N783TW
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 = 'N783TW' 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 = 'N783TW' 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 MJYA20251121013Butterfly Valve · stuckTWO HOURS INTO CRUISE AT FL 350 ENCOUNTERED A LOSS OF CABIN PRESSURE. RAN COM PROCEDURES CABIN ALTITUDE WARNING/RAPID DEPRESSURIZATION. CABIN RECOVERED AND HELD AT 8500 FEET FOR ABOUT 20 MIN BEFORE A RAPID SPIKE IN CABIN CLIMB (FULL SCALE) INITIATED AN EMERSDR MJYA2025031400061Connector · damagedWHILE CRUISING AT FL350 A MASTER WARNING LIGHT ILLUMINATED, THE CABIN PRESSURE LIGHT WAS ALSO ILLUMINATED. BOTH THE CAPTAIN AND FIRST OFFICER COMPLETED THE IMMEDIATE ACTION ITEMS FOR A CABIN PRESSURE WARNING, THEN COMPLETED THE COM PROCEDURE FOR THE WARNING. PSDR MJYA20250314001Elec Connector · damagedWHILE CRUISING AT FL350 A MASTER WARNING LIGHT ILLUMINATED, THE CABIN PRESSURE LIGHT WAS ALSO ILLUMINATED. BOTH THE CAPTAIN AND FIRST OFFICER COMPLETED THE IMMEDIATE ACTION ITEMS FOR A CABIN PRESSURE WARNING, THEN COMPLETED THE COM PROCEDURE FOR THE WARNING. PSDR MJYA20180917002Bolt · shearedTHE ATTACH BOLTS REFERENCE IPC 52-60-04-01 ITEM 105 P/N NAS1203-9 ITEM 110 P/N NAS1103-9 THAT SECURE RETAINER ASSEMBLY (VENTRAL STAIR DOOR BEARING) REFERENCE IPC 52-60-04-01 ITEM 26 P/N 3917209-501 TO ADJACENT STRUCTURE AND AFT STAIR ACTUATING MECHANISIMS SHSDR MJYA20180522001Clamp · looseDURING CRUISE ALTITUDE 35.0, THE AIRCRAFT STARTED LOSING PRESSURIZATION AND THE CABIN ALTITUDE CLIMBED TO 11.5 K FEET. THE PILOT DECLARED AN EMERGENCY AND DECENDED TO 10K FEET, LANDED WITHOUT INCIDENT. FOUND A DUCT CLAMP LOOSE.SDR MJYA20160825012Portable Light · inoperativeEMERGENCY EXIT LIGHT SYSTEM, PORTABLE EMERGENCY EXIT LIGHT WILL NOT ACTIVATE WHEN SELECTED TO ON. AWAITING DETAILS ON REPAIR.SDR 7AHR2016060300001Depressor · gougedFORWARD MAIN ENTRY DOOR JAMB UPPER AFT SEAL DEPRESSOR BENT AND GOUGED.SDR 7AHR548B9082157Panel · cracked1.5 INCH CRACK RT TRAPEZOIDAL PANEL BETWEEN BOLT HOLES COMMON TO THE HORIZONTAL FLANGE OF THE LOWER SUPPORT FITTING.SDR 7AHR201606020451Access Panel · cracked1.75" LONG CRACK IN FUEL TANK ACCESS PANEL LANDING ON LT WING UPPER SURFACE AT WING BS XRS 111.SDR 7AHR20160602Spar Cap · crackedCRACK IN RT INBD L/E UPPER SPAR CAP APPROXIMATELY 2" IN LENGTH THROUGH THE 2 MOST INBD UPPER BOLTS.SDR MJYA20150630004Skin · damagedFUSELAGE WINDOW BELT SKIN REPAIR STATION 422.5, L 11R TO L 15R.SDR MJYA201310150017Cabin Pressure · malfunctionedCLIMBING THROUGH APPROXIMATELY 14,000 FEET OBSERVED NO AIRFLOW COMING FROM THE AIR VENTS, CHECKED THE CABIN ALTITUDE AND IT WAS 9,000 FT AND CLIMBING 1,000 FPM. BEFORE PROCEDURES, CABIN PRESSURE AND MASTER WARNING LIGHTS ILLUMINATED DURING DESCENT THROUGSDR MJYA201309120016Light · inoperativeEMERGENCY LIGHTS INOPERATIVE.SDR MJYA201309120010Spar · crackedLT ELEVATOR SPAR FORWARD SPAR CRACKED BEYOND LIMITS.SDR MJYA201309120014Structure · corrodedLEFT VERTICAL STAB HAS CORROSION.SDR MJYA201309120015Floorboard · crackedMAIN DECK FLOORBOARD CRACKED SEVERAL PLACES.SDR MJYA201309120012Skin · corrodedLT AFT SKIN CORRODED OUT OF LIMITS.SDR MJYA201309120011Tee Fitting · corrodedCANTED BULKHEAD LOWER TEE CORRODED.SDR MJYA201309120013Skin · corrodedRT VERTICAL STABILIZER HAS CORROSION ON EXTERIOR SKIN.SDR MJYA201309120009Frame · corrodedCANTED FRAME AT BS 796 LT IS CORRODED OUT OF LIMITS.SDR MJYA20130827008Frame · corrodedUPPER AND MID LT CANTED FRAME CORRODED AND FOUND TO BE OUT OF LIMITS AT BS 989.SDR MJYA20130813007Structure · corrodedACFT LT SIDE REAR FUSELAGE, UN-PRESSURIZED AREA AFT OF VENT LOUVERS HAS CORROSION.SDR