N901TW, cancelled May 10, 2007

Service difficulty reports · 66

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 = 'N901TW' AND deregistration_id = 'N901TW-2007-05-10'
  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 ZW0A0303101Battery Pack · dischargedTHE OVERHEAD EMERGENCY LIGHT AT SEATS 8 THRU 12 WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 6-28-2002 STL.Mar 10, 2003 · N901TW · Doug DC982 · Emergency LightingSDR ZW0A0302602Battery · dischargedAFTER ARRIVAL DURING P-S FOUND CABIN EXIT SIGN NOT COMING ON. EMERGENCY EXIT SIGNS BATTERY REPLACED TWS 82-4388 CPN 753-4697. OPS CHECK BY TURNING SYSTEM ON AND OFF. CHECK-C STL 6-28-02.Feb 20, 2003 · N901TW · Doug DC982 · Emergency LightingSDR ZW0A0212604Power Supply · dischargedTHE CEILING EMERGENCY LIGHTS AT ROW 8 THROUGH 16 AND ROW 21 THROUGH 31, AND THE EGRESS LIGHTS IN THE FIRST CLASS CABIN, WERE INOPERATIVE. REPLACED THE POWER SUPPLY AT EACH OF THE LOCATIONS.Dec 19, 2002 · N901TW · Doug DC982 · Emergency LightingSDR ZW0A0209503BatteryTHE EMERGENCY AISLE OVERHEAD LIGHTS WERE INOPERATIVE FROM ROW 8 THRU 12. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 6-16-01 STL. --CLOSED--Sep 9, 2002 · N901TW · Doug DC982 · Emergency LightingSDR ZW0A0107903CableTHE EGRESS LIGHTS BACK TO ROW 14 WERE INOPERATIVE. REPLACED THE FLEX CABLE. CHECK-C 6-16-01 STL. --CLOSED--Sep 3, 2001 · N901TW · Doug DC982 · Emergency LightingSDR TWAA0014302Panel · delaminatedDURING CHECK-C MAINT ON RT WING THE REAR SPAR PANEL FWD OF RT GEAR STRUT WELL HAD DELAMINATION AND RIVET HEADS PULLED THRU SKIN AT L/E OF PANEL. REMOVED DELAMINATED PANEL. INSTALLED NEW TWA (P/N 217-2782) PER SPM 6-70-01 PAGE 3B (1) (2) AND DRAWING 9936835. Aug 30, 2000 · N901TW · Doug DC982 · Wing, Plate/SkinSDR TWAA0013317Attach Angle · crackedDURING CHECK-C MAINT, THE DORSAL FIN ATTACH ANGLE WAS CRACKED ON LT SIDE OF ACFT, O/B OF VERT STAB REAR SPAR. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6. CRACKS FOUND WERE STOP DRILLED. ONE INCH CRACK REPAIRED PER SRM 53-05 FIG B.Aug 22, 2000 · N901TW · Doug DC982 · Fuselage, Stabilizer Attach FittingsSDR TWAA0013316Fitting · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE LT SIDE STA 200 AFT EDGE OF DOOR FITTING. REMOVED CORROSION PER SPM 6-80-01. TREATED PER SRM 51-10-03 AND SPM 6-70-01. REINSTALLED ANGLE.Aug 22, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013315Web · crackedDURING CHECK-C MAINT, THE CABIN FLOOR MEMBRANE WAS CRACKED APPROX 2 INCHES FWD SIDE OF 218 FLOORBEAM, RBL 43. REPAIRED PER SRM 51-70-4.Aug 18, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013314Web · corrodedDURING CHECK-C MAINT, THE FLOOR WEB AND TRANSITION STRIP WERE CORRODED FROM STA 148 TO 200, RBL 54. REPLACED WEB AND TRANSITION STRIP PER SPM 6-70-01. PAINTED PER SRM 51-10-03.Aug 18, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013313Floorbeam · corrodedDURING CHECK-C MAINT, FOUND FLOORBEAM CORRODED AT C1 GALLEY, STA 200 FROM RBL 44 TO RBL 56. REMOVED OLD FLOORBEAM AND MADE NEW FROM DAC PRINT 5930536 