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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MWEA98487Door Slide · fell offTHE GALLEY DOOR SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE.SDR MWEA98486Slide Cover · fell offTHE GALLEY DOOR EMERGENCY DOOR SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER.SDR MWEA98470Intercostal · damagedAN INTERCOSTAL AT LONGERON 26 RIGHT LOCATED FROM FUSELAGE STATION 937 TO 945 HAS DOUBLE DRILLED HOLES. MTC REMOVED DAMAGED PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA.SDR MWEA98469Intercostal · damagedAN INTERCOSTAL AT LONGERON 25 RIGHT AT FUSELAGE STATION 937 TO 945 HAS DOUBLE DRILLED HOLES. REMOVED DAMAGED PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA.SDR MWEA98468Intercostal · damagedAN INTERCOSTAL AT LONGERON 25R AT FUSELAGE STATION 889 TO 897 HAS DOUBLE DRILLED HOLES. REMOVED DAMAGED PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA.SDR MWEA98467Intercostal · damagedTHE INTERCOSTAL LOCATED ON LONGERON 29 RIGHT FROM FUSELAGE STATION 897 TO 937 WAS IMPROPERLY MADE. MTC REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA.SDR MWEA98466Intercostal · mismanufacturedINTERCOSTAL AT FUSELAGE STATION 907 FROM LONGERON 29R TO 28R IS OF THE WRONG INTERCOSTAL THICKNESS. REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROACH DATA.SDR MWEA98465Intercostal · damagedTHE INTERCOSTAL AT FS 926 BETWEEN LONGERON 28R AND 29R HAS ELONGATED FASTENER HOLES. MTC REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA.SDR MWEA98464Jamb Pan · corrodedTHE AFT CARGO DOOR CUTOUT JAMB PAN WAS FOUND CORRODED AROUND THE LOWER AREA. MTC REMOVED DAMAGED SECTION INSTALLED REPAIR SECTION USING APPROVED DATA.SDR MWEA98463Splice · corrodedTHE WEB SPLICE AT FUSELAGE STATION 996 IS CORRODED THROUGH. MTC REMOVED OLD SPLICE OBTAINED NEW SPLICE AND INSTALLED SPLICE.SDR MWEA98462Shear Tie · crackedA SHEAR TIE WAS FOUND CRACKED AT FUSELAGE STATION 996. MTC REMOVED OLD SHEAR TIE AND INSTALLED NEW SHEAR TIE.SDR MWEA98461Fitting · corrodedTHE AFT JACK POINT FITTING IS CORRODED. REMOVED AND REPLACED AFT JACK FITTING.SDR MWEA98460Bulkhead Angle · corrodedTHE 996 BULKHEAD LOWER TEE ANGLE WAS FOUND CORRODED. REMOVED AND REPLACED TEE ANGLE.SDR MWEA98459Longeron · corrodedLONGERON 23 RIGHT WAS FOUND CORRODED FROM FUSELAGE STATION 945 TO 996. MTC REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT LONGERON.SDR MWEA98458Doubler · corrodedTHE DOUBLER LOCATED AT LONGERON 22 LEFT JUST FORWARD OF FRAME STATION 965 IS CORRODED. REMOVED AND REPLACED DOUBLER.SDR MWEA98457Fitting · corrodedDURING SKIN REPLACEMENT LONGERON 25 RIGHTS END FITTING AT FUSELAGE STATION 996 WAS FOUND CORRODED. REMOVED AND REPLACED FITTING.SDR ABXA9800358Switch · defectiveWHEN LANDING GEAR WAS PLACED DOWN, THREE GREEN LIGHTS AND THE GEAR DOOR OPEN LIGHT REMAINED ON. REPLACED MAIN LANDING GEAR DOOR POSITION SWITCH.SDR TWAA9806616Panel · tornMCI - DURING OP 16 MAINTENANCE CHECK, FOUND TOP TE PANEL ON RUDDER SEPARATED AND TORN AT JOINT SEAMS. REPAIRED PER SRM 51-90-0. (M)SDR