N271NV
Registered owner: ALLEGIANT AIR 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) (EMERGENCY DECLARED) LDG GEAR AND DOORS NOT CLOSED ON TAKEOFF. PREFORMED GVI OF NLG IAW AMM 32-21-00-200-002A. FOUND SAFTEY LOCK STILL INSTALLED IN NLG LOCK STAY. REMOVED SAFTY LOCK FROM NLG LOCK STAY IAW AMM 32-00-00-081-002A. NO OTHER DEFECTS NOTED AT THIS TIME. ACFT GOOD.
(AIRCRAFT NOT GROUNDED) DURING WEEKLY FOUND EPSU BATTERY 10WL FAILED / REMOVED AND REPLACED 10WL EPSU BATTERY WITH REPAIRED BATTERY IAW AMM 33-51-38-000/400-002-A."
(AIRCRAFT NOT GROUNDED) FWD MEGAPHONE BROKEN / FOUND REPLACEMENT FWD MEGA PHONE. REMOVED AND REPLACED FWD MEGA PHONE IAW AMM 25-65-21. OPS CHECK GOOD"
AIRCRAFT NOT GROUNDED, R2 DOOR EXIT COVER FELL OFF. INSTALLED EXIT COVER AT DOOR R2 PER AMM 33-51-17-400-001A. A/C OK FOR SERVICE.
(AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL IN CABIN AND FLIGHT DECK ON DESCENT / PERFORMED AMM 21-00-00-615-803-B REMOVAL OF THE CONTAMINATION OF THE ECS, NO FAULTS NOTED AND NO SMELL DETECTED. THIS CLEARS MEL 21-52-01-G, CAT C, MDDR#218679 'M' PROCEDURE REVERSED, INOP PLACARD REMOVED. C/W OIL TYPE SMELL-PHASE 3 IAW ALLEGIANT AIR TC 21-000-003. NO SMELL REPRODUCED AT THIS TIME. DAMAGE FOUND WHILE PERFOMING APU BOROSCOPE INSP WO#529958 TASK CARD A32X-21-000-002. APU REPLACED AND PERFORMED TC 21-000-003.
(AIRCRAFT NOT GROUNDED) DIRTY SOCK SMELL OBSERVED DECENDING BELOW 10'000' SMELLED BY CA AND FO / CLEANED APU AIR INTAKE & PLENUM IAW 49-16-00-100-005-A. OPERATED APU & PACKS 1 & 2 - PRECONDITIONED BLEED SYSTEM. OP CK GOOD. NO ODORS DETECTED. C/W THE LEVEL 2 TASK CARD A32X-21-000-002. C/W TC A32X-21-000-003. NO SMELL NOTED AT THIS TIME.
(AIRCRAFT GROUNDED) (EMERGENCY DECLARED) EXCESSIVE CABIN ALTITUDE ECAM / REMOVED AND REPLACED CABIN PRESSURE CONTROLLER CPC 1 AND CPC 2 IAW AMM 21-31-34-000-001-A AND 21-31-34-400-001-A. OP TEST CHECKED GOOD. REMOVED AND REPLACED BOTH AFT GALLEY SAFETY VALVE REF 21-31-52-000-001-A AND 21-31-52-400-001-A. OPS CHECK GOOD. REPLACED 02 GENERATOR CONTAINER ASSY FOR 12DEF ON LOGPAGE 1984723 AND 32DEF ON LOGPAGE 1984708 W/REF TO AMM 35-21-41-400-001-A. REMOVED AND REPLACED OUTFLOW VALVE IAW AMM 21-31-51-400-001-A. C/W OPERATIONAL TEST OF THE PRESSURE CONTROL AND MONITORING SYSTEM IAW AMM 21-31-00-710-002-A. OP'S CHECKS GOOD NO FAULTS NOTED."
