N950U, cancelled Sep 4, 2009

Service difficulty reports · 40

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 = 'N950U' AND deregistration_id = 'N950U-2009-09-04'
  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 AALA20060143Engine · shutdownDEN - RIGHT ENGINE FAILED AFTER TAKEOFF AT ABOUT 300 FEET ABOVE GROUND LEVEL. RIGHT HAND ENGINE EXHAUST GAS TEMPERATURE AT ROTATION WAS ABOUT 570 DEGREES. ENGINE FIRE/DAMAGE/SEPARATION CHECKLIST FOLLOWED, HAD N1 AND N2 BUT NO RESTART. LANDED DEN WITHOUT INCIMar 4, 2006 · N950U · Doug DC982 · Engine (Turbine/Turboprop)SDR ZW0A0400301Battery Pack · inoperativeAFTER BOARDING THE FLIGHT CREW ARMED THE EMERGENCY LIGHTS AND THE AISLE EGRESS LIGHTS BETWEEN ROW 22 AND 28 WERE BLINKING. REPLACED THE BATTERY PACK. CHECK-C STL 12-18-03.Feb 13, 2004 · N950U · Doug DC982 · Emergency LightingSDR ZW0A0302301Seat Track · corrodedDURING CHECK-C MAINT FOUND CORROSION ON CABIN SEAT TRACK AT STA 1150 TO 1164, LBL 22. REMOVED CORRODED SECTION AND SPLICED IN NEW SECTION PER SRM 53-05, FIG 4F, FROM STA 1150 TO 1230.Feb 18, 2003 · N950U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR ZW0A0302103Beam · crackedDURING CHECK-C, THE FWD SERVICE DOOR LOWER BEAM WAS CRACKED AT FWD END IN RADIUS. ALSO A SMALL CLIP WAS CRACKED INSIDE LIGHTENING HOLE AT UPPER AFT CORNER. REPLACED CLIP AND REPLACED LOWER BEAM PER SPM 6-70-01.Feb 11, 2003 · N950U · Doug DC982 · Fuselage Main, StructureSDR ZW0A021196Oil System · leakingOIL LEAKING IN APU CAUSING SMOKE TO ENTER CABIN. REMOVED AND REPLACED LEFT AUTO TEMP CONTROL ANTICIPATOR. LAST CHECK C PERFORMED IN STL 10/29/02 --CLOSED--Nov 26, 2002 · N950U · Doug DC982 · APU Oil SystemSDR ZW0A0211402AccumulatorCREW REPORTED SMELL OF KEROSENE IN COCKPIT AND CABIN. REPLACED THE RH THRUST REVERSER ACCUMULATOR ACCOUNT LEAKING HYDRAULIC FLUID. CHECK-C 10-29-02 STL. --CLOSED--Nov 16, 2002 · N950U · Doug DC982 · Hydraulic Power Accumulator, MainSDR ZW0A0210803Battery · dischargedTHE EMERGENCY LIGHTS IN THE CEILING AT ROWS 23 TO 26, AND THE AFT OVER WING EXIT SIGN WAS INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK FOR THE CEILING LIGHTS AND REPLACED THE BATTERIES FOR THE OVERWING EXIT.Oct 27, 2002 · N950U · Doug DC982 · Emergency LightingSDR ZW0A0203501Sign · inoperativeAFT STAIR EGRESS EXIT SIGN INOP. REPLACED EGRESS EXIT SIGN.Mar 22, 2002 · N950U · Doug DC982 · Emergency LightingSDR ZW0A0202501Battery PackTHE CABIN EGRESS LIGHTS WERE FLICKERING. REPLACED THE NUMBER 3 EGRESS BATTERY PACK. CHECK-C 10-24-2001 STL. --CLOSED---Mar 3, 2002 · N950U · Doug DC982 · Emergency LightingSDR TWAA0101701Battery · dischargedTHE LT AND RT REAR OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. CHECK-C 11-11-00 STL.Jan 28, 2001 · N950U · Doug DC982 · Emergency LightingSDR TWAA0008409Light · explodedDURING TAXI, PASSENGER SERVICES LIGHT EXPLODED AT SEAT 33F. REMOVED THE LIGHT FROM THE SOCKET. *S/D* DETERMINED THAT LAMP SHATTERED RATHER THAN EXPLODING. ASSUME LAMP WAS FAULTY AND HAD AN AIR INTRUSION WHICH CAUSED IT TO OVERHEAT AND SHATTER.May 29, 2000 · N950U · Doug DC982 · Passenger Compartment LightingSDR TWAA0000201Web · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR MEMBRANE BELOW THE AFT SERVICE DOOR, AFT GIRT BAR FLOOR FITTING, STA 1170. REMOVED CORROSION PER SPM 6-80-01, PAGE 123. REPAIRED MEMBRANE PER SRM 53-01, PAGE 918.Oct 24, 1999 · N950U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0000207Seat Track · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON FLOOR TRACK, UNDERSIDE, AT STA 1260 TO 1271, LBL 24. INSTALLED NEW TRACK FROM STA 1220 TO 1322, PER SRM 53-05 FIG 4G.Oct 23, 1999 · N950U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0000206Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN CHAIR TRACK AT LBL 50, STA 1155 TO 1390. REPLACED BAD TRACK PER SRM 53-05, FIG 4F.Oct 22, 1999 · N950U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0000208Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN CHAIR TRACK AT LBL 28, STA 1231 TO 1304. REPLACED TRACK PER SPM 6-70-00.Oct 21, 1999 · N950U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0000202Sill · corrodedDURING OP 16 MAINT CHECK, FOUND IN FORWARD CARGO COMPT, BOTTOM DOOR SILL AREA HAD CORROSION AND WAS DIRTY. REPAIRED LOWER DOOR SILL PER SRM 53-05 FIG 44.Oct 20, 1999 · N950U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0000205Web · crackedDURING OP 16 MAINT CHECK, FOUND CRACK AT INTERIOR OF AFT CARGO DOOR AT AFT LOWER DOOR STOP CASTING AND INTERCOSTAL. REPLACED CRACKED WEB AND STIFFENER PER SPM 6-70-07, PAGE 2 AREA 4B.Oct 18, 1999 · N950U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0000209Frame · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON STA 1309 FORMER, FROM LONGERON 20L TO 28L. REPLACED FORMER FROM L18L TO L28L, PER SRM 53-03, FIG 2A.Oct 17, 1999 · N950U · Doug DC982 · Fuselage Main, FrameSDR TWAA0000210Casting · crackedDURING OP 16 MAINT CHECK, FOUND MID CARGO DOOR UPPER FORWARD INTERIOR DOOR STOP CASTING CRACKED, APPROX 3 IN BELOW TOP OF DOOR, AFT OF FWD EDGE. INSTALLED NEW CASTING PER SPM 6-70-01, PAGE 3.Oct 13, 1999 · N950U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0000306Floorbeam · corrodedDURING OP 16 MAINT CHECK FOUND CABIN FLOOR PANEL SUPPORT, STA 180, WITH CORROSION, RBL 10 TO 43. REPLACED FLOOR PANEL SUPPORT PER SPM 6-70-01.Oct 7, 1999 · N950U · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0000305Rib · crackedDURING OP 16 MAINT CHECK, FOUND VERTICAL STABILIZER DORSAL FIN WITH RIBS CRACKED AT LOWER END, NUMBER 1 AND 5 ON LT SIDE AND 4, 7, AND 8 ON RT