N218NV

Part: BATTERY — NO TEST (ZONE 200) · airframe 57,934 hrs · 35,186 cycles

(AIRCRAFT NOT GROUNDED) BATTERY FAULT AFTER CAPACITY TEST. REMOVED AND REPLACED EPSU REF WO530669.

Part: SEAL — DAMAGED (ZONE 800) · airframe 57,101 hrs · 34,831 cycles

(AIRCRAFT NOT GROUNDED) HIGH SQUEAL PITCH AT EMERGENCY EXIT ROW A/C LEFT PASSING THROUGH 30,000 FEET / REMOVED LH EMERGENCY HATCHES PER AMM 52-21-11-000-001-A, FOUND LH AFT EMERGENCY DOOR SEAL DAMAGED, REMOVED AND REPLACED SEAL PER AMM 52-21-18-960-003-A, PRESSURIZATION TEST GOOD PER AMM 05-53-00-780-001-A, LEAK TEST GOOD. NO WHISTLE NOTED DURING PRESSURE TEST"

Part: ELEC CONNECTOR — FAULTED (ZONE 200) · airframe 57,037 hrs · 34,801 cycles

(AIRCRAFT NOT GROUNDED) CA AND OBSERVER OXYGEN MASKS MICROPHONE INOP. / DISCONNECTED AND RECONNECTED CONNECTOR PLUG ON CAPT'S O2 MASK STORAGE BOX AND CAPT'S OP CKS GOOD IAW AMM 23-51-00-710-004-A OCCUPANT MIC IS NOT CONNECTED PER AMM 23-51-00-710-004-A."

Part: EPSU — NO TEST (ZONE 200) · airframe 56,768 hrs · 34,685 cycles

(AIRCRAFT NOT GROUNDED) EMERG LIGHT TEST FAILS EPSU BATTERY MID L / REMOVED AND REPLACED BATTS AT L MID (11WL) AND AFT L (13WL) AND BOTH POSITIONS BITE CK GOOD. SEE LOG PAGE 1897000 FOR FURTHER TROUBLESHOOTING REF AMM 33-51-38-000/400-002-A."

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 56,768 hrs · 34,685 cycles

(AIRCRAFT NOT GROUNDED) EMERGENCY LIGHT TEST FAILED, EPSU UNIT MID RIGHT / REPLACED MID RIGHT EPSU BATTERY REF A320 AMM 33-51-38-000-002-A & 33-51-38-400-002-A. OPS CHECK GOOD AT THIS TIME. "

Part: HYDRAULIC SYSTEM — LEAKING · airframe 56,312 hrs · 34,484 cycles

(AIRCRAFT NOT GROUNDED) AFT FA REPORTED DIRTY SOCK SMELL IN THE AFT GALLEY AREA. OCCURED ABOUT 1:30 INTO FLIGHT WITH ABOUT 30-40 MIN LEFT. REPRTED SMELL CONTINUED DURING DESCENT AND ALSO AT GATE WITH APU BLEED ON. CABIN ODOR REPORT FILLED OUT. / IN RESPONSE TO 218NV DIRTY SOCK EVENT IT WAS DISCOVERED BY IWAMX TEAM THAT THERE IS A STRONG EVIDENCE OF A HYDRAULIC LEAK WHICH MAYBE CONTAMINATING THE APU. COMPLETED OPS CK REF AMM 49-00-00-860-003A. C/W TC 21-000-002. THIS CLEARS MEL 49-10-01A, MDDR# 202954. PLACARDS REMOVED.

Part: FITTING — GOUGED (ZONE 600) · airframe 56,070 hrs · 34,376 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND #5 SPOILER ON RIGHT WING REAR SPAR O/B LUG IS GOUGED. S/O 193151 NR-00969 HAECO NR 28923

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 56,070 hrs · 34,376 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND LH WING, UPPER SURFACE HAS CORROSION, TOP SKIN PANEL 1, HAS PREVIOUS BLEND APPROX. 48 SQ. IN. AT RIB 9 & 18" INCHES AFT OF FWD SPAR. S/O 193151 NR-1021 HAECO 28256

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,070 hrs · 34,376 cycles

DURING SCHEDULED INSPECTION. FOUND L-1 DOOR SILL CORRODED AT FWD GIRT BAR FITTING ATTACHMENT.