(AIRCRAFT GROUNDED) EPSU BATTERY INOP. EPSU BATTERY (11WL) EMER L REQUIRED A REMOVAL AND REPLACE. / (RESOLVED ON W/O: 511713 TASKCARD: NR-00001 ) REMOVED AND REPLACED (11WL) EMER L EPSU BATTERY. IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK GOOD.ITEM: 1REMOVED AND REPLACED (11WL) EMER L EPSU BATTERY. IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK GOOD."
DURING ACCOMPLISHMENT OF THE WORK CARD A32X-53-260-002 UPPER FUSELAGE FR66 LH SIDE DOOR STOP FITTING # 1 AT UPPER AND LOWER I/B HOLES WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. PERFORMED PERMANENT REPAIR ON SECTION 18 AT FR66 LH STOP FITTING # 1 DUE TO WEB WITH CORROSION AND CRACKED HOLE IAW COOPESA EO # COO-EO-2024-21364-R00 DATED 12-12-2024 AND AIRBUS TD 81502943/032/2024#A. DOCUMENTED APPROVED AND SUBMITTED ON AIRBUS REPAIR AND DESIGN APPROVAL FORM RDAF REF ISSUE 81502943/004/2024#A APPROVED BY ALLEGIANT UNDER ERO A32X-STR-53ERO-00127-R00. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1P229 ITEM 2-51.
DURING ACCOMPLISHMENT OF THE WORK CARD A32X-53-260-003 UPPER FUSELAGE FR68 RH SIDE DOOR STOP FITTING # 1 AT LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. PERFORMED PERMANENT REPAIR ON SECTION 18 AT FR68 LH STOP FITTING # 1 DUE TO WEB WITH CORROSION AND CRACKED HOLE IAW COOPESA EO # COO-EO-2024-21367-R00 DATED 12-12-2024 AND AIRBUS TD 81502889/027/2024#B. DOCUMENTED APPROVED AND SUBMITTED ON AIRBUS REPAIR AND DESIGN APPROVAL FORM RDAF REF ISSUE 81502889/005/2024#B APPROVED BY ALLEGIANT UNDER ERO A32X-STR-53ERO-00126-R00. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1P229 ITEM 2-50.
DURING ACCOMPLISHMENT OF THE WORK CARD A32X-53-260-003 UPPER FUSELAGE FR68 LH SIDE DOOR STOP FITTING # 1 AT LOWER I/B HOLE WITH CRACK INDICATION WAS FOUND.AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. PERFORMED PERMANENT REPAIR ON SECTION 18 AT FR68 LH STOP FITTING # 1 DUE TO WEB WITH CORROSION AND CRACKED HOLE IAW COOPESA EO # COO-EO-2024-21372-R00 DATED 12-12-2024 AND AIRBUS TD 81502946/032/2024#B. DOCUMENTED APPROVED AND SUBMITTED ON AIRBUS REPAIR AND DESIGN APPROVAL FORM RDAF REF ISSUE 81502946/004/2024#B APPROVED BY ALLEGIANT UNDER ERO A32X-STR-53ERO-00125-R00. THIS REPAIR IS DOCUMENTED UNDER COOPESA JOB A1P229 ITEM 2-49.
FA AFT MEGAPHONE INOP. / REPLACED FA AFT MEGA PHONE IAW ALLEGIANT N271NV LOPA"
NRC 5000-0012: 1711-51 ON L/H WING, CORROSION SUSPECTED UNDER TRAIING EDGE SEAL PLATE OUTBORD MAIN HINGE SPOILER #1. / L/H WING TRAILING EDGE OVERHANG EXTENDING FWD OF THE REAR FALSE SPAR, UPPER SKIN PANEL #2 LOWER SURFACE OUTBD OF OUTBD MAIN HINGE SPOILER #1( BTW WX3494-WX4010) PERMANENTLY REPAIRED PER AIRBUS DOSSIER #80990965, REPAIR INSTRUCTION R57258616 ISSUE L AND ALLEGIANT AIR ERO R5721-0136 REV. 00. MAJOR REPAIR WITH 6 MONTHS LIFE LIMITATION PER RDAF #80990965/046/2022#A. SEE NRC 4002030-5000-0053 FOR ZERO STRESS JACKING PROCEDURE. SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS. REFER TO AIRBUS DOSSIER #80990965 FOR MORE DETAILS. AFTER COMPLETION OF WORK M205, M313 AND M360 SENT TO CUSTOMER ON 01/06/2023. SEE RDAF FOR FLIGHT PREPARATION PERFORMANCE. M313 #99000450."
