N203JB, cancelled Dec 17, 2024
Service difficulty reports · 97
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 = 'N203JB' AND deregistration_id = 'N203JB-2024-12-17' 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 = 'N203JB' AND deregistration_id = 'N203JB-2024-12-17' 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 EE4Y2024120521415Skin · crackedPERFORMED PERMANENT REPAIR AT RH WING SLAT 5 BETWEEN RIB 18 AND 21 AS PER COOPESA´S EO COO-EO-2024-21014-R00 REV 00, DUE TO CRACK FOUND AT SKIN AROUND ACTUATOR AREA, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-026551 REV ORIG, THE REPAIR WASSDR EE4Y2024120521414Skin · damagedPERFORMED PERMANENT REPAIR AT RH WING LOWER SKIN SB 190-57-0056 AFT REINFORCEMENT AREA COMMON TO SPAR II COOPESA´S EO COO-EO-2024-21236-R00 REV 00, DUE TO OVERSIZED HOLES FOUND DURING THE ACCOMPLISHMENT OF THE SB 190-57-0056, THE REPAIR WAS FOLLOWED BY THE EMBSDR EE4Y2024120521413Skin · damagedPERFORMED PERMANENT REPAIR AT RH WING LOWER SKIN SB 190-57-0056 REINFORCEMENT AREA COMMON TO SPAR I COOPESA´S EO COO-EO-2024-21119-R00 REV 00, DUE TO OVERSIZED HOLES FOUND DURING THE ACCOMPLISHMENT OF THE SB 190-57-0056, THE REPAIR WAS FOLLOWED BY THE EMBRAER SDR EE4Y2024120521412Skin · crackedPERFORMED TEMPORARY REPAIR AT LH WING SLAT 5 BETWEEN RIB 18 AND 21 AS PER COOPESA´S EO COO-EO-2024-21017-R00 REV 00, DUE TO CRACKS FOUND AT SKIN AROUND ACTUATOR AREA, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-026548 REV ORIG, THE REPAIR WASDR EE4Y2024120521411Rib · crackedPERFORMED TEMPORARY REPAIR AT LH WING RIB 6 AS PER COOPESA´S EO COO-EO-2024-21207-R00 REV 00, DUE TO CRACKS FOUND AT MLG ACTUATOR SUPPORT FITTING, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-029064 REV ORIG, THE REPAIR WAS CONSIDERED TEMPORASDR EE4Y2024120521410Access Panel · corrodedPERFORMED PERMANENT REPAIR AT LH WING TRAILING EDGE SLAT 4 AS PER COOPESA´S EO COO-EO-2024-21029-R00 REV 00, DUE TO CORROSION FOUND AT REAR OUTBOARD AREA, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSITION ETD2024-190-026436 REV ORIG. THIS REPAIR WAS CATEGORIZSDR EE4Y2024120521409Skin · damagedPERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT LH WING SKIN TRAILING EDGE AT RIB 11 AREA, AS PER COOPESA´S EO COO-EO-2024-21043-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISDR EE4Y2024120521408Skin · damagedPERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT RH WING SKIN TRAILING EDGE AT RIB 10 AREA, AS PER COOPESA´S EO COO-EO-2024-21191-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISDR EE4Y2024120521407Skin · damagedPERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT FR01+65MM STR 20L+130MM, (FWD FUSELAGE) AS PER COOPESA´S EO COO-EO-2024-21042-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRAER DISPOSDR EE4Y2024120521406Rib · damagedPERFORMED REPLACEMENT OF PERMANENT REPAIR INSTALLED AT WING TO FUSELAGE RIB FR52, (CENTER FUSELAGE II) AS PER COOPESA´S EO COO-EO-2024-21057-R00 REV 00, SINCE EXISTING REPAIR WAS FOUND WITHOUT MATERIAL TRACEABILITY RECORDS, THE REPAIR WAS FOLLOWED BY THE EMBRSDR YENA2024061100856Skin · damagedDURING HEAVY MAINTENANCE: DURING CURRENT CHECK ON N203JB (MSN: 023) @ MCN, EAMS REPORTED THREE (3) BLEND-OUT SPOTS ON THE CENTER FUSELAGE I EXTERNAL SKIN @ FR30-32 & STGR 25L-26L. SEE REF /1/, ETD REV A, FOR COMPLETE INFORMATION. EMBRAER PROVIDED ENGINEERING SDR YENA2024061100855Skin · crackedDURING HEAVY MAINTENANCE: DURING CURRENT LEASE RETURN CHECK ON N203JB (MSN 023) AT