Part: DOOR SILL — CORRODED (ZONE 200) · corrosion level 2 · airframe 56,070 hrs · 34,376 cycles

DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA, FOUND L/H AFT PASSENGER DOOR AFT LOWER CENTER SILL HAS CORROSION. S/O 193151 NR 28776

Part: FRAME — CRACKED (ZONE 200) · airframe 56,070 hrs · 34,376 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FL FOUND CRACK INDICATION IN OPEN HOLE #A AT 2 O-CLOCK IN FRAME LAYER AT UPPER DOUBLE JOGGLE AREA FR 20 LH SIDE. S/O 193151 NR 28489

Part: FRAME — CRACKED (ZONE 200) · airframe 56,070 hrs · 34,376 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FL FOUND CRACK INDICATION IN OPEN HOLE #5 AT 9 O-CLOCK IN FRAME LAYER AT UPPER DOUBLE JOGGLE AREA FR 20 RH SIDE. S/O 193151 NR 28487

Part: SEAL — TORN (R1 DOOR) · airframe 56,070 hrs · 34,376 cycles

(AIRCRAFT NOT GROUNDED) PANEL 841CZ (R1 DOOR) SLIDE ARMING HANDLE CUTOUT SEAL TORN/MISSING / REMOVED AND REPLACED SLIDE ARMING CUTOUT SEAL/SIGHT CLASS ON 841CZ IAW A320 AMM 25-23-46-960-801-A"

Part: SEAL — TORN (L1 DOOR) · airframe 56,070 hrs · 34,376 cycles

(AIRCRAFT NOT GROUNDED) PANEL 831CZ (L1 DOOR) SLIDE ARMING HANDLE CUTOUT SEAL TORN / REMOVED AND REPLACED SLIDE ARMING HANDLE CUTOUT SEAL/SIGHT GLASS IAW A320 AMM 25-23-46-960-801-A"

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 53,102 hrs · 32,963 cycles

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

Part: ACTUATOR — FAULTED (TE FLAP SYS) · airframe 52,585 hrs · 32,721 cycles

(EMERGENCY DECLARED) ON APPROACH FLT CNTL FLAPS FAULT RAN ECAM ATTEMPTED FLAP RESET BY SELECTING PREVIOUS POSSITION FLAP FAULT REMAINED. PERFORMED TSM 27-51-00-810-810-A, FLAP SYSTEM JAM, FOUND TRIPPED TORQUE LIMITER INDICATOR ON L/H WING OF ACTUATOR ASSY 1, PER TSM 27-51-00-810-810-A REQUIRES ROTARY ACUTATORS WITH TRIPPED INDICATORS TO BE REPLACED, NO DISCREPANICES FOUND DOWNSTREAM.REMOVED L/H TRACK 1 ACUTATOR ASSEMBLY FIN (6205CM) P/N 791A0000-06 S/N V8616 PER AMM 27-54-49-000-001-A, INSTALLATION REQUIRED.INSTALLED FLAP TRACK 1 ACTUATOR ASSY IAW: AMM 27-54-49-400-001-A OPS CHECK GOOD.

Part: NONE — NONE · airframe 52,523 hrs · 32,687 cycles

EMERGENCY CEILING LIGHT AT 206WL INOP / REMOVED AND REPLACED LAMPS ON EMERGENCY CEILING LIGHT IAW AMM 33-51-11-000-001-A AND AMM 33-51-11-400-001-A. OPS CHECK GOOD."

Part: EPSU — NONE · airframe 52,523 hrs · 32,687 cycles

FWD 10 WL EPSU BATTERY FAILED BITE TEST / REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK GOOD."

Part: CYLINDER — LOW PRESSURE · airframe 52,158 hrs · 32,515 cycles

R1 DOOR EMER. OPERATION CYLINDER PRESSURE IS LOW. / SERVICED R1 DOOR EMERGENCY OPERATION CYLINDER IAW A320 AMM 52-10-00. NO LEAKS NOTED."

