N12349, cancelled Dec 31, 2008
Service difficulty reports · 46
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 = 'N12349' AND deregistration_id = 'N12349-2008-12-31' 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 = 'N12349' AND deregistration_id = 'N12349-2008-12-31' 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 CALA0800636Charger · faultyROWS 12 - 20 EMERGENCY SEAT LIGHTS INOPERATIVE. FOUND CHARGER PART NUMBER RPS1-B AT FAULT, LOCATED IN CEILING CENTER AREA BETWEEN AFT GALLEYS. REMOVED AND REPLACED BATTERY CHARGER PER AMM 33-51-51. OPERATIONAL CHECKS GOOD.SDR CALA0600182Skin · crackedINSPECTION FOUND A 0.58 INCH CRACK IN FORWARD CARGO DOOR INNER SKIN AROUND FORWARD LIGHTENING CUTOUTS SPRING COMPARTMENT. A REPAIR WAS INSTALLED IAW ECRA 5232-01075.SDR CALA0600181Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT STA 294, S12L FORWARD OF L-1 DOOR. A REPAIR WAS INSTALLED IAW ECRA 5310-04535.SDR CALA0600180Stringer Splice · crackedINSPECTION FOUND A .75 INCH CRACK IN STRINGER SPLICE CHANNEL AT STA 360, S14L AFT OF L-1 DOOR. A REPAIR WAS INSTALLED IAW ECRA 5310-04535.SDR CALA0600179Pan · crackedINSPECTION FOUND A 0.8 INCH CRACK IN C-2 DOOR PAN AT FORWARD MID SECTION. THE DOOR PAN WAS REPAIRED IAW SRM 51-40-02.SDR CALA0600176Fitting · crackedINSPECTION FOUND A 5 INCH CRACK IN HORIZONTAL STABILIZER CENTER SECTION -X- BRACE RT FORWARD LOWER CORNER FITTING. THE FITTING WAS REPLACED IAW SRM 51-40-02.SDR CALA0600172Beltframe · corrodedAFT CARGO COMPARTMENT BELT FRAME STA 794, S25R - S22R, LOWER SIDE AT C-2 DOOR CUTOUT, STRAP AND REPAIR DOUBLER HAVE SOME CORROSION BY NUT PLATES. REPAIRED BELT FRAME IAW SRM 53-60-53.SDR CALA0600171Pan · crackedINSPECTION FOUND A .75 INCH CRACK IN C-1 DOOR PAN LOWER FORWARD CORNER NEXT TO UPLATCH HOOK, STA 440-500, S17R TO S27R. THE PAN WAS REMOVED AND A NEW PAN WAS INSTALLED IAW SRM 51-10-02, STEP 8 AND SRM 51-40-02, STEP 4 AND 5.SDR CALA0600168Keelbeam · crackedINSPECTION FOUND A 1 INCH CRACK IN LT KEEL BEAM AT STA 540, S29L. THE KEEL BEAM WAS REPAIRED IAW SRM 53-60-12, FIGURE 201, PAGE 205.SDR CALA0600165Stiffener · corrodedINSPECTION FOUND RT CHANNEL STIFFENER CORRODED AT LOWER APB STA 1016, RBL 1. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW BOEING DRAWING 65C28106 AND EA 5310-04045, REV A, OPS 2.SDR CALA0600161Bulkhead · corrodedINSPECTION FOUND FORWARD SIDE OF AFT PRESSURE BULKHEAD CORRODED AT STA 1014 BETWEEN S27R AND S27L. THE AREA WAS REPAIRED IAW SRM 51-40-02.SDR CALA0600160Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 4 TO LBL 36. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-51.SDR CALA0600156Seat Track · corrodedINSPECTION FOUND THE LEFT I/B SEAT TRACK CORRODED AT STA 907 TO 947.5, LBL 25. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0600155Frame · crackedINSPECTION FOUND A .25 INCH CRACK IN LEFT MAIN FRAME BELOW MAIN DECK AT STA 616, LBL 60 TO LBL 61. THE MAIN FRAME WAS REPAIRED IAW ECRA 5311-01158.SDR CALA00128Sensor · intermittentLANDING GEAR UNSAFE LIGHT CAME ON THEN INTERMITTENT AFTER LEVEL AT FL35. REPLACED NLG SENSOR PER AMM 32-61-51.SDR CALA0400640Access Panel · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 ENGINE PYLON ACCESS PANEL NR 5724 CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.SDR CALA0400636Seat Track · crackedINSPECTION FOUND A .5 INCH CRACK IN LT OB SEAT TRACK, OB FLANGE AT STA 727B. A REPAIR WAS INSTALLED IAW ECRA 5321-01202.SDR CALA0400552Charger · inoperativeTHE EMERGENCY EXIT SIGN AT L-2 DOOR WAS FOUND FLICKERING ON AND OFF. THE BATTERY CHARGER AND BATTERY PACK AT L-2 DOOR WERE REMOVED AND REPLACED IAW MM 33-51-51, PAGES 201-207. AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT WAS GOOD.SDR CALA2000266Spoiler#3 SPOILER DENTED AND CRACKED .75X.75 INCHES JUST FWD AND OB OF ACTUATOR ATTACH POINT. INSTALLED DOUBLER PER SRM 57-70-01, FIG 204.SDR CALA0200242Web · corrodedINSPECTION FOUND AFT CARGO DOOR CUTOUT THRESHOLD WEB CORRODED AT STA 793-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0200239Web · corrodedINSPECTION FOUND CORROSION UNDER FLANGE OF VERTICAL THRESHOLD WEB AT AFT BAGGAGE BIN DOORWAY FROM STA 767-847. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0200232Channel · corrodedINSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 794, LBL 3 AND RBL 3. CHANNEL BEAM REPAIRS WERE INSTALLED AT EACH LOCATION IAW SRM 53-00-53, FIGURE 201.SDR CALA0200231Channel · corrodedINSPECTION FOUND CHANNEL CORRODED IN AFT BAGGAGE BIN AT STA 794, RBL 8. REPAIRED IAW SRM 53-00-53.SDR CALA0200230Channel · corrodedINSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5" RBL 3. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603.SDR CALA0200229Channel · corrodedINSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNELS CORRODED AT STA 727D+5", RBL 8 AND LBL 8. REPAIR ANGLES WERE INSTALLED AT EACH LOCATION IAW ECRA 5320-01603.SDR CALA0200228Floor Support · corrodedINSPECTION FOUND AFT BAGGAGE BIN FLOOR SUPPORT CHANNEL CORRODED AT STA 727D+5, LBL 12. A REPAIR ANGLE WAS INSTALLED IAW ECRA 5320-01603.SDR CALA0200224Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 294-312, RBL 15. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0200223Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM UPPER CAP CORRODED AT STA 312. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-10-51.SDR CALA0200219Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER T CAP CORRODED AT FASTENER HOLES, STA 294.5, LBL 20 TO RBL 58. REPAIRED IAW SRM 53-10-51.SDR CALA0200217Web · crackedINSPECTION FOUND A 3" CRACK IN WEB AT R/H SIDEWALL FLOOR BETWEEN STA 559 AND 578. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02.SDR CALA0200216Floorbeam · corrodedINSPECTION FOUND FLOORBEAM T-CAP CORRODED AT FASTENER HOLES, STA 344. REPAIRED IAW SRM 51-10-51.SDR CALA0200212Stringer · crackedINSPECTION FOUND A 1/2" CRACK IN STRINGER 16L JUST FORWARD OF WING ILLUMINATION LIGHT HOUSING AT STA 500C. A NEW STRINGER WAS INSTALLED IAW SRM 53-30-03 AND 53-00-03.SDR CALA0200211Mount · corrodedINSPECTION FOUND AFT O/B LAV MOUNT CORRODED AT STA 1012, LBL 38. THE LAV MOUNT WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0200210Channel · corrodedINSPECTION FOUND AFT O/B CHANNEL OF WEB CORRODED AT STA 986.5-1006, LBL 38. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0200206Stringer · corrodedINSPECTION FOUND STRINGER 26R CORRODED BETWEEN STA 1006 AND 1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0001321Skin · crackedINSPECTION FOUND A 0.4 INCH CRACK IN ABB DOOR INTERIOR SKIN AT LIGHTENING HOLE EDGE. THE EXISTING REPAIR DOUBLERS WERE REMOVED AND A NEW SINGLE DOUBLER REPAIR WAS INSTALLED IAW ECRA 5230-01571.SDR CALA0001320Skin · gougedINSPECTION FOUND AFT BAGGAGE BIN DOOR EXTERIOR SKIN GOUGED. THE SKIN WAS REMOVED AND NEW SKIN WAS INSTALLED IAW SRM 51-40-02.SDR CALA9801163Channel · corrodedINSPECTION FOUND R-1 DOOR Z-CHANNEL CORRODED AT STA 294-328. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA9801161Panel · corrodedINSPECTION FOUND RT TRANSITION PANEL CORRODED AT STA 847-867. THE TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA9801158Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT FS 328-344. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 53-00-52.SDR CALA9801147Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CAP IN FORWARD GALLEY AREA CORRODED AT FS 294.5, RBL 8. THE FLOORBEAM CAP WAS REPAIRED IAW SRM 53-10-51.SDR CALA9801146Floor Track · corrodedINSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 294.5. THE FLOOR TRACK WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 53-00-52.SDR CALA9701804Corroded · corrodedINSPECTION FOUND CORROSION ON FLOORBEAM/TRACK TIEDOWN IN AFT PIT AT STA 947, LBBL 17.2. A NEW TRACK TIEDOWN WAS SPLICED IN IAW SRM 53-00-53, FIGURE 202.SDR CALA9600794Light · inoperativeTHE L-2 DOOR EMERGENCY SLIDE EXIT LIGHT WAS FOUND INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED.SDR CAL960385Nose Link · brokenEWR - FLT 0725 - THE NR 2 LEADING EDGE FLAP TRANSIT LIGHT ON OVERHEAD PANEL AND FORWARD PANEL LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED WITH THE FLAPS RETRACTED WHILE IN CLIMB. THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE NR 2 KRUGER FLAP NOSE LSDR CAL950948O-Rings · cutGSO - FLT 0171 - THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WHILE ON FINAL APPROACH TO GSO. THE NR 2 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY MEASURE. THE CREW REPORTED LOSING LESS THAN 8.5 PSI OIL PRESSURE. MAINTENANCE FOUND THE NR 2 ENGINE ANGLE GE
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