Douglas DC-9-31
Service difficulty reports · 7,433
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 = 'DC931' 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 = 'DC931' 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 USAA951098Blkhd Skin · crackedPIT - DURING B-CHECK INSPECTION, FOUND .25 INCH BY .5 INCH BY .022 DEEP CHAF MARK, AFT PRESSURE BULKHEAD AFT SIDE LEFT BULKHEAD SKIN. INSTALLED .063 DOUBLER AND .025 FINGER DOUBLER PER USAIR EA NR 31415.SDR ABXA9600292Angle · crackedDURING C-CHECK INSPECTION, THE VERTICAL FLOOR SUPPORT ATTACH ANGLE WAS FOUND CRACKED AT STA 965R. REPLACED IAW DC-9 SRM 51-30-5 AND 51-30-1.SDR ABXA9600291Angle · crackedDURING C-CHECK INSPECTION, THE VERTICAL FLOOR SUPPORT ATTACH ANGLE WAS FOUND CRACKED AT STA 965L. REPLACED IAW DC-9 SRM 51-30-5 AND 51-30-1.SDR ABXA9500751Eel Battery · dischargedDURING PRE-FLIGHT INSPECTION, FOUND THE EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED THE NICAD BATTERIES IN THE EMERGENCY LIGHT POWER SUPPLY PACK IAW DC-9 SUPP. M.M. 33-53-0.SDR 9515259991Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN BOTH FS 69 PRESSURE PANEL TO WHEEL WELL WEB ATTACH FITTINGS. REPLACED FITTINGS PER SRM 51-01.SDR 9516379967Blkhd Web · oil cannedDURING H-CHECK, FOUND OIL CANNING IN THE FS 965 PYLON BULKHEAD WEB, LEFT SIDE. REPAIRED WEB (P/N 9912243-3), PER EA 99-103284.SDR 9515049929Engine · low powerDURING TAKEOFF, THE NR 1 ENGINE DID NOT REACH TAKEOFF POWER. ABORTED TAKEOFF AND RETURNED TO THE GATE. RERIGGED AND TRIMMED BOTH ENGINES AND OPERATIONAL CHECK GOOD.SDR 9514969973Pt7 Tube · brokenDURING TAKEOFF ROLL, LEFT ENGINE EPR DECAYED TO APPROXIMATELY 1.6. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED BROKEN PT7 LINE ON LEFT ENGINE. OPERATIONAL CHECK OK ON ENGINE RUN AND AIRCRAFT RETURNED TO SERVICE.SDR 9514959973Epr Ind/Trans · malfunctionedDURING TAKEOFF ROLL, LEFT ENGINE EPR WAS FROZEN AT 1.6 TO 1.7. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED LEFT ENGINE EPR INDICATOR AND TRANSMITTER. OPERATIONAL CHECK OK ON ENGINE RUN AND AIRCRAFT RETURNED TO SERVICE.SDR 9519089946Angle · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE NOSE GEAR FORWARD LEFT DOOR JAMB INNER ANGLE FS 43. REPAIRED ANGLE PER EA 99-102962.SDR 9515219946Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS AND CORROSION IN THE FS 980 TO 996 FLOORBEAM END FITTINGS, LEFT AND RIGHT SIDES. REPLACED ALL FOUR FITTINGS PER SRM 51-01.SDR ABXA9600281Skin · damagedDURING C-CHECK INSPECTION, A PRIOR REPAIR ACCOMPLISHED IAW ABX REA D953-07841-MR REQUIRED INSPECTION. INSPECTED AND REPAIRED IAW ABX REA D953-12979-MR.SDR 9515199967Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE FS 996 FLOORBEAM END FITTING AT THE RIGHT CUSP. REPLACED FITTING PER SRM 51-30.SDR ABXA9600294Skin · corrodedDURING C-CHECK INSPECTION, THE SKIN AT THE LOWER CENTER OF THE AFT LOWER CARGO DOOR WAS FOUND CORRODED. REPAIRED IAW ABX REA D953-12971-MR.SDR ABXA9600293Doubler · corrodedDURING C-CHECK INSPECTION, THE DOUBLER AT THE LOWER CENTER OF THE AFT LOWER CARGO DOOR WAS FOUND CORRODED. REPAIRED THE DOUBLER IAW ABX REA D953-12971-MR.SDR 9515179967Hinge Ftg · corrodedDURING H-CHECK, FOUND CORROSION IN THE NR 3 FORWARD FLAP HINGE BEARING RETAINER PLATE FASTENER HOLES. REPLACED HINGE FITTING (P/N 5919217-502), PER CITEXT 