Douglas DC-9-32

Service difficulty reports · 12,755

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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 = '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 0103609607Pressure Panel · crackedDuring H CK ATL base Maintenance while accomplishing APB inspections per ref F a 1/2 inch crack was found in the upper inboard bend radius of the 5910130-9 channel running downward along the radius. Material is made from .125" 2014-t6 QQ-A-250/3.Oct 16, 2001 · N607NW · Doug DC932 · Fuselage Main, FrameSDR AT0100232Battery · dischargedFOUND PASSENGER CABIN EMERGENCY LIGHTS INOPERATIVE AT AT ROW 10-15. CORRECTIVE ACTION: REMOVED AND REPLACED NICAD BATTERIES. IAW DC9 MM33-50Oct 16, 2001 · N811AT · Doug DC932 · Emergency LightingSDR ABXA010536Engine · failedCLIMBING THROUGH FL 190, CREW HEARD A LOUD POP AND NOTICED THE LEFT ENGINE HAD DECREASED TO 1.35 EPR AND THE EGT HAD INCREASED TO 550. OPERATED ENGINE AT REDUCED POWER AND RETURNED TO LAND. REPLACED THE NR 1 ENGINE IAW DC-9 JOB CARD 9090010 AND DC-9 8A & 8B.Oct 15, 2001 · N982AX · Doug DC932 · Engine (Turbine/Turboprop)SDR 0103579607Cap · crackedDURING H-CHECK AT ATL BASE MAINTENANCE A 2 INCH CRACK WAS FOUND IN THE SLANT PANEL LOWER CAP (P/N 5910005-49) AT XCW=20 LT. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE INSTALLED.Oct 13, 2001 · N607NW · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0200012Skin · crackedFUSELAGE EXTERNAL SKIN HAS THREE (3) CRACKS AROUND RIVET HEADS AT STA 164 APPROX AND LONGERON 4 LEFT. CUT OUT DAMAGED AREA. NDT VERIFIED AFTER CUT OUT IAW NDT SRM PART 6-00-01, NO DISCREPANCIES NOTED. MADE SKIN REPAIR AND FINGER DOUBLER AND INSTALLED REPAIR Oct 11, 2001 · N817AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0200013Web · crackedFORWARD GALLEY AREA AT FS 200/LBL 31 - LBL 40, FOUND CRACKED TO FLOOR WEB ON (2) EXISTING DOUBLER REPAIRS. REMOVED EXISTING DOUBLER AS PER DC-9 SRM 51-30-2. INSTALLED NEW DOUBLER PER DC-9 SRM 53-01-09.Oct 10, 2001 · N817AT · Doug DC932 · Fuselage Miscellaneous StructureSDR 0103549759Spar Cap · corrodedDURING H CHECK IN ATL, CORROSION WAS FOUND ON RT WING REAR SPAR UPPER CAP AROUND THE HOLE FOR NR 3 FLAP HINGE STUD. THE HOLE WAS CLEANED UP WITH A DEPTH OF .040 INCH AND DIAMETER OF 1.26 INCH EXTRUSION 4911204, PER EA 97-185168.Oct 8, 2001 · N759NW · Doug DC932 · Wing SparSDR 0103569607Floorbeam · corrodedDURING M-CK IN ATL, CORROSION HAS BEEN FOUND ON STA 160 CABIN FLOOR BEAM CAP AFT FACING FLANGE WHERE THE OUTBOARD GALLEY MOUNT IS ATTACHED. IT WAS ELECTED TO TO TRIM THE AFT FACING FLANGE TO REMOVE THE DAMAGE. THE RADIUS OF THE CAP WAS NOT TRIMMED. 7075-T6511Oct 8, 2001 · N607NW · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA010532Battery · dischargedTHE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. THE EMERGENCY LIGHT BATTERY PACK WAS DEFERRED FOR REPLACEMENT. THE EMERGENCY LIGHT BATTERY PACK WAS REPLACED.Oct 8, 2001 · N939AX · Doug DC932 · Emergency LightingSDR ZW0A0109401Door · openAFTER GEAR RETRACTION PILOT NOTED A VIBRATION IN THE NOSE GEAR AREA. CREW ACCOMPLISHED FLY BY FOR VISUAL CHECK OF NOSE AREA, THEN RETURNED TO STL. FOUND LEFT NOSE GEAR DOOR NOT MANUALLY LATCHED. SECURED DOOR AND CHECKED MANUAL LOCK OPERATION.Oct 4, 2001 · N996Z · Doug DC932 · Landing Gear Door Retract SectionSDR MWEA011369Anti-Ice System · faultyLEFT ICE PROTECTION TEMP HIGH LIGHT CAME