N326NV

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 53,483 hrs · 38,241 cycles

(AIRCRAFT NOT GROUNDED) FAILED TEST/EPSU / REMOVED AND REPLACED EPSU REF WO535169"

Part: LIGHT — MISSING (ZONE 200) · airframe 53,089 hrs · 37,974 cycles

AIRCRAFT NOT GROUNDED, FA DISCOVERED L2 FLOOR LEVEL EMERGENCY LIGHT MISSING IN FLIGHT. INSTALLED NEW EXIT LIGHT COVER ON L2 EXIT DOOR IAW AMM 33-51-11-400-001-A.

Part: BATTERY — NO TEST (ZONE 200) · airframe 53,016 hrs · 37,928 cycles

(AIRCRAFT NOT GROUNDED) BATTERY FAULT INDICATION DURING EPSU BITE TEST / REMOVED AND REPLACED EPSU BATTERIES, REF WO519197"

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 52,691 hrs · 37,739 cycles

(AIRCRAFT NOT GROUNDED) EPSU FAILED DURING TC #335100-03-1-001 / REMOVED AND REPLACED AFT EPSU/BATTERY 13WL IAW AMM 33-51-38-400-001-A, OPS CHECK GOOD"

Part: MEGAPHONE — EXPIRED (FWD CABIN) · airframe 50,320 hrs · 36,516 cycles

FWD MEGAPHONE EXPIRATION DATE PAST DUE. / REMOVED AND REPLACED FWD GALLEY MEGAPHONE IAW AMM 25-65-51-920-001-A, 25-65-51-410-050-A."

Part: MEGAPHONE — EXPIRED (FWD) · airframe 50,320 hrs · 36,516 cycles

FWD MEGAPHONE EXPIRATION DATE PAST DUE. / REMOVED AND REPLACED FWD GALLEY MEGAPHONE IAW AMM 25-65-51-920-001-A, 25-65-51-410-050-A."

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 50,197 hrs · 36,455 cycles

WHILE PEFORMING EMERGENCY LIGHT TEST, FAULT (ESCAPE SLIDE LT/ EPSU (12WL) EMER R) APPEARED. / T/S PER TSM 25-62-00-810-814-A. FOUND CANNON PLUG DISCONNECTED ON OWS 7505MM. RESECURED CANNON PLUG PER AMM 25-62-42-400-001-A. REPERFORMED BITE CHECK PER AMM 33-51-00-710-001-A. FOUND ESCAPE SLIDE MESSAGE WENT AWAY, BUT EPSU 12WL STILL FAILED. REMOVED AND REPLACED EPSU 12WL PER AMM 33-51-38-000-001-A, 33-51-38-400-001-A. BITE CHECK GOOD PER AMM 33-51-00-710-001-A."

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 50,067 hrs · 36,390 cycles

ALL EPSU BATTERIES FAILED BATTERY CAPACITY CHECK DURING TC 335100-03-1-001 / REPLACED ALL 4 EPSU BATTERIES IAW AMM 33-51-38-400-002-A. OPS CHECK GOOD."

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 49,678 hrs · 36,153 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: ZL-575-01-1-001, IT WAS FOUND AT LHWING, TOP SKIN LOWER SURFACE AT RIB 8 OVERHANG AREA WITH CORROSION. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINAL APPROVAL,AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 80969544. THE REPAIR WAS PERFORMED IN ACCORDANCE INSTRUCTIONS RECEIVED AND IT IS COVER UNDER COOPESA JOB A1N116 ITEM 5-5

Part: SKIN PANEL — CORRODED (ZONE 500) · airframe 49,678 hrs · 36,153 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: ZL-575-01-1-001, IT WAS FOUND AT LH WING, TOP SKIN LOWER SURFACE AT RIB 17 OVERHANG AREA WITH CORROSION. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED REQUESTING REPAIR INSTRUCTIONS AND FINAL APPROVAL, AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 80969544. THE REPAIR WAS PERFORMED IN ACCORDANCE INSTRUCTIONS RECEIVED AND IT IS COVER UNDER COOPESA JOB A1N116 ITEM 5-4

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 49,678 hrs · 36,153 cycles

DURING THE ALLEGIANT TASK 53-210-003 WORK CARD INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE WINDSHIELD FRAME WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE INFORMATION WITH DOSSIER 81242975 AND THE REPLACEMENT OF THE PARTS IS COVERED WITH ENGINEERING ORDER R5311-0214 REV 00. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N116 ITEM 2-34).

