N215NV
Registered owner: SUNRISE ASSET MANAGEMENT LLC, NV (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
(AIRCRAFT NOT GROUNDED) DURING CABIN EMERGENCY LIGHTING CHECK BATTERY CAPACITY IAW AMM 33-51-00-710-003-A, EPSU BAT CAP MID R MESSAGE SHOWN. BATTERY 12WL TO BE REPLACED IAW AMM 33-51-38-000-002-A/400-002-A. BATTERY 12WL REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-000-002-A/400-002-A"
(AIRCRAFT NOT GROUNDED) OPS TEST OF EMERGENCY LIGHTING SHOWS. EPSU BATTERY MID L. (11WL) FAULT / AT EPSU 11WL, BATTERY REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-400-002-A.
DURING THE ACCOMPLISHMENT OF THE WORK CARD AS PER ALLEGIANT WORK CARD # A32X-572042-01-2-002 GENERAL VISUAL INSPECTION RELATED TO AD 2022-15-05, IT WAS FOUND ON RH WING, BOTTOM SKIN, REINFORCEMENT PLATE AT RIB 8 WITH CORROSION. REPAIRED RH WING, BOTTOM SKIN, REINFORCEMENT PLATE IAW COOPESA EO # COO-EO-2025-23502-R01 AND AIRBUS RDAF REF ISSUE 81694232/003/2025 # A AND ALLEGIANT A32X-STR-57ERO-00452-R00. THIS REPAIR IS MAJOR AND LIMITED TO 6 MONTHS. THIS REPAIR IS COVERED BY COOPESA JOB A1Q318 ITEM 6-1.
EMERGENCY EXIT LIGHTS ILLUMINATED DURING TAXI OVER EXIT DOORS AND GALLEY. PER AMM 33-51-00-00 CONF00 EMERGENCY EXIT LIGHTS ARE ON WITH SWITCH ARMED AND LANDING GEAR EXTENDED. LIGHTS ARE EXTINQUISHED WHEN LANDING GEAR RETRACTS.
(AIRCRAFT NOT GROUNDED) FA REPORT LOUD SQUEAL COMING FROM EMERGENCY EXITS RIGHT SIDE. SEE PREVIOUS HISTORY / PERFORMED AMM 05-53-00-780-002-A01. FOUND R/H FWD OVER WING EMER EXIT DOOR SEAL TO BE DAMAGED. REMOVED & REPLACED W/REF TO AMM 52-21-18-960-003-A. FOUND R/H AFT OVER WING EMER EXIT DOOR OUTSIDE HANDLE ASSY GASKET DAMAGED. REMOVED & REPLACED W/REF TO AMM 52-21-11-000-002-A & AMM 52-21-11-400-002-A. LEAK CHECK GOOD. NO SQUEAL PRESENT AT THIS TIME."
(AIRCRAFT GROUNDED) FLASHLIGHT AFT RIGHT NOT BLINKING / REMOVED AND INSTALLED, AND REPLACED BATTERY ON FLASHLIGHT ON AFT RIGHT FA SEAT REF CMM 25-60-02. OP'S CHECK GOOD. "
(AIRCRAFT NOT GROUNDED) FOUND FWD EMER LIGHTS INOP. EPSU TEST FAILED. / REMOVED AND REPLACED EPSU BATTERY (10WL) REF AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CHECK GOOD."
(AIRCRAFT NOT GROUNDED) AFT FLIGHT ATTENDANT JUMP SEAT PBE MISSING SEAL AND DEPLOYED / RESECURED AFT RIGHT PBE PER GMM 21.2.15.2"
(AIRCRAFT NOT GROUNDED) RECEIVED ECAM ENG 1 REVERSER UNLOCK CLIMBING THROUGH 8000 / FINISHED INSTALL OF LH ENG OUTBOARD UPPER BLOCKER DOOR, ACTUATION LEVER, AND BUSHING IN REF TO AMM 78-32-41-400-002-A, CMM 78-32-36, AMM 78-31-17-400-003-A. OPS CHECK GOOD.
