N983Z, cancelled May 30, 2013

Service difficulty reports · 54

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 = 'N983Z' AND deregistration_id = 'N983Z-2013-05-30'
  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 TWAA0103011Attach Angle · crackedDURING CHECK-C MAINT IN THE VERT STAB FOUND CRACK IN RT AFT VERTICAL ATTACH ANGLE. CUT OUT CRACKED AREA AND FABRICATED FILLER AND REPAIR ANGLE AND INSTALLED PER SRM 53-05, FIG 23.Feb 14, 2001 · N983Z · Doug DC931 · Vertical StabilizerSDR TWAA0103010Longeron · crackedDURING CHECK-C MAINT FOUND LONGERON REPAIR AT STA 1079, LONGERON 2R, WAS CRACKED 1.5 INCHES. REPAIRED PER SRM 53-02.Feb 14, 2001 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA0100101Battery Pack · dischargedTHE LEFT NACELLE LIGHT WAS INOPERATIVE ON THE EMERGENCY LIGHT CHECK. REPLACED THE LEFT OVERWING EMERGENCY BATTERY PACK. CHECK-C 12-14-99.Jan 1, 2001 · N983Z · Doug DC931 · Emergency LightingSDR TWAA0011303Battery · dischargedTHE LT AND RT AFT OVERWING EMERGENCY EXIT LIGHTS WERE DIM. REPLACED THE BATTERIES. CHECK-C 12-14-99 STL.Jul 19, 2000 · N983Z · Doug DC931 · Emergency LightingSDR TWAA9916805Skin · dentedDURING OP 16 MAINT CHECK, FOUND AT STA 427 AND LONGERON 29R, HAD BLIND FASTENER PULLED AND SKIN PILLOWING, AND SKIN DENTED 7 IN BY 1 IN BY 0.10 DEEP. FOUND NO CRACK PER SRM 53-603 PART 6. REPAIRED DENT IN SKIN PER ARA 16217 AND SRM 53-05 FIG 105 AND PILLOWEDNov 30, 1999 · N983Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9916804Skin · damagedDURING OP 16 MAINT CHECK, FOUND LARGE FASTENER HOLES IN FUSELAGE SKIN AT LONGERON 29L, STA 579 AREA. INSTALLED SKIN REPAIR AT LONGERON 29L, STA 579, TO REPAIR LARGE FASTENER HOLES PER ARA 16470 AND SRM 53-04, FIG 12B.Nov 30, 1999 · N983Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9916803Frame · corrodedDURING OP 16 MAINT CHECK, FOUND SECTION OF STA 604 BULKHEAD TEE CHORD FROM O/B OF LONGERON 29L TO O/B OF 29R HAD CORROSION. REPLACED LOWER SECTION OF STA 604 TEE CHORD BECAUSE OF OUT OF LIMIT CORROSION BETWEEN L28L TO L28R PER ARA 16470.Nov 30, 1999 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9916703Longeron · crackedDURING OP 16 MAINT CHECK, LONGERON 30 WAS CRACKED AT STA 570, APPROXIMATELY 4 INCHES LONG, LEFT AND RIGHT SIDE OF LONGERON. INSTALLED SPLICE REPAIR PER SRM 53-02, FIG 14.Nov 30, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9916702Skin · damagedDURING OP 16 MAINT CHECK, FOUND LARGE FASTENER HOLES IN FUSELAGE SKIN AT LONGERON 29L, STA 579 AREA. INSTALLED SKIN REPAIR AT LONGERON 29L AT STA 579 TO REPAIR LARGE FASTENER HOLES PER ARA 16470 AND SRM 53-04, FIG 12B.Nov 30, 1999 · N983Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9916701Skin · crackedDURING OP 16 MAINT CHECK, FOUND CRACK INDICATION USING LFEC AT LOWER AFT CORNER OF THE FORWARD CARGO DOOR OPENING. CRACK CONTAINED PER SRM 51-00-03, PART 6. REPAIRED PER SRM 53-05.Nov 29, 1999 · N983Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9916204Frame · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON THE FORMER FOOT AT STA 598, RT SIDE OF LONGERON 30. REMOVED VISIBLE CORROSION PER SPM 6-80-1 AND SRM 51-10-03. INSTALLED NEW FORMER FOOT PER SRM 53-03 FIG 3.Nov 22, 1999 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9916203Frame · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON THE FORMER FOOT AT STA 598, BETWEEN LONGERON 29L AND 30L. REMOVED VISIBLE CORROSION PER SPM 6-80-01 AND SRM 