N902TW, cancelled Feb 4, 2008

Service difficulty reports · 49

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 = 'N902TW' AND deregistration_id = 'N902TW-2008-02-04'
  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 ZW0A0201301Attach Angle · crackedDURING CHECK-C FWD LT DORSAL FIN ATTACH ANGLE, .5 INCH CRACK WAS FOUND ON UPPER LEG VERIFIED WITH EDDY CURRENT. INSTALLED NEW ATTACH ANGLE PER SRM 51-30-02, 51-30-05, & MO 72R22 & ARA 17951.Jan 28, 2002 · N902TW · Doug DC982 · Vertical Stabilizer Miscellaneous StructureSDR ZW0A0107902Battery Pack · dischargedTHE EMERGENCY LIGHT IN THE TAIL CONE AND WALKWAY, AND THE CABIN EMERGENCY LIGHT IN THE CEILING AT THE AFT FLIGHT ATTENDANT SEAT AREA, WERE INOPERATIVE. REPLACED THE BATTERY PACK PN 408822-101 FOR THE TAIL CONE AND WALKWAY, AND REPLACED THE BATTERY POWER SUPPLSep 1, 2001 · N902TW · Doug DC982 · Emergency LightingSDR ZW0A0106901Wire · brokenON ARRIVAL AT THE GATE THE LEADING EDGE SLATS WOULD NOT RETRACT. REPLACED BROKEN FLAP BUS WIRE, RUN 208B. REFERENCE IPC 27-30-00 FIGURE 2B ITEM 32. CHECK-C 2-5-01 STL. --CLOSED--Aug 15, 2001 · N902TW · Doug DC982 · Leading Edge Slat Control SystemSDR ZW0A0102402Power Supply · dischargedTHE EMERGENCY LIGHTS DID NOT COME ON IN HALF OF THE FIRST CLASS SECTION. REPLACED THE POWER SUPPLY. CHECK-C 2-5-01 STL.May 29, 2001 · N902TW · Doug DC982 · Emergency LightingSDR TWAA0018501Battery Pack · inoperativeTHE EMERGENCY LIGHT AT THE TAIL CONE COMPARTMENT AND THE EMERGENCY LIGHTS AT ROWS 7 TO 10 WERE INOPERATIVE. REPLACED THE LAMP, P/N 1315, FOR THE TAIL COMPT, AND REPLACED THE BATTERY PACK, P/N 408822-101, FOR THE CABIN LIGHTS. CHECK-C 4-13-00 MCI.Nov 28, 2000 · N902TW · Doug DC982 · Emergency LightingSDR TWAA0011502Battery · dischargedTHE LT AND RT FWD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 10-25-00 MCI.Jul 22, 2000 · N902TW · Doug DC982 · Emergency LightingSDR TWAA0007502Switch · stuckAFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. CREW FOLLOWED GEAR HANDLE LOCKED PROCEDURE BUT GEAR HANDLE RELEASE BUTTON INEFFECTIVE. CREW LEFT GEAR DOWN AND RETURNED TO SAT. LANDING NORMAL EXCEPT SPOILERS WOULD NOT ARM FOR LANDING. FOUND LANDING GEAR May 13, 2000 · N902TW · Doug DC982 · Landing Gear Retraction/Extension SystemSDR TWAA0005802Skin · crackedDURING C CHECK MAINT FOUND SKIN CRACKED AT FAIRING ATTACH HOLE, LOWER FUSELAGE STA 772, ABOVE LONGERON 29 RT, AND CORROSION AT STA 762 TO 772, LONGERON 28 RT TO 29 RT, GROUND BEYOND LIMITS. REMOVED CORROSION AND DRILLED DAMAGED HOLE TO 3/8 INCHES. NO CRACKApr 3, 2000 · N902TW · Doug DC982 · Fuselage Main, Plate/SkinSDR TWAA0005304Doubler · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON LOWER FWD SIDE OF PRESSURE BULKHEAD DOUBLER, RT OF CENTER LINE. REMOVED AND REMANUFACTURED DOUBLER PER SRM 53-14-3, FIG 7 SHEET 1 AND 4 USING 70756T6 0.080 FASTENERS PER SRM 51-60-0 AND PER DOUGLAS DRAWING 5930760.Mar 30, 2000 · N902TW · Doug DC982 · Fuselage Main, BulkheadSDR TWAA0005303Rib · crackedDURING CHECK-C MAINT, THE RT WING LEADING EDGE RIB WAS CRACKED INSIDE PANEL 1211R BEHIND NUMBER 5 SLAT. REMOVED AND REPLACED RIB PER SPM 6-70-02. INSTALLED FASTENERS PER SRM 51-30-02.Mar 30, 2000 · N902TW · Doug DC982 · Wing, Rib/BulkheadSDR TWAA0004904Floorbeam · corrodedDURING CHECK-C MAINT, THE FLOOR SUPPORT AT STA 160 TO 200, RBL 45 HAD CORROSION. REMOVED AND REPLACED FLOOR SUPPORT PER SPM 6-70-01.Mar 22, 2000 · N902TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0004814Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON CABIN FLOOR SUPPORT BEAM, STA 1250, LBL 24 TO 40. FLOORBEAM WAS CORRODED BEYOND LIMITS. FABRICATED NEW FLOORBEAM, INSTALLED WITH NAS 6703 BOLTS, NAS 1252 WASHERS AND MS2104L3 NUTS.Mar 21, 2000 · N902TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0004707Seat Track · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON SEAT TRACK NUMBER 2, IN TRACK AND SCREW HOLES FOR FLOOR PANEL AT STA 1170 TO 1309. REMOVED CORROSION BY INSTALLING NEW TRACK PER DRAWING 5930565. INSTALLED FASTENERS PER SRM 51-30, 51-10-4, AND 51-60-0. SEALED WITH 8Mar 21, 2000 · N902TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0004706Track · corrodedDURING CHECK-C MAINT, THE MID CARGO BIN BETWEEN STA 769 AND 789 THE RT TRACK WAS CORRODED IN SEVERAL LOCATIONS. INSTALLED NEW TRACK PER SRM 6-70-01, PAGE 1.Mar 21, 2000 · N902TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0004807Window Post · cutDURING CHECK-C MAINT, FOUND WINDOW BELT FRAMES WITH LIGHT CUTS AND SCRATCHES IN FOLLOWING LOCATIONS; LT 22, 46, 45, 44, 42, 43, 24, RT 23, RT AFT EXIT, RT FWD EXIT, LT FWD EXIT, 02-211, 02-358 02-357, 02-221, 02-220, 02-219, 02-218, AND 02-217. ALL WERE REPAIMar 20, 2000 · N902TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0004705Channel · corrodedDURING CHECK-C MAINT, IN THE C3 CARGO COMPT FOUND CORROSION AT STA 1212 TO 1210, BETWEEN LONGERON 30 TO 29R ON U CHANNEL. REMOVED AND REPLACED U CHANNEL PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30-5.Mar 20, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004604Skin · crackedDURING CHECK-C MAINT, THE C3 CARGO DOOR FWD LOWER CORNER OF THE DOOR SKIN, 14 INCHES UP FROM THE BOTTOM EDGE, HAD 4 EACH BENDS. STRENGHTENED ONE AREA. THREE AREAS REPAIRED PER SRM 52-30 PAGE 1 AND SRM 52-01 PAGE 3. ACCOMP HIGH FREQ EDDY CURRENT BUT NO CRACKMar 20, 2000 · N902TW · Doug DC982 · Cargo/Baggage DoorsSDR TWAA0004812Frame · corrodedDURING CHECK-C MAINT, IN THE AFT CARGO COMPT FOUND CORROSION AFT SIDE OF FRAME, STA 1271 STRINGER 29L. REMOVED CORROSION BY FABRICATION OF NEW DOUBLER PER SRM 53-03, FIG 2A. INSTALLED PER SRM 51-30-2.Mar 17, 2000 · N902TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0004811Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT, STA 180, RBL 8 TO 56. REMOVED AND REPLACED CORRODED PART PER SPM 6-70-01.Mar 17, 2000 · N902TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0004810Skin · delaminatedDURING CHECK-C MAINT, THE RT WING T/E UPPER WING T/E PANEL LOWER SURFACE WAS DELAMINATED ABOVE THE O/B FLAP, O/B IDLER HINGE. REMOVED AND REPLACED WITH NEW PART PER SRM 51-01 PAGE 1 PARAGRAPH C. INSTALLED PER SRM 51-10-04, 51-30-02, AND SRM 51-30-01. SEALEDMar 15, 2000 · N902TW · Doug DC982 · Wing, Plate/SkinSDR TWAA0004809Skin · delaminatedDURING CHECK-C MAINT, THE RT WING T/E LOWER SURFACE OF THE WING, UPPER T/E PANEL WAS DELAMINATED AT AILERON QUADRANT. REMOVED AND REPLACED WITH NEW (P/N 172779) PER SRM 51-01, PAGE 1 PARAGRAPH C. INSTALLED PER SRM 51-10, 51-30-02 AND 51-30-01. SEALED PER SRMar 15, 2000 · N902TW · Doug DC982 · Wing, Plate/SkinSDR TWAA0004808Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON LOWER SIDE OF THE FLOOR SUPPORT AROUND FASTENERS, STA 708 TO 712, RBL 8. REMOVED CORROSION, TREATED AND PRIMED METAL AND INSTALLED REPAIR DOUBLER PER SRM 53-01, PAGE 10 FIG 2.Mar 15, 2000 · N902TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0004806Brace · crackedDURING CHECK-C MAINT, THE AFT PRESSURE BULKHEAD, FWD RT SIDE DIAGONAL BRACE WAS CRACKED IN RADIUS UPPER END LONGERON 3R TO 4R, STA 1338. INSTALLED NEW BRACE PER SPM 6-70-01 AND DOUGLAS DRAWING 9915562.Mar 14, 2000 · N902TW · Doug DC982 · Fuselage Main, BulkheadSDR TWAA0004815Support Bracket · corrodedDURING CHECK-C MAINT, THE FWD ENTRY DOOR SILL MOUNT SUPPORT WAS CORRODED, STA 160 TO 200, LBL 55. REMOVED CORRODED SUPPORT, FABRICATED NEW SUPPORT AND INSTALLED.Mar 11, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004214Bolt · corrodedDURING CHECK-C MAINT, FOUND RUSTED HUCK BOLT ON TOP OF WINDOW FRAME BETWEEN STA 636 AND 655. CLEANED RUST FROM FASTENER AND TREATED PER SPM 6-80-01, PAGE 1.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004213Bolt · corrodedDURING CHECK-C MAINT, FOUND RUSTED HUCK BOLTS AT STA 826, LONGERON 17L. REMOVED RUST FROM HUCK BOLT PER SPM 6-80-01.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004212Bolt · corrodedDURING CHECK-C MAINT, FOUND THREE RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 294 AND 313. REPLACED FASTENERS PER MM 56-20-00.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004211Bolt · corrodedDURING CHECK-C MAINT, FOUND RUSTED BOLT ON WINDOW FRAME BETWEEN STA 788 AND 807. REPLACED RUSTED BOLT PER SRM 51-30-0.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004206Fastener · corrodedDURING CHECK-C MAINT, FOUND RUSTED FASTENER AT STA 712, LONGERON 15L. CLEANED RUST FROM FASTENER AND REPLACED NUT AND WASHER.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004205Nut · corrodedDURING CHECK-C MAINT, FOUND RUSTED NUT ON LONGERON 10L AT STA 332. CHANGED NUT AND WASHER PER SPM 6-30-07.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004204Fastener · corrodedDURING CHECK-C MAINT, FOUND RUSTED FASTENER AT STA 712, LONGERON 15L. CLEANED RUST FROM FASTENER AND REPLACED NUT AND WASHER PER SPM 6-30-07.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004203Bolt · corrodedDURING CHECK-C MAINT, FOUND THREE RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 693 AND 712. REMOVED 3 RUSTED BOLTS AND INSTALLED 3 NEW BOLTS AND WASHERS PER SPM 6-30-07.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004202Bolt · corrodedDURING CHECK-C MAINT, FOUND THREE RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 769 AND 788. REPLACED RUSTED BOLTS PER SRM 51-30-0.Mar 5, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004210Bolt · corrodedDURING CHECK-C MAINT, FOUND THREE RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 541 AND 560. REMOVED 3 BOLTS AND INSTALLED 3 NEW BOLTS AND WASHERS PER SPM 6-30-07.Mar 4, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004209Bolt · corrodedDURING CHECK-C MAINT, FOUND FOUR RUSTED BOLTS ON WINDOW FRAME BETWEEN STA 579 AND 598. REMOVED 4 RUSTED BOLTS AND INSTALLED 4 NEW BOLT AND WASHERS PER SPM 6-30-07.Mar 4, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004208Bolt · corrodedDURING CHECK-C MAINT FOUND RUSTED BOLT ON WINDOW FRAME BETWEEN STA 503 AND 522. REMOVED 1 RUSTED BOLT AND INSTALLED 1 NEW BOLT AND WASHER PER SPM 6-30-07.Mar 4, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0004207Bolt · corrodedDURING CHECK-C MAINT, FOUND RUSTED BOLT ON WINDOW FRAME BETWEEN STA 446 AND 465. REMOVED 2 RUSTED BOLTS AND INSTALLED 2 NEW BOLTS AND WASHERS PER SPM 6-30-07.Mar 4, 2000 · N902TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0003930Stringer · corrodedDURING CHECK-C MAINT, FOUND IN THE CABIN, STRINGER 15R ANGLE WAS CORRODED ON AFT SIDE AT STA 1005. FABRICATED NEW PART PER SPM 6-70-01, PAGE 2 AND 3, PARAGRAPH 4. REINSTALLED PART MADE FROM TWA PN 56-2254 WITH HI-LOCK FASTENERS PER SRM 51-30-02.Mar 3, 2000 · N902TW · Doug DC982 · Fuselage Main, Longeron/StringerSDR TWAA9908002Switch · out of positionTHE EGRESS LIGHTING CAME ON WITH EMERGENCY LIGHT SWITCH IN THE OFF POSITION. CHECKS WERE MADE TO VERIFY THE PERFORMANCE OF THE SYSTEM. UNABLE TO DUPLICATE THE REPORTED PROBLEM. CHECK-C 2-9-99 STL.Jun 4, 1999 · N902TW · Doug DC982 · Emergency LightingSDR TWAA9811801Light · inoperativeTHE AFT EGRESS LIGHT STRIP, AFT OF LAST PAX SEAT, WAS INOP AND COVER BROKEN. REPAIRED LIGHT STRIP AND REPLACED LIGHT COVER, CHECK-C 2-1-98 STL. (M)Jul 21, 1998 · N902TW · Doug DC982 · Emergency LightingSDR TWAA9811502Skin · bentDURING OVERNIGHT MAINTENANCE, FOUND THE L-1 CABIN DOOR LOWER FORWARD CORNER OF DOOR SKIN BENT INWARD 9 INCHES. AREA CUT OUT, FILLER AND DOUBLER INSTALLED PER SRM 52-05, FIG 32. CHECK-C 2-1-98 STL. ACFT TT: 48,075 HOURS. ACFT TC: 24,896. (X)Jul 14, 1998 · N902TW · Doug DC982 · Passenger/Crew DoorsSDR TWAA9810101Oil Pump · leakingIN FULL COLD POSN LT AIR COND PACK REPORTED TO CAUSE OILY BURNING SMELL AND MADE CABIN APPEAR FOGGY. CREW WENT TO MANUAL AND SMELL AND FOG WENT AWAY. THE LT AND RT WATER SEPARATORS WERE REPLACED AND CHECKED OK. LATER FLT REPORTED SLIGHT FUMES FROM LT PACK, Jun 22, 1998 · N902TW · Doug DC982 · APU Oil SystemSDR TWAA9804303Compressor · stalledRNO - FLT 224 - ABORTED TAKEOFF AT 100 KTS DUE TO COMPRESSOR STALLS ON RT ENGINE. FOUND COMPRESSOR BLADES DAMAGED FROM APPARENT ICE INGESTION. (M)Mar 24, 1998 · N902TW · Doug DC982 · Turbine Engine Compressor SectionSDR TWAA9802202Battery Pack · dischargedSTL - FLT 30 - THE EGRESS LIGHTING CAME ON IN-FLIGHT BETWEEN ROWS 15 AND 21. REPLACED BATTERY PACK. CHECK-C ON 1-25-98 STL. (X)Feb 11, 1998 · N902TW · Doug DC982 · Emergency LightingSDR TWAA9802001Longeron · damagedSTL - DURING OP-9 MAINTENANCE CHECK, THE LOWER LONGERON LEG WAS FOUND DAMAGED AT L23 STATION 1366 AT APU AREA. REPAIRED L23 PER ARA 12000. (M)Feb 2, 1998 · N902TW · Doug DC982 · Fuselage Main, Longeron/StringerSDR TWAA9712701Slide · deployedSTL - WHILE PARKED AT THE GATE THE TAILCONE EMERGENCY ESCAPE SLIDE WAS INADVERTENTLY DEPLOYED BY SECURITY PERSONNEL. THE SLIDE FUNCTIONED PROPERLY. REMOVED AND REPLACED SLIDE, MFG P/N 100506-201, MANUFACTURED BY BF GOODRICH COMPANY. (M)Oct 23, 1997 · N902TW · Doug DC982 · Escape SlideSDR TWAA9613301Connector · corrodedSTL - ABORTED TAKEOFF AT 50 KNOTS DUE TO A WHEEL NOT TURNING LIGHT ILLUMINATION. CLEANED CORROSION FROM THE ANTI-SKID VALVE CONNECTOR. OPERATIONAL CHECK NORMAL. (M)Oct 31, 1996 · N902TW · Doug DC982 · Brake Anti-Skid SectionSDR 96ZZZM1074Compressor · stalledSLC - DURING CLIMB, SHUT DOWN NR 2 ENGINE DUE TO COMPRESSOR STALLS. FOUND METAL PARTICLES IN ENGINE BLEED AIR DUCT AND CAPS. CHANGED ENGINE. ENGINE OPERATION THEN CHECKED NORMAL. (M)Jun 9, 1996 · N902TW · Doug DC982 · Turbine Engine Compressor SectionSDR 96ZZZX1202Jamb · corrodedMCI - DURING OP-15, FOUND CORROSION ON AFT CARGO DOOR JAMB LOWER BEAM. REPLACED BEAM PER SRM 51-01, PAGE 1, ITEM C. AIRCRAFT TT: 39,822 HRS; 20,932 CYCLES.Feb 20, 1996 · N902TW · Doug DC982 · Fuselage Miscellaneous Structure
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