N272NV
Service difficulty reports · 46
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N272NV' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N272NV' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR WX0A2025121732672Megaphone · inoperative(AIRCRAFT NOT GROUNDED) FWD MEGAPHONE INOPERATIVE. REMOVED AND REPLACED THE FWD MEGAPHONE.SDR WX0A2025102932617Power Supply · no test(AIRCRAFT NOT GROUNDED) EPSU FAILED BITE CHECK. EPSU TEST PANEL SHOWS BATT FAIL ILLUMINATED. REMOVED AND REPLACED 10WL EPSU BATT PACK IAW AMMS 33-51-38-000-002-A/33-51-38-400-002-A. BITE CHECK GOOD.SDR WX0A2025092232573Battery · inoperative(AIRCRAFT NOT GROUNDED) FWD O/B FLIGHT ATTND JUMPSEAT FLASHLIGHT CHARGE INDICATOR DOES NOT BLINK. REMOVED AND REPLACED BATTERY AT FWD F/A JUMPSEAT FLASHLIGHT IAW A320 AMM 25-65-00-00. OPS CHECK GOOD.SDR WX0A2025090532556Girt Bar · out of adjust(AIRCRAFT NOT GROUNDED) FA UNABLE TO ARM THE SLIDE ON R1 DOOR, LEVER WILL NOT COME DOWN FULLY / FOUND ESCAPE SLIDE GIRT FLAP TO BE NOT ADJUSTED CORRECTLY, READJUSTED GIRT FLAP. OPS CHECK GOOD. REF AMM 25-62-44-400-802-A AND AMM 52-10-00-860-001-A. A/C OK FOR SSDR WX0A2025090232552Battery · discharged(AIRCRAFT NOT GROUNDED) FWD MEGAPHONE BATTERY DEAD / R&R MEGAPHONE BATTERIES REF AMM 25-65-51-920-001-A"SDR WX0A2025050532414Battery Pack · no test(AIRCRAFT NOT GROUNDED) DURING EPSU BAT CAP TEST 13WL BATTERY FAULT. / REMOVED AND REPLACED EPSU BATTERY 13WL PER AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPERATIONAL CHECK SATISFACTORY PER 33-51-00-710-001-A AND AMM 23-73-00-740-005-B."SDR EE4Y2025040822152Skin · bulgedLEFT WING REAR SPAR, TOP SKIN LOWER SURFACE OVERHANG AREA BETWEEN RIB 13 AND RIB 15 SEAL PLATE BULGED. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 13 AND RIB 15 IAW COOPESA EO N° COO-EO-2025-21701-R02 DATED 03/21/2025. APPRSDR EE4Y2025040822151Skin · noneL/H WING BOX TOP SKIN PANEL 2 TRAILING EDGE OVERHANG AT RIB 10 BETWEEN FASTENER #437 AND FASTENER #455 REMOVE EXISTING EXTERNAL REPAIR PLATE. PERFORMED BLEND OUT REPAIR AT LOWER SURFACE UNDER REPAIR PLATE RIB 9 TO RIB 11 AND O/B OF THE REPAIR PLATE RIB 10 TO RSDR EE4Y2025040822150Skin · corrodedLH WING BOX TOP SKIN TRAILING EDGE OVERHANG AREA LOWER SURFACE EXISTING BLEND OUT WITH CORROSION AT RIB 14+400MM. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE AT RIB 14+400MM (AREA 7) IAW COOPESA EO N° COO-EO-2025-21701-R02 DATED 03/21/SDR EE4Y2025040722149Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 SECONDARY FINDING LH WING BOX TOP SKIN TEOH UPPER SURFACE WITH CORROSION BETWEEN WX= 4010,2 AND WX= 4390,2. PERFORMED BLEND OUT REPAIRON LH WING TOP SKIN PANEL 2 UPPER SURFACE BETWEEN WX 3494,5 ASDR EE4Y2025040722148Skin · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 LEFT WING BOX TOP SKIN TRAILING EDGE OVERHANG LOWER SURFACE SKIN WITH CORROSION AT WX=3654,5. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN WX 3494,5 AND WX 4010,2 SDR EE4Y2025040722147Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 LEFT WING TOP SKIN LOWER SURFACE OVERHANG AREA AT WX 4274 WITH CORROSION WAS FOUND. PERFORMED BLENT OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN WX 3494.5 AND WX 4490.52 (AREA 2) SDR EE4Y2025040722146Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572179-01-1-001 LEFT WING REAR SPAR TOP SKIN LOWER SURFACE OVER HANG AREA 11 AND 12 SEAL PLATE BULGED WAS FOUND. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 11/12 (AREA 6) ISDR EE4Y2025040722145Fitting · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT EO A32X-E5311-0013 WINDSHIELD CENTRAL NODE CONTINUTIY FITTING OINLY REPLACMENT REPAIR. PERFORMED EO E5311-0013-R00 AD 2020-17-03 WNDISHIELD CENTRAL LOWER NODE CONTINUITY FITTING ONLY REPLACMENT REPAIR.THIS REPAIR WAS DOCUSDR EE4Y2025040722143Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 LH DOOR STOP FITTING # 3 UPPER OUTBOARD HOLE WITH CRACK INDICATION WAS FOUND. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN CREW ENTRY DOOR ASDR EE4Y2025040722141Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR66 RH DOOR STOP FITTING # 5 UPPER OUTBOARD HOLE WITH CRACK WAS FOUND. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN ENTRY DOOR AT FRE66 RH DOOR SDR EE4Y2025040722142Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR66 DOOR STOP FITTING # 4 UPPER OUTBOARD HOLE WITH CRACK. PERFORMED OVERSIZE BOLTS INSTALLATION ON AFT PAX CABIN ENTRY DOOR AT FR66 RH DOOR STOP FITTING #SDR EE4Y2025040722140Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR FR68RH DOOR STOP FITTING # 7 UPPER OUTBOARD HOLE WITH CRACK. PERFORMED FREEZE PLUG AND OVERSIZE BOLT INSTALLATION AT FR68RH DOOR STOP FITTING # 7 UPPER INBSDR EE4Y2025040622139Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 2022-08-08-30200/2 UPPER FUSELAGE FORWARD ENTRY PASSENGER /CREW DOOR FR16 RHDOUGLE JOGGLE AREA STOP FITTING # 7 HOLE # 4 WITH CRACK INDICATION IN FRAME LAYER WAS FOUND. REPAIRED FUSELAGE FRAME AT DOUBLE JOGGLE AREA SDR EE4Y2025040622138Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-002 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR66 LH DOOR STOP FITTING # 1 LOWER INBOARD HOLE WITH CRACK INDICATION WAS FOUND.PERFORMED FREEZE PLUG AND OVER SIZE BOLTS INSTALLATION AT FR66LH DOOR STOPSDR EE4Y2025040622137Door Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN CREW ENTRY DOOR FR68 RH DOR STOP FITTING # 1 HOLE WITH CRACK WAS FOUND.PERFORMED PERMANENT REPAIR ON FUSELAGE FRAME AT FR68RH STOP FITTING #1 IAW A320 SRM TASK 53-41-12-30SDR EE4Y2025040622136Door Frame · crackedDURING ALLEGAINT TASK ACCOMPLISHMENT TASK A32X-53-260-003 UPPER FUSELAGE AFT PAX CABIN/CREW ENTRY DOOR, FR68 LH DOOR STOP FITTING # 1 LOWER INBOARD HOLE WITH CRACK WAS FOUND.PERFORMED PERMANENT REPAIR ON FUSELAGE FRAME SECTION AT FR68 LH STOP FITTING # 1 IAW ASDR WX0A2025010232246Plug · stripped(AIRCRAFT NOT GROUNDED) APPROX HALFWAY THROUGH THE FLIGHT AT FL280. THE FA'S REPORTED THAT THERE WAS A MUSTY ODOR IN THE AFT CABIN WHICH THEN CLEARED APPROX. 10 MINS LATER. REFER TO REPORT SOF-500 / REF WO 510916 TASK CARD 21-000-002. DURING TASK CARD FOUND LOSDR WX0A2024102332204Battery · failed(AIRCRAFT NOT GROUNDED) FWD AED BATTERY FAIL WARNING MESSAGE / REMOVED & REPLACED AED BATTERY I.A.W. AMM 25-64-10-960-005A. PN OFF = 989803139301........ SN OFF = 79401P. PN ON = 989803139301......... SN ON = 04802P"SDR WX0A2024080732148Megaphone · inoperative(AIRCRAFT NOT GROUNDED) FORWARD FLIGHT ATTENDENT MEGAPHONE INOP / REMOVED AND REPLACED FORWARD MEGAPHONE. OPS CHECK GOOD. REFERENCE ALLEGIANT AIR LOPA"SDR WX0A2024042232019Flashlight · no testEMERGENCY FLASHLIGHT UNDER JUMPSEAT #4 IS NOT FLASHING RED TEST LIGHT / REMOVED AND RESEATED #4 FA FLASHLIGHT IAW STANDARD INDUSTRY PRACTICES. OPS CHECK GOOD. PLACARDS REMOVED. THIS CLEARS DMI 117255.SDR WX0A1900010031960Pressure Switch · faultedAPU AUTO SHUTDOWN INFLIGHT / PER TSM 49-00-81-810-819-A, REPLACED LOW OIL PRESSURE SWITCH PER AMM 49-94-14-000-003-A AND LEAK CHECKED, NO LEAKS