TWAA9806601Skin · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WITH CRACK AT LOWER AFT FASTENER IN LE ABOVE LE PANEL NR 1211A. INSTALLED NEW RIB PER SRM 51-01 PAGE 1. (M)SDR TWAA9806515Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED RIB PER SRM 51-01, PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)SDR TWAA9806514Floorbeam · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STA 937 TO STA 965, CABIN FLOORBEAM CAP WITH METAL REMOVED BEYOND LIMITS FOR CORROSION REMOVAL. INSTALLED NEW SECTION AT FLOOR SUPPORT PER SRM 53-05, P21, ITEM 6A, AND ARA 10993. ACFT TT: 75,041 HOURS. ACFT TCSDR TWAA9806413Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED PART PER SRM 51-01, PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TC: 81,086.SDR TWAA9806412Barrel Nut · rustedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT RT BARREL NUT IN FRONT SPAR FOR STABILIZER ATTACH TO CENTER SECTION WAS RUSTY AND EMITTING RUST FROM BOTTOM OF HOLE. REMOVED BOLT AND BARREL NUT AND CLEANED. REAMED AND BUSHED HOLE PSDR TWAA9806410Support · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND METAL REMOVED BEYOND LIMIT FOR CORROSION REMOVAL AT CABIN STA 937 TO STA 965, CENTER FLOOR CAP. INSTALLED NEW SECTION AT FLOOR SUPPORT PER SRM 53-05, P21, 6A, AND ARA 10993. ACFT TT: 75,041 HOURS. ACFT TC: 81,08SDR TWAA9806409Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE HAD CRACK AT LOWER AFT FASTENER IN LE RIB ABOVE LE PANEL NR 1211A. INSTALLED NEW RIB PER SRM 51-01, PAGE 1. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)SDR 9807389605Bulkhead Doubler · crackedDURING LINE CHECK, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD -13 DOUBLER ABOVE THE LEFT DOOR STOP FITTING. REPAIRED PER EA 96-156476.SDR MWEA98445Skin · damagedFORWARD LOWER BELLY SKIN WAS DAMAGED DURING MAINTENANCE. THE SKIN WAS REMOVED FROM FS 229 TO FS 265 LONGERON 26L TO 26R, A REPLACEMENT SKIN WAS SPLICED IN USING APPROVED DATA.SDR MWEA98444Skin · crackedAT FUSELAGE STATION 980 LONGERON 16 RIGHT A SMALL CRACK WAS FOUND IN THE FUSELAGE SKIN. REPAIRED SKIN USING APPROVED DATA.SDR MWEA98443Frame · chafedEXTERIOR FUSELAGE THE FRAME FUSELAGE STATION 1038 WAS FOUND DEEPLY CHAFED AND CORRODED. BLENDED CORROSION, FABRICATED AND INSTALLED REPAIR STRAP USING APPROVED DATA.SDR MWEA98442Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED, BULGING AND HAS RIVETS WITH PULLING HEADS. MTC BLENDED CORROSION AND FOUND SKIN OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER USING APPROVED DATA.SDR MWEA98441Doubler · corrodedAN INTERNAL DOUBLER WAS FOUND CORRODED AT FUSELAGE STATION 996 LONGERON 23 LEFT. MTC REMOVED OLD DOUBLER FABRICATED AND INSTALLED REPLACEMENT DOUBLER USING APPROVED DATA.SDR MWEA98440Doubler · corrodedEXFOLIATION WAS FOUND ON A DOUBLER BETWEEN FUEL DRAIN VALVE AND BOTTOM OF LEFT WING. REMOVED CORRODED DOUBLER FABRICATED AND INSTALLED REPLACEMENT DOUBLER USING APPROVED DATA.SDR MWEA98439Skin · gougedFUSELAGE SKIN WAS FOUND GOUGED AT FUSELAGE STATION 208 LONG 18 RIGHT. MTC BLENDED GOUGE AND REPAIRED AREA USING