Airbus A320-232
Service difficulty reports · 32,653
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 = 'A320232' 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 = 'A320232' 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 CALA2024111101091Hydraulic Line · leakingREF LOG PAGE 9748634, ECRA 2011-01000 MUST BE COMPLIED WITH FOR HYD FUILD SPILL IN AFT PIT ACCOMPLISHED ECRA 2011-01000 PART A, IMMEDIATE CLEAN UP OF HYD FUILD SPILL IN THE AFT PIT, REMOVED PIT FLOORBOARD 151LF IAW AMM 53-42-17, CLEANED LOWER FUSELAGE SKIN FROSDR YENA2024111101446A/C Pack · failedFLT#1441, BOS-SRQ. 'CLIMBING THRU FL260, DIRTY SOCK SMELL FROM COCKPIT AIR VENTS. RAN COCKPIT ODOR ISOLATION PROC. PACK 1 TURNED OFF. ODOR DISSIPATED. MX-270 COMPLETED;C/W INFO NOTICE 2017-T015 SECTION A ISOLATED FAULT TO TYPE 10 ODOR WAS A DIRTY SOCK SMELL PESDR YENA2024111101445Fault Message · abnormalFLT#1333, DCA-PBI. 'ON DECENT ON ARRIVAL 5500-4000 DIRTY SOCK ODOR PERFORMED FUMES CHECKLIST ISOLATED PACK # 1; ACCOMPLISHED INFO-NOTICE 2017-T015K IDENTIFIED ODOR SOURCE APU(OIL SATURATION) TYPE 1. PERFORMED LEVEL A ECS DECON PER TSM 05-50-00-81-085-B. PERFORSDR GTIA2024110838512Bottle · low pressureL1 & R2 DOOR ASSIT BOTTLE REQUIRE SERVICE-SERVICE L1 & R2 DOOR ASSIT BOTTLE IAW AMM 52-10-00 TO PROPER LEVELSDR YENA2024111101448Entertain Sys · corrodedFLT#2476,SJU-BDL. ' IFE INOP ( THALES AVANT IFE (ENTIRE SYSTEM) ) - TV 1 A FLICKERED OFF. A SMELL OF ELECTRIAL FIRE WAS OBSERVED BY INFLIGHT . THE WALL AROUND THE TV WAS NOT AS THE WALL INSIDE CLOSET . PULLED CBS IN CEILING IN FWD GALLEY AS WELL AS SDR GTIA2024110838511Power Supply · no testDURING SVC CHK WHILE PERFORM EPSU BITE CHECK. 11WL FAILED.-R+R 11WL EPSU BATTERY IAW AMM 33-51-38-04. BITE CHECK GOOD. A/C OK FOR CONT'D SVC.SDR YENA2024111201470Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 20 LH SIDE FROM HOLE 7 OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH IS 0.135 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00027) REF AE WO 2024-275/1. N/R# 2024 - SDR YENA2024111201469Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 20 RH SIDE FROM HOLE 3 OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I IS 0.045 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00028) REF AE WO 2024-275/1. N/R# 2024 SDR YENA2024111201468Door · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 LH SIDE FROM HOLE 7 OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I S 0.097 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00029) REF AE WO 2024-275/1. N/R# 2024 -SDR YENA2024111201467Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH SIDE FROM HOLE 8 OF JOOGLE AREA LOC ATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I S 0.087 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00031) REF AE WO 2024-275/1. N/R# 2024 SDR YENA2024111201466Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE LOC. ON FR.16 RH DOOR STOP FITTING 7 LOWER I/B HOLE. CRACK DEPTH IS 0.165 INCH APPROX; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00032) REF AE WO 2024-275/1. N/R# 2024 - 538515. REMOVED AND RESDR YENA2024111201465Door Frame · no discrepancyDURING HEAVY MAINTENANCE: (RESOLVED ON W/O: 1318564 TASKCARD: NR-00033) REF AE WO 2024-275/1. N/R# 2024 - 538516. REMOVED AND REPLACED INTERCOSTAL FITTING LOC. ON FR.16 LH DOOR STOP FITTING 7 I.A.W. A320 SRM 53-11-12-300-010 STEP 2.A. FIGURE 001 (SHEET 1) AND SDR YENA2024111201464Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE LOC. ON FR.16 LH DOOR STOP FITTING 7 LOWER I/B HOLE, CRACK DEPTH IS 0.123 INCH APPROX; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00034) REF AE WO 2024-275/1. N/R# 2024 - 538517. REMOVED AND RESDR YENA2024111201463Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH SIDE FROM HOLE A OF JOOGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH IS 0.084 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00035) REF AE WO 2024-275/1. N/R# 2024 - SDR YENA2024111201462String · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L AND BTW FR58 TO FR60 AFT CARGO COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1318564 TASKCARD: NR-00036) REF AE WO 2024-275/1. N/R# 2024 - 538624. PERFORMED PERMANENT REPAIR ON STRINGER 43L AND BTW FR58 TO FR60 SDR YENA2024111201461Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 42L AND BTW FR58 TO FR59 AFT CARGO COMPARTMENT (CPCP FINDING);(RESOLVED ON W/O: 1318564 TASKCARD: NR-00037) REF AE WO 2024-275/1. N/R# 2024 - 538625. PERFORMED PERMANENT REPAIR ON STRINGER 42L AND BTW FR58 TO FR59 ASDR YENA2024111201460Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH SIDE FROM HOLE B OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH IS 0.081 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00039) REF AE WO 2024-275/1. N/R# 2024 - SDR YENA2024111201459Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 16 RH SIDE FROM HOLE D OF JOGGLE AREA LOCATED AT LEVEL OF DOOR STOP FITTING 7 AT FWD GALLEY AREA. CRACK DEPTH I S 0.101 INCH; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00040) N/R# 2024 - 538560. PERFORMED PESDR YENA2024111201458Fastener · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON OPEN FASTENER HOLE LOC. ON FR.20 RH DOOR STOP FITTING 7 UPPER I/B HOLE. CRACK DEPTH IS 0.081 INCH APPROX; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00041) REF AE WO 2024-275/1. N/R# 2024 - 538513. PERFORMED REPASDR YENA2024111201457Stabilizer · wornDURING HEAVY MAINTENANCE: WEAR ON HINGE 6 UPPER SIDE LOWER AREA ON VERTICAL STABILIZER; (RESOLVED ON W/O: 1318564 TASKCARD: NR-00042) REF AE WO 2024-275/1. N/R# 2024 - 538686. REMOVED AND REPLACED HINGE #6 ON VERTICAL STABILIZER IAW A320 SRM 51-42-11, A320 SRMSDR YENA2024111201456Hinge · wornDURING HEAVY MAINTENANCE: CRACK INDICATION ON FASTENER HOLE FR16 RH STOP FITTING 7 UPPER I/B HOLE. CRACK DEPTH IS 0.18; EF AEROMAN W.O. 2024 275/1 NR 538514 * PERFORMED REPAIR ON FR.16 RH DOOR STOP FITTING 7 UPPER I/B HOLE IAW A320 SRM 53-11-12-300-010. THIS RSDR YENA2024111201455Service difficultyDURING HEAVY MAINTENANCE: WEAR ON STRINGER 39R LOCATED BTW FR47 TO FR 48 AFT CARGO COMPARTMENT; REF AERMAN W.O. 2024 275/1 NR 538884 * REMOVED AND REPLACED STRINGER 39R LOCATED ON AFT CARGO COMPARTMENT BWT FR 50 AND FR 51 IAW A320 SRM 51-72-11 AND DWG D5347SDR YENA2024111201454Hinge · wornDURING HEAVY MAINTENANCE: CORROSION STRINGER 31R LOCATED BTW FR64 TO FR65 IN AFT CARGO COMPARTMENT (CPCP FINDING); REF AEROMAN WO 2024 275/1 NR 538820 * REMOVED AND REPLACED STRINGER LOC. FR64 TO FR65 STRG 31RH IAW A320 SRM 51-42-11 AND DWG D53480505, D5348006SDR YENA2024111201453Hinge · wornDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR 35 & STR 30L / PRESSURE BULKHEAD / HOLES #2 & 6 / CRACK DAMAGE – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-9052-24 REV. 0 (COVER + PARTS 1-5) /2/ AIRBUS RDAF 81474600/004/2024#A
