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 VJ9800060Skin · corrodedEXTERIOR FUSELAGE SKIN AT AFT UPPER ADF ANTENNA CORRODED. BLENDED CORROSION AND REMOVED OUT OF LIMITS AREA. FABRICATED, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS AT UPPER FWD AND AFT ADF LOOP ANTENNA IAW DC9 SRM 53-04, FIG 29, AND AERO EMar 24, 1998 · N917VV · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9809310Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE FRAME STA 89 WITH CRACK IN OUTBOARD RADIUS BETWEEN LONGERONS 18 AND 19. STOP DRILLED CRACK PER SRM 51-10 AND REPAIRED PER SRM 53-01, PAGE 10, FIGURE 2. (X)Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, FrameSDR TWAA9807318Spar Cap · crackedMCI - DURING OP 16 MAINTENANCE CEHCK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HOLES. STOP DRILLED CRACK, REPAIRED PER DAC DWG J060271 AND STD PRACTICES. (M)Mar 23, 1998 · N929L · Doug DC932 · Wing SparSDR TWAA9807317Longeron · brokenMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L BROKEN JUST FORWARD OF FORMER 160. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M)Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9807316Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L CRACKED AT STATION 200. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M)Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9807309Floorbeam · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION ON FLOORBEAM CAP AT FS 160 FROM OL-288. REPLACED FLOORBEAM CAP PER SRM 51-01, PAGE 1 ITEM 1C. SEALED PER SRM 91-20-0. (M)Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9807204Spar Cap · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HOLES. STOP DRILLED CRACK. REPAIRED PER DAC DWG J060271 AND STANDARD PRACTICES. (M)Mar 23, 1998 · N997Z · Doug DC932 · Wing SparSDR TWAA9806809Window Frame · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND CABIN WINDOW 23L HAD WINDOW TO FRAME TIE CRACKED. REPLACED WITH NEW FRAME PER SRM 51-10-1, PAGE 1 ITEM C. (M)Mar 23, 1998 · N997Z · Doug DC932 · Passenger Compartment WindowsSDR TWAA9805003Longeron · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON LONGERON 23L, STATION 945 TO 950. REMOVED CORROSION PER SRM 51-10-03. INSTALLED NEW PART PER SRM 51-01 PAGE 1 ITEM C. (M)Mar 23, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800089Intercostal · corrodedLOWER LEG OF INTERCOSTAL AT FS 980, L28R, CORRODED. FABRICATED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW DC9 SRM 51-30-1, 51-10-2 AND 51-10-3.Mar 22, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800088Sub Floor · corrodedSUB FLOOR UNDER GALLEY WATER LINE DRAIN FS 148 TO 160, BL 43R-58R, CORRODED BEYOND LIMITS IAW DC9 SRM 53-01, FIG 1. FABRICATED SUB FLOOR PANEL, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2, 51-30-2 AND 51-10-3.Mar 22, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800087Angle · corrodedFLOORBOARD ATTACH ANGLES FS 160 TO 220, BL 55L - BL55R, Z=0, CORRODED BEYOND LIMITS. FABRICATED NEW ANGLES, TREATED, PRIMED AND INSTALLED NEW ANGLES IAW DC9 SRM 51-10-3, 51-30-1, 51-30-2 AND 53-01 FIG 1.Mar 22, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800054Switch · failedDURING FLT, SMOKE COMING FROM THE WING LANDING LIGHT SWITCHES WHEN POSITIONED TO EXT AND ON. SMOKE SUBSIDED WHEN SWITCHES WERE TURNED OFF. REPLACED THE SWITCH. OPS CHECKED GOOD. (M)Mar 22, 1998 · N907VJ · Doug DC932 · Exterior LightingSDR TWAA9806104Longeron · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 23L CORRODED, STATION 945 TO 950. REMOVED CORROSION PER SRM 51-10-03. INSTALLED NEW PART PER SRM 51-01, PG 1 ITEM C. (M)Mar 22, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9804819617Wire · brokenDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 5, 6, AND 7 INOPERATIVE. REPAIRED BROKEN WIRE AT ROW 7 LIGHTS, OPERATIONAL CHECK NORMAL.Mar 22, 1998 · N617NW · Doug DC932 · Light System WiringSDR VJ9800171Web · corrodedSTATION 996 LOWER WEBS HAVE EXTENSIVE CORROSION