N989Z, cancelled Oct 19, 2005

Service difficulty reports · 100

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 = 'N989Z' AND deregistration_id = 'N989Z-2005-10-19'
  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 ZW0A0105901SlideTHE LEFT SIDE NUMBER 1 CABIN DOOR ESCAPE SLIDE PRESSURE WAS LOW. REPLACED THE SLIDE. CHECK-C 5-10-01 STL. --CLOSED--Jul 26, 2001 · N989Z · Doug DC931 · Escape SlideSDR TWAA0101902Switch · shortedWHEN CREW WAS ACCOMPLISHING THE LANDING GEAR HANDLE CHECK, SMOKE APPEARED FROM THE LANDING GEAR HANDLE SWITCH. FOUND SWITCH SHORTED. REPLACED THE SWITCH. CHECK-C 4-16-00 MCI.Jan 30, 2001 · N989Z · Doug DC931 · Landing Gear Position and WarningSDR TWAA0016802Battery Pack · dischargedTHE EGRESS LIGHTS FOR ROWS 7 TO 14 WERE INOPERATIVE. REPLACED THE BATTERY PACK AT ROW 14. CHECK-C 4-16-00 MCI.Oct 27, 2000 · N989Z · Doug DC931 · Emergency LightingSDR TWAA0005608Rib · crackedDURING OP 16 MAINT CHECK, FOUND LT WING L/E RIB APPROX 7 INCHES I/B OF NUMBER 11 SLAT TRACK WAS CRACKED AT LOWER AFT FASTENER, AND ANOTHER CRACK 19 INCHES /B OF NUMBER 11 SLAT TRACK AT LOWER AFT FASTENER. REPAIRED PER SRM 57-02 FIG 6.Apr 5, 2000 · N989Z · Doug DC931 · Wing, Rib/BulkheadSDR TWAA0005504Structure · crackedDURING OP 16 MAINT CHECK, THE FWD ENTRY DOOR UPPER AFT STOP HOLE WAS CRACKED .5 IN FWD AND .125 IN AFT. FABRICATED DOUBLERS AND INSTALLED PER SRO 9530252.Apr 2, 2000 · N989Z · Doug DC931 · Passenger/Crew DoorsSDR TWAA0005503Rib · damagedDURING OP 16 MAINT CHECK ON THE RT WING A HOLE WAS WORN IN UPPER AND LOWER FLAP RIB AT METAL SHIM BOTTOM SIDE AT FLEX JOINT APPROX 90 INCHES FROM I/B END. REPLACED PER PRINT 9958105.Mar 31, 2000 · N989Z · Doug DC931 · Trailing Edge FlapsSDR TWAA0005607Skin · dentedDURING OP 16 MAINT CHECK ON LT WING FLAP, FOUND DENT IN LOWER SURFACE TO A DEPTH OF APPROX 0.125 IN LOCATED 48 INCHES FROM I/B END, AND A SECOND DENT TO SAME DEPTH LOCATED 20 INCHES FROM I/B END. REMOVED AND MADE AND INSTALLED NEW WEDGE SKIN PER DRAWING 99575Mar 30, 2000 · N989Z · Doug DC931 · Trailing Edge FlapsSDR TWAA0005007Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 30 CRACKED FROM ABOUT STA 582 TO 586. REPAIRED PER SRM 53-02, FIG 14.Mar 24, 2000 · N989Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0005006Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 30 AT STA 584 WAS CRACKED. REPLACED LONGERON TIE PER DOUGLAS INSTALLATION DRAWING 5910068.Mar 24, 2000 · N989Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0005004Skin · damagedDURING OP 16 MAINT CHECK, FOUND TEMPORARY REPAIR ON RT WING I/B SKIN AT STA 154 JUST AFT OF I/B FLAP HINGE ON THE FLAP L/E. INSTALLED REPAIR PER ARA 16901. MATERIAL AL-CLAD 7075-0, HEAT TREATED TO T6.Mar 23, 2000 · N989Z · Doug DC931 · Wing, Plate/SkinSDR TWAA0005003Frame · damagedDURING OP 16 MAINT CHECK, THE AFT RT LAV AREA HAD A TEMPORARY FORMER REPAIR AT STA 908, STRINGER 