FLIGHT.

Part: STRAP — DAMAGED (FLASHLIGHT) · airframe 18,101 hrs · 15,082 cycles

AIRCRAFT WAS NOT GNDED. FWD FLIGHT ATTENDANT STATION FLASHLIGHT SECURITY STRAP REQUIRES REPAIR. R & R STRAP. OPERATIONAL CHECKED GOOD.

Part: DUCT — LEAKING (ZONE 400) · airframe 17,866 hrs · 14,903 cycles

AIRCRAFT WAS GNDED. AFTER DEPARTURE WHILE CLIMBING, THE NR 1 BLEED SYS FAILED, RESULTING IN A PRESSURIZATION ISSUE AS THE NR 2 BLEED AIR SYS WAS ALREADY ON MEL. DECLARED AN EMER & RETURNED WHERE THE ACFT LANDED SAFELY WITH NO FURTHER INCIDENT. FOUND A BLEED AIR LEAK COMING FROM THE STARTER DUCT IN THE NR 1 PYLON FWD SECTION & REPLACED THE STARTER DUCT IAW AMM 36-11-4 400. NO FAULTS WERE NOTED DURING AN OPERATIONAL CHECK OF THE SYS.

Part: SLIDE — FAULTY (R1 DOOR) · airframe 17,241 hrs · 14,349 cycles

AIRCRAFT WAS NOT GNDED. 1R DOOR WILL NOT ARM. R & R ESCAPE SLIDE. R & R SHEARED FLEX BALL CABLE IAW AMM 52-41-40. OPERATIONS CHECKED OK FOR SERVICE.

Part: CABLE — BROKEN (R1 DOOR) · airframe 17,241 hrs · 14,349 cycles

AIRCRAFT WAS NOT GNDED. 1R DOOR WILL NOT ARM. R & R ESCAPE SLIDE. R & R SHEARED FLEX BALL CABLE IAW AMM 52-41-40. OPERATIONS CHECKED OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, L2 EMER EXIT SIGN HAS LED BURNT OUT. L2 EMER EXIT SIGN HOUSING REPLACED. OPERATIONS CHECKED GOOD IAW AMMS 33-50-17 & 33-50-19.

Part: LENS — DEFECTIVE (EXIT SIGN) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, L3 EMER EXIT SIGN HAS LENS DEFECTIVE. L3 EMER EXIT SIGN LENS REPLACED. OPERATIONS CHECKED GOOD IAW AMMS 33-50-17 & 33-50-19.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, L1 EMER EXIT SIGN HAS LED BURNT OUT. L1 EMER EXIT SIGN HOUSING REPLACED. OPERATIONS CHECKED GOOD IAW AMMS 33-50-17 & 33-50-19.

Part: SIGN — CRACKED (CABIN) · airframe 16,830 hrs · 13,944 cycles

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

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, COCKPIT FLOOR CROSSBEAM ATTACH ANGLE CRACKED AT FRAME 12 & LBL 27. REPLACED ANGLE IAW SRM 51-41-02.

Part: FITTING — CRACKED (RT HORIZ STAB) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, RT HORIZONTAL STABILIZER AFT SPAR, BETWEEN RIB 5 & 6, INBD ELEVATOR PCU FITTING IS CRACKED AT RADIUS. R & R ELEVATOR PCU FITTING IAW DWG 190-09152-411.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, LEFT OVERWING CTR EMER PATH LIGHT INOPERATIVE. FOUND LIGHT DISCONNECTED, RECONNECTED LIGHT IAW WDM 33-50-50. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-00. CHECKED GOOD.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, MAIN CABIN LT & RT PHOTO LUMINESCENT STRIPS ARE DAMAGED, MORE THAN 10%. R & R MAIN CABIN RT PHOTO LUMINESCENT STRIP IAW AMM 33-50-21. SEE ALSO AALA201509309001 FOR LT SIDE.

Part: SIGN — CRACKED (CABIN) · airframe 16,831 hrs · 13,944 cycles

CE3 CHECK, THE R2 DOOR UPPER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R R2 DOOR UPPER EMER EXIT SIGN IAW AMM 33-50-19. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00.

