Douglas DC-9-83

Service difficulty reports · 16,530

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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 aircraft_model_key = 'DC983'
  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 ASAA0080009Handle · lack of lubeSEA - PRIOR TO DEPARTURE OF FLT 460, CREW REPORTED THE AFT CABIN ENTRY DOOR HANDLE WAS DIFFICULT TO OPERATE. LUBRICATED THE DOOR HANDLE MECHANISM AND OPERATED NORMALLY. (M)Jan 14, 2000 · N944AS · Doug DC983 · Passenger/Crew DoorsSDR ASAA0080010Wire · brokenSEA - DURING MAINTENANCE CHECK, ONE OVERHEAD EMERGENCY LIGHT IN THE CATWALKK AREA WAS FOUND INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M)Jan 14, 2000 · N963AS · Doug DC983 · Light System WiringSDR TWAA0001303Floorbeam · corrodedDURING CHECK-C MAINT IN THE MID CARGO BIN AT STA 522 TO 788, RT SIDE, NUT PLATE HOLES WERE CORRODED ON FLOOR TRACK. INSTALLED NEW FLOOR TRACK PER SRM 51-01, PAGE 1 PARA C, AND TWA SPM 6-70-01, PAGE 3 PARA B, FROM STA 427 TO 636, AND 693 TO 788.Jan 14, 2000 · N110HM · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0001302Skin · corrodedDURING CHECK-C MAINT,THE FUSELAGE RT SIDE WINDOW FRAME (50R) AT STA 1155 TO 1174 WAS DAMAGED AND CORRODED LOWER SIDE. BLENDED PER SRM 53-05, FIG 111 SHEET 2 NOTE 12 PAGE 502. ACCOMP NDT INSP USING HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS WEREJan 14, 2000 · N110HM · Doug DC983 · Fuselage Main, Plate/SkinSDR TWAA0001304Cargo Track · crackedDURING CHECK-C MAINT, IN THE AFT CARGO COMPT THE LT TIE DOWN TRACK HAD CORROSION AROUND SCREW HOLES ON THE FLANGE AND INSIDE THE TRACK FROM FWD BULKHEAD TO STA 1231. REPLACED TRACK PER SPM 6-70-01, PAGE 2 AND SRM 53-05 PAGE 10R. SIX INCH REPLACEMENT AT END OJan 14, 2000 · N110HM · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA0080008Battery · dischargedSEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS FOR THE TAILCONE EXIT EMERGENCY EVACUATION SLIDE ILLUMINATION WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M)Jan 13, 2000 · N976AS · Doug DC983 · Emergency LightingSDR TWAA0000901Cover · brokenTHE EGRESS LIGHTING STRIP AT ROWS 16 AND 17 WAS INOPERATIVE. RECONNECTED WIRE SOCKETS AND REPLACED THE BROKEN TRACK COVER. CHECK-C 10-24-99 JFK.Jan 13, 2000 · N9405T · Doug DC983 · Emergency LightingSDR GTIA000026Light · looseCLE - FLT 1402 - AISLE TRACK LIGHT LOOSE AT ROW 8. SECURED TRACK LIGHT SECTION ROW 7 THROUGH 10. OK FOR SERVICE. (M)Jan 13, 2000 · N802NK · Doug DC983 · Emergency LightingSDR AALA016005Battery Pack · dischargedCCI-LAX - CEILING EMERGENCY LIGHTS AT OVERWING EXITS INOPERATIVE. REPLACED B5-104 BATTERY PACK. OPS NORMAL. (M)Jan 11, 2000 · N836RA · Doug DC983 · Emergency LightingSDR ASAA0080007Power Supply · inoperativeSEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M)Jan 11, 2000 · N976AS · Doug DC983 · Emergency LightingSDR 20001114SH008Panel · leakingATL/MBJ - FLT JM 056 - AIRCRAFT HAD TO DIVERT TO MIAMI DUE TO AN IMBALANCE OF 400 KG IN FUEL. IT WAS CONFIRMED THE LEAK WAS FROM 3 ANCHOR NUTS. THESE NUTS WERE REPLACED AND SEALANT APPLIED. NO FURTHER INCIDENT OF THIS NATURE HAS RECURRED. (X)Jan 10, 2000 · N191AJ · Doug DC983 · Wing, Plate/SkinSDR ASAA0080006Wire · disconnectedONT - PRIOR TO DEPARTURE OF FLIGHT 447, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. RECONNECTED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M)Jan 10, 2000 · N975AS · Doug DC983 · Light System WiringSDR AALA006025Power Supply · inoperativeORD - TWENTY-FIVE MINUTES PRIOR TO LANDING FIRST ROW OF EMERGENCY LIGHTS ILLUMINATED IN CABIN NOW BURNED OUT, GALLEY TO ROW 15 A/C RT, ROW 5 WORKS. REPLACED FORWARD ENTRY DOOR POWER PACK EMERGENCY LIGHTS. OPS CHECKED NORMAL. (M)Jan 10, 2000 · N882RA · Doug DC983 · Emergency LightingSDR AALA20000055Light · brokenDFW - DURING OVERNIGHT MAINTENANCE SIDE WALL EMERGENCY EXIT LIGHT AT AFT STAIRWELL INOPERATIVE. REPLACED SIDE WALL EMERGENCY EXIT LIGHT AT AFT STAIRWELL. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Jan 10, 2000 · N563AA · Doug DC983 · Emergency LightingSDR TWAA0101013Stop · corrodedDURING CHECK-C MAINT AT THE AFT CABIN BULKHEAD, THE DOOR EXTRUSION STOP HAD HEAVY CORROSION, BOTTOM LT SIDE OF DOOR AS VIEWED LOOKING FROM AFT. REPLACED DOOR STOP PER SPM 6-70-01 WITH NEW PART.Jan 9, 2000 · N9420D · Doug DC983 · Fuselage Main, BulkheadSDR TWAA0101012Floor Support · corrodedDURING CHECK-C MAINT, THE FIRST CABIN FLOOR SUPPORT INSIDE THE LEFT SIDE NUMBER 1 CABIN DOORWAY HAD CORROSION FROM STA 157 TO 200. REMOVED AND REPLACED FLOOR SUPPORT ANGLE. FABRICATED NEW ANGLE. TREATED PER SRM 51-10-3. INSTALLED PER DRAWING 936535.Jan 9, 2000 · N9420D · Doug DC983 · Fuselage Miscellaneous StructureSDR 20001114SH007Cooler · lack of lubeMBJ/ATL - FLT JM 053 - AFTER TAKEOFF, AIRCRAFT RETURNED TO RAMP WITH NR 2 GENERATOR FAILED AND APU INOPERATIVE. INVESTIGATION REVEALED THE CSD OIL LEVEL WAS LOW. CSD SERVICED, ENGINE RUN AT IDLE FOR 5 MINTUES, NO LEAKS WERE OBSERVED. AIRCRAFT RETURNED TO SEJan 9, 2000 · N191AJ · Doug DC983 · Alternator-Generator DriveSDR TWAA0000913Support · crackedDURING OP 16 MAINT CHECK AT STA 936, RBL 6 IN, FWD SIDE FUSELAGE PANEL SUPPORT STRUCTURE HAD 1.5 IN HORIZONTAL CRACK. REPAIRED PER SRM 53-05, FIG 81 PAGE 267.Jan 9, 2000 · N110HM · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0000912Keel Beam · crackedDURING OP 16 MAINT CHECK AT STA 936, LBL 6 IN, THE AFT SIDE OF KEEL BEAM STRUCTURE HAD 2 EA 5 IN VERTICAL CRACKS, ONE AT RADIUS 1 1/8 AND SECOND AT RADIUS 1/2 IN, BOTH ON SAME MEMBER. REPLACED PER SRM 53-05, FIG 81 PAGE 267, DRAWING NUMBER REF 5936360.Jan 9, 2000 · N110HM · Doug DC983 · Fuselage Main, KeelSDR GTIA000016Light · inoperativeDTW - FLT 419 - AISLE LIGHTS NOT ALL WORKING. REMOVED AND REPLACED EMERGENCY AISLE TRACK LIGHT IAW MD-80 MM 33-50-00. ALL OPS NORMAL. (M)Jan 8, 2000 · N808NK · Doug DC983 · Emergency LightingSDR AALA006012Battery · dischargedSJC-CCI - FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES. OPS CHECK GOOD. (M)Jan 8, 2000 · N880RA · Doug DC983 · Emergency LightingSDR ASAA0080005Connector · looseSEA - PRIOR TO DEPARTURE OF FLIGHT 466, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. SECURED LOOSE CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M)Jan 7, 2000 · N944AS · Doug DC983 · Emergency LightingSDR ASAA0080004Battery Pack · dischargedSEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 24-27 WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER PACK AND ALL LIGHTS OPERATED NORMALLY. (M)Jan 7, 2000 · N963AS · Doug DC983 · Emergency LightingSDR 20000516AP002Battery Pack · dischargedPDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 27-30 AND AT ROWS 31-33 WERE FOUND INOPERATIVE. REPLACED BROKEN LAMP MODULE AT ROWS 27 AND BATTERIES IN AFT POWER PACK. ALL LIGHTS OPERATED NORMALLY. REF ASAA0080003, (M)Jan 7, 2000 · N943AS · Doug DC983 · Emergency LightingSDR ASAA0080003Module · brokenPDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 27-30 AND AT ROWS 31-33 WERE FOUND INOPERATIVE. REPLACED BROKEN LAMP MODUEL AT ROW 27 AND BATTERIES IN AFT POWER PACK. ALL LIGHTS OPERATED NORMALLY. (M)Jan 7, 2000 · N943AS · Doug DC983 · Emergency LightingSDR TWAA0000911Skin · scratchedDURING OP 16 MAINT CHECK, FOUND SCRATCH ON RT SIDE OF FUSELAGE, AT WINDOW FRAME STA 514, BOTTOM OF WINDOW. BLENDED PER SRM 53-05, FIG 111 SHEET 2, NOTE 12 PAGE 502. ACCOMP NDT PER 51-00-03 PART 1. INSTALLED OUTSIDE DOUBLER PER ARA 16486, NOTE PAGE 2 ITEM 15Jan 7, 2000 · N110HM · Doug DC983 · Fuselage Main, Plate/SkinSDR TWAA0000910Frame · crackedDURING OP 16 MAINT CHECK, THE LT MAIN LANDING GEAR DOOR, UPPER FWD CORNER INBD OF TIE IN CLIP INNER FRAME HAD .5 INCH CRACK. ACCOMP HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6 CRACK CONTAINMENT. REPAIRED FWD OTBD CORNER PER SRM 52-05, FIG 38 AND NOTES PAGE 3Jan 7, 2000 · N110HM · Doug DC983 · Landing Gear DoorsSDR TWAA0000909Floorbeam · corrodedDURING OP 16 MAINT CHECK IN THE FORWARD CARGO COMPARTMENT, FOUND CORROSION AROUND NUT PLATE HOLES ON FLOOR SUPPORT BETWEEN FLOOR TRACKS STA 437. REPLACED CORRODED FLOOR SUPPORT WITH NEW FLOOR SUPPORT PER SPM 6-70-01.Jan 7, 2000 · N110HM · Doug DC983 · Fuselage Main, Floor BeamSDR GTIA000012Lens · missingDTW - FLT 378A - LENS COVER FOR PATH LIGHTING LAST ROW, STARBOARD SIDE IS OFF LIGHT. HARDWARE IN FORWARD GALLEY. RELAMPED PATH LIGHTING AND REINSTALLED LIGHT COVER AND TRACKING IAW MD-80 MM 33-53-01. OPS CHECKS GOOD, NO DEFECTS NOTED. (M)Jan 6, 2000 · N808NK · Doug DC983 · Emergency LightingSDR TWAA0000916Fitting · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 200, RBL 18, AT FLOOR FITTING. CORROSION WAS BEYOND LIMITS. NEW PANEL ASSEMBLED. RIVETS NAS 1097AD4-4 PER SRM 51-30-2. SEALED PRC 1422 PER SRM 51-200-P10.Jan 6, 2000 · N110HM · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0000908Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION AROUND NUT PLATE HOLES ON FLOOR SUPPORT, STA 200 RBL 5 IN TO LBL 5 IN. REMOVED CORROSION PER SPM 6-80-01, PAGE 1. FABRICATED FLOOR SUPPORT PER SPM 6-70-01, PAGE 2 AND 3, PARAGRAPH 4.Jan 6, 2000 · N110HM · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0000907Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOORBEAM PANEL WEB FROM STA 160 TO 200, AND BETWEEN 6 IN LBL TO 6 IN RBL. COMPLETED REPAIR ON PANEL WEB FROM STA 160 TO 200, RBL 6 IN TO LBL 6 IN, DONE PER SSRM 53-10-111 AND DOUGLAS SERVICE BULLETIN 53 246 FIG 3 Jan 6, 2000 · N110HM · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0000906Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CABIN CORROSION IN THE CHAIR TRACK AT LBL 22 INCHES, STA 1117 TO 1309. INSTALLED NEW SEAT TRACK PER MM 53-40-01, PAGE 201. SPLICED PER SRM 53-05, PAGE 106 FIG 4F.Jan 6, 2000 · N110HM · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR GTIA000017Cover · missingDTW - EMERGENCY LIGHT COVER IN FORWARD GALLEY MISSING. INSTALLED EMERGENCY LIGHT COVER IN FORWARD GALLEY IAW MD80 MM 33-50-00. OPS CHECK GOOD. (M)Jan 6, 2000 · N802NK · Doug DC983 · Emergency LightingSDR AALA20010127Seat Track · corrodedTUL - FOUND NR 1 SEAT TRACK CORRODED AND GOUGED STATION 671-673. INSTALLED PLUG REPAIR PER SRM 53-05 PART 1 FIG 4A. (M)Jan 5, 2000 · N570AA · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0000905Floor Web · corrodedDURING OP 16 MAINT CHECK, THE CABIN AFT SERVICE DOOR TOP OF FLOOR WEB WAS CORRODED AROUND AFT DOOR JAM AREA, TOP OF WEB AND UNDER WEB STA 1174. REPAIRED PER SRM 53-01, FIG 2, SRM 51-60-00 PAGE 27, AND SRM 51-30-02.Jan 5, 2000 · N110HM · Doug DC983 · Fuselage Floor PanelSDR TWAA0000904Floor Web · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT FLOOR MEMBRANE CRACKED AT STA 159, RBL 8 TO 10 IN. ACCOMP EDDY CURRENT PER NDT MANUAL 51-00-03, PART 6. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 2, PAGE 9.Jan 5, 2000 · N110HM · Doug DC983 · Fuselage Floor PanelSDR TWAA0000303Battery Pack · dischargedTHE MIDDLE CABIN EMERGENCY LIGHTS WOULD NOT SHUT OFF. REPLACED THE BATTERY PACK. CHECK-C 11-20-99 STL.Jan 5, 2000 · N9401W · Doug DC983 · Emergency LightingSDR TWAA0101019Longeron · crackedDURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT STA 1209. REPAIRED CRACKED LONGERON 2R AT STA 1209 PER SRM 53-02, FIG 18.Jan 4, 2000 · N9303K · Doug DC983 · Fuselage Main, Longeron/StringerSDR TWAA0000805Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION IN CABIN ON NUMBER 