N338NV

Part: LENS — BROKEN (ZONE 200) · airframe 53,327 hrs · 34,740 cycles

AIRCRAFT NOT GROUNDED, EXIT LIGHT COVER FROM L1 BROKEN. INSTALLED EXIT LIGHT LENS AT L1 DOOR IAW AMM 33-51-13-400-001-A. A/C OK FOR SERVICE.

Part: SLIDE — FAULTED (ZONE 800) · airframe 52,860 hrs · 34,438 cycles

(AIRCRAFT NOT GROUNDED) LEFT OVERWING SLIDE NOT ARMED / REMOVED AND REINSTALLED LT OVER WING EXIT ROW DOOR TO RESET SLIDE IND. IAW AMM 52-21-11-04 CONF"

Part: COOLING FAN — ODOR (CABIN) · airframe 52,858 hrs · 34,437 cycles

(AIRCRAFT NOT GROUNDED) AFTER LANDING AFT FA'S REPORTED ""DIRTY SOCKS"" SMELL FOR LAST 15 MIN OF FLIGHT ON DESCENT / PERFORMED TC A32X-21-000-001, BEFORE PERFORMING ENGINE RUNS REACTICATED PACK 2 IAW AMM 21-51-00-400-002-A. WHILE AT THE GATE WITH APU BLEED AND BOTH PACKS ON, CAN CONFIRM SMELL. WHILE PERFORMING ENG RUNS WITH PACKS ON AND APU BLEED OFF, NO SMELLS PRESENT. PACING APU ON MEL, REF LP 2053403. TROUBLESHOOTING STILL IN PROGRESS" REMOVED AND REPLACED COOLING FAN IAW AMM 49-52-51-000/400-002-A. OPS CHECK GOOD, NO LEAKS NOTED AT THIS TIME. THIS CLOSES MDDR 214728. C/W MEL 49-10-01-A. PLACARD REMOVED. A/C OK FOR SERVICE.

Part: SLIDE — INOPERATIVE (ZONE 800) · airframe 52,817 hrs · 34,417 cycles

(AIRCRAFT NOT GROUNDED) FA ADVISES L1 DOOR SLIDE WILL NOT ARM / PERFOMED OPS CHECK SEVERAL TIMES IAW AMM 25-42-44-400-006-A NO FAULTS FOUND. NORMAL OPERATION VERIFIED."

Part: FRAME — CRACKED (ZONE 200) · airframe 52,815 hrs · 34,416 cycles

DURING ALLEGIANT INSPECTION PER EO # A32X-E5311-0018, UPPER FUSELAGE DOOR FR16 RH AT DOUBLE JOGGLE AREA IN THE OUTER FLANGE OF THE FRAME AFT ROW OF FASTENER TWO INCHES ABOVE OF THE STOP FITTING 7 FASTENER HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED FASTENER HOLE INDENTIED AS B BUSH REPAIR AND ASSOCIATED HOLE IDENTIFIED AS A OVERSIZED HOLE REPAIR AT FR16 DOUBLE JOGGLE AREA RH SIDE IAW A319 SRM TASK 53-11-12-300-013 PARAG 2A FIG 001 AND 005. THIS REPAIR IS CATEGORIZED AS MAJOR. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q170 ITEM 2-37.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 52,815 hrs · 34,416 cycles

DURING ACCOMPLISHMENT OF THE ALLEGIANT INSPECTION PER WROK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR 66 LHS DOOR STOP FITTING # 2 LOWER I/B HOLE WITH CRACK INDICATION. PERFORMED REPAIR STOP FITTING HOLES OF LH AFT DOOR FR 66 FREEZE PLUG AND OVERSIZED BOLT INSTALLATION FITTING # 2 IAW A319 SRM TASK 53-41-12-300-010 PARAG 2A REV 150 AND TASK 53-41-12-300-008 FING 002 AND FIG 003 REV 150.THIS REPAIR IS CATEGORIZED AS MAJOR. THE REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q170 ITEM 2-42.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 52,815 hrs · 34,416 cycles

DURING ALLEGIANT INSPECTION PER WORK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/ENTRY DOOR FR66 LHS DOOR STOP FITTING # 1 LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED REPAIR STOP FITTING HOLES OF LHS AFT DOOR FR 66 - FREEZE PLUG AND OVERSIZED BOLT INSTALLATION FITTING # 1 IAW A319 SRM TASK 53-41-12-300-010 PARAG 2A REV 150 AND TASK 53-41-12-300-008 FIG 002 AND FIG 003 REV 150. THIS REPAIR IS CATEGORIZED AS MAJOR. THIS REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1Q170 ITEM 2-41.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 52,815 hrs · 34,416 cycles

