N427YX

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,786 hrs · 16,091 cycles

FWD CENTER EMERGENCY EXIT SIGN INOPERATIVE, RE-CONNECTED CONNECTOR FOR CEILING PANEL 227ALC. AMM TASK 25-22-07. OPS CHECK GOOD.

Part: CROSSBEAM — CORRODED (ZONE 200) · airframe 22,787 hrs · 15,393 cycles

WHILE IN HEAVY CHECK- CROSSBEAM FR17 RIGHT SIDE, BELOW FLOORBOARD 226CRF HAS THREE AREAS OF CORROSION ON THE UPPER SURFACE. PERFORMED L ANGLE REPAIR FR17 IAW SRM 53-00-10/R04.

Part: CROSSBEAM — CORRODED (ZONE 200) · airframe 22,787 hrs · 15,393 cycles

WHILE IN HEAVY CHECK - CROSSBEAM FR14 BELOW FLOORBOARD 226BRF RIGHT SIDE HAS TWO AREAS OF CORROSION. PERFORMED SPLICE REPAIR FR14 RIGHT SIDE IAW SRM 53-00-10/R03.

Part: BEAM — CORRODED (ZONE 200) · airframe 22,787 hrs · 15,393 cycles

WHILE IN HEAVY CHECK - AFT PASSENGER DOOR LOWER BEAM HAS CORROSION AT FORWARD EVACUATION SIDE FITTING REPLACED LOWER BEAM IAW SRM 51-40-08

Part: STRINGER — BENT (ZONE 100) · airframe 21,063 hrs · 14,160 cycles

A/C DAMAGED BETWEEN FRA 23-26 AND STR 23R-26R. REMOVED AND REPLACED STR 25R AND STR SPLICE 24R IAW EMB 170/175 SRM 51-43-01 AND 51-43-02. ALSO REF VP-028073-2022 NR 12,13 FOR REPAIRS.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 16,241 hrs · 10,922 cycles

SUPPLEMENTAL INFORMATION: FWD PHOTOLUMINESCENT STRIP HAS MORE THAN 10 DAMAGE, NEEDS REPLACED. R&R FWD PHOTOLUMINESCENT STRIP.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,977 hrs · 10,743 cycles

CABIN EMERGENCY LIGHT INOP (NEXT TO THE LAST OVER THE AISLE). R&R #4 EMERGENCY LIGHT BATTERY.

Part: LIGHT — WORN (CABIN) · airframe 14,955 hrs · 10,055 cycles

PHOTOLUMINESCENT STRIP IN FRONT OF FWD WARDROBE WORN. R&R PHOTOLUMINESCENT STRIP PER AMM 33-50-05.

Part: SEAL REST — CORRODED (FRAMES 24-26) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING A HEAVY CHECK, THE FWD CARGO FWD SEAL REST DOME NUT RIVETS HAVE CORROSION. REMOVED AND REPLACED THE FWD CARGO FWD SEAL REST IAW SRM 51-40-08.

Part: DOUBLER — CORRODED (FRAME 19) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING A HEAVY CHECK, CORROSION WAS FOUND ON THE FWD WET AREA, AFT LT FLOOR DOUBLER CORRODED. REMOVED AND REPLACED FWD WET AREA AFT LT FLOOR DOUBLER IAW SRM 51-40-08.

Part: DOUBLER — CORRODED (FRAME 16) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING A HEAVY CHECK, CORROSION WAS FOUND ON THE FWD WET AREA FWD LT FLOOR DOUBLER FRAME 16. REMOVED AND REPLACED THE FWD LT FLOOR DOUBLER IAW SRM 51-40-08.

Part: SUPPORT — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING HEAVY CHECK, ON REMOVAL OF THE RT SHEAR PANEL, FRAMES 87 - 88, FOUND THE PANEL SUPPORT CORRODED. REMOVED AND REPLACED IAW SRM 51-40-08

Part: DOUBLER — CORRODED (FRAME 90) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

WHILE IN HEAVY CHECK - CORROSION WAS FOUND ON THE AFT WET AREA SPLICE LOCATED AT Y=10.748, FRAME 90. REMOVED AND INSTALLED A NEW DOUBLER IAW SRM 51-40-08

Part: SEAL REST — CORRODED (FRAMES 26) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING HEAVY CHECK, THE FWD CARGO AFT SEAL REST DOME NUT RIVETS HAD CORROSION. REMOVED AND REPLACED THE FWD CARGO AFT SEAL REST IAW SRM 51-40-08.

