Airbus A321-211
Service difficulty reports · 12,327
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 = 'A321211' 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 = 'A321211' 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 DALA2022021500992None · noneFLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM AT 20ABC INOP. RE-SECURED CONNECTOR AT SEAT 20ABC. REF A321 AMM 33-52. OPS CK GOOD. (LP# 6172872)SDR DALA2022021500991None · noneEVALUATE AFT EXTERIOR SKIN DAMAGE. DURING SV IN BHM PERFORMED WORK ON NRC #5 COMPLIED WITH PRI 596293-14 REV O-6 (767121) QC 5209 PRI 596293-14 REV O-6 MATCHES ERA 596293-14 REV O (767121) QC 5209 COMPLIED WITH ERA 596293-14 REV O (767121) QC 5209. (LP# 212066SDR DALA2022021500990None · noneSKIN DAMAGED BELOW C3 CARGO DOOR. DURING SV IN BHM PERFORMED WORK ON NRC # 31 COMPLIED WITH PRI 596659-14 REV O-2 (767121) QC 5209 PRI 596659-14 REV O-2 MATCHES ERA 596659-14 REV O (767121) QC 5209 COMPLIED WITH ERA 596659-14 REV O (767121) QC 5209. (LP# 21206SDR DALA2022021500989None · noneSTRINGER 42RH BETWEEN FRAME 60 AND 61 IS BENT. DURING SV IN BHM PERFORMED WORK ON NRC #9 AND #29 COMPLIED WITH PRI 596416-14 REV O-2 (767121) QC 5209 PRI 596416-14 REV O-2 MATCHES ERA 596416-14 REV O (767121) QC 5209 COMPLIED WITH ERA 596416-14 REV O (767121) SDR DALA2022021500988None · noneSTRINGER 42LH BENT BETWEEN FRAME 58 AND 59. DURING SV IN BHM PERFORMED WORK ON NRC #9 AND #29 .COMPLIED WITH PRI 596416-14 REV O-2 (767121) QC 5209.PRI 596416-14 REV O- MATCHES ERA 596416-14 REV O (767121) QC 5209.COMPLIED WITH ERA 596416-14 REV O (767121) QC SDR DALA2022021500986None · noneREF: N/R 138 - RIGHT SIDE REAR FUSELAGE EXTERNAL SKIN SCRATCHED AT FR52 + 3 INCHES , AT STR 40R. COMPLIED WITH ALL STEPS ON PRI 597290-14 REV. "O" DATED 11 FEB. 2022 23:30E INSURED ALL PRI REVISION STEPS MATCHED WITH FINALE ERA INSTRUCTIONS 597290-14 REV. ORIGSDR DALA2022022301198None · noneFOUND ROW 34 CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED EPSU 12WL PER A320/321 AMM 33-51. (LP# 8482118)SDR AALA202202141679Unknown · fumesAIRCRAFT WAS GROUNDED: OIL FUMES IN CABIN DURING CLIMB. FLIGHT DECLARED AN EMERGENCY AND RETURNED TO DFW, LANDING SAFELY. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)SDR DALA2022022401221None · none***DTE*** A321 / FUSELAGE / DENT AND GOUGES/ PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM REPAIR ACCOMPLISHMENT. LOG-PAGE UPDATED @ 09FEB22 1502 UTC 02 DFRD BY GRAY 00495354 BHM 09FEB22 RII: N ENTR 00495354 W REPAIR APPROVAL IS LIMITED TO 6 MOSDR DALA2022022401220None · none***DTE*** A321 / FUSELAGE / FR61-FR62 / STR 40R -STR 41R / DENT / PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM REPAIR ACCOMPLISHMENT. LOG-PAGE UPDATED @ 09FEB22 