(AIRCRAFT NOT GROUNDED) MEGAPHONE INOP (FWD) / REPLACED FWD MEGAPHONE PER AMM 25-60-00"
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, APPROX 12.5" O/B OF RIB 16 & 17 AND AT STR. 13 HAS CORROSION. S/O 193150 NR 01366005 HAECO OPS 26232
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, APPROX 4.5" I/B OF RIB 13 STR. 16 CORROSION AROUND FASTENER. S/O 193150 NR 01366013 HAECO OPS 26236
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, RIB 11 AND STR. 15 CORROSION AROUND FASTENER. S/O 193150 NR 01365930 HAECO OPS 26240
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, BETWEEN RIB 8 AND 7 AFT SPAR HAS MULTI AREAS OF CORROSION AROUND MULTI FASTENERS. S/O 193150 NR 01366449 HAECO OPS 26249
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, RIB 6 AND BETWEEN STR. 4 - 9 HAS MULTI AREAS OF CORROSION AROUND MULTI FASTENERS. S/O 193150 NR 01366554 HAECO OPS 26250
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, RIB 4 AFT OF 11 HAS MULTI FASTENERS. S/O 193150 NR 01366551 HAECO OPS 26255
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, RIB 3 AND 11" AFT OF STR. 11 HAS MULTI AREAS OF CORROSION AROUND FASTENERS. S/O 193150 NR 01366438 HAECO OPS 26258
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, APPROX. 17.5" I/B OF RIB 3, STR. 11 HAS CORROSION ON SKIN. S/O 193150 NR 01366000 HAECO OPS 26259
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, APPROX 2" O/B OF RIB 12 AND STR. 11 CORROSION AROUND FASTENER. S/O 193150 NR 01365995 HAECO OPS 26239
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA WHILE ACCOMPLISHING AD 2020-18-06 FOUND R/H FR 34 FOOT CRACKED. S/O 193150 NR-01361831 HAECO OPS 26150
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND R/H WING UPPER SURFACE RIB 17 AT STR. 13 HAS CORROSION. S/O 193150 NR 01365927 HAECO OPS 26231
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, APPROX 7" O/B OF RIB 16 ON AFT ROW OF FASTERNERS, CORROSION AROUND FASTENER HOLES. S/O 193150 NR 01365934 HAECO OPS 26233
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, APPROX 17" I/B OF RIB 13 STR. 16 CORROSION AROUND FASTENER. S/O 193150 NR 01366002 HAECO OPS 26238
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FOUND RH WING UPPER SURFACE, APPROX 2" O/B OF RIB 1 STR. 15 CORROSION AROUND FASTENER. S/O 193150 NR 01365942 HAECO OPS 26235
DURING SCHEDULED INSPECTION/MAINTENANCE AT HAECO, LAKE CITY, FOUND R/H FR 16 DOUBLE JOGGLE UPPER HOLE #5 IS LARGER THAN REPORTED AFTER BUSHING REMOVAL. S/O 194150 NR01362425 HAECO 26682
DURING SCHEDULED INSPECTION/MAINTENANCE AT HAECO, LAKE CITY, FLORIDA FOUND L/H WING BOTTOM AILERON HAD CORROSION ON TRAILING EDGE BELOW #2 STATIC WICK (CENTER). S/O 193150 NR-01332720 HAECO 26283
DURING SCHEDULED INSPECTION/MAINTENANCE AT HAECO LAKE CITY, FLORIDA FOUND R2 DOOR AFT LOWER SHAPE SILL CRACKED. S/O 193150 NR-01345212 HAECO 26697
(AIRCRAFT NOT GROUNDED) EPSU'S 11WL AND 12WL FAIL EMERGENCY LIGHT TEST AND WILL NOT BITE TEST / TROUBLESHOT EMERGENCY LIGHTS AND FOUND THE OVERWING HATCH COVER PANELS WERE SWAPPED PREVENTING THE COVER SENSORS FROM MAKING CONTINNUITY. AFTER CORRECTLY PLACING OVERWING HATCH PANELS IN PLACE, BITE TEST OF THE EPSUS 11WL AND 12WL IS GOOD IAW 33-51-00-710-001-A."