Part: LENS — CRACKED (EXTERIOR LIGHT) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, RIGHT AFT WING TO BODY EMER LIGHT LENS IS CRACKED. R & R RT WING TO BODY EMER LIGHT LENS IAW AMM 33-50-25.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, MAIN CABIN LT & RT PHOTO LUMINESCENT STRIPS ARE DAMAGED, MORE THAN 10%. R & R MAIN CABIN LT PHOTO LUMINESCENT STRIP IAW AMM 33-50-21. SEE ALSO AALA201509309024 FOR RT SIDE.

Part: ROLLER — STUCK (EMERGENCY EXIT) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK LEFT WING EXIT DOOR, AFT ROLLER IS STUCK. R & R LT OVERWING ESCAPE HATCH UPPER LATCH FITTING ASSEMBLY IAW AMM 52-21-00. ADJUSTMENT CHECKED GOOD.

Part: LENS — CRACKED (EXIT SIGN) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK THE R1 DOOR UPPER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R R1 DOOR UPPER EMER EXIT MARKING SIGN LENS IAW AMM 33-50-17. OPERATIONAL CHECKED GOOD IAW AMM 33-50-00.

Part: SIGN — CRACKED (CABIN) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, THE L1 DOOR UPPER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R LENS AT THE EXIT SIGN ABOVE L1 DOOR IAW AMM 33-50-17.

Part: SIGN — CRACKED (CABIN) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, THE L2 DOOR LOWER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R L2 DOOR LOWER EMER EXIT SIGN IDENTIFIER. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-00-710-801A & AMM 33-50-15.

Part: SIGN — CRACKED (CABIN) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, THE R2 DOOR LOWER EMER EXIT SIGN IDENTIFIER IS CRACKED. R & R R2 DOOR LOWER EMER EXIT SIGN IDENTIFIER. PERFORMED OPERATIONAL CHECK IAW AMM 33-50-15 & AMM 33-50-00.

Part: SIGN — CRACKED (CABIN) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, THE L1 DOOR, LOWER EMER EXIT IDENTIFIER SIGN IS CRACKED. R & R L1 DOOR EMER EXIT IDENTIFIER SIGN IAW AMM 33-50-15. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: SKIN PANEL — CRACKED (LT WING) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, LT WING LOWER SURFACE SKIN CRACKED AROUND FASTENER HOLE NEAR DRAIN HOLE, AT SPAR 2 & RIB 10. REPAIRED IAW EA 254412.

Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, R1 DOOR PNEUMATIC ASSIST BOTTLE PRESSURES ARE LOW. ACCOMPLISHED CARD 43C82152001.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, R2 DOOR PNEUMATIC ASSIST BOTTLE PRESSURES ARE LOW. ACCOMPLISHED CARD 43C82452001.

Part: ROLLER — STUCK (FUSELAGE) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, RT OVERWING HATCH CUT OUT, FWD ROLLER IS STUCK. R & R RT OVERWING HATCH CUT OUT, FWD ROLLER IAW AMM 20-10-08-000-801-A.

Part: SLIDE — DAMAGED (PAX DOOR) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, AFT PAX DOOR, ESCAPE SLIDE, LOWER RT CORNER ELASTIC STRAP IS BROKEN OFF ACFT. R & R SLIDE IAW CARD 43C81252001.

Part: ACTUATOR — OUT OF ALIGNMENT (R2 DOOR) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, R2 DOOR PNEUMATIC ASSIST ASSEMBLY HAS PLUNGER NOT PROPERLY ALIGNED, RED MARKS DO NOT LINE UP. ACCOMPLISHED CARD 43C82452001.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, L1 DOOR PNEUMATIC ASSIST BOTTLE PRESSURE LOW. ACCOMPLISHED CARD 43C81152001.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 16,831 hrs · 13,944 cycles

C3 CHECK, L2 DOOR PNEUMATIC ASSIST BOTTLE PRESS LOW. ACCOMPLISHED CARD 43C81252001.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, CORROSION ON RT SHEAR PANEL, BETWEEN FRAME 87 & 88, Y=+304.8 TO Y=+1041.4. REPLACED IAW SRM 51-42-01 & 51-42-02.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT LOWER CTR SEAL REST, BETWEEN FRAME 78 - 79 AT STRINGER 26R. REPLACED IAW SRM 53-23-29 & AARD 53-00-00-03 REPAIR 3.