SIDE. REPAIRED RIBS 1, 5, 4, 7 PER SRM 55-02 FIG 19. REPLACED NUMBER 8 PER SPM 6-70-01.Oct 7, 1999 · N950U · Doug DC982 · Vertical StabilizerSDR TWAA0000203Window Frame · crackedDURING OP 16 MAINT CHECK, FOUND CABIN WINDOW FRAME CRACKED AT STA 946, LONGERON 12R, UPPER FORWARD CORNER. REMOVED MATERIAL AND INSTALLED DOUBLER REPAIR PER SRM 53-10-114.Oct 7, 1999 · N950U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0000307Skin · gougedDURING OP 16 MAINT CHECK, FOUND GOUGE IN FWD ENTRY DOOR OUTER SKIN AT GUST LOCK CUTOUT, .5 IN BY .25 IN. BLENDED DAMAGED AREA AND INSTALLED REPAIR DOUBLER TO OUTER SKIN PER SRM 52-05, FIG 20.Oct 6, 1999 · N950U · Doug DC982 · Fuselage Main, Plate/SkinSDR TWAA0000310Support · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT AT STA 200, LBL 14, RBL 53 WAS CORRODED. REPLACED SUPPORT MEMBER PER SPM 6-70-01.Oct 5, 1999 · N950U · Doug DC982 · Fuselage Miscellaneous StructureSDR TWAA0000309Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN FLOOR SUPPORT CORRODED AT RBL 6, STA 160 TO 200. INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01.Oct 5, 1999 · N950U · Doug DC982 · Fuselage Main, Floor BeamSDR TWAA0000204Skin · delaminatedDURING OP 16 MAINT CHECK, FOUND LT ELEVATOR CONTOL TAB WITH DELAMINATION AT THE INBD AREA. CONTROL TAB SENT TO SHOP FOR OVERHAUL. DELAMINATION REPAIRED PER SRM 55-04, PAGE 5 TO 7.Oct 5, 1999 · N950U · Doug DC982 · Elevator, Tab StructureSDR TWAA0000311Frame · cutDURING OP 16 MAINT CHECK, FOUND 2 DEEP CUTS IN FORMER, INNER FLANGE AT STA 522, ABOVE LONGERON 6L. REPAIRED DAMAGED AREA PER SRM 53-03, PAGE 5.Oct 4, 1999 · N950U · Doug DC982 · Fuselage Main, FrameSDR TWAA0000308Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR PANEL SUPPORT (CHAIR TRACK) AT STA 1212 TO 1287, LBL 54. REPLACED SUPPORT TRACK PER SPM 6-70-01.Oct 4, 1999 · N950U · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9900801Blade · failedABORTED TAKEOFF WHEN ANOTHER FLIGHT REPORTED SPARKS COMING FROM THE NR 1 ENGINE. METAL WAS FOUND IN THE ENGINE TAIL PIPE. REPLACED ENGINE. CHECK-C 8-24-98 MCI. *S/D* FOUND AN EIGHTH STAGE COMPRESSOR BLADE FRACTURED DUE TO FATIGUE. THERE WAS SEVERE DOWNSTJan 11, 1999 · N950U · Doug DC982 · Turbine Engine Compressor SectionSDR TWAA9751002Retract Mech · malfunctionedFLT 619 - STL - DURING CLIMB, NOSE LANDING GEAR WOULD NOT RETRACT. ADJUSTED NOSE GEAR OVERRIDE CABLE, CYCLED NOSE GEAR, OPERATIONAL CHECK NORMAL. (M)Apr 20, 1997 · N950U · Doug DC982 · Landing Gear Retraction/Extension SystemSDR 96ZZZM1365Support · corrodedMCI - DURING OP-15, FOUND FLOOR SUPPORT CORROSION, LONGERON 28R, STATION 1211. REPLACED SUPPORT PER SRM 51-30-0.Aug 8, 1996 · N950U · Doug DC982 · Fuselage Miscellaneous StructureSDR 96ZZZM1343Stringer · corrodedMCI - DURING OP-15, FOUND CORROSION ON