N311NV
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 = 'N311NV' 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 = 'N311NV' 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 WX0A2026091132952Knob · missing(AIRCRAFT NOT GROUNDED) FWD MEGAPHONE VOLUME KNOB MISSING / R&R MEGAPHONE FWD CABIN IAW AMM REF 25-65-51-02.OPS CHECK PERFORMED,OPS SCHECK GOOD."SDR EE4Y2026230223981Fitting · damagedDURING THE EXECUTION OF ALLEGIANT WORK CARD A32X 25-127-005_P1-OP-UP-LF RELATED WITH SB A320-25-1BKJ REV. 04 / AD 2023-05-14 IT WAS FOUND AT THE LOWER FUSELAGE, AVIONICS COMPARTMENT, ELECTRONICS RACK FIN 80VU RH LATERAL LOWER FITTING WITH ELONGATE HOLE. PER CSDR EE4Y2026250223982Fitting · damagedDURING ACCOMPLISHMENT AS PER ALLEGIANT WORK CARD A32X—25-127-005_P1-OP-UP-LF. RELATED WITH SB A320-25-1BKJ REV. 04 / AD 2023-05-14, IT WAS FOUND ON LOWER FUSELAGE AVIONICS AT RACK 80VU UPPER LATERAL FITTING (R/H) OUTBOARD VERTICAL FLANGE WITH ELONGATED HOLE.SDR WX0A2025120332655Cover · missing(AIRCRAFT NOT GROUNDED) LEAD FA NOTIFIED FLIGHT DECK THAT BOTH L1 AND L2 DOORS MISSING LOWER EXIT LIGHT COVER MISSING. SECURED THE LIGHT COVERS PER SIP. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR WX0A2025061832463Cover · broken(AIRCRAFT NOT GROUNDED) EMERGENCY EQUIPMENT COVER BY L2 DOOR IS BROKEN. / FOUND EMERGENCY EQUIPMENT COVER HINGE PIN PULLED OUT. REINSTALLED PIN REF AMM 25-27-15-400-001-A."SDR WX0A2025061832464Pin · out of position(AIRCRAFT NOT GROUNDED) LEFT OVERWING EXIT SLIDE SHOWS DISARMED / FOUND LATCH PIN ON LH AFT EMERGENCY EXIT HATCH RELEASED IN DISARMED POSITION PUT LATCH PIN BACK TO ARMED POSITION IAW A319 AMM 25-62-46-400-001-A STEP 5A(3) OPS CHECK GOOD THIS CLEARS MDDR # 214SDR WX0A2025050232407Lens · broken(AIRCRAFT NOT GROUNDED) R2 DOOR EXIT SIGN LENS BROKEN / REMOVED AND REPLACED EXIT SIGN LENS IAW AMM 33-51-13-000/4000-001-A."SDR WX0A2025032432364Oxygen Mask · leaking(AIRCRAFT NOT GROUNDED) CREW REPORTS CAPTAIN O2 MASK LEAKING / REMOVED AND REPLACED CAPTAINS O2 MASK IAW AMM 35-12-41-000-002-A AND 35-12-41-400-002-A. OPS CHECK GOOD"SDR WX0A2024070332103Battery · inoperative(AIRCRAFT GROUNDED) AFT FA MEGAPHONE BATTERY LIGHT NOT FLASHING / REMOVED AND REPLACED BATTERIES ON AFT FA MEGAPHONE IAW AMM 25-65-51-920-001-A. OPS CHECK GOOD."SDR WX0A2024031231973Spring · brokenDOOR ASSIST BOTTLE, SPRING UNDER DEADTIVATION ROD, FOUND BROKEN DURING SLIDE REPLACEMENT. / REMOVED AND REPLACED L-2 DOOR DAMPER/EMERGENCY OPERATION CYLINDER. SEE AMM PRINTED JOB CARDS 52-13-14-400-001-B & 52-13-14-820-002-A FOR WORK ACCOMPLISHED"SDR WX0A2024031231972Slide · noneL2 DOOR SLIDE EXPIRED. REQUIRES REPLACEMENT. / REMOVED AND REPLACED L2(7502MM) SLIDE REF A320 AMM 25-62-44-000-002-A AND 25-62-44-400-006-A."SDR EE4Y2024021419450Frame · out of toleranceDURING ACCOMPLISHMENT OF ALLEGIANT ENGINEERING ORDER E5311-0019 FR 16 LH DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP # 7 HOLES # 1 THRU #6,#8,#B,#D AND AT LEVEL OF DOR STOP#1 HOLES #9 THRU #19 WERE FOUND GREATER THAN THE STARTING HOLE DIAMETER FOR COLDWORK PROCESSDR EE4Y2024021419449Frame · out of toleranceDURING ACCOMPLISHMENT OF ALLEGIANT ENGINEERING ORDER E5311-0018 FR 16 RH DOUBLE JOGGLE AREA AT LEVEL OF DOOR STOP # 7 HOLES # 1,#2,#4 THRU #8, #A THRU D AND AT LEVEL OF DOR STOP #1 HOLES #9,#10,#12 THRU #19 WERE FOUND GREATER THAN THE STARTING HOLE DIAMETER SDR EE4Y2024021419448Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 534123-01-2-001 FR 66 RH SIDE INNER CAP JOINTTO GUSSET PLATE AT STGR 10R FOUND FIRST HOLE (FROM UP TO DOWN) WITH CRACK. THE REPAIR WASPERFORMED FOLLOWING THE REPAIR INSTRUCTIONS AS PER A319 SRM 53-41-12-300-018.THE RSDR EE4Y2024021419447Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 534123-01-2-001 FR 66 LH SIDE INNER CAP JOINT TO GUSSET PLATE AT STGR 15L FOUND SECOND HOLE (FROM UP TO DOWN) WITH CRACK. THE REPAIR WAS PERFORMED FOLLOWING THE REPAIR INSTRUCTIONS AS PER A319 SRM 53-41-12-300-018.THSDR EE4Y2024021419445Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK 534123-01-2-001 FR 66 LH SIDE INNER CAP JOINT TO GUSSET PLATE AT STGR 12L FOUND SECOND HOLE (FROM UP TO DOWN) WITH CRACK. THE REPAIR WAS PERFORMED FOLLOWING THE REPAIR INSTRUCTIONS AS PER A319 SRM 53-41-12-300-018.THSDR EE4Y2024021419444Frame · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT ENGINEERING ORDER E5311-0019 , FR 16 AT DOUBLE JOGGLE AREA LH SIDE HOLE # 13 HAS BEEN FOUND WITH CRACK INDICATION.AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR SOLUTION UNDER DOSSIER 81014204SDR EE4Y2024021419443Frame · crackedDURING ALLEGIANT TASK 53-120-003 ACCOMPLISHMENT FR 16 LH CROSSBEAM SPLICING UPPER ROW OF FASTENER HOLE IDENTIFIED AS H2 WITH CRACK WAS FOUND.AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSIER 81345090. THE RESDR WX0A2023121131914Epsu · unknownFAILED EPSU BATTERY AT FIN LOCATION 12WL / R&R EPSU BATTERY AT FIN LOCATION 12 WL IAW AMM REF 33-51-38-000-002-A AND 33-51-38-400-002-A.OPS CHECK PERFORMED,OPS CHECK GOOD."SDR WX0A2023032431741Epsu · unknownEMERGENCY LIGHTS AND SIGNS ARE INOP AT L1 DOOR AT L1 AND R1 WHILE ON BATTERY POWER / REMOVED AND REPLACED EMERG BATTERY PER AMM 33-51-338-400-002-A"SDR EE4Y2023031017371Frame · corrodedDURING THE STRUCTURE INSPECTION PER ALLEGIANT ENGINEERING ORDER E5316-0002 REV00 WE FOUND FOUND AT UPPER FUSELAGE FR20, RH SIDE, AT LEVEL OF DOOR STOP #1, FRAME WITH CORROSION. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER AIRBUS INSTRUCTIONS STATED IN COOSDR EE4Y2023031017369Fitting · crackedDURING THE STRUCTURE INSPECTION PER ALLEGIANT ENGINEERING ORDER E5316-0002 REV00 WE FOUND FOUND AT UPPER FUSELAGE FR20, RH SIDE, AT LEVEL OF DOOR STOP #1, INTERCOSTAL FITTING WITH CRACKS. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER AIRBUS INSTRUCTIONS STSDR EE4Y2023031017368Fitting · crackedDURING THE STRUCTURE INSPECTION PER ALLEGIANT ENGINEERING ORDER E5316-0002 REV00 WE FOUND AT UPPER FUSELAGE FR16, LH SIDE, AT LEVEL OF DOOR STOP #7, INTERCOSTAL FITTING WITH CRACKS. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER AIRBUS INSTRUCTIONS STATED ISDR WX0A2022070874144Megaphone · noneFWD MEGAPHONE STUCK ON / REMOVED & REPLACED FWD MEGAPHONE IAW AMM 25-65-51"SDR WX0A2022062074118Megaphone · inoperativeFA FOWARD MEGAPHONE INOP / REMOVED AND REPLACED FWD MEGAPHOME IAW A319 LOPA, OPS CHECK GOOD, A/C OK FOR SERVICE"SDR WX0A2022061574115Battery · inoperativeCABIN EMER LIGHTS BATTERIES AT POS 11WL, 12WL AND 13WL FAILED CAPACITY TEST DURING TC 335100-03-1-001 / REMOVED AND REPLACED THE CABIN EMER LIGHTS BATTERIES AT 11WL, 12WL, AND 13WL IAW AMM 33-51-38-000-001-A AND 33-51-38-400-001-A. OPS CKS GOOD."SDR WX0A2022032574040Epsu · failedDURING REPLACEMENT TEST OF THE L/H OFFWING ESCAPE SLIDE GOT BAT/EPSU(13WL)AFT L MESSAGE. / REMOVED AND REPLACED EPSU BATTERY FIN 13WL IAW AMM 33-51-38. OPS CHECK GOOD AT THIS TIME."SDR WX0A2022032574043Door · out of adjustFWD EMER EXIT RIGHT SIDE INDICATED DISARM ON LANDING / FOLLOWED TSM 52-21-00-810-803-A, ADJUSTED TARGET PER AMM 25-23-47 CHECKS GOOD AT THIS TIME."SDR EE4Y2022020515090Frame · crackedDESCRIPTION:
DURING THE ALLEGIANT E.O. NO: E5316-0002 REV:00 INSPECTIONS AS RELATED TO THE REF. AD: 2019-20-10, ALI: 531103-01-01, SB: 53-1330, IT WAS FOUND INTERCOSTAL FITTINGS WITH CRACK AND FRAME WITH CORROSION
ACTION
INTERCOSTAL FITTING REPLACED PER SDR EE4Y2022020515089Frame · crackedDURING SPECIAL DETAILED INSPECTION ON SERVICE DOOR FRAME FR16 AS PER REF. TASK CARD 531153-02-2-001 INSTRUCTIONS, IT WAS FOUND AT FWD SERVICE DOOR AREA, FR16 BETWEEN STR 10R-11R, FRAME OUTER FLANGE WITH CRACK AT DOOR STOP 7 LEVEL
ACTION
REPAIR WAS PERFORMED SDR EE4Y2022020515088Beam · crackedDURING THE STRUCTURE INSPECTION, IT WAS FOUND THE SIDEBOX BEAM FLANGE AT LH IN S15 FR 43 AREA WITH CRACK
ACTION:
PERFORMED PERMANENT REPAIR AT THE SIDEBOX BEAM FLANGE AT LH IN S15 FR 43 AREA PER ALLEGIANT EO # E5331-0009 AND E5331-0010. THIS EO, BASED ON SB SDR EE4Y2022020515087Angle · unknownPER ALLEGIANT AIR EO 5331-0008 AD 2019-08-07 MODIFICATION REPLACEMENT OF KEEL BEAM TITANIUM ANGLES BETWEEN FR40/42 LH/RH HAS BEEN ACOMPLISHED.SDR EE4Y2022020515086Skin Panel · corrodedDURING THE STRUCTURE INSPECTION, IT WAS FOUND REAR FUSELAGE PASSENGER/CREW DOOR LH CUT OUT AREA FROM FR68 TO FR69+150MM SILL WITH CORROSION.
