N415YX

Part: HEATER — FAILED (ZONE 200) · airframe 25,449 hrs · 17,337 cycles

WINDSHIELD HEATER 2 FAIL, WINDSHIELD SHATTERED APPROXIMATELY AT FL200. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FO WINDSHIELD.

Part: BATTERY — NO TEST (ZONE 200) · airframe 24,111 hrs · 16,340 cycles

EMERGENCY LIGHT FWD LH BATTERY FAILED FUNCTIONAL CHECK. R&R FWD LH EMERGENCY LIGHT BATTERY.

Part: STRIP — INOPERATIVE (ZONE 100) · airframe 21,766 hrs · 14,646 cycles

ROW 1 PHOTOLUMINESCENT STRIPS WON'T ILLUMINATE NOR WILL THE STRIP IN FRONT OF THE CLOSET. R&R PHOTOLUMINESCENT STRIPS AT ROW 1 LH RH AND IN FRONT OF CLOSET.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,047 hrs · 13,414 cycles

PHOTOLUMINESCENT STRIPS IN FIRST CLASS NOT WORKING. R&R FWD FIRST CLASS PHOTOLUMINESCENT INSERT.

Part: STRUCTURE — DAMAGED (L1 DOOR) · airframe 17,916 hrs · 12,004 cycles

AIRCRAFT DAMAGE AFT OF L1 DOOR AT FRA 23 AND FRA 24, STR 18L AND 19L. REPAIRED IAW ETD2020-170-029797, ALSO REF VP-033479-2020 N/R 1 FOR WORK PERFORMED.

Part: GLOWSTRIP — WORN (CABIN) · airframe 17,534 hrs · 11,747 cycles

PHOTOLUMINESCENT STRIP WORN IN FRONT OF WARDROBE. R&R PHOTOLUMINESCENT STRIP.

Part: GUSSET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,364 hrs · 11,634 cycles

DURING HEAVY CHECK MAINTENANCE FOUND GUSSET @ RH INBD SEAT TRACK CORRODED. REMOVED AND REPLACED GUSSET AT RH I/B SEAT TRACK AT FR 84.REF EMB SRM 51-40-08. A/C REMAINS IN CHECK.

Part: SPAR — CRACKED (LT WING) · airframe 17,364 hrs · 11,634 cycles

DURING HEAVY CHECK MAINTENANCE FOUND LH WING OUTBD SPAR 1 HAS SUSPECTED CRACK AT LOWER FLANGE RADIUS OUTBD OF LAST RIB. REMOVED AND REPLACED LH SPAR 1 OUTBOARD SEGMENT. REF SRM 51-40-08. PREPPED, PRIMED,AND PAINTED LH WING SPAR 1 REPAIR REF EMB SRM 51-23-04, SRM 51-23-05, SRM 51-23-06. A/C REMAINS IN CHECK.

Part: SPAR — CRACKED (RT WING) · airframe 17,364 hrs · 11,634 cycles

DURING HEAVY CHECK MAINTENANCE FOUND RH WING SPAR 1 IS CRACKED OUTBD OF LAST WING RIB ON LOWER SURFACE OF SPAR. REMOVED AND REPLACED RH SPAR 1 OUTBOARD SEGMENT. REF SRM 51-40-08. PREPPED, PRIMED,AND PAINTED RH WING SPAR 1 REPAIR REF EMB SRM 51-23-04, SRM 51-23-05, SRM 51-23-06. A/C REMAINS IN CHECK.

Part: POWER UNIT — FAULTY (CABIN) · airframe 14,350 hrs · 9,617 cycles

AFT SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT FROM NR 4 POSITION FOR RT AFT SERVICE DOOR EMERGENCY LIGHTS REF AMM 33-50-07-400-801A. OP CHECK GOOD. SEE W/O H6697 SN 017 FOR WORK DETAILS.

Part: POWER UNIT — INOPERATIVE (CABIN) · airframe 13,318 hrs · 8,928 cycles

EMERGENCY LIGHT 4TH LIGHT AFT OF COCKPIT INOP. R&R EMERGENCY LIGHT POWER UNIT 3 IAW AMM 33-50-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,770 hrs · 8,567 cycles

OVERHEAD EMERGENCY LIGHT MID CABIN INOP. R&R OVERHEAD EMERGENCY LIGHT ASSEMBLY IAW AMM 33-50-13.

