N17309
Service difficulty reports not matched to an aircraft · 44
They name N17309, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N17309' AND registry_match IS NULL 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 = 'N17309' AND registry_match IS NULL 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 CALA0500056Channel · crackedINSPECTION FOUND A 10 INCH CRACK IN STIFFENER CHANNEL IN FORWARD CARGO BAY AT VOR ANTENNA, STA 500 BETWEEN S28L AND S28R. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-2.SDR CALA0500052Shear Tie · corrodedINSPECTION FOUND SKIN CLIP CORRODED AT STA 500, RBL 2 IN FORWARD BAGGAGE BIN FLOOR AREA. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-07 FIGURE 207.SDR CALA0500048Stringer · corrodedINSPECTION FOUND STRINGER 27L CORRODED AT RIVET HOLES BETWEEN STA 500 AND 500B. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.SDR CALA0500047Frame · corrodedINSPECTION FOUND STA 500 FRAME CORRODED AT SKIN ATTACH POINT BETWEEN S27R AND S28R, RBL 11-RBL 16. A FRAME REPAIR WAS INSTALLED IAW SRM 53-00-07, FIGURE 203.SDR CALA0300568Wire · brokenINSPECTION FOUND EMERGENCY AISLE LIGHTS AT ROW S 12-20 INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT STA 378 EMERGENCY LIGHT BATTERY PACK. THE BROKEN WIRE WAS REPLACED IAW CHAPTER 20 STANDARD WIRING PRACTICES MANUAL AND WDM 33-50-00.SDR CALA0300560Battery Pack · inoperativeTHE INTERIOR EMERGENCY AISLE LIGHTS AT ROWS 14R, 16L, 19L, 21R, AND 23L WERE FOUND INOPERATIVE. REPLACED BATTERY PACKS AT M1135 AND M1136 POWER SUPPLIES IAW MM 33-51-51, PARAGRAPH 3, PAGES 203-206. OPERATIONAL CHECKS WERE GOOD.SDR CALA0300371Pressure Panel · crackedINSPECTION FOUND A 3 INCH CRACK IN PRESSURE DECK AT STA 665, RBL 35, JUST O/B OF J-BOX IN RT WHEEL WELL CEILING. THE PRESSURE DECK WAS REPAIRED IAW SRM 53-60-51, PAGE 213-221.SDR CALA0300335Uplock · inoperativeTHE RT MLG FAILED TO EXTEND ON FIRST ATTEMPT WHILE ON APPROACH TO IAH. THE FAILURE WAS ACCOMPANIED BY ILLUMINATION OF THE RT MLG RED WARNING LIGHT. A TOWER FLY-BY CONFIRMED THAT THE GEAR WAS NOT EXTENDED. THE LANDING GEAR WAS EXTENDED MANUALLY, CREW RECEIVESDR CALA0300077Beam · corrodedINSPECTION FOUND ALL TORQUE BOX MOUNTING HOLES ELONGATED ON L-2 DOOR. REPAIRED IAW ECRA 5210-01658.SDR CALA0300070Skin · crackedINSPECTION FOUND A 1/2" CRACK IN L-2 DOOR AT WEB OPENING ON INTERIOR SKIN ABOVE INSTALLED TORQUE TUBE. INSTALLED REPAIR IAW ECRA 5210-01653.SDR CALA0300099Strap · corrodedINSPECTION FOUND R/H FLOOR SUPPORT STRAP CORRODED AT STA 793. THE FLOOR SUPPORT STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300067Web · corrodedINSPECTION FOUND THE FORWARD I/B CORNER OF WEB CORRODED AT AFT CARGO DOOR LOWER THRESHOLD. THE THRESHOLD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 53-60-15.SDR CALA0300066Strap · corrodedINSPECTION FOUND STRAP CORRODED UDER VERTICAL WEB AT STA 780-800, RBL 20. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300065Strap · corrodedINSPECTION FOUND CORROSION ON AFT LOWER STRAP ON BOTTOM SIDE OF VERTICAL WEB UPPER FLANGE AT STA 840-853, RBL 19. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300064Web · corrodedINSPECTION FOUND VERTICAL WEB CORRODED IN AFT BAGGAGE BIN AT STA 791-800, RBL 20. A NEW WEB WAS INSTALLED IAW SRM 51-70-11.SDR CALA0300063Frame · corrodedINSPECTION FOUND BELTFRAME CORRODED AT STA 793. THE CORRODED AREA WAS REMOVED AND A TYPICAL FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11.SDR CALA0300058Seat Track · corrodedINSPECTION FOUND L/H O/B SEAT TRACK AT BS 907-947.5 CORRODED. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-00-52, FIGURE 204.SDR CALA0300051Stringer · corrodedINSPECTION FOUND STRINGER 28R AND 29L CORRODED AT STA 323 AT FORWARD SIDE OF E&E DOOR JAMB. THE STRINGER SECTIONS WERE REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300098Pan · corrodedINSPECTION FOUND LAV FLOOR PAN FASTENER CORRODED AT STA 1016, RBL 13. A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-20-02.SDR CALA0300050Strap · corrodedINSPECTION FOUND H-STRAP CORRODED AT STA 1006, BL 0. THE H-STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-40-02.SDR CALA0300049Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 986, BL 0 TO LBL 18. THE UPPER CHORD OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851, REV. B.SDR CALA0300097Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT STA 344 BETWEEN LBL 36 AND RBL 12. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.SDR CALA0300034Galley Track · corrodedINSPECTION FOUND GALLEY FLOOR TRACK CORRODED BETWEEN BS 277 - 294 AT RBL 36. THE TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300031Stiffener · corrodedINSPECTION FOUND STIFFENER CORRODED AT LEFT SIDE AND RIGHT SIDE OF BL0 BELOW FLOOR LINE AT STA 1016. REPAIRED IAW EA 5310-04045, POS 2.SDR CALA0300029Skin · gougedINSPECTION FOUND THE R/H UPPER FUSELAGE SKIN GOUGED BELOW FORWARD R/H SIDE DORSAL FIN MOUNT POINT AT STA 880, STRINGER 2R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-01.SDR CALA0300001Skin · crackedINSPECTION FOUND A 1.5" CRACK IN R/H FUSELAGE SKIN AFT OF TRAILING EDGE OF FLAP, BS 727E, S18R. A DOUBLER WAS INSTALLED IAW SRM 53-00-01 AND ECRA 5330-03191.SDR CALA0101019Skin · crackedINSPECTION FOUND A 1/4" CRACK AT LOWER HINGE OF R-1 DOOR EXTERIOR SKIN. A REPAIR WAS INSTALLED IAW ECRA 5210-01458.SDR CALA0101017Seat Track · corrodedINSPECTION FOUND CABIN L/H O/B SEAT TRACK CORRODED AT STA 887-907. REPAIRED SEAT TRACK IAW SRM 53-00-52, FIGURE 204.SDR CALA0101016Frame · corrodedINSPECTION FOUND FRAME CORRODED AT STA 1006 BETWEEN S16R AND S15R. A FRAME REPAIR SECTION AND SPLICES WERE INSTALLED IAW SRM 53-00-07, FIGURE 201.SDR CALA0101013Skin · crackedINSPECTION FOUND A 1/2" CRACK IN #1 PYLON SKIN PANEL #5727L. REPAIRED IAW ECRA 5430-01230.SDR CALA0101009Bracket · crackedINSPECTION FOUND A 1/4" CRACK IN R/H WING #6 FLAP TRACK FAIRING I/B SUPPORT BRACKET. A NEW BRACKET WAS INSTALLED IAW MM 51-10-02.SDR CALA9901256Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN FORWARD LOWER FUSELAGE SKIN AT BS 373 AT GROUND BLOWER EXHAUST. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02870.SDR CALA9900499Stringer · corrodedSTRINGER 26L IS CORRODED FROM STA 500 TO 500D ALONG WITH STRINGER ATTACH CLIP AT STA 500D FORWARD CARGO PIT. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-00-03 FIG 201.SDR CALA9900468Skin · crackedFUSELAGE SKIN CRACKED UPPER LEFT CORNER OF CAPTAINS WINDSHIELD 1/2 TO RIVET. CONFIRMED WITH HFEC. REPAIRED PER EC/RA 5330-02802.SDR CALA9900460Floorbeam · crackedHOU - FLOORBEAM WEB CRACKED .35 INCH AT STATION 328 LBL 1. INSTALLED REPAIR PER EC/RA 5310-03847. (M)SDR CALA9900445Seat Track · corrodedCABIN RIGHT O/B SEEAT TRACK HEAVY CORROSION AT STA 907 - 917. REMOVED CABIN SEAT TRACK AT STA 907 TO END OF TRACK PER SRM 53-00-52.SDR CALA9900440Seat Track · corrodedCABIN RIGHT SIDE INBOARD SEAT TRACK HEAVY CORROSION BS 907 - BS 930. SPLICED IN NEW SEAT TRACK SECTION AT STA 827 - 947 PER SRM 5300-00-52 FIG 204.SDR CALA9900424Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM UPPER CHORD CORRODED AT STA 344, BL 0 TO LBL 15. THE FLOORBEAM UPPER CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-51, FIGURE 205.SDR CALA9802189Switch · inoperativeTHE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING AT PBI. THE GEAR WAS CYCLED, BUT THE RED LIGHT DID NOT EXTINGUISH. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NSDR CALA9801964Power Supply · inoperativeAFT 4 SEATS AND AFT 3 LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY IN AFT CEILING, STA 920 PER MM 33-51-51.SDR CALA9700318Hyd Line · leakingTHE HYDRAULIC B NR 1 ELECTRIC LOW PRESSURE LIGHT CAME ON FOLLOWED BY NR 2 ENGINE LOW PRESSURE AND HYDRAULIC B QUANTITY DROPPED TO ZERO. THE A/C WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE FROM B ELECTRIC PUMP TOSDR CALA9601257Hyd Line · brokenTHE B-SYSTEM LOW PRESSURE LIGHT FOR NR 2 ENGINE HYDRAULIC PUMP ILLUMINATED FOLLOWED BY B-SYSTEM HYDRAULIC QUANTITY DROP TO 0.5 GALLONS WHILE APPROACHING CLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND B-SYSTEM HYDRAULIC PUMP LINE BROKEN. THE HYSDR CAL950407Hyd Line · leakingFLT NR 0419 - CLE - THE 'A' SYSTEM HYDRAULIC QUANTITY WAS LOST WHILE IN FLIGHT. THE FLUID LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT. THE AIRCRAFT LANED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT MLG ASDR CAL950044Circuit Breaker · failedCLE - FLT 1835 - THE ACFT EXPERIENCED AN ELECTRICAL FAILURE WHILE EN ROUTE TO MDW. THE APU WAS STARTED, BUT IT WOULD ONLY POWER THE LT SIDE. THE TRANSFER BUS OFF LIGHT ON THE RT SIDE WAS ON. THE RT SIDE INSTRUMENTS WERE ALL WORKING. THE CREW ELECTED TO DIV
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