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 MWEA010627Uplock · out of adjAFTER TAKEOFF WITH GEAR SELECTED UP, LEFT GEAR UNSAFE (RED) LIGHT REMAINED ON. CREW CYCLED GEAR WITH SAME RESULT. RETURNED TO MCI AND LANDED WITH THREE GREEN LIGHTS, NO RED. MAINTENANCE ADJUSTED DOOR LATCH MECHANISM AND PERFORMED GEAR SWING. SYSTEM CHECKEDApr 19, 2001 · N401ME · Doug DC932 · Landing Gear Position and WarningSDR 0103409604Bulkhead · corrodedDuring H-check found extensive corrosion on the aft pressure bulkhead web, doubler, and tripler. Repaired per EA. 99-172626.Apr 18, 2001 · N604NW · Doug DC932 · Fuselage Main, BulkheadSDR AT0100139Frame · crackedFOUND CRACK AT BS 1074. PERFORMED PERMINATE REPAIR AT BS 1074 IAW DCI SRM 51-10-3 AND DC9 MM 53-10 FIGURE 811.Apr 17, 2001 · N811AT · Doug DC932 · Fuselage Main, FrameSDR MWEA010605Floorboard · corrodedFLOORBOARD A-6 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. FABRICATED AND INSTALLED FLOORBOARD SKIN AND HAT CHANNELS.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010604Floorboard · corrodedFLOORBOARD A-4 HAS SEVERAL AREAS OF CORROSION ON TOP SURFACE AND CORROSION AROUND SOME OF THE FASTENER HOLES AND BOTTOM HAT CHANNELS HAVE MINOR CHAFES AND CORROSION. REMOVED CORROSION AND CHAFING. REPAIRED FLOOR PANEL IAW DC9 SRM 51-30-2 AND DRW 9915597 & SRApr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010603Intercostal · damagedINTERCOSTAL AT STATION 390 LONGERON 27 RIGHT - 29 RIGHT HAS ELONGATED HOLES AND IS BENT. FABRICATED AND INSTALLED INTERCOSTAL AND INBOARD AND OUTBOARD TEE CLIPS.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010602Intercostal · corrodedINTERCOSTAL AT STATION 1018 AND RBL 15 TO 25 CORRODED AND CRACKED. REMOVED AND REPLACED INTERCOSTAL.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010601Spar · corrodedRIGHT WING INTERNAL AFT LOWER SPAR TEE HAD HEAVY CORROSION. FABRICATED REPAIR FILLERS, INSTALLED IAW BOEING TELEX MWX-ORD-01-00272H, DATED 03 APRIL 2001. PLACED ON WATCH ITEM 5720 FOR FINAL DISPOSITION.Apr 17, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010600Intercostal · crackedINTERCOSTAL BETWEEN STATION 945 - 965 AT CENTERLINE OF AIRCRAFT BELOW SUPPORT IS CRACKED. REMOVED INTERCOSTAL, FABRICATED, DRILLED, AND INSTALLED NEW PART.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010599Longeron · corrodedLONGERON 28 RIGHT IS CORRODED FROM STATION 323 - 360. REMOVED DAMAGED SECTION, FABRICATED SECTION, REPAIR SPLICE, DRILLED AND INSTALLED.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA010598Floorboard · damagedFLOORBOARD A-1 HAD SEVERAL FASTENERS PULLED THRU AND CORROSION; CHAFES AROUND HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED NEW FLOORBOARD, REMOVED CORROSION FROM HAT CHANNELS, FABRICATED ONE NEW HAT CHANNEL AND INSTALLED ALL.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010597Floorboard · corrodedFLOORBOARD E-9 HAD SEVERAL AREAS OF CORROSION AROUND FASTENER HOLES AND ON HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED SKIN, REMOVED CORROSION FROM HAT CHANNELS, ASSEMBLED NEW SKIN AND CHANNELS.