N234JQ
Service difficulty reports · 25
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 = 'N234JQ' 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 = 'N234JQ' 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 R61A2026041400105Hydraulic System · low pressureHYD 2 LO PRESSURE IN FLIGHT AFTER ATTEMPTING TO EXTEND THE GEAR, THEN HYD 2 LO QTY. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HYD LINES.SDR R61A2025111900512Stringer · corrodedWHILE IN HEAVY CHECK - STR 21L HAS EVIDENCE OF CORROSION FROM FR 88 TO 91. REPAIRED STR 21L FROM FR 88 TO 91 BY INSTALLING SPLICE AND REPAIR FILLER REF EMB SRM 51-40-08 AND ETD2020-170-007474SDR R61A2025111900511Skin · crackedWHILE IN HEAVY CHECK - LH WING HAS 1EA CRACK ON LOWER SKIN TRAILING EDGE AT MLG CUTOUT BETWEEN RIBS 3 AND 3A AS MARKED. PERFORMED REPAIR ON LH WING 1EA CRACK ON LOWER SKIN TRAILING EDGE AT MLG CUTOUT BETWEEN RIBS 3 AND 3A AS MARKED AS PER ETD--2025-170-931384SDR R61A2025111900510Skin · crackedWHILE IN HEAVY CHECK - CRACKED SKIN UNDER LH SLAT #2 INBD TRACK CUTOUT TOP SIDE. REPAIRED A CRACK ABOVE THE L/H FIXED LEADING EDGE AT THE INBOARD SLAT TRACK CUT-OUT OF SLAT #2 BY CUTTING THE DAMAGE OUT AND INSTALLING A FABRICATED INTERNAL DOUBLER. IAW ETD2025SDR R61A2023041500231Beam · corrodedUPON REMOVAL OF FWD CARGO FINGER DOUBLERS FOUND LOWER BEAM CORRODED. REMOVED AND REPLACED FWD CARGO DOOR LOWER BEAM. REF EMB SRM 51-40-08.SDR R61A2023041500243Bushing · damagedDURING THE REMOVAL OF LH AILERON TORQUE TUBE SUPPORT 1EA HOLE WAS ELONGATED. REMOVED 1 EA ELONGATION FROM UNDER LH AILERON TUBE SUPPORT AT WING MAIN BOX BY REAMING TO .406" AND INSTALLING REPAIR BUSHINGS. REF EMB ETD2023-170-008650 REV ASDR R61A2023041500244Shear Panel · corrodedSHEAR CLIP CORRODED ON FRAME 76 AND STRINGERS 28R-29R. REMOVED AND REPLACED SHEAR CLIP ON FRAME 76 BETWEEN STGR 28R-29R REFER SRM 51-40-08SDR R61A2023041500230Crossbeam · out of limitsFLOOR CROSS BEAM 84 HAS RAZOR SCRATCH AT RBL +22.0". REMOVED RAZOR SCRATCH ALONG FR 84 UPPER CROSSBEAM FLANGE. . FOUND TO BE OUT OF LIMITS REF: EMB SRM 51-10-03. PERFORMED CUT OUT OF THE AFFECTED AREA, LOCATED AND DRILLED REPAIR PARTS FOR CROSSBEAM FRAME 84. ISDR R61A2023041500229Beam · corrodedCORROSION ON FORWARD PASSENGER DOOR CUTOUT LOWER BEAM INSIDE FORWARD AND AFT GIRT BAR FITTING CUTOUTS. REMOVED AND REPLACED FWD PASSENGER DOOR CUTOUT LOWER BEAM. REF EMB SRM 51-40-08.SDR R61A2021081800654Door · lack of lubeL2 DOOR VENT FLAP HANDLE HARD TO OPERATE. LUBRICATED, PERFORMED OPS CHECK IAW AMM 52-12-00. OPS CHECK GOOD.SDR R61A2021070700534Control Box · defectiveBURNING SMELL IN COCKPIT/CABIN FOLLOWED BY APU GEN OFF BUS. R&R W314 HARNESS AND R&R RICC CABINET.SDR R61A2021060200462Unknown · smokeSMOKE IN CABIN. APU GEN OFF BUS EICAS MESSAGE. APU HAD BEEN RUNNING NORMAL FOR 15-20 MINUTES. PERFORMED INSPECTION OF APU PER FOM 49-10-00-810-813A. COULD NOT DUPLICATE SMOKE DURING POWER UP OF APU REF FIM 49-10-00-810-813.SDR R61A2020031290394Doubler · corrodedCORROSION ON COPILOT FLOOR DOUBLER BETWEEN FR08 AND FR12 AS MARKED. CUT OUT, REMOVED, LOCATED,DRILLED AND DEBURRED SPLICE SECTION OF COCKPIT DOUBLER AND FABRICATED AND INSTALLED SPLICE SECTIONS AS REQUIRED REF ETD2020-170-007754 REV.AND SRM 51-40-08. RESTORED SDR R61A2020031290393Panel · corrodedCORROSION ON INNER FLANGE OF PANEL 192CR. PN 170-13414-003 REMOVED CORROSION CORROSION ON INNER FLANGE OF PANEL 192CR REF EMB