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.

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 EMERNov 21, 2025 · N783TW · Doug DC915F · Cabin Temperature Control SystemSDR 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. PMar 15, 2025 · N783TW · Doug DC915 · Air Conditioning System WiringSDR 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. PFeb 19, 2025 · N783TW · Doug DC915F · Air Conditioning System WiringSDR 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 SHSep 17, 2018 · N783TW · Doug DC915F · Entrance StairsSDR 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.May 20, 2018 · N783TW · Doug DC915F · Air Distribution SystemSDR MJYA20160825012Portable Light · inoperativeEMERGENCY EXIT LIGHT SYSTEM, PORTABLE EMERGENCY EXIT LIGHT WILL NOT ACTIVATE WHEN SELECTED TO ON. AWAITING DETAILS ON REPAIR.Aug 25, 2016 · N783TW · Doug DC915F · Emergency LightingSDR 7AHR2016060300001Depressor · gougedFORWARD MAIN ENTRY DOOR JAMB UPPER AFT SEAL DEPRESSOR BENT AND GOUGED.Jun 3, 2016 · N783TW · Doug DC915F · Fuselage Miscellaneous StructureSDR 7AHR548B9082157Panel · cracked1.5 INCH CRACK RT TRAPEZOIDAL PANEL BETWEEN BOLT HOLES COMMON TO THE HORIZONTAL FLANGE OF THE LOWER SUPPORT FITTING.Jun 3, 2016 · N783TW · Doug DC915F · Fuselage Miscellaneous StructureSDR 7AHR201606020451Access Panel · cracked1.75" LONG CRACK IN FUEL TANK ACCESS PANEL LANDING ON LT WING UPPER SURFACE AT WING BS XRS 111.Jun 2, 2016 · N783TW · Doug DC915F · Wing, Plate/SkinSDR 7AHR20160602Spar Cap · crackedCRACK IN RT INBD L/E UPPER SPAR CAP APPROXIMATELY 2" IN LENGTH THROUGH THE 2 MOST INBD UPPER BOLTS.Jun 1, 2016 · N783TW · Doug DC915F · Wing SparSDR MJYA20150630004Skin · damagedFUSELAGE WINDOW BELT SKIN REPAIR STATION 422.5, L 11R TO L 15R.Jun 30, 2015 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR 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 THROUGOct 12, 2013 · N783TW · Doug DC915F · Cabin Pressure Control SystemSDR MJYA201309120016Light · inoperativeEMERGENCY LIGHTS INOPERATIVE.Sep 6, 2013 · N783TW · Doug DC915F · Emergency LightingSDR MJYA201309120010Spar · crackedLT ELEVATOR SPAR FORWARD SPAR CRACKED BEYOND LIMITS.Sep 3, 2013 · N783TW · Doug DC915F · Elevator, Spar/RibSDR MJYA201309120014Structure · corrodedLEFT VERTICAL STAB HAS CORROSION.Sep 1, 2013 · N783TW · Doug DC915F · Vertical StabilizerSDR MJYA201309120015Floorboard · crackedMAIN DECK FLOORBOARD CRACKED SEVERAL PLACES.Aug 31, 2013 · N783TW · Doug DC915F · Fuselage Floor PanelSDR MJYA201309120012Skin · corrodedLT AFT SKIN CORRODED OUT OF LIMITS.Aug 31, 2013 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR MJYA201309120011Tee Fitting · corrodedCANTED BULKHEAD LOWER TEE CORRODED.Aug 31, 2013 · N783TW · Doug DC915F · Fuselage Main, BulkheadSDR MJYA201309120013Skin · corrodedRT VERTICAL STABILIZER HAS CORROSION ON EXTERIOR SKIN.Aug 29, 2013 · N783TW · Doug DC915F · Vertical Stabilizer, Plate/SkinSDR MJYA201309120009Frame · corrodedCANTED FRAME AT BS 796 LT IS CORRODED OUT OF LIMITS.Aug 27, 2013 · N783TW · Doug DC915F · Fuselage Main, FrameSDR MJYA20130827008Frame · corrodedUPPER AND MID LT CANTED FRAME CORRODED AND FOUND TO BE OUT OF LIMITS AT BS 989.Aug 26, 2013 · N783TW · Doug DC915F · Fuselage Main, FrameSDR MJYA20130813007Structure · corrodedACFT LT SIDE REAR FUSELAGE, UN-PRESSURIZED AREA AFT OF VENT LOUVERS HAS CORROSION.Aug 12, 2013 · N783TW · Doug DC915F · Fuselage Main, StructureSDR MJYA20130813006Skin · crackedSKIN CRACKED AT BS 340 BETWEEN L17 - 18R.Aug 12, 2013 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR MJYA20130813005Skin · corrodedCORROSION ON OUTER SKIN AT BS 566 BELOW OVERWING EXITS.Aug 12, 2013 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR MJYA201308100002Window Frame · crackedRT NR 11 PASSENGER COMPARTMENT WINDOW CUTOUT HAS CRACK INDICATION LOWER AFT CORNER.Aug 7, 2013 · N783TW · Doug DC915F · Fuselage Main, StructureSDR MJYA201308100001Door Frame · crackedAFT PRESSURE BULKHEAD DOOR FRAME CRACKED APPROX 12 INCHES FROM BOTTOM FRAME.Aug 7, 2013 · N783TW · Doug DC915F · Fuselage Main, StructureSDR MJYA201308100003Bulkhead · corrodedAFT PRESSURE BULKHEAD EXTERNAL SIDE, SURFACE CORROSION FOUND UNDER ADHESIVE, 9 O`CLOCK POSITION APPROX 1.5' FROM DOOR FRAME LT BULKHEAD.Aug 6, 2013 · N783TW · Doug DC915F · Fuselage Main, BulkheadSDR MJYA201308090001Skin · crackedFUSELAGE SKIN CRACKED BS256 BETWEEN LONGERONS 4 & 5 LT.Aug 6, 2013 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR EE4Y1009370Frame · crackedUPPER FUSELAGE MAIN CARGO CABIN AT STA Y 446 AT LEVEL LONGERON 18L FRAME WITH CRACK.Sep 2, 2010 · N783TW · Doug DC915F · Fuselage Main, FrameSDR EE4Y1009369Support Fitting · crackedMAIN CARGO CABIN SUPPORT FITTING CRACKED AT STA Y 446 BETWEEN LONGERON 18L AND 19L.Sep 2, 2010 · N783TW · Doug DC915F · Fuselage Miscellaneous StructureSDR EE4Y1009368Door Frame · crackedUPPER FUSELAGE PAX CABIN STA Y 441 BETWEEN LONGERON 18 AND 19 LT DOOR FRAME CRACKED.Sep 2, 2010 · N783TW · Doug DC915F · Fuselage Main, StructureSDR EE4Y1009367Fitting · crackedUPPER FUSELAGE PAX CABIN STA 441 BETWEEN LONGERON 18 AND 19 LT FRAME FWD SECTION FITTING CRACKED.Sep 2, 2010 · N783TW · Doug DC915F · Fuselage Main, Attach FittingsSDR EE4Y1008350Skin · crackedDURING INSPECTION EMPENNAGE VERTICAL STABILIZER RUDDER SKIN WITH CRACK AT ZR27.25 RT.Aug 18, 2010 · N783TW · Doug DC915F · Rudder, Plate/SkinSDR EE4Y1008349Skin · scratchedDURING INSPECTION UPPER FUSELAGE EXTERIOR FUSELAGE SKIN WITH SCRATCH AT STA Y147.Aug 18, 2010 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR EE4Y1008348Skin Panel · corrodedDURING INSPECTION RT WING FLAP T/E PANEL NR 3 LOWER SKIN WITH CORROSION.Aug 18, 2010 · N783TW · Doug DC915F · Trailing Edge FlapsSDR EE4Y1008331Web · crackedUPPER FUSELAGE CARGO CABIN VERTICAL WEB