N315NV

Part: LENS — BROKEN (ZONE 200) · airframe 52,975 hrs · 34,628 cycles

(AIRCRAFT NOT GROUNDED) OVERWING (14ABC) EXIT SIGN COVER FOR EXIT LIGHT LED ASSEMBLY BROKEN. REMOVED AND REPLACED BROKEN COVER FOR LIGHT ASSY AT (14ABC), IAW AMM 33-51-13-000/400-001-A.NO DEFECTS NOTED. THIS CLEARS M313 MDDR #217727 EA 10-2025-021.

Part: PBE — DAMAGED (ZONE 200) · airframe 51,871 hrs · 34,050 cycles

(AIRCRAFT NOT GROUNDED) FWD PBE LOCATED IN FWD F/A JUMPSEAT DAMAGED. RESECURED PBE IAW SIP.

Part: TARGET — OUT OF ADJUST (ZONE 200) · airframe 51,128 hrs · 33,620 cycles

(AIRCRAFT NOT GROUNDED) DOOR R FWD EMER EXIT ECAM APPEARED CLIMBING THRU 8000FT REMAINED ON FOR ENTIRE FLIGHT. / ADJUSTED R FWD EMER EXIT COVER FLAP TARGET IAW AMM 52-71-13-400-001-A. OPS CHECK GOOD."

Part: CONNECTOR — BROKEN (ZONE 200) · airframe 51,127 hrs · 33,619 cycles

(AIRCRAFT NOT GROUNDED) NRC 2000-0114: L/H OVERWING EMERGENCY EXIT SIGN LIGHT CONNECTOR BROKEN. / L/H OVERWING EMERGENCY EXIT SIGN LIGHT REMOVED AS PER AMM TASK 33-51-16-000-001-A AND REPLACED AS PER AMM TASK 33-51-16-400-001-A."

Part: SKIN — GOUGED (ZONE 100) · airframe 51,127 hrs · 33,619 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 2000-0039: (S/M) 34240-09 EXTERNAL FUSELAGE SKIN, BTW FR56 - FR57 AND STGR22L - STGR23L, GOUGE FOUND. / EXTERNAL FUSELAGE SKIN, BTW FR56 - FR57 AND STGR22L - STGR23L, GOUGE BLENDED AND FOUND OUT OF LIMITS AS PER SRM 53-41-11-283-001 DIAGRAM 001 REV. 149. EXTERNAL FUSELAGE SKIN REPAIRED AS PER SRM 53-41-11-300-019 REV. 149. REPAIR CLASSIFIED CATEGORY B WITH FUTURE INSPECTIONS REQUIRED AS PER SRI 53-41-11-205-048 REV. 149. INSPECTION THRESHOLD FROM TIME OF REPAIR EMBODIMENT: 40,200FC / 80,400FH, WHICHEVER COMES FIRST. SUBSEQUENT INSPECTION THRESHOLD: 5,000FC / 10,000FH, WHICHEVER COMES FIRST. METHOD OF INSPECTION: ULTRASONIC / HFEC. SEE AWS FOR DETAILS AND NDT REPORTS."

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 51,127 hrs · 33,619 cycles

(AIRCRAFT NOT GROUNDED) NRC 9000-0007: OVERWING EXIT FWD L/H EMERGENCY LIGHT 61WL BACKSHELL BRONKEN / OVERWING EXIT FWD L/H EMERGENCY LIGHT 61WL BACKSHELL REPLACED IAW AMM 33-51-15-000/400-001-A. TEST TRANSFERRED TO NRC 4002598-7000-0001 AWS-1.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 50,259 hrs · 33,212 cycles

FWD MEGAPHONE INOP AND EXPIRED / REMOVE AND REPLACED FWD MEGAPHONE IAW AMM25-65-51-920-001-A. OPS CHECK GOOD."

Part: BATTERY PACK — UNKNOWN (UNKNOWN) · airframe 50,121 hrs · 33,148 cycles

DURING EPSU BATTER TEST BATTERIES FAILED CAPACITY TEST. / INTALLED NEW EPSU BATTERIES AT POSITIONS: 10WL, 11WL, 12WL, 13WL IAW AIRBUS AMM 33-51-38-000-001-A. NO FURTHER DEFECTS NOTED"

Part: MEGAPHONE — INOPERATIVE (FWD CABIN) · airframe 48,500 hrs · 32,244 cycles

FWD MEGAPHONE IS INOPERATIVE. REPLACED FWD MEGAPHONE IAW AMM 25-65-51. OPS CHECKS GOOD.