MJYA20130813006Skin · crackedSKIN CRACKED AT BS 340 BETWEEN L17 - 18R.SDR MJYA20130813005Skin · corrodedCORROSION ON OUTER SKIN AT BS 566 BELOW OVERWING EXITS.SDR MJYA201308100002Window Frame · crackedRT NR 11 PASSENGER COMPARTMENT WINDOW CUTOUT HAS CRACK INDICATION LOWER AFT CORNER.SDR MJYA201308100001Door Frame · crackedAFT PRESSURE BULKHEAD DOOR FRAME CRACKED APPROX 12 INCHES FROM BOTTOM FRAME.SDR MJYA201308100003Bulkhead · corrodedAFT PRESSURE BULKHEAD EXTERNAL SIDE, SURFACE CORROSION FOUND UNDER ADHESIVE, 9 O`CLOCK POSITION APPROX 1.5' FROM DOOR FRAME LT BULKHEAD.SDR MJYA201308090001Skin · crackedFUSELAGE SKIN CRACKED BS256 BETWEEN LONGERONS 4 & 5 LT.SDR EE4Y1009370Frame · crackedUPPER FUSELAGE MAIN CARGO CABIN AT STA Y 446 AT LEVEL LONGERON 18L FRAME WITH CRACK.SDR EE4Y1009369Support Fitting · crackedMAIN CARGO CABIN SUPPORT FITTING CRACKED AT STA Y 446 BETWEEN LONGERON 18L AND 19L.SDR EE4Y1009368Door Frame · crackedUPPER FUSELAGE PAX CABIN STA Y 441 BETWEEN LONGERON 18 AND 19 LT DOOR FRAME CRACKED.SDR EE4Y1009367Fitting · crackedUPPER FUSELAGE PAX CABIN STA 441 BETWEEN LONGERON 18 AND 19 LT FRAME FWD SECTION FITTING CRACKED.SDR EE4Y1008350Skin · crackedDURING INSPECTION EMPENNAGE VERTICAL STABILIZER RUDDER SKIN WITH CRACK AT ZR27.25 RT.SDR EE4Y1008349Skin · scratchedDURING INSPECTION UPPER FUSELAGE EXTERIOR FUSELAGE SKIN WITH SCRATCH AT STA Y147.SDR EE4Y1008348Skin Panel · corrodedDURING INSPECTION RT WING FLAP T/E PANEL NR 3 LOWER SKIN WITH CORROSION.SDR EE4Y1008331Web · crackedUPPER FUSELAGE CARGO CABIN VERTICAL WEB WITH CRACK AT Y STA 525,+X=58,Z=-1.SDR EE4Y1008324Angle · crackedDURING INSPECTION LOWER FUSELAGE AFT ACCESSORY COMPT LATERAL UPPER ANGLE WITH CRACK AT CANTED STA 962.019,-X=17.5.SDR EE4Y1008323Angle · crackedDURING INSPECTION LOWER FUSELAGE AFT ACCESSORY COMPT LATERAL ANGLE BLENDED AND CRACK AT CANTED STA 965,-X=17.5.SDR EE4Y1008322Skin · crackedDURING INSPECTION UPPER FUSELAGE SKIN WITH CORROSION FROM Y STA 474 AND Y STA 642, BETWEEN LONGERON 16L AND 19L CORRODED.SDR EE4Y1008321Door Frame · corrodedDURING INSPECTION MAIN CARGO CABIN DOOR LOWER JAMB BEAM WITH CORROSION AT SEVERAL PLACES BETWEEN Y STA 303 AND Y STA 439.SDR EE4Y1008320Skin Panel · dentedDURING INSPECTION RT WING FLAP T/E LOWER PANEL SKIN WITH DENTS AT XS 114 AND XS 94.SDR EE4Y1008318Shear Tie · corrodedDURING INSPECTION UPPER FUSELAGE AFT ACCESSORIES COMPARTMENT BETWEEN LONGERON 1L AND 2L Y STA 908 FRAME, SHEAR TIE WITH CRACK.SDR EE4Y1008276Skin · crackedDURING INSPECTION RUDDER WITH CORROSION SKIN AT LT BETWEEN ZR 94 AND ZR 99.SDR EE4Y1008275Angle · crackedDURING INSPECTION LT WING FLAP INTERNAL, FLAP FRONT SPAR LOWER ANGLE WITH CORROSION AT XF 72.SDR EE4Y1008273Frame · crackedDURING INSPECTION UPPER FUSELAGE CARGO CABIN RT AT Y STA 585,-X59,-Z4 OVER WHEEL WELL FRAME AFT POCKET AREA WITH CRACK.SDR EE4Y1008274Skin · dentedDURING INSPECTION LOWER FUSELAGE SKIN WITH DENT BETWEEN Y STA 381 AND Y STA 395 BETWEEN LONGERONS 19L AND 21L.SDR EE4Y1008272Frame · crackedDURING INSPECTION UPPER FUSELAGE MAIN CARGO CABIN Y STA 525 BETWEEN LONGERONS 18L AND 19L FUSELAGE FRAME WEB CRACKED.SDR EE4Y1008271Frame · crackedDURING INSPECTION UPPER FUSELAGE MAIN CARGO CABIN Y STA 544 BETWEEN LONGERONS 18R AND 19R FUSELAGE FRAME WEB CRACKED.SDR EE4Y1008270Skin · crackedDURING INSPECTION LOWER FUSELAGE SKIN WITH CORROSION AT PERIPHERY WTBF ATTACHMENT HOLES AREA Y STA 470 TO Y STA 565 BETWEEN LONGERON 23L AND 30L.SDR EE4Y1008269Frame · crackedDURING INSPECTION AFT FUSELAGE SUPPORT CANTED BULKHEAD LOWER FRAME WITH CORROSION AT CANTED STA 964,-X19.
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