ON. PERFORMED QRH AND LEFT TEMP HIGH LIGHT WENT OUT BUT GOT A PRESSURE ABNORMAL LIGHT ON AND THE LEFT ICE PROTECTION TEMP LOW LIGHT CAME ON. REMOVED AND REPLACED ICE PROTECTION CONTROL ANTICIPATOR.Oct 4, 2001 · N215ME · Doug DC932 · Airfoil Anti/De-ice SystemSDR 0103599607Bulkhead · crackedDuring H-ck at ATL base maintenance, two cracks were found in the station 756 bulkhead. The cracks are located in the upper ends of the verticle stiffeners at x=-11 (.070)"(p/n 9958212-10) and x=-22 (1.0) "(p/n 9958212-121). Material 2014-t6511.Oct 2, 2001 · N607NW · Doug DC932 · Fuselage Main, BulkheadSDR 0103589607Pressure Panel · crackedDuring H-ck at ATL base, four cracks were found in the horizontal pressure panel at station 105, X=+-35. All cracks were less than 2 inches in length. material 9910073-313 web made from .040 2024-t3 aluminum clad sheet.Oct 2, 2001 · N607NW · Doug DC932 · Fuselage Main, BulkheadSDR MWEA011368Skin · inoperativeWHEN GEAR RETRACTED, FORWARD RIGHT NOSE GEAR DOOR WOULD NOT CLOSE. 4 FOOT CABLE PULLED OUT OF SWAGGED END FOR DOOR. -- REMOVED AND REPLACED UPPER STRANDED WIRE DOOR STOP CABLE ASSY. MAINTENANCE FOUND GOUGE LOCATED ON RIGHT FORWARD NOSE LANDING GEAR DOOR INNESep 30, 2001 · N202ME · Doug DC932 · Nose/Tail Landing GearSDR CA011114002Apu · failed(CAN) APU QUIT ON PUSHBACK, OIL LEAK OBSERVED. FOUND APU COMPRESSOR / TURBINE HAD A NON CONTAINED FAILURE CAUSING SEVERE DAMAGE. (TURBINE BLADES FOUND IN APU COMPARTMENT). REPLACED APU AS PER MM 49-10-00 REPLACED FUEL HEATER AS PER MM 49-31-01 CROSSOVER DUCSep 28, 2001 · Doug DC932 · APU Core EngineSDR ABXA010517Power Supply · defectiveEMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE IN THE ON POSITION. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY IAW DC-9 MM. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE.Sep 27, 2001 · N985AX · Doug DC932 · Emergency LightingSDR MWEA011361Doubler · dentedSKIN DENTED AT STATION 330, LONGERON 26 APPROXIMATELY 1 1/4 INCH BY .046 DEEP RIGHT HAND SIDE. -- REMOVED DAMAGE, INSTALLED INTERNAL DOUBLER AND FLUSH PLUG.Sep 27, 2001 · N501ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011350Angle · corrodedEXFOLIATION CORROSION ON AFT END OF VERTICAL STABILIZER ATTACH ANGLE LEFT SIDE, STATION 1121. FABRICATED AND INSTALLED ANGLE REPAIR.Sep 27, 2001 · N401ME · Doug DC932 · Vertical StabilizerSDR MWEA011348Doubler · missingSIX EMPTY FASTNER HOLES, FORWARD CARGO DOOR JAMB BAY, STATION 370 TO 362, LONGERON 29 RIGHT TO 28 RIGHT. -- FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER.Sep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA011347Skin · corrodedFUSELAGE SKIN BETWEEN STATION 813-832 HAS AREAS OF LIGHT CORROSION UNDER CHAFE STRIP AROUND NUT PLATE HOLES FROM LONGERON 21 THROUGH LONGERON 26 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLERS.Sep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA011346Frame · corrodedCORROSION ON LOWER CHANNEL OF FRAME, STATION 313, LONGERON 30. FABRICATED AND INSTALLED REPAIR DOUBLERS AND PLATES.Sep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, FrameSDR MWEA011345Frame · corrodedCORROSION ON LOWER CHANNEL OF FRAME, STATION 332, LONGERON 30. REMOVED AND REPLACED SECTION OF FRAME AND SPLICE DOUBLERS.Sep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, FrameSDR MWEA011343Door Frame · damagedVENTRAL DOOR JAMB HAS 4 EACH HOLES THAT ARE ELONGATED. HOLES ARE UNDER SILL