09-5740-1-9800.SDR 9515159946Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 26L END FITTINGS AT FS 996. REPLACED FITTING PER SRM 51-01.SDR USAA951094Angle · crackedPIT - DURING RON CHECK, 1.25 INCH RUNNING FORE AND AFT AT AFT PASSENGER DOOR FLOOR SILL PLATE SUPPORT ANGLE. INSTALLED DOUBLER REPAIR PER USAIR EA NR 28484A AND SRM 53-05 FIG 40. (M)SDR ABXA9600290Spar Web · crackedDURING COMPLIANCE OF AD 90-18-03; SB 57-129: REV 4, FOUND CRACK INDICATION PER STEP 2B, ON THE RIGHT WING WEB. REPLACED SPAR WEB IAW EA AD-57-03636-MA.SDR ABXA9600289Doubler · crackedDURING COMPLIANCE OF AD 90-18-03, SB 57-129: REV 4, FOUND CRACK INDICATION PER STEP 2B, ON THE RIGHT WING DOUBLER. REPLACED RIGHT WING DOUBLER IAW EA AD-57-03636-MA.SDR 96ZZZX1861Longeron · corrodedDURING C- AND D-CHECK, FOUND LONGERON 24L AT STA 996, AFT SIDE OF PRESSURE BULKHEAD IS CORRODED. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1860Frame · crackedDURING C- AND D-CHECKS, FOUND LEFT WHEELWELL SUPPORT FRAME CRACKED, STA 714. REPAIRED IAW DC9 SB 53-100. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1859Angle · corrodedDURING C- AND D-CHECKS, FOUND AFT CARGO COMPARTMENT FLOOR ATTACH ANGLE AND SUPPORT BEAM CORRODED, FS 956 - FS 996. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1858Angle · corrodedDURING C- AND D-CHECKS, FOUND FLOOR ATTACH ANGLE CORRODED, AFT CARGO COMPARTMENT, STA 917 - STA 956, LONGERON 27L. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1857Structure · corrodedDURING C- AND D-CHECKS, FOUND INTERCOSTAL, SKIN, AND LONGERON CORRODED AT AFT CARGO COMPARTMENT LONGERON 29R. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1856Vane · delaminatedDURING C- AND D-CHECKS, FOUND LEFT WING MOST INBOARD UPPER MOVEABLE FLAP VANE IS DELAMINATED. REPLACED VANE, PN 5912068-501. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1855Intercostal · corrodedDURING C- AND D-CHECKS, FOUND INTERCOSTAL CORRODED, FORWARD CARGO COMPARTMENT, STA 579 - STA 598. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1854Intercostal · corrodedDURING C- AND D- CHECKS, FOUND LONGERON 11L AND INTERCOSTAL AT STA 598-617 CORRODED. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1853Floor · damagedDURING C- AND D-CHECKS, FOUND E AND E COMPARTMENT, CABIN FLOOR AREA JUST ABOVE SERVO DRIVE UNIT CORRODED. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1852Vane · delaminatedDURING C- AND D-CHECKS, FOUND RIGHT WING INBOARD MOVEABLE FLAP VANE DELAMINATED. REPLACED VANE, PN 5910040-1. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1851Vane · delaminatedDURING C- AND D-CHECKS, FOUND RIGHT WING INBOARD MOVEABLE FLAP VANE DELAMINATED. REPLACED VANE, PN 5912168-506. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1850Floor Beam · corrodedDURING C- AND D-CHECKS, FOUND FLOOR BEAM CORRODED, STA 965. REPAIRED IAW DC9 SRM CH 53. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1849Skin · delaminatedDURING C- AND D-CHECKS, FOUND RIGHT WING INBOARD SPOILER DELAMINATED. REPLACED SPILER, PN 5910053-2. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1848Hinge Fitting · crackedDURING C- AND D-CHECKS, FOUND RIGHT WING/AILERON OUTBOARD HINGE FITTING CRACKED. REPLACED FITTING. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1847Skin · delaminatedDURING C- AND D-CHECKS, FOUND RIGHT WING AILERON OUTBOARD TAB DELAMINATED. REPLACED TAB, PN 5910051-502. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1846Skin · delaminatedDURING C- AND D-CHECKS, FOUND LEFT WING AILERON TRIM TAB DELAMINTED. REPLACED TAB, PN 5910051-501. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1845Butt Door · delaminatedDURING C- AND D-CHECKS, FOUND LEFT WING NR 2 BUTT DOOR DELAMINATED. REPLACED DOOR, PN 59195723. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1844Vane · delaminatedDURING C- AND D-CHECKS, FOUND LEFT WING FLAP OUTBOARD MOVEABLE VANES DELAMINATED. REPLACED VANE, PN 5910043-509. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1843Vane · delaminatedDURING C- AND D-CHECKS, FOUND LEFT WING FLAP CENTER MOVEABLE VANE IS DELAMINATED. REPLACED VANE, PN 5910042-503. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1842Skin · delaminatedDURING C- AND D-CHECKS, FOUND RUDDER TAB DELAMINATED. REPLACED RUDDER TAB, PN 5910257. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 96ZZZX1841End Rib · crackedDURING C- AND D-CHECKS, FOUND RIGHT MOVEABLE FLAP VANE END RIB CRACKED. REPLACED VANE, PN 5910041-501. AIRCRAFT TT: 51,653. AIRCRAFT TC: 57,610.SDR 9514799980Switch · malfunctionedDLH - DURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED FOR LANDING. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. REPLACED THE LEFT MAIN GEAR DOOR SWTICH ASDR 9514489945Indication · malfunctionedDURING APPROACH INTO MSP, AFTER SLATS AND FLAPS WERE EXTENDED FOR LANDING, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLAT EXTENDED LIGHT. SLATS WERE VISUALLY CONFIRMED TO BE IN EXTENDED POSITION AND AIRCRAFT LANDED WITHOUT INCIDENT. EMERGENCY EQUIPMENSDR USAA951076Beltframe · crackedPIT - DURING C-1 CHECK INSPECTION, FOUND TWO .5 INCH BY .5 INCH CRACKS, FRAME STATION 1076 AT BOTH LONGERON NR 12 ATTACH FITTINGS. REMOVED DAMAGED SECTION OF BELTFRAME AND INSTALLED FILLER AND DOUBLERS PER SRM 53-03 FIG 34 SHEET 4. (M)SDR USAA951075Longeron · crackedPIT - DURING C-1 CHECK INSPECTION, FOUND .75 INCH CRACK AT STATION 680, LONGERON 6L. REMOVED DAMAGED SECTION OF LONGERON AND SPLICED IN A NEW SECTION PER SRM 53-02. (M)SDR USAA951071Angle · crackedPIT - DURING C-1 CHECK INSPECTION, FOUND .5 INCH CRACK RIGHT FORWARD DORSAL FIN DRAG ANGLE AT APPROXIMATELY STATION 1059. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04 FIG 38. (M)SDR 9514899989Fitting · crackedDURING LINE CHECK, FOUND A CRACK IN THE UPPER AFT CARGO DOOR STOP FITTING, FORWARD CARGO DOOR JAMB. REPLACED FITTING PER SRM 51-30-2.SDR 9514779914Door · missingGRR-DTW - ON ARRIVAL, FOUND THE RIGHT SIDE APU DOOR AND FUEL SHROUD DRAIN MAST WERE MISSING, WITH DAMAGE TO THE APU DOOR JAMB. THE FLIGHT CREW REPORTED NO EFFECT EN ROUTE. REPLACED THE APU DOOR, DRAIN MAST AND REPAIRED THE DOOR JAMB.SDR 9514739949Mount · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT ENGINE AFT MOUNT. REPLACED MOUNT PER MM 71-20-2.SDR 9514449945Retract Mech · malfunctionedDURING SLAT EXTENSION ON APPROACH INTO MSP, SLAT EXTEND LIGHT BEGAN FLICKERING, THEN EXTINGUISHED AND SLAT DISAGREEMENT LIGHT ILLUMINATED. PERFORMED MISSED APPROACH AND CAPTAIN DECLARED AN EMERGENCY. SUCCESSFUL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT WITH
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