N14241, cancelled Jun 15, 1999
Service difficulty reports · 44
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 = 'N14241' AND deregistration_id = 'N14241-1999-06-15' 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 = 'N14241' AND deregistration_id = 'N14241-1999-06-15' 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 CALA9801914Line · chafedTHE 'A' HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO EWR. THE GEAR AND FLAPS WERE LOWERED MANUALLY AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 ENGINE HYDRAULIC PRESSURE LINE IN WING ROOT CHAFED ON CLAMP. THE HYDRAULIC LINE WAS REMSDR CALA9801626Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 435 TO 440, STRINGER 24R. A DOUBLER WAS INSTALLED IAW SRM 53-30-3.SDR CALA9801617Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN FUSELAGE KEEL BEAM LOWER SKIN AT STA 727, RBL 5. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-03, FIGURE 40.SDR CALA9800902Web · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WHEEL WELL SHEAR WEB AT STA 727. A REPAIR WAS INSTALLED IAW DRAWING 65C29228.SDR CALA9701214Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN RT HORIZONTAL STABILIZER SKIN BETWEEN STA 111.1 AND 126.6. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01369.SDR CALA9701218Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED FROM FRAME TO FRAME AT STA 986.5. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-9.SDR CALA9701215Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 967 TO 986, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-3 AND 51-10-2.SDR CALA9701217Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 312, RBL 56. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 53-10-9, FIGURE 6.SDR CALA9701216Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 947.5 TO 995. THE CORRODED SECTION WAS REMOVED, A REPAIR T-SECTION AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.SDR CALA9700076Hyd Line · chafedTHE A-SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO SHORTLY AFTER TAKEOFF. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 2 A-SYSTEM LOW PRESSURE LIGHT. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUSDR CALA9601643Fuel Pump · failedTHE NR 1 ENGINE FLAMED OUT WHILE CRUISING AT FL 250 EN ROUTE. THE AIRCRAFT WAS DIVERTED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE FUEL PUMP AT FAULT. THE FUEL PUMP WAS REMOVED AND REPLACED, LEAK CHECK WAS GOOD AND ALL PARAMESDR CALA9601317Skin · crackedTHE AIRCRAFT SKIN WAS CRACKED AT C1 DOOR DURING CARGO LOADING. THE CRACK WAS LOCATED AT STA 472.4 BETWEEN STRINGER 20R AND 21R AND MEASURED 1.5 INCH LONG. A REPAIR WAS INSTALLED IAW ECRA 5330-02437.SDR CALA9601105Skin · bulgedINSPECTION FOUND FUSELAGE SKIN BULGED AT STA 259, STRINGER 24L. THE BULGED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9601104Floor Beam · crackedINSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM LOWER T-CHORD AT STA 675, BBL ZERO AND A 2 INCH CRACK WAS ALSO FOUND IN CHORD AT STA 685, BBL ZERO. A REPAIR AT STA 675 WAS PERFORMED IAW BOEING DRAWING 65C17173. A REPAIR ANGLE WAS INSTALLED AT STA 685 IAW ECRA 5SDR CALA9601103Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE WEB AT STA 675, BL ZERO TO LBL 1.5. THE CRACKED WEB AREA WAS REMOVED AND A NEW SECTION OF WEB WAS INSTALLED IAW ECRA 5710-01748.SDR CALA9601106Battery Pack · dischargedINSPECTION FOUND THE R-2 DOOR SLIDE LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED AND THE LANYARD SWITCH WAS CLEANED. THE LIGHT TESTED GOOD IAW MM 33-51-0.SDR CAL960382Hyd Line · chafedFLT NR 1598 - GSO - THE AIRCRAFT LOST 'A' SYSTEM HYDRAULIC QUANTITY AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC SUPPLY LINE IN PYLON CHAFED THROUGH. THE LINE WAS REPLACED AND LEAK CHSDR CAL951017Accessory Unit · inoperativeORF - FLT 1215 - WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO ORF, THE NOSE GEAR INITIALLY INDICATED GREEN, THEN THE RED LIGHT ILLUMINATED AND THE GREEN LIGHT WENT OUT. THE CREW PERFORMED A MANUAL GEAR EXTENSION, BUT THE LIGHT REMAINED RED. THE GEAR WAS CONSDR CAL950996Air Data Comp · inoperativeCLE - FLT 1255 - WHILE CRUISING AT FL 220 EN ROUTE FROM BDL TO CLE AND WITH AUTOPILOT ENGAGED IN 'B' MODE, THE AIRCRAFT MADE AN ABRUPT BANK TO THE RIGHT. THE AUTOPILOT WAS DISCONNECTED AND THE AIRCRAFT FLEW NORMAL FOR REMAINDER OF FLIGHT. THE 'B' AUTOPILOT WSDR CAL950583Skin · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FASTENER STA 727A, S10R. THE CRACKED AREA OF SKIN WAS CUT OUT. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 51-30-2. (X)SDR CAL950582Tear Strap · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN TEAR STRAP AT FASTENER HOLE BELOW STR 14, LT STA 727A. A TEAR STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)SDR CAL950581Stringer · crackedGSO - INSPECTION FOUND .25 INCH CRACKS AT THREE FASTENERS ON BOTTOM ROW OF STR 14R AT STA 727A. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)SDR CAL950580Doubler · crackedGSO - INSPECTION FOUND A .25 INCH CRACK AT UPPER FORWARD FASTENER ON DOUBLER REPAIR AT BS 727A, S17L. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 25, PAGE 87. (X)SDR CAL950579Web · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN CUSP MEMBRANE BETWEEN STATION 616 AND 639L. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-0. (M)SDR CAL950578Stringer Ties · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN EACH OF TWO STRINGER TIES AT STRINGERS 4L AND 4R, STATION 702. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)SDR CAL950577Web · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN CUSP MEMBRANE BETWEEN STATION 638 AND 663L. A WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-0. (M)SDR CAL950576Stringer Ties · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN EACH OF THE STRINGER TIES AT STRINGERS 5R, 2L, 3L, AND 4L, STATION 685. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)SDR CAL950575Stringer Ties · crackedGSO - INSPECTION FOUND STRINGER TIES CRACKED AT STATION 767 STRINGERS 4L AND 5L. THE CRACKS WERE .25 INCH LONG. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-30-2. (M)SDR CAL950573Web · crackedGSO - INSPECTION FOUND A 2 INCH CRACK IN WEB AT BS 947 FORWARD OF R-2 DOOR. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M)SDR CAL950572Tear Strap · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN TEAR STRAP AT FASTENER HOLE RT STATION 752 BELOW STRINGER 14. A NEW TEAR STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (M)SDR CAL950571Angle · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN RT OUTBOARD STIFFENER ANGLE AT STATION 291 TO 294. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-0. (M)SDR CAL950570Stringer Ties · crackedGSO - INSPECTION FOUND STRINGER TIES AT STATION 597 STRINGERS 5R, 4R, AND 4L CRACKED. THE CRACKS WERE .25 INCH LONG. THE STRINGER TIES WERE REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. (M)SDR CAL950569Frame · crackedGSO - INSPECTION FOUND A .75 INCH CRACK THROUGH INBOARD CHORD AND WEB OF STATION 639 FRAME AT STRINGER 16R. A NEW CHORD AND WEB WERE INSTALLED PER BOEING DRAWING 65C31658. (M)SDR CAL950568Skin · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN ON RIGHT SIDE AT STATION 727 BELOW S18. REPAIR DOUBLERS WERE INSTALLED IAW DRAWING 65C28086 AND SERVICE BULLETIN 737-53-1077. (M)SDR CAL950565Skin · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN LEFT FORWARD ENTRY DOOR LOWER FRAME SKIN. THE SKIN WAS REPAIRED IAW ECRA 5330-02294 AND BAC DRAWING 65C27257. (M)SDR CAL950564Rib · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN INBOARD SIDE NR 5 RIB FROM THE FRONT OF THE LEFT HORIZONTAL STABILIZER. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 55-10-4, AND 51-10-1. (M)SDR CAL950562Intercostal · corrodedGSO - INSPECTION FOUND CORROSION ON INTERCOSTAL FLANGE AT STATION 847-867 BELOW STRINGER 24. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2. (M)SDR CAL950561Floor Support · corrodedGSO - INSPECTION FOUND A .75 INCH CRACK IN CABIN FLOOR SUPPORT AND ANGLE AT BS 540, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M)SDR CAL950560Support · corrodedGSO - INSPECTION FOUND CORROSION ON FLOOR SUPPORT PANEL ABOVE S25L BETWEEN BS 887 AND BS 907. A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-30-2. (M)SDR CAL950559Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 400 BETWEEN S20L AND S21L. A NEW FRAME AND FASTENERS WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65C25113-A AND SRM 51-30-2. (M)SDR CAL950558Frame · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN FRAME AT BS 420 BETWEEN S20L AND S21L AND A .5 INCH CRACK IN FRAME AT BS 420 S22L. REPAIR WAS INSTALLED IAW BOEING DRAWING 65C25113A AND SRM 51-30-2. (M)SDR CAL950557Stringer · corrodedGSO - INSPECTION FOUND STRINGER 22R CORRODED AT BS 355. A REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 51-30-2. (M)SDR CAL950556Frame · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN FRAME AT BS 500. A NEW FRAME AND FASTENERS WERE INSTALLED IAW B737 DRAWING 65C25113-A AND SRM 51-30-2. (M)SDR CAL950555Frame · crackedGSO - INSPECTION FOUND THE FRAME AT BS 460 CRACKED BETWEEN S22L AND S21L AND BETWEEN S21L AND S20L. BOTH CRACKS WERE .5 INCH LONG. A NEW FRAME AND SPLICE WERE INSTALLED IAW B737 DRAWING 65C25113-7. (M)
Back to N14241, cancelled Jun 15, 1999