N29SW
Service difficulty reports · 100
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 = 'N29SW' AND registry_match = 'registration' 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 = 'N29SW' AND registry_match = 'registration' 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 2002F00416Circuit Breaker · shortedIN FLIGHT, CREW NOTICED CIRCUIT BREAKER POPPED AND ELECTRICAL SMOKE IN COCKPIT. AIRCRAFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. (M)SDR 2002F00415Bottle · dischargedIN FLIGHT, GOT APU OVERHEAT INDICATION. DISCHARGED APU FIRE BOTTLE. AIRCRAFT LANDED WITHOUT INCIDENT. NO EVIDENCE OF FIRE FOUND AFTER APU INSPECTION. (M)SDR 2002F00117Fire Warning · malfunctionedMASTER FIRE WARNING LIGHT FLICKERED ON AND OFF DURING DESCENT. ON FINAL, LIGHT CAME ON STEADY WITH NO OTHER ASSOCIATED FIRE WARNINGS. LIGHT WAS RESET. (M)SDR COOSDR010073Floorbeam · crackedPAX CABIN FROM BS 520 RBL 25 AND WL 208, FLOOR BEAM CRACKED.SDR COOSDR010072Frame · crackedLOWER FUSELAGE LEFT WHEEL WELL, BS 663.75 LBL 25 AND WL 208 CHORD, CRACKED.SDR COOSDR010071Angle · crackedLOWER FUSELAGE RIGHT WHEEL WELL, BULKHEAD BS 727, BL 0 AND WL 208 ANGLE, CRACKED.SDR COOSDR010070Skin · delaminatedLEFT WING GROUND SPOILER NR 5 WITH UPPER SKIN DELAMINATED.SDR COOSDR010069Skin · delaminatedRIGHT WING, FLIGHT SPOILER NR 8 UPPER SKIN, DELAMINATED.SDR COOSDR010068Skin · delaminatedLEFT WING, IB FORE FLAP UPPER SKIN DELAMINATED.SDR COOSDR010067Skin · delaminatedLEFT WING, GROUND SPOILER NR4 UPPER SKIN DELAMINATED.SDR COOSDR010066Skin · delaminatedLEFT WING SLAT NR 3 UPPER SKIN DELAMINATED.SDR COOSDR010064Stringer · crackedFUSELAGE STRINGER SECTION 27L FROM BS 960 TO BS 1016, CRACKED.SDR COOSDR010063Floorbeam · crackedFUSELAGE FLOOR BEAM SECTION UPPER CHORD AT BS 328 BETWEEN RBL 24.5 AND RBL40, CRACKED.SDR COOSDR010062Frame · crackedFUSELAGE FRAME SECTION AT BS 328 BETWEEN STR 1R AND 4R, CRACKED.SDR COOSDR010061Stringer · crackedFUSELAGE STRINGER SECTION FROM BS 306 TO BS 326 AT STR 4R, CRACKED.SDR COOSDR010060Stringer · crackedFUSELAGE STRINGER SECTION FROM BS 429 TO BS 450 AT STR 4R, CRACKED.SDR COOSDR010059Frame · crackedFUSELAGE FRAME SECTION AT BS 344 FROM STR. 4L AND STR 6L, CRACKED.SDR COOSDR010058Stringer · crackedFUSELAGE STRINGER SECTION 9L FROM BS 727A+7 TO BS 727B+12, CRACKED.SDR COOSDR010057Stringer · crackedFUSELAGE STRINGER SECTION 9R FROM BS 755 TO BS 780, CRACKED.SDR COOSDR010056Stringer · crackedUPPER FUSELAGE MAIN CABIN STRINGER 11R AT BS 540, CRACKED.SDR COOSDR010055Stringer · crackedUPPER FUSELAGE MAIN CABIN STRINGER 11L AT BS 540 CRACKED.SDR COOSDR010054Stringer · crackedPAX CABIN, BS 727+9INCHES, STRINGER NR 1 CRACKED.SDR COOSDR010053Skin · canningEXT. FUSELAGE BS 864 BETWEEN STRINGER 16L AND 17L, SKIN WITH OIL CAN.SDR COOSDR010052Floorbeam · crackedFORWARD C/C, FLOOR BEAM, LOWER CHORD, RBL 25 INCHES, WL 201 WITH CRACK.SDR COOSDR010051Stringer · corrodedAFT C/C BAY, STA967, STR 27R CORRODED.SDR COOSDR010050Skin · crackedEXTERNAL FUSELAGE, E & E COMPARTMENT, DOOR AROUND CUT OUT SKIN WITH SHARP EDGES AND CRACKED.SDR COOSDR010049Skin · dentedEXTERNAL FUSELAGE, BETWEEN BS 423 AND BS 435 BETWEEN STR 20R, SKIN DENTED.SDR COOSDR010048Skin · dentedEXTERNAL FUSELAGE BS890 BETWEEN STR 20R AND STR 21R DENTED.SDR COOSDR010044Spar · crackedWING - CENTER WING BOX - REAR SPAR CRACKED - STA 663.0/ RBL6.150/ WL 170.4SDR COOSDR010043Bulkhead · crackedAFT PRESSURE BULKHEAD - BS 1016 WEB CRACKED, Y CHORD INSPECTION.SDR COOSDR010039Frame · crackedPAX CABIN, BS 727, AT STR 14L LEVEL FRAME CRACKED. PROBABLE CAUSE IS FATIGUE.SDR COOSDR010037Floorbeam · corrodedPAX CABIN, STA 947 FLOOR BEAM UPPER FLANGE CORRODED AT LBL 50.SDR COOSDR010036Stringer · crackedPAX CABIN, STA 618, STRINGER 17R, HORIZONTAL FLANGE CRACKED.SDR 2001F00180Floorbeam · corrodedFOUND PASSENGER CABIN, STATION 947 FLOORBEAM UPPER FLANGE CORRODED AT LBL 50. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW EO COO-3-53-233-01. (M)SDR 2001F00146Floorbeam · corrodedFOUND PASSENGER CABIN, STATION 947 FLOORBEAM UPPER FLANGE CORRODED AT LBL 50. THE CORRODED FLOORBEAM SECTION WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW EO COO-3-53-233-01. (M)SDR 2001F00183Skin · dentedTHE FUSELAGE SKIN AT BS 890 BETWEEN STRINGER 20R AND 21R WAS FOUND DENTED. THE DAMAGED AREA WAS REPAIRED IAW BOEING FAX COO-SJD-01-003292MM DATED 6/11/2001. (M)SDR 2001F00145Skin · dentedTHE FUSELAGE SKIN AT BS 890 BETWEEN STRINGER 20R AND 21R WAS FOUND DENTED. THE DAMAGED AREA WAS REPAIRED IAW BOEING FAX COO-SJD-01-00392M DATED 6/11/2001. (M)SDR 2001F00197Stringer · crackedFOUND STRINGER CRACKED AT BS 440, STRINGER 4 RIGHT. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M)SDR 2001F00196Stringer · crackedFOUND STRINGER AT STATION BS 727B STRINGER 9 LEFT HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIG 3. (M)SDR 2001F00195Floorbeam · corrodedTHE FLOORBEAM WAS FOUND CORRODED AT BS 328, RBL 32. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-9 FIGURE 6. (M)SDR 2001F00194Stringer · corrodedAT STRINGER 27L FROM BS 1006 TO BS 1016, CORROSION WAS FOUND. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 1. (M)SDR 2001F00193Angle · crackedFOUND LOWER FUSELAGE, BS 727 BULKHEAD, BLO WL 208 ANGLE CRACKED. DAMAGED AREA WAS REPAIRED PER SB 737-53-1053. (M)SDR 2001F00192Frame · crackedFOUND CRACK IN FRAME STATION BS 344 STRINGER 6 LEFT. THE DAMAGED AREA WAS REPAIRED IAW SRM 51-40-3 FIGURE 1. (M)SDR 2001F00191Stringer · crackedFOUND STRINGER CRACKED AT BS 312, STRINGER 4 RIGHT. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-3 FIGURE 3. (M)SDR 2001F00190Skin · canningTHE FUSELAGE SKIN WAS FOUND WITH OIL CANNING. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-30-3 FIGURE 3. (M)SDR 2001F00189Frame · damagedTHE FRAME WAS FOUND WITH ELONGATED HOLES AT BS 328 BETWEEN STRINGER 2R AND STRINGER 3R. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-4 FIGURE 1. (M)SDR 2001F00188Floorbeam · crackedFOUND FLOORBEAM FOUND CRACKED AT BS 520 RBL 25 WL 208. THE DAMAGED AREA WAS REPAIRED IAW SB 737-53-1120. (M)SDR 2001F00187Floorbeam · crackedFOUND FLOORBEAM AT BS 520 RBL 25 INCH LOWER CHORD HAS CRACK. THE DAMAGED AREA WAS REPAIRED IAW SRM 53-10-9 FIGURE 7. (M)SDR 2001F00186Slat · delaminatedTHE NR 3 SLAT WAS FOUND DELAMINATED. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-3-57-239-01. (M)SDR 2001F00185Flap · wornTHE UPPER SURFACE OF THE INBOARD FORE FLAP WAS SHOWING WEAR. THE DAMAGED AREA WAS REPAIRED IAW EO COO-CMP-A57-243-01, DATED JUNE 06-01. (M)
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