N73283
Service difficulty reports · 71
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 = 'N73283' 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 = 'N73283' 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 CALA2019110101870Frame · dentedFRAME DENTED AT BS 5OOG INNER CORD AT S-24L TO S-26L FRAME AT STA 500G REPAIRED PER EC/RA5311-02279 REF FLEET CYCLE L OG PG.9702467 FOR ALL WORK PERFORMED. INITIATE D.I.P PER EC/RA 5 311-02279 STEP 11 TO "ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE AIRSDR CALA2019110101868Skin · crackedEA 5510-01843 REV H; FOUND ON LEFT SIDE HORIZONTAL STAB, LOWER S KIN, AT STAB STA 129.5 MEASSURED FROM THE AFT SPAR GOING FORWARD 10 INCHES. THE CRACK MEASURES 3/4 INCH IN LENGTH. MARKED. REF F LEET CYCLE NON ROUTINE 9700271. COMMON DOUBLER INSTALLED ON L/H HOSDR CALA2019110101867Skin · crackedREF EA5510-01843 REV H . FOUND A CRACK RH SIDE HORIZONTAL STAB LOWER SKIN AT STAB STA 157.1,MEASURED FROM THE AFT SPAR GOING FWD 9 INCHES . TE CRACK MEASURES 3/4 INCH IN LENGHT . REF FLEET CYCLE N/R 9700274 FOR ALL WORK PERFORMED PER SRM 55-10 -01 REPAIR 11 . SDR CALA2019110101865Beam · corrodedCORROSION FOUND IN APU COMPARTMENT LOWER LEFT FLANGE BETWEEN MIDDLE DOOR LATCH AND FWD DOOR LATCH NEAR NUT PLATE . REPAIRED REF ECRA5311-02282 . INITIATE A DIP TO ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE AIRCRAFT REACHING 75.000 TOTAL FLIGHT CYCLESSDR CALA2019102501818Fitting · crackedL-1 WINDOW POST CRACKED AT UPPER LEFT CORNER L-1 WINDOW POST HAS BEEN REPAIRED IAW ECRA 5311-02271 ACCOMP AN INITIAL INSP PER PART 2 SECTION A ON OR BEFORE THE AIRCRAFT REACHING 50000 TOTAL FLT CYC''S. ACCOMP REPETITIVE INSP''S PER PART 2. SECTION A AT INTERVASDR CALA20191011730Skin · corrodedREF FCD 5100-02772 LAV VENT PORT HAS CORROSION STA 917L BETWEEN STRINGERS 21L AND 22L FUSELAGE SKIN AT STA 917 BETWEEN STR''S 21L AND 22L HAVE BEEN REPAIRED IAW SRM 53-70-01 REP 3 INSP THRESHOLD @ 50,000 TOT F/C FOLLOWED BY REPEAT INTERVALS AT EACH SUBSEQUENT SDR CALA2019100541686Skin · crackedREFERENCE EA 5510-01843 REV H; FOUND ON RIGHT SIDE HORIZONTAL ST AB , LOWER SKIN, AT STAB STA 120.3 MEASURED FROM THE AFT SPAR GO ING FORWARD 10 INCHES. THE CRACK MEASURES 1/2 INCH IN LENGHT.MAR KED. REF FLEET CYCLE NON ROUTINE 9700273. R/H HORIZ STAB LOWER INSDR CALA2019100541685Skin · crackedREF EA 5510-01843 REV H FOUND ON R/H HORIZ STAB LOWER SKIN AT STA 101.90 CRACK MEASURING 10" FWD AF AFT SPAR 1" IN LENGTH R/H HORIZ STAB LOWER INSPAR SKIN STA 101.90 HAS BEEN REPAIRED IAW SRM 55-10-01 REP 11 REF F/C N/R 9700272 INSP THRESHOLD AT 56''000 TOT F/SDR CALA2017110303884Sensor · faultedLEADING EDGE FLAPS TRANSIT LIGHT STAYS ON 1. EMERGENCY DECLARED. PERFORMED VISUAL INSPECTION OF FLAP AND SLATS, WITH FLAPS EXTENDED PERFORMED HARNESS SHAKE DOWN, NO DEFECTS NOTED. IAW FIM TA SK 27-51-00 PERFORMED FSEU BITE, NO FCURRENT FUALTS NOTED. ON FAULT HSDR CALA2017101303606Light · inoperativeEMERGENCY EXIT SIGN DOES NOT TURN ON 20A. RESET THE LIGHT ASSY.SDR