N7635U, cancelled Jun 14, 2013
Service difficulty reports · 92
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 = 'N7635U' AND deregistration_id = 'N7635U-2013-06-14' 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 = 'N7635U' AND deregistration_id = 'N7635U-2013-06-14' 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 C7WA200600009Valve · failedAIR RETURN, LOST A-SYSTEM HYDRAULIC SYSTEM ON TAKEOFF ZERO QUANITY AND PRESSURE. COMPLETED CHECK LIST, NORMAL LANDING FOUND LT MLG DOOR SEQUENCE VALVE BLOWN. REMOVED AND REPLACED SEQUENCE VALVE. OPERATIONAL AND LEAK CHECKS GOOD. (K)SDR C7WA200400061Flap Track · corrodedRT WING IB FLAP OB TRACK AFT MOUNT PAD HAS CORROSION. RT WING IB FLAP OB. TRACK NR 6 PN 65192493, CORROSION ON AFT MOUNT PAD REMOVED. MATERIAL REMOVED WAS 0.020. REPAIR ACOMPLISHED IAW EO.SDR C7WA200400060Keelbeam · corrodedAFT CARGO COMPARTMENT, STA 1007 RT KEELBEAM CHORD HAS CORROSION. INSTALLED INTERNAL SPLICE REPAIR ON RT HEELBEAM CHORD SECTION BETWEEN BS 980 AND BS 1007. DAMAGED KEELBEAM CHORD SECTION REMOVED. NEW KEELBEAM CHORD SECTION FABRICATED IAW SAMPLE AND MFG DWG 6SDR C7WA200400059Structure · damagedRT HORIZONTAL STABILIZER BALANCE PANELS NR 2, NR 3, AND NR 4 CAVITIES T/E LOWER BEAM RUB BLOCKS ADJUSTMENT SCREW SAFETY WIRE HOLES CRACKED. INSTALLED SPLICE REPAIR ON RT HORIZONTAL STABILIZER T/E BEAM BALANCE PANELS CAVITIES NR 2, NR 3, AND NR 4. DAMAGED CHOSDR C7WA200400057Floorbeam · corrodedFLOOR TRAVERSE BEAM AT STA 600 HAS LIGHT CORROSION BETWEEN BL0 AND RBL 24.5 AND BETWEEN LBL 45.5 AND LBL50. INSTALLED INTERNAL FLOORBEAM REPAIR ON DAMAGE LOCATED AT BS 600 BETWEEN BL0 AND LBL 24.50. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DISDR C7WA200400056Floorbeam · corrodedTRAVERSE FLOORBEAM STA 720 HAS CORROSION BETWEEN BL0 AND LBL 24.5. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 720A, BETWEEN BL0.0 AND LBL 24.5. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DIMENSION WAS 6.00 INCH X 2.00 INCH. REPAIR SECTION FABRSDR C7WA200400055Shear Tie · crackedSHEAR TIE CRACKED AT FRAME STA 930 BETWEEN STRINGER 13 RT AND STRINGER 14 RT. INSTALLED INTERNAL REPAIR ON SHEAR TIE AT BS 930 BETWEEN STRINGER 13 RT AND 14 RT. DAMAGED SHEAR TIE REMOVED. REPAIR PART FABRICATED FROM 7075-T6, X .063. REPAIR PARTS AND BARE ESDR C7WA200400054Beam · corrodedBULKHEAD STA 1183 HAS A 6 INCH CRACK IN THE VERTICAL BEAM AT LBL 24.5, WL 250. INSTALLED INTERNAL REPAIR ON DAMAGED VERTICAL BEAM AT BS 1183 AT LBL 24.50, WL 250. DRILLED STOP HOLE .250. REPAIR CHANNEL 65C33556-45 AND SHIMS INSTALLED IAW SB. REPAIR PARTS ASDR C7WA200400053Floorbeam · corrodedFLOORBEAM AT BS 660 RBL 45.50 HAS LIGHT CORROSION. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 660, RBL 45.50. REMOVED DAMAGED CHORD PORTION, FINAL TRIM OUT WAS 2.00 INCH. FABRICATED REPAIR SECTION FROM ALUM 7075-0 X 0.090 INCH X 16 INCHES. HEAT TREATED TO TSDR C7WA200400052Skin · crackedNR 3 RT COCKPIT WINDOW UPPER SKIN (EXTERIOR) HAS AN APPROXIMATELY 1 INCH CRACK. INSTALLED EXTERNAL SKIN REPAIR ON RT NR 3 WINDOW UPPER SKIN. REMOVED DAMAGED SKIN PORTION. SKIN TRIM OUT 4.00 X 5.00. FABRICATED AND INSTALLED REPAIR FILLER PLATE FROM 2024-T3 SDR 277847Pump · leakingDURING CRUISE FLIGHT, EXPERIENCED A LOSS OF HYDRAULIC FLUID ON (B) SYSTEM. AN EMERGENCY LANDING WAS INITIATED AND THE AIRCRAFT LANDED, WITHOUT INCIDENT. REMOVED AND REPLACED B SYSTEM HYDRAULIC PUMP.SDR RYN2002F00036Web · corrodedAT (C) CHECK, FOUND WEB WITH EXFOLIATED CORROSION, FROM STATION 1110 TO 1130, RBL 54.0.SDR 2002F00726Seat Track · corrodedAT C-CHECK, FOUND SEAT TRACK CORRODED AT STATION 870, RBL 48. (M)SDR 2002F00733Structure · corrodedAT C-CHECK, FOUND FLAP JOINT CORRODED AROUND RIVETS, AT STATION 480, STRINGER 26L. (M)SDR RYN2002F00032Rib · crackedAT (C) CHECK, FOUND CRACK IN RIGHT WING NUMBER THREE TANK, ON LOWER WEB, OUTBOARD STATION 686.5, STRINGER NUMBER SIX.SDR 2002F00871Splice · crackedAT C-CHECK, FOUND CRACK AT FORWARD CARGO COMPARTMENT, ON LEFT STRINGER SPLICE, AT STATION 685 STRINGER 26L. (M)SDR 2002F00737Floorbeam · corrodedAT C-CHECK, FOUND CORROSION AT CABIN FLOORBEAM, AT STATION 1110.0, BL 0 TO LBL 60. (M)SDR 2002F00736Rivet · missingAT C-CHECK, FOUND LEFT ELEVATOR TRAILING EDGE WITH LOOSE AND MISSING RIVETS, AT STATION 125. (M)SDR 2002F00735Fitting · crackedAT C-CHECK, FOUND UPPER T-FITTING CRACKED, ON CENTER WING FUEL TANK FRONT SPAR, STATION 760, LBL 25. (M)SDR 2002F00734Fitting · crackedAT C-CHECK, FOUND CENTER WING FUEL TANK FRONT SPAR UPPER FITTING CRACKED, AT STATION 740, LBL 45. (M)SDR 2002F00728Rib · crackedAT C-CHECK, FOUND RIGHT WING TIP RIB CRACKED AT WBL 62.5. (M)SDR RYN2002F00030Seat Track · corrodedAT (C) CHECK, FOUND CORROSION ON CABIN SEAT TRACK AT STATION 1090TO 1180, LBL 94.SDR 2002F00729Trunnion · corrodedAT C-CHECK, FOUND LEFT MAIN LANDING GEAR TRUNNION ATTACH FITTING WITH CORROSION AND GOUGES IN SPOT FACE AREAS. (M)SDR RYN2002F00028Skin · corrodedAT (C) CHECK, FOUND FUSELAGE SKIN CORRODED WITH RIVETS DISHED AND SKIN BULGED. BELOW FORWARD JACK POINT, AT STATION 340.SDR 2002F00854Seat Track · corrodedAT C-CHECK, FOUND SEAT TRACK WITH CORROSION AROUND NUTPLATES, AT STATION 780-846, LBL 48. (M)SDR 2002F00741Floor Support · corrodedAT C-CHECK, FOUND CARGO FLOOR SUPPORT CORRODED IN AFT CARGO COMPARTMENT, AT STATION 1035, RBL 2. (M)SDR 2002F00740Angle · crackedAT C-CHECK, FOUND SUPPORT ANGLE FOR THE FLOORBEAM HAS A .5 INCH CRACK AT STATION 820, LBL 48. (M)SDR 2002F00739Frame · crackedAT C-CHECK, THE FORWARD CARGO COMPARTMENT LOWER LOBE FRAME HAS A THREE INCH CRACK AT STATION 500, RBL 50. (M)SDR 2002F00738Angle · corrodedAT C-CHECK, FOUND AFT PIT ATTACH ANGLE WITH EXFOLIATION AT STATION 1183, STRINGER 18R. (M)SDR 2002F00731Floor Support · crackedAT C-CHECK, FOUND BOTTOM SIDE OF FLOOR SUPPORT CRACKED AT CABIN STATION 846, BL 0.0. (M)SDR 2002F00730Web · crackedAT C-CHECK, FOUND CRACK IN AFT CARGO COMPARTMENT WEB, AT STATION 1030 TO 1050, STRINGER 26L. (M)SDR RYN2002F00005Panel · corrodedC-CHECK, FOUND CORROSION IN AFT CARGO COMPARTMENT, ON LEFT TRANSITION PANEL, AT STATION 950E +8 TO 950F, LBL 18.SDR RYN2002F00035Frame · crackedAT (C) CHECK, FOUND FORWARD CARGO COMPARTMENT LOWER LOBE FRAME HAS A THREE INCH CRACK, AT STATION 520, RBL50.SDR RYN2002F00034Floorbeam · crackedAT (C) CHECK, FOUND CABIN FLOOR BEAM WITH .5000 INCH CRACK PROTRUDING FROM LIGHTENING HOLE, AT STATION 820, LBL 48.SDR RYN2002F00033Panel · corrodedAT (C) CHECK, FOUND FORWARD PIT TRANSISTION PANEL WITH CORRODED AREAS, STATION 620 TO 720D, RBL 20 TO 26, ON UPPER AND LOWER SURFACES.SDR 2002F00855Floorbeam · corrodedAT C-CHECK, FOUND FLOORBEAM EXFOLIATED IN SEVERAL AREAS, FROM LBL 60 TO RBL 60 UPPER CHORD, AT STATION 1130. (M)SDR 2002F00822Web · crackedAT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, RIGHT TORQUE BOX VERTICAL WEB, .5 INCH LONG, AT STATION 1223. (M)SDR 2002F00796Web · crackedAT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, LEFT TORQUE BOX VERTICAL WEB, AT STATION 1223. M)SDR 2002F00795Web · crackedAT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, IN LEFT TORQUE BOX VERTICAL WEB, .5 INCH LONGERON AT STATION 1235. (M)SDR 2002F00794Web · crackedAT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, RIGHT TORQUE BOX VERTICAL WEB, .75 INCHES LONG AT LIGHTENING HOLE, AT STATION 1235. (M)SDR 2002F00793Web · crackedAT C-CHECK, FOUND CRACK AT VENTRAL STAIRWAY, RIGHT TORQUE BOX VERTICAL WEB, AT LOWER LIGHTENING HOLE, .25 INCH LONG, AT STATION 1263. (M)SDR 2002F00745Floor Support · corrodedAT C-CHECK, FOUND FLOOR SUPPORTS WITH CORROSION, AT STATION 520 TO 590, RBL 2-7. (M)SDR 2002F00744Skin · damagedAT C-CHECK, FOUND LEFT ELEVATOR LEADING EDGE SKIN CREASED, AT ELEVATOR STATION 188. (M)SDR 2002F00743Skin · dentedAT C-CHECK, FOUND RIGHT HORIZONTAL STABILIZER WITH DENT BEYOND LIMITS, AT STABILIZER STATION 20. (M)SDR 2002F00742Floor Support · corrodedAT C-CHECK, FOUND FLOOR SUPPORTS WITH CORROSION, AT STATION 520 TO 590, RBL 2-7. (M)SDR RYN2002F00008Stringer · crackedC-CHECK, FOUND IN AFT CARGO COMPARTMENT STATION 970, STRINGER 26L HAS A CRACK THAT IS STOPPED DRILLED. CRACK IS CONTINUING PAST THE STOP DRILL HOLE.SDR RYN2002F00007Floor Support · crackedC-CHECK, FOUND IN AFT CARGO COMPARTMENT, FLOOR SUPPORT CRACKED AND HOLES DRILLED IN RADIUS OF ANGLE, AT STATION 950F B/L 0.SDR RYN2002F00031Web · corrodedAT (C) CHECK, FOUND CABIN SHEAR WEB SEVERAL AREAS OF CORROSION AT STATION 1148 TO 1183, RBL 24 TO 48.SDR 2002F00873Skin · corrodedAT C-CHECK, FOUND CORROSION AT RIGHT WING TOP SKIN, AT LEADING EDGE SPAR, AT APPROXIMATELY WING STATION 464. (M)SDR 2002F00872Skin · corrodedAT C-CHECK, FOUND CORROSION ON RIGHT WING TOP SKIN, AT LEADING EDGE SPAR, AT STATION 655. (M)
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