MCN DATED 05/2024, A DENT WAS FOUND ON THE FWD FUSELAGE SKIN BETWEEN FR 1-2 & STRR 22L-24L. SEE REF /1/ ETD FOR DETAILS. THE DENT IS MEASURED TO BE 0.70” L X 0.50” W AND 0.008”SDR YENA2024061100854Skin · damagedDURING HEAVY MAINTENANCE CHECK ON N203JB (MSN: 023) @ MCN, EAMS REMOVED THE EXISTING DOUBLER REPAIR IAW ETD2019-190-137093 REV A. THE DENT IS LOCATED OVER 3 BAYS AND THE REPAIR CROSSES OVER A ROW OF RIVETS BETWEEN FR98-99 AND STGR 25R-29R. AN HFEC INSPECTION WSDR YENA2024061100863Light · inoperativeDURING HEAVY MAINTENANCE: EMERGENCY LIGHT ON FWD PASSENGER DOOR CEILING PANEL INOP; REF EAMS WO H9417 NR 00140 REMOVED AND REPLACED FWD PAX ENTRANCE EMERGENCY/COURTESY LIGHT ASSY IAW AMM 33-26-01. OPS TEST GOOD IAW AMM 33-26-00-710-801-A.'SDR YENA2024061100862Cover · crackedDURING HEAVY MAINTENANCE: LH WING TO BODY FAIRING LOWER EVACUATION LIGHT COVER CRACKED; REMOVED AND INSTALLED NEW LH WING TO BODY FAIRING LWR EVAC LIGHT COVER IAW EMBRAER 190 AMM 33-50-25.'SDR YENA2024061100861Power Supply · no testDURING HEAVY MAINTENANCE: ELPU FUNCTIONAL TEST FAILS, MULTIPLE EMERGENCY LIGHTS THROUGHOUT THE CABIN AND EXTERIOR OF AIRCRAFT ARE INOP; REMOVED AND REPLACED #4 AND #5 ELPU REF EMB190 AMM 33-50-01-000-801-A. OPERATIONAL CHECK GOOD PER EMB190 AMM 33-50-01-710-8SDR YENA2024061100860Light · no testDURING HEAVY MAINTENANCE: CABIN OVERWING EMERGENCY EXIT CEILING LIGHT INOP; PERFORMED OPERATIONAL TEST OF THE EMERGENCY LIGHT SYSTEM PER E190 AMM33-50-00-710-801-A. OPERATIONAL TEST IS GOOD AT THIS TIME. REF EAMS W/O H9417 NR 00139.SDR YENA2024061100859Skin · dentedDURING HEAVY MAINTENANCE: PER CUSTOMER REQUEST: CENTER FUSELAGE I EXTERNAL SKIN BTW FR30 AND FR32 STGR 25L AND STGR 26L WITH DENTS (3EA) RE-EVALUATE EMBRAER NR-00097 W/O H9417; REPAIRED 3EA AREAS ON FUSELAGE I EXTERNAL SKIN BTW FR30 AND FR32, STGR25L AND STGRSDR YENA2024061100858Skin · dentedDURING HEAVY MAINTENANCE: RE-EVALUATE DENT AT FR98-FR99 & STR25R-STR29R, THE DENT IS LOCATED OVER 3 BAYS AND REPAIR CROSSES OVER 1 RIVET ROW REF. EMBRAER NR-00179 W/O: H9417; REMOVED EXISTING REPAIR DOUBLER AND INSTALLED NEW REPAIR DOUBLER AND FILLER AT FR98-SDR YENA2024061100857Skin · dentedDURING HEAVY MAINTENANCE: COMPLY WITH E24-606-01 (REV 6-5-24 ) FUSELAGE / FWD FUSELAGE / EXTERNAL SKIN BETWEEN FR1-2 & STG 22L-24L / DENT & CRACK PERMANENT REPAIR REF. EMBRAER NR-00210 WO: H9417; COMPLIED WITH E24-606-01 REV 6-5-24.SDR YENA2023122901665Unknown · unknownFLT#221, BOS-PBI. 'BLEED 2 LEAK CAUTION AT FL 280 CABIN ALT HI WARNING ON DESCENT; ACCOMPLISHED FIM TASK 36-21-00-810-815-A00 R/R 1 EA. CORRODED CERAMIC PIN AT LOOP 5 CONNECTORS ICAS FAULT CLEARED SYS OP CK NORM ACCOMPLISHED HIGH POWER ENGINE ASSURANCE RUN SDR YENA2023122701649Unknown · unknownFLT#250, SAV-BOS. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO SAV) ' CLIMBING THROUGH APPROX 15,000 ' WE NOTICED A STRONG, SHARP ACRID SMELL IN THE COCKPIT. FA'S REPORTED THE SAME THING, STRONGEST AT MID CABIN. WE DECLARED EMERGENCY AND RSDR YENA2023111701427Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: CRACK ON RIB 22 AT LH WING; ALL WORK ACCOMPLISHED REF TOMX W/O2362 NR 00187 RIB # 22 AT LH WING WAS REPLACED PER EMB 190 SRM 51-43-04 AND SRM 51-43-03.SDR YENA2023111701425Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING] CORROSION ON FRAME 80 BTW STRG 28R/27R AT AFT CARGO DOOR CUTOUT STRUCTURE; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00012 ) CORROSION ON FRAME 80 BTW STRG 26R/27R WAS EVALUATED OUT OF