N959U, cancelled Aug 19, 2008
Service difficulty reports · 73
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 = 'N959U' AND deregistration_id = 'N959U-2008-08-19' 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.
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 = 'N959U' AND deregistration_id = 'N959U-2008-08-19' 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 AALA20060138Smoke · detectedDEN - FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN ON CLIMBOUT. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. SMOKE HAD DISSIPATED AT LANDING. ACCOMPLISHED WORK CARD 21-96-01. ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUSTING PER MAINTENANCE MANUAL 21-2SDR AALA20041063Battery Pack · inoperativeDFW - AFT OVERWING EMERGENCY EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR AFT OVERWING EMERGENCY EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20041028Switch · inoperativeDFW - FLIGHT ATTENDANT SWITCH WILL NOT ILLUMINATE EMERGENCY LIGHTS. REPLACED FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH AND AFT CARGO EMERGENCY LIGHT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ZW0A0205601Light · defectiveMAL-FWD OVERHEAD GALLEY LIGHT PN 293-0077 GETS VERY HOT AND SMELLS OF ELECTRICAL BURNING ODOR. DEACTIVATED AND REMOVED BULB. PLACARDED PER MEDP 33-2. PULLED AND BANDED FWD MIS CABIN AND LAV LT CB. HEAT AND SMELL GONE. LAST CHECK-C STL 6/28/01SDR ZW0A0108801Light · contaminatedTHE EGRESS LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. CLEANED AND DRIED OUT THE LIGHT STRIP. CHECK-C 6-28-01 STL.SDR ZW0A0107202Light · inoperativeTHE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 21 TO 26. REPLACED BROKEN CONTACT ON POWER STRIP AT THE LIGHT TRACK.SDR ZW0A0101501Light · inoperativeTHE EGRESS LIGHTING IN THE FIRST CLASS SECTION WAS INOPERATIVE. REMOVED THE LIGHT STRIP. CLEANED THE TRACK AND ELECTRICAL CONTACTS. PRESERVED CONTACTS WITH MOISTURE LOCKOUT BEFORE RE-INSTALLING. CHECK-C 12-3-00 MCI.SDR TWAA0018616Seat Track · corrodedDURING CHECK-C MAINT FOUND FASTENER HOLES FOR FLOOR AND SIDEWALL PANELS CORRODED AT LT FLOOR TRACK STA 1170 TO STA 1221. REPLACED CORRODED SECTION OF TRACK PER SRM 53-05, FIG 4G.SDR TWAA0018615Casting · corrodedDURING CHECK-C MAINT ON LT WING THE O/B FLAP I/B MOUNT CASTING ON SPAR TOP I/B STUD WAS EMITTING RUST. REPLACED 2 UPPER STUDS AND INSTALLED NEW HINGE CASTING PER MM 57-40-01.SDR TWAA0018419Beam · corrodedDURING CHECK-C MAINT IN AFT CARGO COMPT FOUND DOOR BEAM CORRODED AT STA 1155 TO 1211. REMOVED CORROSION PER SPM 6-80-01. BEAM OUT OF LIMITS AND REPLACED PER DRAWING 5936038-501. INSTALLED PER SRM 51-30-02 AND 51-30-05. TREATED AND PAINTED PER 51-10-3.SDR TWAA0018416Frame · corrodedDURING CHECK-C MAINT IN THE AFT CARGO COMPARTMENT A FORMER WAS CORRODED AT STA 1308, LONGERON 28R TO 23L. REMOVED FRAME FROM LONGERON 18R TO 18L. INSTALLED NEW FRAME. INSTALLED SPLICE BETWEEN LONGERON 25R AND 26R PER SRM 53-03, PAGE 4C, AND FIG 2A FOR THICKSDR TWAA0018418Seat Track · corrodedDURING CHECK-C MAINT FOUND CORROSION ON TRACK AT STA 200 TO 237, RBL 44. REMOVED CORROSION PER SPM 