N230NV

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 70,221 hrs · 37,038 cycles

DURING ACCOMPLISHMENT OF ALLEGIANT WORK CARD 531135-03-1-001 & NTM TASK CARD 53-11-35-250-801-C01CARDS (SDI) THAT ARE RELATED TO ALI TASK 531135, MPD 531135-03, IT WAS FOUND THE WINDSHIELD SIDE POST, FR 4 LT, UPPER ATTACHMENT, UPPER FRAME HORIZONTAL FLANGE WITH FASTENER HOLES (2EA) WITH CRACK INDICATIONS, DUE TO OVALITY AND BURR. REPAIRED COCKPIT WINDSHIELD SIDE POST FR4 LH UPPER ATTACHMENT UPPER FRAME HORIZONTAL FLANGE WITH FASTENER HOLES WITH CRACK INDICATIONS DUE TO QUALITY AND BURR IAW COOPESA EO COO-EO-2025-23602 R2 REV 02 AND AIRBUS REPAIR INSTRUCTION AND RDAF DOSSIER #80222159. THIS REPAIR IS COVERED BY COOPESA JOB A1Q279 ITEM 2-12

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 69,417 hrs · 36,640 cycles

(AIRCRAFT NOT GROUNDED) EPSU FAILED CAPACITY CHECK / REMOVE AND REPLACE 4EA EPSU BATTERIES IAW AMM 33-51-38-400-002-A. OPS CHECK GOOD.ITEM: 1REMOVE AND REPLACED 4EA EPSU BATTERIES IAW AMM 33-51-38-400-002-A. OPS CHECK GOOD. "

Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 69,374 hrs · 36,615 cycles

(AIRCRAFT GROUNDED) (EMERGENCY DECLARED) ECAM ENG 1 OIL LO PR. OIL PRESSURE WAS LESS THAN 13 PSI. OIL QUANITY IS 0 QT SHUT DOWN ENG 1 IN FLT / REMOVE AND REPLACE ENG#1 IAW TC 71-400-002. OPS AND LEAKS CHECK GOOD. A/C OK FOR SERVICE. REMOVED L/H ENG LUBRICATION UNIT FOR REPLACEMENT. IAW AMM 79-21-10-000-004-A. INSTALLED NEW L/H ENG LUBRICATION UNIT IAW AMM 79-21-10-400-004A. NO LEAKS AT THIS TIME. ALL OPS CHECKS GOOD AT THIS TIME. DUE TO IN FLIGHT SHUT DOWN, INSPECTION AFTER WINDMILLING REQUIRED. FOLLOWED TSM 05-51-34-200-001A. PERFORMED AMM 72-00-00-100-007. ENGINE OPERATED AT IDLE POWER WITHIN 24 HOURS AFTER LANDING. ENGINE DRY OUT AND RE-LUBE NOT REQUIRED.

Part: UNKNOWN — ODOR (CABIN) · airframe 69,188 hrs · 36,521 cycles

(AIRCRAFT NOT GROUNDED) BOTH AFT FA'S REPORT STRONG DIRTY SOCK SMELL DURING FINAL 10 MINUTES OF FLIGHT NO ILLNESS REPORTED / PERFORMED TC A32X-21-000-001 APU HAD NO SIGNS OF LEAKS WITH AND WITH OUT BLACK LIGHT, RAN APU NO ODOR DETECTED WITH PACK 1 OR 2. PERFORMED ENGINE RUNS NO ODOR WAS NOTED FROM EITHER PACK OR ENGINE BLEED. AFT GALLEY AND AFT LAVS HAD NO ODOR FWD GALLEY AND LAV HAD NO ODOR DURING APU RUN OR ENGINE RUNS NO ODOR WAS NOTED IN FLIGHT DECK OR ANYWHERE IN MAIN CABIN PASSENGER COMPARTMENT.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 68,533 hrs · 36,244 cycles