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA FOUND AFT SIDE OF FR 68R, STR. 8 HAS CRACK IN RADIUS OF FRAME. S/O 193150 NR-01361612 HAECO NR 26340
DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA WHILE ACCOMPLISHING CPCP TASK 572651-01-1 FOUND LEFT MAIN LANDING GREAR RETRACTION JACK FITTING ACTUATOR ATTACH BEARING, OUTER SLEEVE HAD PITTED INTERNAL AND CORROSION AROUND UPPER MATING SURFACE. S/O 193150 N/R01361194 HAECO 26188
(AIRCRAFT GROUNDED) FWD R/H OVERWING EMERGENCY EXIT IDENTIFIER INOP / TROUBLE SHOT AND DISCOVERED LOOSE CONNECTOR. CLEANED AND RESECURED ELECTRICAL CONNECTIONS, OPERATIONAL CHECKS GOOD IAW A320 AMM 33-51-13-400-001-A"
(AIRCRAFT NOT GROUNDED) MULTIPLE BULBS IN THE EMERGENCY EXIT SIGNS THROUGHOUT CABIN ARE INOP / RELAMPED BAD BULBS IN THE EMERGENCY EXIT SIGNS IAW AMM 33-51-17-400-01-A. OPERATIONAL CHECK OF THE EMERGENCY POWER SUPPLY UNITS IS GOOD IAW AMM 33-51-00-710-001-A AND OPERATIONAL OF EMERGENCY LIGHTING SYSTEM INCLUDING ALL LIGHTS AND SIGNS IS GOOD IAW 33-51-00-710-805-A."
DURING SCHEDULED INSPECTION, FOUND FR 68 L/H DOOR STOP 1 LOWER I/B HOLE HAS CRACK INDICATION IN FRAME LAYER @ 6 O'CLOCK. 100% SHEET HEIGHT. S/O 193150 NR-01349473 OPS 26298
DURING SCHEDULED INSPECTION, WHILE (WORKING CORROSION TASK CARD 531180-01-10 FOUND L1 DOOR CUTOUT SHAPE SILL, UPPER SURFACE AROUND MULTI FASTENERS HOLES HAD CORROSION. S/O 193150 NR-01346375 OPS 26335
DURING SCHEDULED INSPECTION, FOUND L/H FR 68 HAS CRACK INDICATION AT LOWER RADIUS OF STR. 22 BEGINNING AT I/B RADIUS OF INNER FRAME CAP EXTENDING OUT APPROX. 1.3 INCHES. S/O 193150 NR-01349466 OPS 26297
DURING SCHEDULED INSPECTION AT HAECO, LAKE CITY, FLORIDA WHILE ACCOMPLISHING AD 2020-18-06 FOUND L/H FRAME 43 FOOT CRACKED. S/O 193150 NR 26151 ALLEGIANT NR-01343371
NRC: 7000-0019 ALL 4 EMERGENCY POWER SUPPLY BATTERY DISCHARGED BEYOND RECHARGE CAPACITY. / ALL 4 EMERGENCY POWER SUPPLY UNIT BATTERY REPLACED AND TESTED SERVICEABLE IAW AMM 33-51-38-400-002-A."
NRC 7000-0016: IN PASSENGER CABIN, SEVERAL EMERGENCY LIGHT LAMPS INOP. / IN PASSENGER CABIN, ALL FAULTY EMERGENCY LIGHT RELAMPED AND TESTED SERVICEABLE IAW AMM 33-51-11-400-001-A AND AMM 33-51-13-400-001-A"
NRC 6000-0027: R/H WING TRAILING EDGE UPPER SKIN BETWEEN RIB 9-11 (APPROX. WMRX 22175 TO WMRX 2549.926) REPAIR TO BE ACCOMPLISHED AS PER TD/80468604/051/2022#C/RH WING TRAILING EDGE UPPER SKIN BETWEEN RIB 9-11 (APPROX WMRX 2217.5 TO WMRX 2549.926) PERMANENTLY REPAIRED PER AIRBUS DOSSIER #80468604, TECHNICAL DISPOSITION TD/80468604/051/2022#C, REPAIR INSTRUCTIONS R572-58944 ISSUE E, R572-58943 ISSUE E, R572-58483 ISSUE C AND ERO #R5721-0111 REV.00. MAJOR REPAIR CATEGORY B PER RDAF #80468604/030/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 80468604 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
NRC 6000-0021: (1684-005) AT R/H WING T/E OVERHANG SKIN, QTY 1 HOLE FOUND CRACKED DURING ROTOTEST INSPECTION AT RIB 7 AND AT PANEL 2 EDGE. (AREA FWD OF SPOILER #1)/NDT ROTO TEST CARRIED OUT ON SUSPECTED DAMAGED HOLE AND NO FAULT FOUND AS PER AWS #9. UPON REMOVAL OF SEAL PLATE ON AWS #2 CORROSION WAS FOUND RH WING TOP SKIN TRAILING EDGE UPPER SKIN LOWER SURFACE, AT RIB 7 (FORWARD OF SPOILER 1) AND PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER # 80468604 (ITEMS #1-1A-1B), TECHNICAL DISPOSITION TD/80468604/051/2022#C, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0106 EV.00. MAJOR REPAIR CATEGORY A PER RDAF #80468604/083/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 80468604 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
