N353NB
Service difficulty reports · 157
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 = 'N353NB' 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 = 'N353NB' 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 DALA2026101005578Engine · bird ingestionON T/O ROLL POSSIBLE BIRD INGESTION ON RT ENGINE. HIGH VIBRATION MESSAGE ON ROTATION & CLIMB. N1 AS HIGH AS 9.0 IN CRUISE N1 VIB AROUND 5.2. PERFORM BIRD STRIKE INSPECTION IAW AMM 72-00-00-200-001-001-A. FOUND NR 2 ENGINE WITH FAN BLADE DAMAGE. INSTALLED PESDR DALA2026091705194Structure · damagedDURING GVI OF FR68 LH AFT PASSENGER DOOR INNER CAP AND FLANGE, A REPAIR PART WAS IDENTIFIED. PER ER/A 605954-14AD REV A, SRM 53- 41-12-300-011 WAS ACCOMPLISHED WITHOUT DEVIATION. DUE TO LOCATION OF GUSSET ON TOP OF REPAIR PART FLANGE, UNABLE TO PERFO COMPLETEDSDR DALA2026061503564Computer · faultedBOTH ENGINES RUNNING, REJECTED TAKEOFF DUE TO ELAC 1 PITCH FAULT MESSAGE AT 10 KNOTS. DUE TO HISTORY - APPLING ELAC 1 TO MEL & PLAC PER A319/320/321 MEL 27-93-01. M PROC C/W, MCC NOTIFIED. (LP: 8778668, AIRCRAFT WAS GROUNDED)SDR DALA2026050102766Computer · faultedATO - AT APPROXIMATELY 10KTS DUE TO F/CTL ELAC 1 PITCH FAULT. ELAC 1 PLACED ON MEL AND CONTINUED. LATER REPLACED ELAC 1. (LP 8038066 - AIRCRAFT WAS GROUNDED)SDR DALA2026030401478Fan · faultedVENT AVIONICS SYS FAULT DISPLAYED. WARM ELECTRICAL ODOR IS PRESENT. R & R AEVC IAW AMM 21-26. STILL REQ OPS CHK. OPS TEST OF AEVC FAULTED 21-26-51 EXTRACT FAN 18HQ AND 21-26-55 ISOLATION VALVE 24HQ. R & R EXTRACT FAN 18HQ IAW AMM 21-26. AEVC TESTED GOOD,SDR DALA2025111208292Skin · damagedELONGATED HOLE FUEL TANK CUT OUT LOWER SURFACE LOC. BTW RIB17/18 (1E/A ) ON RT WING. PERFORMED PERMANENT REPAIR ON FUEL TANK CUT OUT LOWER SURFACE AS PER A319 SRM 57-21 -11-300-002. (1299055).SDR DALA2025111208290Elec Connector · brokenBROKEN ELECTRICAL CONNECTOR (31CE10A) LOC. ON SPOILER ACTUATOR 5 RH WING. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR (31CE10A) LOC. ON SPOILER ACTUATOR #5 RH WING AS PER AIRBUS ESPM 20-44-11. (1299225).SDR DALA2025111208284Frame · crackedCRACK FOUND ON THE HORIZONTAL FLEANGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1299202).SDR DALA2025111208283Skin · dentedDENTS ON EXISTING REPAIR EXTERNAL SKIN LOCATED BTW FR 62 TO FR 64 AND BTW STR 36R TO STR 41R AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 503435-14AD. (1299184).SDR DALA2025111208282Window Post · crackedCRACK FOUND AT RH WINDSHIELD CENTER POST LOWER ATTACHMENT AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 584325-14AD. (1299124).SDR DALA2025111108234Skin · ground damageCATERING TRUCK DAMAGED SKIN LOCATED BETWEEN FR 62-64 AND BETWEEN S 37-41R. CORRECTIVE ACTION: COMPLIED WITH ER/A 503435-14AD (1298120).SDR DALA2025111108239Frame · crackedCRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297446).SDR DALA2025111108238Frame · crackedCRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297432).SDR DALA2025111108237Frame · crackedCRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297420).SDR DALA2025111108236Frame · crackedCRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297300).SDR DALA2025111108235Frame · crackedCRACK