N919TW, cancelled Feb 28, 2012

Service difficulty reports · 37

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 = 'N919TW' AND deregistration_id = 'N919TW-2012-02-28'
  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 AALA20060106Switch · inoperativeSMOKE IN CAB IN AND COCKPIT. SOURCE UNDETERMINED. LANDED STL WITHOUT INCIDENT. REPLACED LEFT PACK 130 DEGREE TEMPERATURE LIMIT SWITCH AND BOTH WATER SEPARATORS. ACCOMPLISHED SPECIAL ITEMS CARD 21 96 01. SYSTEM GROUND CHECKED NORMAL OPERATIONS.Feb 19, 2006 · N919TW · Doug DC982 · Cabin Cooling SystemSDR ZW0A0305101Battery · inoperativeTHE EGRESS LIGHTS AT THE OVERWING EMERGENCY EXITS, CAME ON IN FLIGHT WITH THE SWITCH IN ARM POSITION. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-28-03 STL.May 25, 2003 · N919TW · Doug DC982 · Emergency LightingSDR TWAA0102005Generator · malfunctionedAT FL 330 CAPT INSTRUMENTS WENT DEAD AND FLT GUIDANCE CONTROL PANEL FROZE. LT AND RT GEN VOLTS AND FREQS NORMAL. MADE UNSCHEDULED LANDING AT TPA. AFTER LANDING NOTICED LT CSD TEMP WAS LOW. TURNED OFF LT GEN AND INDICATIONS RETURNED TO NORMAL. REPLACED THEJan 31, 2001 · N919TW · Doug DC982 · AC Generation SystemSDR TWAA0100302Smoke · detectedON SHORT FINAL SMOKE APPEARED IN THE CABIN WHEN ANTI-ICE WAS TURNED ON. ACCOMPLISHED PACK BURN OUT AND DEACTIVATED APU PER MEL. CHECK-C 5-12-00 MCI.Jan 3, 2001 · N919TW · Doug DC982 · APU Oil SystemSDR TWAA0008204Motor · damagedDURING DESCENT HAD A CABIN PRESSURIZATION PROBLEM. PASSENGER OXYGEN MASKS DROPPED. FERRY TO MCI FOR CORRECTIONS. AC04 01-28-00 DFW. REPLACED THE OUTFLOW VALVE MOTOR. FOUND THE TACH WINDINGS OF THE MOTORS WERE OPEN.May 22, 2000 · N919TW · Doug DC982 · Pressure Regulator/Outflow ValveSDR TWAA0007205Intercostal · corrodedDURING CHECK-C MAINT INTERCOSTAL AT RBL 16 BETWEEN STA 1307 AND 1323, HAD CORROSION AT BOTH ENDS. REMOVED AND REPLACED INTERCOSTAL AT STA 1322, RBL 15. INSTALLED WITH HI-LOKS PER SRM 51-30-5, AND AD RIVETS PER SRM 51-30-2. INTERCOSTAL FABRICATED PER DAC DRAMay 2, 2000 · N919TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0007204Frame · corrodedDURING CHECK-C MAINT, FOUND FORMER FOOT CORRODED AT STA 1287, AT LONGERON 20L. REMOVED CORROSION PER SPM 6-80-01.May 2, 2000 · N919TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0006913Frame · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON LOWER FLANGE OF FORMER STA 1307, LONGERON 25L TO 28R. SPLICED IN NEW FORMER PER DOUGLAS DRAWING 9912243 AND SRO 9530057.May 1, 2000 · N919TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0008307Outflow Valve · corrodedDURING CC24C, FOUND INTERGRANULAR CORROSION ON THE OUTFLOW VALVE CASTING (SUGAR SCOOP) LOWER AFT SIDE. REPLACED DOUBLER MANUFACTURE NUMBER 5914558-5012 VING TWA NUMBER 163497 PER MDC PRINT NUMBER 5936021. CC24C MCI 04-27-00.Apr 27, 2000 · N919TW · Doug DC982 · Pressure Regulator/Outflow ValveSDR TWAA0007003Cargo Track · corrodedDURING CHECK-C MAINT, THE RT AFT CARGO COMPT TIE DOWN TRACK HAD NUMEROUS PLACES OF CORROSION AT TOP AND BOTTOM OF CLIP NUT LOCATIONS FROM STA 1212 TO 1320. REMOVED AND REPLACED TIE DOWN FLOOR TRACK FROM STA 1212 TO 1320, INSTALLED WITH NAS 7103 SCREWS PER SRMApr 27, 2000 · N919TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0006609Frame · corrodedDURING CHECK-C MAINT, FOUND CORROSION IN LOWER FLANGE OF FORMER 1271, BETWEEN LONGERON 28L AND 30. REMOVED CORROSION PER SRM 53-10-03. REPAIRED PER SRM 53-03, PAGE 4A. PRIMED PER SRM 51-10-3B.Apr 24, 2000 · N919TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0006309Floor Support · corrodedDURING CHECK-C MAINT, FOUND CORROSION BEYOND LIMITS ON FLOOR SUPPORT STA 1322, LONGERON 23R TO 23L. FABRICATED NEW FLOOR SUPPORTS FROM 0.040 2024 PER SPM 6-70-01 AND SRM 51-10-2A. INSTALLED FASTENERS PER SRM 51-30-2.Apr 23, 2000 · N919TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0006308Skin · damagedDURING CHECK-C MAINT, THE FWD LT PAX DOOR SKIN ALONG THE BOTTOM EDGE WAS DISTORTED. REPAIRED SKIN ALONG BOTTOM EDGE BY STRENGHTENING AND REPAIRED PER SRM 52-05, FIG 32 SHEET 1 AND 3.Apr 21, 2000 · N919TW · Doug DC982 · Passenger/Crew DoorsSDR TWAA0006307Casting · crackedDURING CHECK-C MAINT, THE LT WING FWD END OF GROUND SPOILER ATTACH CASTING WAS CRACKED BOTH I/B AND O/B SIDE OF ACT ATTACH FWD END. STOP DRILLED CRACKS PER SRO 9570010-5. INSTALLED DOUBLER FILLER AND STIFFENER PER SRO 9570010-5, FIG 6 PAGE 45-62.Apr 20, 2000 · N919TW · Doug DC982 · Drag Control ActuatorSDR TWAA0006306Actuator · crackedDURING CHECK-C MAINT, THE RT WING FWD END OF GROUND SPOILER ACTUATOR ATTACH CASTING WAS CRACKED I/B AND O/B SIDE AT FWD END, PER BOEING DAC SB 57-180 VIEW DD CONDITION 4. ACCOM HIGH FREQ EDDY CURRENT PER TWA NDT 51-00-01 PART 6 FOR CRACK CONTAINMENT. STOP DRApr 20, 2000 · N919TW · Doug DC982 · Drag Control ActuatorSDR TWAA0006305Structure · bentDURING CHECK-C MAINT, THE FWD ENTRY DOOR WAS BENT AT THE BOTTOM FWD AND AFT ENDS. REPAIRED SKIN PER SRM 52-05 PAGE 32, AND 52-03 PAGE 1.Apr 19, 2000 · N919TW · Doug DC982 · Passenger/Crew DoorsSDR TWAA0006304Dome Nut · corrodedDURING CHECK-C MAINT, FOUND RT FUSELAGE CORROSION AROUND DOME NUT HOLES AT STA 769 TO 807, AREA OF LONGERON 28R. REMOVED CORROSION PER SPM 6-80-01. CHECKED MATERIAL LOSS 45 PER CENT BY NDT. REPAIRED PER SRM 53-04 FIG 53 SHEET 1 TO 5. TREATED PER SRM 51-10.Apr 18, 2000 · N919TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0006303Seat Track · corrodedDURING CHECK-C MAINT, THE RT CHAIR TRACK HAD CORROSION FROM STA 1079 TO 1155, WL 200. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK USING SCREWS NAS 7103, WASHERS (P/N NAS1252-10H), NUTS (P/N MS21042L3), AND RIVETS MS 20426AD6.Apr 18, 2000 · N919TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0006005Seat Track · corrodedDURING C CHECK, THE LT OTBD SEAT TRACK WAS BLENDED BEYOND LIMITS, STA 1231 TO 1240, LONGERON 54. REPLACED SEAT TRACK AT STA 1231 TO 1309 PER DRAWING 5930566. ---CLOSED---Apr 14, 2000 · N919TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0006004Floor Support · corrodedDURING C CHECK, IN AFT CARGO BAY, STA 1211, LONGERON 29 LT, AFT FACE OF SUPPORT HAD CORROSION ON FLOOR SUPPORT AT STA 1211, LONGERON 29 RT TO 30 RT. REPLACED FLOOR SUPPORT WITH NEW PER SRM 51-10-4. ---CLOSED---Apr 14, 2000 · N919TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0006110Forging · crackedDURING C CHECK, AT CABIN STA 1338, LONGERON 18 RT, WHERE 3 LEGGED FORGING ATTACHES TO FRAME TO FLOORBEAM, THE VERTICAL LEG WAS CRACKED AND CORRODED. REPLACED FITTING PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-10-5B. PAINTED PER SRM 51-10-3B. ---CLOSApr 11, 2000 · N919TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0005803Floorbeam · crackedDURING C CHECK, MAINT FOUND CRACK IN FLOORBEAM CAP AT STA 237, RBL 4, CARGO CEILING AREA. FABRICATED NEW FLOORBEAM CAP PER SPM 6-70-01 AND SRM 51-10-03. ---CLOSED---Apr 7, 2000 · N919TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0004002Link · brokenON LANDING GEAR RETRACTION, THE RT GEAR UNSAFE LIGHT AND GEAR DOOR WARNING LIGHT WERE ON. SLOWED TO 180 KTS AND CYCLED GEAR, NO HELP. FLIGHT RETURNED TO STL. REPLACED THE LOWER ACTUATOR LINK ON THE RT MAIN GEAR. CHECK-C 5-5-99 MCI.Mar 10, 2000 · N919TW · Doug DC982 · Landing Gear Door Retract SectionSDR TWAA0003403Light · inoperativeTHE LEFT SIDE FORWARD CABIN DOOR PORTABLE EMERGENCY LIGHT ON-OFF SWITCH WAS BROKEN. REPLACED THE LIGHT ASSY. CHECK-C 5-5-99 MCI.Feb 29, 2000 · N919TW · Doug DC982 · Emergency LightingSDR TWAA9906801Link · brokenAFTER TAKEOFF AND GEAR RETRACTION THE LEFT GEAR RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ON. RECYCLED THE GEAR, NO HELP. FLIGHT RETURNED TO STL. FOUND THE LEFT GEAR DOOR ACTUATOR UPLINK BROKEN. REPLACED THE LINK ASSEMBLY. CHECK-C 4-19-99 MCI.May 10, 1999 · N919TW · Doug DC982 · Landing Gear Door Retract SectionSDR TWAA9902902Beam · crackedFOUND THE FORWARD RIGHT CABIN DOOR HAD THE BOTTOM DOOR BEAM CRACKED. INSTALLED NEW DOOR BEAM PER SRM 51-30-2. CHECK-C 8-27-98 STL.Feb 18, 1999 · N919TW · Doug DC982 · Service DoorsSDR TWAA9817101Batteries · dischargedOVERHEAD EMERGENCY EXIT LIGHTS AND COCKPIT EMERGENCY LIGHTS WERE REPORTED INOPERATIVE. REPLACED BATTERIES IN FWD POWER SUPPLY. CHECK-C 8-27-98 STL.Oct 22, 1998 · N919TW · Doug DC982 · Emergency LightingSDR TWAA9814001Bulkhead Tee · creasedDURING CHECK-C MAINT, FOUND CREASE ON BULKHEAD TEE STA 1338, BETWEEN LONGERON 29R AND 29L. REMOVED AND REPLACED TEE PER SRM 53-03, FIG 37A.Aug 24, 1998 · N919TW · Doug DC982 · Fuselage Main, BulkheadSDR TWAA9809701Compressor · stalledDCA - FLT 797 - AT FL 330 TO 350 RT ENGINE HAD SEVERAL STALLS. REDUCED THROTTLE TO IDLE AND STALLS STOPPED. DECLARED EMERGENCY AND DIVERTED TO DCA. REPLACED ENGINE. (M)Jun 17, 1998 · N919TW · Doug DC982 · Turbine Engine Compressor SectionSDR TWAA9808301Oven · malfunctionedSTL - FLT 100 - DURING CRUISE, THE COACH GALLEY OVEN L2 EMITTED STRONG ELECTRICAL FUMES. REPLACED THE AFT GALLEY L2 OVEN MFG P/N 50381. (M)May 25, 1998 · N919TW · Doug DC982 · Buffet/GalleysSDR TWAA9803102Target · missingOMA - FLT 38 - AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO OMA. DOOR INDICATION PLACARDED PER MEL. ON ACFT LAYOVER, THE DOOR SENSOR WAS REPLACED AND THE MISSING DOOR SENSOR TARGET WAS INSTALLED. SENSOR PART NR 8-340-02. CHECK-C 8-9-97 MCI.Mar 3, 1998 · N919TW · Doug DC982 · Door Warning SystemSDR TWAA9802402Bearing · failedMEM - FLT 1226 - DURING FLIGHT, THE LEFT ENGINE, SPOOLED DOWN. MADE UNSCHEDULED LANDING AT MEM. REPLACED ENGINE. ENGINE WAS DISASSEMBLED AND FOUND NR 3 BEARING WAS THE INITIAL FAILURE. IT THEN CAUSED OTHER FAILURES. (M)Feb 16, 1998 · N919TW · Doug DC982 · Turbine Engine Compressor SectionSDR TWAA9714101Pressure Reg · failedJFK - FLT 783 - AFTER TAKEOFF ROTATION, RIGHT AIRCONDITIONING TEMPERATURE SUPPLY HIGH INDICATION LIGHT CAME ON. REPLACED THE PILOT PRESSURE REGULATOR. (M)Dec 3, 1997 · N919TW · Doug DC982 · Cabin Pressure Control SystemSDR TWAA9807909Longeron · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION AT STATION 200 TO 218, LONGERON 18L FORWARD AND AFT OF LAV VENT. CLEANED CORROSION PER SRM 51-10-3, PAR 31-42, AND INSTALLED NEW MEMBRANE PER SRM 53-05, FIG 96. (M)Aug 14, 1997 · N919TW · Doug DC982 · Fuselage Main, Longeron/StringerSDR TWAA9807908Frame · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FORMER RING STATION 1380 BELOW LONGERON 4L WITH GOUGE WORN INTO FORMER BY IMPROPERLY INST AIR VALVE. REMOVED DAMAGED AREA AND APPLIED FILLER AND DOUBLER PER SRM 53-01 PAGE 9. (M)Aug 14, 1997 · N919TW · Doug DC982 · Fuselage Main, FrameSDR 95ZZZX4256Filter · dirtyICT - FLT 65 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 1206, DUE TO HIGH OIL PRESSURE AND INCREASING OIL TEMPERATURE. REPLACED ENGINE OIL FILTER AND ENGINE OIL PRESSURE RELIEF VALVE. ENGINE OPERATION AND LEAK CHECK NORMAL. ENGINE TOTAL TIME: 21,726 HOURS; Aug 4, 1995 · N919TW · Doug DC982 · Turbine Engine Oil SystemSDR 95ZZZX547Engine · failedJFK - FLT 481 - DURING CLIMB, SHUT DOWN LEFT ENGINE DUE TO LOUD BANG AND INCREASING EGT. FOUND METAL PARTICLES IN TAILPIPE. REPLACED ENGINE, SN 3218. GROUND RUN-UP AND OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 27,663 HOURS; 14,695 CYCLES. CHECK OP-16 Jan 13, 1995 · N919TW · Doug DC982 · Engine (Turbine/Turboprop)
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