Part: NONE — NONE · airframe 51,537 hrs · 32,216 cycles

NRC 7000-0008: SEVERAL EMERGENCY LIGHT BULB TO BE RELAMP. / ALL EMERGENCY LIGHT BULB INOP REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-16-400-001-A"

Part: SIGN — INOPERATIVE · airframe 51,229 hrs · 32,068 cycles

CABIN WALL MOUNTED EMERGENCY EXIT MARKER ON L2 DOOR HAS MOST LIGHTS OUT, R/H OVERWING HAS 2 LIGHTS OUT AND FWD R1 DOOR HAS 2 LIGHTS OUT / REMOVED AND REPLACED BULBS IAW AMM 33-51-13 PB 401. OPS CHECK OF ALL LIGHTS GOOD."

Part: CONNECTOR — DIRTY (11WL) · airframe 50,596 hrs · 31,700 cycles

11WL FAILS EMERG LIGHT TEST / REMOVED AND CLEANED CONNECTOR AT L MID BATT 11WL AND MESSAGE CLEARED FROM CIDS1; TEST OK REF TC 05-000-002 AND AMM 33-51-00. ALSO REF ESPM 20-55-40"

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,414 hrs · 31,614 cycles

MULTIPLE EMERGENCY EXIT SIGN LAMPS INOP AT RH OVERWING EXIT AND CENTER OVERHEAD SIGN / REPLACED MULTIPLE EMERGENCY EXIT SIGN LAMPS AT RH OVERWING EXIT AND CENTER OVERHEAD SIGN IAW AMM 33-51-11, OPS CHECK GOOD."

Part: CONNECTOR — CONTAMINATED (HYD SYSTEM) · airframe 50,339 hrs · 31,576 cycles

DURING CRUISE GREEN HYD RSVR OVERHEAT FOLLOWED BY SYS LO PRESSURE. OVERHEAT OUT AFTER 25 MIN. \ FOUND CANNON PLUG CONTAMINATED @ ENG PUMP SOLENOID VALVE, CLEANED IAW ESPM 20-55-50. REMOVED AND REPLACED ENGINE 1 GREEN HYDRAULIC PUMP (1030GK) IAW AMM 29-11-51. OPS CHECK AND LEAK CHECK GOOD. REF CT00842429 FOR HYDRAULIC FLUID SAMPLING DUE TO OVERHEAT CONDITION."

Part: LINE — LEAKING (HYD SYSTEM) · airframe 50,335 hrs · 31,574 cycles

DURING CRUISE BEFORE TOP OF DESCENT YELLOW HYDRAULIC RESEVOIR LOST ALL FLUID. ECAM FOR HYD LO LVL ANF PRESSURE. FOLLOWED ECAM AND LANDED NORMALLY / REMOVED AND REPLACED YELLOW HYDRAULIC SYSTEM HCU PIPE ON ENG 2 IAW AMM 29-13-49 OP'S/LEAK CHECK GOOD A/C OKAY FOR SERVICESERVICED YELLOW HYDRAULIC SYSTEM IAW AMM 12-12-29"

Part: DOOR FRAME — CRACKED (FRM 24A S35-36R) · airframe 49,520 hrs · 31,115 cycles

DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND A DENT WITH CRACK LOCATED AT FR24A BETWEEN STR35RH AND STR36RH, THE DAMAGE WAS FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM, DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AFTER AIRBUS EVALUATION, REPAIR INSTRUCTIONS WERE PROVIDED UNDER MESSAGE 80916960/028 DTD MAY 13, 2021. THE REPAIR WAS UNDLE UNDER AIRBUS REF:80916960.

Part: SKIN — DAMAGED (FRM 24 S42-43R) · airframe 49,520 hrs · 31,115 cycles

DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND THE LOWER FUSELAGE AT FR24+385MM, BETWEEN STRG 42R AND STRG 43R SKIN WITH NICKS, THE DAMAGE REMOVAL WAS FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM, DUE TO THIS FACT A REPAIR WAS PERFORMED AS PER A320 SRM TASK 53-00-11-300-029 PARAG. 2A FIG 001. REV 136 UNDER THE JOB A1K164 COO ÍTEM 1-18.