(AIRCRAFT NOT GROUNDED) DOOR R FWD EMER EXIT ECAM CAME ON IN FLIGHT. CABIN PRESSURE & RATE NORMAL. FA SAID COVER WAS OFF & REPLACED. ECAM WENT AWAY. / INSPECTED INSTALLATION OF COVER, NO DEFECTS NOTED REF AMM 52-21-11-700-050-B"

Part: PROXIMITY SWITCH — DIRTY (ZONE 800) · airframe 68,512 hrs · 36,234 cycles

(AIRCRAFT GROUNDED) GOT ECAM - DOOR R FWD EXIT ON CLIMBOUT. CABIN HELD PRESSURE. ""DOOR R FWD EMER EXIT"" / INSPECTED PROX SWITCH AND FOUND CONTAMINATION. CLEANED PROX SWITCH IAW ESPM 20-55-50. ALSO FOUND ELECTRICAL CONNECTOR LOOSE. RESECURED CANNON PLUG. OPS CHECK GOOD IAW AMM 52-71-00-710-001-A."

Part: BATTERY — NO TEST (ZONE 200) · airframe 68,448 hrs · 36,203 cycles

DURING ALLEGIANT TASK A32XX335100-03-1-001-_P1-OP-UP-E-E/001 CABIN EMERGENCY LIGHTINING CHECK BATTTERY CAPACITY TEST SHOWS EPSU BAT CAP AFT L FAILED. REPLACED PAX CABVIN AFT LH EPSU BATTERY (FIN 13WL) IAW AMM TASK 33-51-38-000-002-A AND 33-51-38-400-02-A SATISFACTORY CNDITION.THIS REPLACEMENT WAS DOCUMENTED UNDER COOPESA JOB A1P083 ITEM 2-40.

Part: SCREW — MISSING (SLIDE) · airframe 67,804 hrs · 35,855 cycles

(AIRCRAFT NOT GROUNDED) OVERWING A/C LEFT STRIP OVER EMERGENCY ESCAPE SLIDE MISSING A SCREW / INSTALLED SCREW ON LEFT OVERWING SLIDE PANEL REF AMM 25-62-42-400-001-A"

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 67,596 hrs · 35,745 cycles

(AIRCRAFT NOT GROUNDED) EMERGANCE BATTERY FALLED CAP TEST FIN WL11 / REPLACED EMERGANCE BATTERY FIN WL11, OPS CHECK GOOD REF AMM 33-51-00-710-003"

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 68,450 hrs · 36,204 cycles

(AIRCRAFT GROUNDED) EPSU FAILURE / R/R EPSU REF WO505887"

Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 66,388 hrs · 35,145 cycles

R/H EPSU BATTERY FAULTY. / EMER R/H (12WL) EPSU BATTERY REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-400-002A"

Part: FITTING — CRACKED (ZONE 200) · airframe 65,255 hrs · 34,546 cycles

DUE TEMPORARY REPAIR EXPERIATION LH WINDSHIELD SIDE AIRBUS WAS CONTACTED REQUESTING INFORMATION ABOUT THE KITS REQUIRED AND REPLACEMENT AND REPAIR INSTRUCTIONS.CORRECTIVE ACTION: DAMAGE REPORT WAS SENT TO AIRBUS AND PERMANENT REPAIR INSTRUCTIONS WERE HANDLED UNDER AIRBUS DOSSIER 80222159 AND COOPESA EO # COO-EO-2023-17148-R00

Part: SKIN PANEL — CORRODED (ZONE 100) · airframe 65,255 hrs · 34,546 cycles

PLEASE NOTE THAT DURING THE STRUCTURAL INSPECTION AS PER ALLEGIANT INSPECTION TASK ZL-145-01-1-001 MPD TASK, SEVERAL CORROSION ON CENTER WING BOX TOP SKIN UPPER SURFACE BETWEEN FR41 AND FR42 AND +Y 1292 AND RIB 1 DATUM WAS FOUND, COMMON TO APU FUEL FEED FITTING BASE CONTOUR. CORRECTIVE ACTION: DAMAGE REPORT WAS SENT TO AIRBUS, AND THE REPAIR INTRUCTIONS WERE HANDLED UNDER AIRBUS DOSSIER 81176407 AND COOPESA JOB A1N004, NRI 2-30