FOUND ON THE HORIZONTAL FLANGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297285).SDR DALA2025111108233Frame · crackedCRACK FOUND ON THE HORIZONTAL FALNGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. CORRECTIVE ACTION: COMPLIED WITH ER/A 605954-14AD. (1297278).SDR DALA2025111108232Frame · crackedCRACK FOUND ON THE HORIZONTAL FLANGE RADIUS OF THE FR68 LOCATED BETWEEN THE FRAME WEB AND FRAME STIFFENER AT LEVEL OF S22L. COMPLIED WITH ER/A 605954-14AD. (1297326).SDR DALA2025111108229Plate · crackedCRACK FOUND AFFECTING THE UPPER PLATE OF LT PAX/CREW DOOR 831 CREW DOOR 831 IN PASSENGER CABIN. COMPLIED WITH ER/A 630181-14. (1297839).SDR DALA2025111108227Window Frame · crackedCRACK FOUND AT RH WINDSHIELD CENTER POST LOWER ATTACHMENT AREA. COMPLIED QITH ER/A 629316-14AD. (1297842).SDR DALA2025111008208Access Panel · erodedEROSION ACCESS PANEL 191DB AT LOWER FUSELAGE. COMPLIED WITH ER/A 629770-14. (1296589).SDR DALA2025111008207Door Frame · crackedCRACK INDICATION FOUND ON FRAME 20 LH DOUBLE JOGGLE AREA HOLE 6 DOOR STOP FITTING 7. CORRECTIVE ACTION: COMPLIED WITH ER/A 629422-14AD. (1296575).SDR DALA2025111008210Window Post · crackedCRACK FOUND AT RT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA. COMPLIED WITH ER/A 584325-14AD. (1295928).SDR DALA2025111008209Window Post · crackedCRACK FOUND AT RT WINDSHIELD CENTER POST LOWER ATTACHMENT AREA. COMPLIED WITH ER/A 629316-14AD. (1295911).SDR DALA2025111008206Elec Connector · corrodedCORROSION ON ELECTRICAL CONNECTOR 16CA LOCATED ARTIFICIAL FEEL AND RUD DER TRAVEL LIMITING AT VERTICAL STABILIZER. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR (16CA-A) AS PER AIRBUS ESPM 20-44- 11. (1295830).SDR DALA2025111008205Post · corrodedCORROSION ON LATERAL POST AFT RH SIDE AT LAV A. COMPLIED WITH ER/A 629473-14. (1295785)SDR DALA2025111008204Elec Connector · corrodedCORROSION ELECTRICAL CONNECTOR ON IB ELEVATOR SERVO CONTROL ACTUATOR (1E/A) AND OB ELEVATOR SERVO CONTROL ACTUATOR (2E/A) ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTORS (34CE3-C) (34CE3-A) (34CE1-C) AS PER AIRBUS ESPM 20-44-11. SDR DALA2025111008202Floorbeam · crackedCRACK INDICATION FOUND IN FASTENER HOLE H3, LOCATED AT FR16RH CROSSBEA M SPLICING AREA. FWD FUSELAGE PASSENGER CABIN. COMPLIED WITH ER/A 629518-14AD. (1295791).SDR DALA2025111008201Floorbeam · crackedCRACK INDICATION FOUND IN FASTENER HOLE H2, LOCATED AT FR16RH CROSSBEAM SPLICING AREA. FWD FUSELAGE PASSENGER CABIN. COMPLIED WITH ERA 629518-14AD. (1295790).SDR DALA2025111008200Crossbeam · crackedCRACK INDICATION FOUND IN FASTENER HOLE H1, LOCATED AT FR16RH CROSSBEAM SPLICING AREA. FWD FUSELAGE PASSENGER CABIN. COMPLIED WITH ER/A 629518-14AD. (1295786).SDR DALA2025111008198Web · crackedCRACK WEB LOC. FR 52 LH AT BELLY FAIRING. CORRECTIVE ACTION: COMPLIED WITH ER/A 629731-14. (1295808).SDR DALA2025111008197Skin · dentedDENT EXTERNAL SKIN LOCATED FR 3 AND 17 INCHES BELOW -Y675 LOWER FUSELAGE. COMPLIED WITH ER/A 629682-14. (1295801).SDR DALA2025111008196Bushing · wornWEAR ON FIXED FLANGED BUSHING OF FWD LUG ON RH KEEL BEAM MLG DOOR HING E FITTING FWD SIDE. COMPLIED WITH ER/A 629519-14AD. (1295862).SDR DALA2025111008195Bushing · wornWEAR ON