Part: PANEL — CORRODED (FUSELAGE) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, CORROSION ON CTR SHEAR PANEL, BETWEEN FRAME 87 - 88 & BETWEEN Y=-222.3 - Y=+222.3. REPLACED IAW SRM 53-00-00-3 REPAIR 3.

Part: SUPPORT RIB — CRACKED (VERTICAL STAB) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, VERTICAL STABILIZER REAR SPAR ABOVE NR 3 HINGE FITTING, SUPPORT RIB IS CRACKED. R & R RIB 9 &10 TE PN 170-63629-005, BATCH 0002845448 AT VERTICAL STABILIZER REAR SPAR ABOVE NR 3 HINGE FITTING IAW SRM PART II 51-41-02 PARA 4, PARA 6 & 51-41-01 PARA 4 & PARA 6.

Part: SEAL REST — CORRODED (FUSELAGE) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, CORROSION ON FWD CARGO COMPARTMENT DOOR CUTOUT LOWER CTR SEAL REST, BETWEEN FRAME 25 - 26 AT STRINGER 26R. REPLACED IAW SRM 51-41-01 & AARD 53-00-00-3 REPAIR 3.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 16,830 hrs · 13,944 cycles

C3 CHECK, CABIN FLOOR GUSSET AT FRAME 90 & RBL 20 IS CORRODED. FABRICATED & INSTALLED REPLACEMENT GUSSET IAW SRM 51-41-02 & DWG 170-60001-823.

Part: ACM — CONTAMINATED (ZONE 100) · airframe 14,887 hrs · 12,305 cycles

FUMES & HEAVY PETROLEUM SMELL IN COCKPIT & CABIN WHILE DESCENDING BELOW 12,OOO'. FOUND COFFEE RESIDUE COATING THE RT PACK HEAT EXCHANGER & ACM. R & R THE RT PACK HEAT EXCHANGER & ACM. THE RECIRCULATION FILTERS WERE ALSO REPLACED.

Part: A/C PACK — CONTAMINATED (ZONE 100) · airframe 14,887 hrs · 12,305 cycles

FUMES & HEAVY PETROLEUM SMELL IN COCKPIT & CABIN WHILE DESCENDING BELOW 12,OOO'. FOUND COFFEE RESIDUE COATING THE RT PACK HEAT EXCHANGER & ACM. R & R THE RT PACK HEAT EXCHANGER & ACM. THE RECIRCULATION FILTERS WERE ALSO REPLACED.

Part: HINGE — BROKEN (COCKPIT DOOR) · airframe 14,476 hrs · 11,901 cycles

WHILE CLIMBING OUT THE COCKPIT DOOR OPENED. THE CREW TRIED TO SECURE THE DOOR CLOSED BUT A HINGE WAS BROKEN & LOOSE & THE DOOR WOULD NOT SECURE. THE CREW ADVISED THE TRAVELING FAMS. THE CREW ELECTED TO DIVERT FOR MX. AN EMER WAS DECLARED & THE FLIGHT LANDED & TAXIED TO GATE WITHOUT INCIDENT. R & R THE COCKPIT DOOR HINGES.

Part: SHEAR PIN — LOOSE (RT PYLON) · airframe 14,225 hrs · 11,685 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 (RT PYLON) · airframe 14,225 hrs · 11,685 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 14,225 hrs · 11,685 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 14,225 hrs · 11,685 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: SENSOR — INOPERATIVE (LE SLAT) · airframe 13,866 hrs · 11,407 cycles

FLIGHT 2187, LGA - DCA. SLAT FAIL EICAS MSG WITH SLATS AT 3 ON APPROACH. THE CREW DECLARED AN EMERGENCY & THE ACFT HAD AN UNEVENTFUL LANDING. R & R THE RT OTBD SLAT SKEW SENSORS.

Part: SENSOR — INOPERATIVE (LE SLAT) · airframe 13,866 hrs · 111,407 cycles

FLIGHT 2187, LGA - DCA. SLAT FAIL EICAS MSG SLATS AT 3 ON APPROACH. THE CREW DECLARED AN EMERGENCY & THE ACFT HAD AN UNEVENTFUL LANDING. R & R THE RT OTBD SLAT SKEW SENSORS.

