N294NV

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 36,334 hrs · 21,314 cycles

(AIRCRAFT NOT GROUNDED) EMERGENCY LEFT BAT/EPSU 11WL & 10WL FAULT FROM EPSU CAP TEST / REMOVED AND REPLACED EPSU PER WO536709"

Part: BULB — INOPERATIVE (ZONE 200) · airframe 35,282 hrs · 20,856 cycles

(AIRCRAFT NOT GROUNDED) EMERGENCY EXIT LIGHT BULB INOP BY SEAT 14A. / PERFORMED EMERGENCY LIGHT OPS CHECK IAW AMM 33-51-00-7110-007-A. FOUND EMERGENCY LIGHTS TO BE WORKING. NO OTHER DEFECTS NOTED.

Part: ENGINE — STALLED (NR 2) · airframe 34,331 hrs · 20,400 cycles

(AIRCRAFT GROUNDED) ENG 2 STALL @CRUISE WITH TURBULENCE. REMOVED AND REPLACED #2 ENGINE REF TC 71-400-001 & 71-400-002 WO 511396 SEE THESE REF'S FOR WORK DETAILS"

Part: MEGAPHONE — MALFUNCTIONED (ZONE 200) · airframe 33,590 hrs · 19,980 cycles

(AIRCRAFT NOT GROUNDED) NO FEEDBACK FROM REAR MEGAPHONE. / PERFORMED OPERATIONAL TEST OF MEGAPHONE IN AFT PER AMM 25-65-51-410-002A. OPS CHECK GOOD."

Part: MEGAPHONE — UNKNOWN (AFT CABIN) · airframe 33,194 hrs · 19,780 cycles

(AIRCRAFT NOT GROUNDED) MEGAPHONE IN REAR OF AIRCRAFT INOP / PERFORMED OPS CHECK OF MEGAPHONE IAW AMM 25-65-51-920-001-A OPS CHECK GOOD"

Part: VALVE — FAULTED (NR 2 ENGINE) · airframe 33,106 hrs · 19,733 cycles

ENG 2 STALL ECAM AT TOD. ENGINE 2 N1 ROLLED BACK WITH RYTHMIC SURGING. WITH THRUST LEVER AT IDLE, ENGINE RETURNED TO NORMAL. RESUMED NORMAL OPS. / REMOVED AND REPLACED #2 ENG PRV(4001HA) PER WORK ORDER 00504443 STEP 3 AND IAW AMM 36-11-52-400-042-A. LEAK CHECK AND OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. PERFORM ENGINE WASH PER TASK CARD 72-440-003."

Part: SWITCH — FAULTED (HYD SYSTEM) · airframe 33,043 hrs · 19,703 cycles

(EMERGENCY DECLARED) HYD YELLOW RSVR LO LEVEL ECAM HYD RESV LEVEL SHOWED NORMAL / PERFORMED TSM 29-13-00-810-801-A FOUND LOW LEVEL SWITCH TO BE AT FAULT AND FAILING. REMOVED AND REPLACED YELLOW HYD RESERVOIR LOW LEVEL SWITCH AS PER A320 AMM 29-13-41-000-004-A AND 29-13-41-400-004-A. NO LEAKS NOTED AT THIS TIME. OPS CHECK GOOD AT THIS TIME"

Part: ACTUATOR — OUT OF ADJUST (NR 2 VSV) · airframe 32,994 hrs · 19,682 cycles

NUMBER 2 ENGINE STALL WHEN GOING FLT IDLE AT TOP DECENT. ENGINE POPPED TWO TIMES WITHIN 2-3 SECONDS. ENGINE STALL ECOM CAME UP BUT BEFORE ECAM ACTIONS COULD BE RUN THE ENGINE CLEARED UP AND ALL INDICATIONS WERE NORMAL AFTER THE EVENT. VBV DOORS AND BALLSCREW ACTUATOR REFERENCE CLOSE POSTION FOUND TO BE OUT OF LIMITS-PERFORMED ADJUSTMENT OF THE REFERENCE CLOSED POSITION OF THE VBV SYSTEM FOR #2 ENG FROM -1.25 DEGREES TO -0.19 DEGREES REF AMM 75-31-00-820-001-A OPS CK GOOD.

