Airbus A320-251N
Service difficulty reports · 663
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'A320251N' 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 aircraft_model_key = 'A320251N' 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 F3LA2023060800073Mechanism · inoperativeDISCREPANCY REFERENCE LP374249 .THIS IS A SDR REPORTABLE ITEM. OVER WING SLIDE NOT ARMED. CORRECTIVE ACTION: REMOVED AND REPLACED SLIDE RELEASE MECHANISM IAW AMM 52-21-400-003-A. FOR OPS CHECK REF LP347250-3. A/C OK FOR SERVICE.//END//SDR F3LA2023061900081Door Sill · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 14018.0238 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. L2 DOOR, DOOR SILL FASTENERS CORRODED
CORRECTIVE ACTION: EVALUATED 2EA NUT PLATE HOLES AT L2 DOOR AFT DOOR SILL AFTER FURTHER EVALUATION FOUND OUTSDR F3LA2023061900080Shear Plate · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 14018.0237 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULE MX. R/H AFT GALLEY SHEAR PLATE HAS SURFACE CORROSION
CORRECTIVE ACTION: REMOVED & REPLACED MAIN CABIN FLOOR STRUCTURE R/H FR69-70 SHEAR PLATE IAW A320 SDR F3LA2023061600079Shear Plate · crackedDISCREPANCY: REFERENCE AIRBONRE/PEMCO N/R 14018.0236 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX/ L/H AFT GALLEY SHEAR PLATE CRACKED
CORRECTIVE ACTION: REMOVED & REPLACED MAIN CABIN FLOOR STRUCTURE L/H FR69-70 SHEAR PLATE IAW A320 SRM 51-72-11SDR F3LA2023052300062Unknown · unknownDISCREPANCY: REFERENCE LP378169 AIRCRAFT WAS GROUNDED AS A RESULT OF SDR REPORTALE EVENT. 'HYD REVR LO LVL'. REPLACE HYDRAULIC PIPE BY MACHINED PART IN PYLON FRONT SECONDARY STRUCTURE WAS COMPLIED WITH. NO LEAKS FOUND. REF PEMCO VISIT N366FR-4SDR F3LA2023052300061Battery · failedREFERENCE LOG PAGE LP346884 ITEM #2, AIRCRAFT WAS NOT GROUNDED AND WAS AN OVERNIGHT LINE MX CHECK. EPSU BAT. 12WL FAILURE. REPLACED EPSU BAT 12WL REF. AMM 33-51-38-000-002-A/400-002-A. OPS TEST GOOD AT THIS TIME. A/C OK FOR SERVICE.SDR F3LA2023052200060Battery · failedDISCREPANCY: REFERENCE LOG PAGE LP264465 ITEM #1, AIRCRAFT WAS NOT GROUNDED AND WAS AN OVERNIGHT LINE MX CHECK. EPSU TEST FAULT.
CORRECTIVE ACTION: REMOVED AND REPLACED 10WL EPSU BATTERY PER AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPS TEST GOOD PER AMMSDR F3LA2023052300059Unknown · unknownDISCREPANCY: REFERENCE LP 239748 AIRCRAFT WAS GROUNDED AS A RESULT OF AN SDR REPORTABLE EVENT.ON DESCENT COCKPIT & FWD CABIN DETECTED BURNT ORDER. COMPLETED THE ELIMINATION OF ORDOR PROCEDURES DETERMINED PACK 1 WAS RESPONSIBLE FOR ODOR. CORRECTIVE ACTION: PERFSDR F3LA2023051900058Line · leakingDISCREPANCY REFERENCE LP378825 ITEM 1: AIRCRAFT WAS GROUNDED AS A RESULT OF AN SDR REPORTABLE EVENT.HYD Y RSVR LO LVL. REMOVED AND REPLACED PIPE IN YELLOW HYDRAULIC SYSTEM REF AMM 29-13-49-400-B13A, LEAK TEST REQUIRED. ITEM 3: PERFORMED OPERATIONAL TEST OF YESDR F3LA2023061300077Seal · corrodedDISCREPANCY: REFERENCE NR 5001239094--0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORRODED AFT DOOR SILL BEAM ON LH SIDE REQUIRES EVALUATION AS PER A320NEO SRM 53-41-14-283-002 REV. 36