Part: PRECOOLER — LEAKING (BLEED AIR SYS) · airframe 13,525 hrs · 11,135 cycles

FLIGHT CREW RECEIVED BLEED 2 LEAK EICAS MSG ON CLIMB OUT OF PHL AT FL300. CREW DECLARED AN EMERGENCY & PERFORMED A RAPID DESCENT DOWN TO 10,000FT. FLIGHT RETURNED TO PHL & LANDED NORMALLY. R & R THE NR 2 & NR 1 ENG PRE COOLER.

Part: MECHANISM — OUT OF ADJUST (L1 DOOR) · airframe 13,492 hrs · 11,116 cycles

L1 DOOR EMERGENCY OPENING SYS FAILED WHEN PERFORMING FUNCTIONAL CHECK. MX ACCOMPLISHED ADJUSTMENT TEST OF THE CONTROL MECHANISM, CHECKED NORMAL.

Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 13,489 hrs · 11,112 cycles

PHL, EVACUATION SLIDE FUNCTIONAL TEST DUE ON L1 DOOR, NO LIGHTS ON SLIDE PACK. THIS IS RECORDED AS A SYS FAIL.

Part: BOTTLE — LOW PRESSURE (AFT PAX DOOR)

AFT LEFT PAX ENTRY DOOR REQUIRES DOOR ASSIST BOTTLE PRESSURE SERVICING . MAINTENANCE SERVICED AFT LEFT PAX ENTRY DOOR.

Part: BOTTLE — LOW PRESSURE (FWD PAX DOOR)

FWD PAX ENTRY DOOR REQUIRES DOOR ASSIST BOTTLE PRESSURE SERVICED. MAINTENANCE ACCOMPLISHED FORWARD RIGHT PAX ENTRY DOOR ASSIST BOTTLE SERVICE AFTER 24 AND 48 HOURS.

Part: PNEUMATIC SYSTEM — LOW PRESSURE (PAX DOOR) · airframe 11,701 hrs · 9,767 cycles

LEFT AFT PASSENGER DOOR EMERGENCY PNEUMATIC ASSY NEEDS SERVICING. MX SERVICED LEFT AFT PASSENGER DOOR EMERGENCY PNEUMATIC ASSY.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - EMERGENCY POWER SUPPLY NR 5 FAILS TEST. BATTERY FAILED TEST, LIGHT ASSEMBLY INOP AT AFT PASSENGER DOOR. REPLACED EMERGENCY POWER SUPPLY NR 5 IAW EMBRAER E190 AMM 33-50-01.

Part: PAN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WASTE PAN BETWEEN FR85 TO FR88, S23L. REPLACED WASTE PAN BETWEEN FR85 TO FR88, S23L IAW EMBRAER E190 SRM 2, 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR19, LBL 11. REPAIRED FLOORBEAM BETWEEN FR16 TO FR19, LBL 11 IAW EA 504962.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WASTE BOX DOUBLER BETWEEN FR88 TO FR89, S28R. REPLACED WASTE BOX DOUBLER BETWEEN FR88 TO FR89, S28R IAW E190 SRM 2, 53-42-01.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - CORROSION ON SUPPORT RIB AT FR45, -Y26. REPLACED SUPPORT RIB AT FR45, -Y26 IAW EMBRAER E190 SRM 51-10-04.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD CARGO FLOORBEAM BETWEEN FR26 TO FR27, -Y10. REPLACED FORWARD CARGO FLOORBEAM BETWEEN FR26 TO FR27, -Y10 IAW EMBRAER E190 SRM 2, 51-43-04.

