N37077, cancelled Nov 4, 2005
Service difficulty reports · 42
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 = 'N37077' AND deregistration_id = 'N37077-2005-11-04' 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 = 'N37077' AND deregistration_id = 'N37077-2005-11-04' 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 CALA0100048Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED IN PASSENGER CABIN AT STA 495, LT SIDE. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-31-01.SDR CALA0100047Floor Support · corrodedINSPECTION FOUND TRANSVERSAL SUPPORT UNDER FLOOR PANEL 244AF IN MID PASSENGER CABIN CORRODED AT STA 816. REPLACED SUPPORT IAW SRM 51-31-01.SDR CALA0100036Frame · crackedINSPECTION FOUND A 0.8 INCH CRACK IN FRAME AT STA 1841 IN CENTER CARGO AREA. REPAIRED IAW SRM 53-00-01, FIGURE 4, SHEET 2.SDR CALA0100035Floor Support · corrodedINSPECTION FOUND LEFT O/B GALLEY FLOOR SUPPORT CORRODED IN MID PASSENGER CABIN, STA 824 - 840. THE SUPPORT WAS REPLACED IAW SRM 51-31-01.SDR CALA0100034Floor Support · corrodedINSPECTION FOUND AFT PASSENGER CABIN RT SUPPORT IN CENTER LAV CORRODED. THE SUPPORT WAS REPLACED IAW SRM 51-31-01.SDR CALA0100033Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT LT MID PASSENGER CABIN, STA 857 - 899. A NEW FLOORBEAM WAS INSTALLED IAW SRM 51-31-01.SDR CALA0100028Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN CENTER CARGO FRAME AT STA 1841. REPAIRED IAW SRM 53-00-01, FIGURE 4, SHEET 2.SDR CALA0100027Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING I/B BRACKET AT I/B SIDE PANEL. A NEW BRACKET WAS INSTALLED IAW ECRA 5730-01741.SDR CALA9900100Elevator · damagedINSPECTION FOUND IMPACT DAMAGE TO RT ELEVATOR TIP CAUSED BY HANGAR DOOR. A NEW ELEVATOR WAS INSTALLED IAW MM 27-30-09, PAGE 401. ELEVATOR OPERATION CHECKED GOOD IAW MM 27-30-03, PAGE 601.SDR CALA9900099Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE DROOP PANEL UPPER SKIN. TWO RIBS WERE REMOVED AND REPLACED. THE SKIN WAS REINFORCED WITH DOUBLER AND INSTALLED IAW SRM 57-10-00, FIGURE 55, 51-21-01, AND 51-31-01.SDR CALA9900098Rib · crackedINSPECTION FOUND A .25 INCH CRACK IN NR 1 SLAT RIB. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-31-01.SDR CALA9900090Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED IN MAIN DECK AT STA 1871 NEAR LAV E. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 53-70-00, 51-21-01, AND 51-31-01.SDR CALA9800101Hyd Pump · leakingTHE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT CAME ON JUST PRIOR TO LANDING AT LGW. THE ELEVATOR FEEL CHANNEL LIGHT CAME ON AFTER LANDING. THE AIRCRAFT HAD LOST FLUID FROM THE NR 3 HYDRAULIC SYSTEM. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN RIGHT HYDRAULIC PUMP SDR CALA9700336Relay · inoperativeTHE GROUND REFUEL POWER, FUEL TANK FILL VALVE, AND BATTERY BUS SENSING CIRCUIT BREAKERS POPPED WHILE EN ROUTE FROM FCO TO EWR. THE BATTERY BUS OFF LIGHT ILLUMINATED AND THE FUEL FILL VALVES CLOSED. FUEL COULD NOT BE TRANSFERRED. THE AIRCRAFT WAS DIVERTED TO LSDR CALA9700105Skin · crackedINSPECTION FOUND RT DOOR ACCESS CUTOUT SKIN CRACKED AT STA 1308.5 AND STA 1255. BOTH CRACKS WERE 1 INCH LONG. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 4 AND SRM 51-35-01.SDR CALA9700104Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT BS 1986 LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01 FIGURE 1.SDR CALA9700161Support · corrodedINSPECTION FOUND T-ANGLE FLOOR SUPPORT CORRODED IN FORWARD CARGO COMPARTMENT AT STA 1099, RBL 20. THE CORRODED AREA WAS CUT OUT, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-00-01, PAGE 8 AND 51-21-01.SDR CALA9700162Hinge Angle · crackedINSPECTION FOUND A 5.5 INCH CRACK IN UPPER RADIUS OF LOWER AFT FAIRING 535JL INBOARD HINGE AT OUTBOARD LT FLAP INBOARD FACE. THE FAIRING WAS REMOVED AND THE CORRODED AREA OF SKIN WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW DRAWING SKB 02SDR CALA9700106Slat · gougedINSPECTION FOUND RT NR 6 SLAT CHAFED AND GOUGED AT INBOARD END, 12 INCHES UP FROM L/E TIP. THE SLAT WAS REPAIRED IAW ECRA 5750-02573.SDR CALA9700107Support · corrodedINSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT STA 472 LBL 54. A FLOOR SUPPORT REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, 51-21-01, 51-31-01, 51-35-01 AND 53-60-01 FIGURE 1.SDR CALA9601868Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED STA 1509-1521, XCW 25 TO XCW -25. SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5330-02465 AND SRM 51-31-01.SDR CALA9601870Doubler · crackedINSPECTION FOUND BOTH INBOARD AND OUTBOARD FORWARD UPPER ATTACH DOUBLERS OF NR 3 PYLON AFT FAIRING 489AL CRACKED THROUGH. THE CRACKED DOUBLERS WERE REMOVED IAW SRM 51-30-01. NEW DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM'S 51-21-01, 51-31-01, AND 53-00-0SDR CALA9601852Support · corrodedINSPECTION FOUND THE UPPER HORIZONTAL SURFACE OF FORWARD END FLOOR SUPPORT CORRODED AT STA 1900, RBL 57. THE CORRODED SECTION WAS REMOVED, A NEW SECTION WAS SPLICED IN IAW SRM 53-70-00, FIGURE 13.SDR CALA9601869Skin · crackedINSPECTION FOUND A .50 INCH CRACK ON LT AND RT CORNERS OF NR 3 ENGINE PYLON FORWARD END. THE CRACKED AREAS WERE CUT OUT. TWO EACH DOUBLERS, FILLERS, AND TRIPLERS WERE FABRICATED AND INSTALLED IAW SRM 54-00-01, FIGURE 2A.SDR CALA9601866Skin · dentedINSPECTION FOUND THE RT WING NR 4 SLAT DENTED AT XORS 480. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 12.SDR CALA9601865Skin · gougedINSPECTION FOUND FUSELAGE SKIN GOUGED IN TWO PLACES AT STRINGER 48R, B.S. 1581 AND 1585. THE GOUGES WERE REMOVED IAW SRM 53-00-01, FIGURE 1. TWO DOUBLERS, FILLER, AND A FINGER DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6.SDR CALA9601854Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1986, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.SDR CALA9601853Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AROUND FLOOR PANEL ATTACH HOLES FROM BS 1986 TO 2007, RBL 27. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-60-01 FIGURE 1, 51-31-01 AND 51-20-01.SDR CALA9601851Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1963, LBL 27. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.SDR CALA9601848Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1882, LBL 36. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-21-01, 51-31-01 AND 53-60-01, FIGURE 1.SDR CALA9601856Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 457, RBL 29. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-35-01 AND 53-11-01, FIGURE 1A.SDR CALA9601874Skin · crackedTHE LT WING FIXED LEADING EDGE SKIN HAD A 2.5 INCH CRACK FROM LOWER EDGE RUNNING FORWARD AT APPROXIMATELY XORS 810. THE CRACKED AREA WAS REMOVED. DOUBLER, FILLERS, AND FASTENERS WERE INSTALLED IAW SRM 57-00-01.SDR CALA9601873Skin · dentedINSPECTION FOUND LT WING NR 1 LEADING EDGE SLAT DENTED ON LEADING EDGE NOSE STARTING 30 INCHES OUTBOARD OF XFS 145. THE DENTED AREA WAS CUT OUT AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, FIGURE 43.SDR CALA9601864Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1308.5, AT CABIN FLOOR. THE SKIN WAS REPAIRED BY FABRICATING AND INSTALLING A DOUBLER IAW SRM'S 51-21-01 AND 53-00-01, FIGURE 4.SDR CALA9601863Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN INNER SKIN AT RT DOOR CUT-OUT SURROUNDING FRAME STRUCTURE, STA 1255, AT CABIN FLOOR. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-01, FIGURE 4, SRM 51-21-01, AND 51-35-01.SDR CALA9700163Clip · corrodedINSPECTION FOUND CLIP FROM RT WHEEL WELL PRESSURE PANEL TO FRAME CORRODED ON UPPER FORWARD FACE OF FLANGE AT STA 1501, SIX INCHES BELOW CABIN FLOOR. A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, 53-00-01, FIGURE 1 AND 53-14-01, FIGURE 11SDR CALA9601855Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 472, LBL 54. TWO ANGLES, FILLER AND A FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-31-01, 51-21-01, 51-35-01 AND 53-60-01 FIGURE 1.SDR CALA9601871Hinged Panel · crackedINSPECTION FOUND A .50 INCH CRACK AROUND FASTENER OF LT HORIZONTAL STABILIZER LOWER TRAILING EDGE HINGED PANEL AT STA XE 158. THE AREA WAS REPAIRED IAW SRM 51-70-00.SDR CALA9601872Blkhd Stiffener · corrodedINSPECTION FOUND CORROSION AROUND LOWER BOLT HOLE OF T-SHAPED VERTICAL STIFFENER AT CENTER WHEELWELL AFT FACE OF FORWARD BULKHEAD, XCW -15.0. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM'S 51-10-00, 51-21-01, AND 51-31-01.SDR CALA9601867Frame · corrodedTHE RT CENTER MLG DOOR AFT FRAME WAS FOUND CORRODED. THE AFT FRAME WAS REMOVED AND REPLACED IAW SRM'S 51-35-01 AND 51-35-02.SDR CALA9601850Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1009 TO 1029, STRINGER 52. THE CORRODED AREA WAS CUT OUT. REPAIR DOUBLERS, FINGER DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.SDR CALA9601849Skin · corrodedINSPECTION FOUND CORROSION ON FUSELAGE SKIN AT BS 1049 TO 1069, STRINGER 52. THE CORRODED AREA WAS REMOVED. REPAIR DOUBLERS, FINGER DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-20-00, FIGURE 7.
Back to N37077, cancelled Nov 4, 2005