N410YX

Part: CROSSBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 27,810 hrs · 19,073 cycles

FR 84 CROSSBEAM HAS CORROSION. REPAIRED CROSSBEAM WITH INTERNAL DOUBLER PER ETD2025-170-903688

Part: DOUBLER — CHAFED (ZONE 400) · airframe 27,810 hrs · 19,073 cycles

CHAFE DOUBLER ON CENTER HEAT BLANKET ON LH INBD TR, FABRICATED A PATCH REPAIR AND WELDED REPLACEMENT ON PER 170EA-78-31-0004

Part: DOUBLER — CHAFED (ZONE 400) · airframe 27,810 hrs · 19,073 cycles

CHAFE DOUBLER ON RH OUTBD TR CENTER HEAR BLANKET. FABRICATED REPAIR PATCH, INSTALLED NEW CHAFE PLATE PER 170EA-78-31-0004 MR_1

Part: A/C PACK — FAILED (NR 2) · airframe 26,147 hrs · 17,899 cycles

PAC 2 FAIL DURING ENG START WITH SMOKE SMELL. REMOVED AND REPLACED PACK 2 ACM REF AMM 21-51-05. OPS CHECK GOOD.

Part: LIGHT — UNKNOWN (UNKNOWN)

PHOTOLUMINESCENT STRIPS AT ROWS 1 AND 2 FWD CLOSET INOP. R&R EMERGENCY FLOOR INDICATION STRIPS AT FWD CLOSET AND ROW 1 AND 2.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 22,625 hrs · 15,397 cycles

LH HORIZONTAL STAB RIB 14 CRACKED AT UPPER TRAILING EDGE; REMOVED AND REPLACED LH HSTAB RIB 14. REF SRM 51-40-08.

Part: WINGLET — DAMAGED (RT WING) · airframe 22,625 hrs · 15,397 cycles

RH WINGLET UPPER EDGE HAS COMPOSITE DAMAGE POSSIBLE LIGHTNING STRIKE. REMOVED AND REPLACED RH WINGLET REF E175 AMM 57-35-00.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 22,625 hrs · 15,397 cycles

FWD CARGO DOOR CUTOUT-LOWER HORIZONTAL BEAM FWD AND AFT FINGER DOUBLERS HAVE CORROSION/CHAFFING AS MARKED. REMOVED AND REPLACED FWD CARGO DOOR CUTOUT-LOWER HORIZONTAL BEAM FWD AND AFT FINGER DOUBLERS REF SRM 51-40-08.

Part: PRESSURE SWITCH — MALFUNCTIONED (PARKING BRAKE) · airframe 18,277 hrs · 12,253 cycles

PARKING BRAKE SHOWS SET IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R EMERGENCY BRAKE PRESSURE SWITCH.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 18,032 hrs · 12,105 cycles

EMERGENCY LIGHT POWER UNIT CENTER FUSELAGE OUTBOARD MALFUNCTIONING. R & R NUMBER 3 ELPU.

Part: CROSSBEAM — CORRODED (FRAME 17) · airframe 17,421 hrs · 11,705 cycles

WHILE IN HEAVY CHECK CORROSION ON FR 17 CROSSBEAM BETWEEN LT AND RT SEAT TRACK & OUTBOARD OF RT SEAT TRACK. REPAIRED BY CUTOUT, USING FILLER, DOUBLERS PER SRM 53-00-10/R3 FIG 203.

Part: GLOWSTRIP — INOPERATIVE (CABIN) · airframe 16,897 hrs · 11,345 cycles

PHOTOLUMINESCENT STRIPS FROM ROW 2C TO FORWARD CLOSET INOPERATIVE ON AIRCRAFT. R&R PHOTOLUMINESCENT STRIP FROM FWD CLOSET TO 2ND ROW RH SIDE IAW SAMM 33-50-00-1.

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION FOUND ON THE GUSSET PLATE AT FRAME 90. REMOVED AND REPLACED GUSSET IAW SRM 51-40-08.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION WAS FOUND ON THE RT SHEAR PANEL BETWEEN FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-40-08

Part: SPLICE PLATE — CORRODED (FRAME 89) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION FOUND ON THE SPLICE PLATE AT FRAME 89, +273. REMOVED AND REPLACED THE SPLICE PLATE IAW SRM 51-43-03

Part: CLOSEOUT PANEL — CORRODED (FRAMES 77-80) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION ON THE AFT CARGO CLOSE OUT PANEL. REMOVED AND REPLACED THE CLOSE OUT PANEL IAW SRM 53-01-45.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION WAS FOUND ON THE CENTER SHEAR PANEL BETWEEN FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-40-08

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION WAS FOUND ON THREE PROFILES ON PANEL 1441FR. REMOVED AND REPLACED THE PROFILES.