PLATE. FABRICATED AND INSTALLED SCUFF PLATE AND REPAIR DOUBLER.Sep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011342Frame · corrodedCORROSION ON BOTTOM FACE OF FRAME, STATION 218, BETWEEN AND EXTENDING UNDER LONGERONS 30 AND 29 LEFT. FABRICATED AND INSTALLED REPAIR ANGLES AND PLATES.Sep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, FrameSDR MWEA011341Frame · corrodedE&E COMPARTMENT FRAME STATION 180 HAS LIGHT CORROSION ON FORWARD SIDE FROM LONGERON 28 RIGHT TO 30. FABRICATED AND INSTALLED FRAME REPAIR.Sep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, FrameSDR MWEA011366Doubler · misdrilledLEFT ELEVATOR, UPPER OUTBOARD SKIN AT FORWARD SPAR HAS A FINGER DOUBLER MISDRILLED. -- FABRICATED AND INSTALLED REPLACEMENT DOUBLER.Sep 27, 2001 · N602ME · Doug DC932 · Elevator StructureSDR MWEA011365Doubler · damagedFORWARD CARGO INTERIOR SKIN HAS A CUT BETWEEN STAITON 360 THROUGH 364 AND LONGERON 27 LEFT THROUGH 28 LEFT. -- FABRICATED AND INSTALLED REPAIR DOUBLER.Sep 27, 2001 · N602ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA011364Doubler · chafedAFT ACCESSORY COMPARTMENT FRAME STATION 1019 HAS CHAFFE MARKS BETWEEN LONGERON 14 LEFT AND 15 LEFT WITH TWO BROKEN CLAMPS FOR INSTRUMENT AIR LINES. -- FABRICATED AND INSTALLED REPAIR ANGLE, DOUBLER, AND FILLER AND REMOVED AND REPLACED CLAMPS.Sep 27, 2001 · N602ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA011362Pan · gougedFORWARD CARGO DOOR HAS A DEEP GOUGE IN THE PAN RADIUS JUST OUTBOARD OF THE DOOR FORWARD ROTATING CAM LOCK. FABRICATED AND INSTALLED DOUBLER REPAIR.Sep 27, 2001 · N602ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA011360Pan · corrodedAFT CARGO BAY FORWARD JAMB PAN HAS AREAS OF LIGHT CORROSION BETWEEN LONGERON 25 THROUGH LONGERON 26 RIGHT. FABRICATED AND INSTALLED REPLACEMENT SECTION OF PAN, DOUBLERS, AND SHIM.Sep 27, 2001 · N602ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA011359Longeron · corrodedLONGERON 23 RIGHT HAS LIGHT CORROSION AT STATION 579-580. FABRICATED AND INSTALLED LONGERON AND REPAIR SPLICE.Sep 27, 2001 · N602ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA011357Intercostal · bentFORWARD PIT INTERCOASTAL IS BENT LOCATED BETWEEN FRAMES 484 AND 503 BEWEEN LONGERONS 28 LEFT AND 27 LEFT. -- FABRICATED AND INSTALLED INTERCOSTAL.Sep 27, 2001 · N602ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011340Fitting · crackedFRAME FITTING CRACKED, STATION 427, LONGERON 28 LEFT -- FABRICATED AND INSTALLED FITTINGSep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011339AngleTOOL DAMAGE, CORROSION AROUND BN NUT, ONE ELONGATED FASTENER HOLE AND THREE EMPTY FASTENER HOLES, FORWARD CARGO DOOR JAMB BAY, STATION 427 TO 435, LONGERON 28 RIGHT TO 26 RIGHT -- REMOVED, FABRICATED AND INSTALLED REPAIR ANGLE.Sep 27, 2001 · N401ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011355Intercostal · bentFORWARD PIT INTERCOSTAL IS BENT BETWEEN FRAMES 351 AND 370 AT LONGERON 29 LEFT. -- FABRICATED AND INSTALLED INTERCOSTAL.Sep 27, 2001 · N602ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011354Web · corrodedAFT CARGO BAY JAMB WEB BETWEEN STATION 889 THROUGH STATION 897 HAS SEVERAL AREAS OF LIGHT CORROSION AROUND FASTENER HOLES (INTERNAL AND EXTERNAL) BETWEEN LONGERON 24 RIGHT THROUGH LONGERON 28 RIGHT. REMOVED CORROSION FROM STIFFENERS AND FABRICATED AND INSTALLESep 27, 2001 · N602ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA011353Skin · corrodedTOPSIDE OF LEFT ELEVATOR HAS AN AREA OF CORROSION 36 INCHES INBOARD FROM OUTBOARD TIP. FABRICATED AND INSTALLED SKIN/PANEL.Sep 27, 2001 · N602ME · Doug DC932 · Elevator, Plate/SkinSDR MWEA011352Control Box · faultyIN CRUISE NOSE GEAR UNSAFE LIGHT CAME ON, RIGHT GEAR HANDLE UP, RED LIGHT ON IN CRUISE AND APPROACH, LOWERED GEARS, NOSE GEAR RED STAYED ON. QRH PERFORMED, CONFIRMED VISUALLY NOSE GEAR DOWN AND LOCKED. INSPECTED NOSE GEAR SYSTEM, REMOVED AND REPLACED PROXIMITSep 24, 2001 · N212ME · Doug DC932 · Landing Gear Position and WarningSDR AT0100230Battery · dischargedFOUND SEVERAL EMERGENCY CEILING LIGHTS OUT. REMOVED AND REPLACED EMERGENCY LIGHT NICAD BATTERIES IN CABIN CEILING AT ROW 18 IAW DC9 MM 33-50.Sep 24, 2001 · N828AT · Doug DC932 · Emergency LightingSDR MWEA011278Longeron · crackedLONGERON 28 LEFT CRACKED STATION 560 -- REMOVED AND REPLACED LONGERON.Sep 20, 2001 · N602ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011277Frame · crackedFRAME CRACKED AT STATION 980 LONGERON RIGHT -- FABRICATED AND INSTALLED FRAME SPLICE, LONGERON ANGLE AND FILLER FRAME MATERIALS.Sep 20, 2001 · N602ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011276Shear Tie · crackedSHEAR TIE CRACKED IN 2 PLACES AT STATION 945 LONGERON 15 RIGHT. FABRICATED AND INSTALLED SHEAR TIE.Sep 20, 2001 · N602ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011275Longeron · gougedAFT CARGO BAY LONGERON 26 LEFT IS GOUGED AT STATION 794 -- FABRICATED AND INSTALLED LONGERON AND SPLICES.Sep 20, 2001 · N602ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011274Support Bracket · damagedAFT CARGO DOOR FUSELAGE SUPPORT BRACKET (AFT HINGE FORWARD BRACKET) HAS VERY ELONGATED FASTENER HOLES. FABRICATED AND INSTALLED SUPPORT BRACKET.Sep 20, 2001 · N602ME · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA010496Switch · defectiveDURING DEPARTURE WHEN LANDING GEAR WAS RETRACTED, A RED NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE LANDING GEAR WAS RECYCLED AND THE GEAR RETRACTED NORMALLY. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK AND DOWN LOCK SWITCHES. OPERATIONAL CHECKS WERE CSep 19, 2001 · N980AX · Doug DC932 · Landing Gear Position and WarningSDR ABXA010474Light · shortedTHE FIRST OFFICERS OVERHEAD MAP LIGHT WENT OUT AND CAME BACK ON. A BURNING ELECTRICAL SMELL WAS NOTED. THE ASSOCIATED MAP LIGHT CIRCUIT BREAKER OPENED, NO FURTHER PROBLEMS WERE NOTED. MAINTENANCE INSPECTED AND FOUND EVIDENCE OF THE LIGHT ASSY TOUCHING A CAMSep 18, 2001 · N901AX · Doug DC932 · Flight Compartment LightingSDR ABXA010473Battery · dischargedEMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW DC9 AMM 33-53-02-04.Sep 17, 2001 · N901AX · Doug DC932 · Emergency LightingSDR AT0100229Wire · brokenFOUND FORWARD RED LIGHTS OF THE PASSENGER EMERGENCY EGRESS PATH LIGHTING SYSTEM INOPERATIVE. REPAIRED BROKEN WIRE AT FORWARD LEFT PORTION OF TRACK IAW DC9 MM 33-50.Sep 15, 2001 · N810AT · Doug DC932 · Light System WiringSDR MWEA011272Web · chafedFOUND MINOR CHAFE ON WEB IN NOSE WELL. -- BLENDED CHAFE AND REPAIRED WITH DOUBLER REPAIR.Sep 15, 2001 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA011260Splice · corrodedE&E COMPARTMENT, LONGERON 29 LEFT HAS AREAS OF LIGHT CORROSION BETWEEN STATION 160 AND 170. REMOVED AND REPLACED SPLICE.Sep 15, 2001 · N401ME · Doug DC932 · Fuselage Miscellaneous Structure
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