THROUGH OUT. LOWER CAP HAS CORROSION. FABRICATED LOWER WEBS FROM 7075 T6 .040 BY 9.5 BY 61 BY 12 BY 22 2 EACH. INSTALLED IAW DC-9 SRM 51-10-4, 51-30-5, AND 51-10-3.Mar 21, 1998 · N967VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800052Light · inoperativeMAIN CABIN DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECKED GOOD IAW MM 33-50. (M)Mar 21, 1998 · N948VV · Doug DC932 · Emergency LightingSDR VJ9800058Fitting · gougedATTACH FITTING RT WING, NR 1 SLAT MAIN TRACK (CENTER), GOUGED. BLENDED AREA IAW DC9 SRM 53-01, FIG 1. BLEND DEPTHS WITHIN LIMITS PER RES 1 1668, TREATED AREA IAW SRM 51-10-3 AND AERO EO 98-822, COMPLETED FORM 8110-3. (M)Mar 20, 1998 · N917VV · Doug DC932 · Leading Edge DevicesSDR MWEA98374Slide · fell offTHE GALLEY SLIDE CAME UNATTACHED UPON ARRIVAL. MTC REINSTALLED GALLEY SLIDE.Mar 20, 1998 · N204ME · Doug DC932 · Emergency EquipmentSDR MWEA98372Skin · crackedFOUND CRACK ON FORWARD PASSENGER DOOR LOWER EDGE AFT CORNER OF OUTER SKIN. MTC INSTALLED INTERNAL DOUBLER REPAIR.Mar 20, 1998 · N202ME · Doug DC932 · Passenger/Crew DoorsSDR 9804789925Line · brokenLOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE OCCURRED IMMEDIATELY AFTER GEAR RETRACTION. NOSE GEAR RETRACTED NORMALLY BUT BOTH MAIN GEARS WERE STILL EXTENDED WITH GEAR DOOR OPEN LIGHT ILLUMINATED. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENMar 20, 1998 · N925US · Doug DC932 · Hydraulic System, MainSDR TWAA9809406Spar · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TRAILING EDGE INBD FLAP REAR SPAR, INBD FLAP CASTING MOUNT HOLE LOWER INBD HOLE, WITH CRACK EXTENDING INTO RADIUS ON FWD SIDE OF FUEL TANK. SPLICED SECTION OF LOWER SPAR FROM STA XRS 111.510 TO XRS 195.210, Mar 19, 1998 · N997Z · Doug DC932 · Wing SparSDR TWAA9807303Spar · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TE INBOARD FLAP REAR SPAR INBOARD FLAP CASTING MOUNT HOLE, LOWER INBOARD HOLE, WITH CRACK EXTENDING INTO RADIUS FORWARD SIDE OF FUEL TANK. SPLICED SECTION OF LOWER SPAR FROM STATION XRS 111.510 TO XRS 195.21Mar 19, 1998 · N997Z · Doug DC932 · Trailing Edge FlapsSDR TWAA9806922Longeron · crackedMCI - DURING OP15 MAINTENANCE CHECK, FOUND LONGERON 14R AT STATION 1076 WITH CRACKED FORMER. REPAIRED FRAME PER SRM 53-03, FIG 4, AND STANDARD PRACTICES. (M)Mar 19, 1998 · N997Z · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98371Cover · fell offTHE FORWARD ENTRANCE SLIDE POPPED OFF. MTC REINSTALLED SLIDE COVER.Mar 19, 1998 · N602ME · Doug DC932 · Emergency EquipmentSDR 9804769982Compressor · stalledDURING TAKEOFF ROLL AT 80 KNOTS, THE LEFT ENGINE EXPERIENCED COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE, OPERATIONAL CHECK OK.Mar 19, 1998 · N982US · Doug DC932 · Turbine Engine Compressor SectionSDR 9804689606Engine · failedAS TAKEOFF POWER WAS APPLIED, A NOISE WAS HEARD FOLLOWED BY VIBRATIONS FROM THE RIGHT ENGINE. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE, OPERATIONAL CHECK OK.Mar 19, 1998 · N606NW · Doug DC932 · Engine (Turbine/Turboprop)SDR VJ9800086Sub Floor · corrodedSUB FLOOR FS 160 TO 175, X20L, Z=0, CORRODED. FABRICATED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800085Sub Floor · corrodedSUB FLOOR BULGED AT FS 200, X48L, Z=0. REMOVED, TREATED, PRIMED AND INSTALLED SUB FLOOR IAW DC9 SRM 51-10-2, 51-10-3, AND 51-30-2.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800084Angle · corrodedFLOOR ATTACH UPPER FLANGE FS200, X 0-22R, CORRODED. FABRICATED FLOOR SUPPORT IAW DC9 SRM 51-10-1 AND 51-10-4. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800083Sub Floor · corrodedSUB FLOOR FS 200, X46-53R, CORRODED. FABRICATED, TREATED AND PRIMED NEW SUB FLOOR IAW DC9 SRM 51-10-2, 51-10-3 AND 51-30-2.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800082Sub Floor · corrodedSUB FLOOR WEB AT FS 168, X54R, Z0, CORRODED. FABRICATED, TREATED AND PRIMED NEW SUB FLOOR IAW DC9 SRM 51-10-2, 51-10-3 AND 51-30-2.