FIXED FLANGED BUSHING OF FWD LUG ON LH KEEL BEAM MLG DOOR HING E FITTING FWD SIDE. COMPLIED WITH ER/A 629573-14AD. (1295792).SDR DALA2025111008194Flap Track · corrodedCORROSION ON OTBD FLAP BEARING HOUSING AT TRACK 3 LT WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 629676-14. (1295851).SDR DALA2025111008211Door Frame · crackedCRACK INDICATION AT HOLE #6 AT THE DOUBLE JOGGLE AREA OF THE FR20LH AROUND THE PASSENGER SERVICE DOOR. COMPLIED WITH ER/A 629422-14AD. (1293811).SDR DALA2025111008193Floor Panel · delaminatedDELAMINATED TOP LAYER FLOOR PANEL 211GF IN COCKPIT. COMPLIED WITH ER/A 629679-14. (1294723).SDR DALA2025111008192Floor Panel · delaminatedDELAMINATED TOP LAYER FLOOR PANEL 212GF IN COCKPIT. COMPLIED WITH ER/A 629679-14. (1294717).SDR DALA2025111008191Floor Panel · delaminatedSHIP 3153 DELAMINATED TOP LAYER FLOOR PANEL 231CF IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH ER/A 629679-14. (1294714).SDR DALA2025111008212Hinge Fitting · corrodedFUSELAGE MLG DOOR KEEL BEAM RH FWD HINGE FITTING WEAR AND CORROSION. CORRECTIVE ACTION: REPAIRED PER ERA 629519-14AD. (1292906)SDR DALA2025110708126Keelbeam · corrodedSHIP 3153 WEAR AND CORROSION FUSELAGE MLG DOOR KEEL BEAM LH FWD HINGE FITTING. CORRECTIVE ACTION: REPAIRED PER ERA 629573-14AD. (1291431)SDR DALA2025110708121Power Supply · faultedSHIP 3153 EMERGENCY POWER SUPPLY UNIT FAULT 11WL. CORRECTIVE ACTION: R/R EPSU 11WL ON UNSERVICEABLE CONDITION AS PER A320 FAM AMM 33-51-38-000-001-A. (1291827).SDR DALA2025110708120Power Supply · faultedSHIP 3153 EMERGENCY POWER SUPPLY UNIT FAULT 12WL. CORRECTIVE ACTION: R/R EPSU AS PER A320 FAM AMM 33-51-38-000-001-A. (1291831).SDR DALA2025110508071Flap Track · corrodedCORROSION ON LT WING OTBD FLAP TRACK NR 3, INNER AND OUTER RIB 5, AT ECCENTRIC BEARING. REPAIRED PER ERA 629676-14. (1287999)SDR DALA2025110508070Skin · wornWEAR ON EXTERNAL SKIN LOC. BTW FR73 TO FR74 AND STR17/18 LH ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A 630030-14. (1288502).SDR DALA2025110308005Stringer · wornWEAR ON STRINGER 39R LOCATED BTW FR 47 / 51 TO FR 52 IN AFT CARGO COMPARTMENT. REPLACED STRINGER AND FASTENERS LOC.STR39 R/H BTW FR 47 / 51 TO FR 54 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM51-72-11. (1283932).SDR DALA2025110308002Pin · brokenSHIP 3153 BROKEN PIN ON CONECTOR ON OFFWING SLIDE LH. CORRECTIVE ACTION: R/R OFFWING ESCAPE SLIDE LH SIDE IAW AMDS CARD 2562-4001. (1282257).SDR DALA2025102707830Seat Track · corrodedCORROSION SEAT TRACK +Y1292 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 LOCATED FROM FR12 TO FR24 AT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (1269662).SDR DALA2025102407776Seat Track · corrodedCORROSION SEAT TRACK -Y765 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y765 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 A319 SRM 51-72-11. (1267628).SDR DALA2025102307753Track · corrodedSHIP 3153 CORROSION ON FLAP BEARING TRACK 3 ON O/B FLAP L/H WING (1 E/A). CORRECTIVE ACTION: REPLACED FLAP BEARING TRACK #3 ON O/B FLAP L/H WING (1 E/A) AS PER A320 FAM AMM 57-52-21-000-001-A AND A320 FAM AMM 57-52-21- 400-001-A. (1266205).
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