Douglas DC-9-32

Service difficulty reports · 12,755

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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"

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SDR CALA9800973Angle · corrodedINSPECTION FOUND CORROSION ON ATTACH ANGLE BELOW GENERATOR AT STA 160. THE CORRODED SECTIONS OF ANGLE WERE REMOVED IAW SRM 51-30-2. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-01, FIGURE 2, 51-10-3, AND 51-30-2.Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800972Web · crackedINSPECTION FOUND CABIN INTERIOR WEB CRACKED AT FS 617, RBL 50 TO 55. THE CUSP WEB WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 53-01, FIGURE 9.Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800971Fillet · corrodedINSPECTION FOUND LT FUSELAGE FILLET PANEL MATING SURFACE CORRODED AT STA 756 TO 832. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30-2.Jun 5, 1998 · N12538 · Doug DC932 · Aerodynamic FairingsSDR CALA9800970Floorboard · crackedINSPECTION FOUND FLOORBOARD NR 71 WITH THREE EACH BLOWN OUT HOLES AND ONE CRACKED. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED ON FLOORBOARD OVER BLOWN OUT HOLES AND CRACK IAW SRM 53-01, FIGURE 2, 51-10-3, PAGE 15 AND 16, 51-10-Jun 5, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR VJ9800184Bulhead · damagedREMOVED STA 37 LOWER BULKHEAD ASSY, FABRICATED ANTENNA DISH IAW EO 9-53-003. ORDERED, DRILLED AND INSTALLED STA 37 LOWER BULKHEAD SERRATED ASSY, SUPPORT STRUCTURE AND REMAINING BULKHEAD ASSEMBLY. INSTALLED RADOME, PERFORMED FIT CHECK IAW DC9 MM 53-50-1 PG 20Jun 4, 1998 · N948VV · Doug DC932 · Fuselage Main, BulkheadSDR VJ9800179Power Supply · inoperativeAFT CABIN OVERWING EXIT LIGHTS DO NOT ILLUMINATE WHEN EMERGENCY SWITCH ON. REPLACED POWER SUPPLY IAW MM 33-00, OPS CHECKS GOOD.Jun 4, 1998 · N914VV · Doug DC932 · Emergency LightingSDR TWAA9809204Skin · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND SKIN PILLOWING AROUND RIVETS ON REPAIR AT FS 207 TO 229, LONG 20R TO 21R. REMOVED REPAIR. NO CORROSION FOUND. INSTALLED NEW REPAIR PER SRM 53-04, FIG 26 SHEET 2, AND SHIMMED AS REQUIRED. (M)Jun 4, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9809203Skin · damagedMCI - DURING OP16 MAINTENANCE CHECK, FOUND SKIN PILLOWED AND RIVET HEADS PULLED FROM FS 200 TO 220, LONG 18R TO 19R. REMOVED REPAIR AND FOUND NO CORROSION. INSTALLED NEW REPAIR PER SRM 53-04, FIG 26 SHEET 2, AND SHIMMED AS REQUIRED. (M)Jun 4, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9801096Pan · crackedINSPECTION FOUND TWO CRACKS AT AFT END OF BEAM NR 4 OF AFT CARGO COMPARTMENT DOOR OUTER PAN. ONE CRACK WAS .3 LONG IN RADIUS AND THE OTHER WAS .7 LONG AT FASTENER. BOTH CRACKS WERE STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5261-C-01000.Jun 4, 1998 · N12538 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9800966Floorboard · crackedINSPECTION FOUND FLOORBOARD NR 72 FORWARD LEADING EDGE AND AFT SCREW HOLES CRACKED AND WORN BETWEEN STA 756 AND 832. TWO EACH REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-21, FIGURE 4, 53-01, FIGURE 2, SHEET 3, 51-10-3, AND 51-30-2.Jun 4, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9800965Floorboard · corrodedINSPECTION FOUND FLOORBOARD NR 36 HAD CORROSION AT FOUR SCREW HOLES ON END OF PANEL, STA 389. THE FLOORBOARD WAS REPAIRED IAW SRM 53-01, FIGURE 1, SHEET 2, SRM 53-21-0, AND 51-30-2.Jun 4, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9800964Channel · crackedINSPECTION FOUND A 1 CRACK IN Z-CHANNEL OF RT MLG DOOR FORWARD INNER CORNER. THE CRACKED AREA OF CHANNEL WAS CUT OUT IAW SRM 52-05, FIGURE 14. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 52-05, FIGURE 14.Jun 4, 1998 · N12538 · Doug DC932 · Landing Gear DoorsSDR CALA9800963Pan · crackedINSPECTION FOUND A 1 CRACK IN AFT CARGO DOOR OVERHEAD PAN AT STA 929. THE CRACK WAS STOP DRILLED IAW SRM 53-01. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 53-01.Jun 4, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800962Angle · crackedINSPECTION FOUND A 1 CRACK IN ANGLE OF LT WING FORWARD SIDE AT WING ROOT, WHERE FORWARD SPAR GOES INTO FUSELAGE. THE SEAL BRACKET AND ANGLE AT WING ROOT WERE REMOVED IAW SRM 51-30-3. AN ANGLE WAS FABRICATED IAW SRM 51-10-4. THE ANGLE AND SEAL BRACKET WERE IJun 4, 1998 · N12538 · Doug DC932 · Wing Miscellaneous StructureSDR TWAA9809212Skin · damagedMCI - DURING OP 15 MAINTENANCE CEHCK, THE AFT CARGO DOOR CUTOUT FUSELAGE SKIN WAS DAMAGED AT AFT LOWER EDGE. REPAIRED DAMAGED SKIN PER SRM 54-05 FIG 80, AND TWA STD PRACTICES. (M)Jun 3, 1998 · N920L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9809202Skin · crackedDURING OP-15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN WITH .125 INCH CRACK ON CARGO DOOR CUTOUT EDGE, FS 937 AND L26R. TRIMMED DAMAGED AREA AND CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-05, FIG 8C AND TWA STD PRACTICES. (M)Jun 3, 1998 · N920L · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98640Cover · detachedMKE - FLT 584 - THE GALLEY DOOR SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY SLIDE COVER. (M)Jun 3, 1998 · N204ME · Doug DC932 · Emergency EquipmentSDR MWEA98639Channel · crackedMKE - FOUND CRACK ON VENTRAL DOOR LOWER LEFT DOOR FRAME CHANNEL. MAINTENANCE FABRICATED AND INSTALLED NEW DOOR CHANNEL. (M)Jun 3, 1998 · N204ME · Doug DC932 · Fixed Inner DoorsSDR MWEA98637Cover · detachedMKE - FLT 712 - THE GALLEY DOOR SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE COVER. (M)Jun 3, 1998 · N502ME · Doug DC932 · Emergency EquipmentSDR CALA9800961Panel · crackedINSPECTION FOUND A 3 CRACK IN FORWARD ADF SENSE ANTENNA PANEL. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-2.Jun 3, 1998 · N12538 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9800960Skin · crackedINSPECTION FOUND TWO .0625 INCH CRACKS AT RIVETS IN LT FUSELAGE FORWARD NOSE SECTION EXTERIOR SKIN, STA 695. A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5330-02413 AND DOUGLAS DRAWING SR09530239.Jun 3, 1998 · N12538 · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9800959Bulkhead Angle · crackedINSPECTION FOUND A 2 CRACK IN Z-ANGLE AT LT FORWARD PIT BULKHEAD STA 218, LBL 17. THE CRACK WAS STOP DRILLED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 10.Jun 3, 1998 · N12538 · Doug DC932 · Fuselage Main, BulkheadSDR CALA9800957Support · crackedINSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT OF LT FORWARD CARGO COMPARTMENT, STA 228. THE FLOOR SUPPORT WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, 51-10-3, AND 51-30-2.Jun 3, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800956Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN FORWARD WING TO FUSELAGE FAIRING ATTACH BRACKET AT STA 579. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-3, AND 51-30-5.Jun 3, 1998 · N12538 · Doug DC932 · Aerodynamic FairingsSDR CALA9800955Longeron · crackedINSPECTION FOUND A 3 INCH CRACK IN LONGERON 3L AT STA 140. A LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 17.Jun 3, 1998 · N12538 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9800954Bracket · crackedINSPECTION FOUND A 3 INCH CRACK AT OUTBOARD FORWARD RADIUS OF RT WING NR 2 FORWARD FLAP HINGE FAIRING RETAINING BRACKET. THE BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-10-4, 51-10-2, AND 51-30-2.Jun 3, 1998 · N12538 · Doug DC932 · Trailing Edge FlapsSDR CALA9800953Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 980, RBL 18. THE L-ANGLE, FILLER, AND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4A.Jun 3, 1998 · N12538 · Doug DC932 · Fuselage Main, Floor BeamSDR CA980629019Control Cable · stiff(CAN) ON LANDING ROLL, GEAR DOOR OPEN LIGHT ON, LT GEAR DOOR OPEN CONFIRMED BY TOWER. MAINTENANCE CHECK FOUND CABLE OF LT MAIN GEAR DOOR SEQUENCE STIFF AND TORQUE TUBE RIVET SHEARED. CABLE CLEANED AND LUBRICATED, REPLACED DOOR AND RIVET, FOLLOW-UP CABLE RIGGJun 3, 1998 · Doug DC932 · Landing Gear Door Retract SectionSDR CALA9801095Frame · crackedINSPECTION FOUND A 4.5 INCH CRACK IN FRAME AT STA 180, LONGERON 5L AND 6L. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 36.Jun 2, 1998 · N12538 · Doug DC932 · Fuselage Main, FrameSDR CALA9801094Seat Track · corrodedINSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 610 TO 620. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED, A NEW SECTION OF TRACK, SPLICE AND PLATE WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2.Jun 2, 1998 · N12538 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9800945Longeron · crackedINSPECTION FOUND A 11.25 INCH CRACK IN LONGERON 14R AT STA 955.091. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02, FIGURE 2. LONGERON AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 53-02, FIGURE 18, 51-10-3, 51-30-2, FIGURE 8, AND 51-Jun 2, 1998 · N12538 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9800944Shear Tie · crackedINSPECTION FOUND A .25 INCH CRACK IN SHEAR TIE AT FS 965 BETWEEN STRINGER 13R AND 12R, FORWARD OF AFT LAV. THE CRACK WAS STOP DRILLED, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 28.Jun 2, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800943Support · crackedINSPECTION FOUND A 2.75 INCH CRACK IN LT FORWARD PIT FLOOR SUPPORT AT FS 256, LBL 35. THE CRACK WAS STOP DRILLED AND AN L-ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263, SRM 51-30-2 AND 51-10-3.Jun 2, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800942Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN BRACKET OF RT WING LEADING EDGE PANEL FRAME. THE BRACKET WAS REMOVED, A NEW ANGLE BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 51-30-5.Jun 2, 1998 · N12538 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9800941Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN FORWARD PIT RT INTERCOSTAL FRAME L-ANGLE AT FS 237, RBL 17. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-10-3.Jun 2, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800940Longeron · crackedINSPECTION FOUND A 2 INCH CRACK IN LONGERON 2L AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, SHEET 1, 51-30-2, AND 51-30-5.Jun 2, 1998 · N12538 · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800266Skin · corrodedOUTFLOW VALVE CUTOUT CORRODED BEYOND LIMIT AT STA 900, LT L22. FABRICATED NEW SPLICE FROM 7075T651 IAW DWG 3914675. TREATED, PRIMED AND INSTALLED NEW SPLICE IAW SRM 53-01, FIG 1, 51-10-3, 51-30-5. REINSTALLED FLOOR SUPPORT, FRAME, SPLICE AND STIFFENER IAW DJun 1, 1998 · N935VV · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9800934Frame · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD PIT FRAME AT STA 446, STRINGER 29R. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.Jun 1, 1998 · N12538 · Doug DC932 · Fuselage Main, FrameSDR CALA9800933Doubler · crackedINSPECTION FOUND A 4 INCH CRACK IN CABIN INTERIOR DOUBLER AT BS 598, RBL 55. THE DOUBLER WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30.Jun 1, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800932Web · crackedINSPECTION FOUND CABIN INTERIOR WEB CRACKED AT BS 598, RBL 55. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2.Jun 1, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800931Seat Track · corrodedINSPECTION FOUND RT INBOARD CABIN SEAT TRACK CORRODED AT STA 470 TO 456. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F, AND 53-20-1, PAGE 205.Jun 1, 1998 · N12538 · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR CA980629018Spacer · cracked(CAN) DURING DISASSEMBLY OF A TIME EXPIRED ENGINE, THE FRONT COMPRESSOR ROTOR THIRD TO FOURTH STAGE SPACER WAS FOUND CRACKED. THERE WERE 8 CRACKS EXTENDING FROM THE TIE ROD SLEEVE HOLES TO THE INSIDE, AND THERE WAS ONE SMALL CRACK STARTING FROM THE TIE ROD SLEJun 1, 1998 · Doug DC932 · Turbine Engine Compressor SectionSDR ABXA9800487Battery · dischargedCOCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED POWER SUPPLY BATTERIES.Jun 1, 1998 · N905AX · Doug DC932 · Emergency LightingSDR MWEA98633Cover · fell offTHE FORWARD ENTRANCE DOOR SLIDE COVER ASSEMBLY FELL OFF. MAINTENANCE REINSTALLED SLIDE COVER ASSEMBLY.May 31, 1998 · N207ME · Doug DC932 · Emergency EquipmentSDR MWEA98632Battery Pack · dischargedFOUND THE EMERGENCY LIGHT FROM SEAT ROW 18 AFT INOP. MAINTENANCE REPLACED BATTERIES IN EMERGENCY BATTERY PACK.May 31, 1998 · N602ME · Doug DC932 · Emergency LightingSDR VJ9800265Frame · corrodedFS 503 FRAME LONGERON 29R TO 29L CORRODED BEYOND LIMIT. INSTALLED REPAIR PARTS AND REPAIRED IAW DC9 SRM 53-03 FIG 5 PG 6 AND 53-01 FIG 1.May 30, 1998 · N935VV · Doug DC932 · Fuselage Main, FrameSDR VJ9800183Skin · dentedCUT OUT DENTED SECTION OF LT CENTER NOSE SKIN. FABRICATED NEW SKIN SECTION, INTERNAL DOUBLER AND FINGER DOUBLER AND INSTALLED IAW EO 9-53-003.May 30, 1998 · N948VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800182Skin · dentedREPLACED LOWER RT NOSE CROWN SKIN. CUT OUT DENTED SECTION, ORDERED NEW SECTION, FABRICATED INTERNAL DOUBLER AND FINGER DOUBLER IAW EO 9-53-003. DRILLED, COUNTERSUNK AND INSTALLED SKIN IAW EO 9-53-003.May 30, 1998 · N948VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800181Skin · dentedREMOVE AND REPLACE RT UPPER NOSE CROWN SKIN NOSE SECTION. FABRICATED, DRILLED, COUNTERSUNK AND INSTALLED NEW NOSE SKIN IAW EO 9-53-003.May 30, 1998 · N948VV · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98630Longeron · crackedFOUND CRACK ON LONGERON 5R AT STATION 639. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR.May 30, 1998 · N302ME · Doug DC932 · Fuselage Main, Longeron/Stringer
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