NRC 6000-0016: (1684-002) CORROSION FOUND AT PREVIOUSLY REPAIRED AREA ON R/H WING T/E TOP SKIN UPPER SURFACE BTW RIB 7 AND RIB 9. AREA FWD OF SPOILER #1./RH WING TOP SKIN TRAILING EDGE UPPER SKIN, FWD OF SPOILER #1 AND BETWEEN RIB 7 AND 9. PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER # 80468604 (ITEMS #2-2A-2B-2C), TECHNICAL DISPOSITION TD/80468604/051/2022#C, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0106 REV.00. MAJOR REPAIR CATEGORY A PER RDAF #80468604/083/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 80468604 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
NRC 6000-0004: 292-03 CORROSION SUSPECTED AT R/H WING T/E UPPER SKIN AT SPOILER #2 AREA BTW RIBS 10 AND 12./RH WING TOP SKIN TRAILING EDGE UPPER SKIN, AT SPOILER #2 AND BETWEEN RIB 10 AND 12. PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER # 80468604 (ITEMS #4-5), TECHNICAL DISPOSITION TD/80468604/051/2022#C, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0106 REV.00. MAJOR REPAIR CATEGORY B PER RDAF #80468604/083/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 80468604 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
NRC 5000-0026: (1684-001) CORROSION FOUND ON L/H WING TRAILING EDGE UPPER SKIN LOWER SURFACE, UNDER T/E SEAL PANEL, AT SPOILER #/ AND BETWEEN RIB 7 AND 8./LH WING TOP SKIN TRAILING EDGE UPPER SKIN LOWER SURFACE, UNDER TRAILING EDGE PANEL, AT SPOILER #1 AND BETWEEN RIB 7 AND 8 PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER #81082830 (ITEMS #1-2), TECHNICAL DISPOSITION TD/81082830/028/2022#B, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0107 REV.00. MAJOR REPAIR CATEGORY A PER RDAF #81082830/005/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 81082830 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS DETAILS."
NRC 6000-0005: 292-04 CORROSION SUSPECTED AT R/H WING T/E UPPER SKIN AT SPOILER #3 AREA BTW RIBS 14 AND 15./RH WING TOP SKIN TRAILING EDGE UPPER SKIN, AT SPOILER #3 AND BETWEEN RIB 13 AND 18. PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER # 80468604 (ITEMS #6-6A-7-8-9-10-11-12-12A), TECHNICAL DISPOSITION TD/80468604/051/2022#C, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0106 REV.00. MAJOR REPAIR CATEGORY B PER RDAF #80468604/083/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 80468604 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
NRC 5000-0019: 1711-10 CORROSION SUSPECTED AT L/H WING TRAILING EDGE UPPER SKIN UNDER T/E SEAL PANEL AT SPOILER #3 BETWEEN RIB 15 AND 16./LH WING TOP SKIN TRAILING EDGE UPPER SKIN UNDER TRAILING EDGE PANEL, AT SPOILER #3 AND BETWEEN RIB 14 AND 17. PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER #81082830 (ITEMS #3-4-5-5A-6-7), TECHNICAL DISPOSITION TD/81082830/028/2022#B, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0107 REV.00. MAJOR REPAIR CATEGORY B PER RDAF #81082830/005/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 81082830 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