WITH CRACK AT Y STA 525,+X=58,Z=-1.Aug 11, 2010 · N783TW · Doug DC915F · Fuselage Miscellaneous StructureSDR EE4Y1008324Angle · crackedDURING INSPECTION LOWER FUSELAGE AFT ACCESSORY COMPT LATERAL UPPER ANGLE WITH CRACK AT CANTED STA 962.019,-X=17.5.Aug 10, 2010 · N783TW · Doug DC915F · Fuselage Miscellaneous StructureSDR EE4Y1008323Angle · crackedDURING INSPECTION LOWER FUSELAGE AFT ACCESSORY COMPT LATERAL ANGLE BLENDED AND CRACK AT CANTED STA 965,-X=17.5.Aug 10, 2010 · N783TW · Doug DC915F · Fuselage Miscellaneous StructureSDR EE4Y1008322Skin · crackedDURING INSPECTION UPPER FUSELAGE SKIN WITH CORROSION FROM Y STA 474 AND Y STA 642, BETWEEN LONGERON 16L AND 19L CORRODED.Aug 10, 2010 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR EE4Y1008321Door Frame · corrodedDURING INSPECTION MAIN CARGO CABIN DOOR LOWER JAMB BEAM WITH CORROSION AT SEVERAL PLACES BETWEEN Y STA 303 AND Y STA 439.Aug 10, 2010 · N783TW · Doug DC915F · Fuselage Main, StructureSDR EE4Y1008320Skin Panel · dentedDURING INSPECTION RT WING FLAP T/E LOWER PANEL SKIN WITH DENTS AT XS 114 AND XS 94.Aug 10, 2010 · N783TW · Doug DC915F · Trailing Edge FlapsSDR EE4Y1008318Shear Tie · corrodedDURING INSPECTION UPPER FUSELAGE AFT ACCESSORIES COMPARTMENT BETWEEN LONGERON 1L AND 2L Y STA 908 FRAME, SHEAR TIE WITH CRACK.Aug 10, 2010 · N783TW · Doug DC915F · Fuselage Internal Mounting StructureSDR EE4Y1008276Skin · crackedDURING INSPECTION RUDDER WITH CORROSION SKIN AT LT BETWEEN ZR 94 AND ZR 99.Aug 6, 2010 · N783TW · Doug DC915F · Rudder, Plate/SkinSDR EE4Y1008275Angle · crackedDURING INSPECTION LT WING FLAP INTERNAL, FLAP FRONT SPAR LOWER ANGLE WITH CORROSION AT XF 72.Aug 6, 2010 · N783TW · Doug DC915F · Trailing Edge FlapsSDR EE4Y1008273Frame · crackedDURING INSPECTION UPPER FUSELAGE CARGO CABIN RT AT Y STA 585,-X59,-Z4 OVER WHEEL WELL FRAME AFT POCKET AREA WITH CRACK.Aug 6, 2010 · N783TW · Doug DC915F · Fuselage Main, FrameSDR EE4Y1008274Skin · dentedDURING INSPECTION LOWER FUSELAGE SKIN WITH DENT BETWEEN Y STA 381 AND Y STA 395 BETWEEN LONGERONS 19L AND 21L.Aug 6, 2010 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR EE4Y1008272Frame · crackedDURING INSPECTION UPPER FUSELAGE MAIN CARGO CABIN Y STA 525 BETWEEN LONGERONS 18L AND 19L FUSELAGE FRAME WEB CRACKED.Aug 6, 2010 · N783TW · Doug DC915F · Fuselage Main, FrameSDR EE4Y1008271Frame · crackedDURING INSPECTION UPPER FUSELAGE MAIN CARGO CABIN Y STA 544 BETWEEN LONGERONS 18R AND 19R FUSELAGE FRAME WEB CRACKED.Aug 6, 2010 · N783TW · Doug DC915F · Fuselage Main, FrameSDR 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.Aug 6, 2010 · N783TW · Doug DC915F · Fuselage Main, Plate/SkinSDR EE4Y1008269Frame · crackedDURING INSPECTION AFT FUSELAGE SUPPORT CANTED BULKHEAD LOWER FRAME WITH CORROSION AT CANTED STA 964,-X19.Aug 6, 2010 · N783TW · Doug DC915F · Fuselage Main, Frame
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