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800081Seat Track · corrodedSEAT TRACK, FS 200 TO 230, BL 45L, CORRODED. REPLACED SEAT TRACK FROM FS 200 TO 230, BL 45L IAW DC9 SRM 53-05, FIG 4D, 51-30-1 AND 51-30-2.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800080Seat Track · corrodedSEAT TRACK FS 245, BL 44.5R, CORRODED. REPLACED SEAT TRACK SPLICE IAW DC9 SRM 51-30-1, 51-30-2 AND 53-05.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800079Seat Track · corrodedSEAT TRACK FS 200 TO 245, BL 44.5R, CORRODED. REPLACED SEAT TRACK FROM FS 200 TO 245, BL 44.5R, IAW DC9 SRM 51-30-1, 51-30-2 AND 53-05.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800078Seat Track · corrodedSEAT TRACK FS 200 TO 220, BL 22L, CORRODED. REPLACED SEAT TRACK FROM FS 200 TO 325 IAW DC9 SRM 51-30-1 AND 53-05.Mar 18, 1998 · N905VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR VJ9800051Battery Charger · inoperativeEMERGENCY LIGHTS INOP FROM ROWS 24 BACK INTO TAIL COMPARTMENT. REPLACED AFT CEILING BATTERY CHARGER.Mar 18, 1998 · N921VV · Doug DC932 · Emergency LightingSDR VJ9800049Battery Pack · dischargedFORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPS CHECKED NORMAL IAW MM 33-50-0.Mar 18, 1998 · N939VV · Doug DC932 · Emergency LightingSDR MWEA98370Battery Pack · discharegdTHE FIRST SECTION OF FLOOR TRACK LIGHTING WOULD NOT LIGHT UP. MAINTENANCE REMOVED AND REPLACED FIRST SECTION FLOOR TRACK EMERGENCY BATTERY PACK.Mar 18, 1998 · N301ME · Doug DC932 · Emergency LightingSDR MWEA98359Clips · crackedFOUND THE AFT PRESSURE BULKHEAD RT RADIAL FORMER CRACKED ON OUTBOARD END. MTC TRIMMED OUT FORMER AND FITTED WITH NEW CLIPS.Mar 18, 1998 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98358Door Pan · gougedFOUND THE LT AND RT AFT OVERWING EXIT DOOR FRAME PANS GOUGED AT TOP CENTER AREA. MTC BLENDED GOUGES AND FABRICATED REPAIR DOUBLERS AND INSTALLED.Mar 18, 1998 · N207ME · Doug DC932 · Emergency ExitsSDR MWEA98357Intercostal · crackedFOUND CRACK ON INTERCOSTAL BOTTOM FLANGE LT SIDE FUSE STA 1132.60 TO 1143.01. MTC FABRICATED DOUBLER AND INSTALLED.Mar 18, 1998 · N207ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA98356Pan · crackedFOUND CRACK AROUND UPPER LT DOOR STOP ON AFT VENTRAL DOOR. MTC REMOVED AND REPLACED PAN.Mar 18, 1998 · N207ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA98355Angle · crackedFOUND CRACK ON NR 3 BEAM ON RT SIDE OF AFT VENTRAL DOOR. MTC REMOVED AND REPLACED ANGLE.Mar 18, 1998 · N207ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA98354Skin · corrosionFOUND MODERATE CORROSION ON LT SIDE AFT ACCESSORY COMPARTMENT FUSE SKIN STA 1130. MTC REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER.Mar 18, 1998 · N207ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98353Blkhd Doubler · crackedFOUND A RADIAL CRACK ON AFT PRESSURE BULKHEAD DOOR JAMB UPPER LEFT CORNER OF -13 DOUBLER. MTC REMOVED AND REPLACED -13 DOUBLER.Mar 18, 1998 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98352Blkhd Skin · crackedFOUND VERTICAL CRACK ON AFT PRESSURE BULKHEAD UPPER LEFT CORNER OF VENTRAL DOOR JAMB ON 3 WEB SKIN. MTC SPLICED NEW 3 SECTION SKIN.Mar 18, 1998 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98351Jamb · crackedFOUND CRACK IN AFT PRESSURE BULKHEAD FORWARD SIDE UPPER LEFT CORNER OF DOOR JAMB ON JAMB FLANGE. MTC SPLICED NEW JAMB SECTION.Mar 18, 1998 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA98350Jamb · crackedFOUND CRACK ON AFT VENTRAL DOOR JAMB WEB LEFT SIDE. MTC SPLICED IN NEW SECTION WITH DOUBLER AND FILLER.Mar 18, 1998 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR CALA9800482Switch · inoperativeTHE LEFT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF FROM ABQ. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ON. THE FLIGHT WAS CONTINUED TO IAH WITH PUMPS IN HIGH AND WHEN GEAR WAS EXTENDED INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE OVERLINK SWITCH. Mar 18, 1998 · N18513 · Doug DC932 · Landing Gear Position and Warning
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