N12230, cancelled Jul 22, 1999
Service difficulty reports · 53
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 = 'N12230' AND deregistration_id = 'N12230-1999-07-22' 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 = 'N12230' AND deregistration_id = 'N12230-1999-07-22' 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 CALA9801229Angle · crackedINSPECTION FOUND A 5 INCH CRACK IN FLOOR SUPPORT ANGLE AT STA 648-767, RBL 45. THE CRACKED AREA WAS CUT OUT. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND MM 51-20-11.SDR CALA9800854Wire · brokenESCAPE PATH LIGHT INOP AT ROW 24. BROKEN WIRE AND MISSING LENS. REPAIRED LIGHT SOCKET WIRE AND REPLACED LENS SET PER MM 33-51-5.SDR CALA9601704Fuel Pump · inoperativeTHE NR 2 ENGINE FLAMED OUT DURING CLIMB AT 900 FEET AGL. THE AIRCRAFT WAS RETURNED TO CHS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE FUEL PUMP AT FAULT. THE FUEL PUMP WAS REMOVED AND REPLACED IAW MM 73-11-1. A POWER ASSURANCE RUN WSDR CALA9601382Hyd Line · crackedTHE A-HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE ON APPROACH. THE A-SYSTEM HYDRAULIC QUANTITY LOSS CHECKLIST WAS COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 SLAT ACTUATOR HYDRAULIC PRESSURE LINE CRACKED AT B-BUT. THE LISDR CALA9601320Hyd Line · crackedTHE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY UPON LANDING. THE AIRCRAFT STOPPED SAFELY AND WAS TOWED TO THE GATE. MAINTENANCE FOUND HYDRAULIC LINE JUST OUTBOARD OF NR 2 SLAT ACTUATOR CRACKED. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO RSDR CALA9600806Fire Loop · burnedTHE APU FIRE WARNING LIGHT BEGAN TO FLASH INTERMITTENTLY APPROXIMATELY FIVE MINUTES INTO THE FLIGHT WITH THE APU SHUT DOWN. THE APU FIRE HANDLE WAS PULLED AND THE FIRE LIGHT FLASHING CEASED AFTER 45 SECONDS. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WSDR CALA9600689Frame · crackedINSPECTION FOUND A 1 INCH AND 1.5 INCH CRACK IN FRAME AT STA 480 BETWEEN STRINGER 22L AND 23L. THE CRACKED FRAME SECTION WAS REMOVED, A NEW FRAME SECTION WAS FABRICATED AND INSTALLED IAW BOEING DRAWING NR 65C25113.SDR CALA9600721Frame · crackedINSPECTION FOUND TWO, .5 INCH CRACKS IN FRAME AT BS 328 BETWEEN STRINGER 2OR AND 21R. THE CRACKED AREAS WERE REMOVED, FILLER AND REPAIR PLATES WERE FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-2.SDR CALA9600720Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 328, STRINGER 26L. THE CRACKED AREA WAS REMOVED AND A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-40-3 AND 51-30-2.SDR CALA9600719Frame · crackedINSPECTION FOUND TWO 1 INCH CRACKS AT NUTPLATE HOLES OF FRAME AT BS 440, LT SIDE. THE FRAME WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113.SDR CALA9600718Frame · crackedINSPECTION FOUND A 2 INCH CRACK AT NUTPLATE HOLE OF FRAME, BS 420, STRINGER 22L. THE FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113.SDR CALA9600706Frame · crackedINSPECTION FOUND A 1.5 CRACK AT NUTPLATE HOLE OF FRAME, BS 500A, RT SIDE. THE FRAME SEGMENT WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW BOEING DRAWING 65C25113.SDR CALA9600704Floorbeam · crackedINSPECTION FOUND A .75 CRACK IN FLOORBEAM AT STA 676, RBL 24. THE BEAM WAS REPAIRED IAW EA 5710-01638.SDR CALA9600700Frame · crackedINSPECTION FOUND A 1 INCH CRACK AT TWO NUTPLATE LOCATIONS ON FRAME AT BS 500, RT SIDE. THE CRACKED FRAME SEGMENT WAS REMOVED AND REPLACED IAW BOEING DRAWING 65C25113.SDR CALA9600698Splice · crackedINSPECTION FOUND A 1.5 INCH CRACK IN STRINGER SPLICE AT STA 