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 49,678 hrs · 36,153 cycles

DURING THE ALLEGIANT TASK 53-210-003 WORK CARD INSTRUCTIONS ACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE WINDSHIELD FRAME WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED THE INFORMATION WITH DOSSIER 81242975 AND THE REPLACEMENT OF THE PARTS IS COVERED WITH ENGINEERING ORDER R5311-0214 REV 00. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N116 ITEM 2-33).

Part: FITTING — CRACKED (ZONE 200) · airframe 49,678 hrs · 36,153 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 LH/RH CONTINUITY FITTING WITH CRACK. AIRBUS WAS CONTACTED TO REQUEST THE KITS P/N FOR REPLACEMENT. AIRBUS PROVIDED THE INFORMATION WITHDOSSIER 81242975 AND THE REPLACEMENT OF THE PARTS IS COVERED WITH ENGINEERING ORDER E5311-0013 REV 00. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N116 ITEM 2-26).

Part: FRAME — CRACKED (ZONE 200) · airframe 49,678 hrs · 36,153 cycles

DURING ALLEGIANT TASK INSPECTION 53-260-002 REAR FUSELAGE AFT PASS DOOR RH SIDE FR66 DOOR STOP FITTING # 7 AREA I/B UPPER FASTENER HOLE WITH CRACK WAS FOUND. COOPESA PERFORMED REPAIR IN ACCORDANCE A319 SRM TASK 53-41-12-300-010. THIS REPAIR IS COVERED WITH COOPESA JOB A1N116 ITEM 2-29.

Part: SERVO VALVE — FAULTY

(EMERGENCY DECLARED) AFTER SELECTING GEAR DOWN RECEIVED BRAKES ALTN R RELEASED, ECAM MESSAGE ""ALTN R BRK"" WAS DISPLAYED ON STATUS PAGE./ R&R BRK ALTN SERVOVALVE,R&R PRESS XDCR-BRK,YELLOW R (100GG) IAW AMM 32-44-29,R&R PRESS XDCR 100GG CONNECTOR (100GGA) IAW ESPM 20-48-21. FAULT WAS CORRECTED, ALTN R/H BRAKES WORK AS NORMAL, GOOD FOR SVC."

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 48,454 hrs · 35,626 cycles

REF: NRI 3-2 - APU EXHAUST ACCESS FAIRING 317AL FRAME WITH CORROSION./REPLACED FRAME PART NUMBER D524853820200 IAW A319 SRM 51-72-11-911-001 ATTACHED WITH SOLID RIVETS IAW A319 SRM 51-42-11 PARAG 2E(4) AND 51-42-11 PARAG 2E(2) REV.142 DATED:08-01-2022 AND IPC REFERENCE 52-41-18-01-A REV.37 DATED:08-01-2022 AND AIBUS DRAWING 19 D52485380 ISSU P. COOPESA A1M128 3-2."

Part: EPSU — DIRTY · airframe 47,384 hrs · 35,008 cycles

EPSU TEST FAILS 12WL. / CLEANED CONNECTOR AT 12 WL CANON PLUG , BITE TESTED OK & OPS CHECK GOOD I/A/W AMM 33-51-38-400-001.AND ESPM 2055-30."

Part: EPSU — FAILED INSP (12WL) · airframe 46,879 hrs · 34,755 cycles

BATTERY CAP TEST FAILED 12WL. / BITE CHECK 12WL CONFIRM BATTERY FAULT, REMOVED AND REPLACED BATTERY AT 12WL, BITE CHECK GOOD, EPSU TEST OK. REF AMM 33-51-38 PB 401."

Part: EPSU — FAULTY (10WL) · airframe 46,878 hrs · 34,754 cycles

DURING EPSU SYSTEM TEST FOUND FAULTY EPSU AT 10WL / REMOVED AND REPLACED FRONT EPSU 10WL IAW A319 AMM 33-51-31 PB401 OPS CHECK GOOD."