Part: FRAME — UNKNOWN (ZONE 200) · airframe 65,255 hrs · 34,546 cycles

DURING THE EO E5311-0051, 53-0004-19 ALLEGIANT EO´S ACCOMPLISHMENT RELATED TO AD 2022-08-08 PARAGRAPH (G) AND SB 53-1379 REV. 00, SB 53-1380 REV. 01, SB 53-1381 REV. 01 WERE FOUND HOLES AT FR16 (HOLE #4) UPPER FWD CORNER LH SIDE WITH DIAMETER THAT IS MORE THAN OR EQUAL TO THE MINIMUM STARTING HOLE DIAMETER, THIS CONDITION WAS APPROVED PER AIRBUS UNDER DOSSIER 80567936 AND REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N004 ITEM 2-21).

Part: FITTING — CRACKED (ZONE 200) · airframe 65,255 hrs · 34,546 cycles

PLEASE NOTE THAT DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD Nº: 531135-01-2-001 MPD, IT WAS FOUND RH WINDSHIELD SIDE POST UPPER AND FITTING P/N: D5311086520303 ATTACHMENT AT FRAME 4 (1 HOLE WITH CRACK INDICATION) CORRECTIVE ACTION: DAMAGE REPORT WAS SENT TO AIRBUS, AND THE REPAIR INTRUCTIONS WERE HANDLED UNDER AIRBUS DOSSIER 81176882 AND COOPESA JOB A1N004, NRI 2-27 AND NRI 2-36

Part: FRAME — UNKNOWN (ZONE 200) · airframe 65,255 hrs · 34,546 cycles

DURING THE ALLEGIANT EO E5311-0017 ALLEGIANT EO ACCOMPLISHMENT RELATED TO REF. AD 2022-08-08 PARAGRAPH G AND SB 53-1379 REV. 02, IT WAS FOUND A HOLE AT FR20 (HOLE # 9 LOWER CORNER) LH SIDE WITH A DIAMETER THAT IS MORE THAN OR EQUAL TO THE MINIMUM STARTING HOLE DIAMETER. DAMAGE REPORT WAS SENT TO AIRBUS, AND THE REPAIR INTRUCTIONS WERE HANDLED UNDER AIRBUS DOSSIER 81176268 AND COOPESA JOB A1N004, NRI 9-7 AND NRI 9-10

Part: FITTING — CRACKED (ZONE 200) · airframe 65,255 hrs · 34,546 cycles

DURING THE ALLEGIANT TASK 53-210-003_P1-OP-UP-NDT/00 WORK CARD INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE RH CONTINUITY FITTING WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST THE KITS P/N FOR REPLACEMENT. AIRBUS PROVIDED THE INFORMATION WITH DOSSIER 81175803 AND THE REPLACMEENT OF THE PARTS IS COVERED WITH ENGINEERING ORDER E5311-0013 REV 00. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N004 ITEM 2-24).

Part: STRINGER — CORRODED (ZONE 100) · airframe 65,255 hrs · 34,546 cycles

DURING ACCOMPLISHMENT CORROSION TASK 532180-01-2, IT WAS FOUND LOWER FUSELAGE, FWD CARGO COMPARTMENT, AT FR 29 +355MM, STGR 41R, STRINGER WITH CORROSION.DUE THIS FACT. IT WAS REPAIRED STRINGER SECTION AT STGR 41 R/H, FROM FR 29 TO FR 30 +460 MM, IAW A320-SRM-53-21-13-300-003 FIG 001, AND DWG N° D532-31712 ISSUE C, AND D532-31586 ISSUE D. THIS IS A CATEGORY B REPAIR WITH REPETITIVE INSPECTIONS.IAW TASK SRI 53-21-13-205-005

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,194 hrs · 34,515 cycles

EMERGENCY LIGHTS INOP AT L2,R2 WHEN AC BUS 1 AND 2 ARE DE ENGERGIZED / REMOVED AND REPLACED (11WL&13WL) BATTERIES IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. PERFORMED OPS TEST REF AMM 33-51-00-710-001. OPS TEST GOOD"

