N17252, cancelled Oct 14, 1998
Service difficulty reports · 24
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 = 'N17252' AND deregistration_id = 'N17252-1998-10-14' 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 = 'N17252' AND deregistration_id = 'N17252-1998-10-14' 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 CALA9801327Torsion Link · shearedTHE LT MLG LOWER TORSION LINK SHEARED AFTER LANDING IN EWR. THE LT MLG LOWER TORSION LINK WAS REMOVED AND REPLACED. IN ADDITION, THE SHIMMY DAMPER AND BOTH INBOARD AND OUTBOARD GUIDE BRACKETS WERE REPLACED. A GEAR SWING WAS PERFORMED AND OPERATION CHECKED GSDR CALA9800918Axle · failedTHE NR 4 MAIN WHEEL SEPARATED FROM AIRCRAFT DURING TAXI IN. MAINTENANCE FOUND THE AXLE SHEARED OFF, NO OTHER AIRCRAFT DAMAGE WAS FOUND. THE RT MLG INNER CYLINDER WAS REMOVED AND REPLACED IAW MM 32-11-21 AND 12-15-31. *S/D* INVESTIGATION BY ENGINEERING CONCSDR CALA9700917Skin · crackedINSPECTION FOUND A 8.25 INCH CRACK ON THE LT NOSE WHEEL WELL SIDEWALL AND A 3 INCH CRACK ON THE RT NOSE WHEEL WELL SIDEWALL AT STA 259.5, WL 180. REPAIRS WERE INSTALLED IAW ECRA 5310-03512.SDR CALA9700609Fuel Pump · shaft shearedAFTER ROTATION NR 2 ENGINE FAILURE RETURNED TO CLE. NR 2 ENGINE FUEL PUMP SHAFT SHEARED. REMOVED AND REPLACED PER MM 73-11-01/72-60, PERFORMED POWER ASSURANCE RUN MM 71-09-266 PARTS CHG COMPLETE.SDR CALA9700232Hyd Line · leakingTHE A-SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE EN ROUTE. THE GEAR AND FLAPS WERE EXTENDED MANUALLY AND THE AIRCRAFT LANDED AT CLE. MAINTENANCE FOUND A HOLE IN PRESSURE HYDRAULIC LINE FROM NR 1 ENGINE PUMP. THE HYDRAULIC LINE AND THE NR 1 ENGINE PUMP WERE RESDR CALA9600974Logic Cards · inoperativeTHE RED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. A NOSE GEAR SWING WAS PERFORMED IAW MM 32-61-00, PAGE 501 TO 504 AND ALL GEAR OPERATION AND INDICATISDR CALA9600986Floor Beam Web · crackedINSPECTION FOUND A CRACK IN FLOOR BEAM WEB AT STA 294.5, RBL 47. THE CRACKED SECTION WAS REMOVED AND A NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2.SDR CALA9600985Battery · dischargedINSPECTION FOUND LOW VOLTAGE AT THE FORWARD ENTRY DOOR SLIDE LIGHT. THE BATTERY PACK WAS REMOVED AND REPLACED, OPERATION OF THE LIGHT CHECKED GOOD.SDR CALA9600984Battery · dischargedTHE SLIDE LIGHT VOLTAGE AT AFT ENTRY DOOR WAS FOUND LOW AND THE BULB WAS BURNED OUT. THE BATTERY PACK AND BULB WERE REMOVED AND REPLACED.SDR CALA9600983Battery · inoperativeINSPECTION FOUND EMERGENCY LIGHT OVER R-2 DOOR INOPERATIVE. THE BATTERY WAS REMOVED, RECHARGED AND REINSTALLED IAW MM 33-50-42. OPERATION OF THE LIGHT CHECKED GOOD.SDR CALA9600982Battery · inoperativeINSPECTION FOUND EMERGENCY LIGHT OVER L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED, OPERATION OF THE LIGHT WAS RESTORED.SDR CALA9600981Stringer · crackedINSPECTION FOUND A CRACK IN LT WING STRINGER 13 AT RIB MOUNTING POINT, FIRST RIB OUTBOARD OF WING ROOT, WBL 92.5. THE CRACK WAS