SRM 51-10-03.MAT'L IS .050". MAXIMUM DAMAGE IS L= 2.0" X W= 1.5" X H= .020"LOCATED AND DRILLED NEW INNER FLANGE (SPACER) ON PANEL 192SDR R61A2020031320399Skin · crackedWHILE IN HEAVY CHECK-MAJOR REPAIR- DISCOVERED RH WING UPPER SKIN HAS SMOKING RIVETS AND SIGNS OF A CRACK AT THE #3 SPOILER INBD ATTACH FITTING AS MARKED. REMOVED DAMAGE AT THE RH WING UPPER SKIN, AT THE #3 SPOILER INBD ATTACH FITTING, BY CUTTING OUT CRACK. FSDR R61A202003070373Bracket · corrodedDURING HEAVY CHECK MAINTENANCE FOUND STGR 21L AND ATTACHED BONDING BRACKET CORRODED AT ATTACHMENT BETWEEN FR 89-FR90. REMOVED DAMAGED PORTION OF STGR
21L, FROM FR 88 - 90.5. LOCATED, DRILLED AND INSTALLED REPAIR FILLER AND REPAIR SPLICE, ON STGR 21L, AT FR 88SDR R61A202003070372Seal Rest · corrodedDURING HEAVY CHECK MAINTENANCE FOUND FWD CARGO AFT CORNER SEAL REST HAS AN AREA CORROSION. REMOVED DAMAGED SEAL REST AT FWD CARGO AFT CORNER. LOCATED, DRILLED AND INSTALLED NEW
SEAL REST AT FWD CARGO AFT CORNER. SURFACE PROTECTION APPLIED. REF SRM 51-40-02 51SDR R61A202003070376Shear Tie · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORRODED SHEAR CLIPS 2 EA, AT STR. 21L, ONE AT FR. 89 AND ONE AT FR. 90. REMOVED, FABRICATED AND INSTALLED 2EA
STANDOFF CLIPS. 1 AT FR 89 AND 1 AT FR 90 STR 21L. REF ENGINEERING DRAWING 170-65671-001 AND SRM 51-31-00. RESTSDR R61A202003070375Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND R/H I/B SEAT TRACK GOUGED AND CORRODED BETWEEN FR. 31-32. REMOVED DAMAGE FROM R/H I/B SEAT TRACK, BETWEEN FR.31-32, BY PERFORMING EMB SRM
53-00-10/REPAIR 02/. A/C REMAINS IN CHECK.SDR R61A202003070374Panel Support · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON R/H AFT PANEL SUPPORT AT FRM90. REMOVED AND REPLACED R/H AFT PANEL SUPPORT AT FRM90 PER SRM 51-40--
08. APPLIED SURFACE PROTECTIION PER SRM 51-23-05, 51-23-06. A/C REMAINS IN CHECK.SDR R61A202003070371Doubler · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION, FORWARD WET AREA ON FLOOR DOUBLER FORWARD EDGE AT FRAME 19. REMOVED DAMAGED FLOOR DOUBLER AT FRAME 19 (LH SIDE) FWD WET AREA.
LOCATED, DRILLED AND INSTALLED NEW FLOOR DOUBLER AT FRAME 19 (LH SIDE) FWD WET AREA. SDR R61A202003070370Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION, FORWARD WET AREA ON LH INBOARD SEAT TRACK IN MULTIPLE LOCATIONS ALONG THE SPAN FROM FRAME 16 TO 20 REMOVED CORROSION ON LH SEAT TRACK FRAME
16-20 REF SRM 51-10-03. OUT OF LIMITS SRM 53-1010/AD01. REMOVED AND RESDR R61A202003070367Seat Track · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION, FORWARD WET AREA ON RH INBOARD SEAT TRACK AROUND 7 FLOORBOARD SCREW
HOLES BETWEEN FRAMES 14 AND 19. REMOVED CORROSION AND REPAIRED RH INBOARD SEAT TRACK BETWEEN FRAMES 14 AND 19 REF SRM 51-10-03, SRM 53-10-10. RSDR R61A202003070369Mount Fitting · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION, FORWARD WET AREA ON THE FORWARD LAVATORY AFT LH FLOOR MOUNT FITTING ON FRAME 16. REMOVED AND REPLACED NEW FORWARD LAVATORY
AFT LH FLOOR MOUNT FITTING ON FRAME 16 REF.EMB SRM 51-40-08. PAINTED TOP COAT REF SRM 51SDR R61A202003070368Gusset · corrodedDURING HEAVY CHECK MAINTENANCE FOUND CORROSION ON R/H AFT GUSSET PLATE AROUND PUCK MOUNT ON CROSSBEAM AT FRM90. REMOVED DAMAGED GUSSET PLATE, AT FR
90. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW GUSSET PLATE, AT FR 90. SURFACE PROTECTION APPLIED.REF EMB S
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