16R TO 18R. INSTALLED NEW FRAME SECTION AND SPLICED PER SRM 53-03, FIG 32, PAGE 131 AND 132.Mar 22, 2000 · N989Z · Doug DC931 · Fuselage Main, FrameSDR TWAA0004704Longeron · crackedDURING OP 16 MAINT CHECK, LONGERONS 28R, 29R, AND 29L AT STA 584 WERE CRACKED. REPLACED LONGERON TIE FOR EACH, (P/N 5920332-IN), PER DOUGLAS DRAWING 5910068, WITH RIVETS AND HI-LOKS.Mar 21, 2000 · N989Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0004709Keelbeam · crackedDURING OP 16 MAINT CHECK, KEEL BEAM CENTER WEB WAS CRACKED AT STA 618, UPPER END AT CENTER FUEL TANK LOWER SKIN. REPAIRED CRACK WEB PER ARA 16584 PAGES 1 AND 2.Mar 20, 2000 · N989Z · Doug DC931 · Fuselage Main, KeelSDR TWAA0004708Skin · crackedDURING OP 16 MAINT CHECK, FUSELAGE SKIN WAS CRACKED AT TOP FASTENER HOLE OF FRAME, BELOW STRINGER 14R AT STA 980 RT SIDE. INSTALLED AND FINISHED REPAIR PER ARA 16705. SUBSTITUTION OF FASTENERS PER EMLR 7073.Mar 20, 2000 · N989Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0004703Angle · crackedDURING OP 16 MAINT CHECK, THE RT PYLON UPPER ATTACH ANGLE WAS CRACKED, RT SIDE APPROX STA 980. CRACK RUNS FWD .25 INCH. STOP DRILLED CRACK PER SRM 34-04, FIG 10. MANUFACTURED REPAIR ANGLE PER SRM 54-04 FIG 10 SHEET 4. INSTALLED REPAIR ANGLE WET AND WITH APMar 20, 2000 · N989Z · Doug DC931 · Nacelle/Pylon StructureSDR TWAA0004702Frame · crackedDURING OP 16 MAINT CHECK, THE LT KEEL BEAM AREA, A FORMER FOOT WAS CRACKED APPROXIMATELY STA 622, BETWEEN LONGERON 28L AND 29L. REPAIRED CRACK IN FORMER FOOT PER SRM 53-03, FIG 6 PAGE 7.Mar 20, 2000 · N989Z · Doug DC931 · Fuselage Main, FrameSDR TWAA0004215Floorbeam · crackedDURING OP 16 MAINT CHECK HAD CRACK ON FITTING ON O/B FLOOR SUPPORT BEAM AT STA 996, LBL 60 INCHES. INSTALLED NEW FITTING (P/N 5913700-IN) PER 5910163 DRAWING WITH HI-LOKS.Mar 16, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0004218Frame · crackedDURING OP 16 MAINT CHECK, THE AFT FUSELAGE FRAME AT STA 1076 WAS CRACKED AT LOWER AFT CORNER OF THE LT HEAT EXCHANGER PORT. REPAIRED CRACK IN FRAME PER SRM 53-03 FIG 32 SHEET 4. SEALED PER SRM 51-20-0. INSTALLED FASTENERS PER SRM 51-30-5.Mar 14, 2000 · N989Z · Doug DC931 · Fuselage Main, FrameSDR TWAA0004217Skin · chafedDURING OP 16 MAINT CHECK AT STA 937, LT SIDE A WORN AREA IN FUSELAGE AT L/E OF LT PYLON. INSTALLED DOUBLER PER SRM 53-04 FIG 3A.Mar 11, 2000 · N989Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0004216Angle · crackedDURING OP 16 MAINT CHECK AT STA 996 AND BELOW LONGERON 18L, THE BULKHEAD L-ANGLE WAS CRACKED. INSTALLED NEW PIECE OF (P/N 5910763-79) AND SPLICE PER SRM 53-05, FIG 3 SHEET 1. INSTALLED WITH RIVET AND HI-LOKS.Mar 9, 2000 · N989Z · Doug DC931 · Fuselage Main, BulkheadSDR TWAA0003928Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT AT STA 200, JUST OTBD OF NUMBER 4 TRACK, HAD CORROSION. FABRICATED LIKE PART FROM 7075-T65 EXTRUSION PER IPC 