51-10-3. INSTALLED NEW FORMER FOOT PER SRM 53-03, FIG 3.Nov 22, 1999 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9915805Longeron · crackedDURING OP 16 MAINT CHECK, FOUND AN EIGHT INCH CRACK AT STA 579 TO 598, LONGERON 29L, AT THE CENTER OF THE LONGERON AT SPLICE JOINT. INSTALLED NEW FITTING PER SPM 6-70-1.Nov 8, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9915804Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 29L AFT OF STA 579, WITH ABOUT A 6 INCH CRACK IN THE I/B SIDE OF FLANGE OF LONGERON. INSTALLED LONGERON END AND SPLICE PER SRM 53-02, FIG 14 AND ARA 16211B.Nov 8, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9915807Spar · crackedDURING OP 16 MAINT CHECK, FOUND A CRACK ON RT WING INSIDE THE I/B TOP HOLE FOR THE I/B FLAP HINGE CASTING UPPER SPAR AREA AT 11 O'CLOCK POSITION. REAMED OUT HOLE AND INSTALLED BUSHING AND DOUBLER REPAIR PER J060271 AND ARA 16217.Nov 3, 1999 · N983Z · Doug DC931 · Leading Edge DevicesSDR TWAA9914801Former · corrodedDURING OP 16 MAINT CHECK, THE AFT CARGO FORMER CAP ANCHOR NUT HOLE WAS CORRODED AT STA 937, LONGERON 28L. REMOVED AND REPLACED FORMER CAP PER SRM 6-70-01.Oct 21, 1999 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9914102Skin · crackedDURING OP 16 MAINT CHECK, FOUND CRACK INDICATION AT THE FORWARD CARGO DOOR, UPPER FORWARD CORNER OF THE FUSELAGE SKIN. REPAIRED SKIN CRACK PER DOUGLAS SERVICE BULLETIN 53-277 AND SRM 53-05, FIG 105.Oct 5, 1999 · N983Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9914104Angle · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON THE UPPER FLANGE OF FLOOR ATTACH ANGLE, STA 160 RBL 1.5 INCHES TO 10 IN. REMADE FLOOR SUPPORT ANGLE WITH (P/N S2652479-12000). REINSTALLED FASTENERS IN FLOOR SUPPORT PER SRM 51-30-5.Oct 1, 1999 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9913517Membrane · corrodedDURING OP 16 MAINT CHECK, FOUND THE FLOOR MEMBRANE UNDER THE FORWARD GALLEY WATER SUPPLY PAN WAS CORRODED. REMADE GALLEY MEMBRANE FROM SAME MATERIAL 7075-T6, 0.020. REINSTALLED RIVETS IN MEMBRANE PER SRM 51-30-2. REINSTALLED HI-LOCKS IN MEMBRANE AND FLOOR SSep 29, 1999 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9915906Frame · crackedDURING OP 16 MAINT CHECK, FOUND FUSELAGE FRAME (P/N 9911505-7) CRACKED 2 PLACES AT STA 83, APPROX 1.25 INCH CRACK. REPLACED FRAME PER SRO 9530268 DRAWING AND EMLR 70039.Sep 28, 1999 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9915904Frame · crackedDURING OP 16 MAINT CHECK, CENTER FRAME ANGLE 5912350-17 WAS CRACKED APPROX 1.5 IN RADIUS AT I/B END, STA 83.55 X=10.00, Z=42 IN LT SIDE. REPLACED ANGLE PER SRO9530268 DRAWING AND EMLR 70039.Sep 25, 1999 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9915902Bulkhead · crackedDURING OP 16 MAINT CHECK, FOUND RT STA 965.091 BULKHEAD CRACKED 3 PLACES BETWEEN 220 AND 225. REPLACED RT STA 965.091 BULKHEAD ANGLE CHORD PER DRAWING JO60119 AND DRAWING 5936993.Sep 25, 1999 · N983Z · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9915905Frame · crackedDURING OP 16 MAINT CHECK, CENTER FRAME ANGLE 5912350-17 WAS CRACKED APPROX 1.75 INCHES IN RADIUS AND 1.5 IN AT ATTACH RIVETS AT I/B END, STA 83.55, X=-10 IN, Z=42, RT SIDE. REPLACED ANGLE PER SRO 9530268 DRAWING AND EMLR 70039.Sep 24, 1999 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9913515Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND NUMBER 1 CHAIR TRACK CORRODED AND GROUND BEYOND LIMITS AT STA 200. REPLACED