1711-12 CORROSION SUSPECTED AT L/H WING TRAILING EDGE UPPER SKIN UNDER T/E SEAL PANEL AT SPOILER #4 BETWEEN RIB 17 AND 18./LH WING TOP SKIN TRAILING EDGE UPPER SKIN UNDER TRAILING EDGE PANEL, AT SPOILER #4 AND BETWEEN RIB 17 AND 20. PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER #81082830 (ITEMS #8-9), TECHNICAL DISPOSITION TD/81082830/028/2022#B, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0107 REV.00. MAJOR REPAIR CATEGORY B PER RDAF #81082830/005/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 81082830 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
1711-14 CORROSION SUSPECTED AT L/H WING TRAILING EDGE UPPER SKIN UNDER T/E SEAL PANEL AT SPOILER #5 BETWEEN RIB 21 AND 22./LH WING TOP SKIN TRAILING EDGE UPPER SKIN UNDER TRAILING EDGE PANEL, AT SPOILER #5 AND BETWEEN RIB 21 AND 22. PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER #81082830 (ITEMS #10-11), TECHNICAL DISPOSITION TD/81082830/028/2022#B, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0107 REV.00. MAJOR REPAIR CATEGORY A PER RDAF #81082830/005/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 81082830 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
NRC 6000-0012: 292-11 CORROSION FOUND ON L/H T/E UPPER SKIN BTW RIB 24 AND 25. (FWD OF AILERON)/RH WING TOP SKIN TRAILING EDGE UPPER SKIN, BETWEEN RIB 24 AND 26 (FORWARD OF AILERON). PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER # 80468604 (ITEMS #14-14A-15-16), TECHNICAL DISPOSITION TD/80468604/051/2022#C, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0106 REV.00. MAJOR REPAIR CATEGORY A PER RDAF #80468604/083/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 80468604 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
NRC 6000-0006: 292-05 CORROSION SUSPECTED AT R/H WING T/E UPPER SKIN AT SPOILER #5 AREA BTW RIBS 22 AND 23./RH WING TOP SKIN TRAILING EDGE UPPER SKIN, AT SPOILER #5 AND BETWEEN RIB 20 AND 23. PERMANENTLY REPAIRED AS PER AIRBUS DOSSIER # 80468604 (ITEMS 13-13A-13B), TECHNICAL DISPOSITION TD/80468604/051/2022#C, REPAIR INSTRUCTION R572-58616 ISSUE K AND ERO #R5721-0106 REV.00. MAJOR REPAIR CATEGORY A PER RDAF #80468604/083/2022#A. REFER TO NRC 4001945-6000-0022 FOR SHORING. REFER TO AIRBUS DOSSIER # 80468604 FOR MORE DETAILS (ADMINISTRATIVE DOSSIER). SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. "
DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND THREE DENTS LOCATED BETWEEN FR28 AND FR29, BETWEEN STR28RH AND STR30RH, THE DENTS WERE FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM TASK 53-21-11-283-020 PARAG. 2A, DUE TO THIS FACT A REPAIR WAS PERFORMED AS PER A320 ALLEGIANT ERO NO 5321-0021 REV 00 AND REPAIR DRAWING A2532100R01-G4 REV. APPROVED BY 8110-3 FAA FORM DTD MAY 15, 2021. JOB A1K167 COO ÃTEM 9-4
DURING MAINTENANCE ACCOMPLISHMENT WERE FOUND A DENT LOCATED AT BETWEEN FR16+190-17+130 BETWEEN STR25RH AND STR26RH, THE DENT WAS FOUND OUT OF ALLOWABLE DAMAGE LIMITS AS PER A320 SRM TASK 53-11-11-283-012 PARAG. 2A, DUE TO THIS FACT A REPAIR WAS PERFORMED AS PER A320 SRM 53-00-11-300-043 PARAG. 2A FIG 001. JOB A1K167 COO ÃTEM 1-37
DURING THE VISUAL INSPECTION PER ALLEGIANT TASK CARD 51-000-001_P1-VISUAL-INSP, LIGHTNING STRIKE WAS FOUND COMMON TO LOWER FUSELAGE SKIN AT FR32+144MM AND STR 43R. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED AS PER A320 SRM TASK 53-00-11-300-042 PARAGRAPG 2A FIGURE 001. FOR ADDITIONAL INFORMATION SEE COOPESA´S WORK ORDER A1K167 SUB JOB 1 ITEM 34.
FWD AND ATF EPSU BATTERIES FAILED TEST, PER TC335100-03-1-001. REMOVED AND REPLACED FWD AND AFT EPSU BATTERIES, IAW AMM 33-51-38. OPERATIONS CHECK GOOD.