APPROVED DATA.SDR MWEA98438Fitting · corrodedOUTBOARD SLAT TRACK FITTING CORRODED AT WING STATION 240 RIGHT WING. MTC REMOVED AND REPLACED SLAT TRACK FITTING USING APPROVED DATA.SDR MWEA98437Fitting · corrodedINBOARD SLAT TRACK FITTING AT XRS 240 RT WING WAS FOUND CORRODED. MTC REMOVED AND REPLACED INBOARD FITTING USING APPROVED DATA.SDR MWEA98436Clip · crackedRIGHT WING UPPER ATTACH CLIP CRACKED AT STATION XRS 69 WEB BETWEEN 31 AND 32 STRINGERS. MTC REMOVED OLD CLIP FABRICATED AND INSTALLED REPLACEMENT USING SERVICEABLE DATA.SDR ABXA9800356Window · lack of lubeCAPTAIN'S SLIDING CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEAR VIEW WINDOW IAW DC9 MM.SDR 9906689986Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE OVERHEAD EMERGENCY LIGHT DIM. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR 9806689986Battery Pack · dischargedDURING LINE INSPECTION, FOUND TAIL CONE OVERHEAD EMERGENCY LIGHT DIM. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR TWAA9809304Bulkhead · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND 1104 CANTED BULKHEAD AT NR 3 LONGERON RT AND LT SIDE, WITH 2 EACH FASTENERS MISSING. HFEC AREA FOUND 2 INCH CRACK. REPAIRED PER SRM 53-05, PAGE 49. (X)SDR TWAA9809301Bulkhead Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT PYLON UPPER AFT BULKHEAD ANGLE CRACKED AT INBOARD AND OUTBOARD ENDS. MADE AND INSTALLED NEW ANGLE PER SRM 51-01, PAGE 1, ITEM C. (X)SDR TWAA9807320Fitting · flat spotMCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZ STABILIZER LEFT PIVOT BEARING LUG, IN LT SIDE OF STAB CENTER SECTION RIB, WITH FLAT SPOT IN BEARING BORE AT APPROX 3 O'CLOCK POSITION, .017 IN DEEP AND LUG IS .010 IN THICKER AT TOP 12 O'CLOCK POSITION AT SPOT SDR TWAA9807202Skin · corrodedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN BENEATH DOOR THRESHOLD HAD CORROSION AT STATION 916 TO 945, L29R TO L27R. REPAIRED AS PER ARA 15272 AND STD PRACTICES. (M)SDR MWEA98435Fuel Panel · corrosionRIGHT WING LOWER FUEL PANEL NR 1456 HAS CORROSION AROUND AND INSIDE COUNTERSUNK HOLES AND ON BOTTOM SIDE. MTC REMOVED AND REPLACED FUEL PANEL WITH SERVICEABLE UNIT.SDR MWEA98434Frame · crackedTHE CANTED FRAME AT FUSELAGE STATION 1143 HAD AN IMPROPER REPAIR. REPAIRED FRAME USING APPROVED DATA.SDR MWEA98433Spar · damagedTHE RIGHT WING FORWARD LOWER SPAR CAP HAS AN UNDOCUMENTED REPAIR. MTC REPAIRED SPAR CAP USING APPROVED DATA.SDR MWEA98432Skin · damagedFUSELAGE SKIN IS DENTED AND GOUGED AT FS 978. ALSO, A CRACK WAS FOUND IN SKIN. REPAIRED FUSELAGE SKIN USING APPROVED DATA.SDR MWEA98431Floorbeam · corrodedTHE FLOORBEAM AT FUSELAGE STATION 237 RIGHT BOTTLINE 41 WAS FOUND CORRODED. MTC REMOVED CORROSION AND REPAIRED FLOORBEAM.SDR MWEA98430Longeron · crackedLONGERON 16 RIGHT WAS FOUND CRACKED AT FS 980. MTC REMOVED OLD PART FABRICATED AND INSTALLED REPAIR SECTION OF LONGERON.SDR MWEA98429Splice · damagedCENTER WING TANK SPLICE ON STRINGER NR 15 HAS TOOLING DAMAGE. MTC REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT PART.
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