N17410, cancelled Jul 22, 2004
Service difficulty reports · 60
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 = 'N17410' AND deregistration_id = 'N17410-2004-07-22' 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 = 'N17410' AND deregistration_id = 'N17410-2004-07-22' 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 EISA20010151Skin · tornACCOMPLISHED SHEET METAL REPAIR AREA FORWARD OF RT OUT FLOW VALVE, STA 1166, STR. 24R.CORRECTIVE ACTION:CUT OUT DAMAGED AREA. FABRICATED DOUBLER .071 2024-T3 8" X 12" IAW B727 SRM 53-30-3, FIG. 3. TREATED & PRIMED AND INSTALLED DOUBLER IAW B727 SRM 51-10-2 & SDR EISA20010119Structure · crackedRT HORIZONTAL STAB O/B T/E CORNER IS CRACKED, TOP SIDE. FOUND DURING B-CHECK. ROUTED OUT CRACK IAW B727 SRM 55-10-1. NDT VERIFIED CRACK BEING REMOVED. FABRICATED DOUBLER AND FILLER PER EO NR 01-236. INSTALLED REPAIR PER EO 01-236 & B727 SRM 57-30-2 WITH APPRSDR EISA20000196Plate · misalignedPACK FAN REMAINED ON AFTER FLAPS UP. RUDDER LOAD LIMITER LIGHT REMAINED ON FOR 4 MINUTES AFTER FLAPS UP. REMOVED AND REPLACED RIVETS ON STRIKER ON INBOARD FLAP CONTROL VALVE FOLLOW UP PULLEY. OPS CHECKED INBOARD FLAP FOLLOW UP CABLES, RUDDER LOAD LIMITER INSDR EISA2000001Receiver · shortedNR 1 NAV RECEIVER INOPERATIVE. INSTALLED SERVICEABLE NAV RECEIVER. (M)SDR CALA9800863Fuel Pump · failedNUMBER 2 ENGINE FAILED AT ROTATION. FOUND FUEL PUMP SHAFT SHEARED. REPLACED NUMBER 2 ENGINE FUEL PUMP AND FUEL CONTROL PER MM 71-00-67.SDR CALA9800856Battery · dischargedEMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED BATTERY PACK.SDR CALA9800469Stiffener · crackedINSPECTION FOUND A .1562 INCH CRACK THROUGH FASTENER HOLE AT BOTTOM OF STIFFENER AT INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0, ACCESS CUTOUT 6303. A REPAIR WAS INSTALLED IAW SRM 51-14-1.SDR CALA9800468Floor Track · corrodedINSPECTION FOUND FLOOR TRACK CORRODED AT STA 380 TO 420, RBL 25. THE TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-05-01 AND 51-10-01.SDR CALA9800467Skin · wornINSPECTION FOUND A GROOVE WORN ON BOTTOM OF LT WING NR 7 SPOILER. THE NR 7 SPOILER WAS REMOVED AND REPLACED.SDR CALA9800466Window · delaminatedINSPECTION FOUND A BURNED SPOT AND A DELAMINATION BUBBLE IN R-1 WINDOW UPPER EDGE. THE R-1 WINDOW WAS REMOVED AND REPLACED IAW MM 56-11-11.SDR CALA9800465Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN J-BEAM ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE J-BEAM WAS REPAIRED IAW ECRA 5750-02193 AND EA 26865-5075.SDR CALA9800464Foreflap · damagedINSPECTION FOUND LT INBOARD FOREFLAP CRUSHED (4 AREA) AT INBOARD END. THE FOREFLAP WAS REMOVED AND REPLACED.SDR CALA9800463Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN R-1 DOOR CUTOUT AT FS 417. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5307-01141.SDR CALA9800442Skin · dentedINSPECTION FOUND LT OUTBOARD AILERON OUTBOARD UPPER TRAILING EDGE HAD A PREVIOUSLY FILLED SMALL DENT WITH FILLER BREAKING OUT. THE DENTED AREA WAS CUT OUT AND A HOT BONDED REPAIR WAS INSTALLED IAW SRM 51-40-6.SDR CALA9800441Skin · crackedINSPECTION FOUND A .375 INCH CRACK IN LT WING FIXED LEADING EDGE CUTOUT ABOVE NR 3 SLAT OUTBOARD TRACK AREA. A SKIN FLUSH REPAIR WAS INSTALLED IAW SRM 57-30-4.SDR CALA9800440Skin · dentedINSPECTION FOUND A DENT 19.5 INCHES FROM OUTBOARD END IN LT WING NR 2 LEADING EDGE SLAT UPPER SKIN. A REPAIR WAS INSTALLED IAW SRM 57-50-3.SDR CALA9800439Splice · crackedINSPECTION FOUND A 3 INCH CRACK AT SPLICE PLATE ON LOWER SURFACE OF LT WING UPPER LEADING EDGE SKIN DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR, FSS 224. THE SPLICE PLATE WAS CUT OUT, A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-2.SDR CALA9800438Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN BRACKET AT AFT FACE OF LT GEAR BEAM WHERE HYDRAULIC LINES PASS THROUGH ACCESS DOOR 8405. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 51-10-2, AND 51-30-2.SDR CALA9800437Angle · crackedINSPECTION FOUND A .5 INCH CRACK THROUGH AFT FASTENER HOLE AT REPAIR ANGLE INSIDE LT WING LEADING EDGE RIB, WS 330, AFT OF NR 4 SLAT, INBOARD END. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6.SDR CALA9800436Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 1 SLAT LOWER LEADING EDGE SKIN TO INBOARD TRACK ATTACH BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1.SDR CALA9800435Skin · disbondedINSPECTION FOUND RT TRAILING EDGE INBOARD FOREFLAP DISBONDED IN TWO AREAS. THE FOREFLAP WAS REMOVED AND REPLACED.SDR CALA9800434Angle · crackedINSPECTION FOUND A 1.6 INCH CRACK AT BOTTOM OF LEFT CURVED SIDEWALL SUPPORT ANGLE MOUNTED TO FORWARD SIDE OF CIRCUMFERENTIAL STA 950D. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-3.SDR CALA9800433Skin · corrodedINSPECTION FOUND CORROSION IN SKIN ATTACH LEG AT FORWARD SIDE OF CIRCUMFERENTIAL, BS 1148, STRINGER 28L AND 29L. THE CORROSION WAS CUT OUT IAW SRM 51-10-6. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-6.SDR CALA9800432Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL UPPER SUPPORT ANGLE BETWEEN FLOORBEAM SUPPORT, STA 720 AND 720A. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800431Skin · crackedINSPECTION FOUND A .0937 INCH CRACK AT LT WING UPPER SKIN CUTOUT FOR NR 2 SPOILER. THE FASTENERS WERE REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, 51-10-2, AND 57-30-2.SDR CALA9800430Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN FALSE SPAR LOWER ANGLE BELOW AND INBOARD OF NR 7 SPOILER ACTUATOR INBOARD COVE AREA. REPAIRED FALSE SPAR LOWER ANGLE IAW EA NR 26865-5182 AND REINSTALLED ADJACENT STRUCTURE IAW SRM 51-30-2.SDR CALA9800429Hinge · crackedINSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR BALANCE PANEL NR 9214 FORWARD HINGE. THE HINGE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2.SDR CALA9800428Stringer · crackedINSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 9 RT NR 3 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5.SDR CALA9800427Stringers · crackedINSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 6 RT NR 3 STRINGER AND NR 5 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED FASTENERS IAW SRM 51-30-2. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5.SDR CALA9800426Gusset · crackedINSPECTION FOUND A 2 CRACK IN GUSSET ON FORWARD SIDE OF RT FUSELAGE FRAME AT STA 825, RBL 70. THE GUSSET WAS REMOVED AND A NEW ONE WAS INSTALLED IAW EA SA012-5310-01870.SDR CALA9800425Web · crackedINSPECTION FOUND A 7 CRACK JUST BELOW DRAIN CHUTE IN LT AFT LAV FLOOR WEB AT BS 1176, LBL 50. THE CRACKED SECTION OF WEB WAS REMOVED. A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-20-01.SDR CALA9800424Skin · bulgedINSPECTION FOUND RT FUSELAGE SKIN BULGED JUST AFT AND BELOW FORWARD LAV SERVICE PANEL. THE BULGED AREA WAS REMOVED. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-2.SDR CALA9800423Floor Track · corrodedINSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1050 TO 1130, BL 25R. THE CORRODED SECTION OF FLOOR TRACK WAS REPLACED IAW SRM 53-10-5 AND 51-10-1.SDR CALA9800422Floor Track · corrodedINSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1100, BL 45R. THE CORRODED SECTION OF FLOOR TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5.SDR CALA9800718Battery Pack · dischargedTHE EMERGENCY EXIT SIGN IVER COCKPIT DOOR FELL OUT AND WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK AND LENSE ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.SDR CALA9800421Intercostal · crackedINSPECTION FOUND A 1.25 CRACK IN SUPPORT INTERCOSTAL AT AFT BAGGAGE COMPARTMENT BETWEEN BS 1030 AND 1050 ABOVE STRINGER 25L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.SDR CALA9800143Light · inoperativeINSPECTION FOUND EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED.SDR CALA9700787Brake Housing · crackedACFT RETURNED TO THE GATE AFTER DRAGGING THE NR 3 BRAKE DURING TAXI. THE NR 3 TIRE CAUGHT ON FIRE, FOAM WAS USED TO EXTINGUISH THE FIRE. THE NR 3 AND 4 MAIN TIRE/WHEEL ASSEMBLIES AND BRAKES WERE REMOVED AND REPLACED. THE NR 3 BRAKE DEBOOST VALVE WAS ALSO RESDR CALA9700516Skin · corrodedINSPECTION FOUND AFT CARGO COMPARTMENT INTERIOR SKIN CORRODED AT ANTENNA, STA 1030 TO 1050, STRINGER 29R TO 30. THE AREA WAS REPAIRED IAW SRM 51-40-3.SDR CALA9700581Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN VENTRAL STAIRWELL TORQUE BOX ANGLE AT STAIR ACTUATOR FITTING, STA 1272, RBL 22. A REPAIR WAS INSTALLED IAW BOEING DRAWING 65C27136.SDR CALA9700519Skin · disbondedINSPECTION FOUND LT INBOARD MIDFLAP UPPER SURFACE OF TRAILING EDGE WEDGE DISBONDED 24 INCHES FROM INBOARD END. THE DISBONDED AREA WAS CUT OUT, CORE AND DOUBLERS WERE FABRICATED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6.SDR CALA9700515Skin · corrodedINSPECTION FOUND LT FUSELAGE SKIN CORRODED AT STA 1130. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.SDR CALA9700512Spar Web · crackedINSPECTION FOUND A .75 CRACK IN WEB AT FRONT SPAR JUST OUTBOARD OF LT FORWARD TERMINAL PIN FITTING. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-40-2.SDR CALA9700511Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT AFT OUTBOARD END OF CUTOUT FOR NR 6 SLAT OUTBOARD HOOK OF RT WING FIXED LEADING EDGE. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 57-30-4.SDR CALA9700580Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD TRACK CUTOUT, STA 216. THE CRACK WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5730-01489.SDR CALA9700518Skin · delaminatedINSPECTION FOUND OUTBOARD END OF LT OUTBOARD AILERON TAB DELAMINATED. THE TAB WAS REMOVED AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6. THE TAB WAS REINSTALLED.SDR CALA9700514Skin · disbondedINSPECTION FOUND LEFT OUTBOARD FOREFLAP DISBONDING AT INBOARD END. THE END CAP WAS REMOVED, THE DISBONDED AREA WAS CUT OUT, A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-6 AND THE END CAP WAS REINSTALLED.SDR CALA9700513Rib · crackedINSPECTION FOUND A 1 INCH CRACK BETWEEN TWO AFT UPPER BOLTS OF LT WING LEADING EDGE RIB AT SLAT STA 0. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.SDR CAL960427Frame · crackedINSPECTION FOUND A 1.5 INCH CRACK IN AFT BAG PIT FLOOR LEVEL FRAME AT BS 1166, RBL 24. THE CRACKED AREA WAS CUT OUT. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-30-2. (M)SDR CAL960431Floorbeam · oversized holeINSPECTION FOUND OVERSIZED HOLE ON MAIN CABIN INTERIOR FLOORBEAM AT BS 350, RBL 40. THE EFFECTED SECTION WAS REMOVED. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2, 51-30-8 AND MM 51-20-2. (M)
Back to N17410, cancelled Jul 22, 2004