CORRECTIVE ACTION: REPAIRED AFT DOOR SILL BEAM LH AS SDR F3LA2023053000072Seat Track · corrodedDISCREPANCY: REFERENCE NR 5001239088-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION CORRODED SEAT TRACK FOUND BETWEEN FR 68 AT Y765 CORROSION REMOVAL REQUIRED AS PER SRM 51-74-00 REV. 36. PERFORMED BLEND-OUT ON SEAT TRACKSDR F3LA2023053000068Shear Tie · crackedDISCREPANCY: REFERENCE NR 5001239121-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. LH SHEAR PLATE CRACK BETWEEN FRAME 68-70 REPLACEMENT REQUIRED AS PER SRM 51-72-11REV. 36. 4 CRACKS 0.9665IN, 0.2450IN, 0.5675IN, 0.4870IN
CORRECTIVE ACTION: SDR F3LA2023053100069Shear Tie · crackedDISCREPANCY: REFERENCE NR 5001239155-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. RH SHEAR PLATE CRACK BETWEEN FRAME 68-70 REPLACEMENT REQUIRED AS PER SRM 51-72-11REV. 36
CORRECTIVE ACTION: REPLACED RH SHEAR PLATE BETWEEN FR 68-70 AS PER SSDR F3LA2023081700130Unknown · unknownDURING TOP OF DECENT TO JECTR MODERATE INTENSITY - IN COCKPIT & FWD GALLEY AREA. -COCKPIT EYE VENTS. TROUBLESHOT OIL SMELL IN THE FWD GALLEY AREA PER TSM 71-00-00-810-802-A. TSM 05-50-00-810-085-085-A IS THE NEXT STEP TO CONFIRM THE CAUSE FOR CABIN ODOR AND FSDR F3LA2023061300076Beam · corrodedDISCREPANCY: REFERENCE NR 5001238780-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION CORRODED FLOOR BEAM FOUND BETWEEN FR 12-24 AT Y254 REPAIR REQUIRED AS PER EO-A32F-53-22485-00-FINAL & EA# N2-53R-37670
CORRECTIVE ACTION:SDR F3LA2023053000071Seat Track · corrodedDISCREPANCY: REFERENCE NR 5001238812-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION CORRODED SEAT TRACK FOUND BETWEEN FR 12-24 AT -Y765 CORROSION REMOVAL REQUIRED AS PER SRM 51-73-00 AND SRM 51-74-00 REV. 36. PERFORMED SSDR F3LA2023053000070Web · corrodedDISCREPANCY: REFERENCE NR 5001238803-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION CORRODED WEB FOUND BETWEEN FR 12-16 LH AT Y1581 REPLACEMENT REQUIRED AS PER SRM 51-72-11-911-001 REV. 36. REPLACED WEB BETWEEN FR 12-16LHSDR F3LA2023053000067Seat Track · corrodedDISCREPANCY: REFERENCE NR 5001238793-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION CORRODED SEAT TRACK FOUND BETWEEN FR 12-24 AT Y1292 CORROSION REMOVAL REQUIRED AS PER SRM 51-74-00 REV. 36. PERFORMED BLEND-OUT ON SEAT TSDR F3LA2023053000066Seat Track · corrodedDISCREPANCY: REFERENCE NR 5001238818-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION CORRODED SEAT TRACK FOUND BETWEEN FR 12-16 AT Y503.2 CORROSION REMOVAL REQUIRED AS PER SRM 51-74-00 REV. 36. PERFORMED SMOOTH BLEND-OUT OSDR F3LA2023053000065Seat Track · corrodedDISCREPANCY: REFERENCE NR 5001238796-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION CORRODED SEAT TRACK FOUND BETWEEN FR 12-24 AT Y765 