Part: SEAL PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAL PLATE BETWEEN FR24 TO FR25, -Y10. REPLACED SEAL PLATE BETWEEN FR24 TO FR25, -Y10 IAW E190 SRM 2, 51-41-01.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, -Y22. REPLACED GUSSET AT FR90, -Y22 IAW E190 SRM 2, 51-41-02.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON GUSSET AT FR90, -Y10. REPLACED GUSSET AT FR90, -Y10 IAW E190 SRM 2, 51-41-02.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSS BEAM AT FR17 & BETWEEN -Y26 TO -Y28. REPAIRED CROSS BEAM AT FR17 & BETWEEN -Y26 TO -Y28 IAW EA 504965.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR14 TO FR17, -Y10. REPLACED FLOORBEAM BETWEEN FR14 TO FR17, -Y10 IAW EMBRAER E190 SRM 2, 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FORWARD RIGHT SILL BETWEEN FR17 TO FR18 & BETWEEN -Y41 TO -Y48. REPLACED FORWARD RIGHT SILL BETWEEN FR17 TO FR18 & BETWEEN -Y41 TO -Y48 IAW EMBRAER E190 SRM 51-41-02 & 51-43-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CROSSBEAM PANEL SUPPORT AT FR16, -Y29. REPLACED CROSSBEAM PANEL SUPPORT AT FR16, -Y29 IAW E190 SRM 51-41-0.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE BETWEEN FR12 TO FR14, -Y38. REPLACED SILL PLATE BETWEEN FR12 TO FR14, -Y38 IAW E190 SRM 2, 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN -Y10 TO Y10. REPLACED SILL PLATE BETWEEN FR12 TO FR14, -Y38 IAW E190 SRM 2, 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON UPPER SHEET BETWEEN FR86 TO FR87, Y10.750. REPLACED UPPER SHEET BETWEEN FR86 TO FR87, Y10.750 IAW E190 SRM 2, 51-41-01.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR86 TO FR87, -Y10.75. REPLACED FLOORBEAM BETWEEN FR86 TO FR87, -Y10.75 IAW EMBRAER E190 SRM 2, 51-41-01.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN -Y12 TO -Y37. REPLACED SHEAR PANEL BETWEEN FR87 TO FR88 & BETWEEN -Y12 TO -Y37 IAW EMBRAER E190 SRM 2, 51-40-02.

Part: SEAL PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 10,899 hrs · 9,158 cycles

C2 CHECK - LEVEL 2 GALVANIC CORROSION ON SEAL PLATE BETWEEN FR24 TO FR27, -Y10. REPLACED SEAL PLATE BETWEEN FR24 TO FR27, -Y10 IAW E190 SRM 51-40-01.

Part: THRESHOLD — MISINSTALLED (FUSELAGE)

PHL - 1L DOOR WILL NOT CLOSE. REMOVED AND RE-INSTALLED THRESHOLD PLATE AND RESEALED. DOOR CHECKS GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 8,754 hrs · 7,326 cycles

FLIGHT 183, PHL - DFW - DESCENDING THRU FL 190 CAPTS WINDSHIELD SHATTERED AND STARTED ARCHING, FOLLOWED QRH PROCEDURE. REPLACED L1 WINDSHIELD AND REPLACED CONTROLLLER REF MM 56-11-00. OPERATIONAL AND LEAK CK GOOD.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 7,876 hrs · 6,665 cycles

BOS - EMERGENCY LT BATT FAULT. MAINTENANCE REMOVED AND REPLACED LT EMERGENCY-LIGHT POWER UNIT PER E190 AMM 33-50-01, OPS TEST GOOD.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 7,779 hrs · 6,596 cycles

BOS - UPON ARRIVAL TO AIRCRAFT, MAINT FOUND L-1 DOOR SLIDE PARTIALLY DEPLOYED. MAINTENANCE REPLACED NR 1 DOOR SLIDE ASSY PER AMM 25-65-01, CHECKS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

FLIGHT 1267, PHL-DFW - BREAK AWAY FLASHLIGHT 2R DOES NOT BLINK. MAINTENANCE REMOVED AND REPLACED 2R FLASHLIGHT. OPERATIONAL CHECK IS SATISFACTORY.

Part: GLOWSTRIP — MISSING (CABIN)

LGA - ROW 1 AC RIGHT FLOOR PATH LIGHTING MISSING. PLACED ON MEL. JUNE 5TH - MAINTENANCE REPLACED MISSING PHOTOLUMINESCENT FLOOR PATH LIGHTING SECTION. THIS CLEARS THE MEL.

