N401YX

Part: INDICATOR — WARNING MESSAGE (ZONE 800) · airframe 22,473 hrs · 15,209 cycles

DOOR PAX AFT OPEN INDICATION IN FLIGHT, L2. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. DEFERRED L2 DOOR POSITION INDICATION.

Part: ENGINE — SMOKE (ZONE 100) · airframe 22,399 hrs · 15,160 cycles

SMELL OF SMOKE (PERHAPS ELECTRICAL BURNING). DECLARED EMERGENCY, REJECTED TAKEOFF BELOW 80 KTS. VISIBLE LIGHT SMOKE IN COCKPIT. FA EMERGENCY CALL STATING VISIBLE SMOKE AND BURNING SMELL IN FWD CABIN. EMERGENCY EVAC SLIDES 1L, 2L, AND 2R BLOWN. EVACUATED. ACCOMPLISHED COMP RINSE OF #1 ENGINE. PERFORMED ENGINE RUNS AT 804 904 N2 AND NO FURTHER SMELLS NOTED.

Part: SEAT TRACK — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 11,560 hrs · 7,867 cycles

CORROSION FOUND ON THE RT INBD SEAT TRACK, FRAMES 12 - 14. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01, 51-41-02, AND 51-471-03

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

FRAME 14 CROSSBEAM JUST INBD OF RT SILL IS CORRODED. CUT OUT DAMAGED SECTION AND REPAIRED FR 14 REF SRM 53-00-10.

Part: CROSSBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

FRAME 14 CROSSBEAM JUST OTBD AND RUNNING UNDER RT SEAT TRACK IS CORRODED. PREFORMED CUTOUT TO REMOVE DAMAGE IAW SRM 53-00-10. FABRICATED AND DRILLED A DOUBLER AND FILLER IAW SRM 53-00-10. FABRICATED AND DRILLED 2 ADDITIONAL SHIMS. TREATED AND PRIMED REPAIR IAW SRM 51-23-04, AND 51-23-05.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

CORRODED FLOORBOARD SUPPORT AT RT FRAME 86. REMOVED AND INSTALLED NEW FLOORBOARD SUPPORT AT RT FRAME 86 REF SRM 51-41-01 PN 170-66797-001. SEE W/O H5978 SN 443 FOR WORK DETAILS. AIRCRAFT REMAINS IN HEAVY CHECK.

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

PANEL 1431DL HAS 3 CORRODED ATTACHMENT FLANGES. BLENDED ALL THREE FLANGES ON PANEL 1431DL AND FOUND DAMAGE ON TWO TO BE OUT OF ALLOWABLE LIMITS. REMOVED, LOCATED AND DRILLED, REPLACE, AND INSTALLED FLANGES ON PANEL 1431DL REF SRM 51-40-08. RESTORED ORIGINAL FINISH REF SRM 51-23-04, 51-23-05, 51-23-06.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

FWD RT SILL FRAME 12-FRAME 14 RBL 36" - RBL 49" CORRODED. REMOVED AND REPLACED RT FLOOR SILL, FR 12-14 REF SRM 51-40-08. AIRCRAFT REMAINS IN HEAVY CHECK.

Part: SPLICE — CORRODED (FLOOR PANEL) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

CORROSION IN AFT WET AREA ON THE RT SLICE PANEL FLOOR STRUCTURE LOCATED AT FR90. REMOVED AFT WET AREA RT FLOOR PANEL SPLICE AT FR90 REF SRM 51-41-02 LOCATED DRILLED AND ALODINE NEW AFT WET AREA RT FLOOR PANEL SPLICE AT FR90 REF SRM 51-41-02, 51-23-04. AIRCRAFT REMAINS IN HEAVY CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 90-91) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

CORROSION IN AFT WET AREA ON THE RT FLOOR SUPPORT BETWEEN FRAMES 90-91. COMPLIED WITH ETD2017-170-100277. PERFORMED DOUBLER & FILLER REPAIR.