TRACK PER SPM 6-70-01.Sep 23, 1999 · N983Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9915907Spar · crackedDURING OP 16 MAINT CHECK, FOUND LEFT WING HAD CRACK APPROX 1 INCH LONG AT LOWER I/B HOLE ON FACE OF REAR SPAR AT I/B FLAP HINGE AREA, 5 O'CLOCK POSITION. STOP DRILLED CRACK PER DWG JO60271. REPAIRED LT WING REAR SPAR AT I/B FLAP HINGE AREA PER DOUGLAS PRINT Sep 20, 1999 · N983Z · Doug DC931 · Wing SparSDR TWAA9915903Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 4L WITH 2 INCH CRACK AT STA 160 AND 200. REPLACED LONGERON PER SPM 6-70-01, PAGE 2.Sep 15, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9913516Angle · corrodedDURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON UPPER FLANGE OF FLOOR ATTACH ANGLES, STA 160 TO 200, BL 0 INCHES. REPLACED FLOOR SUPPORT PER SPM 6-70-01, PAGE 3.Sep 15, 1999 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9913518Splice · corrodedDURING OP 16 MAINT CHECK, FOUND LONGERON 30 SPLICE CORRODED AT STA 960. REMOVED SPLICE AND INSTALLED NEW SPLICE PER SRM 51-60-0, PAGE 27, AND SRM 51-30-5, AND DOUGLAS INSTALLATION DRAWING 5919707.Sep 14, 1999 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9913101Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND NUMBER 3 CHAIR TRACK CORRODED BETWEEN STA 200 AND 218. REPLACED TRACK PER SPM 6-70-01, PAGE 3.Sep 12, 1999 · N983Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9912411Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND AT STA 69, X-10, UPPER END OF VERTICAL STIFFENER WAS CRACKED AT RIVET HOLE. REPLACED PART PER SRM 51-01.Sep 10, 1999 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9912410Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND AT STA 69, X-10, UPPER END OF VERTICAL STIFFENER WAS CRACKED ABOVE AND BELOW RIVET HOLE. REPLACED PARTS PER SRM 51-01.Sep 10, 1999 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9912409Longeron · crackedDURING OP 16 MAINT CHECK, LONGERON 17R HAD APPROX .5 IN CRACK AT AFT SIDE OF STA 965 BULKHEAD. INSTALLED LONGERON HAT SECTION REPAIR PER SRM 53-02, FIG 18, SHEETS 1-4 AND 5.Sep 8, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9912408Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 16R WITH A CRACK AT AFT SIDE OF STA 965 BULKHEAD, AT TOP FLANGE OF LONGERON, APPROX 1.5 INCHES LONG. REPAIRED LONGERON 16R WITH HAT SECTION REPAIR PER SRM 53-02, FIG 18 SHEETS 1-4 AND 5.Sep 8, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9912407Frame · crackedDURING OP 16 MAINT CHECK, FOUND (P/N 9911505-5) FRAME CRACKED AT STA 83.5, X+10. INSTALLED DOUBLER PER SRM 53-03, FIG 34 AND TWA SPM 6-70-1 PAGE 3.Sep 8, 1999 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9912406Frame · crackedDURING OP 16 MAINT CHECK, FOUND (P/N 9911505-6) FRAME CRACKED AT STA 83.5, X-10. INSTALLED DOUBLER PER SRM 53-03, FIG 34 AND TWA SPM 6-70-01 PAGE 3.Sep 8, 1999 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9912405Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND NUMBER 3 CHAIR TRACK CORRODED BETWEEN STA 200 AND 218. REPLACED TRACK PER SPM 6-70-01, PAGE 3.Sep 8, 1999 · N983Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9912404Skin · crackedDURING OP 16 MAINT CHECK, FOUND SKIN CRACK AT FASTENER 18 INCHES RIGHT OF CENTER LINE, STA 69.5. REPAIRED PER MC8-AD-DU AND DRAWING SR09530239.Sep 3, 1999 · N983Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9912403Skin · crackedDURING OP 16 MAINT