53-11-1 PAGE 53. REMOVED CORROSION PER SPM 6-80-1. TREATED AND PAINTED PER SRM 51-10-3.Mar 8, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003927Seat Track · corrodedDURING OP 16 MAINT CHECK, NUMBER 4 SEAT TRACK HAD CORROSION AT STA 232, RBL 44. REPLACED SECTION OF TRACK FROM STA 200 TO 284, NUMBER 4 TRACK PER SRM 53-05 FIG 4F FOR SPLICE, AND IPC 53-40-00 FOR TRACK AND FASTENERS. TREATED PER 51-10-3.Mar 8, 2000 · N989Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0003915Intercostal · damagedDURING OP 16 MAINT CHECK, INTERCOSTAL WAS DEFORMED AT STA 400, RBL 6 TO 12. REPLACED INTERCOSTAL PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING 5910142.Mar 7, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003914Intercostal · damagedDURING OP 16 MAINT CHECK, FOUND DEFORMED INTERCOSTAL AT STA 380, RBL 6 TO 12. REPLACED INTERCOSTAL PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING 5910142.Mar 7, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006109Floorbeam · crackedDURING OP 16 MAINT CHECK, AT CABIN STA 200 RT, STRINGER 18, FLOOR MEMBRANE WAS CRACKED AND HEAVLY CORRODED. REMOVED MEMBRANE AND FABRICATED NEW MEMBRANE PER SRM 53-11-2, FIG 5 SHEET 2, AND DOUGLAS DRAWING 5910840 AND 9910734. INSTALLED WITH AD 5 RIVETS. Mar 6, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003911Seat Track · corrodedDURING OP 16 MAINT CHECK, NUMBER 3 CABIN FLOOR TRACK HAD CORROSION AT STA 216, RBL 22 INCHES. REPLACED NUMBER 3 SEAT TRACK FROM STA 216 TO STA 266 EXISTING SPLICE WITH NEW SECTION OF TRACK TWA PN 16-4883, WITH NEW FASTENERS PER SRM 51-30-2.Mar 6, 2000 · N989Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0003910Floorboard · crackedDURING OP 16 MAINT CHECK, CABIN FLOOR PANEL 11, TOP SIDE HAD CORROSION IN SEVERAL AREAS. FABRICATED NEW FLOOR PANEL USING OLD PANEL AS A TEMPLATE. USED 2024-T3, 0.063 FOR PANEL. USED 0.032, 7075-T6 FOR HAT SECTION. NAS1097AD RIVETS WERE USED PER SSRM 53-00Mar 6, 2000 · N989Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0003912Intercostal · misdrilledDURING OP 16 MAINT CHECK, INTERCOSTAL WAS DEFORMED AND HAD MISDRILLED HOLES AT STA 350 TO 370, RBL 6 INCHES. REPLACED INTERCOSTAL PER 6-70-01, PAGE 3 AND DOUGLAS DRAWING 9957909.Mar 5, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003917Intercostal · damagedDURING OP 16 MAINT CHECK, INTERCOSTAL WAS DEFORMED AT STA 389, RBL 6 TO 12. REPLACED INTERCOSTAL PER SPM 6-70-01, PAGE 3, AND BOEING DRAWING 5910142.Mar 4, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003916Intercostal · damagedDURING OP 16 MAINT CHECK, INTERCOSTAL WAS DEFORMED AT STA 409, RBL 6 TO 12. REPLACED INTERCOSTAL PER SPM 6-70-01, PAGE 3, AND DOUGLAS DRAWING 5910142.Mar 4, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003913Floorbeam · crackedDURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CRACKED AT STA 592, RBL 40 IN TO 48 IN. STOP