Part: SEAT TRACK — CORRODED (FRAMES 13-14) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

FWD RT BEAM OUTBOARD OF RT SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK FRAMES 12-20. IAW SRM 51-41-01, AND 51-43-03.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

CORROSION IN AFT WET AREA ON CENTER SHEAR PANEL LOCATED BETWEEN FR87-88. REMOVED CENTER SHEAR PANEL LOCATED BETWEEN FR87-88 LOCATED, DRILLED AND TREATED FASTENER HOLES ON NEW CENTER SHEAR PANEL LOCATED BETWEEN FR87-88 REF SRM 51-40-02, 51-23-04. AIRCRAFT REMAINS IN HEAVY CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 88-89) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

CORROSION IN THE AFT WET AREA ON THE LT FLOOR SUPPORT LOCATED BETWEEN FRAMES 88 - 89. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-41-01, 51-42-01, AND 51-43-03.

Part: SHEAR PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

CORROSION IN THE AFT WET AREA ON THE RT SHEAR PANEL LOCATED BETWEEN FR87-88. REMOVED AND REPLACED RT SHEAR PANEL LOCATED BETWEEN FR87-88 REF SRM 51-40-02 SRM 51-23-04. AIRCRAFT REMAINS IN HEAVY CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,435 hrs · 7,816 cycles

LT I/B SEAT TRACK CORRODED AT FRAME 19. BLENDED CORROSION AND FOUND IT TO BE 100% MATERIAL LOSS ON THE SEAT TRACK AT FRAME 19. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR DOUBLER REF SRM 53-10-10. ALODINED, PRIMED, AND PAINTED REF SRM 51-23-04, 51-23-05, 51-23-06. AIRCRAFT REMAINS IN HEAVY CHECK.

Part: LINER — OUT OF ADJUST (R1 DOOR) · airframe 9,482 hrs · 6,590 cycles

R1 DOOR INDICATION NOT SHOWING ARMED OR DISARMED. ADJUSTED R1 DOOR LINER IAW AMM 25-23-6. CONFIRMED INDICATOR SHOWING, OPS CHECK GOOD.

Part: DOOR — BINDING (L2) · airframe 8,510 hrs · 5,891 cycles

CREW REPORTED THAT THE L2 DOOR WOULD NOT OPEN. MAINTENANCE OPS CHECKED THE DOOR FROM BOTH OUTSIDE AND INSIDE IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 8,182 hrs · 5,669 cycles

CREW REPORTED THAT THE CAPTAIN`S FLASHLIGHT WAS NOT SHOWING THE RED CHARGING LIGHT. MAINTENANCE REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 8,135 hrs · 5,638 cycles

CREW REPORTED THAT THE 2 PHOTOLUMINESCENT STRIPS IN THE FIRST CLASS SECTION WERE INOPERATIVE. ACFT WAS FLOWN VIA MAINTENANCE FERRY, WHERE MAINTENANCE R & R PHOTOLUMINESCENT STRIPS IAW AMM AND OPS CHECKED GOOD.

Part: CIRCUIT BOARD — DAMAGED (LIGHTS) · airframe 6,469 hrs · 4,445 cycles

CREW REPORTED THAT THE RAINBOW LIGHTS WERE INOPERATIVE. R & R AFT LAV PCB IAW AMM AND OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 4,344 hrs · 2,913 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT DAMAGED AND WOULD NOT ILLUMINATE. MAINTENANCE R & R THE LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 4,127 hrs · 2,754 cycles

CREW REPORTED THAT THE CAPTAINS FLASHLIGHT WAS INOPERATIVE. MAINTENANCE R & R THE CAPTAINS FLASHLIGHT BATTERIES IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 3,440 hrs · 2,281 cycles

CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS INOPERATIVE.

Part: FLASHLIGHT — DIM (FWD CABIN) · airframe 2,808 hrs · 1,832 cycles

CREW REPORTED THAT THE FORWARD F/A FLASHLIGHT IS VERY DIM. MAINTENANCE R & R FORWARD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (L2 DOOR) · airframe 1,678 hrs · 1,048 cycles

CREW REPORTED THAT THE INDICATION ON THE L2 DOOR WENT RED. F/A REPORTED THAT THE DOOR DID NOT SHOW CLOSED. CREW ELECTED TO RETURN TO DEPARTURE, AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED PRESSURE CHECKS TO THE L2 DOOR IAW AMM AND ALL CHECKS PASSED. ACFT IS GOOD FOR SERVICE.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 309 hrs · 186 cycles

F/A OPENED THE L1 DOOR BEFORE DISARMING THE ESCAPE SLIDE, CAUSING IT TO FALL OUT INTO THE JETWAY. MX R & R THE L1 SLIDE AND RESERVICED THE ASSIST BOTTLE IAW AMM. OPS CHECKED GOOD.