N26210
Service difficulty reports · 82
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 = 'N26210' 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 = 'N26210' 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 CALA2012041200257Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN HAS 3 INCH CRACK AT LES 142.45" FROM AFT SPAR. COMPLETED REPAIR LT HORIZONTAL STABILIZER LOWER SKIN REF SRM 55-10-01.SDR CALA2012041200256Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN HAS 2.25 INCH CRACK AT LES 142. 45 AND ABOUT 16.5" FROM AFT SPAR. COMPLETED REPAIR LT HORIZONTAL STABILIZER LOWER SKIN REF SRM 55-10-01.SDR CALA2012041200255Skin · crackedLEFT HORIZONTAL STABILIZER LOWER SKIN HAS 1 INCH CRACK AT LES 142.45 AND ABOUT 6" FROM AFT SPAR. COMPLETED REPAIR LT HORIZONTAL STABILIZER LOWER SKIN REF SRM 55-10-01.SDR CALA2012041100252Intercostal · corrodedCORROSION AT AFT SURROUND AND RT TRANSITION PANEL (INSIDE BOX AREA) OF AFT CARGO DOOR CUTOUT BS 847 AND BETWEEN STRINGERS 25 AND 26R. REMOVED AND REPLACED INTERCOSTAL AND INSTALLED TRANSITION PANEL IAW SRM 51-40-02.SDR CALA2012040900245Cargo Track · crackedAFT CARGO TRACK CRACKED 4 PLACES BETWEEN STA 727G AND 767. CTN 53-140-00 REMOVED AND SPLICED IN NEW CARGO TRACK IAW SRM 53-0053 REPAIR 3.SDR CALA2012040900244Transition Panel · corrodedAFT CARGO, RT TRANSITION PANEL CORRODED STA 767 TO 787. CTN 53-140-00. REMOVED DAMAGED TRANSITION PANEL, LOCATED AND DRILLED NEW PANEL INSTALLED NEW PANEL REF SRM 51-10-02, 51-40-02, AND AMM 51 21-00.SDR CALA2012040900243Floorbeam · corrodedCOCKPIT FLOORBEAM ANGLE HAS LIGHT CORROSION ON UPPER SURFACE BS 270 LBL 6 TO RBL 12. REPAIRED IAW ECRA-5321 -01566.SDR CALA2012040400230Frame · crackedFRAME IS CRACKED AT BS 440 BETWEEN S-8R AND S-9R. REPAIRED PER EA 5310-04716 REV C.SDR CALA2012040400229Frame · crackedFRAME IS CRACKED AT BS 727B BETWEEN S-8L AND S9-L. COMPLETED REPAIRED FRAME AT BS 727B STRINGER 8L-9L REF ECRA 5310-04716 REV C.SDR CALA2012040400228Frame · crackedFRAME IS CRACKED AT STA 440L BETWEEN S-8L AND S-9L. REMOVED SUPPORT BRACKET, CUT OUT DAMAGE, NDT AREA, FABRICATED REPAIR ANGLES A&B TREATED & PRIMED, COLD WORKED 6 HOLES & INSTALLED, INSTALLED SUPPORT BRACKET, APPLIED FILLET SEAL REF EA 5310-04716 REV C FIG 3SDR CALA2012040400227Frame · crackedFRAME IS CRACKED AT BS 500C BETWEEN S-8L AND S9L. FABRICATED AND INSTALLED REPAIR ANGLES A, B COLD WORKED HOLES, REF EA 5310-04716 REV C OPERATION 02.SDR CALA2012040400226Frame · crackedFRAME IS CRACKED AT BS 480L BETWEEN STR 8L AND 9L. REPAIRED PER EA 5310-04716 REV C OP 2.SDR CALA2012040200224Frame · crackedFRAME IS CRACKED AT STA 500C BETWEEN S-8R AND S-9R. REPAIRED FRAME PER EA-5310-04716 OP 02 PAGE 26 TO 28 STEPS 1 TO 13.SDR CALA2012040200223Frame · crackedFRAME CRACKED AT STA 380 BETWEEN S-8R AND S-9R. REPAIRED FRAME PER EA 5310-04716 REV C OP 2.SDR CALA2012040200222Frame · crackedFRAME IS CRACKED AT STA 400 BETWEEN S-8R AND S-9R. REPAIRED FRAME, REF-EA 5310-04716 OP 02, PG, 26-28 STEPS 1-13. NO EC/RA REQUIRED.SDR CALA2012040200221Frame · crackedFRAME IS CRACKED AT STA 480 BETWEEN S-8R AND S-9R. REPAIRED FRAME AT STA 480 