Part: SKIN — CORRODED (LT WING) · airframe 47,570 hrs · 31,698 cycles

NRC 5000-0044: 33284-36 LH WING, AREA FWD OF SPOILER #2 (BETWEEN RIB 10 AND 11) SUSPECTED CORROSION (02 RIVET DAMAGED AND PRC MISSING) / AFTER INVESTIGATION, CORROSION FOUND AT LH WING UPPER SKIN AREA FWD OF SPOILER #2 AND RIB 10 AREA. LH WING UPPER SKIN FWD OF SPOILER #2 AND RIB 10 AREA, REPAIRED AS PER AIRBUS DOSSIER # 80969544, AIRBUS R572-58944, AIRBUS RDAF 80969544/009/2021#A AND COMPLY WITH ALLEGIANT ERO R5721-0085. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO: 48857-6. REPAIR MAJOR CATEGORY B WITH FURTHER INSPECTIONS DEFINED IN RDAF 80969544/009/2021#A."

Part: NONE — NONE · airframe 32,152 hrs · 23,794 cycles

NRC 2000-0049: 031-11 AFT PASSENGER CABIN FLOOR STRUCTURE, CORROSION FOUND AT RH THRESHOLD BEAM LOWER MAIN SILL AREA BTW FRAME 66-68. / AFT PASSENGER CABIN FLOOR STRUCTURE LOWER MAIN SILL AREA BTW FRAME 66-68, PERMANENTLY REPAIRED PERFORMED AT THRESHOLD BEAM IAW SRM 53-41-14-300-001 SHEET 3 PRINCIPLE 5. REPAIRED CATEGORY A, NO FURTHER ACTION REQUIRED. SEE AWS FOR DETAILS AND NDT REPORT MWO: 48857-7. EXTRUSION: P/N: AND10136-2004 7075T6, P/O: 1559749. FILLER: P/N: 7075T6 .063"", P/O: 1694322. HI-LOCK: HL11VF6-3, P/O: 1658950. HI-LOCK: P/N: HL10VF6-5, P/O: 1717789. HI-LOCK: P/N: HL10VF6-4, P/O: 1727233. HI-LOCK: P/N: HL10VF6-3, P/O: 1569232. COLLAR: P/N: HL70-6, P/O: 1707708. PRC: P/N: PRC870B2 #655, P/O: 1724389."

Part: FITTING — CORRODED (GIRT BAR) · airframe 30,539 hrs · 20,179 cycles

NRC 2000-0075: (823-12) CORROSION FOUND UNDER R1 DOOR FWD GIRT BAR FITTING,AROUND HI-LOCK. / ON FWD CREW DOOR CUTOUT LOWER MAIN SILL BEAM AREA UNDER GIRT BAR FITTING HOLE LOCATION, PERMANANTLY REPAIRED PERFOMED IAW SRM 53-11-14-283-005. FIG 001 SHEET 5, MAJOR REPAIR, CATEGORY B. FOR FUTURE INSPECTIONS SEE TASK SRI 53-11-14-205-001.SEE AWS FOR DETAILS AND NDT REPORT MWO 48857-32. HI-LOCK: P/N: HL10VF5-5, P/O: 1714529. HI-LOCK: P/N: HL10VF5-4, P/O: 1718904. HI-LOCK: P/N: HL10VF-5, P/O: 1700429. BOLT: EN6115V4-7, P/O: 1559750. NUT SELF: P/N: ASNA2528-4, P/O: 1737831. HI-LOCK P/N: HL10VF5-5 P/O:1714529 HI-LOCK P/N:HL10VF5-4 P/O:1718904 COLLAR P/N: HL70-5 P/O:1700429 BOLT P/N: EN6115V4-7 P/O:1559750 NUTSELF P/N: ASNA2528-4 P/O: 1737831"

Part: NONE — NONE · airframe 32,152 hrs · 23,794 cycles

NRC 2000-0048: 031-9 AFT PASSENGER CABIN FLOOR STRUCTURE, CORROSION FOUND AT LH THRESHOLD BEAM LOWER MAIN SILL AREA BTW FRAME 66-68. / AFT PASSENGER CABIN FLOOR STRUCTURE, LOWER MAIN SILL AREA BTW FRAME 66-68, LH THRESHOLD BEAM PERMANENTLY REPAIRED AS PER SRM 53-41-14-300-001 FIGURE 001 SHEET 3 PRINCIPLE 5 AND SHEET 5 PRINCIPLE 8. REPAIR CATEGORY A, NO FURTHER ACTION REQUIRED. SEE AWS FOR STEP DETAILS AND NDT REPORT MWO 48857-13 AND MWO 48857-36."

