Douglas DC-9-32

Service difficulty reports · 12,755

Newest first. General aviation reporting is voluntary.

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 = 'DC932'
  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 MWEA020056Frame · chafedCANTED FRAME AT STATION 1168 HAS A CHAFED AREA ON LOWER AFT SIDE AT 7 O'CLOCK POSITION. -- FABRICATED AND INSTALLED REPAIR DOUBLERS.Jan 23, 2002 · N203ME · Doug DC932 · Fuselage Main, StructureSDR AT0200019Stud · crackedRIGHT WING FLAP HINGE LOWER OUTBOUND ATTACHMENT STUD AT X IN=33.148 SHOWS A CRACK INDICATION.Jan 22, 2002 · N831AT · Doug DC932 · Trailing Edge FlapsSDR AT0200022Seat Track · corrodedMAIN CABIN FLOOR SEAT TRACK RBL 22 HAS SPOTS OF LIGHT CORROSION BS 470, BS 484, BS 515, BS 525, BS 545, BS 579, AND BS 605.Jan 22, 2002 · N831AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT0200021Seat Track · corrodedMAIN CABIN FLOOR SEAT TRACK HAS LIGHT CORROSION BETWEEN BS 237 AND BS 250 AT RBL 22 AND RBL 44, RBL 44 + 22 FROM STA 200 TO STA 410 AND REMOVED CABIN SEAT TRACK RBL 44 FROM STA 237 TO 331.Jan 22, 2002 · N831AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT0200001Socket · missingFOUND ROW 25 EMERGENCY PATH LIGHT ASSEMBLY MISSING. CORRECTIVE ACTION: REPLACED SOCKET. IAW DC9 MM33-53Jan 19, 2002 · N828AT · Doug DC932 · Emergency LightingSDR GTIA012218Web · crackedFTW - NR 1 ENGINE PYLON LOWER SURFACE AFT HINGE PANEL OUTBOARD LOWER WEB CRACKED AT ANGLE. REMOVED WEB. FABRICATED NEW WEB. INSTALLED WEB. REMOVED DAMAGED SECTION OF ANGLE. FABRICATED REPAIR ANGLE AND DOUBLERS. INSTALLED REPAIR ANGLE AND DOUBLERS IAW DC9Jan 17, 2002 · N12536 · Doug DC932 · Nacelle/Pylon, Main FrameSDR 0200119603Door Frame · crackedDURING HCK IN ATL, THE VENTRAL DOOR JAMB AND CAP WERE FOUND CRACKED. REPAIRED PER EA 96-185463.Jan 17, 2002 · N603NW · Doug DC932 · Fuselage Main, StructureSDR 0200109603Rib · crackedDuring HCK in ATL the lower cap of the pylon closong rib YN165 was found cracked. Repaired per EA 96-185454.Jan 14, 2002 · N603NW · Doug DC932 · Nacelle/Pylon, Main FrameSDR GTIA020012Battery Pack · dischargedDTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM. OPS CHECK GOOD PER MM 33-53-01. (M)Jan 13, 2002 · N12536 · Doug DC932 · Emergency LightingSDR GTIA020009Battery Pack · dischargedDTW - FOUND OVERWING EXIT LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK SYSTEM, OPS CHECK GOOD PER DC9 MM 33-53-01. (M)Jan 13, 2002 · N12536 · Doug DC932 · Emergency LightingSDR 0200099603Panel · crackedDuring HCK in ATL a crack was found in the aft flange of the right trapezoidal panel. Repair accomplished in accordance with EA 96-185424.Jan 8, 2002 · N603NW · Doug DC932 · Wing Main, Frame StructureSDR ABXA010680Longeron · crackedLONGERON 13 RIGHT WAS CRACKED BETWEEN FS 1076 AND FS 1087. REPLACED LONGERON IAW DC-9 SRM 54-30-2.Jan 8, 2002 · N985AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020031Bracket · crackedAFT CARGO DOOR BEAM #3 END FITTING CRACKED, AFT SIDE OF DOOR. -- REMOVED FITTING AND ANGLE SUPPORT BRACKET. LOCATED AND DEBURRED NEW FITTING AND ANGLE SUPPORT BRACKET.INSTALLED END FITTING AND ANGLE SUPPORT BRACKET.Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020030Pan · crackedAFT CARGO DOOR INNER PAN IS CRACKED UNDER NUMBER 2 AFT. WORKING CORROSION NRI 12570. -- FABRICATED REPAIR ANGLE AND INSTALLED REPAIR ANGLE AND FITTING.Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020029Fitting · crackedAFT CARGO DOOR BEAM NR 4 END FITTING CRACKED, AFT SIDE OF DOOR. REMOVED AND REPLACED NEW FITTING.Jan 7, 2002 · N212ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020028Doubler · crackedRIGHT AFT PYLON WEB DOUBLER P/N 9912246 AT STATION 1038 HAS CRACKS EMINATING FROM THE UPPER STRAP ATTACHMENT HOLES. -- FABRICATED AND INSTALLED DOUBLER.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020027WebTHE AFT PYLON BULKHEAD HAS OVERSIZED HOLE WHERE THE UPPER PYLON STRAP ATTACHES TO IT. -- FABRICATED AND INSTALLED WEB AND DOUBLERS.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020026Web · oversizedRIGHT AFT PYLON SPAR WEB (P/N 9958154-21) UPPER HOLES ARE OVERSIZED. -- FABRICATED AND INSTALLED WEB.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020025Spar · damagedREMOVE PYLON SPAR WEB (P/N 9958154-29). THE WEB HAS OVERSIZED HOLES. REMOVED DOUBLER. FABRICATED NEW DOUBLER. INSTALLED WEB.Jan 7, 2002 · N212ME · Doug DC932 · Nacelle/Pylon, Frame/Spar/RibSDR MWEA020024Channel · corrodedCORROSION AROUND AND ON NUT PLATES LOCATED AT STATION 351 ON U-CHANNEL THAT'S RIVETED TO FLOORBEAM APPROXIMATELY 28 INCHES AND 33 INCHES TO THE LEFT OF CENTER. REMOVED CHANNEL, LOCATED HOLES, INSTALLED NUT PLATES ON CHANNEL, AND INSTALLED CHANNEL.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020023Channel · corrodedCORROSION AROUND AND ON NUT PLATES LOCATED ON U-CHANNEL THAT'S ATTACHED TO FLOORBEAM 427 ABOVE FORWARD AT CARGO DOOR OPENING. FABRICATED AND INSTALLED U-CHANNEL.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020022Frame · damagedSTATION 1038 RIGHT FRAME CAP (P/N 9912246-103) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON ATTACHES. REPAIRED PER TELEX MWX-ORD-01-00570H 19 DEC 2001.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020021Frame · damagedSTATION 1038 RIGHT FRAME CAP (P/N 9912246-105) HAS TWO OVERSIZED HOLES WHERE THE AFT UPPER ENGINE PYLON STRAP ATTACHES. FABRICATED AND INSTALLED DOUBLER.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020020Frame · crackedKEEL AREA FRAME AT STATION 637 IS CRACKED AT OUTBOARD END ON LEFT SIDE. FABRICATED AND INSTALLED REPAIR ANGLE.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020019Web · corrodedWEB AT GALLEY SERVICE DOOR, FROM STATION 150 TO STATION 200, IS CORRODED AT FORWARD SIDE OF SERVICE DOOR OPENING AND AFT SIDE OF SERVICE DOOR OPENING. FABRICATED AND INSTALLED WEB.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020018Longeron · chafedLONGERON 22 RIGHT HAS CHAFE DAMAGE ON UPPER LEG (VIEW THROUGH RIGHT THRUST REVERSER BY PASS DOOR). FABRICATED AND INSTALLED LONGERON SECTION, LONGERON SPLICE AND NEW STRAPS. REMOVED CORROSION FROM SHOVEL CLIP AND REINSTALLED.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020017Frame · crackedFUSELAGE FORMER CRACKED BELOW LONGERON 15 RIGHT VIEW FROM FORWARD SIDE OF FUSELAGE FRAME 1038. REMOVED AND REPLACED FORMER.