Part: SPLICE PLATE — CORRODED (FRAME 84) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION WAS FOUND ON THE SPLICE PLATE AT FRAME 84, -673. REMOVED AND REPLACED THE SPLICE PLATE IAW SRM 51-43-03,

Part: PROFILE — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION WAS FOUND ON THREE PROFILES ON PANEL 1431DL. REMOVED AND REPLACED THE PROFILES.

Part: FLOOR SUPPORT — CORRODED (FRAME 84) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION WAS FOUND ON THE RT FLOOR SUPPORT AT FRAME 84. COMPLIED WITH A PERMANANT REPAIR IAW ETD 2018-170-057854

Part: GUSSET — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION FOUND ON THE GUSSET PLATE AT FRAME 90. REMOVED AND REPLACED THE GUSSET IAW SRM 51-40-08.

Part: SPLICE PLATE — CORRODED (FRAME 84) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

CORROSION WAS FOUND ON THE SPLICE PLATE AT FRAME 84, +673. REMOVED AND REPLACED SPLICE PLATE IAW SRM 51-43-0.

Part: FLOOR SUPPORT — CORRODED (FRAME 98) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

RT FLOOR SUPPORT AT FRAME 89 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-14) · corrosion level 2 · airframe 11,699 hrs · 8,012 cycles

RT FLOOR SUPPORT, FRAMES 12 TO 14 CABIN FLOOR CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-08.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,682 hrs · 6,691 cycles

FWD EMERGENCY LIGHT CEILING INOPERATIVE. R & R RT FWD EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,196 hrs · 6,381 cycles

FIRST CEILING EMERGENCY LIGHT IN COACH IS INOPERATIVE. R & R THE NR 2 BATTERY PACK IAW AMM 33-50-01. OPS CHECKED NORMAL.

Part: SLIDE — PARTIAL DEPLOY (DOOR) · airframe 7,635 hrs · 5,338 cycles

FLIGHT ATTENDANT OPENED THE DOOR WITHOUT DISARMING DOOR WHICH CAUSED THE SLIDE TO PARTIALLY DEPLOY. MAINTENANCE REMOVED AND REPLACED SLIDE PER AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 7,170 hrs · 5,035 cycles

CREW REPORTED THAT THE AFT EMERGENCY LIGHT ASSEMBLY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 5,642 hrs · 3,941 cycles

MAINTENANCE REPORTED THAT THE CAPTAIN`S FLASHLIGHT WAS DIM. MAINTENANCE R & R THE FLASHLIGHT BATTERIES IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 5,610 hrs · 3,920 cycles

CREW REPORTED THAT THE FURTHEST AFT EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE R & R NR 4 EMERGENCY POWER UNIT BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 1,180 hrs · 736 cycles

CREW REPORTED THAT WITH THE BRAKES IN AUTO MODE ON MEDIUM, THE ACFT SEEMED LIKE IT WOULD NOT SLOW DOW EVEN WHILE PRESSING DOWN ON PEDALS AS HARD AS POSSIBLE. AFTER THE ACFT HIT 10 KNOTS THE PLANE WOULD STOP SUDDENLY. MAINTENANCE BLED THE BRAKE SYSTEMS, INSPECTED BRAKES AND TEMP SENSORS AND PEFORMED TAXI CHECKS IAW AMM. NO DEFECTS NOTED AND ACFT IS GOOD FOR SERVICE.

Part: HANDLE — DIRTY (L1 DOOR) · airframe 312 hrs · 189 cycles

CREW REPORTED THAT THE L1 DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED IAW AMM, REMOVED DEBRIS FROM THE L1 DOOR HANDLE AND DOOR OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: UNKNOWN — VIBRATION (R1 DOOR) · airframe 310 hrs · 188 cycles

R1 DOOR HAD EXCESSIVE VIBRATION AND A HUMMING NOISE. AN EMERGENCY WAS NOT DECLARED, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK OF DOOR IAW AMM AND FOUND NO DEFECTS. ACFT IS GOOD FOR SERVICE.

Part: DEFLECTOR — UNKNOWN (R2 DOOR) · airframe 273 hrs · 166 cycles

CREW REPORTED A LOUD HUM COMING FROM THE R2 DOOR. AN EMERGENCY WAS NOT DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE R & R THE R2 DOOR DEFLECTOR IAW AMM AND OPS CHECKED GOOD.