AND 5930540 FROM EXTRUSION AND FASTENED PER SRM 51-30-02 PAGE 3.Aug 18, 2000 · N901TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0013312Angle · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON CUSP ANGLE AT STA 229 TO 237, LT SIDE BEHIND TIE PLATE. REMOVED CORROSION PER SRM 51-10-3 PAGE 21. TREATED PER SRM 51-10-3 PAGE 16. INSTALLED NEW TIE PLATE WITH SEALER AND FASTENERS PER DRAWING 992366.Aug 17, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013311Floorbeam · corrodedDURING CHECK-C MAINT, THE STA 200 FLOORBEAM WEB WAS CORRODED AT LBL 64. REPAIRED WEB PER SRM 53-01, PAGE 18. INSTALLED NEW SUPPORT CASTING PER DRAWINGS 9911518 AND 9911595.Aug 17, 2000 · N901TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0013310Fitting · corrodedDURING CHECK-C MAINT, THE LONGERON END TIE WAS CORRODED BEYOND LIMITS AT STA 1338, LONGERON 28R. REPLACED STRINGER TIE WITH NEW PER SRM 51-30-5. TREATED SURFACE PER SRM 51-10-3.Aug 14, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013309Seat Track · corrodedDURING CHECK-C MAINT, THE NUMBER 3 CHAIR TRACK SUPPORT TO UPPER WING SKIN WAS CRACKED APPROX 8 INCHES BELOW TRACK AT STA 845. REMOVED CRACKED FLOOR SUPPORT ANGLE FROM NUMBER 3 CHAIR TRACK AT STA 845. INSTALLED NEW PER DOUGLAS INSTALLATION DRAWING 9936634.Aug 14, 2000 · N901TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0013308Stringer · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON STRINGER 26L, STA 1287 TO 1290. REMOVED VISABLE CORROSION PER SPM 6-80-01 AND TREATED PER SRM 51-10-03, AND ARA 17044A.Aug 14, 2000 · N901TW · Doug DC982 · Fuselage Main, Longeron/StringerSDR TWAA0013307Attach Angle · crackedDURING CHECK-C MAINT, FOUND CHAIR TRACK ATTACH ANGLE CRACKED AT STA 927, RBL 22 AT WING SKIN. REMOVED CRACKED FLOOR SUPPORT ANGLE AT STA 927, RBL 22, NUMBER 3 CHAIR TRACK, AND INSTALLED NEW PER DOUGLAS INSTALLATION DRAWING 3925819.Aug 14, 2000 · N901TW · Doug DC982 · Fuselage Main, Attach FittingsSDR TWAA0013225Frame · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FORMER AT STA 1322, BETWEEN STRINGER 27L AND 23L. REMOVED FORMER BY CUTTING AND SPLICING PER SRM 53-03 FIG 2A PAGE 4A. TREATED SURFACES PER SRM 51-10-3.Aug 14, 2000 · N901TW · Doug DC982 · Fuselage Main, FrameSDR TWAA0013224Stringer · corrodedDURING CHECK C MAINT, THE AFT CARGO COMPT HAD CORROSION ON STRINGER 26R, STA 1287 TO 1324. MADE AND INSTALLED REPAIRS PER ARA 17126A. TREATED MATERIAL PER SRM 51-10-3.Aug 11, 2000 · N901TW · Doug DC982 · Fuselage Main, Longeron/StringerSDR TWAA0013223Beam · corrodedDURING CHECK-C MAINT IN AFT CARGO BIN THE DOOR LOWER THRESHOLD BEAM WAS CORRODED AND HAD 3 FIELD REPAIRS INSTALLED. REMOVED CORRODED BEAM AND INSTALLED NEW BEAM (P/N 593638-501) PER SPM 6-70-01 PAGE 3 ITEM B1, 2, AND SRM 51-60-0 PAGE 9, SRM 51-60-0 PAGE 936, Aug 9, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013222Floorbeam · crackedDURING CHECK-C MAINT, AFT CARGO COMPT AT STA 1155 THE FLOORBOARD SUPPORT WAS CRACKED AT LBL 20 TO RBL 5 IN. REPLACED FLOOR SUPPORT PER SPM 