NRC 5000-0013: 1711-57 ON L/H WING, CORROSION SUSPECTED UNDER TRAILING EDGE SEAL PLATE AT INBORD HINGE SPOILER #2. / L/H WING, TRAILING EDGE OVERHANG SKIN PANEL #2 AT INBD HINGE OF SPOILER #2 (BTW RIBS 9-11) UPPER AND LOWER SURFACE PERMANENTLY REPAIRED PER AIRBUS DOSSIER #80990965, TD/80990965/089/2022#A, REPAIR INSTRUCTIONS R57258483 ISSUE C, R57258616 ISSUE L, R57258943 ISSUE E, R57258944 ISSUE E AND ALLEGIANT AIR ERO R5721-0136 REV. 00. REPAIR MAJOR WITH 6 MONTHS LIFE LIMITATION PER AIRBUS RDAF 80990965/046/2022#A. SEE AWS FOR REPAIR STEPS AND ACCESS DETAILS, SEE NRC 4002030-5000-0053 FOR ZERO STRESS JACKING PROCEDURE. REFER TO DOSSIER #80990965 FOR MORE DETAILS. AFTER COMPLETION OF WORK M205, M313 AND M360 HAVE BEEN SENT TO CUSTOMER ON 01/06/2022. SEE RDAF FOR FLIGHT PREPARATION PERFORMANCE. M313 #99000451"
FWD MEGAPHONE IS NOT WORKING / REMOVED AND REPLACED FWD MEGAPHONE IAW ALLEGIANT LOPA DRAWING A2250011L03"
AFT CABIN MEGAPHONE INOP / REMOVED AND REPLACED AFT CABIN MEGAPHONE PER LOPA A2250011L03"
FA STATED EXIT LIGHTS STAYED ON AFTER FOUR CHIMES MIDCENTER AFTCENTER. A/C LEFT OVER WING EXIT. / PERFORMED EPSU BITE TEST.TEST FAILED FOR BATTERY 10WL AND 11WL IAW AMM 33-51-00. REMOVED AND REPLACED BOTH 10WL AND 11WL BATTERIES IAW AMM 33-51-38. OPS-CHECK GOOD."
NRC 5000-0011: 1237-15. LH WING, UPPER SKIN PANEL, SEVERAL CORROSION SPOTS (5X) FOUND AT REAR SPAR AREA BTW RIB 18-20. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (5X) AT REAR SPAR AREA BTW RIB 18-20 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58616 ISSUE K PARA. D AND COMPLY WITH ALLEGIANT ERO #R5721-0087. MAJOR REPAIR NOT CATEGORIZED AND SOLUTION LIFE OR LIMITATIONS OF 6 MONTHS AS PER RDAF 80990965/004/2021#A. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO49436-12. BLEND MAX DIMENSIONS: LENGHT: 3.500IN, WIDTH: 1.400IN, DEPTH: 0.026IN. M360 FORM HAS BEEN SENT TO CUSTOMER DEC/01/2021."
NRC 5000-0014:1237-18. LH WING, UPPER SKIN PANEL, SEVERAL CORROSION SPOTS (7X) FOUND BTW REAR SPAR AND FALSE SPAR AND RIB 7-9. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (7X) BTW REAR SPAR AND FALSE SPAR AND BTW RIB 7-9 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58616 ISSUE K PARA. D AND COMPLY WITH ALLEGIANT ERO #5721-0087. MAJOR REPAIR NOT CATEGORIZED AND SOLUTION LIFE OR LIMITATIONS OF 6 MONTHS AS PER RDAF 80990965/004/2021#A. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO49436-15. BLEND MAX DIMENSIONS: LENGHT: 2.000IN, WIDTH: 1.800IN, DEPTH: 0.016IN. M360 FORM HAS BEEN SENT TO CUSTOMER DEC/01/2021."
