N981Z, cancelled Sep 19, 2016

Service difficulty reports · 41

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 = 'N981Z' AND deregistration_id = 'N981Z-2016-09-19'
  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 ZW0A0109001Skin · crackedTHE FUSELAGE SKIN WAS CRACKED AT STA 168 AND LONGERON 29R, 1.625 INCHES AFT OF AREA CUT OUT FOR CORROSION, VERIFIED BY EDDY CURRENT. ACCOMPLISHED SKIN REPAIR AT STA 168 AND LONGERON 29R PER SRM 53-04 AND ARA 17918.Sep 19, 2001 · N981Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9915502Power Supply · inopTWO FORWARD CABIN OVERHEAD EMERGENCY LIGHTS REMAINED ON AFTER ALL ELECTRICAL POWER WAS OFF. REPLACED THE POWER SUPPLY, (P/N 60030451LB) AND BATTERY (P/N 408822101). CHECK-C 8-29-99 MCI.Nov 14, 1999 · N981Z · Doug DC931 · Emergency LightingSDR TWAA9910303Longeron · crackedDURING OP 16 MAINT CHECK, FOUND STA 965 LONGERON 17L WAS CRACKED AT LONGERON TO FORMER. CRACK APPROX .75 INCH LONG. REPLACED LONGERON FROM STA 955 TO 990 PER SRM 53-02, FIG 18.Jul 14, 1999 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9910302Skin · crackedDURING OP 16 MAINT CHECK, FOUND RT WING UPPER WING SKIN CRACKED AT FUEL TANK ACCESS PLATE 1410A. HIGH FREQ EDDY CURRENT ACCOMP PER 51-00-03, PART 6. CRACK WAS CONTAINED AT PLATE ACCESS HOLE. REPAIRED PER SRM 57-03 FIG 23.Jul 14, 1999 · N981Z · Doug DC931 · Wing, Plate/SkinSDR TWAA9910301Intercostal · corrodedDURING OP 16 MAINT CHECK, FOUND INTERCOSTAL AT LONGERON 28R WITH INTERGRANULAR CORROSION BETWEEN STRINGER 937 AND 950. PART MADE PER DRAWING 9957723. REPLACED INTERCOSTAL, INSTALLED WITH HI-LOKS, BECAUSE THEY WERE ORIGINAL FASTENER.Jul 13, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9908905Angle · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT CENTER FRAME ANGLE 9911505-7 WAS CRACKED APPROXIMATELY 1.5 INCH IN RADIUS AT I/B END STA 83.55, X=10.00, Z=42, ON LT SIDE. INSTALLED NEW FRAME PER ITEM 30 OF EMLR 69590.Jun 23, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9908909Frame · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT FRAME 5 ON LT SIDE WAS CRACKED IN RADIUS AT X=+10 CONFIRMED WITH EDDY CURRENT. CRACK WAS APPROXIMATELY .75 INCH LONG AT STA 83.55. REPAIRED PER SRM 53-03 FIG 34, SHEETS 1 TO 7.Jun 22, 1999 · N981Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9908908Frame · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT FRAME CRACKED AT STA 83.55, X=-11 INCHES, APPROXIMATELY 1.5 INCHES LONG ON RT SIDE. REPAIRED PER SRM 53-03, FIG 34 SHEET 1 TO 7.Jun 22, 1999 · N981Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9908601Longeron · crackedDURING OP 16 MAINT CHECK, FOUND CRACK AT LONGERON TO FRAME FASTENERS AT STA 200, LONGERON 2L. SPLICED IN NEW LONGERON PER SRM 53-02, PAGES 48 TO 53, FROM STA 190 TO 228.Jun 22, 1999 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9908910Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND STA 200 FLOORBEAM CAP CORRODED JUST OUTBOARD OF NUMBER 4 CHAIR TRACK. REPAIRED FLOORBEAM PER SRM 53-05, PAGE 31.Jun 18, 1999 · N981Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA9908907Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT NUMBER 2 SEAT TRACK TO CENTERLINE, STA 200. REPLACED FLOOR SUPPORT PER SPM 6-70-01, PAGE 3.Jun 17, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9908906Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 200, BETWEEN NUMBER 1 AND 2 SEAT TRACKS. REPLACED FLOOR SUPPORT PER STD PROCESSES MANUAL 6-70-01, PAGE 3.Jun 17, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9908202Bulkhead Web · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION WITH POPPED RIVETS AND PILLOWING AT AFT PRESSURE BULKHEAD, STA 996 BETWEEN LONGERON 26L AND 28L. REMOVED CORROSION PER SPM 6-80-01 AND INSTALLED DOUBLER PER SRM 53-03, FIG 24.Jun 2, 1999 · N981Z · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9907904Skin · corrodedDURING OP 16 MAINT CHECK, FOUND SKIN CORROSION BEYOND LIMITS AT STA 756 TO 803, RBL 26L TO 26R. REPLACED SKIN PER DOUGLAS DRAWING 5911421 AND 5916154, AND SPM 6-70-01.May 28, 1999 · N981Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9907903Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 200. NUMBER 1 FLOOR TRACK TO MEMBRANE AREA, LBL 50. CORROSION WAS REMOVED PER SRM 6-80-01, PAGE 1 AND REPLACED FLOOR SUPPORT PER SPM 6-70-01.May 25, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9907902Floor · damagedDURING OP 16 MAINT CHECK, FOUND REPAIR ON FLOOR MEMBRANE BETWEEN STA 190 TO 210, LBL O IN TO 22 IN, WAS COMING LOOSE AND HAD POPPED RIVETS INSTALLED. REPLACED MEMBRANE PER SPM 6-70-01, 775T3 30 PER ORIGINAL SAMPLE.May 25, 1999 · N981Z · Doug DC931 · Fuselage Floor PanelSDR TWAA9907506Frame · bentDURING OP 16 MAINT CHECK, FOUND ON RT SIDE OF AIRCRAFT AT CUSP LINE STA 996, THE FWD EDGE OF THE FLANGE WAS BLENDED AND REPAIRED. INSTALLED TEE CAP PER SRM 53-03, FIG 37.May 18, 1999 · N981Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9907510Casting · crackedDURING OP 16 MAINT CHECK, FOUND LT WING REAR SPAR I/B FLAP ATTACH CASTING HAD CRACK INDICATION AT LOWER O/B HOLE AT 8 O'CLOCK AND LOWER I/B HOLE AT 5:30 AND 6:00 O'CLOCK POSITIONS. REPAIRED PER MC8-AD-34 AND DRAWING JO60271M.May 11, 1999 · N981Z · Doug DC931 · Wing, Control Surface Attach FittingsSDR TWAA9906904Bulkhead · crackedDURING OP 16 MAINT CHECK, FOUND STA 965 BULKHEAD CRACKED BETWEEN LONGER 15 AND 16L. REMOVED AND REPLACED WEB PER SPM 6-70-01.May 10, 1999 · N981Z · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9907001Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND FLOORBEAM AT STA 160, RBL 48, WITH CORROSION MATERIAL LOSS BEYOND LIMITS TO THE TOP CAP AFT FLANGE. REPAIRED PER SRM 53-05, FIG 20A.May 7, 1999 · N981Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA9907301Floorbeam · crackedDURING OP 16 MAINT CHECK, FOUND CABIN FLOORBEAM REPAIR CRACKED 2 INCHES LONG IN UPPER CAP RADIUS AT FWD SIDE OF STA 180, LBL 15. REPLACED FLOORBEAM TEE UPPER CAP PER SRM 53-11-1, FIG 13 SHEET 1, PAGE 45 AND 47, FIG 13 SHEET 2 AND DAC DRAWING 9923484. INSTALLMay 5, 1999 · N981Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA9906903Splice · crackedDURING OP 16 MAINT CHECK, FOUND IN FWD CARGO COMPT THAT LONGERON 30 PRODUCTION SPLICE HAD 2 CRACKS APPROX 1 INCH LONG AT STA 229. REPLACED CRACKED SPLICE PER DOUGLAS INSTALLATION DRAWING 5913508.May 5, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9906902Casting · crackedDURING OP 16 MAINT CHECK, FOUND RT WING T/E REAR SPAR CENTER FLAP ATTACH CASTING HOLES LINER O/B HOLE AT 6 O'CLOCK POSITION WITH CRACK INDICATION. FIFTEEN PERCENT THICKNESS GROUND OUT AND CRACK WAS GONE. REPAIRED REAR SPAR AREA PER DOUGLAS SERVICE REWORK DRAMay 5, 1999 · N981Z · Doug DC931 · Wing, Control Surface Attach FittingsSDR TWAA9906901Former · corrodedDURING OP 16 MAINT CHECK, FOUND FORMER AND WEB CORRODED AT STA 200 TO 206, LONGERON 18L AND ABOVE. REMOVED CORROSION PER SPM 6-80-1, PARAGRAPH 3, SECTION A FIG 1. INSTALLED NEW WEB PER SPM 6-70-1.May 4, 1999 · N981Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9906405Membrane · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE BELOW CABIN FLOOR AT RBL 45 TO RBL 55 IN, AT STA 218 TO 237. REMOVED CORRODED MEMBRANE AND INSTALLED NEW ONE PER SPM 6-70-01.Apr 29, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9906702Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965. REPLACED LONGERON PER SRM 53-02 FIG 18 AND LONGERON IDENTIFICATION 53-11-3. LONGERON REPLACED FROM STA 950 TO 996.Apr 24, 1999 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9906004Depressor · damagedDURING OP 16 MAINT CHECK, FOUND A CRACK FROM RIVET HOLE LOWER FWD CORNER OF AFT CARGO DOOR CUT OUT. REMOVED LOWER SECTION OF DEPRESSOR, LOCATED AND DRILLED