ACTION:
PERFORMED PERMANENT REPAIR AT PAX/CREW DOOR LH LOWER SILL WEB FROM FR68 AND FR68+160MM, +Y 1260 IAW A319 SRSDR EE4Y2022020515085Skin Panel · corrodedDURING THE STRUCTURE INSPECTION, IT WAS FOUND EXTERNAL LOWER REAR FUSELAGE BETWEEN 150MM AFT OF FR69 AND 200MM OF FR70, STRG 31R AND STRG 32R SKIN WITH CORROSION.
ACTION:
PERFORMED PERMANENT REPAIR AT REAR FUSELAGE BETWEEN 115MM AFT OF FR69 AND 175MM FWD OSDR WX0A2021122773910Megaphone · failedCABIN MEGAPHONE PTT STUCK ON / REMOVED AND REPLACED MEGAPHONE OPS CHECK GOOD REF AMM 25-65-51"SDR WX0A2021072373788Battery Pack · no testEMERG BATTRY FIN 11WL FAILED CAP TEST OVERTEMP / REMOVED AND REPLACED EMERG BATTERY FIN 11WL IAW A319 AMM 33-51-38 OPS CHECK GOOD"SDR WX0A2021072373787Battery Pack · no testEMERG BATTERY FIN 10WL FAILED CAP TEST OVERTEMP / REMOVED AND REPLACED EMERG BATTERY FIN 10WL IAW A319 AMM 33-51-38 OPS CHECK GOOD"SDR WX0A2021072373786Battery Pack · no testEMERG BATTERY FIN 13WL FAILED CAP TEST OVERHEAT / REMOVED AND REPLACED EMERG BATTERY FIN 13WL IAW A319 AMM 33-51-38 OPS CHECK GOOD"SDR WX0A2021072373785Epsu · no testEMERG BATTERY FIN 12WL FAILED CAP TEST OVERTEMP / REMOVED AND REPLACED EMERG BATTERY FIN 12WL IAW A319 AMM 33-51-38 OPS CHECK GOOD"SDR WX0A2021060773733Sign · brokenCABIN WALL-MOUNTED EMERGENCY LENS EXIT SIGN L/H AFT BROKEN. / REMOVED AND REPLACED EMERGENCY LENS EXIT SING L/H AFT IAW AMM 33-51-13. OPS CHECK GOOD."SDR WX0A2021042373685Epsu · faultedEPSU BATTERY AT FIN 12 WL FAULT / REMOVED AND REPLACED EPSU BATTERY ON FIN 12WL, OPS CHECK GOOD, W/REF TO AMM 33-51-38 PB 401"SDR WX0A2020052273507Epsu · failedEPSU BATTERY FIN# 10WL FAILED EPSU BAT CAP TEST / REPLACED EPSU BATTERY"SDR WX0A2019070373404Megaphone · inoperativeCABIN MEGAPHONE INOP. R&R MEGAPHONE.SDR WX0A2019042673393Megaphone · inoperativeAFT MEGAPHONE INOP / R&R MEGAPHONE"SDR WX0A073243Fan · failedVENT EXTRACT FAULT WITH BURNING ELECTRICAL ODOR. R & R AVIONICS EXTRACT FAN.SDR WX0A2016042973145Engine · failedNUMBER 2 ENG FAILED DURING GO AROUND. DISCHARGED NR 1 FIRE BOTTLE. R&R NR 2 ENGINE PER T/C 71-400-001. ALL OPS AND LEAK CHECKS GOOD.
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