1425 UTC 02 DFRD BY GRAY 00495354 BHM 09FEB22 RII: N ENTR 00495354 W REPAIR APPROVSDR DALA2022022401219None · none***DTE*** A321 / FUSELAGE / FR 58 - 61 / STR 42R, 43R, & 42L / DEFORMED. REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM REPAIR ACCOMPLISHMENT. REPAIR APPROVAL IS LIMITED TO 6 MONTHS AFTER SECTION I (FEB. 9, 2022). ADDITIONAL ENGINEERING AUTHORIZATION (ER/A) REVISSDR DALA2022021500987None · noneR-4 DOOR SLIDE REQUIRES REPLACEMENT. REMOVED AND INSTALLED R-4 DOOR SLIDE IAW A321 AMM 25-62-4-000- 804-A AND A321 AMM 25-62-44-400-803-A. W SEQUIERA 1948861U 08 FEB 22 SLIDE, RAFT-SLI OFF 30-2561-9-0002 18101 ON 30-2561-9-0002. (LP# 2115916)SDR DALA2022020900864None · noneWHEN L1 DOOR IS LOCKED AND CLOSED CB P10 & P11 TRIP. TROUBLE SHOT, FOUND DAMAGED L1 DOOR 'ARM SLIDE' LIGHT HARNESS . REPLACED L1 DOOR 'ARM SLIDE' LIGHT / HARNESS ASSEMBLY. OPS CHECK GOOD PER A321 AMM 52-73-21-000-001-A AND 52-73-21-400-001-A. CIRCUIT BREAKS P1SDR DALA2022020900863None · noneFOUND DURING SERVICE CHECK SEAT ROW 20C FLOOR EMERG LIGHT INOP. FOUND 20C FLOOR EMER LIGHT CONNECTOR LOOSE. RECONNECTEDZ SAME OPS CHK NML IN REF W/ A321 AMM 33-50. MCO AND PLAC REMOVED. A/C OKAY FOR SVC. (LP# 8344874)SDR DALA2022020400733None · noneUPON LANDING RECIEVED AVIONICS SMOKE MESSAGE CLEARED RUNWAY AND COMPLETED ECAM AND QRH NO PERCEPIBLE SMOKE ARFF WAS CALLED AND THEY REPORTED NO SMOKE FROM EXTERIOR OF PLANE. CREW REPORTED AVIONICS MESSAGE WITH NO SMOKE INSPECTED AVIONICS BAYS FOR EVIDENCE OF SSDR DALA2022020400732None · noneDTE - REPAIR APPROVAL IS LIMITED TO 6 MONTHS SERVICE FROM DATE OF APPROVAL ONLY (BY 20JUN2022). ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEER: DAMAGE TOLERANCE EVALUATION IS REQUIRED SDR AALA202202033293Slide · noneAIRCRAFT IN BASE MAINTENANCE: AFT LEFT PASSENGER DOOR SLIDE FAILS EMERGENCY POWER SUPPLY UNITS BITE TEST. REPLACED SLIDE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-62-44-000-002-A AND AMM 33-51-00-710-001A.SDR DALA2022020200694None · noneSUPPLEMENTAL INFORMATION' SHIP 3014 - ATO - AT 100KTS DUE TO A FALSE PREDICTIVE WINDSHEAR ALERT. WARNINGS CONTINUED AFTER CLEARING RUNWAY. AIRCRAFT CMS DID NOT LOG ANY FAULTS. CORRECTIVE ACTION: DEFERRED PREDICTIVE WINDSHEAR WARNING SYSTEM PER MEL. AIRCRAFT RTSDR AALA202202024827Slide · faultyAIRCRAFT IN BASE MAINTENANCE: AFT LEFT PASSENGER DOOR SLIDE EMERGENCY POWER SUPPLY UNIT FAILS BITE TEST. REPLACED SLIDE PER AMM 25-62-44. ACCOMPLISHED SATISFACTORY BITE TEST PER AMM 33-51-00-710-001A.SDR F3LA2022012600100Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R #11998.0367 FR66-FR-70-Y765 LONGITUDINAL BEAM CORRODED ON UPPER SURFACE OF BEAM CAP. CORRECTIVE ACTION: EVALUATED & REPLACED WET AREA FLOOR BEAM Y765 