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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR TWAA0103010Longeron · crackedDURING CHECK-C MAINT FOUND LONGERON REPAIR AT STA 1079, LONGERON 2R, WAS CRACKED 1.5 INCHES. REPAIRED PER SRM 53-02.SDR 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.SDR TWAA0011303Battery · dischargedTHE LT AND RT AFT OVERWING EMERGENCY EXIT LIGHTS WERE DIM. REPLACED THE BATTERIES. CHECK-C 12-14-99 STL.SDR 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 PILLOWEDSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 SSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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)SDR 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)SDR 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. THSDR 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)SDR 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. SDR 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)SDR 96ZZZM1353Power Supply · inoperativeSTL - DURING CRUISE, EMERGENCY EGRESS LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED POWER SUPPLY, MFG P/N 5822-2. OPERATIONAL CHECK NORMAL.SDR 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)
Back to N983Z, cancelled May 30, 2013