DRILLED, INSTALLED DOUBLER PER SRM 53-01, PAGE 9.Mar 4, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003730Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND TRACK CORRODED ON INSIDE AT STA 237 TO 304, NUMBER 2 TRACK LBL 22 INCHES. INSTALLED NUMBER 2 TRACK SPLICE AT STA 200 TO 322, LBL 22 IN PER SRM 53-05, FIG 4F. BURNISHED CORROSION FROM SPLICE PER SPM 6-80-01. WITHIN LIMIT PER SMar 4, 2000 · N989Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0003918Seat Track · corrodedDURING OP 16 MAINT CHECK, NUMBER 1 CABIN FLOOR TRACK HAD CORROSION FROM STA 200 TO 237. TREATED METAL PER SRM 51-10-03. REPLACED NR 1 TRACK AND SPLICE FROM STA 200 TO 303 WITH NEW TRACK INSTALLED WITH FASTENERS PER SRM 51-30-2.Mar 3, 2000 · N989Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0003722Floorbeam · corrodedDURING OP 16 MAINT CHECK, FLOOR WEB AT STA 200 TO 218, BL 0 AND LBL 56, HAD CORROSION ON TOP SIDE OF WEB. REPLACED FLOOR MEMBRANE FROM LBL 20 TO BL 0 WITH RIVETS PER SRM 51-30-2. REMOVED CORROSION FROM LBL 20 TO LBL 56 PER SPM 6-80-1 AND SRM 51-1--3 FROM STAMar 3, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003719Intercostal · misdrilledDURING OP 16 MAINT CHECK, INTERCOSTAL WAS DEFORMED AND HAD MISDRILLED HOLES AT STA 370 TO 427, RBL 6. REPLACED INTERCOSTAL PER SPM 6-70-1, PAGE 3 AND DOUGLAS DRAWING 5910142.Mar 3, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006106Structure · crackedDURING OP 16 MAINT CHECK, THE SUPPORT STRUCTURE IN SIDE OF RT WING FLAP OTBD IDLE HINGE WAS CRACKED AT INBD AND OTBD SIDE. INSTALLED INBD AND OTBD RIBS PER DRAWING 5910134, SHEET 2 ZONE 18. ---CLOSED---Mar 1, 2000 · N989Z · Doug DC931 · Wing Miscellaneous StructureSDR TWAA0003727Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND HEAVY SEALANT OVER CORRODED FLOOR WEB AT STA 218, LBL 0 TO 12 INCHES. REPLACED FLOOR MEMBRANE FROM BL 0 TO LBL 20 IN WITH RIVETS PER SRM 51-30-02.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003726Floorbeam · corrodedDURING OP 16 MAINT CHECK, CABIN FLOOR WEB STA 160 TO 200 AND LBL 22 IN TO LBL 43 INCHES HAD LIGHT CORROSION TOP OF WEB. REMOVED MEMBRANE CORRODED AREA FROM STA 160 TO 175, LBL 22 IN TO 45 IN PER SPM 6-80-1 AND SRM 51-10-3. REPLACED MEMBRANE STA 175 TO 200 WIMar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003725Floorbeam · corrodedDURING OP 16 MAINT CHECK, FLOOR SUPPORT WEB AT STA 160 TO 200 HAD LIGHT CORROSION, LB 0 TO LBL 24. REMOVED CORROSION FROM BL 0 TO LBL 24 PER SPM 6-80-1 AND SRM 51-10-3. REPLACED MEMBRANE FROM STA 180 TO 200 WITH RIVETS PER SRM 51-30-2.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003724Floorbeam · corrodedDURING OP 16 MAINT CHECK AT STA 200 AND BL 0 TO LBL 24 INCHES, FOUND HEAVY CORROSION AND SEALANT INSTALLED ON FLOOR WEB. PARTIAL MEMBRANE REMOVED. REPLACED FLOOR MEMBRANE FROM STA 175 TO 200, BL 0 TO LBL 44 WITH RIVETS PER SRM 51-30-2.