/3/ AIRBUS MESSDR YENA2024111201452Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / FR 20 RH / DOUBLE JOGGLE AREA / DOOR STOP FITTING 7 HOLE 6 / CRACK - PERMANENT REPAIR (FRAME REPLACEMENT); REFERENCES: /1/ AEROMAN EA 53-9051-24 REV. 0 (COVER & PART 1 - 2) /2/ AIRBUS SB A320-53-1374 REVSDR YENA2024111201451Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER NODE & CONTINUITY FITTING LH/RH AREAS / CRACKS - PERMANENT REPAIR; REFERENCE: /1/ AEROMAN EA 53-9043-24 COVER REV.0 & PART 1-5 /2/ AIRBUS SB A320-53-1331 (REF. FAA ADSDR CALA2024111202836Stringer · corrodedMAIN CABIN BELOW FLOOR AT FRAME 65 RT STRINGER 25RT HAS EXFOLIAT ED CORROSION. REMOVED AND REPLACED STRINGER 25RT FR 65-66 IAW A320 SRM 51-72-1 1.SDR CALA2024111102813Fitting · crackedCRACK INDICATION AROUND FASTENER AS MARKED AT 2 O''CLOCK POSITION BTW FR 40 AND 41 LH SIDE KEEL BEAM SIDE PANEL BEHIND THE VAPOR SEAL. GENERATED BY V947494 ON HAECO LCQ NR 9290461/36461 REMOVED + REPLACED CRACKED KEEL BEAM FITTING AT L/H FR40-41 IAW A320 SRM 5SDR YENA2024110801442Phone · intermittentFLT#1497, PVD-FLL. 'R2 INTERMITTENTLY DISARMED IN FLIGHT STAYED ARMED FOR REST OF FLIGHT BUT LEARNED THAT FA PUT BANDAIDS ON THE HANDLE; REF TSM: 52-13-00-810-805-A. JUMPED PINS B AND C ON 7WN2-A - INDICATION AVAILABLE. ADJUSTED PROX SWITCH 7WN2 IAW AMM: 52-71SDR AALA202411076544Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED L1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.SDR GTIA2024110838508Megaphone · damagedFOUND AFT MEGAPHONE VOLUME KNOB MISSING-R&R AFT MEGAPHONE IAW NKS DRAWING A320 EMER EQUIP REV. 5SDR YENA2024110801441Bleed Valve · unknownFLT#787, JFK-SXM. "DESCENDING THROUGH 10,000 INFLIGHT CALLED TO INFORM A DIRTY SOCK SMELLIN THE CABIN COMMING FROM ROW 16 TO THE FWD CABIN. CUSTOMERS ALSO NOTIFIED THE ODOR , INFLIGHT DESCROBED THE SMELL AS PERSISTANT AND SAID ODOR REMAINED TILL AFTER BLOCKINGSDR CALA2024110801080None · noneFA EMERGENCY CHECKLIST BEHIND SEAT 3B NEEDS TO BE REPLACED. VERIFIED F/A EMERGENCY CHECKLIST WAS REPLACED IN THE BACK OF SEAT 3B.SDR CALA2024110701062Door · no discrepancyLEFT AFT EMER EXIT DOOR OPENED REINSTALLED LEFT OVERWING AFT EMERGENCY EXIT DOOR IAW AMM 52-21-00 LH AFT OVERWING HATCH INSTALLED INFLATION BOTTLE PIN REMOVED . PETTINATO DENQCSDR CALA2024110701061Bottle · no discrepancyINSTALLED PIN FOR LEFT INFLATION RESERVOIR IN AFT PIT FOR OVERWING EXIT DOOR. REMOVED PIN AND STOWED FOR LEFT INFLATION BOTTLE. OVERWING SLIDE INFLATION BOTTLE LH IN AFT CARGO PIT PIN REMOVED AND STOWED . PETTINATO DENQCSDR CALA2024110701060Seal · leakingF/A REPORTS LOUD SQUEALNOISE FROM LEFT OVERWINGEXIT AREA. PRESSURIZED AIRCRAFT TO 3 PSI AND COULD HEAR AIR LEAKING FROM THE TOP AFT CORNER OF THE AFT LH OVER WING EXIT FROM INSIDE THE AICRAFT AS WELL AS LOUDLY FROM THE OUTSIDE REF AMM 05-53-00-780-001-A01 REQUSDR CALA2024110601054Duct · contaminatedBLEED AIR HAS STRONG BURNING PLASIC ODOUR WITH APU OR ENGINE RUN NING PACKS ITEM LOCKED BY TOMC ITEM UNLOCKED BY TOMC. PERFORMED INSP REF AMM 05-50-00-810-831-A. IN CONJUCTION WITH LOGPAGES 9773868 AND 9773874. FOUND SIGNS ON HYD FLUID ON DUCTS AND BOTH SYSTEMSDR CALA2024110601047Warning Light · false activationDOOR 2L ECAM UPON LANDING. DOOR SHOWED OPEN ON DOORS SYNOPTIC PAGE. DOOR WAS VERIFIIED DOOR 2R INDICATED PER PFR AND LAST LEG RPT. PLACED DOOR 2R ECAM INDICATION ON MEL 5270AV. REQUIRES TO BE CHECKED BEFORE EA. DEPARTURE. .APPROVED PLACED DOOR 2R ECAM INDICATISDR CALA2024110502799Skin · damagedL/H ELEVATOR HAS LIQUID INGRESS DAMAGE 105 INCHES FROM I/B