NRC 5000-0008: 1237-12. LH WING, UPPER SKIN PANEL SEVERAL CORROSION SPOTS (4X) FOUND AT REAR SPAR AREA BTW RIB 25-26. / LH WING, UPPER SKIN PANEL CORROSION SPOTS (4X) AT REAR SPAR BTW RIB 25-26 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58616 ISSUE K PARA. D AND COMPLY WITH ALLEGIANT ERO #R5721-0087. MAJOR REPAIR NOT CATEGORIZED AND SOLUTION LIFE OR LIMITATIONS OF 6 MONTHS AS PER RDAF 80990965/004/2021#A. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO49436-10. BLEND MAX DIMENSIONS: LENGHT: 6.440IN, WIDTH: 2.720IN, DEPTH: 0.017IN. M360 FORM HAS BEEN SENT TO CUSTOMER DEC/02/2021."
NRC 1000-0005: CRACKS FOUND AT LH SIDEBOX BEAM FLANGE AT S15, FR43, UPPER AND MID FASTENER HOLES / AT LH SIDE BOX BEAM FLANGE LOCATION AT S15 FR43 UPPER AND MID FASTENER HOLE CRACKED ON PRESSURE PLATE ONLY AND REPAIRED AS PER AIRBUS TRM 80991084/001/010/017, RDAF 80991084/004/2021#A AND COMPLY WITH ERO R5331-0038. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO: 49436-23 REPAIR MINOR CATEGORY A NO FURTHER INSPECTION REQUIRED NOTE THAT SB1320-53-1251 EMBODIED AT LH AND RH SIDE AS TERMNINATING ACTION TO AD 2020-02-2020"
NRC 5000-0010: 1237-14. LH WING, UPPER SKIN PANEL, CORROSION FOUND AROUND BONDING SPIGOT HOLE (FRONT SPAR INBD OF RIB 20 AREA) / LH WING, UPPER SKIN PANEL CORROSION AROUNF BONDING SPIGOT HOLE (FRONT SPAR INBD OF RIB 20 AREA) REPAIRED IAW AIRBUS DOSSIER 80990965, TD/80990965/009/2021#A, RDAF 80990965/004/2021#A AND COMPLY WITH ALLEGIANT ERO #R5721-0087. MAJOR REPAIR NOT CATEGORIZED AND SOLUTION LIFE OR LIMITATIONS OF 6 MONTHS AS PER RDAF #80990965/004/2021#A. SEE AWS FOR WORK STEP AND NDT REPORT MWO49436-17 AND 49436-21. BLEND MAX DIMENSIONS: LENGHT: 2.400IN, WIDTH: 1.900IN, DEPTH: 0.014IN. M360 FORM HAS BEEN SENT TO CUSTOMER DEC/02/2021."
NRC 5000-0012: 1237-16. LH WING, UPPER SKIN PANEL, CORROSION FOUND AT REAR SPAR AND RIB 17 AREA. / LH WING, UPPER SKIN PANEL CORROSION AT REAR SPAR AREA AND RIB 17 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58616 ISSUE K PARA. D AND COMPLY WITH ALLEGIANT ERO #R5721-0087. MAJOR REPAIR NOT CATEGORIZED AND SOLUTION LIFE OR LIMITATIONS OF 6 MONTHS AS PER RDAF 80990965/004/2021#A. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO49436-13. BLEND MAX DIMENSIONS: LENGHT: 3.700IN, WIDTH: 2.200IN, DEPTH: 0.034IN. M360 FORM HAS BEEN SENT TO CUSTOMER DEC/01/2021."
