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 MWEA98649Spar · damagedTHE LEFT PYLON UPPER SPAR CAPS WERE FOUND DAMAGED. REMOVED AND REPLACED SPAR CAPS USING APPROVED DATA.Jun 9, 1998 · N215ME · Doug DC932 · Nacelle/Pylon StructureSDR MWEA98648Angle · damagedTHE LEFT PYLON FWD SPAR AFT INBOARD SURFACE HAS A IMPROPER REPAIR. MAINTENANCE REMOVED DAMAGED AREA INSTALLED REPLACEMENT PARTS USING APPROVED DATA.Jun 9, 1998 · N215ME · Doug DC932 · Nacelle/Pylon StructureSDR MWEA98647Bulkhead Channel · crackedAFT PRESSURE BULKHEAD CHANNELS HAVE CRACKS IN UPPER CORNERS. MAINTENANCE REMOVED CRACKS BY BLENDOUT IAW SABRETECH EA.Jun 9, 1998 · N215ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98646Bulkhead Double · crackedTHE AFT PRESSURE BULKHEAD -13 DOUBLER WAS FOUND CRACKED. MAINTENANCE REMOVED OLD DOUBLER OBTAINED NEW DOUBLER AND INSTALLED USING APPROVED DATA.Jun 9, 1998 · N215ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98645Battery Pack · dischargedTHE EMERGENCY OVERWING EXIT LIGHTS WENT OUT AFTER A 14 HOUR CHARGE. MTC REMOVED AND REPLACED BATTERY PACK.Jun 9, 1998 · N501ME · Doug DC932 · Emergency LightingSDR MWEA98644Battery Pack · dischargedTHE EMERGENCY CEILING LIGHTS WOULD NOT COME ON DURING TEST. MTC REMOVED AND REPLACED EMERGENCY CEILING BATTERY PACK.Jun 9, 1998 · N501ME · Doug DC932 · Emergency LightingSDR CALA9801106Bracket · crackedINSPECTION FOUND A CRACK WITH CORROSION IN LT WING FLAP XRS 270 LEADING EDGE SUPPORT BRACKET CAP. THE SUPPORT BRACKET CAP WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2.Jun 9, 1998 · N12538 · Doug DC932 · Trailing Edge FlapsSDR CALA9801105Rib · crackedINSPECTION FOUND A 1.5 INCH CRACK WITH CORROSION ON LT WING STA XRS 280 FLAP RIB ON LEADING EDGE PANEL FLANGE. THE RIB WAS REMOVED FROM SUPPORT CAP, A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.Jun 9, 1998 · N12538 · Doug DC932 · Wing, Rib/BulkheadSDR CALA9801104Floorboard · crackedINSPECTION FOUND CRACKS AT SCREW HOLES OF FLOORBOARD NR 51, STA 465 TO 579 AND FLOORBOARD NR 40, STA 578 WITH SCREWS PULLING THROUGH. NEW FLOORBOARDS WERE FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 1, 51-20-0, 51-30-2, 51-10-2, 51-10-3, AND 51-70-2.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801014Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT CHANNEL OF RT NLG WHEEL WELL FORWARD FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, AND 51-10-6.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801013Hinge · crackedINSPECTION FOUND A .375 INCH CRACK IN AFT LOBE OF RT MLG DOOR UPPER HINGE. A NEW HINGE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-4.Jun 9, 1998 · N12538 · Doug DC932 · Landing Gear DoorsSDR CALA9801012Seat Track · corrodedINSPECTION FOUND LT OUTBOARD SEAT TRACK CORRODED AT STA 260. THE CORRODED SECTION OF SEAT TRACK WAS CUT OUT, A NEW REPAIR SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4F.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9801011Strap · corrodedINSPECTION FOUND STRAP CORRODED BETWEEN LONGERONS 27L AND 28L AT STA 851 TO 870. THE STRAP WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-2A, 51-10-04, 51-10-3, 51-30-2, AND 53-01.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801010Rib · crackedINSPECTION FOUND A 3 INCH CRACK IN RT WING LEADING EDGE RIB. THE RIB WAS REMOVED AND A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-00-00.Jun 9, 1998 · N12538 · Doug DC932 · Wing, Rib/BulkheadSDR CALA9801009Longeron · gougedINSPECTION FOUND LONGERON 5L GOUGED AT STA 207. TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9801008Support · crackedINSPECTION FOUND LT WING STA 280 FLAP LEADING EDGE SUPPORT CAP CRACKED AND CORRODED. THE SUPPORT CAP WAS REMOVED, A NEW SUPPORT CAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-2.Jun 9, 1998 · N12538 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9801007Web · crackedINSPECTION FOUND A 2 INCH CRACK IN WEB AT STA 589 ON LT SIDE OF FUSELAGE. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-30-2, AND 53-10-2.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9801006Floorbeam · gougedINSPECTION FOUND AFT PIT UPPER FLOORBEAM GOUGED AT STA 917. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 86, 51-30-1, AND 51-30-2.