N217NV

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 52,067 hrs · 33,026 cycles

PERFORMED NDT EDDY CURRENT INSPECTION I/A/W AIRBUS 320 NTM TASK 51-10-08-250-803-A01. @ L/H FWD FUSELAGE @ FRAME 14 BETWEEN STRINGERS 12-13 FOUND CRACK AFT OF RIVET 9MM LENGTH/INSTALLED EXTERNAL DOUBLER AND FILLER IAW TD/81261153/005/2023#A. SEE NR1178600, NR1178631, NR1178632, NR1178666, NR1178671 AND CT1178606 OR ADDITIONAL WORK ACCOMPLISHED."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 51,224 hrs · 32,608 cycles

ALL EMERGENCY EXIT SIGNS HAVE 1 OR MORE LAMPS INOP. / REMOVED AND REPLACED INOP LAMPS OF ALL EMERGENCY EXIT SIGNS REF AMM 33-51-16-000-001-A AND 33-51-16-400-001-A AND CMM 33-50-03. OPS CHECK GOOD."

Part: SKIN PANEL — NICKED (ZONE 100) · airframe 50,587 hrs · 32,324 cycles

DURING A VISUAL INSPECTION AS PER ALLEGIANT TASK IT WAS FOUND THE LOWER FUSELAGE SKIN WITH A NICK AT FR26+385MM BETWEEN STR42L AND STR43L. THE REPORTED DAMAGED AREA WAS REPAIRED I/A/W A320 SRM 53-21-11-300-076 PARAGRAPH 2A, FIGURE 001. SEE COOPESA WORK ORDER A1M146, 1-19 FOR FURTHER DETAILS.

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 50,750 hrs · 32,406 cycles

WHEN ACTIVATED L2AND R2 EMERGENCY LIGHTS ILLUMINATE FOR 15-20 SECONDS AND THEN EXTINGUISH / REMOVED & REPLACED AFT BATTERY PACK OPS CK NORMAL IAW AMM 33-51-400-001A"

Part: SKIN — CORRODED (ZONE 500) · airframe 50,587 hrs · 32,324 cycles

DURING THE STRUCTURAL INSPECTION PER WORK ZL-575-01-1-001 CORROSION ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 16 AND RIB 20 WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTATCTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81140764. THE REPAIR WAS PERFORMED UNDER COOPESA JOB: A1M146 JOB: (ITEM 5-2)

Part: SKIN — CORRODED (ZONE 600) · airframe 50,587 hrs · 32,324 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-500-03-1-002, CORROSION AT RH WING TEOH BETWEEN RIB 7 AND RIB 8 WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81140719. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB: A1M146 (ITEM 6-6)

Part: SKIN — CORRODED (ZONE 600) · airframe 50,587 hrs · 32,324 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-500-03-1-002 , IT WAS FOUND AT RH WING TEOH AREAS BETWEEN RIB 10 TO RIB 13 WITH CORROSION. DAMAGED WAS FOUND BEYOND SRM LIMITS AND AIRBUS WAS CONTACTED IN ORDER TO OBTAIN REPAIR INSTRUCTIONS.CORRECTIVE ACTIONS: AIRBUS PROVIDED REPAIR INSTRUCTIONS AND FINAL APPROVAL UNDER DOSSIER 81140719, THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1M146 ITEM 6-5.

Part: SKIN — CORRODED (ZONE 600) · airframe 50,587 hrs · 32,324 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-500-03-1-002, CORROSION AT RH WING TEOH AREAS BETWEEN RIB 13 AND RIB 16 WAS FOUND. THE DAMAE WAS FOUND BEYOND SRM LIMITS. AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81140719 AND REPAIR WAS DOCUMENTED UNDER COOPESA JOB: A1M146 (ITEM 6-45)

Part: SKIN — CORRODED (ZONE 500) · airframe 50,587 hrs · 32,324 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-575-01-1-001 CORROSION ON LH WING TOP SKIN PANEL 2 LOWER SURFACE. BETWEEN RIB 13 AND RIB 16. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81140764. THE REPAIR WAS PERFORMED UNDER COOPESA JOB: A1M146 (ITEM 5-2)