Part: SEAL REST — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

REMOVED AND REPLACED FWD CARGO DOOR CENTER LOWER SEAL REST REF SRM 51-40-02.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

REMOVED, REPAIRED AND REINSTALLED WASTE BOX. REMOVED AND REPLACED CORRODED BONDING PLATE ON UPPER SURFACE SRM 51-73-00 PN 170-65079-405.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

REMOVED AND REPLACED FWD CARGO DOOR LOWER BEAM FLOOR PANEL SUPPORT. REF SRM 51-40-02 PN170-67451-001.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

REMOVED AND REPLACED RT BEAM PN 170-65669-004 REF SRM 51-40-08.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

REMOVED AND REPLACED RT SHEAR PLATE FR87-88 REF SRM 51-40-08, 51-23-05, 51-23-06 PN 170-91919-001.

Part: SPLICE — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

SPLICE CORRODED AT FRAME 90. INSTALLED A NEW SPLICE IAW 51-40-08.

Part: PANEL SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

REMOVED AND REPLACED CENTER FUSELAGE III WET AREA 53-23 LT AFT PANEL SUPPORT FR 86/90 REF SRM 51-40-08, 51-40-02, 51-23-04, 51-23-06, CPM 51-25-00 P/N 170-86139-005.

Part: THRESHOLD — CORRODED (FRAMES 85-88) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

THRESHOLD TRIM CORRODED. REPLACED AFT PAX DOOR CENTER THRESHOLD METAL TRIM IAW SRM 51-41-02, AND 51-40-08.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 11,707 hrs · 7,914 cycles

INSTALLED RT SILL AT FR13 & FR14 PN170-05663-003 REF SRM 51-40-08 APPLIED TOPCOAT RT SILL AT FR 13 AND FR 14 PN170-05663-003 REF SRM 51-23-06.

Part: SLIDE — CRACKED (L1 DOOR) · airframe 11,707 hrs · 7,914 cycles

CRACK BACKBOARD ON L1 DOOR SLIDE PN 4A4030-7 SN ED0138. REMOVED AND REPLACED IAW AMM 52-11-40.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 11,707 hrs

REMOVED AND REPLACED CENTER SHEAR PLATE PANEL PN: 170-65928-001 REF SRM 51-40-08.

Part: BATTERY PACK — UNSECURE (FLASHLIGHT) · airframe 7,665 hrs · 5,315 cycles

CREW REPORTED THAT THE AFT FLIGHT ATTENDANT FLASHLIGHT WAS INOPERATIVE. MAINTENANCE SECURED AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 7,500 hrs · 5,203 cycles

CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE RESET ACFT POWER IAW AMM AND OPS CHECKED GOOD.

Part: BRAKE ASSY — SLUGGISH (MLG) · airframe 6,661 hrs · 4,642 cycles

THE CREW REPORTED THAT THE AIRCRAFT'S BRAKES WERE SLUGGISH ON LANDING. THE ACFT CAME TO A STOP AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE BLED THE BRAKES. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

Part: PUMP — SPLIT (HYD SYSTEM) · airframe 5,166 hrs · 3,570 cycles

CREW REPORTED A HYD SYSTEM 1 LOW QUANTITY MESSAGE. DID NOT DECLARE AN EMERGENCY AND DIVERTED, LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN PUMP SPLIT AT INTERFACE. MAINTENANCE R & R ENGINE DRIVEN PUMP IAW AMM AND OPS CHECKED GOOD.

Part: NONE — NONE (NONE) · airframe 5,109 hrs · 3,537 cycles

CREW REPORTED THAT THE AFT EMERGENCY LIGHTS WOULD NOT TURN OFF. MAINTENANCE PERFORMED, OPS CHECK OF THE EMERGENCY LIGHTS SYSTEM IAW AMM AND LIGHTS, OPS CHECKED GOOD. ACFT IS GOOD FOR SERVICE.

Part: LINE — DISCONNECTED (HYD SYSTEM) · airframe 4,722 hrs · 3,235 cycles

CREW RECEIVED A HYD NR 1 LOW QUANTITY MESSAGE. CREW ELECTED TO RETURN TO DEPARTURE, BUT DID NOT DECLARE AN EMERGENCY. CREW LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R NR 1 ENGINE PSI HYD LINE FROM PYLON TO QD DISCONNECT IAW AMM AND OPS CHECKED GOOD.

Part: LIGHT — WORN (CABIN) · airframe 4,702 hrs · 3,215 cycles

MAINTENANCE REPORTED THAT THE 2 FORWARD PHOTOLUMINESCENT STRIPS WERE WORN. MAINTEANCE R & R PHOTOLUMINESCENT STRIPS IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 2,269 hrs · 1,499 cycles

CREW REPORTED THAT THE AFT F/A FLASHLIGHT WAS NOT CHARGING. MAINTENANCE R & R AFT F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.