Part: SKIN — CORRODED (RT WING) · airframe 49,520 hrs · 31,115 cycles

DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND CORROSION AT RH WING UPPER SKIN SURFACE AT TRAILING EDGE OVERHANG AND FRONT SPAR AREA, EVALUATED RH WING UPPER SKIN UPPER SURFACE FRONT SPAR AREA BETWEEN RIB 8 AND RIB 9 AND IT WAS FOUND OUT ALLOWABLE DAMAGE LIMITS IAW A320 SRM TASK 57-21-11-283-014 PARAGRAPH 2A (1) FIGURE 001 AND 002 SHEET 2. NOTE: OUT OF LIMITS DUE TO MM² IS MORE THAN 4400MM². THE EVALUATED REWORKED AREAS AT RH WING UPPER SKIN UPPER SURFACE T/E OVERHANG AREA FROM RIB 6A (WX3059) TO WX2440 (GEAR RIB OUTER) AND FROM WX3622 (OUTER JACK RIB) TO RIB 7A (WX4013)AND THEY WERE FOUND OUT OF LIMITS IAW A320 SRM 57-21-11-283-007 PARAGRAPH 2B(2)(A) TABLE 001. THE DAMAGE REPORT WAS SENT TO AIRBUS TO EVALUATION, AND REPAIR INSTRUCTIONS. THE DAMAGE WAS HANDLED UNDER AIRBUS REFERENCE DOSSIER 80917709. JOB A1K164 COO ÍTEM 6-2, 6-3 AND 6-11.

Part: SKIN — DENTED (CARGO DOOR) · airframe 49,520 hrs · 31,115 cycles

DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND THE BULK CARGO DOOR SKIN WITH DENT LOCATED AT FR60+100 BETWEEN BEAMS 5 AND 6, THE DENT WAS FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM, DUE TO THIS FACT A REPAIR WAS PERFORMED AS PER A320 SRM 52-33-00-300-008 FIG 001. REV 136 UNDER THE JOB A1K164 COO ÍTEM 1-27

Part: SKIN — CORRODED (ZONE 600) · airframe 49,520 hrs · 31,115 cycles

DURING THE INSPECTION PER TASK CARD ZL-500-03-1-002_P1-OP-UP/0, CORROSION WAS FOUND COMMON TO RIGHT WING UPPER SKIN FRONT SPAR AREA, BETWEEN RIB 7 AND RIB 8. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER AIRBUS DOSSIER# 80917709 AND APPROVED ON RDAF 80917709/005/2021#A DTD 05-17-2021. FOR ADDITIONAL INFORMATION SEE COOPESA´S WORK ORDER A1K164 SUB JOB 6 ITEM 11.

Part: SKIN — CORRODED (ZONE 600) · airframe 49,520 hrs · 31,115 cycles

DURING THE VISUAL INSPECTION PER ALLEGIANT TASK CARD ZL-500-03-1-002_P1-OP-UP/0, RIGHT WING UPPER SKIN LOWER SURFACE WAS FOUND CORRODED AT OVERHANG AREA RIB 7. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER AIRBUS DOSSIER# 80917709 AND APPROVED ON RDAF 80917709/033/2021#A DTD 05-17-2021. FOR ADDITIONAL INFORMATION SEE COOPESA´S WORK ORDER A1K164 SUB JOB 6 ITEM 3.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,221 hrs · 30,940 cycles

DURING CHECK OF BATTERY CAPACITY, AFT BATTERY(13WL) FAILED / REMOVED AND REPLACED AFT BATTERY(13WL) PER AMM 33-51-38. OPS CHECK GOOD."

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,221 hrs · 30,940 cycles

DURING CHECK OF BATTERY CAPACITY, MID L/H BATTERY(11WL) FAILED / REMOVED AND REPLACED MID L/H BATTERY(11WL) PER AMM 33-51-38. OPS CHECK GOOD."

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,221 hrs · 30,940 cycles

DURING CHECK OF BATTERY CAPACITY, MID R/H BATTERY(12WL) FAILED / REMOVED AND REPLACED MID R/H BATTERY(12WL) PER AMM 33-51-38. OPS CHECK GOOD."

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 49,221 hrs · 30,940 cycles

DURING CHECK OF BATTERY CAPACITY, FWD BATTERY(10WL) FAILED / REMOVED AND REPLACED FWD BATTERY(10WL) PER AMM 33-51-38. OPS CHECK GOOD."