EDGE 5 1/2 INCHES FROM TRAILING EDGE 5 INCHES IN DIAMETER PER HAECO LCQ N/R 9298194/22194 GEN BY V061632 REPAIRED L/H ELEVATOR 105 IN FROM I/B 5.5 IN FROM T/E 5 IN DIA ZONE C IAW A320 SRM 55-21-11-300-SDR CALA2024110502796Skin · contaminatedL/H ELEVATOR HAS LIQUID INGRESS 176IN FROM INBOARD EDGE 5IN FROM TRAILING EDGE 4IN IN DIAMETER PER HAECO LCQ N/R 9298195/22195 GEN BY V061632 DRILLED WITNESS ON L/H ELEVATOR 176 IN FROM I/B 5 IN FROM T/E 1.5 IN DIA ZONE C IAW A320 AMM 55-20-00-200-006-A01 PARASDR YENA2024110501426Apu · odorFLT#1379, DCA-FLL. ' ODOR OF DIRTY SOCKS NOTED BY MULTIPLE CREW DESCENDING BELOW 6,000FT SEEMED TO DISSIPATE WITH PACK 1 OFF, LEVEL 2; C/W INFO NOTICE 2017-T015K . ISOLATED ODOR TO APU. PERFORMED AMM 21-00-00-615-803A. COMPLIED WITH INFORMATION NOTICE 2017-T01SDR CALA2024110601045Control Servo · faultedECAM WHEEL N/W STRG FAUL T IN CRUISE FL340 T/S PER TSM REF. 32-51-00-810-826-A, REMOVED AND REPLACED N/W STEERING SERVO CTL PER AMM REF. 32-51-51-000-001-A, FOUND CONNECTOR CLOCKED DIFFERENT. ADDED ROTABLE PARTS CHANGE INFORMATION. ROTABLE PARTS CHANGE WAS INDSDR YENA2024110501437Crossbeam · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE H1, LOCATED ON CROSSBEAM SPLIC ING AREA FR16 LH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.106 INCHES, CRACK DIRECTION: 11 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1321566 TASKCARD: NR-00013) REF AE SDR YENA2024110501436Crossbeam · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FASTENER HOLE H2, LOCATED ON CROSSBEAM SPLIC ING AREA FR16 LH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.113 INCHES, CRACK DIRECTION: 12 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1321566 TASKCARD: NR-00014) REF AE SDR YENA2024110501435Crossbeam · crackedDURING HEAVY MAINTENANCE: DISCREPANCY DESCRIPTION: CRACK INDICATION FOUND ON FASTENER HOLE H2, LOCATED ON CROSSBEAM SPLIC ING AREA FR16 RH SIDE ON PASSENGER CABIN. CRACK DEPTH = 0.091 INCHES, CRACK DIRECTION: 11 OCLOCK LOOKING FWD; (RESOLVED ON W/O: 1321566 TASDR YENA2024110501434Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR68 RH AT LOWER INB FASTENER HOLE OF DOOR S TOP FITTING Ñ1 AREA. CRACK DIRECTION 5 OCLOCK VIEW LOOKING AFT. CRACK D= 0.170 INCH; (RESOLVED ON W/O: 1321566 TASKCARD: NR-00021) REF AEROMAN NR 2024-521414 WO 20SDR YENA2024110501433Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER POST LOWER NODE / AREA LH/RH CRACKS - PERMANENT REPAIR; REFERENCES: /1/ DOSSIER REFERENCE 81461224 /2/ AEM EA 53-9039-24 (COVER, P1 THROUGH P5) /3/ R53113672 ISSUE C /4/ R531134SDR YENA2024110501432Skin · damagedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT / STR 30LH / FASTENER HOLES / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-9040-24 REV. 0 (COVER + PARTS 1-4) /2/ AIRBUS RDAF 81463325/004/2024 ISSSDR YENA2024110501429Girt Bar · out of adjustFLT#2080, FLL-DCA. 'R2 DOOR ARMED INDICATION INTERMITTENT DURING FLIGHT ON DOOR PAGE AS WELL AS ON FLIGHT ATTENDANT PANEL ( SLIDE INDICATIONS ON ECAM - PAX DOOR NOT ARMED ); CLEANED AND ADJUSTE R2 DOOR SLIDE GIRT BAR REF. AMM 25-62-44. OPS CHECK GOOD, NO FAULSDR CALA2024110400984Contactor · failedFCDC 1 COCKPIT INDICATIONS. FOUND MULTIPLE MSGS ON ARRIVAL. TOP LEVEL MSG "ELEC DC ESS BUS SHED" WARNING REF TSM 24-60-00-810-801-A. FOUND CB 1PH POPPED. REF ASM 24-62-01 CB 1PH IS INLINE AND POWERS 8PH DC SHED ESS CONTACTOR. REPLACED 8PH REF AMM 24-62-55-401
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