BETWEEN STR-8R AND STR-9R. COMPLIED WITH STEPS 1-13, PAGES 26, AND 27 OF EA 5310-0471602 OP 02.SDR CALA2011101800664Coffeemaker · malfunctionedFLT ATTD REPORTED LARGE SPARK (BLUE FLASH) AND HEARD A LOUD POP NOISE AT FWD C/M`S. SHUT BOTH C/MAKERS OFF. NOT SURE WHICH ONE COULD NOT DUPLICATE TROUBLES ABOVE. INSPECTED C/MAKER CAVITY AND ASSOCIATED WIRING. NO DEFECTS OR EVIDENCE NOTED. REMOVED AND REPSDR CALA2011082400556Battery Pack · dischargedC/B "PASS CABIN" LIGHTING EMERG CHGR CB POPPED IN FLIGHT. TROUBLESHOT SYSTEM PER AMM 20-60-01. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER AMM 33-51-06. OPS CKS GOOD ACFT OK TO CONTINUE. BAT AND CHARGE REMOVED AND REPLACED WAS M1673.SDR CALA0800529Tire · blownNORMAL LANDING AND ROLLOUT UNTIL 80-100 KTS. AIRCRAFT VEERED LEFT WITH AN ASSOCIATED LOUD POP. TOWER AND AIR CREW VERIFIED RIGHT MAIN OUTBOARD TIRE SEPARATION. NUMBER 3 AND 4 TIRES REMOVED AND REPLACED. PER AMM 05-51-54-210-801, TIRE BURST INSPECTION OK PESDR CALA0700261Battery Pack · inoperativeTHE FIRST CLASS EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-06.SDR CALA0700099Channel · corrodedCENTER FLOOR PANEL SUPPORT MEMBER CORRODED. REPAIRED IAW ECRA 5310-04614.SDR CALA0600249Battery · inoperativeTHE R-2 DOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-00.SDR CALA0500153Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, BL 0 TO RBL 12. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01220.SDR CALA0500152Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE NEAR R-1 DOOR, STA 320, BL 0 TO RBL 24. REPAIRED FLOORBEAM IAW ECRA 5321-01216.SDR CALA0500151Door Frame · corrodedINSPECTION FOUND R-2 DOOR FRAME CORRODED AT Z-CHANNEL SILL, STA 990, RBL 64 TO LBL 24. THE FRAME WAS REPAIRED IAW ECRA 5311-01225.SDR CALA0500150Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 8 TO LBL 12. REPAIRED IAW ECRA 5321-01219.SDR CALA0500149Floorbeam · corrodedINSPECTION FOUND THE L-2 DOOR AREA FLOORBEAM NUT CLIP HOLES CORRODED AT STA 986.5, LBL 22.5 TO LBL 43. REPAIRED IAW ECRA 5321-01215.SDR CALA0500172Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 947-967, RBL 50, I/B OF R-2 DOOR FRAME. THE INTERCOSTAL WAS REPAIRED IAW ECRA 5321-01218.SDR CALA0500115Module · looseAISLE LIGHTING IN THE FIRST CLASS CABIN LOOSE AT G7 GALLEY. REPLACED LIGHT MODULE.SDR CALA0300434Skin · damagedTHE FUSELAGE SKIN SUSTAINED DAMAGE BELOW L-2 DOOR AT BS 958 BETWEEN S22L AND S23L. THE DAMAGE WAS REPAIRED IAW ECRA 5330-03261. A DIP WAS ISSUED TO ACCOMPLISH AN EXTERNAL DETAIL VISUAL INSPECTION OF THE FILLER AND DOUBLER LOOKING FOR CRACKS AND LOOSE OR MISSDR CALA0300336Skin · puncturedINSPECTION FOUND A HOLE PUNCTURED INTO THE FUSELAGE SKIN THREE FEET BELOW THE L-2 DOOR AT BS 958, S22L-S23L. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5330-03261.SDR CALA0200064Actuator · inoperativeTHE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE FAILURE WAS ACCOMPANIED BY ILLUMINATION OF THE NLG UNSAFE LIGHT AND VIBRATION FROM THE NOSE GEAR AREA. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NLG LOCK ACTUATOR AND LOCK MANIF
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