6-80-1. REPLACED 47 INCHES OF TRACK PER SRM 53-08 FIGURE 4F.SDR TWAA0018417Web · crackedDURING CHECK-C MAINT FOUND MEMBRANE CRACKED AT STA 237, RBL 46. REPLACED CRACKED MEMBRANE WITH SHOP FABRICATED NEW ONE. INSTALLED WITH FASTENERS PER SRM 51-30-02.SDR TWAA0018415Web · corrodedDURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 170 TO 200, RBL 56 TO 58, AND ON MEMBRANE UNDER FLOOR SUPPORT AT STA 180 TO 200, RBL 53. INSTALLED NEW MEMBRANES FROM STA 160 TO 200, RBL 44 TO 57, PER SRM 53-01 PAGE 9 FIGURE 2, DRAWING 9936534, SRM 51-SDR TWAA0018414Web · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CUSP AT STA 170 TO 200, AT FWD SERVICE DOOR SILL AREA. RE-INSTALLED FASTENERS REMOVED FOR CORROSION REMOVAL. REMOVAL PER SRM 51-30-1, 51-30-2, AND 51-30-5.SDR TWAA0018413Web · corrodedDURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE UNDER RT SERVICE DOOR SILL AT STA 170 AND ON MEMBRANE AT STA 160, RBL 43. INSTALLED NEW MEMBRANE FROM STA 160 TO 200, RBL 44 TO 57 PER SRM 53-01, PAGE 9 FIG 2, DRAWING 9936534, SRM 51-30-2, AND SRM 51-30-5. SESDR TWAA0018412Floor Support · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOOR SUPPORT STA 180, RBL 10 TO RBL 44. NEW FLOOR SUPPORT FABRICATED PER DRAWING 9936534. PAINTED PER SRM 51-10. INSTALLED FASTENERS PER SRM 51-30-2, SRM 51-30-05. SEALED STIFFENER PER SRM 51-20-0.SDR TWAA0018411Web · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE AT STA 200 RT SIDE, AND UNDER T-ANGLE BOTTOM DOOR FRAME (JAMB) SUPPORT. INSTALLED NEW MEMBRANE FROM STA 160 TO 200, RBL 44 PER SRM 53-01 PAGE 9, FIG 2, DRAWING 993634.SDR TWAA0018410Web · corrodedDURING CHECK-C MAINT FOUND CORROSION ON MEMBRANE AT STA 200, RBL 46 TO 50, AND ON MEMBRANE RT SIDE AT SIDEWALL TO FLOOR SUPPORT ANGLE STA 160 TO 180, RBL 53 TO 57. INSTALLED NEW MEMBRANES FROM STA 160 TO 200, RBL 44 TO RBL 57, PER SRM 53-01 PAGE 9 FIGURE 2, DSDR TWAA0018614Seat Track · corrodedDURING CHECK-C MAINT FOUND FASTENER HOLES CORRODED FOR FLOOR AND SIDE WALL PANELS AT LT FLOOR TRACK STA 1221 THRU 1322. REPAIRED PER SRM 53-05, FIG 4G.SDR TWAA0018613Floor Support · corrodedDURING CHECK-C MAINT FLOOR SUPPORT WAS CORRODED AT STA 160 TO 200, RBL 44 IN. NEW FLOOR SUPPORT FABRICATED PER DRAWING 9936534. PAINTED PER SRM 51-10-3.SDR TWAA0018612Floor Support · corrodedDURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 160 TO 180, RBL 53 INCHES. FABRICATED NEW FLOOR SUPPORT PER DRAWING 9936534. PAINTED PER SRM 51-10-3.SDR TWAA0018409Floor Support · corrodedDURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 200, RBL 10 IN TO RBL 48 INCHES. FABRICATED NEW FLOOR SUPPORT PER DRAWING 9936534. PAINTED AND TREATED PER SRM 51-10-3. INSTALLED NEW SUPPORT PER SRM 51-30.SDR TWAA0018408Floorbeam · corrodedDURING CHECK-C MAINT, THE CABIN FLOOR AND GALLEY DRAIN PAN SUPPORT WAS CORRODED AT STA 160, RBL 53 INCHES. INSTALLED SUPPORT ANGLE PER SRM 51-30. REMADE FLOOR SUPPORT FROM RAW STOCK.SDR TWAA0018407Frame · corrodedDURING CHECK-C MAINT FOUND CORROSION AT PREVIOUS REPAIR FWD SIDE OF FORMER STA 1287, LONGERON 29L THRU L29R. FORMER FRAME SEGMENT WAS REPLACED FROM LONGERON 18L