Part: SWITCH — OUT OF ADJUST (PAX DOOR)

BOS - THE AFT LEFT AND RIGHT EMERGENCY LIGHTS ABOVE THE DOOR SLIDES ARE ON. MAINTENANCE ADJUSTED THE AFT LEFT PASSENGER DOOR COURTESY LIGHT MICRO-SWITCH PER 33-26-15. A SUCCESSFUL OPERATIONAL CHECK WAS PERFORMED, THE EMERGENCY LIGHTS CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (LE SLAT)

BOS - FLT 1980 EN-ROUTE PHL TO PVD. UPON DESCENT INTO PVD, THE CREW RECEIVED A SLAT FAIL EICAS MESSAGE. AFTER A DISCUSSION WITH MAINTENANCE AND OPERATIONS, IT WAS DECIDED THAT THE FLIGHT SHOULD DIVERT TO A MAINTENANCE BASE. THE CREW DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED TO BOS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT OUTBOARD SLAT SKEW SENSOR 2/3.

Part: DIAPHRAGM — PUNCTURED (PAX DOOR)

BOS - THE AFT PASSENGER DOOR PNEUMATIC ASSEMBLY DIAPHRAGM PUNCTURED. MAINTENANCE REMOVED AND REPLACED THE PNUEMATIC ASSEMBLY DIAPHRAGM PER AMM 52-11-53.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 5,886 hrs · 4,910 cycles

PIT - C1 - EES - FORWARD SERVICE DOOR SLIDE INFORMATION TAG ON GAGE ILLEGIBLE & BOTTLE PRESSURE READS 0 PSI. REPLACED FORWARD SERVICE DOOR SLIDE IAW JOB CARD 43C82152001.

Part: BOTTLE — LOW PRESSURE (R1 DOOR)

BOS - THE R1 DOOR ASSIST BOTTLE REQUIRES SERVICING. MAINTENANCE SERVICED THE R1 DOOR ASSIST BOTTLE PER AMM 52-11-51-03.

Part: BOTTLE — LOW PRESSURE (L1 DOOR)

BOS - THE L1 DOOR ASSIST BOTTLE NEEDS SERVICING. MAINTENANCE SERVICED THE L1 DOOR ASSIST BOTTLE PER AMM 52-11-51-03 A.

Part: POWER CABLE — OUT OF POSITION (COCKPIT)

PHL - THE CAPTAIN'S SEAT WOULD NOT LOCK IN PLACE. MAINTENANCE REPOSITIONED SEAT ELECTRIC CORD AND LUBED. OPERATIONAL CHECK IS GOOD, AC OKAY FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (SERVICE DOOR)

ATL - THE RIGHT SERVICE DOOR ASSIST BOTTLE IS LOW. MAINTENANCE SERVICED THE RIGHT DOOR PNEUMATIC ASSIST BOTTLE.

Part: HINGE — LOOSE (COCKPIT DOOR)

CLT - THE COCKPIT DOOR CAME OFF THE HINGES WHEN THE DOOR WAS OPENED. MAINTENANCE REMOVED AND REPLACED THE COCKPIT DOOR UPPER HINGE AND PERFORMED ADJUSTMENTS OF THE COCKPIT DOOR.

Part: MODULE — DAMAGED (TAT)

FLIGHT 1569, BDL-PHL - THE CREW REPORTED AUTO THROTTLE FAIL MESSAGE IN FLIGHT ALONG WITH TAT 2 FAIL, LOSING LEFT NAVIGATION. THE CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. UPON LANDING REPORTED A FAINT ELECTRICAL SMOKE ODOR IN THE COCKPIT AND CABIN. MAINTENANCE REPLACED SPDA DC POWER SUPPLY MODULE. AOA AND TOTAL TEMPERATURE SENSORS WERE ALSO REPLACED.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

CLT - FLIGHT ATTENDANT FLASHLIGHT NOT SHOWING THAT IT IS CHARGING. MX R&R THE BATTERY.

Part: WIRE HARNESS — DAMAGED (NLG STEERING)

THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR UPON TAKEOFF. THE FLIGHT RETUREND TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANIDNG CONTROL LEVER AND THE PROXIMITY SENSOR MODULE. HOWEVER, ON THE FIRST FLIGHT OUT, THE HANDLE TO RETRACT THE GEAR WOULD NOT MOVE PREVENTING THE GEAR FROM RETRACTING. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEEL SENSOR/STEERING SENSOR FEEDBACK ELECTRICAL HARNESS. (K)