360, STRINGER 21R. THE SPLICE WAS REMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 53-30-2.SDR CALA9600695Skin · crackedINSPECTION FOUND SEVERAL CRACKS IN SECTION 41 FUSELAGE SKIN ON LT SIDE, BS 188 TO 251, WL 207 TO 234. THE CRACKS RANGED FROM .125 INCH TO .25 INCH IN LENGTH. THE CRACKED AREAS WERE CUT OUT, FILLERS AND DOUBLERS WERE FABRICATED AND INSTALLED IAW EA 5310-01188SDR CALA9600694Stringer · crackedINSPECTION FOUND A .5 INCH CRACK AND CORROSION AT FASTENER HOLE OF STRINGER 26L, BS 323. THE CRACKED STRINGER WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-30-5 AND 51-10-2.SDR CALA9600688Stringer · corrodedINSPECTION FOUND STRINGER 22L CORRODED AT STA 727. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SPLICE ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.SDR CALA9600693Angle · corrodedINSPECTION FOUND FRAME UPPER L-ANGLE AND WEB CORRODED AT BS 259, RT SIDE. THE L-ANGLE AND WEB WERE REMOVED AND REPLACED IAW SRM 51-40-2, 51-40-4, 51-30-2, 51-10-6 AND 51-10-2.SDR CALA9600723Frame · crackedINSPECTION FOUND TWO, .75 INCH CRACKS IN FRAME AT BS 500B BETWEEN STRINGERS 22R AND 24R. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW BOEING DRAWING 65C25113.SDR CALA9600715Skin · delaminatedINSPECTION FOUND THE LT WING AILERON TAB SKIN DELAMINATING. THE DELAMINATED AREA WAS REMOVED AND A FIBERGLASS OVERLAY REPAIR WAS INSTALLED IAW SRM 51-40-9.SDR CALA9600714Skin · damagedINSPECTION FOUND IMPACT DAMAGE TO FORWARD CARGO DOOR OUTER SKIN. THE DAMAGED AREA WAS REMOVED AND A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3.SDR CALA9600717Stringer · corrodedINSPECTION FOUND CHORD CORRODED AT STA 294 TO 335, STRINGER 26R. THE CHORD SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-0.SDR CALA9600705Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK EXTENDING FROM RIVET OF FLOORBEAM AT STA 707, BBL 0. A REPAIR WAS INSTALLED IAW EA 5710-01322.SDR CALA9600709Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 887, STRINGER 25R. THE DENTED AREA OF SKIN WAS CUT OUT, A SKIN SECTION AND SPLICE DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.SDR CALA9600708Skin · puncturedINSPECTION FOUND A HOLE IN FUSELAGE SKIN AFT OF AFT CARGO DOOR. A FILLER AND DOUBLER SMALL FLUSH REPAIR WAS INSTALLED IAW SRM 53-30-3.SDR CALA9600707Skin · dentedINSPECTION FOUND A DENT IN RT WING LEADING EDGE SKIN JUST OUTBOARD OF LANDING LIGHT. THE DENTED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-1 AND 51-30-2.SDR CALA9600701Frame · crackedINSPECTION FOUND A .75 CRACK IN FRAME AT RT SIDE OF E AND E DOOR CUTOUT. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 57-40-3.SDR CALA9600697Beam · crackedINSPECTION FOUND VERTICAL BEAM CRACKED IN HALF AT BS 540, RBL 24.8. THE BEAM WAS REMOVED AND A NEW BEAM WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-2.SDR CALA9600722Bulkhead Web · crackedINSPECTION FOUND A 7 INCH CRACK IN BULKHEAD PRESSURE WEB AT STA 664, RBL 30. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9600713Stringer · corrodedINSPECTION FOUND STRINGER 23R CORRODED AT STA 355. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS INSTALLED IAW SRM 53-10-3.SDR CALA9600712Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 400 LOWER LOBE. THE CRACKED AREA WAS REMOVED, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2.SDR CALA9600711Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED AT STA 360 TO 420. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND 51-30-5.SDR CALA9600710Stringer · corrodedINSPECTION FOUND STRINGER 20R CORRODED AT STA 383. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.SDR CALA9600702Skin · crackedINSPECTION FOUND A 1.33 CRACK AT FASTENER HOLE IN AFT CARGO DOOR FRAME AFT SKIN. THE CRACKED AREA WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2.SDR CALA9600699Frame · crackedINSPECTION FOUND A 3 INCH CRACK AT NUTPLATE HOLE OF FRAME AT BS 500, LT SIDE. THE CRACKED FRAME SECTION WAS REMOVED AND A NEW FRAME SEGMENT WAS SPLICED IN IAW BOEING DRAWING 65C25113.SDR CALA9600696Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL BETWEEN STA 500 AND 500A, STRINGER 26L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW BOEING DRAWING 69-41473.SDR CALA9600691Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 500A BELOW WINDOW BELT ON BOTH LEFT AND RIGHT HAND SIDE OF FUSELAGE. BOTH AREAS WERE REPAIRED IAW SRM 53-30-3.SDR CALA9600690Skin · corrodedINSPECTION FOUND FUSELAGE SKIN AND FRAME SHEAR TIES CORRODED AT STA 328, STRINGER 18R. THE CORRODED AREAS OF SKIN AND SHEAR TIES WERE CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, SHEAR TIES WERE FABRICATED AND INSTALLED IAW SRM SDR CALA9600716Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1040. THE DENTED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.SDR CALA9600703Skin · dentedINSPECTION FOUND A DENT IN RT FUSELAGE AT STA 1040. THE DENTED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.SDR CALA9600692Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK AT FASTENER HOLE OF L-1 DOOR LOWER SKIN. THE CRACKED SKIN WAS REMOVED, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3 AND 51-30-2.SDR CALA9600687Skin · dentedINSPECTION FOUND SKIN DENTED FROM STA 360 TO 447 RT SIDE, STRINGER 19R TO 25R. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CALA9600686Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED FROM STA 259 TO 360, STRINGER 19R TO 24R. THE SKIN WAS REMOVED AND REPLACED IAW SRM 51-30-2.SDR CAL960453Connector · shortedCAE - FLT 1598 - THE NR 1 ENGINE FIRE LIGHT FLICKERED OFF AND ON AND THEN THE FIRE LIGHT AND BELL CAME ON STEADY WHILE EN ROUTE FROM TPA TO GSO. THE NR 1 ENGINE WAS SHUT DOWN. ONE FIRE BOTTLE WAS DISCHARGED, BUT THE LIGHT REMAINED ON. THE SECOND FIRE BOTTLESDR CAL960309Wire · shortedFLT NR 1087 - EWR - THE CREW NOTICED APPROXIMATELY ONE THIRD OF THE EMERGENCY PATH LIGHTING SYSTEM WAS INOPERATIVE AFTER LOSING GROUND POWER. MAINTENANCE FOUND SHORTED WIRING BY ROW 4 WITH ASSOCIATED FUSES BLOWN. THE WIRING WAS REPAIRED AND THE FUSES WERE RESDR CAL960280Hyd Line · leakingFLT NR 512 - EWR - THE 'B' HYD SYSTEM WAS LOST AFTER TAKEOFF FROM EWR. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF SYSTEM 'B' LOW PRESSURE LIGHTS. THE 'B' SYSTEM PUMPS WERE TURNED OFF AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MASDR CAL950944Overheat Light · illuminatedFLT NR 1444 - EWR - AIRCRAFT INBOUND, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATES WITH THROTTLE ADVANCE. RETURNED TO BASE. MAINTENANCE REPLACED CONNECTOR AND ELEMENTS. (M)SDR CAL950765Prox Sensor · inoperativeFLT NR 1580 - GSO - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM GSO. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR/GROUND PROXIMITY SENSOR AT FAULT. THE SENSOR WAS REPLACED AND GEAR RETRACTION WAS NORSDR CAL950749Stringer · corrodedMIA - INSPECTION FOUND CORROSION ON STRINGER 27L FROM STATION 947.5 TO 967. A STRINGER SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-3. (M)
Back to N12230, cancelled Jul 22, 1999