N216FR, cancelled Dec 27, 2023

Service difficulty reports · 29

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 = 'N216FR' AND deregistration_id = 'N216FR-2023-12-27'
  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.

SDR F3LA2023081500129Floorbeam · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. FLOORBEAM-Y969 AT FR66-68 CORRODED. REMOVED AND REPLACED WITH NEW FLOORBEAM FROM FR64-70 P/N D5347219320400 AND P/N D5347209001500 IAW A320 SRM 51-44-11, 53-41-14-283-009, 51-72-11-911-001, 51-42-11Jul 21, 2023 · N216FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2023081500127Plate · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0606 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. RH SHEAR PLATE FR70 CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED RH SHEAR PLATE FR70 PER A320 SRM 51-72-11 MX ACTION IS ACCEPTABLE. /END/Jul 21, 2023 · N216FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2023081500128Floorbeam · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0607 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. FLOORBEAM Y1292 AT FR68 CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM-Y1292 @FR68 PER A320 SRM 51-42-11. MX ACTION IS ACCEPTABLE. /END/Jul 21, 2023 · N216FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2023081100123Door Sill · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0611 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. R2 DOR SILL FWD ARES CORRODED 3 PLCS CORRECTIVE ACTION: REMOVED AND REPLACED WITH NEW R2 DOOR SILL P/N D5348004320701 IAW A320 SRM 53-41-14-300-00Jul 21, 2023 · N216FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2023081100122Plate · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0604 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. LH SHEAR PLATE FR70 CORRODED CORRECTIVE ACTION: AFT FUSELAGE MAIN CABIN L/H SHEAR PLATE AT FR 70 REMOVED AND REPLACED IAW A320 SRM 51-42-11; APPLJul 21, 2023 · N216FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2023081000121Floorbeam · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0610 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. FLOORBEAM Y512.5 AT FR64-FR68 CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM Y512.5 AT FR64-FR70 PER A320 SRM 51-42-11.MX ACTION IS AJul 21, 2023 · N216FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2023081000120Floorbeam · corrodedREFERENCE AIRBORNE/PEMCO N/R 13876.0609 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. FLOORBEAM Y765 AT FR66-FR68 CORRODED. REMOVED AND REPLACED FLOORBEAM Y765 AT FR64-FR70 PER A320 SRM 51-42-11. MX ACTION IS ACCEPTABLE. /END/Jul 21, 2023 · N216FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2023081000119Fitting · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0556 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. R1 DOOR SCUFF PLATE TRIM CORRODED CORRECTIVE ACTION: EVALUATED REMOVED AND REPLACED R1 DOOR SCUFF PLATE FITTING IAW A320 SRM 51-42-11, 51-44-11, 5Jul 21, 2023 · N216FR · Airbus A320214 · Fuselage Main, Attach FittingsSDR F3LA2023081000118Door Sill · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. L2 DOOR SILL OUTER TRIM CORRODED. EVALUATED REMOVED AND REPLACED L2 CENTER SHAPE FITTING IAW A320 SRM51-72-11. MX ACTION IS ACCEPTABLE.Jul 21, 2023 · N216FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2023080900115Fitting · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13876.0555. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. L1 DOOR SCUFF PLATE TRIM CORRODED CORRECTIVE ACTION: REMOVED AND REPLACED L1 DOOR SCUFF PLATE FITTING IAW A320 SRM 51-11-00, 51-72-11, 51-42-11. Jul 21, 2023 · N216FR · Airbus A320214 · Standard Practices/StructuresSDR F3LA2022071200071Apu · leakingDISCREPANCY: REFERENCE LP279524 #1 WHEN APU BLEED WAS USED FOR PACK 1&2 DIRTY SOCK SMELL WAS NOTED THROUGHTOUT WHOLE AC. CORRECTIVE ACTION: PERFORMED INSPECTION OF CABIN ODOR REF 05-50-810-085-A ISOLATED ODOR TO APU INSPECTED APU PER AMM 49-00-00-200-811-A PJul 10, 2022 · N216FR · Airbus A320214 · APU Bleed Air SystemSDR F3LA2022061300057Apu · odorDISCREPANCY: REFERENCE LP228413 DIRTY SOCK SMELL DECENDING THROUGH 10000 FEET FOR SJU FORWARD AND AFT F/A REPORT SMELL AND LIGHT HEADEDNESS EVENT LASTED APPROXIMATLY 5 MINUTES F/O REPORTS OIL NEAR PACK 2 INLET ON POST FLIGHT CABIN SMELL VERIFIED BY CAPT AND F/Jun 11, 2022 · N216FR · Airbus A320214 · Cabin Temperature Control SystemSDR F3LA2022032800011None · noneDISCREPANCY: REFERENCE LP1276686 ITEM: DIRTY SOCK ODOR IN FLIGHT DECK AT 5000 FEET ON DESCENT BURNT RUBBER ODOR IN AFT GALLEY AT 3000 FEET CORRECTIVE ACTION REFERENCE LP1276686 ISOLATED PROBLEM TO PACKS. PERFORMED PACK BURNOUT PROCEDURE IAW AMM 21-00-00-615-8Mar 15, 2022 · N216FR · Airbus A320214 · Cabin Cooling SystemSDR F3LA202007130030Oil System · overservicedONCOMING CREW REPORTED TO MX THERE WAS A SMELLY SOCK ODOR WHEN THEY TURNED ON APU BLEED. MX TROUBLESHOT AND FOUND THE APU TO BE OVERSERVICED. MX RAN BLEEDS TO BURN OUT PACKS AND BLEED LINES NO ODOR REMAINED. PERFORMED TSM FOR ODOR EVENT, FOUND APU OVER SERJul 11, 2020 · N216FR · Airbus A320214 · APU Oil SystemSDR F3LA2018102200458A/C Pack · odorDISCREPANCY: REFERENCE LP1133373 ITEM 2 AND 3, ODOR EVENT INFLIGHT INITIALLY NOTICED AT 9000 FT IN CLIMB. RAN QRH PROC AND ISOLATED WITH NR 2 PACK OFF. AFTER SPEAKING WITH AFT FLIGHT ATTENDANT ODOR DISSIPATED. LEFT NR 2 PACK OFF. AT TOP OF DESCENT THE FLIGHT AOct 19, 2018 · N216FR · Airbus A320214 · Cabin Cooling SystemSDR F3LA2018100200449Proximity Switch · defectiveDISCREPANCY: REFERENCE LP 1160067-3, DOOR 4R WILL NOT STAYED ARMED INFLIGHT. BOTH DOORS PAGE LOWER ECAM AND FAP SHOWED DOOR 4R DISARMED INFLIGHT. CORRECTIVE ACTION: REF N/R 2129N1, REMOVED AND REPLACED 4R DOOR PROXIMITY SWITCH PAX IAW AMM 52-71-11-000-001, 52-Sep 29, 2018 · N216FR · Airbus A320214 · Door Warning SystemSDR F3LA2018100100447Unknown · odorDISCREPANCY: REFERENCE LP1160063-1, DISCREPANCY STRONG DIRTY SOCKS SMELL IN THE COCKPIT AND AFT GALLEY ON APPROACH DURING LEVEL OFF AND ENGINE SPOOL. FA'S SMELLED ODOR FROM THE AFT GALLEY TO THE EMERGENCY EXITS OVER THE WINGS. NO ODOR IN THE FWD GALLEY. CORRESep 26, 2018 · N216FR · Airbus A320214 · Air Distribution SystemSDR F3LA2018092700446Unknown · odorODOR EVENT DURING BASE TURN TO LAND. CABIN AND COCKPIT CREW NOTICED A BURNING WAX SMELL. SMELL DISSIPATED AFTER LANDING. NO PACKS WERE TURNED OFF. PER EA A0-21T-34386 TSM TASK 05-50-00-810-831-A, PLACED ON TDI 1142918 DUE:60 FLT CYCLES. AC WAS RELEASED FOR SERSep 25, 2018 · N216FR · Airbus A320214 · Air Distribution