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010596Floorboard · corrodedFLOORBOARD A-5 HAD AREAS OF CORROSION AROUND HOLES AND ON HAT CHANNELS. REMOVED FLOORBOARD, FABRICATED PANEL, HAT CHANNELS, ASSEMBLED AND INSTALLED TOGETHER.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010595Shear Tie · corrodedFOUND CORROSION ON SKIN SPLICE DOUBLER AND FORWARD SIDE OF RIGHT LAV FLOORBEAM AT STATION 996. REMOVED SHEAR TIE, LOCATED, DRILLED, AND INSTALLED NEW SHEAR TIE.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010594Spar · gougedREMOVED LEFT WING SPAR WEB AT TRUNNION AND FOUND GOUGES OUT OF LIMITS. FABRICATED, DRILLED AND INSTALLED NEW WEB SECTION.Apr 17, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010592Fitting · gougedFOUND DEEP GOUGES ON FITTING AT STATION XRS 353 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. REMOVED FITTING, FABRICATED, DRILLED AND INSTALLED NEW FITTING.Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010591Clip · corrodedCORROSION FOUND ON OUTBOARD OF XCW 58 LOWER TEE CAP, HORIZONTAL LEG BETWEEN STRINGER 23. REMOVED 2 CLIPS FOR OUT OF LIMITS CORROSION. FABRICATED DRILLED AND INSTALLED NEW CLIPS.Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010590Structure · corrodedAT LEFT WING FOUND CORROSION ON LOWER TEE CAP HORIZONTAL LEG BETWEEN STRINGER 13 AND 14. REMOVED CORROSION, SUBMITTED BLENDOUTS TO BOEING AND ARE ACCEPTABLE PER TELEX MWX-ORD-01-00146H DATED 21, FEB, 2001. PLACED ON WATCH ITEM 5616 FOR REPETITIVE INSPECTION.Apr 17, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010589Clip · damagedSEVERAL CLIPS (6) REQUIRED REPLACEMENT BETWEEN STATION 370 - 427. REMOVED CLIPS, FABRICATED AND INSTALLED NEW CLIPS.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010588Floor Panel · crackedFLOORBOARD D-5 CHAFE FLEXIBLE JOINT HAD CRACKED HOLES. REMOVED FLEXIBLE JOINT. FABRICATED AND INSTALLED NEW JOINT.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010587Intercostal · corrodedCABIN INTERCOSTAL BETWEEN FLOORBEAM AT STATION 351-370 INBOARD OF NR 1 SEAT TRACK HAS CORROSION AROUND NUT PLATES. REMOVED FABRICATED, DRILLED, AND INSTALLED NEW INTERCOSTAL.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010586Bracket · corrodedAT FORWARD CARGO DOOR JAMB FOUND LIGHT CORROSION ON L-BRACKET, INSIDE BOX STRUCTURE. REMOVED BRACKET, DRILLED AND INSTALLED NEW BRACKET.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010585Bracket · corrodedAT FORWARD CARGO DOOR JAMB FOUND LIGHT CORROSION ON L-BRACKET INSIDE BOX STRUCTURE. REMOVED BRACKET, DRILLED AND INSTALLED NEW BRACKET.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA010584Fitting · corrodedFORWARD CARGO DOOR JAMB, FOUND T-FITTING CORRODED INSIDE BOX STRUCTURE TOP OF DOOR JAMB ABOVE AFT STOP FITTING. REMOVED BRACKET, FABRICATED, DRILLED, AND INSTALLED NEW FITTING.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010583Fitting · corrodedFORWARD CARGO DOOR JAMB TEE FITTING WAS EXFOLIATED INSIDE BOX STRUCTURE TOP OF DOOR JAMB. REMOVED FITTING, FABRICATED, AND INSTALLED NEW TEE FITTING.