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 31,029 hrs · 18,701 cycles

EPSU BATTERY FAILED DURING BATT CAPACITY CHECK AT LOCATION 10WL,11WL,12WL,13WL. / REMOVED AND REPLACED EPSU BATTERY AT LOCATION 10WL,11WL,12WL,13WL, OPS CHECK GOOD IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A."

Part: BEAM — CORRODED (ZONE 200) · airframe 30,956 hrs · 18,661 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 531166-01-2-001, IT WAS FOUND THE CREW DOOR SILL BEAM WITH TWO AREAS CORRODED. THE FIRST OPTION WAS REPLACING THE PART HOWEVER, IT IS NOT AVAILABLE. DUE TO THIS FACT, DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL.AIRBUS PROVIDED REPAIR INSTRUCTION UNDER DOSSIER 81223470. COOPESA PERFORMED REPAIR UNDER EO COO-EO-2023-17746-R00 THE RPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N083 ITEM2-16).

Part: NONE — NONE · airframe 28,725 hrs · 17,606 cycles

NRC 9000-0012 : 425-04 PASSENGER CABIN CEILING EMERGENCY LIGHT ON PANEL 231 BC FOUND INOP. / FOUND WIRES INSTALLED INCORRECTLY ON CABIN CEILING EMERGENCY LIGHT AT PANEL 231 BC. SEE AWS#1 FOR CORRECTIVE ACTION."

Part: NONE — NONE · airframe 28,725 hrs · 17,606 cycles

NRC 5000-0018: 33284-23 LH WING , FUEL PANEL 540LB CUTOUT , HOLES ELONGATED / ON L/H WING, FUEL PANEL 540LB CUTOUT ELONGATED HOLES REPAIR PER AIRBUS DOSIER #81053466 AND AIRBUS TD 81053466/009/2022#B. REPEAT INSPECTION PER AIRBUS RDAF 81053466/005/2022 ISSUE A CLASSIFIED MAJOR CATEGORY B. THRESHOLD INSPECTION 3300FC/6600FH INTERVAL 3300FC/6600FH METHOD OF INSPECTION GVI INSPECTION WITH DOOR IN SITU, AND COMPLIED WTH ALLEGIANT ERO R5721-0098, SEE AWS FOR DETAIL AND NDT W/O MWO50918"

Part: DAMPENER — LOW PRESSURE (L2) · airframe 28,053 hrs · 17,279 cycles

L2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT 1450 PSI / SERVICED L2 DOOR DOOR DAMPER AND EMERGENCY OPERATION CYLINDER TO 1700 PSI, ADDED 250 PSI, LEAK CHECK GOOD, W/REF TO AMM 52-10-00-614-001-A"

Part: EPSU — DIRTY (10WL) · airframe 27,975 hrs · 17,239 cycles

EMERGENCY LIGHT SYSTEM TASK FAULTED BAT/EPSU (10WL) FWD L / GAINED ACCESS TO EMERGENCY POWER SUPPLY UNIT 10WL. DISCONNECTED CANNON PLUG, CLEANED, AND RECONNECTED. BITE TESTED OK. I/A/W AMM 33-51-38 PB 401, AND ESPM 20-55-50."