Part: ACTUATOR — MALFUNCTIONED (LT WING TE FLAP) · airframe 48,744 hrs · 30,673 cycles

F/CTL FLAPS FAULT ON ECAM WHEN FLAPS SELECT TO FLAP 2. PER TSM 27-51-00-810-810-A STEP 4A(5) REMOVED AND REPLACED FLAP ACTUATOR 1 ON LT WING, IAW AMM 27-54-49. OPERATIONS CHECK GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 47,987 hrs · 30,253 cycles

REF R OFFWING ESCAPE SLIDE R & R, UPON OPERATIONAL CHECK OF EMERGENCY LIGHTING SYS, RECEIVED EPSU INT LOAD AFT L MAINTENANCE MESSAGE / PER TSM 33-51-00-810-807-A, PERFORMED VISUAL CHECK OF CABIN EMERGENCY LIGHT SYSTEM, FOUND AFT LEFT CABIN DOOR OVERHEAD FWD LAMP INOP, RELAMPED & OPS CHECK OK W/ REF TO AIRBUS AMM 33-51-00-710-009 & TSM 33-51-00-810-807-A, INITIAL FAULT REMAINS. REPLACED AFT EPSU BATTERY (13WL), OPERATIONAL TEST OF EMERGENCY LIGHTING OK, SYSTEM OK W/ REF TO AMM 33-51-38 PB 401 & AMM 33-51-00-710-001."

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,608 hrs · 30,037 cycles

EPSU BATTERY FIN# 10WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,608 hrs · 30,037 cycles

EPSU BATTERY FIN# 11WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,608 hrs · 30,037 cycles

EPSU BATTERY FIN# 13WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"

Part: MEGAPHONE — INOPERATIVE (NOT REPORTED) · airframe 43,854 hrs · 27,989 cycles

FLT ATT REPORTED THE MEGAPHONE WAS INOPERATIVE. R & R THE MEGAPHONE.

Part: SERVO VALVE — FAILED (NLG STEERING) · airframe 39,695 hrs · 25,810 cycles

DURING CRUISE, RECEIVED N/W STRG FAULT ON UPPER ECAM. RESET UNSUCCESSFUL. EMERGENCY DECLARED. REPLACED STEERING SERVO VALVE"

Part: CONNECTOR — CONTAMINATED (NLG) · airframe 39,695 hrs · 25,809 cycles

EMERGENCY DECLARED, DURING CRUISE RECEIVED WHEEL NW STRG FAULT ON UPPER ECAM. UNABLE STEER AIRCRAFT WITH EITHER TILLER PER MAINTENANCE REQUEST. TROUBLE SHOT PER TSM, CLEANED WATER OFF SERVO CONNECTOR. FAULT CLEARED, OPS CHECK AND TAXI CHECK WITH CREW WAS SUCCESSFUL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 35,503 hrs · 23,701 cycles

EMERGENCY EXIT LIGHT LAMP BURNED. REPLACED LAMP IN EMER EXIT SIGNS AS REQUIRED IAW AMM 33-51-16 PB 401. OPERATIONS NORMAL.

Part: SCREEN — DIRTY (SMOKE DETECTOR) · airframe 34,573 hrs · 23,252 cycles

LAVATORY SMOKE ALARM WENT OFF DURING OUR DESCENT. CHECKED LAVATORY SMOKE DETECTORS & CLEANED DUST FROM SCREENS. PERFORMED A CIDS BITE TEST. OPERATIONS CHECKED NORMAL IAW AMM 26-17-00.

Part: GUIDE VANE — DAMAGED (NR 1 ENGINE)

OGV AT 5:30 POSITION ENG 1. DAMAGE BEYOND LIMITS. R & R OGV AT THE 5:30 O CLOCK POSITION ON ENG NR 1 IAW AMM 72-23-00. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 33,867 hrs · 22,931 cycles

SEVERAL BULBS BURNED OUT ON EMER EXIT LOCATION SIGNS AT L1, L2, R1 & R2 DOORS. RELAMPED EMER EXIT LOCATION SIGNS AT L1, L2, R1 & R2 DOORS IAW MM 33-51-11. OPERATIONS CHECKED GOOD.