N29717
Service difficulty reports · 70
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 = 'N29717' 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 = 'N29717' 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 CALA2012123100900Web · corrodedWEB CORRODED AT BS 986.5, RBL 32. INSTALLED NEW WEB IAW SRM 51-40-02 & DWG 147A5700.SDR CALA2012123100896Floor Support · corrodedLEFT OTBD FLOOR SUPPORT BETWEEN BS 947-967 AND LBL 50 HAS SURFACE CORROSION AT FASTENER HOLES. R & R FLOOR SUPPORT IAW SRM 51-40-02.SDR CALA2012123100895Attach Angle · corrodedE & E BAY, CORROSION ON SKIN ATTACH ANGLE BS 359, S28L. R & R ATTACH ANGLE, 141A8513-48, REF SRM 51-40-02 AND DWG 140A9101.SDR CALA2012123100894Angle · corrodedFLOOR TRANSITION ANGLE AT L2 DOOR AREA HAS SURFACE CORROSION BETWEEN BS 947-1006. REMOVED CORRODED ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-40-02.SDR CALA2012123100892Frame · crackedFRAME BS 867L BETWEEN STRINGERS 8 AND 9L HAS A CRACK AT RIVET ATTACH BRACKET. REPAIRED CRACKED FRAME, REF EA 5310-04716, OP 01.SDR CALA2012122800883Angle · corrodedR1 DOOR ANGLE HAS CORROSION BS 294 TO 355. REMOVED DAMAGED INNER ANGLE, DRILLED AND INSTALLED NEW INNER ANGLE IAW SRM 51-40-02.SDR CALA2012122800889Frame · crackedFRAME, BS 747 BETWEEN STRINGERS 8 & 9L HAS A CRACK AT ATTACH BRACKET. REPAIRED FRAME AS REQUIRED IN EA 5310-04716, REV D.SDR CALA2012122800888Frame · crackedLEFT FUSELAGE FRAME, BS 787 BETWEEN STRINGERS 8 AND 9L HAS CRACK AT RIVET ATTACH BRACKET. REMOVED DAMAGE AND INSTALLED DOUBLERS REF EA5310-04716, REV D.SDR CALA2012122800882Frame · crackedFRAME, BS 380 BETWEEN STRINGERS 8 AND 9L HAS CRACKED AT RIVET ATTACH BRACKET. REMOVED DAMAGES AREA AND FABRICATED AND INSTALLED REPAIR ANGLE IAW EA5310-04716, REV D.SDR CALA2012122700879Frame · crackedLEFT FUSELAGE FRAME BS 500C, BETWEEN STRINGERS 8 AND 9L HAS CRACKED AT RIVET ATTACH BRACKET. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW EA 5310-04716, REV D, FIG 3.SDR CALA2012122700878Frame · crackedLEFT FUSELAGE FRAME, BS 727D BETWEEN STRINGERS 8 AND 9L HAS CRACKED AT RIVET ATTACH BRACKET. FABRICATED AND INSTALLED REPAIR ANGLES IAW EA 5310-04716, REV D.SDR CALA2012122600876Floorbeam · corrodedMAIN DECK FLOORBEAM, BS 328, RBL 13 TO RBL 50 HAS CORROSION REPAIRED FLOORBEAM STA 328, RBL13 TO RBL 50 INSTALLED REPAIR PARTS FROM RBL 35 TO RBL 50 REF SRM 53-10-51, REPAIR 8, ALT 3, RBL 13 TO RBL 35 WAS WITHIN LIMITS AFTER BLEND OUT REPAIRED IAW ECRA 5321-01SDR CALA2012122600875Floor Support · corrodedFLOOR SUPPORT BS 328 TO 344 LBL 11 HAS CORROSION. R & R FLOOR SUPPORT IAW SRM 51-40-02.SDR CALA2012122100873Floor Support · crackedFLOOR SUPPORT BS 328 TO 344, LBL 45 CRACKED. R & R FLOOR SUPPORT IAW SRM 51-40-02.SDR CALA2012031400181Block · corrodedEMERGENCY LIGHT UNDER OVERHEAD AT SEAT 27D ILLUMINATES WHEN LIGHTS TURNED OFF. FOUND GROUND BLOCK GD3808-DC (FOR BUNDLE W4142, P/N BACC50AN16) CORRODED SEE WDM 33-51-14. R & R'D GROUND BLOCK WITH A SERVICEABLE GND BLK. OPS CHECKS NORMAL IAW 33-51-00.SDR CALA2011091600601Indication Sys · malfunctionedLARGE DISPARITY BETWEEN FOB GAUGES AND FMC FUEL. GAUGES DISPLAYED 900LBS LESS TOTAL FUEL. CORRECTED STA TO BHM (IAH ENTERED IN ERROR) PERFORMED FUEL QTY BITE TEST IAW FIM 28-41-00-810-801 NO FAULTS FOUND. VERIFIED FUEL LOAD USING STICKS NR 6 RT 5.4 AT 7,498SDR CALA2011030400118Window · crackedR2 WINDOW STARTED DEVELOPING CRACKS IN LOWER RIGHT CORNER. CREW OBSERVED PROGRESSIVE AREA LENGTHENING IN DELAMINATION AND CRACKS REMOVED AND REPLACED R2 WINDOW PER AMM 56-12-11. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1433394 S/N OFF 02399 IPC REFERENCE NSDR CALA2009080400433Power Supply · dischargedEMERGENCY LIGHT SIGN ON CENTER AND R1 DOOR CUTS ON AND OFF WHEN TURNED ON. CONFIRMED WEAK BATTERY AT PWR SUPPLY M1675. REPLACED POWER SUPPLY, SYS OPS CHECKS GOOD. REF AMM 33-51-06-960-805 AND 33-51-06-960-806.SDR CALA0800477Bulkhead · dentedDENT IN AFT PRESSURE BULKHEAD STR 12 C, WATERLINE 246. REPAIRED DAMAGE TO AFT PRESSURE BULKHEAD AT STRINGER 12L, WATERLINE 246 IN COMPLIANCE WITH SRM 53-80-08 REPAIR 1, ECRA 5344-01001.SDR CALA0600250Bulkhead · buckledINSPECTION FOUND THE AFT PRESSURE BULKHEAD OIL CANNED AT 11 O'CLOCK POSITION, ZONE 2, BS 1016. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5311-01261. A DIP WAS INITIATED TO ACCOMPLISH PT 2A INSPECTION AFTER 49K FLIGHT CYCLES, BUT BEFORE 50K FLIGHT CYCLES, AND
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