CORROSION REMOVAL REQUIRED AS PER SRM 51-73-00 AND SRM 51-74-00 REV. 36. PERFORMED SMOSDR F3LA2023053000064Seat Track · corrodedDISCREPANCY: REFERENCE NR 5001238768-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION CORRODED SEAT TRACK FOUND BETWEEN FR 12-24 AT -Y1292 CORROSION REMOVAL REQUIRED AS PER SRM 51-73-00 AND SRM 51-74-00 REV. 36. PERFORMED SSDR F3LA2023061300075Skin · corrodedDISCREPANCY: REFERENCE NR 5001238053-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING THE INSPECTION OF FWD AND AFT AVIONIC FOUND FR20-24 AT Y520 - Y-175 CORRODED REMOVAL OF CORROSION IS REQUIRED AS PER A320NEO SRM 51-74-00 REV. 36
CSDR F3LA2023051000055Floor Panel · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. UPON INSPECTION FOUND AFT WET AREA FLOOR PANELS IN POOR CONDITION AND REQUIRES EVALUATION. AFT THRESHOLD PANEL 262LG FOUND WITH MULTIPLE SPOTS OF CORROSION ON THE TOP SKIN AND LOWER SKIN. PERFORMED BLSDR F3LA2023050400050Beam · corrodedDISCREPANCY:REFERENCE NR 5001232178-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF AFT CABIN CORRODED FLOOR BEAM FOUND BETWEEN FR.66-70 LH. EVALUATION IS REQUIRED. PERFORMED REWORK MEASUREMENT AS PER A320NEO SRM 51-11-SDR F3LA2023050300049Seat Track · corrodedAFTER EVALUATION FOUND CORROSION IN SEAT TRACK Y-1292 AT FR 20 EVALUATION IS REQ AS PER SRM TASK 53-11-14-283-007 REV.35 PERFORMED REWORK MEASUREMENT AS PER A320NEO SRM 51-11-15 REV.35 L = 64.33MM, W = 49.18MM, D = 1.7MM ORIGINAL THICKNESS = 2.2MM MAXIMUM SDR F3LA202305030047Door Seal · corrodedDISCREPANCY: DURING INSPECTION CORRODED AFT DOOR SILL BEAM FOUND BETWEEN FR.67-68 L/H. EVALUATION IS REQUIRED
CORRECTIVE ACTION: PERFORMED REWORK MEASUREMENT AS PER A320 SRM 51-11-15 REV. 35 L = 40.89MM, W = 35.13MM,
D = 0.87MM NOMINAL SKIN THICKNESS = 1.6MMSDR F3LA2023050300047Web · crackedDISCREPANCY: CRACK WEB ON FWD CABIN FR.12-16 LH DAMAGE OR TASK EVALUATION REFERENCE: A320NEO SRM
53-11-14-06A REV.35, 51-72-11 REV.35.
CORRECTIVE ACTION: PERFORMED REMOVAL OF WEB AT FR12-16 L/H IAW A320NEO SRM 51-42-11 REV.35. PERFORMED INSTALLATION OF NEW PSDR F3LA2023050300046Plate · crackedDISCREPANCY: DURING INSPECTION FOUND L/H AND R/H SHEAR PLATE FR69-70 CRACKED.REQUIRES REPLACEMENT IAW SRM51-72-11-911-001 REV. 35.
CORRECTIVE ACTION: L/H AND R/H SHEAR PLATE WAS REPLACED IAW SRM 51-72-11-911-001 REV.35. P/N: D5347112420200, D5347112420300//ESDR F3LA2023050800053Threshold · corrodedCORRODED UP THRESHOLD SHEET ON FWD CRG BETWEEN FR.24-28 AT STGR.41RH -Y607. EVALUATION IS REQUIRED. CORRODED THRESHOLD SHEET ON FWD CARGO REQUIRES CORROSION REMOVAL AS PER A320NEO SRM 51-74-00 REV.35 PERFORMED REWORK MEASUREMENT AS PER SRM 51-11-15 REV.35 . SDR F3LA2023061300078Panel · corrodedDISCREPANCY: REFERENCE NR 5001238797-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. FWD THRESHOLD PANEL 221FF FOUND CORROSION ON LOWER SURFACE SIDE NO ALLOWABLE DAMAGE FOUND ON SRM. TICKET RAISED TO ENGINEERING.