EMERGENCY EVACUATION HORN SOUNDED. MUST USE HORN SHUT OFF. RESET EVACUATION HORN IAW TSM 24-00-00-810-077-A. HORN SILENCED.
MID CABIN L EMERGENCY LIGHT BATTERY PACK FAILS THE TEST FROM THE PTP. / REMOVED AND REPLACED ESPU (11WC) BATTERY IAW A320 AMM 33-51-38-000-002-A AND A320 AMM 33-51-38-400-002-A. OPERATIONAL CHECK GOOD IAW A320 AMM 33-51-38-740-053-A."
MID CABIN R BATTERY PACK FAULT IS DISPLAYED ON THE PTP EMERGENCY LIGHTS TEST. REMOVED AND REPLACED MID CABIN R EPSU (12WL) AND BATTERY IAW AMM 33-51-38-000-001-A AND AMM 33-51-38-400-001-A. OPERATIONAL CHECK GOOD IAW AMM SUBTASK 33-51-38-410-052-A.
DIRTY SOCK SMELL REPORTER BY FA DURING FINAL APPROACH. FOUND LOAD COMPRESSOR PLUG BROKEN. R&R APU.
MOLDY SOCK ODOR IN COCKPIT. CLEANED OIL RESIDUE FROM INLET AND APU COWLING. R & R BOTH RECIRCULATION FILTERS.
STRONG ELECTRICAL SMELL AFT OF AC CABIN. PERFORMED INSPECTION OF APU INLET & EXHAUST, NO DEFECTS NOTED.
SIGNIFICANT ELECTRICAL ISSUES IN FLIGHT. CAPTAINS PFD, ND & UPPER ECAM FLICKERED. LOTS OF CLICKING HEARD BEHIND CIRCUIT BREAKERS. ON PARKING, SHUTTING DOWN ENG 1 RESULTED IN ABNORMAL ISSUES ENDING. R & R NR 1 ENG IDG. OPERATIONS & LEAK CHECK GOOD IAW AMM 24-21-51 PB 401.
AFTER TAKEOFF, LG DOOR NOT CLOSED, FAULT APPEARED ON ECAM. AFTER ALL CHECKLISTS WERE COMPLETED RT MAIN GEAR DOOR REMAINED OPENED. ACCOMPLISHED WITHOUT 1570 319 NO4 & ERO 3231-001. OPERATIONS & LEAKS CHECK GOOD, NO LEAKS NOTED IAW AMM 32-33-00, 32-31-00 & 32-12-16. THIS ACTION CLEARS DMI 17898 & MEL 32-12-01A. MCC NOTIFIED & ALL PLACARD REMOVED.
PACK 2 AIR FAULT, MEL 21-26-10A AVIONIC EQUIP VENTILATION COMPUTER, AEVC, ALREADY ON THIS ACFT. THE ACFT HAD AN AIR CONDITIONING PACK FAIL AFTER TAKEOFF. WITH THE MEL CONDITION THEY COULD NOT MAINTAIN NORMAL PRESSURIZATION CONDITIONS. THE CABIN PRESS SLOWLY CLIMBED TO 9,700 FEET. THE CREW DECLARED AN EMER & DID THE ECAM PROCEDURE FOR RAPID DESCENT. THE MAXIMUM RATE OF DESCENT FOR THIS PROCEDURE WAS ABOUT 3,000 FEET PER MINUTE. THE AIRPORT DID ROLL THE EMER EQUIP. THEY DID NOT HAVE THE PAXS BRACE FOR LANDING. TROUBLE SHOT IAW TSM 21-61-00-810-804-A, TSM. R & R PACK 2 FCV, FLOW CONTROL VLV. LEAK CHECK & OPERATIONS CHECKED GOOD ON GND AT THIS TIME. ACFT OK FOR SERVICE IAW AMM 21-51-51.
FLIGHT ATTENDANT SEAT 36 MISSING PBE. REPLACED FLIGHT ATTENDANT PBE AT SEAT 36 IAW AMM 25-60-00.
SEVERAL BULBS INOPERATIVE ON LT & RT EMER OVERWING EXIT SIGN. RELAMPED LT & RT EMER OVERWING EXIT SIGN AS REQUIRED IAW MM 33-51-11. OPERATIONS CHECKED GOOD.