NRC 5000-0013: 1237-17. LH WING, UPPER SKIN PANEL SEVERAL CORROSION SPOTS (3X) FOUND AT REAR SPAR AREA BTW RIB 14-15. / LH WING, UPPER SKIN PANEL CORROSION SPOTS AT REAR SPAR AREA BETWEEN RIB 14-15 REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R572-58616 ISSUE K PARA. D AND COMPLY WITH ALLEGIANT ERO #R5721-0087. MAJOR REPAIR NOT CATEGORIZED AND SOLUTION LIFE OR LIMITATIONS OF 6 MONTHS AS PER RDAF 80990965/004/2021#A. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO49436-14. BLEND MAX DIMENSIONS: LENGHT: 5.500IN, WIDTH: 1.700IN, DEPTH: 0.067IN. M360 FORM HAS BEEN SENT TO CUSTOMER DEC/01/2021."
NRC 5000-0015: 1237-19. LH WING, UPPER SKIN PANEL, CORROSION FOUND BTW REAR SPAR AND FALSE SPAR AT RIB 6 AREA. / LH WING, UPPER SKIN PANEL CORROSION BETWEEN REAR SPAR AND FALSE SPAR AT RIB 6 AREA REPAIRED AS PER AIRBUS DOSSIER 80990965 AND REPAIR DRAWING R57258616 ISSUE K PARA.D AND COMPLY WITH ALLEGIANT ERO #5721-0087. MAJOR REPAIR, NOT CATEGORIZED AND SOLUTION LIFE OR LIMITATIONS OF 6 MONTHS AS PER RDAF #80990965/004/2021#A. SEE AWS FOR STEPS DETAILS AND NDT REPORT MWO49436-16. BLEND DIMENSIONS: LENGTH: 5.050IN, WIDTH: 1.700IN, DEPTH: 0.039IN. M360 FORM HAS BEEN SENT TO CUSTOMER DEC/01/2021."
FWD OUTBOARD EMERGENCY FLASHLIGHT BATTERY LOW. / REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT BATTERY IAW CMM 25-60-02. OPS CHECK GOOD."
(EMERGENCY DECLARED) F/CTL SLAT SYS 2 FAULT AFTER LANDING IN ONTARIO / SFCS 2 SLAT PCU VALVE BLOCK PLACED ON MEL 27-84-02A, CAT B, DMI #82402. WTB TEST ACCOMPLISHED IAW AMM 27-81-00-040-001-A - TEST OK. DEACTIVATION OF FSCC 2 ACCOMPLISHED IAW AMM 27-51-00-040-005-A. PLACARDS INSTALLED. M PROCEDURES ACCOMPLISHED."
REF T/C 335100-03-1-001,33-51-00-710-003-A, MANAGEMENT REQUESTS ALL FOUR BATTERIES BE REPLACED / R+R EPSU BATTERY 10WL, 11WL, 12WL,13WL REF AMM 33-51-38PB401, OPS CHECK GOOD"
MID RIGHT EPSU BATT INOP / REMOVED AND REPLACED MID RIGHT EPSU BATT IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD AT THIS TIME.
FWD EPSU BATT INOP / REMOVED AND REPLACED FWD EPSU BATT IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD AT THIS TIME.
AFT EPSU BATT INOP / REMOVED AND REPLACED AFT EPSU BATT IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD AT THIS TIME.
MID LEFT EPSU BATT INOP / REMOVED AND REPLACED MID LEFT EPSU BATT IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS CK GOOD AT THIS TIME.
DURING SLAT EXTENSION WE HAD THE ECAM SLAT FAIL MESSAGE. SLATS LOCKED AT 0 (DEGREES). REPLACED SLAT PCU, REF AMM 27-84-51 PB 401. LEAK AND OPERATIONS CHECK GOOD. NO FURTHER DEFECTS.
CREW REPORTS CAPT MASTER CAUTION LIGHT (AMBER) HAS MISSING BULBS. REPLACED MASTER WARNING SWITCH, IAW ESPM 20-45-11. OPS CHECK GOOD.