FR66-FR70 IAW A321 SRM 53-00-14-283-002, 51-44-11 & 51-72-11-911-001SDR F3LA2022012600099Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R 11998.0366 LONGITUDINAL BEAM FROM FS 65-FS 66-Y919 CORRODED AROUND AFT MOUNTING LUG HOLE. CORRECTIVE ACTION: EVALUATED & REMOVED AND REPLACED LONGITUDIONAL BEAM FROM FR65-66-Y919 IAW A321 SRM 53-00-14-283-002 & SRM 51-72-11-911SDR F3LA2022012600098Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R# 11998.0363 FR66-FR70 Y65 LONGITUDINAL BEAM CORRODED ON UPPER SURFACE OF BEAM CAP. CORRECTIVE ACTION: EVALUATED & REPLACED WET AREA FLOORBEAM Y765 FR66 TO FR70 IAW A321 SRM 53-00-14-283-002, 51-44-11 & 51-72-11-911-001SDR F3LA2022011700101Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO N/R #11998.0298 FWD WET AREA: FLOORBEAM Y-254 MAIN BEAM CORRODED BETWEEN FR12-FR16. CORRECTIVE ACTION:REPAIRED Y-254 FLOOR BEAM AT FR16 IAW A321 SRM 53-11-14-300-001 PER DOSSIER REF 81021673SDR F3LA2022011700097Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO NR#11998.0300 FWD WET AREA: FLOORBEAM Y-254 MAIN BEAM CORRODED BETWEEN FR12-FR16 CORRECTIVE ACTION:REMOVED CORROSION AREA, AFTER EVALUATION FOUND TO BE OUT OF LIMITS OF CLIP-NUT AROUND IAW A 321 SRM 53-11-14-283-007. REMOVED AND RESDR F3LA2022011700096Floorbeam · corrodedDISCREPANCY: REFERENCE PEMCO NR#11998.0297 FWD WET AREA: FLOORBEAM Y-1292 MAIN BEAM CORRODED BETWEEN FR12-FR18
CORRECTIVE ACTION: EVALUATED AND REPAIRED FWD WET AREA FLOOR BEAM Y-1292 BETWEEN FR-12 AND FR-18 IAW A321 SRM 53-11-15-300-005 PER AIRBUS DOSSIER#81SDR DALA2022020200692None · noneR1 DOOR HAS DENT ON LOWER AFT CORNER IN GRAY BAND. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 008-0010:1222-6066/001 00005 COMPLETED R1 EXTERNAL DOOR SKIN REPAIR PER A321 SRM 52-10 -00-300-003. REQUIRES INSPECTION COMPLETE. SUMMARY SEE NR FOR ADDITIONAL INFORMASDR DALA2022020200693None · noneWHILE PERFORMING L-1 DOOR WARNING CHECK FOUND DOOR ASSIST ACTUATOR BOTTLE PRESSURE LOW. REF NRWC 00022. (LOG CREATED FOR PARTS TRACKING). REMOVED AND REPLACED L1, DOOR ASSIST ACTUATOR IAW A321 AMM 52-22 -14-00-000-001-A, AND 52-22-14-400-001-A. 2125795. TOOL USDR AALA202201311674Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: L1 DOOR ASSIST BOTTLE FOUND WITH LOW PRESSURE. AND WOULD NOT HOLD PRESSURE. REPLACED DOOR ASSIST BOTTLE PER AMM 52-11-14-400-001-B.SDR AALA202201286827Slide · out of positionAIRCRAFT WAS GROUNDED: LOUD SQUEAL COMING FROM LOWER GALLEY DOOR 1R. RE-POSITIONED R1 DOOR SLIDE FLAP, NO OTHER DISCREPANCIES NOTED. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-11-18.SDR DALA2022030101315None · noneDENT FOUND LH SIDE OF FUSELAGE AFT OF L1 DOOR. DENT IS BETWEEN FR 23&24 LH SIDE 32" BELOW FIRST CLEAR WINDOW. DENT IS 3" TALL, 1" WIDE, .059 DEEP. ALLOWABLE DAMAGE PER SRM 53 -00-11-283-005 FIG 2. REPAIR CATEGORY C REPAIR WITHIN 200 FLIGHT CYCLES FROM FLIGHT 1SDR DALA2022030401423None · noneERA 595953-14 REV ORIG AND REV A ISSUED FOR REPAIR AND ONE TIME INSPECTION OF GROUND DAMAGE AT S34R-S35R, FRAME 62. ERA REVISED TO REV 'B' WITH STAGE II DTE COMPLETE. FOLLOW ON ACTION REQUIRED. CCOMPLISH SECTION III PRIOR TO 65,600 FLIGHT CYCLES OR 131,300 FLISDR DALA2022012600547Unknown · odorON FINAL APPROCH FLIGHT ATTENDANT REPORT SMOKE SMELL IN AFT GALLEY NO SMOKE OR FUMES PERCEPTIBLE IN COCKPIT. AFTER LANDINGDS , FLIGHT ATTENDANT DESCRIBED SMELL AS ELECTRICAL IN NATURE. INSPECTED CABIN NO EVIDENCE SMOKE SMELL FOUND, ALSO FOUND LIGHTS IN 20 ROW SDR DALA2022012600546None · noneWHILE WORKING SVC CHK FOUND EMER EXIT LIGHTS @ ROWS 15,19 +23 ABC SIDE INOP. TROUBLE SHOOT PER A321 TSM 33-51-00 FOUND FAULT 11WL. REMOVED AND REPLACED EPSU PER A321 AMM 33-51. OPS CHECK GOOD. MEL AND PLACARD REMOVED. (M) PROCEDURES REVERSED. (L/P# 8182004)SDR F3LA2022011700089None · noneREFERENCE LOG PAGE LP 206435 ITEM 2, IN FLIGHT ENG 1 STALL ECAM WITH VIBRATIONS, OIL PRESSURE XX, LOUD NOISE ASSOCIATED WITH THE STALL. ALTITUDE WAS 25,000. - AIRCRAFT IS GROUNDED.
CORRECTIVE ACTION: REMOVED AND REPLACED #1 ENGINE ASSEMBLY REF MP71042-01, MP7SDR DALA2022012000405Fcu · leakingAFTER STARTING APU & BLEED NOTICED A STRONG DEICE SMELL ON FLT DECK. AFTER 30-40 MINUTES STRONG SMELL STILL PRESENT. BEGAN WORKCARD 0550-2002 AND FOUND LEAKING FUEL CONTROL UNIT ON APU AND EVIDENCE OF DE-ICE FLUID IN APU. (555681). REMOVED & REPLACED APU FUEL SDR AALA202201143922Damper · inoperativeAIRCRAFT WAS NOT GROUNDED: CENTRALIZED INTERCOMMUNICATION DATA SYSTEM CAUTION LIGHT ILLUMINATED AT TOP OF DECENT. SERVICED 2L DOOR EMERGENCY EXIT DAMPER PER JOB CARD 26L80052003.SDR DALA2022011100228None · nonePERMANENT REPAIR INSTRUCTIONS : GROUND DAMAGE LEFT FUSELAGE / FR30-32 STR26L - STR27L ( REFERENCE ERA 596397-14 REV. ORIG ). COMPLIED WITH SKIN REPAIR ERA 596427-14 REV. ORIG ON NR 00001 ASSOCIATED ER/A 14-596427 ADDED FOR AC 3062. (LP# 2080234)SDR DALA2022011300275None · noneDTE LOGPAGE FOR ERA 596427-14. DTE LOGPAGE FOR ERA 596427-14. ?REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM DATE OF APPROVAL ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTE TO ENGINEESDR DALA2022010700135None · noneEMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:607 / ACARS TEXT: FRC256001607 EMERGENCY EXIT SIGN INOP AND COVER IS BROKEN. EMER. EXIT LIGHT - OPS CHECK GOOD. EMER EXIT LENS MISSING. REPLACED LENS AT LOCATION 607. OK FOR SERVICE REF A321 AMM 33-51. (LP#2077823)SDR DALA2022010700134None · noneFOUND DAMAGE ON RT FWD NOSE FUSELAGE UNDER FO WINDOW. REMOVAL OF SIDE STICK ASSEMBLY IAW A321 27-92-41-000-001-A. A/W REMOVAL UP TO STEP D. (3) (GS 812718). REMOVAL OG THE OXYGEN MASK STOWAGE BOX IAW A321 AMM 35-12-41-000-001-A C/W REMOVAL UP TO STEP D. OPENINSDR AALA202201050044Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN AFT DRY AREA FLOOR PANEL #251 YF DELAMINATED. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-013.SDR AALA202201046387Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FORWARD CABIN FLOOR SUPPORT AT FR 21 AND Y254. REPLACED FLOOR SUPPORT PER SRM 51-42-11.SDR AALA202201033702Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: RECEIVED NEW FORWARD SLIDE AND FOUND SLIDE PRESSURE BOTTLE LOW (R1). **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)SDR DALA2021122808115Smoke Detector · faultedDURING CRUISE FLIGHT VENT BLOWER FAULT AND VENT EXTRACT FAULT FAINT SMELL OF ELECTRICAL SMOKE. T/S PER A321 TSM 21-26-00-810-849-A. ECAM REPORTED VENT AVNCS SYS FAULT, VENT BLOWER FAULT, VENT EXTRACT FAULT, AND AVIONICS SMOKE. CLASS 3 FAULT 26-15-15 SMOKE DETESDR DALA2021122808113None · noneER/A 595953-14 SECTION I WAS ISSUED FOR FUSELAGE SKIN DAMAGE AT THE AFT FRAME OF THE BULK CARGO DOOR OPENING. SECTION I WAS ACCOMPLISHED DURING SPECIAL VISIT IN MSP 10DEC21 ON N/R 8. FOLLOW ON ACTION IS REQUIRED. ACCOMPLISH SECTION II PERMANENT REPAIR WITHIN 2SDR DALA2021122808114None · noneGRN EMERGENCY LIGHT 2R INOP. MVD CEILING PNL AT 2R DOOR FOR ACCESS TO EPSU 14WL. EPSU NOT RESPONSIVE' CIDS EPSU SYS TEST FAULTED 14WL. BATT PRVS RPLD 12/15. RPLD EPSU REAND BATT PACK REF A319/20 MM 33-51. BITRE AND OP TEST GOOD. POWER SUPPLY, E OFF 33-3351-9-0SDR DALA2021122808112None · noneDURING HIDDEN DAMAGE INSPECTION OF NLG JACK CONTACT. FOUND FRAME TO BE DAMAGED APPROXIMATELY 9" O/B OF THE CENTER LINE ON R /H SIDE OF A/C. REMOVED AND REPLACED DAMAGED FRAME WITH SERVICEABLE PN# D5311341120003 @ FR 8, LOWER FRAME SECTION PER ER/A 595840-14. SSDR DALA2021122808111None · noneWHILE JACKING A/C FOR NOSE STRUT SERVICING, JACK FAILED AND DAMAGED SKIN @ FR 8, 10.5" R/H OF CENTER LINE NEAR EXTERNAL POWER RECEPTACLE. REPAIRED DAMAGED SKIN @ FR 8, 10.5" R/H OF CENTERLINE NEAR EXTERNAL POWER RECEPTACLE PER ERA 595840-14. REPAIR APPROVAL ISSDR AALA202201042692Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: FORWARD FLOOR SUPPORT RAIL HAS CRACKED FLOOR PANEL ATTACH HOLE, AT FR 21 AND Y254. **SUPPLEMENTAL REPORT FOR AALA202112222692: REPLACED FLOOR SUPPORT PER SRM 51-42-11.** (CLOSED)SDR AALA202112222692Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: FORWARD FLOOR SUPPORT RAIL HAS CRACKED FLOOR PANEL ATTACH HOLE, AT FR 21 AND Y254. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
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