Part: SKIN — CORRODED (ZONE 500) · airframe 50,587 hrs · 32,324 cycles

DURING THE STRUCTURAL INSPECTION PER WORK ZL-575-01-1-001 CORROSION ON LH WING TOP SKI PANEL 2 LOWER SURFACE BETWEEN RIB 10 AND RIB 12 WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81140764. THE REPAIR WAS PERFORMED UNDER COOPESA JOB: A1M146 (ITEM 5-27)

Part: SKIN — CRACKED (ZONE 600) · airframe 50,587 hrs · 32,324 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-575-01-1-002, ON RH WING TEOH ARE HOLE # 207 WAS FOUND WITH CRACK INDICATION. DUE THE DAMAGE IS BEYOND THE SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED DOSSIER 81140719 WITH REPAIR INSTRUCTIONS. THE DAMAGE WAS REPAIRED UNDER JOB: A1M146 ( ITEM 6-47).

Part: SIGN — INOPERATIVE · airframe 50,158 hrs · 32,107 cycles

L-2 DOOR EXIT LIGHT HAS BULBS OUT. / REMOVED AND REPLACED BULBS ON L-2 DOOR EXIT LIGHT SIGN IAW AMM 33-51-16-PB-401. OPS CHECK GOOD."

Part: NONE — NONE · airframe 49,832 hrs · 31,941 cycles

FA REPORTS ""L1 EXIT SIGN IS NOT LIGHTED PROPERLY"". THIS IS THE SIGN JUST ABOVE THE L1 DOOR / RELAMPED EMERGENCY EXIT SIGN OVER L1 DOOR IAW AMM 33-51-16 PB 401 OPS CHECK GOOD."

Part: FLASHLIGHT — INOPERATIVE · airframe 49,079 hrs · 31,518 cycles

F/A REPORTS AFT F/A JS FLASHLIGHT INOP / REMOVED AND REPLACED AFT FA FLASHLIGHT BATTERY IAW CMM 25-60-02. OPS CHECK GOOD."

Part: COVER PLATE — CRACKED (HORIZONTAL STAB) · airframe 46,621 hrs · 30,204 cycles

DURING SCHEDULED INSPECTION, A TEMPORARY REPAIR FOR CRACK DAMAGE TO RT THS LEADING EDGE STEEL PROTECTIVE COVER REQUIRED A PERMANENT REPAIR S/O 193116 ROUTINE NR 9006.

Part: SKIN — CORRODED (RT WING) · airframe 46,621 hrs · 30,204 cycles

DURING SCHEDULED AT HAECO LAKE CITY, FLORIDA FOUND RIGHT WING UPPER SURFACE TRAILING EDGE ON AREA RIB 26 AND 27 HAS CORROSION. S/O 1931116 N/R 20206.

Part: COVER PLATE — CRACKED (HORIZONTAL STAB) · airframe 46,621 hrs · 30,204 cycles

DURING SCHEDULED INSPECTION, A TEMPORARY REPAIR FOR CRACK DAMAGE TO RT THS LEADING EDGE STEEL PROTECTIVE COVER REQUIRED A PERMANENT REPAIR S/O 193116 ROUTINE NR 9006.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 46,621 hrs · 30,204 cycles

DURING SCHEDULED INSPECTION, FOUND 2 EACH DENTED AREAS THAT REQUIRED A PERMANENT REPAIR, IAW A320 SRM 57-33-00-300-102 ZONE 2 PG 3 AND A320 SRM 57-33-00-300-100 ZONE 2 PG 3-5. S/O 193116 ROUTINE NR 9004.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,372 hrs · 30,061 cycles

EMERGENCY EXIT LIGHT BULBS INOPERATIVE. REPLACED THE BULBS.