Part: NONE — NONE · airframe 63,757 hrs · 33,808 cycles

SEVERAL EMERGENCY EXIT SIGNS HAVE BULBS BURNT OUT / REMOVED AND REPLACED ALL BURNT OUT BULBS IN EMERGENCY EXIT SIGNS IAW AMM 33-51-00"

Part: EPSU — NONE · airframe 63,744 hrs · 33,801 cycles

EMERGENCY LIGHTS AT L1 AND R1 INOP DURING POWER LOSS. / REMOVED AND REPLACED EPSU AND BATTERY PER AMM 33-51-38 PB 401, OPS CHECK GOOD."

Part: NONE — NONE · airframe 63,721 hrs · 33,789 cycles

RH MLG DOOR ACTUATOR FITTING, AFT SIDE PLAIN BUSH MIGRATED OUT OF FITTING./INSTALLED 1 EA STRAIGHT BUSHING AS REQUIRED IAW ERO R5336-0015. / WITH REFERANCE TO SRM 51-72-12-911-002."

Part: BULB — MISSING (EMERGENCY LIGHT) · airframe 62,327 hrs · 33,065 cycles

R1,L1 AND AFT CABIN EMER EXIT SIGNS MISSING BULBS. SIGNS NOT FULLY ILLUMINATED / REMOVED AND REPLACED LAMPS FROM EXIT LIGHTS NOTED ABOVE IAW AMM 35-51-16"

Part: BATTERY PACK — NOT REPORTED (EMERGENCY LIGHTS) · airframe 62,067 hrs · 32,923 cycles

PERFORMED TC 33-51-00-03-1-001 FROM 1A PHASE 1 ALL 4 EMERGENCY BATTERY NEEDS TO BE REPLACED / REPLACED ALL 4 EMERGENCY BATTERY PER AMM 33-51-38 OPS CHECK OK."

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 61,344 hrs · 32,489 cycles

DURING CABIN LIGHTING CAP CHECK, BAT 11WL DETECTED FAIL. / REMOVE AND REPLACED EMERGENCY LT BATTERY @ 11WL REF AMM 33-51-38-000-002A & 33-51-38-400-002A."

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,504 hrs · 32,011 cycles

WHILE PERFORMING OPERATIONAL TEST OF EMERGENCY LIGHT. RECEIVED EPSU FWD BATTERY FAULT. REMOVED AND REPLACED ESPU BATTRY (10WL), PER A320 AMM 33-51-38 PB 401. OPERATIONS CHECK GOOD.

Part: SLIDE — MALFUNCTIONED (R1 DOOR) · airframe 58,711 hrs · 31,025 cycles

R1 EMERGENCY SLIDE WILL NOT ARM / REMOVED AMD REPLACED R1 SLIDE IAW AMM 25-62-44-400-802-A. OPS CHECKS GOOD, NO FURTHER DEFECTS NOTED."

Part: BUSHING — MISSING (TAILCONE)

DURING OK TO CLOSE ACCESS DOOR 312AR THE QUALITY INSPECTOR FOUND MISSING BUSHING ON TAIL CONE ATTACHMENT LOWER POSITION BTW FR77 TO FR78 IN THS COMPARTMENT (ACCESS DOOR 312AR).

Part: BUSHING — MISSING (TAILCONE)

DOOR 312AR THE QUALITY INSPECTOR FOUND MISSING BUSHING ON TAIL CONE ATTACHMENT LOWER POSITION BTW FR 77 TO FR 78 IN THIS COMPARTMENT, ACCESS DOOR 312AR.

Part: APU — LEAKING (APU BAY) · airframe 55,076 hrs · 28,965 cycles

DIRTY SOCK ODOR PRESENT DURING DESCENT. FOUND OIL INSIDE APU PLENUM, COMING FROM LOAD COMPRESSOR CAVITY. CLEANED THE PLENUM. REMOVED AND REPLACED THE APU.