TO AND BETWEEN LONGERON 25R AND L26R PER SRM 53-03, FIG 2A, AND DRAWING 9957739.SDR TWAA0018406Frame · corrodedDURING CHECK-C MAINT FOUND CORROSION AT FORMER FOOT STA 1287, BETWEEN LONGERON 30R AND LONGERON 29R. NEW FORMER FOOT WAS INSTALLED PER DRAWING 9957739.SDR TWAA0018405Splice · corrodedDURING CHECK-C MAINT FOUND CORROSION ON SPLICE PLATE AFT SIDE OF FORMER STA 1287, LONGERON 30 AND 28L. FORMER FRAME SEGMENT WAS REPLACED FROM LONGERON 18L AND BETWEEN L25R AND L26R PER SRM 53-03, FIG 2A, AND DRAWING 9957739.SDR TWAA0018404Frame · corrodedDURING CHECK-C MAINT FOUND CORROSION ON FORMER AT STA 1287, FROM LONGERON 30 T0 23L, FWD SIDE. FORMER FRAME SEGMENT WAS REMOVED FROM LONGERON 18L AND BETWEEN L25R AND L26R. NEW FRAME WAS INSTALLED PER SRM 53-03, FIG 2A AND PER DRAWING 9957739.SDR TWAA0017907Skin · damagedDURING CHECK-C MAINT, THE FUSELAGE SKIN WAS REMOVED TO A THICKNESS OF 0.029 IN AT LT STA 237 BETWEEN LONGERON 17L AND 18L, MEASURED WITH NDT U.T. THICKNESS STRESSTEL INSTRUMENT. REMEASURED SKIN THICKNESS WITH NORTEC 1000 AND KRAUTKRAMER PENCIL THINKNESS PROBESDR TWAA0017906Skin · delaminatedDURING CHECK-C MAINT, ON RT WING T/E THE I/B FLAP T/E WEDGE WAS DELAMINATED APPROX 65 INCHES TO 72 INCHES FROM I/B END OF FLAP. CLEANED DAMAGED AREA AND REPAIRED PER SRM 51-90-0.SDR TWAA0017905Seat Track · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON TRACK AT LBL 59 AT GALLEY TIE DOWN STA 1208. ALSO CORROSION ON TRACK AT LBL 58 ON FLANGE AND AT GALLEY TIE DOWN STA 1236. CORROSION ALSO FOUND ON TRACK AT LBL 58 AT GALLEY TIE DOWN AT STA 1174. REPLACED TRACK FROM SSDR TWAA0017904Seat Track · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON NUMBER 2 CHAIR TRACK O/B OF FLOOR PANEL 1 ATTACH FLANGE, STA 1265 TO 1309. ALSO CORROSION ON TRACK FLANGE STA 1193 TO 1212 AT LBL 48. REPLACED CHAIR TRACK FROM STA 1032 TO 1307 PER SPM 6-70-01. INSTALLED SPLICE PER SSDR TWAA0102403Seat Track · corrodedDURING CHECK-C MAINT FOUND CORROSION IN SEAT TRACK AT LBL 24 INCHES, STA 1205 TO 1309. MATERIAL .25 INCH THICK MISSING. REMOVED AND REPLACE CHAIR TRACK AT LBL 24 IN FROM STA 1180 TO 1309 WITH STOCK MATERIAL, SPLICE AND PLATE. ATTACHED WITH HI-LOKS, MS250 WASDR TWAA0017903Frame · corrodedDURING CHECK-C MAINT, FOUND FORMER CORRODED ABOVE LONGERON 29L, AT STA 1193. REMOVED FORMER, FABRICATED, HEAT TREATED AND INSTALLED NEW FORMER PER DRAWING 9936073.SDR TWAA0017902Strap · corrodedDURING CHECK-C MAINT, FOUND STRAP UNDER TRACK AT LBL 59 IN WAS CORRODED FROM STA 1136 TO 1142, AND THE FASTENER HEADS WERE POPPED. REPAIRED, REPLACED NEW STRAP PER SPM 6-70-01. PAINTED PER SRM 51-30-05. INSTALLED FASTENERS PER SRM 51-30-05.SDR TWAA0017901Floor Panel · corrodedDURING CHECK-C MAINT, FOUND CORROSION AT BOTTOM OF CABIN FLOOR MEMBRANE, STA 1163, LBL 5 INCHES. REMOVED CORROSION PER SPM 6-80-01. INSTALLED REPAIR PER SRM 53-01-18. PAINTED PER SRM 51-10-03. INSTALLED FASTENERS PER SRM 51-30-05.SDR TWAA0102402Seat Track · corrodedDURING CHECK-C MAINT FOUND CORROSION IN THE SEAT TRACK AT RBL 24, AT STA 247 AND FROM STA 206 TO 210. CUT OUT TRACK AT BOTH LOCATIONS AND INSTALLED NEW TRACK