FORMER, ABOVE STRINGER 30, BS 207, AFT OF DOOR. REMOVED CORROSION PER SRM 51-10-3 AND REINSTALLED FASTENERS PER SRM 51-30-0. (M)Aug 8, 1996 · N950U · Doug DC982 · Fuselage Main, Longeron/StringerSDR 96ZZZM1071Sensor · dirtySTL - ON TAKEOFF AFTER LANDING GEAR RETRACTION, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FOUND TARGET AND SENSOR DIRTY. CLEANED TARGET AND SENSOR, MFG P/N 8-337-03, AND NOSE LANDING GEAR INDICATION CHECKED NORMAL. (M)Jun 4, 1996 · N950U · Doug DC982 · Landing Gear Position and WarningSDR 96ZZZM797Air Distribution · smokeDURNG DESCENT, SMOKE FROM AN UNDETERMINED SOURCE APPEARED IN THE COCKPIT AND CABIN. PERFORMED MD9-21-02 AIR CONDITIONING DUCT OIL CONTAMINATION CHECK, AND MD9-49-04 APU AND ECS PERFORMANCE CHECK, ALL CHECKS NORMAL.Apr 1, 1996 · N950U · Doug DC982 · Air Distribution SystemSDR 96ZZZX1228Strut Seal · failedSTL - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT. IT WAS DETERMINED THE NOSE GEAR WAS DOWN ALND LOCKED. REMOVED AND REPLACED NOSE GEAR SEAL KIT, MFG PN A03772REVH. GEAR SWING CHECKED NORMAL. CHECK C-1D - 4-13-95 - MCI.Jan 28, 1996 · N950U · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR 96ZZZM241Seal · failedSTL - AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT, IT WAS DETERMINED THAT THE NOSE GEAR WAS DOWN AND LOCKED. REMOVED AND REPLACED NOSE GEAR SEAL KIT, MFG P/N A03772REVH. GEAR SWING CHECKED NORMAL.Jan 28, 1996 · N950U · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR 96ZZZM196Schrader Valve · crackedTPA - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR WOULD NOT RETRACT. FOUND NOSE LANDING GEAR INFLATION LOW DUE TO CRACKED SCHRADER VALVE. REPLACED SCHRADER VALVE, MFG P/N A00314, AND SERVICED NOSE LANDING GEAR, OPERATION THEN CHECKED NORJan 21, 1996 · N950U · Doug DC982 · Nose/Tail Landing Gear Strut/AxleSDR 95ZZZW751Oven · failedSTL - DURING CRUISE E GALLEY OVEN, MFG P/N 50381, BEGAN SMOKING WHEN TURNED ON. TURNED OFF OVEN. REPLACED OVEN AND OPERATION CHECKED NORMAL.May 19, 1995 · N950U · Doug DC982 · Buffet/GalleysSDR 95ZZZX894Air Distribution · odorOMA - FLT 142 - DURING CRUISE, HAD ODOR AND SMOKE IN COCKPIT. ELECTRICAL SYTEMS AND AIR CONDITIONING SYSTEM APPEARED NORMAL. CHECKED ELECTRICAL PANELS IN COCKPIT AND ELECTRICAL EQUIPMENT COMPARTMENT AND NO ABNORMALITIES FOUND. CHECK C-2D - 1-13-94 - MCI.Feb 10, 1995 · N950U · Doug DC982 · Air Distribution SystemSDR 95ZZZW155Air Distr · odorOMA - FLT 142 - DURING CRUISE HAD ODOR AND SMOKE IN COCKPIT. ELECTRICAL SYSTEMS AND AIR CONDITIONING SYSTEM APPEARED NORMAL. CHECKED ELECTRICAL PANELS IN COCKPIT AND ELECTRICAL EQUIPMENT COMPARTMENT AND NO ABNORMALITIES FOUND. CHECK C-2D - 1-13-93 - MCI.Feb 10, 1995 · N950U · Doug DC982 · Air Distribution System
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