NEW DEPRESSOR, SEALED AND INSTALLED PER SPM 6-70-01, PAGE 3.Apr 19, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9904206Longeron · crackedFOUND LONGERON 7R CRACKED AT STA 617, .375 INCH OUT OF BOLT HOLE. REMOVED CRACKED LONGERON FROM STA 610R TO 644R. REPAIRED PER SRM 53-2 FIG 18 AND STANDARD PRACTICES. CHECK-C 8-25-98 STL.Mar 15, 1999 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9806401Vane · separatedDTW - FLT 349 - RT ENGINE STALLED ON TAKEOFF ROLL. ABORTED TAKEOFF. SHUT ENGINE DOWN. TOWER REPORTED FIRE OUT TAIL PIPE. FIRE FIRE EXTINGUISHING BOTTLES. PASSENGERS EXITED FROM FWD EVACUATION SLIDES. REPLACED ENGINE. CHECK-C 5-22-97 STL. ONE EACH SEVENApr 25, 1998 · N981Z · Doug DC931 · Turbine Engine Compressor SectionSDR TWAA9744001Uplimit Switch · failedSTL - FLT 565 - DURING CLIMB, FOLLOWING GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON. REMOVED AND REPLACED NOSE GEAR UPLIMIT SWITCH, MFG P/N H14-6, MANUFACTURED BY EATON CORP. OPERATION CHECK NORMAL. (M)Mar 31, 1997 · N981Z · Doug DC931 · Landing Gear Position and WarningSDR 96ZZZM799Power Supply · inoperativeDURING A PREFLIGHT CHECK OF THE EMERGENCY EGRESS LIGHTS, THEY REMAINED ILLUMINATE. REMOVED AND REPLACED EGRESS POWER SUPPLY, MFG P/N 5322-2. OPERATIONAL CHECK NORMAL.Apr 1, 1996 · N981Z · Doug DC931 · Emergency LightingSDR 96ZZZM789Longeron · corrodedDURING OP-15, FOUND .75 INCH CRACK IN LONGERON 22L AND CORROSION AT STATION 190. REPAIRED BY INSTALLING NEW LONGERON AND HI-LOKS IN LONGERON 22L PER SRM 53-02, FIGURE 2.Mar 20, 1996 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 96ZZZM788Longeron · crackedDURING OP-15, FOUND A .75 INCH CRACK AT BELT RING ATTACH POINT OF LONGERON 23L, STATION 200. REPAIRED BY INSTALLING NEW LONGERON PER SRM 53-02, FIGURE 2.Mar 20, 1996 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 96ZZZM791Blkhd Web · crackedDURING OP-15, FOUND A SIX INCH CRACK AT LOWER OUTBOARD CORNER OF RIGHT FORWARD ENGINE MOUNT BULKHEAD WEB, STATION 965. REPAIRED PER SRM 53-03, FIGURE 21.Mar 13, 1996 · N981Z · Doug DC931 · Nacelle/Pylon, Bulkhead/FirewallSDR 96ZZZM792Angle · crackedDURING OP-15, FOUND .75 INCH CRACK IN LEFT PYLON ATTACHED ANGLE VERTICAL LEG TOP SIDE, STATION 980. STOP DRILLED CRACK AND REPAIRED PER SRM 54-04.Mar 12, 1996 · N981Z · Doug DC931 · Nacelle/Pylon StructureSDR 96ZZZM782Floorbeam · corrodedDURING OP-15, FOUND CORROSION AROUND TWO ADJACENT NUT PLATES UPPER CAP, FLOORBEAM STATION 980, INBOARD OF CUSP ANGLE. REMOVED CORRODED AREAS AND INSTALLED REPAIR PER SRM 53-05, FIGURE 20A.Mar 8, 1996 · N981Z · Doug DC931 · Fuselage Main, Floor BeamSDR 96ZZZM783Longeron · corrodedDURING OP-15, FOUND CORROSION AT LONGERON SPLICE OF LONGERON 30, STATION 400. REPAIRED BY INSTALLING NEW SECTION OF LONGERON PER ARA 10074 AND SRM 53-07, FIGURE 14. (M)Mar 7, 1996 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 96ZZZM784Longeron · crackedDURING OP-15, FOUND A ONE INCH CRACK IN E/E COMPARTMENT, STATION 160, LONGERON 25L, AT ATTACH POINT. REPAIRED PER SRM 53-02, PAGE 2A, FIGURE 2.Mar 5, 1996 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 96ZZZM786Longeron · crackedDURING OP-15, FOUND TWO CRACKS IN LONGERON 5R, .5 INCH AT STATION 699, AND .25 INCH AT STATION 737. REPAIRED BOTH PER SRM 53-02, FIGURE 2.Mar 2, 1996 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 96ZZZM785Longeron · crackedDURING OP-15, FOUND A .75 INCH CRACK IN LONGERON 4R, STATION 617. REPAIRED BY INSTALLING NEW SECTION OF LONGERON PER SRM 53-04.Mar 2, 1996 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 96ZZZM790Longeron · crackedDURING OP-15, FOUND LONGERON 30 CRACKED APPROXIMATELY 10 INCHES FROM STATION 794, AFT TO SPLICE. REPLACED LONGERON 30 FROM STATION 756 TO 813 PER SRM 51-30 AND TWA STANDARD PRACTICES.Mar 14, 1995 · N981Z · Doug DC931 · Fuselage Main, Longeron/Stringer
Back to N981Z, cancelled Sep 19, 2016