LIMITS, THEREFORESDR YENA2023111701424Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: CRACK BEAM AT FWD AVIONICS ACCESS DOOR (123BL); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00013 ) REF TOMX WO 2362 NR 00064: BEAM ON FWD AVIONICS ACCESS DOOR (123BL) WAS REPLACED PER EMB 190 SRM 51-41-01,SRM 51-43-03 SDR YENA2023111701423Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR BEAM BTW FR87-89 AND +Y=300 AT AFT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00014 ) CORROSION ON FLOOR BEAM BTW FR87-89 AND +Y=300 AT AFT FLOOR STRUCTURE WAS RESDR YENA2023111701422Unknown · unknownDURING HEAVY MAINTENANCE: IN REF TO RC E12-111-02: CORROSION ON PREVIOUS REPAIR DOUBLER ON CTR SEAT TRACK BEAM, LOCATED BTW FR14 TO FR20 AND Y=280 LH, FLOOR STRUCTURE (W1). EVALUATION; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00015 ) CORROSION ON PREVIOUS REPAISDR YENA2023111701421Shear Tie · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION: [CPCP FINDING] CORROSION ON SHEAR CLIP IN FR81 BTW STGR 28R/27R AT AFT CARGO; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00016 ) REFERENCE TOMX W/O# 2362, N/R# 00190. CORROSION ON SHEAR CLIP IN FR81 BTW STGR 28R/27R WASDR YENA2023111701420Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON CTR BEAM LOCATED BTW FR13 TO FR19 AND Y=270 RH IN PASSENGER FLOOR STRUCTURE W1; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00017 ) REFERENCE TOMX W/O #2362, N/R# 00250. CORROSION ON CTR BEAMSDR YENA2023111701419Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON FLOOR BEAM BTW FR87-88 AND -Y=300 AT AFT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00018 ) REFERENCE TOMX W/O # 2362, N/R # 00217. CORROSION ON FLOOR BEAM BTW FR87-88 SDR YENA2023111701418Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON CROSS-BEAM LOCATED BTW FR17 AND Y=400 TO Y=810 RH IN PASSENGER FLOOR STRUCTURE W1 (PREVIOUS REPAIRED); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00021 ) REF TOMX WO# 2362. N/R# 00252.WIP: CSDR YENA2023111701417Unknown · unknownDURING HEAVY MAINTENANCE: INITIAL INSPECTION [CPCP FINDING]: CORROSION ON CROSSBEAM BTW FR84 AND -Y=300-1200 AT AFT FLOOR STRUCTURE (W2); (RESOLVED ON W/O: 1260255 TASKCARD: NR-00022 ) REF TOMX WO# 2362, N/R # 00223. CORROSION ON CROSSBEAM BTW FR84 AND -Y=300-SDR YENA2023111701416Unknown · unknownDURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER INTERCOSTALS REMOVAL IN REF TO NRC 00302 CORROSION ON SHARE CLIP FR 88 BTW STGR 28-29 RH AT C2. WAS FOUND;(RESOLVED ON W/O: 1260255 TASKCARD: NR-00023 ) REF TOMX WO# 2362, N/R# 00333. CORROSION ON SHARE CLIP FR 8SDR YENA2023111701415Unknown · unknownDURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER INTERCOSTALS REMOVAL IN REF TO NRC 00302 CORROSION ON STGR 27 RH BTW FR 86-87 AT C2. WAS FOUND;(RESOLVED ON W/O: 1260255 TASKCARD: NR-00024 ) REF TOMX W/O# 2362 N/R# 00332. STGR 27 RH BTW FR 86-87 AT C2 WAS REPAIRSDR YENA2023111701414Unknown · unknownDURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER INTERCOSTALS REMOVAL IN REF TO NRC 00302 CORROSION ON SHEAR CLIP FR 86 STGR 28/27 RH AT C2. WAS FOUND; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00025 ) REF TOMX W/O# 2362, N/R #00334. SHEAR CLIP FR 86 STGR 28/27 RH SDR YENA2023111701413Unknown · unknownDURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER INTERCOSTALS REMOVAL IN REF TO NRC 00301 CORROSION ON STGR 28 RH BTW FR 86-87 AT C2. WAS FOUND; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00026 ) REF TOMX W/O# 2362, N/R #00335. STGR 28 RH BTW FR 86-87 AT C2 WAS REPASDR YENA2023111701412Unknown · unknownDURING HEAVY MAINTENANCE: SECONDARY NRC IN REF NRC 00313: REPLACE INBD UPPER SPAR RH PYLON; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00027 ) REF TOMX W/O# 2362, N/R # 00350. INBD UPPER SPAR RH PYLON WAS REPLACED PER EMB-190 SRM 51-43-03 SRM 51-43-04 AND SRM 51- SDR YENA2023111701411Unknown · unknownDURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER DOUBLER REMOVAL IN REF NRC 00042, CORROSION ON SHEAR CLIP ABOVE FR 88 BTW STGR 28RH/STGR27RH WAS FOUND; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00028 ) REF TOMX W/O #2362, N/R # 00283.CORROSION ON SHEAR CLIP ABOVE SDR YENA2023111701410Shear Tie · unknownDURING HEAVY MAINTENANCE: SECONDARY NRC: AFTER SHEAR CLIP REMOVAL IN REF TO NRC 00303, CORROSION ABOVE FR 87 AND BTW STGR 28R/27R WAS FOUND; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00029 ) REF TOMX W/O# 2362, N/R# 00336. CORROSION ABOVE FR 87 AND BTW STGR 28R/2SDR YENA2023111701409Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON UPPER SKIN AND FASTENERS AREA COVERED BY LIVE TV RADOME; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00038 ) REPAIRED PER LETBLUE EC E23-991-0. REF TOMX NR 00168.SDR YENA2023111701408Shear Tie · unknownDURING HEAVY MAINTENANCE: CORROSION ON SHEAR CLIP ABOVE FR 87 BETWEEN STGR 28R/27R; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00037 ) REMOVED AND REPLACED SHEAR CLIP PER EMB-190 SRM 51-41-01 AND 51-41-02. REF TOMX NR 00303.SDR YENA2023111601396Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE /FUSELAGE / FLOOR STRUCTURE / BTW FR14 TO FR20 / Y=-273.0 / CTR SEAT TRACK BEAM / PREVIOUS DOUBLER /CORROSION/ PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023111601395Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE III / FR 80 BTW STGR 28R - 27R / CORROSION- TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023111601394Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CTR FUSELAGE III / FR 80 BTW STGR 28R - 27R / CORROSION- PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023111601393Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III STR28R / BWTN FR86-FR90 /CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023111601392Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / STR27R / BWTN FR86-FR87 /CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023111601391Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE SKIN / FR 62-66 & STGR 02L-02R / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR YENA2023061600670Unknown · unknownFLT#2933, DCA-MCO. (AIRCRAFT DIVERTED TO JAX) 'BLEED 1 FAIL; INTERROGATED CMC AND NO CORRELATED MESSAGES WITH BLEED 1 FAIL. PERFORMED OPS CHECK OF #1 BLEED PER AMM 36-11-. AL CHECKS NORMAL. AT THIS TIME IN MANY CONFIGURATIONS WITH PACKS AND OTHER BLEED / CLOSSSDR YENA2023060500574Unknown · unknownFLT#2534, PBI-DCA. 'ELPU 2 BATTERY CAPACITY TEST FAILED; REMOVED AND REPLACED ELPU 2 IN REF TO AMM 33-50-01. THE OPS CHECK IS GOOD. OK FOR FURTHER SERVICE. PARTS TRANSACTION COMPLETED UNDER W/O # 1257900 TASK CARD. E190-33-50-01-720-801-FWD.'SDR YENA2021071400460Unknown · odorFLT 1539, MVY-JFK. DURING FLIGHT COCKPIT SMELLED OF EXHAUST FUMES AT VARIOUS STAGES OF THE FLIGHT, ESPECIALLY ON THE DESCENT. FA'S DIDNT NOTICE IT BUT BOTH PILOTS NOTED IT ON BOTH LEGS. THOUGHT IT WAS AN ANOMOLLY OR TRANSIENT ODOR FIRST LEG THEN SAW ITS A REP
Back to N203JB, cancelled Dec 17, 2024