Part: EPSU — NONE · airframe 48,060 hrs · 31,996 cycles

EPSU (11WL) FAILS EMERGENCY LIGHT TEST, BATTERY FAULT / REMOVED AND REPLACED EPSU BATTERY AT 11WL LEFT CABIN IAW AMM 33-51-38-000-001A AND 33-51-38-400-001A OPS CHECK GOOD."

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 47,854 hrs · 31,875 cycles

DURING THE STRUCTURAL INSPECTION PER TASK 534147-01-2 WERE FOUND ON UPPER FUSELAGE, AFT PASSENGER CABIN AT FR68+68+150MM,+Y160.5, FLOORBEAM WITH CORROSION OUT LIMITS . DUE TO THIS FACT THE PART WAS REPLACED PER NEW BEAM P/N D5347219620000 IAW A319 SRM 51-72-11-911-001

Part: NONE — NONE · airframe 47,677 hrs · 31,789 cycles

AFT FA FLASHLIGHT INOP. / REPLACED AFT FA FLASHLIGHT BATT., CHECKS NORMAL, IAW LOPA# A1250004L03."

Part: NONE — NONE · airframe 47,282 hrs · 31,598 cycles

FWD RIGHT F/A FLASHLIGHT INOP. / REMOVED AND REPLACED F/A FLASHL;IGHT PER A320 EMERGENCY EQUIPMENT LOPA."

Part: MEGAPHONE — INOPERATIVE · airframe 47,272 hrs · 31,594 cycles

FWD F/A MEGA-PHONE BATTERY DIMINISHED / REMOVE & REPLACED MEGAPHONE REF S.I.P."

Part: NONE — NONE · airframe 47,219 hrs · 31,565 cycles

F/A MEGAPHONE NOT WORKING. / CHENGED BATTERIES AND REAPPLIED MX-024 STICKER IAW GMM 21.13.1.2. OPS CHECKED GOOD"

Part: NONE — NONE · airframe 47,080 hrs · 31,487 cycles

R2 SLIDE DOES NOT ARMED IN FLIGHT / ADJUSTED R2 DOOR SLIDE ARMING HANDLE PROXIMITY SENSOR IAW AMM 52-71-00-820-002-A01"

Part: EPSU — FAILED INSP · airframe 47,038 hrs · 31,460 cycles

WHILE PREFORMING EPSU EMERGENCY LIGHT TEST FOUND BATTERIES AT LOCATIONS 10WL AND 13WL WOULD NOT TEST / REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES AT LOCATIONS 10WL AND 13WL IAW AMM 33-51-38-000-002-A"

Part: DOOR — NONE (ZONE 800) · airframe 46,582 hrs · 31,224 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H AFT DOOR FRAME, FRAME 68 DOOR STOP #3, OUTBOARD LOWER HOLE HAS A DAMAGED/OUT OF ROUND INDICATION. S/O 193124 N/R 30093 NR00832597

Part: FRAME — CRACKED (ZONE 800) · airframe 46,582 hrs · 31,224 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND L/H AFT PASSENGER FRAME, FRAME 66, DOOR STOP #1 HAS A CRACK INDICATION IN THE INBOARD LOWER HOLE OF FRAME AT THE 7 O'CLOCK POSITION.

Part: WARNING MESSAGE — ILLUMINATED (CABIN PRESSURE) · airframe 46,508 hrs · 31,178 cycles

WE EXPERIENCED A CABIN DEPRESSURIZATION DURING DESCENT. MULTIPLE ECAM MESSAGES WERE RECEIVED. IN ORDER THEY ARE: VENT EXTRACT FAULT, VENT BLOWER FAULT, CAB PR EXCESS CAB ALT, VENT EXTRACT FAULT, VENT BLOWER FAULT, CAB PR SAFETY VALVE OPEN. / REF W/O 439476,NRT 820903,820946,820763. A/C OK FOR SERVICE AT THIS TIME."

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 45,676 hrs · 30,731 cycles

EPSU BATT (11WL) FAILED EPSU TEST. REPLACED EPSU BATT (11WL) W/REF TO AMM 33-51-38 PB 401. OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,963 hrs · 29,881 cycles

EPSU BATTERY FIN# 13WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"

Part: BATTERY — DISCHARGED (CABIN) · airframe 43,950 hrs · 29,874 cycles

EPSU BATTERY FIN# 10WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"