6-70-01 PAGE 3, DRAWING 5936597, SRM 51-60 AND SRM 51-20.Aug 9, 2000 · N901TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0013221Skin · dentedDURING CHECK-C MAINT FOUND FUSELAGE DENT AT STA 218L, BETWEEN LONGERON 18L AND 19L, 3 .625 INCH LONG, 2 .375 INCH WIDE AND 0.150 DEEP. ACCOMP EDDY CURRENT INSP PER NDT 51-00-03 AND NO CRACK FOUND. CUT OUT DAMAGED AREA. INSTALLED A FLUSH DOUBLER 16 BY 17 INCAug 4, 2000 · N901TW · Doug DC982 · Fuselage Main, Plate/SkinSDR TWAA0013220Structure · bentDURING CHECK-C MAINT, THE FWD CARGO DOOR LOWER FWD CORNER WAS BENT. REPAIRED CORNER PER SRM 52-05 FIG 20A AND SRM 51-01 PAGE 2B1, 2, 3. TREATED PER SRM 51-10-3. INSTALLED PER SRM 51-30-02 AND SEALED PER SRM 51-20-0.Aug 4, 2000 · N901TW · Doug DC982 · Cargo/Baggage DoorsSDR TWAA0013219Floor Support · corrodedDURING CHECK-C MAINT IN THE FWD CABIN, THE FLOOR SUPPORT WAS CORRODED AT LBL 10, STA 150 TO 200. REMOVED CORROSION PER SRM 51-10-3 PAGE 21 ITEM 35. ALODINED PER SRM 51-10-3 PAGE 18 ITEM 30. APPLIED PRIMER PER SRM 51-10-3 PAGE 16 ITEM 23 AND REINSTALLED FLOOAug 3, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013218Door Frame · corrodedDURING CHECK-C MAINT FOUND CORROSION ON DOOR FRAME AFT CORNER OF RT SERVICE DOOR FRAME, UNDER SILL, STA 200. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PRIMED PER SRM 51-10-03B. INSTALLED SPLICE PER DRAWING JO60288 SHEET 1.Aug 3, 2000 · N901TW · Doug DC982 · Fuselage Main, StructureSDR TWAA0013217Door Frame · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN DOOR FRAME SKIN FWD LOWER SIDE OF RT SERVICE DOOR AND UNDER SILL AREA, STA 160. REMOVED CORROSION PER SPM 6-80-01. TREATED AND PRIMED PER SPM 51-10-3. INSTALLED SPLICE PER DRAWING JO60288 SHEET 1.Aug 3, 2000 · N901TW · Doug DC982 · Fuselage Main, StructureSDR TWAA0013216Skin · damagedDURING CHECK-C MAINT FOUND BLIND FASTENER INSTALLED AT STA 218, LONGERON 6R. REMOVED BLIND FASTENER. FOUND SKIN DAMAGE. REMOVED DAMAGED AREA OF SKIN WITH .625 INCH SPOTFACE. INSTALLED TITANIUM DOUBLER PER SRM 53-04 FIG 38.Aug 3, 2000 · N901TW · Doug DC982 · Fuselage Main, Plate/SkinSDR TWAA0013215Longeron · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPT, FOUND INNER GRANNULAR CORROSION ON AFT END OF LONGERON 28L, STA 1336. REMOVED LONGERON BY CUTTING AND SPLICING PER SRM 53-02, FIG 18 PAGE 50. TREATED SURFACES PER SRM 51-10-3.Aug 2, 2000 · N901TW · Doug DC982 · Fuselage Main, Longeron/StringerSDR TWAA0013214Structure · crackedDURING CHECK-C MAINT, FOUND IN AFT CARGO COMPT THE FWD SERVICE DOOR LOWER HINGE BOX WAS CRACKED AND CORRODED INSIDE LOWER FWD LIGHTENING HOLE. REPLACED LOWER HINGE BOX RIB. INSTALLED HI-LOKS AND RIVETS PER SRM 51-30-05.Aug 1, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013213Intercostal · corrodedDURING CHECK-C MAINT, FOUND IN AFT CARGO COMP, INTERCOSTALS AT LONGERON 21L AND 22L, BETWEEN STA 1322 AND 1338, WERE CORRODED. FABRICATED INTERCOSTALS AND CLIPS PER PRINT 5911423. PRIMED AND PAINTED PER 51-10-3. INSTALLED INTERCOSTALS AND CLIPS PER PRINT 59Jul 31, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013212Angle · crackedDURING CHECK-C MAINT, FOUND CRACK IN ANGLE FOR LOUVERS AT STA 1463, RT SIDE. FABRICATED NEW ANGLE FROM 7075-T6, 0.080 PER DOUGLAS DRAWING 9923630. TREATED PER SRM 51-10-3 AND INSTALLED ON ACFT PER SRM 51-30-05.Jul 31, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013211Angle · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON CUSP ANGLE AT RT SERVICE DOOR, STA 160 TO 200. REMOVED CORROSION PER SPM 6-80-01. REPLACED CORRODED SECTION OF CUSP PER SPM 6-70-01. INSTALLED CUSP SPLICE PER DRAWING JO60288 SHEET 1.Jul 31, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013210Door Frame · corrodedDURING CHECK-C MAINT, THE AFT CARGO DOOR FRAME AT STA 1155 AND STA 1211, LOWER CORNER CASTINGS WERE CORRODED. REMOVED CORROSION PER SPM 6-80-01 PAGE 1 ITEM 3. GROUND BEYOND LIMITS. REPLACED CORNER CASTINGS PER SPM 6-70-01 PAGE 3, DRAWING 5936469, SRM 51-60 Jul 31, 2000 · N901TW · Doug DC982 · Fuselage Main, StructureSDR TWAA0013209Door · crackedDURING CHECK-C MAINT IN THE LT WHEEL WELL, THE WHEEL WELL DOOR FWD O/B CORNER WAS CRACKED. STOP DRILLED CRACK WITH 0.250 DRILL BIT. MANUFACTURED DOUBLER FROM 7075-0, 0.063 MATERIAL. HEAT TREATED TO 7075-T6 CONDITION. FABRICATED DOUBLER PER ARA 17041. ATTAJul 31, 2000 · N901TW · Doug DC982 · Landing Gear DoorsSDR TWAA0013208Seat Track · corrodedDURING CHECK-C MAINT, IN THE COCKPIT THE AFT EXTENSION OF THE F/O SEAT O/B TRACK WAS CORRODED. REPLACED F/O SEAT TRACK AFT O/B PER DRAWING 9957871-535 AND LOCATED MOUNT HOLES. INSTALLED ON NON-ROUTINE.Jul 31, 2000 · N901TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0013206Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE AT STA 200, LBL 55, TOP OF FLOORBEAM. REMOVED CORROSION BY CUTTING OLD MEMBRANE OUT AND INSTALLED DOUBLER PER SRM 53-07 FIG 2.Jul 30, 2000 · N901TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0013205Seat Track · corrodedDURING CHECK-C MAINT, THE AFT EXTENSION OF THE F/O SEAT TRACK, O/B WAS CORRODED. REPLACED F/O SEAT TRACK AFT O/B PER DRAWING 9957871-503 AND LOCATED MOUNTING HOLES.Jul 30, 2000 · N901TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0013204Cargo Track · corrodedDURING CHECK-C MAINT IN AFT CARGO COMPT THE LT TIE DOWN TRACK WAS CORRODED AT STA 1155 TO 1320. MANUFACTURED AND DRILLED HOLES FOR NEW TIE DOWN TRACK SECTIONS MADE FROM P/N 1D0026B21700 AND S2922357-14400.Jul 30, 2000 · N901TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0013203Fitting · corrodedDURING CHECK-C MAINT, THE SILL AREA IN AFT CABIN HAD CORROSION ON MEMBRANE WIDTH OF DOOR, INTERGRANNULAR BELOW AFT GIRT BAR MOUNT FITTING, STA 1136L TO 1193L, LBL 50 TO LBL 54. REMOVED LIGHT TO MODERATE CORROSION. TREATED, PRIMED AND PAINTED PER SRM 51-10-03Jul 29, 2000 · N901TW · Doug DC982 · Fuselage Main, Attach FittingsSDR TWAA0013202Seat Track · corrodedDURING CHECK-C MAINT, CHAIR TRACK LBL 44 HAD CORROSION AT STA 1260 TO 1309. INSTALLED TRACK PER SRM 51-30-1 AND SRM 51-30-2. REPLACED TRACK PER SPM 