DURING ALLEGIANT INSPECTION PER WORK CARD A32X-53-260-002, UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 RHS DOOR STOP FITTING # 1 LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED REPAIR STOP FITTING HOLES OF RHS AFT DOOR FR 66 FREEZE PLUG AND OVERSIZED BOLT INSTALLATION FITTING # 1 IAW A319 SRM TASK 53-41-12-300-010 PARAG 2A REV 150 AND TASK 53-41-12-300-008 FIG 002 AND FIG 003 REV 150.THIS REPAIR IS CATEGORIZED AS MAJOR.THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1Q170 ITEM 2-40.

Part: FITTING — CRACKED (ZONE 200) · airframe 52,815 hrs · 34,416 cycles

DURING ACCOMPLISHMENT OF THE ALLEGIANT WORK CARD A32X-53-210-003, UPPER FUSELAGE COCKPIT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTINGS WITH CRACK WERE FOUND. CONTINUITY FITTINGS WERE REPLACED PER ALLEGIANT EO # A32X-STR-53ERO-00285-R00.THIS REPAIR IS CATEGORIZED AS MAJOR. THE REPLACMENT WAS DOCUMENTED UNDER COOPESA JOB A1Q170 ITEM 2-43.

Part: OXYGEN BOTTLE — FAULTED (ZONE 200) · airframe 52,590 hrs · 34,302 cycles

(AIRCRAFT NOT GROUNDED) OXYGEN CONTAINER ROW 26ABC CAME DOWN AFTER TAKE OFF. / REMOVED AND REPLACED EMERGENCY O2 CONTAINER AT 26ABC IAW AMM 35-21-41-000/400-001-A. OPS CHECK GOOD. THIS CLEARS MEL 35-21-01A. MDDR# 209815. PLACARDS REMOVED."

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 52,550 hrs · 34,280 cycles

(AIRCRAFT NOT GROUNDED) EMERGENCY EXIT LIGHT ABOVE R1 DOOR INOP / REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD IAW AMM 33-51-11-04 CONF 00"

Part: STOWAGE BOX — NO TEST (ZONE 200) · airframe 52,210 hrs · 34,140 cycles

(AIRCRAFT NOT GROUNDED) F/O OXYGEN MASK NOT TESTING PROPERLY / REMOVED & REPLACED F/O'S MASK AND BOX REF AMM 35-12-41-400-001-A OPS AND LEAK OK"

Part: SKIN — DENTED (FR21+300) · airframe 51,981 hrs · 34,015 cycles

(AIRCRAFT NOT GROUNDED) (DISCREPANCY NOTED DURING AIRCRAFT HEAVY MX VISIT) PERMANENT REPAIR PER EA 79-2024-184 NEED ACCOMPLISHED. DENT FWD FUSE AT FR21 +300MM, BELOW STR 23L / PERMANENT REPAIR PER EA 79-2024-184 ACCOMPLISHED. DENT FWD FUES AT FR21+300 MM BELOW STR 23L (BTW FR 21-24 AND BTW STGR 22L-25L) AS PER SRM 53-11-11-300-0041 AND ALLEGIANT AIR ERO A32X-STR-53ERO-00122 REV 00 REPAIR CATEGORY B SEE SRI 53-11-11-205-037 FOR INSPECTION REQUIREMENT. INPSECTION THRESHOLD FROM TIME OF REPAIR EMBODIEMENT 60000 FC/120000 FH WHICHEVER OCCURS FIRST, SUBSEQUENT INSPECTION INTERVALS : TBD, INSPECTION METHOD: TBD."

Part: EPSU — NO TEST (EMERGENCY LIGHTS) · airframe 50,525 hrs · 33,269 cycles

DURING EPSU BATTERY CAPACITY TEST ALL FOUR BATTERIES FAILED. / REMOVED AND REPLACED EPSU BATTERIES (10WL, 11WL, 12WL, 13WL) REF AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS TEST GOOD."

