N821DX
Service difficulty reports · 168
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 = 'N821DX' 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 = 'N821DX' 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 DALA2018021400895Lever · detached(AIRCRAFT 6821, L/P 9973752) 1R DOOR ARMING LEVER DETACHED. RMVD R1 DOOR BUSSLE, FOUND FOD IMPEDING GIRT BAR OPERATION, RMVD FOD OPS CHK OK. OK FOR SVC. REF B757 AMM 52-11, ARM AND DISARM OK.SDR DALA2018032301855Threshold · dentedAFT CARGO DOOR THRESHOLD DENTED 9 INCHES FROM AFT SIDE OF DOOR AND 8 INCHES LONG. THE THRESHOLD WAS REPAIRED IAW ER/A 06 489967-14MA, REV G.SDR DALA2017122608895Spring · detachedEMERGENCY LIGHT COVER SPRING DETACHED. R & R EMERGENCY LIGHT IAW AMM 33-51. OPS CHECKED NORMAL.SDR DALA2017121308599Pushrod · brokenL4 PASSENGER DOOR LOWER LATCHING TORQUE TUBE FWD PUSH ROD FAILED IS BROKEN. REMOVED AND REPLACED L4 PASSENGER DOOR LOWER FWD PUSH ROD IAW SRM 51-40-02 ADJUSTMENT TO BE ACCOMPLISHED ON AMDS 2566-9001-4L.SDR DALA2017020701022Control Unit · faultyHAD A BRAKE TEMP LIGHT AND ANTI-SKID FAULT WHICH CLEARED ON ENROUTE. ON LANDING AT LEAST ONE TIRE DEFLATED WITH THREE MORE DEFLATING AT THE GATE. MAINTENANCE BITE OF ANTISKID CONTROL UNIT PER FIM. REPLACED ANTISKID CONTROL UNIT, NR 4 BRAKE ASSEMBLY, NUMBER 3,SDR DALA2016103108096Light · inoperative4R EXTERIOR EMERG LIGHT RELAMP. REPLACED DOOR 4R SLIDE LIGHT ASSY PER AMM33-51. VISUALLY CHECKED ELEC WIRE BEHIND THE LIGHT ASSY THEN NTF. ALSO CHECKED GRD/PWR WITH MULTIMETER, NTF REF WDM33-51 CHECKED.SDR DALA2016032402333Skin · dentedRT T/E FLAP 20" FROM OTBD END 3" FROM T/E. T/E WEDGE UPPER SKIN HAS DENT. T/E WEDGE UPPER SKIN REPAIRED DENT IAW SRM.SDR DALA2016032302258Cable · out of limitsL-1 PASSENGER DOOR EMERGENCY ACTUATION CABLE SYS FAILED TRAVEL CHECK IAW CARD 5211-3001-1L, STEP 4. ADJUSTED L-1 DOOR EMERGENCY ACTUATION CABLE IAW AMM 52-11-32-404-010 PAR E 16, CABLE TRAVEL CHECK GOOD 0.95.SDR DALA2016022701567Floorbeam · corrodedCABIN FLOORBEAM BS 365, RBL 1 - 50, TOP SURFACE HAS CORROSION AND CUTS. BLENDED AND REMOVED CORROSION TOP SURFACE IAW SRM 53-00-51, FIG 101 ALLOWABLE DAMAGE DETAIL IV. ORIGINAL MATERIAL THICKNESS .125" IAW DWG BAC 1518-338. MATERIAL LOSS .030. FOUND OUT OFSDR DALA2016022701566Stringer · damagedWHILE WORKING, NR 100-41, FOUND DOUBLE DRILLED HOLE THRU STR 28R AT BS 1320. ACCOMPLISHED PERMANENT REPAIR ON BS 1320, STR 28R IAW ER/A 542500-14, REV ORIGINAL. TRACKING OF REPAIR TO BE ACCOMPLISHED.SDR DALA2016030401791Frame · corrodedCORROSION ON FUSELAGE FRAME AT AFT CARGO COMPARTMENT, BS 1320, FWD SIDE, BETWEEN STR 27R AND 28R. REMOVED CORROSION ON FRAME AT BS 1320, STR 27R-28R IAW SRM 53-00-07, FIG 101. ORIGINAL MATERIAL THICKNESS .071" IAW SRM 53-60-07, FIG 1 AND DWG 146N1028. MATERSDR DALA2016020301027Frame · dentedTHREE DENTS ON FWD CARGO LT FRAME UPPER FLANGE AT BS 660 BETWEEN STR 23L AND 25L. DENTS NOT ALLOWED AND FOUND OUT OF LIMITS IAW SRM 53-00-07 ALLOWABLE DAMAGE 1. REPAIRED THE FRAMEIAW SRM 53-00-07, REPAIR 5, FIG 201.SDR DALA2016012600666Frame · dentedTWO DENTS ON FWD CARGO LT FRAME AT BS 580 BETWEEN STRINGERS 23-25L. TRIMMED-OUT THE DENTS AT FWD CARGO FRAME IAW SRM 53-00-07, REPAIR 5, PG 201. REPAIRED IAW SRM 53-00-07, REPAIR 5.SDR DALA2016012600639Floorbeam · corrodedCABIN FLOORBEAM, BS 377.7/LBL 61-RBL10, TOP SURFACE CORRODED AND HAS TOOLING MARKS/CUTS CP53-221-01L. REMOVED CORROSION ON FLOORBEAM TOP SURFACE AT BS 377.7, LBL 61 TO RBL 10 IAW SRM 53-00-51, FIG 101. ORIG MAT .125", MATERIAL LOSS AT LBL 20 TO LBL61 MEASURESDR DALA2016012100511Frame · dentedTWO DENTS ON AFT CARGO FUSELAGE FRAME AT BS 1400 AT AND JUST BELOW STR 23L. NO DENTS ALLOWED ON FRAME FLANGE IAW SRM 53-00-07, FIG 101, ALLOWABLE DAMAGE 1. REPAIRED FRAME AT BS 1400 BELOW STR 23L IAW SRM 53-00-07, REPAIR 5. REPAIR IS PERMANENT CAT "B" ZONE 1SDR DALA2016012200533Frame · corrodedAFT CARGO BS 1540 BETWEEN STR 28R-29R, FRAME FWD SIDE HAS CORROSION AT PREVIOUS BLEND AND CORROSION AT AFT SIDE SHEAR TIE. R & R SHEAR TIE AT BS 1540 BETWEEN STR 28R-29R IN REF TO SRM 51-40-02, PAGE 4-7. DWG NR 140N2002, ORIGINAL MATERIAL ON THE FRAME BS 154SDR DALA2016011300251Skin · dentedLEFT INBD MAIN FLAP UPPER CENTER SKIN, BS 141 DENT FOUND TO BE OUT OF LIMITS. REPAIRED LT INBD MAIN FLAP UPPER CENTER SKIN BS 141 IAW SRM 51-70-10. DAMAGE MEASURES 2" DIAMETER. PN:113N2003-63, SN: SB001115.SDR DALA2017120408423Stiffener · corroded(AIRCRAFT 6821, L/P 2266204) MONITOR INSPECTION LOG REFERENCE ER/A 539845-14 REQUIRES STAGE II DTA APPROVAL WITHIN 24 MONTHS OF 04 DEC 2015. ACCOMPLISHED PERMANENT REPAIR IAW ER/A 539845-14 REV ORIG. CUT OUT CORROSION DAMAGE AND CUT THE STIFFENER AT LBBL 0.23"
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