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020014Floor Support · corrodedFLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN NR 3 SEAT TRACK AND NR 4 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020013Floor Support · corrodedFLOORBOARD SUPPORT AT STATION 200 HAS CORROSION BEYOND LIMITS LOCATED BETWEEN CENTER FLOOR SUPPORT AND NR 3 SEAT TRACK. REMOVED AND REPLACED FLOOR SUPPORT.Jan 7, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA010662Battery Pack · dischargedEMERGENCY LIGHTS INTERMITTENTLY INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC-9 MM 33-53-02-4.Jan 6, 2002 · N902AX · Doug DC932 · Emergency LightingSDR MWEA020012Floor Support · corrodedFLOORBOARD SUPPORT LOCATED JUST FORWARD OF NUMBER 4 SEAT TRACK FROM STATION 160 TO 200 HAS TWO AREAS OF CORROSION ON TOP SIDE AND SEVERAL AREAS OF CORROSION ON LOWER SURFACE OF FLANGE AROUND THE HOLES. REMOVED, LOCATED, DRILLED AND INSTALLED FLOORBOARD SUPPORJan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020010Frame · chafedFUSELAGE FRAME 1059 HAS CHAFE DAMAGE ON UPPER LEG AT LONGERON 21 RIGHT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED, FIT, DRILLED AND INSTALLED REPAIR.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020009Web · damagedSUBFLOOR HAS SEVERAL AREAS OF BARE METAL AND RIVET HEAD WEAR MARKS FROM STATION 200 TO 218 BETWEEN NUMBER 2 SEAT TRACK AND CENTER FLOOR SUPPORT. FABRICATED AND INSTALLED REPAIR DOUBLER.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020008Seat Track · corrodedNUMBER 3 SET TRACK HAS HEAVY CORROSION FROM STATION 218 TO 248. CUT AND REMOVED SEAT TRACK. LOCATED, DRILLED AND INSTALLED SEAT TRACK.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA020007Floor Support · corrodedCENTER FLOOR SUPPORT HAS LIGHT CORROSION AROUND SEVERAL FASTENER HOLES FROM STATION 192 TO 200. REMOVED CENTER FLOOR SUPPORT. DRILLED, TRIMMED AND INSTALLED NEW CENTER FLOOR SUPPORT.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020006Skin · crackedSTATION 1010, RIGHT HAND SIDE FUSELAGE SKIN HAS A SMALL CRACK ORIGINATING FROM RIVET BETWEEN LONGERON 14 RIGHT AND 16 RIGHT. CUT OUT CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER.Jan 4, 2002 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020002Panel · delaminatedRIGHT WING OUTBOARD TRAILING EDGE PANEL HAS APPROXIMATELY 80 SQUARE INCHES OF DELAMINATION ON THE TOP AREA, INCLUDES MOST OF THE TRAILING EDGE. REMOVED, LOCATED, DRILLED AND INSTALLED NEW TRAILING EDGE PANEL.Jan 4, 2002 · N212ME · Doug DC932 · Wing, Plate/SkinSDR GTIA012321Oxygen Mask · malfunctionedFTW - FOUND OXYGEN MASK DID NOT DROP IN AUTO. PERFORMED TROUBLE SHOOTING AND FOUND OXYGEN LEAK ON OXYGEN LINES. INSTALLED PROPERLY OXYGEN LINES. OPS CHECK GOOD IAW DC9 MM 35-20-0. (M)Jan 3, 2002 · N12536 · Doug DC932 · Passenger Oxygen SystemSDR CA020121004Rod · failed(CAN) ON TAKEOFF FROM THUNDERBAY TO TORONTO, THE PLANE FELT HEAVY AND THE PROBLEM WAS SUGGESTED TO A FAULTY STAB AUGMENTATION COMPUTER, THAT WAS REPLACED THE NEXT MORNING. WITH ALL SYSTEMS OK, THE NEXT LEG