N14335, cancelled Mar 21, 2013
Service difficulty reports · 75
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 = 'N14335' AND deregistration_id = 'N14335-2013-03-21' 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 = 'N14335' AND deregistration_id = 'N14335-2013-03-21' 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 CALA2009042000209Skin · crackedDURING C-SCAN INSPECTION FOUND 1EA 1.75 INCH LONG CRACK ON S-23LT 3 INCHES AFT OF STA 727D. INSTALLED REPAIR PER 53-00-01, REPAIR 31, FIG 201, PROCEDURE V. PLACED ON DIP PER EC/RA 5331-01399, BEFORE THE ACCUMULATION OF 60,000 TOTAL AIRCRAFT FLT CYCLES, ACCOMPSDR CALA2009032400162Battery Pack · dischargedL2 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED AFT LEFT BATTERY PACK FOR THE L2 DOOR EMERGENCY LIGHTS.SDR CALA2009031600142Skin · crackedRT AFT FUSELAGE AFT OF STA 787 S-18R SHOWS CRACK APPROX 2 INCHES LONG. REPAIRED AS PER SRM REF 53-00-01 REPAIR 5.SDR CALA2009031600141Skin · crackedRT AFT FUSELAGE AT STA 767 S-23R C-SCAN SHOWS INDICATION OF CRACK. REPAIRED AS PER SRM 53-00-01 REPAIR 5.SDR CALA0800115Intercostal · crackedBS 294.5 STRINGER 7L INTERCOSTAL WEB CRACKED AT IB FORWARD CORNER. REMOVED AND REPLACED PER ECRA 5310-04700.SDR CALA0800114Link · corrodedRT MAIN GEAR STABILIZER LINK HAS CORROSION AT END. REMOVED AND REPLACED RT MAIN GEAR STABILIZER LINK PER MM 57-15-00.SDR CALA0800106Attach Angle · crackedATTACH ANGLE CRACKED AT STA350 STRINGER 15L AFT SIDE OF L-1 DOOR. REMOVED AND REPLACED ANGLE PER SRM 51-40-02 AND EA 354-53-002 CAL REV 2.SDR CALA0800107Seat Track · corrodedFOUND RBL 18 HAS SIGNS OF SURFACE CORROSION. REMOVED FLOORBOARDS FOR FOM IAW SRM 51-40-02. REMOVED AND REPLACED CORRODED SEAT TRACK SECTION IAW SRM 53-00-52 FIG 201 AND SRM 51-40-02. REINSTALLED FLOORBOARDS IAW SRM 51-40-02 SEALED FLOORBOARDS PER AMM 51-30-SDR CALA0500283Keelbeam · corrodedINSPECTION FOUND KEEL BEAM CORRODED AT STA 500D-540, S28R. THE CORRODED SECTION OF KEEL BEAM WAS CUT OUT AND A NEW SECTION OF KEEL BEAM WAS INSTALLED IAW ECRA 5311-01236.SDR CALA0500270Stringer · corrodedINSPECTION FOUND STRINGER 25R IN THE AFT BAGGAGE BIN CORRODED AT STA 867-887, RBL 27. A SECTION OF STRINGER AND DOUBLERS WAS INSTALLED IAW SRM 53-00-03.SDR CALA0500267Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN LT MAIN FRAME BELOW MAIN DECK FLOOR AT STA 616, S18L TO S19L. A FILLER AND ANGLE REPAIR WAS INSTALLED IAW ECRA 5311-01158, PAGE 1-9.SDR CALA0500090Skin · crackedA 3 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN DURING WALKAROUND. THE CRACK WAS LOCATED APPROXIMATELY 2.5 FEET FORWARD OF AFT CARGO DOOR AND 2.5 FEET BELOW WATER LINE AND BETWEEN STRINGERS 19R AND 20R (THREE FEET FORWARD OF STA 767). A REPAIR DOUBLER WAS INSTSDR CALA0400465Charger · inoperativeTHE EMERGENCY LIGHTS IN FIRST CLASS CABIN AND AT FORWARD SERVICE ENTRY DOOR WERE FOUND INOPERATIVE. THE BATTERY CHARGER AT STA 338 WAS REPLACED IAW MM 33-51-51.SDR CALA0400105Skin · crackedINSPECTION FOUND A 0.75 INCH CRACK IN NR 2 PYLON STRUT SKIN AT ACCESS DOOR 5824R CUTOUT, TOP FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5430-01204.SDR CALA0400100Skin · delaminatedINSPECTION FOUND THE NR 1 T/E FOREFLAP DELAMINATED BELOW NR 2 SPOILER PANEL, LT WING. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-37.SDR CALA0400099Skin · puncturedINSPECTION FOUND RT WING NR 6 FLIGHT SPOILER PANEL PUNCTURED IN CENTER SECTION. REPAIRED SPOILER PANEL IAW SRM 57-70-1.SDR CALA0400091Strap · corrodedINSPECTION FOUND STRAP UNDER BEAM AT C-2 DOOR CUTOUT I/B SILL STRUCTURE CORRODED AT STA 800. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0400090Strap · corrodedINSPECTION FOUND STRAP I/B OF C-2 DOOR THRESHOLD CORRODED FROM STA 787 TO 847 IN AFT BAG BIN. REPLACED STRAP IAW SRM 51-40-02.SDR CALA0400082Attach Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN ATTACH ANGLE I/B OF NR 2 PYLON JUST AFT OF MIDSPAR ATTACH BOLT. REPAIRED ANGLE IAW SRM 51-70-12.SDR CALA0300520Fan · seizedTHE NR 2 ENGINE GAVE OFF A LOUD BANG FOLLOWED BY VIBRATION AND THE ENGINE SPOOLED DOWN TO IDLE. THE ENGINE NEVER DID SHUTDOWN. CREW WAS UNABLE TO GET POWER ABOVE IDLE. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ENGSDR CALA0300005Pressure Panel · crackedINSPECTION FOUND AN 8 INCH CRACK IN LT MAIN WHEEL WELL PRESSURE DECK WEB AT STA 664-675. THE AREA WAS REPAIRED IAW SRM 53-60-51.SDR CALA0300003Skin · crackedINSPECTION FOUND A 1/4" CRACK IN BELLY SKIN AFT OF EXHAUST DUCT. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02894.SDR CALA0200587Oven · malfunctionedFLIGHT ATTENDANTS REPORTED SMOKE COMING FROM BEHIND OVENS IN AFT GALLEY WHILE AT CRUISE EN ROUTE TO CLE. ASSOCIATED CIRCUIT BREAKERS WERE PULLED AND THE SMOKE CEASED. THE FLIGHT WAS CONTINUED TO CLE WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUNDSDR CALA0200492Megaphone · weakINSPECTION FOUND AFT PORTABLE MEGAPHONE WEAK. THE MEGAPHONE WAS REMOVED AND REPLACED.SDR CALA0100961Skin · gougedFORWARD BAG BIN DOOR INNER SKIN PREVIOUS REPAIR DAMAGED / GOUGED. INSTALLED REPAIR DOUBLER PER EC/RA 5230-01633.SDR CALA0100957Skin · crackedLIGHTING HOLES DAMAGED ABOVE COUNTER BALANCE CABLES AT A/B/B (1" CRACK). INSTALLED REPAIR AS PER EC/RA 5230-01632.SDR CALA0100955Web · dentedFORWARD CARGO DOOR INNER SKIN LOWER CENTER DENT AT LIGHTENING HOLE. INSTALLED DOUBLER REPAIR PER EC/RA 5230-1631.SDR CALA0100949Skin · crackedTHIRD LIGHTENING HOLE FROM AFT END OF DOOR AND THIRD LIGHTENING HOLE FROM TOP OF DOOR HAS A CRACK. INSTALLED REPAIR PER EC/RA 5230-01630.SDR CALA0100945Doubler · gouged#2 ENGINE PYLON UPPER LEFT SIDE OF PYLON ACCESS PANEL 5827 SUPPORT FOR PANEL HAS DEEP GOUGES. BLENDED AREA. INSTALLED DOUBLER PER EC/RA 5430-01230.SDR CALA0100939Sill · corrodedINSPECTION FOUND AFT BAGGAGE BIN FORWARD LOWER SILL CORRODED AT STA 767-787, S26R. THE SILL WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100938Cargo Track · corrodedINSPECTION FOUND RT TIE DOWN CHANNEL CORRODED AROUND FASTENERS AT STA 500A-500D IN FORWARD BAGGAGE BIN. THE TIE DOWN CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100937Seat Track · crackedINSPECTION FOUND A 2 INCH CRACK COMING FROM HI-LOC HOLE IN BOTH THE RT AND LT O/B FLOOR TRACKS AT STA 727B. BOTH FLOOR TRACKS WERE REPAIRED IAW ECRA 5310-04202.SDR CALA0100935Doubler · damagedINSPECTION FOUND SKIN DOUBLER TORN IN TWO LOCATIONS AT EXHAUST DUCT ATTACH POINT IN E&E COMPARTMENT BELLY OF AIRCRAFT. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100928Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CAP CORRODED AT STA 947.5, LBL 6 TO RBL 6. THE FLOORBEAM UPPER CAP WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100925Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT STA 294, RBL 53. THE FLOORBEAM UPPER SURFACE WAS REPAIRED IAW SRM 53-10-51.SDR CALA0100921Fitting · corrodedINSPECTION FOUND GALLEY MOUNT FITTINGS ON FLOORBEAM CORRODED AT STA 270-294, RBL 43 AND AT STA 294, RBL 12. THE TWO GALLEY MOUNT FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0100919Angle · corrodedINSPECTION FOUND FWD LAV WALL MOUNT L-ANGLES ON HAT SECTION CORRODED AT STA 302, LBL 36-56 AND AT STA 306, LBL12-43. NEW ANGLES WERE INSTALLED IAW SRM 51-40-02.SDR CALA0100920Channel · corrodedINSPECTION FOUND FWD LAV WALL HAT SECTION CORRODED AT STA 306, LBL 36-56. THE HAT SECTION WAS REPLACED IAW SRM 51-40-02.SDR CALA0100918Channel · corrodedINSPECTION FOUND U-CHANNEL UNDER L-1 DOOR THRESHOLD CORRODED AT STA 312-344. THE CHANNEL WAS REPLACED IAW SRM 51-40-00.SDR CALA0100917Seat Track · corrodedINSPECTION FOUND L/H O/B SEAT TRACK CORRODED AT STA 360-380. THE SEAT TRACK WAS REPLACED IAW SRM 53-00-52.SDR CALA0100916Fitting · corrodedINSPECTION FOUND L-1 DOOR GIRT BAR LATCH ATTACH FITTING CORRODED AT STA 344. THE ATTACH FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100915Angle · corrodedINSPECTION FOUND ANGLE BELOW SCUFF PLATE AREA OF R-1 DOOR JAMB CORRODED AT STA 298-328. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100914Stiffener · crackedINSPECTION FOUND AN 8" CRACK IN STIFFENER LOCATED JUST FORWARD OF HORSE COLLAR IN #6 FLAP TRACK FAIRING. THE STIFFENER WAS REPLACED IAW SRM 51-10-02.SDR CALA0100913Angle · corrodedINSPECTION FOUND L-1 DOORWAY ANGLE CORRODED AT STA 312-344, LBL 60. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100912Stiffener · crackedINSPECTION FOUND A 5" CRACK IN ANGLE STIFFENER INSIDE #3 FLAP TRACK FAIRING. THE ANGLE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0100911Splice · crackedINSPECTION FOUND A 5" CRACK IN #3 FLAP TRACK FAIRING SPLICE. THE #3 FAIRING SPLICE WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0100908Skin · crackedINSPECTION FOUND A 1.125" CRACK AT UPPER R/H CORNER I/B SIDE OF CO-PILOT'S R/H WINDOW POST SKIN AND GUSSET. THE CRACKED AREA WAS ROUTED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-10-1, FIGURE 210.SDR CALA0100906Angle · crackedINSPECTION FOUND A 2" CRACK IN INTERCOSTAL UPPER ANGLE AT STA 380-400, BL 0. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-02.SDR CALA0100905Stringer · crackedINSPECTION FOUND A 6" CRACK IN STRINGER 10R AT STA 338. A NEW STRINGER WAS INSTALLED IAW SRM 51-40-02.SDR CALA0100904Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 967-986.5, LBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Back to N14335, cancelled Mar 21, 2013