N14337, cancelled Jul 21, 2009
Service difficulty reports · 63
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 = 'N14337' AND deregistration_id = 'N14337-2009-07-21' 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 = 'N14337' AND deregistration_id = 'N14337-2009-07-21' 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 CALA0600269Stiffener · crackedINSPECTION FOUND A CRACK IN THE WING CENTER SECTION REAR SPAR VERTICAL STIFFENER AT LBL AND RBL 6.15. THE VERTICAL STIFFENER WAS REPAIRED IAW ECRA 5714-01018.SDR CALA0600076Stringer · corrodedINSPECTION FOUND STRINGER 27L CORRODED JUST FORWARD OF STA 1016. A REPAIR SECTION WAS INSTALLED IAW SRM 53-00-03.SDR CALA0600075Web · corrodedINSPECTION FOUND AFT PRESSURE BULKHEAD WEB FORWARD FACE CORRODED AT LEFT AND RIGHT CHANNEL, STA 1016, BL 0. A WEB AND CHANNEL REPAIR WAS INSTALLED IAW BOEING DRAWING 65C28106.SDR CALA0600074Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1009, S27L. THE CORRODED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, REPAIR 31.SDR CALA0600072Stringer · corrodedINSPECTION FOUND STRINGER 27L IN FORWARD BAGGAGE BIN CORRODED AT STA 440-460. AN ANGLE REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201, DETAIL VI.SDR CALA0600070Stringer · corrodedINSPECTION FOUND STRINGER 27L CORRODED AT STA 480-500B. A NEW SECTION OF STRINGER WAS SPLICED IN IAW SRM 53-00-03, FIGURE 201.SDR CALA0600065Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME AT STA 616 JUST BELOW MAIN DECK FLOOR, LBL 0 TO LBL 60. REPAIRED FRAME IAW ECRA 5311-01158.SDR CALA0600167Floorbeam · corrodedINSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 277, LBL 19. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED IN IAW ECRA 5310-04464.SDR CALA0600166Floorbeam · corrodedINSPECTION FOUND LEFT O/B EDGE OF FLOORBEAM UPPER CHORD CORRODED AT BS 294.5, LBL 20. THE CORRODED SECTION OF UPPER CHORD WAS REMOVED AND A NEW CHORD WAS SPLICED IN IAW ECRA 5310-04463.SDR CALA0500070Threshold · corrodedINSPECTION FOUND R-1 DOOR THRESHOLD DRAIN FRAME CORRODED AT STA 294-342, BL 0 TO RBL 36. A CHORD WAS INSTALLED IAW SRM 51-40-02 AND DRAWING 55-45875.SDR CALA0500067Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 21, RBL 36, AND RBL 49. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51.SDR CALA0500062Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED IN E&E COMPARTMENT ON RT SIDE ABOVE AIRFONE CONTROL BOX AT STA 312, RBL 21. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51.SDR CALA0500061Floorbeam · crackedINSPECTION FOUND A 1.625 INCH CRACK IN FORWARD GALLEY FLOORBEAM WEB AT STA 312, RBL 18. THE WEB WAS REPAIRED IAW ECRA 5310-04462.SDR CALA0400635Skin · dentedINSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 264 ABOVE S19L. THE SKIN WAS REPAIRED IAW ECRA 5330-03366. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR IAW PART III WITHIN 50 FLIGHT CYCLES.SDR CALA0400480Floorbeam · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 540, RBL 48. THE FLOORBEAM WAS REPAIRED IAW ECRA 5331-01146.SDR CALA0400476Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON ANGLE JUST AFT OF I/B MIDSPAR ATTACH BOLT. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00.SDR CALA0400464Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN ANGLE FOR RIGHT RAM AIR INLET AT BS 540, S22R. THE CRACKED SECTION WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 51-70-11.SDR CALA0400461Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LEFT WING L/E NR 3 SLAT ACTUATOR CUTOUT. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-40-01, FIGURE 201, PROCEDURE 2.SDR CALA0400447Seat Track · brokenTHE RIGHT I/B SEAT TRACK UPPER LOBE BROKE DURING REMOVAL AT STA 827. A SEAT TRACK REPAIR SECTION WAS INSTALLED IAW SRM 53-00-52.SDR CALA0400444Seat Track · brokenTHE RIGHT O/B SEAT TRACK UPPER LOBE BROKE DURING SEAT REMOVAL AT STA 887, RBL 34. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, FIGURE 204.SDR CALA0400413Charger · inoperativeTHREE EMERGENCY LIGHTS OVER EMERGENCY ESCAPE HATCH ARE INOP. REPLACED BATTERY CHARGERS AND BATTERIES PER MM 33-51-51.SDR CALA0200127Skin · crackedINSPECTION FOUND TWO INCH CRACKS AT THE EDGES OF THREE LIGHTENING HOLES IN C-2 DOOR INNER SKIN OVER CENTER BALANCE SPRINGS. A 1" CRACK WAS FOUND AT THE EDGE OF A LIGHTENING HOLE IN C-2 DOOR INNER SKIN AT PULLEY ACCESS PANEL. REPAIR DOUBLERS WERE INSTALLED IAW SDR CALA0200126Skin · crackedINSPECTION FOUND A 1" CRACK IN CAPTAIN'S WINDSHIELD O/B POST OUTER SKIN AT UPPER CORNER. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-01104.SDR CALA0200125Skin · crackedINSPECTION FOUND A 1.25" CRACK IN C-2 DOOR INNER SKIN AT AFT LOWER CORNER. THE SKIN WAS REPAIRED IAW ECRA 5230-01650.SDR CALA0200124Web · crackedINSPECTION FOUND A 1/2" CRACK IN WEB AT LIGHTENING HOLE AFT OF STA 1040 AND I/B OF TAIL COMPARTMENT ACCESS. A REPAIR WAS INSTALLED IAW ECRA 5320-01768.SDR CALA0200122Spar Cap · crackedINSPECTION FOUND A 1/2" CRACK AT HOLE IN SPAR CAP AT R/H WING MLG BEAM ATTACH FITTING. REPAIRED IAW ECRA 5740-02000. THE ITEM WAS PLACED ON DIP TO PERFORM AN HFEC INSPECTION ON THE R/H WING REAR SPAR AT MLG BEAM ATTACH FITTING AT THE LOCATION REFERENCED IN ECRSDR CALA0200118Skin · crackedINSPECTION FOUND A 3" CRACK IN R/H HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR JUST I/B OF #4 ELEVATOR HINGE. A PERMANENT REPAIR DOUBLER WAS INSTALLED IAW ECRA 5510-01584.SDR CALA0200117Web · wornINSPECTION FOUND C-1 AFT DOOR JAMB LOWER WEB WORN AROUND EDGES. A NEW WEB WAS INSTALLED IAW SRM 51-70-13.SDR CALA0200116Keelbeam · chafedINSPECTION FOUND LT AFT UPPER SURFACE OF KEEL BEAM FLANGE HAD WORN HOLES ON UPPER SURFACE FROM PANEL ATTACH NUTS AT STA 719-727. REPAIRED IAW ECRA 5310-03740.SDR CALA0200115Skin · crackedINSPECTION FOUND A 4" CRACK IN #4 L/E SLAT PANEL AT O/B ACTUATOR. REPAIRED IAW SRM 57-43-01.SDR CALA0200108Strap · corrodedINSPECTION FOUND FLOOR H-STRAP CORRODED AT STA 1022-1026, LBL 3. A NEW H-STRAP WAS INSTALLED IAW SRM 51-10-2 AND 51-30-3.SDR CALA0200107Skin · wornINSPECTION FOUND UPPER FUSELAGE SKIN WORN AT STA 867, RBL 6. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 214.SDR CALA0200099Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ABOVE AND BELOW NUT CLIP HOLES AT STA 986, RBL 46 TO LBL 46. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03851.SDR CALA0200096Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN CABIN FLOOR SUPPORT AT STA 578, BBL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-2.SDR CALA0200095Collar · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 FLAP FAIRING HORSE COLLAR. A NEW COLLAR WAS INSTALLED IAW SRM 51-10-2.SDR CALA0200094Skin · crackedINSPECTION FOUND A 1/2" CRACK IN R/H WING #6 FLAP FAIRING LOWER SKIN WITH RIVETS PULLING THROUGH. A STIFFENER WAS INSTALLED IAW SRM 51-10-2.SDR CALA0200093Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1006-1016, LBL 7 AND RBL 7. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-02-01.SDR CALA0200092Floor Support · corrodedINSPECTION FOUND A RT AND LT LAV FLOOR SUPPORT CORRODED AT STA 994, RBL 14 TO RBL 44, AND LBL 14 TO LBL 44. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0200091Floor Support · corrodedINSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT STA 986-1006. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0200090Web · crackedINSPECTION FOUND A 1/2" CRACK IN WEB AT STA 270, S14R. A WEB INTERCOSTAL WAS INSTALLED IAW SRM 51-10-02.SDR CALA0200088Stringer · crackedINSPECTION FOUND A 1" CRACK IN STRINGER 16L AFT OF STA 500C. REPAIRED STRINGER IAW SRM 53-00-03, FIGURE 201.SDR CALA0200087Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 663.75, LBL 65. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0200086Angle · corrodedINSPECTION FOUND Z-ANGLE CORRODED AT L-2 DOOR JAMB, STA 927. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-05.SDR CALA0200084Floor Support · crackedINSPECTION FOUND A 2 INCH CRACK IN AC BAY FLOOR SUPPORT AT STA 559, RBL 24, IN FORWARD BAGGAGE BIN. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0200081Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 1016, RBL 37 TO LBL 37. THE FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851.SDR CALA0200080Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AROUND NUT CLIP HOLES AT STA 967, LBL 50 TO RBL 50 AND AT RBL 18 TO LBL 18. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 202.SDR CALA0200079Angle · crackedINSPECTION FOUND A 3" CRACK IN ANGLE AT STA 927-947, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-03.SDR CALA0200078Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 951, LBL 14 TO LBL 16 AND AT LBL 18 TO LBL 24. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0200077Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 967-986, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0200076Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 947-967, LBL 18 AND RBL 18. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
Back to N14337, cancelled Jul 21, 2009