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010582Doubler · corrodedINTERCOSTAL AT LONGERON 29 RIGHT, STATION 351-362 HAD LIGHT CORROSION ON LOWER FLANGE AND TOP DOUBLER. REMOVED CORROSION, REMOVED TOP DOUBLER, DRILLED AND INSTALLED NEW TOP DOUBLER.Apr 17, 2001 · N209ME · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0100172Frame · crackedFOUND FRAME AT BS 598 LONGERON 11 CRACKED. FABRICATED AND INSTALLED REPAIR IAW REO-L00432.Apr 16, 2001 · N803AT · Doug DC932 · Fuselage Main, FrameSDR AT0100160Longeron · crackedFOUND LONGERON 11 FRAME AT BS 598 CRACKED. INSTALLED REPAIR IAW REO L00432.Apr 16, 2001 · N803AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA010579Trunnion · corrodedLEFT MAIN LANDING GEAR TRUNNION: LIGHT CORROSION ON BOTH FACES OF SIDE BRACE OF ATTACH LUG. FABRICATED AND INSTALLED STRUT ASSY SHIMS.Apr 16, 2001 · N209ME · Doug DC932 · Wing, Landing Gear Attach FittingsSDR MWEA010578Spar Cap · corrodedLEFT WING INTERNAL HAS LIGHT CORROSION ON LOWER TEE CAP LEG FORWARD OF AFT SPAR AT APPROX XRS 67. LOCATED, DRILLED, AND DEBURRED HORIZONTAL FLANGE OF SPAR CAP AND VERTICAL FLANGE OF SPAR CAP. INSTALLED FASTENERS.Apr 16, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010577Stiffener · corrodedXRS 86 WEB SUPPORT STIFFENER END TEE IS EXFOLIATED. FABRICATED AND INSTALLED END TEE.Apr 16, 2001 · N209ME · Doug DC932 · Wing Miscellaneous StructureSDR MWEA010576Floorbeam · corrodedCORROSION GOUGES AND ELONGATED HOLES ON RT LAV FLOORBEAMS AT STATION 996. FABRICATED AND INSTALLED FLOORBEAM ANGLE.Apr 16, 2001 · N209ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA010575Frame · misdrilledSTATION 427 FRAME FROM LONGERON 25 RIGHT THRU 28 RIGHT HAS SEVERAL DOUBLE DRILLED HOLES ON TOP FLANGE OF FRAME. FORMED AND INSTALLED DOUBLER REPAIR.Apr 16, 2001 · N209ME · Doug DC932 · Fuselage Main, FrameSDR AT0100159Attach Angle · crackedFOUND DORSAL FIN ATTACH ANGLES CRACKED BEYOND LIMITS. REPLACED ATTACH ANGLES IAW EO 09-5350-29-E1645.Apr 15, 2001 · N803AT · Doug DC932 · Fuselage, Stabilizer Attach FittingsSDR GTIA010212Track · looseACY - FLT 616 - FOUND EMERGENCY FLOOR LIGHTING STRIP LOOSE AT ROW 14. REINSTALLED LIGHTING TRACK, OPS CHECK GOOD IAW MM 33-53-00. (M)Apr 14, 2001 · N133NK · Doug DC932 · Emergency LightingSDR MWEA010580Switch · inoperativeTAKE OFF WARNING HORN CAME ON AT 105 KNOTS DURING TAKE OFF ROLL. ABORTED TAKE OFF. MAINTENANCE FOUND PARKING BRAKE SWITCH INOPERATIVE AND REPLACED SWITCH.Apr 13, 2001 · N212ME · Doug DC932 · Landing Gear Brake SystemSDR AT0100131Control Valve · groovedFOUND GROOVES IN SHAFT OF THRUST REVERSER CONTROL VALVE SECTOR. REPAIRED GROOVED SHAFT OF THRUST REVERSER CONTROL VALVE SECTOR BY MACHINING, FABRICATING AND INSTALLING REPAIR SLEEVE/BUSHING IAW TIMCO REO-L00340.Apr 11, 2001 · N837AT · Doug DC932 · Engine Thrust ReverserSDR MWEA010568Cargo Track · corrodedFORWARD BAG PIT, CARGO TIE DOWN MOUNT FITTING AT STATION 365 BETWEEN LONGERON 30 AND LONGERON 29 RIGHT IS CORRODED. FABRICATED AND INSTALLED FITTING.Apr 11, 2001 · N209ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA010573Gusset · corrodedLEFT TRUNNION LOWER GUSSET CORRODED, XRS 111. FABRICATED AND INSTALLED NEW GUSSET.Apr 11, 2001 · N209ME · Doug DC932 · Wing, Landing Gear Attach FittingsSDR MWEA010572Spar · corrodedLIGHT CORROSION ON XCW 58 TEE LOWER SIDE JUST UNDER THE INBOARD FORWARD LOWER END OF STRINGER 22, LEFT WING INTERNAL. -- REMOVED CORROSION. BLEND OUT IS ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00146H.Apr 11, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010571Spar · corrodedLEFT WING INTERNAL, LIGHT CORROSION ON XCW 58 TEE HORIZONTAL LEG BETWEEN STRINGER 15 AND 16. REMOVED CORROSION. BLENDOUTS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00146H.Apr 11, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010570Spar · corrodedLEFT WING INTERNAL, LIGHT CORROSION ON XCW 58 TEE HORIZONTAL LEG BETWEEN STRINGER 12 AND 13. REMOVED CORROSION AND BLENDED. BLENDOUTS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00171H DATED 2/28/01.Apr 11, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010569Spar · corrodedLEFT WING INTERNAL, 4 AREAS OF LIGHT CORROSION ON BOTTOM HORIZONTAL LEG OF FORWARD SPAR FROM XCW 58 TO 12 INCHES OUTBOARD OF XCW 58. -- BLENDED AREAS. AREAS ARE ACCEPTABLE FOR STRENGTH, IAW BOEING TELEX MWX-ORD-01-00147H DATE 21 FEB 01.Apr 11, 2001 · N209ME · Doug DC932 · Wing SparSDR MWEA010567Handle · inoperativeLEFT FORWARD OVERWING EXIT DOOR HAS A HANDLE THAT OPENS INTERMITTENLY. -- REMOVED AND REPLACED HOUSING ASSEMBLY.Apr 11, 2001 · N209ME · Doug DC932 · Emergency ExitsSDR MWEA010557Skin · chafedVERTICAL STABILIZER SKIN JUST AFT OF LEFT LEADING EDGE SIDE ROLLER TRACK HAS A CHAFE MARK. FABRICATED AND INSTALLED HORIZONTAL STAB CUTOUT PANEL.Apr 10, 2001 · N209ME · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR MWEA010563Angle · crackedFORWARD SERVICE DOOR UPPER BEAM FORWARD END AHD ANGLE THAT WAS CRACKED. REMOVED ANGLE, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW ANGLE.Apr 10, 2001 · N204ME · Doug DC932 · Service DoorsSDR MWEA010562Beam · crackedPAX DOOR HAD A CRACK ON THE NR 6 BEAM LOWER SIDE AT CENTER OF DOOR. STOP DRILLED CRACK, FABRICATED LOCATED DRILLED AND ISNTALLED REPAIR DOUBLERS.Apr 10, 2001 · N204ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA010561Longeron · corrodedLONGERON 29 LEFT WAS EXFOLIATED AT STATION 913 JUST AFT OF SPLICE. REMOVED DAMAGED AREA, LOCATED, DRILLED AND INSTALLED NEW LONGERON SPLICE AND LONGERON.Apr 10, 2001 · N204ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA010560Angle · crackedPAX DOOR AFT END DOOR PAN SPLICE ANGLE HAD A CRACK AT CUT OUT FOR BAYONET. FABRICATED REPAIR ANGLE, LOCATED, DRILLED AND INSTALLED.Apr 10, 2001 · N204ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA010559Longeron · crackedLONGERON 13 LEFT CRACKED AT BULKHEAD, STATION 965 LOWER ATTACH POINT. REMOVED DAMAGED SECTION, FABRICATED REPAIR SPLICE, LONGERON SECTION, DRILLED AND INSTALLED.Apr 10, 2001 · N204ME · Doug DC932 · Fuselage Main, Longeron/Stringer
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