PER SRM 53-05, FIG F.SDR TWAA0017617Skin · dentedDURING CHECK-C MAINT, THE LT WING O L/E SLAT HAD DENT IN L/E APPROX CENTER OF SLAT. ACCOMP NDT AND NO CRACK FOUND PER PART 6-51-08-03 HFEC OF AREA IN SHOP PER TWA NDT SPM NUMBER 3 REPAIR PART NUMBER 6, NO CRACK. FOUND OK TO CLOSE LOWER SKIN. REPAIRED L/E PESDR TWAA0017509Galley Track · corrodedDURING CHECK-C MAINT FOUND CORROSION ON GALLEY TRACK AT STA 1136 TO 1178. REPLACED 42.75 INCH SECTION OF GALLEY TRACK PER SRM 53-05, PAGE 11, FIG 4H. INSTALLED TRACK PER SRM 51-30-1.SDR TWAA0017508Floorbeam · corrodedDURING CHECK-C MAINT FOUND CORROSION ON FLOORBEAM CAP AT STA 1250, LBL 24 IN TO LBL 48 INCHES. REPLACED FLOOR PANEL SUPPORT PER DRAWING 9930612.SDR TWAA0017507Floorbeam · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOORBEAM CAP AT STA 1155, LBL 24 TO LBL 47. REMOVED AND REPLACED FLOORBEAM CAP PER SPM 6-70-01, PAGE 2 AND 3. INSTALLED BEAM CAP USING HI-LOKS PER SRM 51-30-5, PAGE 12, AND PER TORQUE VALUES SRM 51-30-1, PAGE 11SDR TWAA0017506Web · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON MEMBRANE UNDER END OF SUPPORT AT STA 201, RBL 10 INCHES. REMOVED CORROSION PER SRM 6-80-01. TREATED CORROSION PER SRM 51-10-3. REPAIRED MEMBRANE PER SRM 53-01 PAGE 9.SDR TWAA0017505Skin · crackedDURING CHECK-C MAINT, THE FWD CARGO DOOR INTERNAL DOOR SKIN HAD A 2 INCH CRACK IN THE RADIUS OUTBOARD SIDE OF AFT BOTTOM LATCH AND .5 INCH CRACK BETWEEN ADJACENT FASTENER HOLE. CRACK CONTAINED PER EDDY CURRENT PART L 51-00-03. INSTALLED DOUBLER PER SRM 52-05SDR TWAA0017303Structure · dentedDURING CHECK-C MAINT, THE LT WING L/E NUMBER 3 SLAT INBOARD L/E HAD WIND EROSION ON DENT FILLER IN DENT APPROX 2 FEET FROM INBOARD END. ACCOMP NDT AND NO CRACK FOUND PER PART 6 OF 51-00-03. SANDED OUT OLD FILLER AND REPLACED WITH NEW PER SRM 57-03 PAGE 20A.SDR TWAA0008403Battery Pack · inoperativeDURING OVERNIGHT INSPECTION FOUND EGRESS FLOOR LIGHTING AND FORWARD ENTRY DOOR EMERGENCY EXIT SIGNS INOP. REPLACED EGRESS BATTERY PACK. AC04 04-30-00 DFW.SDR TWAA9913602Battery Pack · dischargedTHE EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 7, 8, 11 AND 33, AND THE AIRSTAIRS. REPLACED THE BATTERY PACK, PART NR 5822-2, IN THE CABIN AND REPAIRED WIRING IN THE AIRSTAIRS. CHECK-C 7-6-99 JFK.SDR TWAA9908703Battery Pack · dischargedTHE EGRESS LIGHTS AT ROWS 15 TO 21 CAME ON IN FLIGHT AND WOULD NOT RESET. REPLACED THE BATTERY PACK AT ROW 20. CHECK-C 10-10-98 STL.SDR TWAA9908705Battery Pack · dischargedTHE CABIN EGRESS LIGHTS AT ROW 15 TO 20 ILLUMINATED INTERMITTENTLY IN FLIGHT. REPLACED THE MID CABIN EGRESS LIGHT BATTERIES. CHECK-C 10-10-98 STL.SDR TWAA9820002Excitor · shortedTHE LT CSD TEMP WAS HIGH AND CREW DISCONNECTED THE CSD. ATTEMPTED TO START APU FOR GENERATOR BUT APU WOULD NOT START. CORRECTED THE APU BY REPLACING THE OIL PRESS SEQUENCE SWITCH, MFG 692525-9, THE IGNITION COIL, MFG 10-381175-9, AND THE IGNITOR PLUG MFG CH31SDR TWAA9816601Battery · dischargedEGRESS LIGHTS IN FLOOR AFT OF ROW 29 CAME ON IN FLIGHT AND REMAINED ON. REPLACED BATTERIES IN POWER SUPPLY. CHECK-C 10-1-98 STL.
Back to N959U, cancelled Aug 19, 2008