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9801005Floorboard · crackedINSPECTION FOUND CRACKS IN LT FLOORBOARD NR 58. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-70-1, AND 51-70-3, PAGE 1 AND 2.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801004Floorboard · delaminatedINSPECTION FOUND FLOORBOARD AT STA 200 TO 244 DELAMINATING. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 122B.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801003Floorboard · puncturedINSPECTION FOUND A HOLE IN FLOORBOARD PANEL NR 71. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, PAGES 15-16, AND 51-30-2, PAGES 1-30.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801002Floorboard · crackedINSPECTION FOUND .5 INCH CRACKS AT SCREW HOLES OF FLOORBOARD NR 51. REPAIRED IAW SRM 53-01, FIGURE 2, PAGE 3.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801001Floorbeam · corrodedINSPECTION FOUND LT FLOORBEAM AT BS 996, LBL 18 CORRODED. AN UPPER CAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-0 AND 51-10-1.Jun 9, 1998 · N12538 · Doug DC932 · Fuselage Main, Floor BeamSDR CA980706030Oven Socket · failed(CAN) DURING APPROACH, AN ELECTRICAL BURNING SMELL WAS DETECTED COMING FROM THE GALLEY. THE GALLEY POWER WAS TURNED OFF, SMELL DISSIPATED AND A/C LANDED SAFELY. MAINTENANCE FOUND OVEN POSITION NR 17 SOCKET BURNT. OVEN POSITION NR 17 SOCKET WAS REPLACED.Jun 9, 1998 · Doug DC932 · Buffet/GalleysSDR 9809499621Coalescer Bag · dirtyAT FL280, THE CABIN PRESSURE CLIMBED RAPIDLY. THE FLIGHT CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET AND GAINED CONTROL OF CABIN PRESSURIZATION. NO FURTHER PROBLEMS WERE NOTED AND THE AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLAJun 9, 1998 · N621NW · Doug DC932 · Humidity Control SystemSDR CALA9801103Floorpanel · corrodedINSPECTION FOUND COCKPIT FLOORBOARD PANEL NR 12 CORRODED. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0 AND 53-05, PAGE 1.Jun 8, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9801098Stiffener · crackedINSPECTION FOUND CABIN FLOORBOARD STIFFENER CRACKED AND BENT AT FLOOR SUPPORT BS 313, RT CENTER OF CEILING. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-05 AND NEW SKIN WAS INSTALLED IAW SRM 53-05, 51-30-2, AND 51-70-2.Jun 8, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800997Doubler · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE FRAME UPPER DOUBLER AT STA 438. THE ANGLE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.Jun 8, 1998 · N12538 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9800992Support · crackedINSPECTION FOUND A .75 INCH CRACK IN FORWARD PIT RT FLOOR SUPPORT FRAME ABOVE LONGERON 9R AT STA 351. THE CRACKED SECTION OF STANDOFF FLOOR SUPPORT WAS REMOVED. A STANDOFF FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.Jun 8, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800989Rib · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING FLAP RIB AT WS XRS 270 WITH CORROSION AT INBOARD END OF RIB. THE RIB WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3.Jun 8, 1998 · N12538 · Doug DC932 · Trailing Edge FlapsSDR CALA9800988Angle · corrodedINSPECTION FOUND L-ANGLE CORRODED AT STA 996, RBL 28. THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10, 51-10-2, 51-30-1, AND 51-10-3.Jun 8, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800987End Cap · crackedINSPECTION FOUND A 1 INCH CRACK IN END CAP OF LONGERON 19L AT AFT PRESSURE BULKHEAD STA 996. THE END CAP WAS REMOVED AND REPLACED IAW SRM 51-10-4.Jun 8, 1998 · N12538 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9800986Floorboard · corrodedINSPECTION FOUND CO-PILOT'S FLOORBOARD CORRODED AT STA 130, RBL 34 TO RBL 50. THE FLOORBOARD AND SKIN WERE REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, FIGURE 2F, 51-30-2, 51-10-2, 51-10-4, 51-10-3 AND MM 53-20-1.Jun 8, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR VJ9800187Switch · failedGEAR HORN SOUNDED AND 3 UNSAFE LIGHTS ILLUMINATED. FLIGHT CREW ELECTED TO RETURN TO BASE AND CREW OBTAINED 3 SAFE LANDING GEAR DOWN LIGHTS. AIRCRAFT FERRIED TO ATL. MAINTENANCE BASE FOR JACKING OF AIRCRAFT AND GEAR SWING AND REAIRS AS NECESSARY. REPLACED FJun 7, 1998 · N938VV · Doug DC932 · Landing Gear Position and WarningSDR CALA9801097Strap · corrodedINSPECTION FOUND AFT CARGO PIT RT SIDEWALL PANEL STRAP CORRODED AT STA 945 TO 996. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 51-10-2.Jun 7, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800985Panel · crackedINSPECTION FOUND THREE .5 INCH CRACKS AT CORNER OF INNER DOUBLER ON NR 1 ENGINE PYLON PANEL NR 8103. THE CRACKED AREA WAS CUT OUT. A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4.Jun 7, 1998 · N12538 · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR CALA9800984Fairing · crackedINSPECTION FOUND A 1 INCH CRACK IN INBOARD AFT CORNER OF RT ELEVATOR GEAR TAB CONTROL ROD FAIRING. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2, 51-10-2, 51-30-2, AND 51-10-3.Jun 7, 1998 · N12538 · Doug DC932 · Elevator StructureSDR CALA9800983Fitting · crackedINSPECTION FOUND A 2 INCH CRACK IN SUPPORT FITTING ON LT AFT END MLG DOOR CUTOUT. THE CRACK WAS TRIMMED OUT IAW SRM 53-05, FIGURE 71. A REPAIR WAS FABRICATED AND INSTALLED SRM 53-05, FIGURE 71 AND 51-10-3.Jun 7, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800982Angle · corrodedINSPECTION FOUND L-1 DOOR SILL ATTACH ANGLE CORRODED. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30-2, AND 51-30-5.Jun 7, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800981Bulkhead Beam · crackedINSPECTION FOUND A .5 INCH CRACK IN HORIZONTAL BEAM OF RT AFT LAV AFT PRESSURE BULKHEAD. THE CRACK WAS LOCATED JUST AFT OF STA 996, 62 INCHES UP FROM THE FLOOR AT THE OUTBOARD CORNER. THE CRACK WAS STOP DRILLED IAW SRM 53-01. REPAIR ANGLES WERE FABRICATED AJun 7, 1998 · N12538 · Doug DC932 · Fuselage Main, BulkheadSDR VJ9800267Frame · corrodedAFT CARGO PIT LT SIDE, AFT AND BELOW CABIN AIR OUTFLOW VALVE, FRAME CORRODED BEYOND LIMIT. REMOVED STRUT AND INSTALLED NEW STRUT IAW DC9 SRM 51-10-4, 51-10-2, 51-10-3, AND 53-11-3.Jun 5, 1998 · N935VV · Doug DC932 · Fuselage Main, FrameSDR VJ9800185Skin · dentedREMOVED VERTICAL STABILIZER, FABRICATED DOUBLER AND FILLER FROM 7075 T6.063. CUT OUT DENTED AREA, TRIMMED, DRILLED AND INSTALLED REPAIR IAW EO 9-53-004, REINSTALLED VERTICAL STABILIZER LEADING EDGE.Jun 5, 1998 · N948VV · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR TWAA9809116Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK AT STATION 200, LONGERON 2L HAD 2 CRACKS. CUT OUT APPROX 17 INCHES OF LONGERON. ADDED NEW MATERIAL PLUS TWO REPAIR SPLICES PER SRM 53-02, FIG 18. (M)Jun 5, 1998 · N998R · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9800980Floorboard · puncturedINSPECTION FOUND SURFACE SKIN OF CABIN FLOORBOARD PANEL NR 77 PUNCTURED. A DOUBLER, HAT SECTION, AND REPAIR PANELS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 1, 51-70-2, 51-10-3, AND 51-20.Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9800979Skin · crackedINSPECTION FOUND A CRACK IN SKIN OF APU COMPARTMENT AT LT SIDE FORWARD BELOW INSPECTION PANEL ACCESS. THE CRACK WAS STOP DRILLED IAW SRM 51-10-44. TWO REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-01.Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9800978Fairing · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN RADIUS OF ATTACH FLANGE ON LT VERTICAL STABILIZER LOWER FAIRING. THE CRACKS WERE STOP DRILLED IAW SRM 51-01. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.Jun 5, 1998 · N12538 · Doug DC932 · Vertical StabilizerSDR CALA9800977Skin · crackedINSPECTION FOUND THREE 1 INCH CRACKS AT FASTENER HOLES IN FUSELAGE SKIN AT STA Y= 1104, X= 30. THE CRACKS WERE STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9800976Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 1121, FIFTEEN INCHES BELOW RT NEGATIVE PRESSURE LOUVERS. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2.Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9800975Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN FITTING AT STA 897 BETWEEN LONGERONS 27L AND 28L. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5, 51-30-2, AND 51-10-3.Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800974Floorboard · corrodedINSPECTION FOUND COCKPIT FLOORBOARD CORRODED ON PILOT'S SIDE IN CORNER FORWARD OF E AND E COMPARTMENT ACCESS DOOR AT STA 15L. THE FLOOR PANELS WERE REMOVED IAW SRM 51-30-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 51-30-2.Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Floor Panel
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