CHECK, FOUND RIVET HOLE 16 INCHES RIGHT OF CENTER, AT STA 69, SHOWING A CRACK USING HIGH FREQ EDDY CURRENT. REPAIRED PER MD8-AD-DU, AND DRAWING SRO9530239.Sep 3, 1999 · N983Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9910306Longeron · crackedFOUND LONGERON 5L CRACKED AT STA 699. SPLICED IN NEW LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 1-5-99 STL.Jul 19, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9910305Longeron · crackedFOUND LONGERON 5L CRACKED AT STA 680. SPLICED IN NEW LONGERON SECTION PER SRM 53-02 FIG 18. CHECK-C 1-5-99 STL.Jul 19, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9910304Longeron · crackedFOUND LONGERON 5R CRACKED AT STA 699, APPROX .375 INCH. CUT OUT DAMAGED AREA AND SPLICED IN NEW PER SRM 53-02 FIG 18. CHECK-C 1-5-99 STL.Jul 19, 1999 · N983Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9820305Jamb · crackedDURING CHECK-C, MAINT FOUND FWD SERVICE DOOR JAMB WITH A 1.5 INCH CRACK IN LOWER AFT CORNER FROM A NUT PLATE AREA. REPAIRED PER SRM 53-05, FIG 112.Dec 31, 1998 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9810204Frame · damagedSTL - FOUND AFT OF AFT CARGO DOOR DAMAGED AT STA 945. REPAIRED FRAME PER ARA 15094 AND SRM 53-05, FIG 80. CHECK-C 10-12-97 MCI. TOTAL TIME: 67,905. TOTAL CYCLES: 78,196. (X)May 17, 1998 · N983Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9810203Doubler · damagedSTL - FOUND INTERNAL DOUBLER AFT OF AFT CARGO DOOR AT STA 945 DAMAGED. REMOVED AND REPLACED INTERNAL DOUBLER PER ARA 15094, AND SRM 53-05, FIG 80. CHECK-C 10-12-97 MCI. TOTAL TIME: 67,905 HOURS. TOTAL CYCLES: 78,196. (X)May 17, 1998 · N983Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9803402Chamber · crackedRDU - FLT 503 - RT ENGINE INJESTED BIRD ON ROTATION FOR TAKEOFF. EGT ROSE TO 620 DEGREES. N1 AND N2 STEADY. NO VIBRATION. REDUCED POWER AND RETURNED TO RDU. REPLACED ENGINE. S/D: EXAMINATION OF THE ENGINE SHOWED SEA GULL WAS INGESTED CAUSING STALLS. THMar 9, 1998 · N983Z · Doug DC931 · Turbine Engine Combustion SectionSDR TWAA9701002Restrictor Valve · failedSTL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR. REMOVED AND REPLACED LEFT MAIN LANDING GEAR RESTRICTOR VALVE. OPERATIONAL AND LEAK CHECKS NORMAL. (M)Jan 16, 1997 · N983Z · Doug DC931 · Landing Gear Retraction/Extension SystemSDR TWAA9616104Strut · req'd serviceDSM - DSM - FLT 539 - AFTER TAKEOFF, LANDING GEAR SELECTOR HANDLE WAS LOCKED IN THE DOWN POSITION. RETURNED TO DSM. FOUND NOSE LANDING GEAR STRUT AIR PRESSURE LOW. SERVICED NOSE LANDING GEAR STRUT WITH NITROGEN. LANDING GEAR OPERATION THEN CHECKED NORMAL. Dec 29, 1996 · N983Z · Doug DC931 · Nose/Tail Landing Gear Strut/AxleSDR TWAA9614901Linkage · lack of lubeSTL - FLT 212 - DURING APROACH WHEN LANDING GEAR WAS EXTENDED, LEFT MLG DOWN AND LOCKED LIGHT WAS SLOW TO ILLUMINATE. LUBRICATED SWITCH AND LINKAGE. LANDING GEAR INDICATION THEN CHECKED NORMAL. CHECK C - 8-1-96 - STL. (X)Nov 30, 1996 · N983Z · Doug DC931 · Landing Gear Retraction/Extension SystemSDR 96ZZZM1353Power Supply · inoperativeSTL - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL.Aug 5, 1996 · N983Z · Doug DC931 · Emergency LightingSDR 96ZZZM1361Doubler · crackedSTL - DURING OP-15, FOUND .5 INCH CRACK INSIDE REPAIR DOUBLER INSIDE LONGERON 2R, STATION 1076. REPAIRED PER SRM 53-02, PGES 8-10, SECTION 2. (M)Jul 26, 1996 · N983Z · Doug DC931 · Fuselage Miscellaneous Structure
Back to N983Z, cancelled May 30, 2013