STOP DRILLED IAW BOEING DRAWING NR 65C34533. A STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C34533. THE SSDR CALA9600980Frame · crackedINSPECTION FOUND FORWARD CARGO PIT FRAME CRACKED AT STA 460 BETWEEN STRINGER 20L AND 21L. THE CRACKED SECTION OF FRAME WAS REMOVED IAW SRM 51-30-2 AND A NEW FRAME WAS INSTALLED IAW BOEING DRAWING NR 65C25113.SDR CALA9600978Skin · creasedINSPECTION FOUND FUSELAGE SKIN CREASED AT STA 992 BETWEEN STRINGER 27L AND 27R. THE DAMAGED SECTION OF SKIN WAS REMOVED, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 6, 51-10-2 AND 51-30-2.SDR CALA9600977Stringer · damagedINSPECTION FOUND FUSELAGE SKIN DENTED AND STRINGER DAMAGED AT STA 400, STRINGER 18L. THE DAMAGED AREA OF STRINGER WAS REMOVED IAW SRM 53-10-3. THE SKIN WAS RETURNED TO ORIGINAL CONTOUR IAW SRM 51-70, FIGURE 4. REPAIR PARTS FOR STRINGER WERE FABRICATED AND ISDR CALA9600975Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500 TO 510 BETWEEN STRINGER 3L AND 4L. THE DENTED AREA WAS REMOVED, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2.SDR CALA9600979Skin · crackedINSPECTION FOUND A CRACK IN SKIN AT FORWARD GALLEY DOOR FORWARD LOWER CUTOUT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, FILLER, DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-2.SDR CALA9600976Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AROUND FASTENERS BELOW AFT CARGO DOOR. THE CORRODED AREA WAS CUT OUT, A SKIN SECTION, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-6 AND 51-10-2.SDR CAL960069Light · wire brokenFLT NR 1630 - EWR - THE AFT CABIN RIGHT EMERGENCY EXIT LIGHT NEAR BACK WALL ON FLOOR WOULD NOT ILLUMINATE. MAINTENANCE FOUND A WIRE TO THE EXIT LIGHT BROKEN. THE WIRE WAS REPAIRED AND THE LIGHT WAS RELAMPED. (M)SDR CAL960006Hyd Pump · leakingIAH - FLT 1607 - THE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 2 PUMP WAS REMOVED AND REPLACED. IN ADDITION, THE NR 1 ENGINE DRIVESDR CAL951051Battery · dischargedFLT NR 1205 - EWR - INSPECTION FOUND THE AFT GALLEY R-2 DOOR SLIDE PACK DOOR LIGHT INOPERATIVE. THE BATTERY FOR THE LIGHT WAS REPLACED AND OPERATION CHECKED GOOD. (M)SDR CAL950807Hyd Line · leakingGSO - FLT 1867 - THE AIRCRAFT WAS RETURNED TO GSO AFTER LOSING THE A-HYDRAULIC SYSTEM IN-FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLEX LINE TO OUTBOARD SPOILER PANEL IN LT WING OUTBOARD OF GEAR LEAKING. THE FLEX LINE WAS REPLACED. INSDR CAL950782Hyd Pump · leakingGSO - FLT 1495 - THE A-HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST WHILE EN ROUTE TO GSO. THE AIRCRAFT LANDED AT GSO WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACSDR CAL950115Hyd Module · leakingCLE - FLT 1255 - THE 'A' HYDRAULIC SYSTEM WAS LOST AFTER DEPARTING LGA. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND PLUG BROKEN ON 'A' SYSTEM HYDRAULIC MODULE. THE 'A' SYSTEM HYDRAULIC MODULE WAS REMOVED AND REPLACED AND LEAK CHECKS WERE
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