CORRECTIVE ACTION: FWD THRESSDR F3LA2023033100033Unknown · unknownDISCREPANCY: REFERENCE LP264048 ITEM 1 ENG 1 FEDEC FAULT IN FLIGHT. CORRECTIVE ACTION: PERFORMED UP TO STEP 4.B.(B) SDR F3LA2023040700038Threshold · corrodedDISCREPANCY: REFERENCE NR 5001226088-0020 UPON REMOVAL FOR ACCESS ON INSPECTION FOUND 261LG PANEL CORRODED AND REQUIRES REPLACEMENT.
CORRECTIVE ACTION: REPAIRED 261LG PANEL AS PER EA# N2-53R-37571 REV. ORIG REV DATE. N/A
TASK SUBJECT TO RII. THE EMBODIED REPSDR F3LA2023040700037Beam · corrodedDISCREPANCY: REFERENCE NR 5001226012-0010 CORROSION ON BEAM Y-254 BETWEEN FR12-FR24 AT FR15 MEASUREMENTS REWORK #1L-31.31MM W=22.56MM D=1.08MM REWORK#2 L-21MM W=2.96MM D=100% OF MATERIAL LOSS AREA FOUND OUT OFF LIMITS NO ALLOWABLE LIMITS IN SRM.
CORRECTIVE SDR F3LA2023040600036Door Seal · corrodedDISCREPANCY: REFERENCE NR: 5001225799-0010 CORRODED ANCHOR NUT HOLE ON LH AFT PASSENGER DOOR SILL AT FRAME 68.
CORRECTIVE ACTION: PERFORMED REPAIR PER A320 NEO SRM 53-41-14-300-001 REV. 35//END//SDR F3LA2023040600035Beam · corrodedDISCREPANCY: REFERENCE NR 5001225807-0010 FOUND CORROSION ON BEAM Y-1162.5 FR 68-69 MEASUREMENTS: L=109MM W= 80.6MM D=0.43MM AREA FOUND OUT OF LIMITS AS PER SRM TASK 53-41-14-283-009 REV. 35.
CORRECTIVE ACTION: REPLACED BEAM Y-1162.5 FR 68-69 AS PER SRM 51-SDR F3LA2023040600034Seat Track · corrodedDISCREPANCY: REFERENCE NR 5001225819-0010 FOUND CORROSION ON SEAT TRACK Y1292 AT FR16-17 MEASUREMENTS L-50MM W=20MM D=0.88MM AREA FOUND OUT OFF LIMITS AS PER SRM TASK 53-11-14-283-007 REV. 35
CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 AT FR16-17 AS PER SRMSDR F3LA2023031000030Ruddervator · uncontrollableDISCREPANCY: RUDDER TRIM SYSTEM MADE 4 UNCOMMANDED TRIM INPUTS BETWEEN 1.3 AND 1.9 UNITS RIGHT. RUDDER TRIM RETURNED TO NEUTRAL WITHIN 1 MINUTE OF EACH EVENT.
CORRECTIVE ACTION: AS PER TSM 22-62-00-810-809-A STEP 4A CONTINUITY CHECK PERFORMED. REMOVED AND REPSDR F3LA2023030800029None · faultyDISCREPANCY: ENG 1 FAIL AFTER NORMAL START CORRECTIVE ACTION: REF LP361869 #1 TSWS MDDR# 1192603 FOR T/S OF REPLACEMENT OF ENGINE #1 VSV ACTUATOR R/H. OPS CHECK GOOD. AC OK FOR SERVICE TSM 75-32-00-810-862-A//END//SDR F3LA2023022400024Slide Raft · failedDISCREPANCY, LP257416 ITEM 1 & NR 127475: FAILED EPSU TEST (10WL) (L1 DOOR).