Part: SKIN — CORRODED (LT WING) · airframe 47,260 hrs · 34,951 cycles

NRC 5000-0042: 33284-34 LH WING, UPPER SURFACE, CORROSION FOUND ON AREA FWD OF SPOILER #3 (BETWEEN RIB 13 AND 14) / LH WING UPPER SURFACE SKIN, FWD OF SPOILER #3 BTW RIB 13-14, UPPER SKIN REPAIRED AND FOUND STRUCTURALLY ACCEPTABLE IAW AIRBUS DOSSIER # 80969544,AIRBUS R572 58998, ISSUE G, PARA A, AIRBUS RDAF 80969544/009/2021#A AND COMPLY WITH ALLEGIANT ERO R5721-0085. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO: 48857-5. REPAIR MAJOR CATEGORY B WITH FURTHER INSPECTION AT THRESHOLD OF 45000FC/80000FH FROM REPAIR EMBODIEMENT. INTERVAL TBD. METHOD TBD. SCREW P/N: NAS1153-5, P/O: 1536024. BOLT P/N: NAS4403-6, P/O: 1559751. NUT P/N: NSA 5472-3K7, P/O: 1712779. PN: EN6114V3-9 PO: 1559750"

Part: NONE — NONE · airframe 47,260 hrs · 34,951 cycles

NRC 1000-0129: AFT CARGO DOOR STRUCTURE, CORROSION LOCATED ON UPPER SURFACE OF FR 55A AT FASTENERS HOLE BTW STR 39RH-38RH / AFT CARGO DOOR SURROUND STRUCTURE ON UPPER SURFACE OF FR55A AT FASTENERS HOLES (QTY.2) BTW STR38RH-39RH SHEET ASSY REPAIRED AS PER AIRBUS MESSAGE 80969195/021 AND COMPLY WITH AIRBUS RDAF #80969195/003/2021#A. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO: 48857-34. 48857-34 REPAIR CATEGORY A. NO FURTHER INSPECTIONS REQUIRED. M360 FORM HAS BEEN SENT TO CUSTOMER NOV/06/2021WORKED PERFORMED IN COMPLIANCE WITH AIR ALLEGIANT ERO II R5341-0063."

Part: SKIN — CORRODED (RT WING) · airframe 47,260 hrs · 34,951 cycles

NRC 6000-0048: 1237-66. RH WING, CORROSION FOUND ON BOTTOM SKIN PANEL #3 UPPER SURFACE, BETWEEN REAR SPAR AND FASLE SPAR AREA, INBD OF RIB #6. / RH WING BOTTOM SKIN PANEL #3 UPPER SURFACE BTW REAR SPAR AND FALSE REAR SPAR AREA INBOARD OF RIB #6, CORROSION REMOVED AND FOUND STRUCTURALLY ACCEPTABLE IAW AIRBUS DOSSIER # 80972667 AND COMPLY IAW REPAIR INSTRUCTIONS R572-58616 ISSUE K SECTION E. CLASSIFICATION MAJOR REPAIR IAW RDAF #80972667/004/2021#A, SOLUTION LIFE OR LIMITATION 6 MONTHS. SEE AWS FOR DETAILS AND NDT REPORT MWO: 48857-42. WORK PERFORMED IAW AIR ALLEGIANT ERO #5721-0084."