OVER BACK TO THUNDERBAY THE PLANE REPORTED TO HAVE Dec 27, 2001 · Doug DC932 · Elevator Tab Control SystemSDR 0105209613Spar Cap · corrodedDuring Mck in DHN the right wing rear spar upper cap was found corroded at the inboard hole. Repaired per EA 96-187657.Dec 27, 2001 · N613NW · Doug DC932 · Wing Main, Frame StructureSDR 0105129618Hydraulic Line · rupturedDURING APPROACH TO LANDING, THE CREW NOTICED LOSS OF RIGHT HYDRAULIC SYSTEM FLUID AND LOW PRESSURE. COMPLIED WITH COM PROCEDURE AND AIRCRAFT LANDED SAFELY. MAINTENANCE FOUND THE PRESSURE LINE FROM THE AUXILIARY PUMP RUPTURED. REPLACED THE LINE, BOTH THE RIGHT Dec 26, 2001 · N618NW · Doug DC932 · Hydraulic System, MainSDR AT0100244Engine · failedFOUND NR 1 ENGINE LOST OIL QUANTITY. OIL TEMPERATURE WENT UP AND OIL PRESSURE WENT DOWN. ENGINE WAS SHUT DOWN, ENGINE TURNED FOR 25-30 MINUTES AT LESS THAN 10 PSI. REMOVED AND REPLACED THE NR 1 ENGINE IAW DC9 72-00.Dec 22, 2001 · N836AT · Doug DC932 · Engine (Turbine/Turboprop)SDR 0105189985Door · crackedDuring HCK in DHN a crack was found in the Aft cargo Door Inner and Outer Pans. The damage to the outer pan was repaired in accordance with TRM 51-72-01. The inner pan was repaired per EA 99-187654.Dec 21, 2001 · N985US · Doug DC932 · Cargo/Baggage DoorsSDR GTIA012319Rib · crackedFTW - FOUND RIGHT WING NR 4 SLAT 8TH INNER RIB FROM OUTBOARD END OF SLAT IS CRACKED. REMOVED RIB. FABRICATED NEW RIB. INSTALLED NEW RIB IAW DC9 SRM 51-30-2. (M)Dec 20, 2001 · N12536 · Doug DC932 · Leading Edge DevicesSDR GTIA012313Panel · warpedFTW - FOUND RIGHT WING INBOARD FLIGHT SPOILER WARP. REMOVED RIGHT INBOARD SPOILER PANEL. INSTALLED RIGHT INBOARD SPOILER PANEL IAW MM DC9 27-61-1. (M)Dec 20, 2001 · N12536 · Doug DC932 · SpoilersSDR 0105199601Door · crackedDuring an Hck in DHN a .6" crack was found in the forward galley service door pan at the #4 door stop. Repaired per EA 96-187652.Dec 20, 2001 · N601NW · Doug DC932 · Service DoorsSDR AT0100243O-Ring · inoperativeFOUND #1 ENGINE LOST ALL OIL, SHUT DOWN #1 ENGINE AT 38 PSI OIL PRESSURE-ALL OTHER ENGINE PARAMETERS DID NOT EXCEED ILIMITATIONS. CORRECTIVE ACTION: FOUND BAD O-RING ON GEAR BOX TO OIL COOLER. REPLACED O-RING. IAW DC9 MM 79-20-2Dec 20, 2001 · N836AT · Doug DC932 · Engine Oil PressureSDR MWEA011487Longeron · chafedKEEL AREA LONGERON 27 LEFT HAS A CHAFE AT STATION 655 AB5. REMOVED, DRILLED AND INSTALLED LONGERON.Dec 17, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA012095Doubler · crackedFTW - NR 2 ENGINE NOSE COWL 2ND INTERNAL RIB (FROM AFT) 6 O'CLOCK POSITION REPAIR DOUBLER CRACKED. REMOVED DOUBLER REPAIR CRACKED. FORMED NEW SPLICE DOUBLER, INSTALLED NEW REPAIR IAW DC9 SRM 51-30-5. (M)Dec 15, 2001 · N12536 · Doug DC932 · Engine Cowling SystemSDR GTIA012156Web · crackedFTW - RIGHT NOSE COWL INBOARD AREA AT 6 O'CLOCK POSITION DOUBLER CRACKED. REMOVED CRACKED DOUBLER. AFTER FURTHER EVALUATION FOUND WEB ALSO CRACKED. CUT DAMAGED AREA (ON WEB). FABRICATED DRILLED AND LOCATED REPAIR PARTS FILLED DOUBLER. INSTALLED REPAIR PARDec 15, 2001 · N12536 · Doug DC932 · Engine Cowling System
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