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 50,116 hrs · 33,060 cycles

EPSU 11WL FAILED WEEKLY BITE CHECK / TROUBLESHOT PER TSM 33-51-00-810-834-A. REMOVED AND REPLACED 11WL BATTERY PER AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. OPS CHECK GOOD"

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 49,821 hrs · 32,910 cycles

FOUND FWD EMERGANCY LIGHTS OUT / REPLACED EMER BATTERY PACK, FWD FIN 10WL, OPS CHECK GOOD REF AMM 33-51-38-400-002A"

Part: EPSU — UNKNOWN (UNKNOWN) · airframe 49,717 hrs · 32,852 cycles

EPSU BATTERY 13WL AFT, FAILED CAP TEST PER T/C 335100-03-1 / REPLACED AFT EPSU BATTERY FIN 13WL IAW AMM 33-51-38-000-002A AND 33-51-38-400-002A. OPS CHECKS NORMAL."

Part: FRAME — UNKNOWN (ZONE 200) · airframe 49,411 hrs · 32,719 cycles

DURING THE STRUCTURAL INSPECTION AS PER ALLEGIANT TASK: 534124-01-2-001 AN EXISTNG REPAIR WHICH INTERFERES WITH THE INSPECTION AND WITH A DEVIATION WAS FOUND. ALL DETAILS ABOUT EXISTING REPAIR WERE SENT TO AIRBUS ASKING ABOUT FORM APPROVAL TO COVER THE DEVIATION AND THE CHANGE TO MANDATORY INSPECTIONS. AIRBUS PROVIDED THE REPAIR INSTRUCTIONS UNDER DOSSIER 81240187 AND REPAIR WAS DOCUMENTED UNDER COOPESA JOB A1N122 ITEM2-15).

Part: NONE — CORRODED (ZONE 200) · airframe 47,765 hrs · 31,914 cycles

DURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PASSENGER CREW DOOR CUTOUT BETWEEN FR 66 AND FR 68 AT STRG 23R SILL BEAM WITH CORROSION. DUE TO THIS FACT SILL BEAM P/N D5348004320701 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2B. THE REPLACE WAS HANDLED UNDER COOPESA JOB: A1M116 ITEM 2-24

Part: BEAM — CORRODED (ZONE 200) · airframe 47,765 hrs · 31,914 cycles

DURING TH ESTRUCTURE INSPECTION WAS FOUND AT UPPER FUSELAGE FORWARD PAX CABIN AT FR 16, Y503.2 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N: D5311282720200 FROM FR 12 TO FR 16 Y503.2 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE REPLACE WAS HANDLED UNDER COOPESA JOB: A1M116 ITEM 2-28

Part: FRAME — NONE (ZONE 200) · airframe 47,765 hrs · 31,914 cycles

DURING TH ESTRUCTURE INSPECTION WAS FOUND IN THECCKPIT WINSHIEL SIDE POST FR 4LH UPPER ATTACHMENT FITTING AND FRAME SECTION WITH DOUBLE HOLE. DUE TO THIS FACT FITTING P/N D5311086620200 AND FRAME P/N D53111068202200 WERE REPLACED. THE REPAIR WAS HANDLED UNDER COOPESA JOB: A1M116 ITEM 2-15

Part: BEAM — CORRODED (ZONE 200) · airframe 47,765 hrs · 31,914 cycles

DURING TH ESTRUCTURE INSPECTION WAS FOUND IN THE UPPER FUSELAGE AFT PAX CABIN AT FR 68 Y765 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM P/N D5472192200000 WAS REPLACED IAW A319 SRM 51-72-11-911-001 PARAGRAPH 2 . THE REPAIR WAS HANDLED UNDER COOPESA JOB: A1M116 ITEM 2-20

Part: SKIN PANEL — CORRODED (ZONE 200) · airframe 47,765 hrs · 31,914 cycles

DESCRIPTION: DURING THE STRUCTURAL INSPECTION PER ALLEGIANT WORK CARD 200003-01-1-001_P1-OP-UP/0 PROCESS, COO FOUND AT EMPENNAGE, DORSAL FIN AREA WITH CORROSION BETWEEN THE SKIN AND CONNECTOR 7113VC. CORRECTIVE ACTION REPAIRED FUSELAGE SKIN SECTION FROM FR69 TO FR70 BETWEEN STRG 1 AND STRG 2 RH IAW AIRBUS DOSSIER 81077405. SEE COOPESA ITEM 3-8

Part: FITTING — NONE (ZONE 300) · airframe 47,765 hrs · 31,914 cycles

DESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #7 BEARING WITH PLAY. CORRECTIVE ACTION: REPLACED FORK AND END FITTING AT HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-008. SEE COOPESA WORK ORDER A1M116 3-17