Part: NONE — NONE · airframe 49,370 hrs · 31,718 cycles

NRC 5000-0027: 1237-20 LH WING REAR SPAR, MLG RETRACTION ACTUATOR JACK ANCHORAGE FITTING, CORROSION FOUND AROUND BUSHING ON UPPER AND LOWER FACE. / LH MLG RETRACTION,JACK ANCHORAGE FITTING REPAIRED AS PER SRM 57-26-13-300-025. SEE AWS FOR DETAILS.REPAIR CATEGORY C,REPAIR LIFETIME LIMIT OF 30000FC FROM REPAIR EMBODIEMENT AP PER LIFETIME TABLE 001 OF SRM 57-26-13-300-025.REPAIR ACCOMPLISHED AT 34687FC.ANCHORAGE FITTING TO BE REPLACED OR AIRBUS MUST BE CONTACTED NLT 64687FC."

Part: NONE — NONE · airframe 47,260 hrs · 34,951 cycles

NRC 1000-0095: 31594-12 FLOOR LEVEL, ON CARGO DOOR ENTRANCE BTW FRAMES 59 TO 55A, SURFACE CORROSION ON TOP AND UNDER THE FLOOR FRAME STRG 38RH TO 37RH / AT AFT CARGO DOOR ENTRANCE UNDER FLOOR LEVEL BTW FR55A-FR59 AND STR37-38RH AREA, DOORSILL BEAM REPLACED AS PER AIRBUS DOSSIER 80969195, AIRBUS R534 70899A AND COMPLY WITH AIRBUS RDAF 80969195/003/2021#3. NOTE THAT AIRCRAFT JACKING PROCEDURES PERFORMED ON NRC 4001639-1000-0137. PN: D5347715020200 PO: 1737131. WORK PERFORMED IN COMPLIANCE WITH AIR ALLEGIANT ERO # R5341-0063"

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 45,685 hrs · 34,106 cycles

CIDS EPSU SYS TEST FAULTING EPSUC (12WL) / REPLACED EPSU-POWER SUPPLY UNIT, OPS CHECK GOOD, REF AMM 33-51-38"

Part: LIGHT — FAULTED (EMERGENCY EXIT) · airframe 45,652 hrs · 34,088 cycles

NOTICED LH EXIT ROW EMERG LIGHTS REMAIN ILLUMINATED-BITE CK EPSU SYS TEST WITH FAULTS 11WL/DEUB. / "

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 45,060 hrs · 33,787 cycles

EPSU TEST FAILS 13WL AFT LT EMERGENCY SLIDE LT. PERFORMED TSM 25-62-00-810-819-A REMOVED AND REPLACED 13WL ESPU AND FAILS EXTERIOR LIGHTS. CONTINUED TROUBLESHOOTING AND FOUND CONNECTER UNDER SLIDE COVER AT L2 DOOR SLIDE DISCONNECTED. RECONNECTED SLIDE WIRE HARNESS AND EPSU TEST OK, REF AMM 33-51-38 PB 401.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 44,663 hrs · 33,556 cycles

DURING WEEKLY EPSU TEST BATTERY 11WL FLAGGED DURING TEST. REMOVED AND REPLACED EPSU BATTERY 11WL REF A319 AMM 33-51-38 PB 401. OPS CHECK GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 43,676 hrs · 32,998 cycles

WHILE PERFORMING EMERGENCY LIGHT TEST GOT A BAT/ EPSU 13WL AFT L MSG. / REMOVED AND REPLACED EPSU BATTERY ON EPSU 13WL REF A319 AMM 33-51-58 PB401. OPS CHECK GOOD."

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 43,676 hrs · 32,998 cycles

WHILE PERFORMING EMERGENCY LIGHT TEST GOT A BAT/ EPSU 13WL AFT L MSG. / REPLACED EPSU BATTERY ON EPSU"

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 33,374 hrs · 27,587 cycles

AFTER TAKEOFF FROM NLG INDICATOR DISPLAYED, UNLK, ACCOMPANIED WITH ECAM MSG, LG DOORS NOT CLOSED, & LG NOT LOCKED. THE CONDITION WAS OBVIOUS, CONFIRMED, DUE TO EXCESSIVE GEAR NOISE. PERFORMED ECAM PROCEDURE WHICH CORRECTED THE ISSUE. PERFORMED INSPECTION OF NLG PROX SENSORS & TARGET CLEARANCES IAW AMM 32-31-73-200-002-A. SENSORS ARE CURRENTLY WITHIN TARGET LIMITATIONS. NO PHYSICAL DEFECTS NOTED.