Part: SEAT TRACK — CORRODED (FRAMES 86-87) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING A HEAVY CHECK, CORROSION WAS FOUND ON THE AFT WET AREA RT INBD SEAT TRACK, Y+10.748 . REMOVED AND INSTALLED A NEW SEAT TRACK BETWEEN FRAMES 86 - 87 IAW SRM 51-40-08.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING HEAVY CHECK, CORROSION ON THE AFT WET AREA, RT SHEAR PANEL BETWEEN FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PANEL IAW SRM 51-40-08.

Part: FINGER DOUBLER — CORRODED (FRAME 24-25) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING HEAVY CHECK, THE FWD CARGO FWD DOOR BEAM FINGER DOUBLER HAD EVIDENCE OF CORROSION. REMOVED AND REPLACED THE CARGO FINGER DOUBLER IAW SRM 51-40-02.

Part: CLOSEOUT PANEL — CORRODED (FRAMES 24-26) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING HEAVY CHECK, COROOSION WAS FOUND ON THE FWD CARGO THRESHOLD CLOSE OUT PANEL. REMOVED AND REPLACED THE CLOSEOUT PANEL.

Part: SEAT TRACK — CORRODED (FRAMES 84-85) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING A HEAVY CHECK, CORROSION WAS FOUND ON THE AFT WET AREA RT INBD SEAT TRACK BETWEEEN FRAMES 84 - 85. REMOVED CORROSION, INSTALLED A FILLER AND DOUBLER IAW SRM 51-40-08.

Part: SHEAR PANEL — CORRODED (FRAMES 87-88) · corrosion level 2 · airframe 11,603 hrs · 7,876 cycles

DURING A HEAVY CHECK, CORROSION WAS FOUND ON THE AFT WET AREA, LT SHEAR PANEL BETWEEN FRAMES 87 - 88. REMOVED AND REPLACED THE SHEAR PANEL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,444 hrs · 5,855 cycles

FOUND R2 DOOR EXIT LIGHT INOPERATIVE DURING A TWO-DAY CHECK. R & R THE AFT RT EMERGENCY LIGHT BATTERY IAW AMM 33-50-01. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,639 hrs · 4,658 cycles

MAINTENANCE REPORTED THAT THE EMERGENCY BATTERY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PER EMB AMM AND OPS CHECKED GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,350 hrs · 4,459 cycles

CREW REPORTED THAT THE R1 DOOR INDICATED OPEN WHEN THE DOOR WAS UNARMED AND WHEN THE DOOR WAS CLOSED ALL INDICATIONS WERE NORMAL. MAINTENANCE PERFORMED OPS CHECK OF THE R1 DOOR IAW AMM AND OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — PULLED (EMERGENCY LIGHTS) · airframe 6,126 hrs · 4,316 cycles

CREW REPORTED THAT THE STERILE, EMERGENCY PILOT AND PILOT TO CABIN RAINBOW LIGHTS IN CABIN WERE NOT FUNCTIONING. MAINTENANCE FOUND CB FORWARD FLASH CHARGER, E15, PULLED. MAINTENANCE RESET CB IAW AMM AND OPS CHECKED GOOD.

Part: LIGHT — DAMAGED (CABIN) · airframe 4,914 hrs · 3,493 cycles

MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT BESIDE THE WARDROBE WAS DAMAGED. MAINTENANCE R & R THE LIGHT STRIP IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,908 hrs · 3,487 cycles

CREW REPORTED THAT THE EMERGENCY EXIT SIGN AT THE L2 DOOR FLOOR SIGN WAS INOPERATIVE. ACFT WAS FLOWN VIA MAINTENANCE FERRY, WHERE MAINTENANCE R & R L2 DOOR EMERGENCY BATTERY IAW AMM AND OPS CHECKED GOOD.

Part: FLASHLIGHT — MISSING (CABIN) · airframe 4,496 hrs · 3,193 cycles

MAINTENANCE REPORTED THAT THE FORWARD F/A FLASHLIGHT WAS MISSING. MAINTENANCE REPLACED FORWARD F/A FLASHLIGHT IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,813 hrs · 1,267 cycles

AFT EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY BATTERY PACK IAW AMM AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 1,813 hrs · 1,267 cycles

R1 DOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY BATTERY PACK IAW AMM AND OPS CHECKED GOOD.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 897 hrs · 663 cycles

CREW REPORTED THAT THE L1 DOOR SLIDE WAS FALLING OUT THE DOOR. MAINTENANCE INSPECTED AND FOUND THE SLIDE PARTIALLY DEPLOYED WITH THE ASSIST BOTTLE ENGAGED. MAINTENANCE REPLACED THE SLIDE & DIAPHRAM IAW AMM, WITH NO LEAKS NOTED. ACFT IS GOOD FOR SERVICE.