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003723Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT ANGLE, STA 200 LBL 0 TO 20 INCHES. INSTALLED NEW FLOOR SUPPORT MADE FROM TWA PN S2652479-1200, WITH RIVETS PER SRM 51-30-2.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003721Longeron · crackedDURING OP 16 MAINT CHECK, LONGERON 17L WAS CRACKED AT THE AFT SIDE OF STA 965 BULKHEAD. REPLACED LONGERON 17L FROM STA 955 TO 996 PER DRAWING 5911427. INSTALLED RIVETS PER SRM 51-30-2. PAINT PER SRM 51-10-3.Mar 1, 2000 · N989Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0003720Hinge · crackedDURING OP 16 MAINT CHECK, THE RT WING SUPPORT STRUCTURE INSIDE OF THE FLAP OTBD IDLE HINGE WAS CRACKED INBD AND OTBD SIDE.. INSTALLED INBD AND OTBD RIBS PER DRAWING 5910134, SHEET 2 ZONE 18.Mar 1, 2000 · N989Z · Doug DC931 · Trailing Edge FlapsSDR TWAA0006105Splice · corrodedDURING OP 16 MAINT CHECK CUSP ANGLE SPLICE HAD CORROSION AT STA 210 RT. NEW SPLICE MADE PER CUSP ANGLE CORROSION REPAIR, SRM 53-05, PAGE 141. --CLOSED---Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0006108Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND HEAVY CORROSION AT STA 200, LBL 24 AND LBL 43. INSTALLED NEW FLOOR SUPPORT WITH RIVETS PER SRM 51-30-2. PATTERN FROM OLD PART. ALODINED, PRIMED, AND PAINTED WHITE. ---CLOSED---Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0006107Floorbeam · corrodedDURING OP 16 MAINT CHECK, CABIN FLOOR SUPPORT AT LBL 46 TO LBL 56 HAD HEAVY CORROSION. REPLACED FLOOR SUPPORT AT STA 200 FROM LBL 46 TO 56 WITH RIVETS PER SRM 51-36-02. PATTERN FROM OLD PART. ALODINED, PRIMED, AND PAINTED WHITE. ---CLOSED---Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003729Web · corrodedDURING OP 16 MAINT CHECK, FOUND SEVERE CORROSION AT STA 220, RBL 58, THE RT SIDE CUSP ANGLE. REPAIRED PER SRM CUSP ANGLE CORROSION REPAIR 53-05, PAGE 141 AND DOUGLAS DRAWING 9923667 AND 9910078..Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0003718Floorbeam · canningDURING OP 16 MAINT CHECK, THE CABIN FLOOR WEB AT STA 160 TO 200 WAS OIL CANNING AND STRETCHED EXCESSIVELY, BL 0 AND LBL 42 INCHES. INSTALLED NEW MEMBRANE FROM STA 175 TO 200, BL 0, TO LBL 44 IN, WITH RIVETS PER SRM 51-30-2.Feb 29, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003728Floorbeam · corrodedDURING OP 16 MAINT CHECK, FLOOR WEB HAD CORROSION AT STA 20, LBL 48 INCHES, BELOW FWD END OF CHAIR TRACK. REMOVED CORROSION PER SPM 6-80-1. INSTALLED NEW MEMBRANE AT STA 200 FWD OF NUMBER 1 TRACK WITH PROPER FASTENERS PER SRM 51-30-2.Feb 28, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA0003717Floorbeam · crackedDURING OP 16 MAINT CHECK, THE FLOORBEAM DOUBLER WAS CRACKED AT STA 180, LBL 19 TO BL 0. REPAIRED PER SRM 53-05, PAGE 224, AND DOUGLAS PRINT 99223484.Feb 28, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor Beam
Back to N989Z, cancelled Oct 19, 2005