Part: EPSU — INOPERATIVE (L1 AND R1) · airframe 27,981 hrs · 17,242 cycles

EMERGENCY LIGHTS ABOVE L1 AND R1 DOORS ARE INOP WHEN AIRCRAFT POWER IS LOST / REMOVED AND REPLACED L1 EPSU IAW AMM 33-51-38"

Part: EPSU — DIRTY (10WL) · airframe 27,895 hrs · 17,199 cycles

CIDS EPSU SYS TEST FAULTED EMERGENCY LIGHTING BAT/EPSUK(10WL) FWD L . / DISCONNCETED CANNON PLUG AT 10WL IN FWD L/H CEILING CABIN, CLEANED AND RECONNECTED. OPS CHECK BITE TESTED OK I/A/W AMM 33-51-38-400-002-A & ESPM 20-55-10."

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 26,887 hrs · 16,678 cycles

CABIN EMERGENCY LIGHTING BATTERY ALL FAILED CHECK. / REMOVED AND REPLACED ALL 4 CABIN EMERGENCY LIGHTING BATTERIES IAW AMM 33-51-38. OPS CHECK GOOD AT THIS TIME."

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 26,229 hrs · 16,342 cycles

ALL FOUR EPSU BATTERIES FAILED TEST / R/R FWD EPSU BATTERY PER 33-51-38-000-002-A AND 33-51-38-400-002-A"

Part: PTU — MALFUNCTIONED (HYD SYSTEM) · airframe 25,868 hrs · 16,192 cycles

(EMERGENCY DECLARED) HYD Y RSVR LO LVL AND HYD Y ENG 2 PUMP LO PR ECAMS / REMOVED THE GREEN-YELLOW POWER TRANSFER UNIT REF AMM 29-23-41-000-001-A AND REPLACED REF AMM 29-23-41-400-001-A, OPS AND LEAK CHECK GOOD."

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 25,283 hrs · 15,936 cycles

AFT EMERGENCY EXIT LIGHT FLICKERS THEN TURNS OFF. R & R EPSU BATTERY 13WL, PER A320 AMM 33--51-38 PB 401. R & R AFT EMERGENCY LIGHT ASSEMBLY, PER A 320 AMM 33-51-16 PB 401.

Part: SKIN — GOUGED (FUSELAGE) · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND FR 25 - 26, STR. 25L TO BE GOUGED. S/O 418149 N/R 28001

Part: SKIN — DENTED (FUSELAGE) · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND A DENT IN FUSELAGE EXTERIOR SKIN R/H FR5-6, STR.24-25R. S/O 194086 N/R 24284

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT CABIN FLOOR BEAM -Y1294 FR 69. S/O 193086 N/R 24163

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT CABIN FLOOR BEAM -Y254 FR69+20 HAS CORROSION AT MOUNT POINT. S/O 193086 N/R 24161

Part: FITTING — CORRODED (L2 DOOR) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT CABIN L2 DOOR AFT LOWER CORNER FITTING HAD CORROSION. S/O 193086 N/R 24135

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 2,511 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND L2 DOOR SHAPE SILL WAS CORRODED. S/O 194086 N/R 24063

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AFT CABIN R/H R2 DOOR SILL AT FS67 + 16 TO FR 68 HAS CORROSION. S/O 193086 N/R 24165

Part: FITTING — CORRODED (R2 DOOR) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT CABIN R/H R2 DOOR CORNER FITTING AT FS 68 HAS CORROSION. S/O 193086 N/R 24167

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT CABIN L2 DOOR SILL HAS CORROSION AT SEVERAL PLACES. S/O 193086 N/R 24134

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO , LAKE CITY, FLORIDA FOUND R2 DOOR SHAPE SILL CORRODED. S/O 193086 N/R 24064

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND SPOTS OF CORROSION AT -Y765 FLOOR BEAM BETWEEN FR67 AND FR 68 S/O 193086 N/R 24022

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT CABIN L/H FLOOR BEAM Y1292 FR68 - FR 69 HAS CORROSION AT MOUNT POINTS. S/O 193086 N/R 24139

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 25,111 hrs · 15,850 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND SPOTS OF CORROSION AT Y765 FLOOR BEAM BETWEEN FR67 AND FR68, STRINGER 23 L/H S/O 193086 N/R 24023