Part: FITTING — EXCESS PLAY (ZONE 300) · airframe 47,765 hrs · 31,914 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE#5 BEARING WITH PLAY. REPLACED FORK AND END FITTING AT HINGE ARM BR5 IAW A319-SRM TASK 55-36-42-300-008. SEE COOPESA WORK ORDER A1M116 3-16

Part: SKIN PANEL — DENTED (ZONE 500) · airframe 47,765 hrs · 31,914 cycles

DESCRIPTION: DURING THE STRUCTURAL INSPECTION, IT WAS FOUND AT LH WING SLAT #1 FROM TRACK #2 100MM O/B AND 111MM FROM THE LOWER EDGE, EXTERNAL SKIN WITH DENT CORRECTIVE ACTION EVALUATED DENT AND IT WAS FOUND WITHIN LIMITS IAW A319 SRM 57-40-00-283-001 FIGURE 001 SHEET 4 AND FIGURE 4 AND PERFORMED PERMANENT FILLING AT SLAT #1 IAW A319 SRM TASK 5740-00-300-106 PARAGRAPH 2A(2)FIGURE 002 SEE COOPESA ITEM 5-28

Part: BEAM — CORRODED (ZONE 200) · airframe 29,009 hrs · 17,557 cycles

DURING TH ESTRUCTURE INSPECTION WAS AT UPPER FUSELAGE AFT PAX CABIN AT FR 68+80MM Y160.5 LONGITUDINAL BEAM WITH CORROSION. DUE TO THIS FACT LONGITUDINAL BEAM FROM FR 68 TO FR 70 Y160.5 WAS REPLACED IAW A319 SRM 51-72-11-911-001. THE REPLACE WAS HANDLED UNDER COOPESA JOB: A1M116 ITEM 2-21

Part: FITTING — EXCESS PLAY (ZONE 300) · airframe 47,765 hrs · 31,914 cycles

DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE#4 BEARING WITH PLAY. REPLACED FORK AND END FITTING AT HINGE ARM BR4 IAW A319-SRM TASK 55-36-42-300-008. SEE COOPESA WORK ORDER A1M116 3-15

Part: FITTING — NONE (ZONE 300) · airframe 47,765 hrs · 31,914 cycles

DESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE #3 BEARING WITH PLAY. CORRECTIVE ACTION: REPLACED FORK AND END FITTING AT HINGE ARM BR3 IAW A319-SRM TASK 55-36-42-300-008. SEE COOPESA WORK ORDER A1M116 3-18

Part: FITTING — CORRODED (ZONE 300) · airframe 47,765 hrs · 31,914 cycles

DESCRIPTION: DURING THE STRUCTURAL INSPECTION PER WORK CARD Nº: 553006-01-2-001 MPD, IT WAS FOUND AT EMPENNAGE RUDDER HINGE ARM#7 WITH CORROSION. CORRECTIVE ACTION: REPLACED HINGE ARM BR7 IAW A319-SRM TASK 55-36-42-300-003. SEE COOPESA WORK ORDER A1M116 3-6

Part: MEGAPHONE — NONE (FWD CABIN) · airframe 48,648 hrs · 32,363 cycles

FWD MEGAPHONE FAILED PRE FLIGHT INSPECTION / PERFORMED OPS CHECK ON MEGAPHONE ""FLASHING GREEN"" INDICATES GOOD BATTIERIES. OPS CHECK GOOD PER AMM 25-65-710-002"

Part: MEGAPHONE — NO TEST (EMERGENCY LIGHTS) · airframe 48,648 hrs · 32,363 cycles

AFT MEGAPHONE FAILED PRE FLIGHT INSPECTION / REMOVED AND REPLACED MEGAPHONES PER LOPA ""A125000L03"" REV ""00"" AND PER AMM 25-65-51"

Part: NONE — NONE · airframe 48,120 hrs · 32,100 cycles

R2 DOOR SLIDE INADVERTENTLY DEPLOYED / REPLACED R2 SLIDE PER AMM 25-62-44-000-802-A. GOOD FOR SERVICE."

Part: EPSU — NONE · airframe 48,086 hrs · 32,089 cycles

EPSU BATTERY (10WL) FWD L FAILED WHEN PERFORMING TC CHECK BATTERY CAPACITY 335100-03-1-001. / R&R EPSU BATTERY (10WL) FWD L IAW TSM 33-51-00-810-822-A. OPS CHECK GOOD. NO DEFECTS NOTED."