2 TRACK FLANGE AT LBL 44, OTBD SIDE NUT PLATE HOLES, STA 1150 TO 1155. REPLACED SEAT TRACK AND MADE SPLICE PER SRM 51-01, PAGE 1 PARA L AND SRM 53-05, FIG 4F SHEET 5. INSTALLED FASTENERS PER SRM 51Jan 4, 2000 · N110HM · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR AALA006011Battery · discharged1 TAIL CONE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERIES IN CHARGER AS REQ. (M)Jan 4, 2000 · N882RA · Doug DC983 · Emergency LightingSDR AALA006010Power Supply · inoperativeEMERGENCY LIGHTS IN 1ST CLASS 1-4 INOPERATIVE, COACH 6-10 INOPERATIVE. REMOVED AND REPLACED L-1 POWER SUPPLY AND BATTERIES. SYSTEM OPS CHECKS NORMAL. (M)Jan 4, 2000 · N882RA · Doug DC983 · Emergency LightingSDR AALA006001Pin · missingON CLIMB-OUT, RIGHT THROTTLE STOPPED GOVERNING. POWER REMAINED AT TAKEOFF POWER AND WOULD NOT FOLLOW THROTTLE POSITION. FLEW APPROXIMATELY 25 MINUTES SINGLE ENGINE TIME. NO ENGINE LIMITATIONS WERE EXCEEDED. LANDING WAS MADE AT 137,000 POUNDS. FOUND BOLT Jan 2, 2000 · N834RA · Doug DC983 · Fuel Control/Turbine EnginesSDR AALA006003Wire · damagedEMERGENCY LIGHT ON AISEL SEAT 22 DOES NOT ILLUMINATE. REPAIRED DAMAGED WIRES UNDER SEAT 22DEF IAW MM, LIGHT OPS NORMAL. (M)Jan 1, 2000 · N872RA · Doug DC983 · Light System WiringSDR TWAA0000811Skin · tornRT WING LE SKIN WAS TORN AND DENTED DUE TO GROUND DAMAGE BETWEEN 2 OTBD TRACKS FOR NUMBER 3 SLAT, RT WING, 37 IN LONG. REPLACED LE CAP PER DOUGLAS BLUE PRINT 5937513 SHEET 1.Dec 31, 1999 · N9626F · Doug DC983 · Wing, Plate/SkinSDR TWAA0000810Skin · scratchedRT WING LE CAP WAS SCUFFED ON LOWER SURFACE, 6 IN BY 4 INCHES OFF OF NUMBER 4 SLAT. REMOVED AND REINSTALLED SERVICEABLE NUMBER 4 LE CAP PER DOUGLAS BLUE PRINT 5937523, SHEET 1. CHECK-C 10-2-99 STL.Dec 31, 1999 · N9626F · Doug DC983 · Wing, Plate/SkinSDR TWAA0000103Lamp · looseTHE EGRESS LIGHTING WAS INOPERATIVE AROUND CABIN ROW 20. SECURED A LOOSE LAMP IN THE CONNECTOR. NO CHECK-C.Dec 31, 1999 · N982TW · Doug DC983 · Emergency LightingSDR GTIA0000004Light · disconnectedEWR - FLT 447 - EMERGENCY TRACK FLOOR LIGHTING IS OUT IN BACK. RECONNECTED EMERGENCY TRACK RED LIGHT. OPS CHECK OK. (X)Dec 31, 1999 · N808NK · Doug DC983 · Emergency LightingSDR TWAA0000804Bulkhead · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON AFT PRESSURE BULKHEAD AT BOTTOM CENTER END TIE AND BULKHEAD. REMOVED CORROSION IN ACCORDANCE WITH SRM 51-10-3, PAGE 21-22 AND SPM 6-80-01, PAGE 1 AND 2.Dec 30, 1999 · N110HM · Doug DC983 · Fuselage Main, BulkheadSDR TWAA0000803Flange · crackedDURING OP 16 MAINT CHECK, FOUND CRACK IN THE FORWARD CARGO DOOR FLANGE ON FWD SIDE NEXT TO DOOR HOLD OPEN LATCH. STOP DRILLED CRACK AND INSTALLED CARGO DOOR PAN CRACK REPAIR PER SRM 52-05, PAGE 110A TO 110C, VIEW C-C.Dec 30, 1999 · N11OHM · Doug DC983 · Cargo/Baggage Doors
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