CORRECTIVE ACTION: REPLACED L1 DOOR SLIDE/RAFT ASSY. REF AMM 25-62-44-400-007-A. SEE NR 127475. OPS CHECKED GOOD. T/W S/N F9TAB2940C CAL DUE 7-2023. //END//SDR ANCF20231002003Valve · unserviceablePILOT REPORT
07.FEB.2023 WO 17'032'404=> FUEL CTR L AND R XTR FAULT
FUEL CTR L XFR FAULT ECAM CAUTION CAME ON DURING CRUISE; ECAM PROCEDURE PERFORMED. AFTER ECAM WAS PERFORMED FUEL L WING TANK OVERFLOW ECAM CAUTION CAME ON AND VIBRATION IN THE AIRCRAFT STARSDR F3LA2023030200018Slide · failedDISCREPANCY LP284230 ITEM 2: R2 DOOR SLIDE FAILED EPSU TEST
CORRECTIVE ACTION: REMOVED AND REPLACED SLIDE. TEST OK . T/W F9TAB113036 CAL DUE 07/2023. REF AMM 25-62-44-000-012-A AND 25-62-44-400-803-A//END//SDR F3LA2023030200017Slide · failedDISCREPANCY LP284230 ITEM 1 & N/R 123334: L2 DOOR SLIDE FAILED EPSU TEST
CORRECTIVE ACTION: REF NON ROUTINE 126664 FOR CORRECTIVE ACTION. REMOVED AND REPLACED SLIDE. TEST OK . T/W F9TAB113036 CAL DUE 07/2023. REF AMM 25-62-44-000-012-A AND 25-62-44-400-803SDR F3LA2023060200019Not Reported · not reportedDISCREPANCY: REFERENCE LP274382 ITEM 1, 1R DOOR WILL NOT ARM.
CORRECTIVE ACTION: LUBRICATED R1 DOOR SAFETY PIN GUIDES FITTING AND DOOR ARMING/DISARMING MECHANISM TELESCOPIC CABLE REF. AMM 12-22-52-640-014A AND N/R 127174 AND N/R 127176. OPS CHECK NORMAL.//ENDSDR F3LA2023013010016Fmu · defectiveENGINE 2 STALL ECAM. STALL WAS HEARD AND FELTED, 14,000 FEET 340 KNOTS, ECAM WANT AWAY IMMEDIATELY AND ENGINE PARAMETERS NORMAL. REMOVED & REPLACED ENG #2 FMU PER STEP 4.B.(5).(A). OPS CHECK AND LEAK CHECK GOOD.//END//SDR F3LA2023220100015Battery · failed12WL EPSU BATTERY FAILED. REMOVED AND REPLACED 12WL EPSU BATTERY AMM 33-51-38-400-001-A. OPS TEST GOOD.SDR F3LA2023130100011Warning Message · illuminatedCLIMBING THRU APPROXIMATELY 10,000 FT ENGINE LOW OIL LEVEL ADVISORY WAS FLASHING & LOST OIL RAPIDLY SHORTLY AFTER THAT WE HAD A MASTER WARNING FOR ENG 2 OIL LO PR SHUT ENGINE DOWN PER ECAM. OPENSDR F3LA2023130100010Actuator · faultedFCLT SLATS FAULT. REMOVED AND REPLACED ACTUATOR 6045CM IAW AMM 27-84-48-400-001-A & AMM 27-84-49-000-001-A. RAN OPS TEST OF SLAT SYSTEM OPS CHECK GOOD T/W F9192.SDR F3LA2023100100008A/C Pack · odorDISCREPANCY: REF LP247487 ITEM #2 - ODOR EVENT THROUGHOUT CABIN AND COCKPIT OILY, ACRID MUSTY SMELL. BURNING EYES / TINGLING, HEADACHE, LIGHT HEADED. ODOR EVENT CHECK LIST ENDED WITH PACK 2 OFF AS ODOR STRONGEST IN AFT CABIN.**CORRECTIVE ACTION: REFERENCE LP24SDR F3LA2023100100007Cabin Air Sys · contaminatedSTRONG ODOR OF DEICE FLUID IN COCKPIT AND CABIN. PERFORMED IDENTIFICATION CAUSE FOR CABIN ODOR IAW TSM 05-50-00-810-831-A SUBTASK 05-50-00-810-085-E, TYPE 8 CAUSED BY DE-ICING FLUID INGESTION. PERFORMED LEVEL A DECONTAMINATION IAW AMM 21-00-00-615-802-A REFSDR F3LA2023050100006Elt · failedAFT FIXED ELT 110MX FAILED OPERATIONAL CHECK AMM 25-65-00-710-001 REF TASK CARD 256535-02-1. REMOVED AND REPLACED FIXED ELT IAW AMM 25-65-35-000-001-A AND 25-65-35-400-001-A. OPS CHECKS GOOD IAW AMM 25-65-00-740-001-A. COMPLIED WITH EA# N2-25R-37366 IN INSTA
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