Part: MEGAPHONE — NONE · airframe 47,925 hrs · 32,012 cycles

R2 MEGAPHONE INOP / R&R'D MEGAPHONE IN REF TO AMM 25-65-11. OPS CHECK GOOD."

Part: FRAME — CRACKED (ZONE 200) · airframe 47,765 hrs · 31,914 cycles

DURING THE STRUCTURAL INSPECTION PER 531135-01-2-001 MPD, IT WAS FOUND LH WINDSHIELD SIDE POST UPPER ATTACHMENT AT FRAME 4 WITH A HOLE WITH CRACK INDICATION AND FITTING WITH A DOUBLE HOLE AND FRAME SECTION WITH TOOL MARK. . DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL UNDWE AIRBUS DOSSIER 81076000 AND COOPESA´S EO COO-EO-2022-15817-R02 .

Part: COVER — MISSING (R/H FWD) · airframe 46,985 hrs · 31,532 cycles

THE R/H FWD EMERGENCY EXIT WALL MOUNTED LIGHT COVER MISSING / REPLACED MISSING LENS COVER ON THE R/H FWD EMERGENCY EXIT WALL MOUNTED LIGHT IAW AMM 33-51-13"

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 46,410 hrs · 31,198 cycles

WHEN POWER IS DISCONNECTED AND EMERGENCY LIGHTS ARE SUPPOSED TO TRIGGER ON, ONLY THE REAR CABIN EXIT SIGN AND OVERHEAD LIGHTS AT SEAT ROWS 19 AND 28 ILLUMINATE. ALL OTHER OVERHEAD LIGHTS ARE INOP, INCLUDING OVERWING EXIT SIGNS AND L1 & R1 EXIT SIGNS. / FOUND (10WL , 11WL AND 12WL) EPSU BATTERY TO BE FAULTING REPLACED ALL 3 BATTERY IAW AMM 33-51-38 PB 401 OPS CHECK GOOD AT THIS TIME."

Part: BATTERY PACK — FAULTED (EMERGENCY LIGHTS) · airframe 46,408 hrs · 31,197 cycles

WHEN POWER IS DISCONNECTED AND EMERGENCY LIGHTS ARE SUPPOSED TO TRIGGER ON, ONLY THE REAR CABIN EXIT SIGN AND OVERHEAD LIGHTS AT SEAT ROWS 19 AND 28 ILLUMINATE. FOUND (10WL , 11WL AND 12WL) EPSU BATTERY TO BE FAULTING REPLACED ALL 3 BATTERY IAW AMM 33-51-38 PB 401.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 45,570 hrs · 30,713 cycles

R/H OVER WING EMERGENCY POWER PACK BATTERY FAILS TEST. / REPLACED R/H EMERGENCY POWER PACK BATTERY AND PERFORMED OPS TEST PER AMM 33-51-38 P/B 401. OK FOR SERVICE."

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 44,171 hrs · 29,962 cycles

CABIN EMERGENCY BATTERY CLASS 1 FAULT AFT L (13WL) / REMOVED AND REPLACED AFT L EMERGENCY SUPPLY BATTERY UNIT IAW AMM 33-51-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD"

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 44,134 hrs · 29,943 cycles

DESCENDING THROUGH APPROXIMATELY FL320 RECEIVED ECAM CAB PR EXCESS CAB ALT AND COMPLIED WITH THOSE PROCEDURE. CABIN PRESSURE GOT AS HIGH AS 12500 FT. MASK DID NOT DEPLOY. OTHER ECAM THAT FOLLOWED WERE CABPR LO DIFF PR, DOOR R AFT CABIN, AND CAB PR SAFETY VALVE OPEN. R & R BOTH 1 & 2 C.P.C.'S AND OUTFLOW VALVE. OPS TEST OF ALL 3 ITEMS GOOD IAW AMM 21-31-00-710-002, & 21-31-00-710-003."

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 43,374 hrs · 29,545 cycles

DURING EMERGENCY LIGHT TEST FOUND EMERGENCY BATTERY PACK 12WL INOP / "

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 43,374 hrs · 29,545 cycles

DURING EMERGENCY LIGHT TEST FOUND EMERGENCY LIGHT BATTERY PACK 11WL INOP. / "