6-70-01.Jul 29, 2000 · N901TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0013127Seat Track · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON RIGHT O/B CHAIR TRACK AT STA 1120, 1136, 1153, 1158, 1180, 1212, AND 1242, BL-X54. REPLACED CHAIR TRACK FROM STA 1031 TO 1303 AND SPLICED PER SRM 53-05, FIG 4F.Jul 28, 2000 · N901TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0013126Flange · crackedDURING CHECK-C MAINT, THE MID CARGO DOOR FWD PAN FLANGE WAS CRACKED AT CAM LATCH AREA. REPAIRED PER SRM 52-05, PAGE 16A.Jul 28, 2000 · N901TW · Doug DC982 · Cargo/Baggage DoorsSDR TWAA0013125Hinge · crackedDURING CHECK-C MAINT, ON RT MLG DOOR, THE RT MAIN GEAR DOOR HINGE WAS CRACKED AT FWD END. REMOVED AND REPLACED CRACKED SECTION OF DOOR HINGE PER SPM 6-70-1 AND SRM 51-30-1. INSTALLED HI-LOKS PER SRM 51-60-0 PAGE 36, AND SRM 51-30-5.Jul 28, 2000 · N901TW · Doug DC982 · Landing Gear DoorsSDR TWAA0013124Floor Support · corrodedDURING CHECK-C MAINT IN MID CARGO COMPT HAD LITE CORROSION ON FLOOR SUPPORT ANGLE APPROX STA 694 TO 704, RBL 13 AT CLIP NUT LOCATION. REMOVED VISABLE LITE CORROSION PER SRM 51-10-3 AND SPM 6-80-1. FABRICATED NEW FLOOR SUPPORT ANGLE FROM 0.90 CLAD 7075-T6 PEJul 28, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0013123Floorbeam · corrodedDURING CHECK-C MAINT FLOORBEAM UPPER FLANGE AT STA 1338 HAD CORROSION, RBL 22 TO O/B END. INSTALLED NEW UPPER FLANGE. TREATED AND PAINTED SAME. INSTALLED ALL FASTENERS AND ATTACHING PART PER SRM 51-30-0 AND DAC DRAWING 9915561.Jul 27, 2000 · N901TW · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0013122Skin · crackedDURING CHECK-C MAINT, THE MID CARGO DOOR SKIN AFT EDGE WAS CRACKED. CRACK WAS BLENDED OUT TO 9/36 INCH DEEP BY 1.25 INCH WIDE. EDGE DISTANCE TO FASTENER WAS 0.5. REPAIRED PER SRM 52-05 FIG H PAGE 5. ENGR TASK 004 (H005180A).Jul 26, 2000 · N901TW · Doug DC982 · Cargo/Baggage DoorsSDR TWAA0013121Skin · crackedDURING CHECK-C MAINT, ON LEFT WING FOUND CRACK AND DEEP DENT IN COVER BETWEEN I/B AND CENTER VANE ON O/B FLAP. REPAIRED CRACK AND DENT PER SRM 57-01, FIG 5 AND DOUGLAS DRAWING 5930496. ACCOMP NDT CHECK FOR CRACK CONTAINMENT.Jul 25, 2000 · N901TW · Doug DC982 · Trailing Edge FlapsSDR TWAA0013120Stiffener · wornDURING CHECK-C MAINT, FOUND ON LEFT WING THE O/B FLT SPOILER O/B END WAS WORN. INSTALLED NEW STIFFENER PER DAC DRAWING 5910055.Jul 25, 2000 · N901TW · Doug DC982 · SpoilersSDR TWAA0013119Seat Track · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON LEFT O/B CHAIR TRACK AT STA 1000 TO 1060, STA 1079 TO 1136, AND STA 1000. REPLACED SEAT TRACK FROM STA 1000 TO 1136. REPLACED AT SPLICE WITH NEW SEAT TRACK PER SRM 53-05, FIG 4F.Jul 25, 2000 · N901TW · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0013118Pan · corrodedDURING CHECK-C MAINT, THE FLOOR PAN WAS CORRODED AT STA 1022 TO 1041, RL18. REMOVED CORROSION BY CUSP MEMBRANE CUTOUT PER SRM 53-05, VIEW U OF FIG 4F.Jul 25, 2000 · N901TW · Doug DC982 · Fuselage Miscellaneous Structure
Back to N901TW, cancelled May 10, 2007