SystemSDR F3LA2018082000392Unknown · odorDIRTY SOCK ODOR DETECTED BY THE FLIGHT CREW AND FLIGHT ATTENDANTS. ORIGINATED IN AFT CABIN. THE ACFT WAS AT FL360. NO POWER CHANGE WAS MADE. PACK 2 WAS TURNED OFF AND THE ODOR DISAPATED, SUSPECT PACK 2 CONTAMINATION. AT TOP OF DESCENT, POWER REDUCTION, THAug 18, 2018 · N216FR · Airbus A320214 · Air Distribution SystemSDR F3LA2018081400387Apu · odorDIRTY SOCK OR BURNING OIL ODOR NOTICED BY ALL CREW MEMEBERS WHEN BOARDING THE ACFT. ODOR NOTICED IN COCKPIT AND ENTIRE CABIN. BLEED CONFIGURATION, APU BLEED ON, NR 2 PACK ON, NR 1 PACK OFF. PERFORMED TSM 05-50-00-810-831-A. CAUSE INDICATED TO BE APU AND PAug 11, 2018 · N216FR · Airbus A320214 · Airborne Auxiliary Power Unit (APU) SystemSDR F3LA2018040300307Diaphragm · damagedFWD SERVICE DOOR ASSIST BOTTLE WILL NOT HOLD PRESSURE. REMOVED AND REPLACED THE ASSIST BOOTLE DIAPHRAGM. OPS TESTED GOOD. R1 DOOR SERVICED TO 1700 PSI IAW AMM 52-10-00-420-061A, AND 52-10-00, PB 301, CONF 00. AIRCRAFT OK TO CONTINUE.Apr 2, 2018 · N216FR · Airbus A320214 · Passenger/Crew DoorsSDR F3LA2018021600287Starter · arcedECB FAULT ACTIVATED. REMOVED AND REPLACED ECB IAW AMM-49-61-34-000-003-A. FAULT CLEAR, APU START MOTOR REMAINS FAULTED. REMOVED AND REPLACED APU STARTER ASSY 8KA IAW AMM 49-42-51 AND REPLACED MONITORING WIRE RING TERMINAL. REMOVED AND REPLACED POSITIVE Feb 14, 2018 · N216FR · Airbus A320214 · APU Start/Ignition SystemSDR F3LA2017092100228Tube · leakingREPORTS OF AN ODOR IN THE COCKPIT AND CABIN BY THE FLIGHT CREW. FOUND HEAVY OIL LEACKAGE AND POOLING IN THE APU COMPARTMENT. LEAK SOURCE FOUND TO BE APU OIL COOLER FEED AND RETURN LINES. REMOVED AND REPLACED FEED AND RETURN LINES IAW AMM 20-21-11-991, AND Sep 14, 2017 · N216FR · Airbus A320214 · APU Oil SystemSDR F3LA2017092100227Tube · bentDISCREPANCY: REFERENCE LOG PAGES 9044632, 9044633 AND PEMCO NR 1781N1 REPETITIVE REPORTS OF ODOR IN THE COCKPIT AND CABIN BY THE FLIGHT CREW. FOUND HEAVY OIL LEACKAGE AND POOLING IN THE APU COMPARTMENT. LEAK SOURCE FOUND TO BE APU OIL COOLER FEED AND RETURN LSep 14, 2017 · N216FR · Airbus A320214 · APU Oil SystemSDR F3LA2017091400224Line · leakingODOR IN CABIN. FOUND OIL SUPPLY LINE LEAKING. REMOVED AND REPLACED THE O-RING AND SECURED IAW AMM 49-99-44-400-802-A. PERFORMED OPERATIONAL CHECK FLIGHT. NO ODOR NOTED.Sep 12, 2017 · N216FR · Airbus A320214 · APU Oil SystemSDR F3LA2017032200092Door Sill · corrodedR2 DOOR SILL CORRODED AT NUTPLATE HOLES. FOUND THE R2 DOOR SILL NUT PLATE HOLES EXCEEDED ALLOWABLE LIMITS IAW SRM 53-41-14-283-002. REPAIRED THE AREA IAW SRM 51-41-14-300-001, REPAIR 5. RESTORED SURFACE PROTECTION IAW SRM 51-75-12 AND 51-23-12.Mar 16, 2017 · N216FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2012040600731Bulkhead · damagedFUSELAGE FWD BULKHEAD RT SIDE HAS DAMAGED.Apr 3, 2012 · N216FR · Airbus A320214 · Fuselage Main, BulkheadSDR F3LA2012040600730Skin · damagedRIGHT SKIN PANEL FROM FRAME 1 TO FRAME 12, RT WINDSHIELD LOWER SECTION TO RT SIDE STRINGER, DAMAGED .Apr 3, 2012 · N216FR · Airbus A320214 · Fuselage Main, Plate/SkinSDR F3LA2012040600729Skin · damagedRIGHT SKIN PANEL FROM FRAME 1 TO FRAME 24, STRINGER 29 TO STRINGER 37 RT, DAMAGED.Apr 3, 2012 · N216FR · Airbus A320214 · Fuselage Main, Plate/Skin
Back to N216FR, cancelled Dec 27, 2023