Part: EPSU — FAILED (CABIN) · airframe 45,944 hrs · 29,826 cycles

EPSU BATTERIES FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,464 hrs · 29,592 cycles

RH EMERGENCY EXIT SIGN HAS BULBS INOP / REPLACED INOP BULBS"

Part: BULB — INOPERATIVE (EMEGENCY LIGHT) · airframe 45,464 hrs · 29,592 cycles

LH EMERGENCY EXIT SIGN HAS BULBS INOP / REPLACED INOP BULBS"

Part: OIL SYSTEM — LEAKING (APU) · airframe 38,029 hrs · 25,608 cycles

PACKS PRODUCE DIRTY GYM SOCK ODOR. PERFORMED ULTRA-VIOLET INSPECTION ON APU AND FOUND SOME OIL RESIDUE IN THE APU INLET PLENUM. CLEANED RESIDUE AND RAN APU AND NO NEW RESIDUE WAS FOUND.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 37,891 hrs · 25,553 cycles

WHEN DESCENDING BELOW 5,000 AGL COCKPIT AND FWD CABIN SMELL LIKE DIRTY SOCKS. FROM TSM FAULT ISOLATION 49-00-00 FOUND APU OIL OVER SERVICED. REMOVED APPROX 1 QT OIL FROM RESERVOIR. BOTH RECIRC FILTERS REPLACED.

Part: MEGAPHONE — INOPERATIVE (FWD CABIN) · airframe 34,739 hrs · 24,006 cycles

FWD F/A MEGA PHONE INOPERATIVE. R & R FWD MEGAPHONE, OPS CHECK GOOD, REF GMM 21-4-5-12".

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 34,383 hrs · 23,829 cycles

AT CRUISE, ALTITUDE WITH BMC 2 OPERATING THE PRESSURIZATION, THE CABIN PRESS OCCASIONALLY VARIED +- 500 FPM ALONG WITH A RUSHING AIR SOUND BELOW THE COCKPIT FLOOR. REF LOG PAGES 588359, 588365 FOR CORRECTIVE ACTIONS. PERFORMED BMC2 & CABIN PRESSURIZATION CHECKS & SYS OPERATIONS CHECKED GOOD IAW AMM 36-20-00, NO DEFECTS NOTED.

Part: COVER — BROKEN (L1 DOOR) · airframe 34,329 hrs · 23,799 cycles

L1 DOOR EMER LIGHT COVER IS BROKEN. ITEM IS TRANSFERRED TO NEF 25-01A-07 NR 19893 CAT D. L1 DOOR EMER LIGHT COVER IS SECURED.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,805 hrs · 23,526 cycles

EMERGENCY FLASHLIGHT FWD JUMP SEAT INOPERATIVE. REPLACED FLASHLIGHT BATTERY & FLASHLIGHT HOLDER IAW AMM 25-65-00 PB001 CONF 00. THIS CLEARS MEL 25-60-08A CAT C 18053. PLACARD REMOVED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT)

LANDING GEAR SYS DISAGREE ECAM ILLUMINATED ON LANDING. PERFORM FAULTS LT, LG DOOR CLOSED PROX SENSOR 29GA, TGT POS. PERFORMED BITE TEST ON LGCIU 2 IAW MM 32-69-00-740-001. NO FAULTS SHOWN. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 32,974 hrs · 23,115 cycles

EMERGENCY EXIT SIGNS HAVE BURNED OUT LAMPS. RELAMPED EMER EXIT SIGNS. OPERATIONS CHECKED OK IAW AMM 33-51-00.

Part: BATTERY — DISCHARGED (MEGAPHONE)

AFT CABIN MEGA PHONE INOPERATIVE. R & R AFT MEGA PHONE BATTERIES. OPERATIONS CHECKED GOOD IAW MM 25-60-00.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 32,540 hrs · 22,926 cycles

AFT GALLEY MEGA PHONE INOPERATIVE. INSPECTED AFT GALLEY MEGA PHONE. OPERATIONS CHECKED GOOD IAW AMM 25-60-00.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 32,540 hrs · 22,926 cycles

AFT GALLEY MEGA PHONE INOPERATIVE. INSPECTED AFT GALLEY MEGA PHONE. OPERATIONS CHECKED GOOD IAW AMM 25-60-00.

Part: MEGAPHONE — INOPERATIVE (CABIN)

FLIGHT ATTENDANT MEGA PHONE INOPERATIVE. R & R FWD MEGA PHONE IAW AMM 25-65-51. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: BATTERY — DISCHARGED (FLASHLIGHT)

AFT FLIGHT ATTENDANT`S FLASHLIGHT READY LIGHT NOT BLINKING. REPLACED BATTERY IN AFT FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT & OPERATIONS CHECKED GOOD IAW AMM 25-60-00.