CALA2017081802781Battery Pack · dischargedM1694, M1695, M1676, M1671 EMERGENCY LIGHTS POWER SUPPLY BATTERIES FAIL CAPACITY CHECK PER W/C 29-3350-1-7100. REPLACED CHARGER ASSY M1671 IAW AMM 33-51-06. REPLACED BATTERY PACKS IN CHARGERS M1671, M1676, M1694, M1695 IAW AMM 33-51-06.SDR CALA2016090900641Skin · damagedFUSELAGE SKIN DAMAGE AT EXTERNAL POWER DOOR CUT OUT, FWD EDGE AT LOWER HINGE AREA. THE SKIN AT BS 227 WL 180 HAS BEEN REPAIRED IAW ECRA 5330-04930 PART 3, AND SRM 53-10-15 REP. 5.SDR CALA2015101400848Trim Motor · failedMAIN ELEC TRIM & AUTOPILOT TRIM FAILED IN FLIGHT. FLAPS 15 LANDING, SOFT & BELOW MAX LANDING WEIGHT. TRIM SWITCH CONFIGURATION LEFT IAW QRH CHECKLIST. R & R STABILIZER TRIM MOTOR IAW AMM 27-41-71-400-801. REF FORM 44-0008 FOR WORK PERFORMED. OPERATIONS CHSDR CALA2014031000304Frame · crackedFRAME AT STATION 727D BETWEEN STRINGER 8RT & STRINGER 9RT FOUND TO HAVE 1/2 INCH CRACK USING MFEC AT INBD FASTENER HOLE FOR AIR CONDITIONING RAIL BRACKET. CUT OUT DAMAGE AT STATION 727D LOCATED BETWEEN STRINGER 8RT & STRINGER 9RT. INSTALLED REPAIR ANGLES TWOSDR CALA2014031000302Frame · crackedFRAME AT STATION 867 BETWEEN STRINGER 8RT & STRINGER 9RT FOUND TO HAVE A 1/8 INCH CRACK USING MFEC AT INBD RIVET FOR AIR CONDITIONING RAIL BRACKET. CUTOUT DAMAGE AT STATION 867 LOCATED BETWEEN STRINGER 8R & STRINGER 9R. INSTALLED ANGLES TWO EACH & SEALED ARESDR CALA2014030600285Frame · crackedFRAME AT STATION 400 BETWEEN STRINGER 8RT & STRINGER 9RT FOUND TO HAVE A 1/2 INCH CRACK FOUND VISUALLY & CONFIRMED USING MFEC AT INBD RIVET FOR AIR CONDITIONING RAIL BRACKET CABIN. ACCOMPLISHED ANGLE REPAIR IAW EA 5310-04716 REV F, FIG 3.SDR CALA2014030600282Frame · crackedFRAME AT STATION 787 BETWEEN STRINGER 8RT & STRINGER 9RT FOUND TO HAVE A 1/8 CRACK. FOUND USING MFEC AT INBD RIVET FOR AIR CONDITIONING RAIL BRACKET. REPAIR OF FRAME AT STATION 787 BETWEEN STRINGER 8RT & STRINGER 9RT IAW EA 5310-04716 REV F FIGURE 3.SDR CALA2013082800588Battery Pack · dischargedEMERGENCY LIGHTS EXIT L1 DOOR & EXIT LIGHT ABOVE COCKPIT DOOR STAY ON ONLY 3-4 SECONDS. THIS IS SFR ITEM. R & R POWER SUPPLY BATTERY PACK AT L1 DOOR IAW AMM 33-51-06-960-8 05. OPERATIONS CHECKED GOOD.SDR CALA2011050400338Skin · crackedSUPPORT TASK LT HORIZONTAL STAB LOWER SKIN SHOW CRACK AT STA 101.90 JUST I/B OF DRAIN HOLE. APROX 1 INCH IN LENGHT (MARKED) C-SCAN. REPAIRED AD REFINISHED PER EC/RA 5510-02165 AND ISSUED DIP TO INSPECT REPAIR IN 56,000 FLIGHT CYCLES PER SRM 55-10-01 REPAIR ISDR CALA2011050400337Skin · crackedSUPPORT TASK - RT HORIZONTAL STAB LOWER INSPAR SKIN SHOW CRACK AT STA. 175.50 APPROX 6 INCHES AFT OF DRAIN HOLE. CRACK 1 INCH LENGHT. (MARKED) C-SCAN. REPAIRED AND REFINISHED PER EC/RA 5510-02166 AND ISSUED DIP TO INSPECT REPAIR IN 56,000 FLIGHT CYCLES PER SSDR CALA2009030600126Frame · damagedFBB RT WS 500D AT STRINGER 25R HAS DAMAGE. COMPLIED WITH EC/RA 5310-04909 ON FRAME REPAIR AT STA 500D AT STR 24RT TO STR 25RT.
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