NOTED AND SERVICED APU OIL PER AMM 49-90-00-600-007-A (REASON FOR DELAYED REPORT: REGULATORY INTERPRETATION REEVALUASDR WX0A2024012231949Megaphone · inoperativeFWD MEGAPHONE INOP / FWD CABIN MEGAPHONE REPLACED IAW DWG A2250020L03 REV 01."SDR WX0A2023092531850Unknown · unknownREAR AND FRONT MEGAPHONE CHANGE BELOW 50% (NO GREEN LIGHT) / REPLACED FWD AND AFT MEGAPHONE BATTERIES IAW AMM 25-65-51 PB 201.A.C OK FOR SERVICE"SDR WX0A2023090531828Megaphone · unknownFWD MEGAPHONE TIME EXPIRED. / REMOVED AND INSTALLED AFT MEGAPHONE PER L.O.P.A. PERFORMED OPS CHECKS PER AMM 25-65-51-710-002. OPS CHECKS GOOD."SDR WX0A2023090531827Megaphone · unknownFOUND AFT MEGAPHONE EXPIRED. / REMOVED AND INSTALLED AFT MEGAPHONE PER AMM 25-65-51-920-001-A. PERFORMED OPS CHECKS PER AMM 25-65-51-710-002. OPS CHECKS GOOD."SDR WX0A2022113031667Battery Pack · faultedDURING TC 33-51-00-710-003-A EPSU BATTERY 12WL FAULTED. REMOVED AND REPLACED THE EPSU BATTERY 12WL IAW AMM 33-51-38-400-002-A.SDR WX0A2022090674229Megaphone · noneDURING WEEKLY CHECK FOUND AFT MEGAPHONE INOP / REMOVED AND REPLACED BATTERIES IAW AMM 25-65-51, NO HELP. REMOVED AND REPLACED MEGAPHONE IAW LOPA DRAWING# A2250011L03, OPS CHECKS GOOD."SDR WX0A2022090674228Epsu · noneDURING WEEKLY CHECK, PERFORMED OPS TEST OF EMERGENCY LIGHTS. FOUND 10WL EPSU DISPLAYING UNIT FAULT RED LIGHT. / PER TSM 33-51-00-810-822-A REMOVED AND REPLACED ESPU (10WL) IAW AMM 33-51-38."SDR WX0A2022090674227Epsu · noneDURING WEEKLY CHECK FOUND EPSU (12WL) EMER R FAILING. / REMOVED AND REPLACED 12WL BATTERY WITH INSPECTED BATTERY IAW AMM 33-51-38-000-002-A. OPS CHECK GOOD FOR EMER R."SDR WX0A2022020473952Megaphone · inoperativeFWD MEGAPHONE INOP / REMOVED AND REPLACED MEGAPHONE IAW AMM 25-65-51. OPS CHECK GOOD."SDR WX0A1900010073985Skin · corrodedNRC 5000-0011: ( 2062-08 ) L/H WING UPPER SURFACE, FWD OF SPOILER #1 CORROSION FOUND / LH WING UPPER SURFACE, FWD OF SPOILER #1 CORROSION REMOVED AND FOUND STRUCTURALLY ACCEPTABLE IAW AIRBUS DOSSIER # 80111252 AND COMPLY IAW REPAIR DRAWING R572-58616 ISSUE K ASDR WX0A2021120873886Epsu · failedEPSU BATTERY FAIL DURING CAP CHECK TC / REMOVED AND REPLACED EPSU BATTERY, FIN 11WL, IAW AMM 31-51-38. OPS CHECK GOOD."SDR WX0A2021051273713Megaphone · inoperativeCABIN EMERGENCY MEGAPHONE INOP / REPLACED MEGAPHONE BATTERIES IAW AMM 25-65-51-920-001-A OPS CK GOOD."SDR WX0A2020080373541Battery Pack · no testEPSU BATTERY (12WL) FAILED BATTERY CAP TEST. / REMOVED AND REPLACED BATTERY IAW AMM 33-51-38-000-002-A AND AMM 33-51-38-400-002-A. OPS CHECK GOOD."SDR WX0A2020071373526Battery Pack · no testEMERGENCY LIGHT TEST FAILED, REPLACED THE BATTERY AT 10WL IAW MM 33-51-38-000-002-A AND MM 33-51-38-400-02-A. OPS CHECKED GOOD IAW MM 33-51-00-710-001-A.SDR DU4R20180412005Skin Panel · corrodedDURING SCHEDULED C CHECK FOUND CORROSION BETWEEN RIB 19 - 20 AT BONDING SPIGOT ON LT WING, TOP SKIN, PANEL 2, UPPER SURFACE.SDR DU4R20180409004Skin · corrodedDURING C-CHECK CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LT NR 1 SKIN PANEL BETWEEN RIBS 1 AND 2 AT THE FRONT SPAR. CORROSION REMOVAL EXCEEDED SRM LIMITS.SDR DU4R20180313003Attach Fitting · gougedRIGHT OUTBOARD ELEVATOR ACTUATOR ATTACH FITTING GOUGED.SDR DU4R20180301002Door Sill · corrodedL2 DOOR SILL HAS CORROSION ON UPPER SURFACE AT FASTENER HOLE FRAME 68, STRINGER 23L.SDR DU4R20180301001Door Sill · corrodedR2 DOOR SILL FASTENER HOLE HAS CORROSION ON UPPER SURFACE FRAME 67 + 14, STRINGER 23R.
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