Douglas DC9-15
Service difficulty reports · 926
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 = 'DC915' 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 = 'DC915' 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 95ZZZW739Longeron · crackedDURING SPECIAL CHECK, FOUND A TWO INCH CRACK IN LONGERON 19L, STATION 218. REPAIRED PER SRM 53-02.SDR MWEA95158Eel Battery · dischargedDURING ROUTINE INSPECTION, THE AFT CABIN EMERGENCY FLASHLIGHT WOULD NOT TEST. REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.SDR 9505369103Clips · out of adjustDURING LINE CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR HANDLE FROM THE CLIPS. ADJUSTED CLIPS, CHECKED OK.SDR 9504799105Skin · loose fastenersDURING LINE CHECK, FOUND APPROXIMATELY 40 - 50 LOOSE FASTENERS ON BOTH SIDES OF THE RUDDER. REPLACED FASTENERS.SDR GRAA119531Control System · malfunctionCHEYENNE, WYOMING - ON CLIMB-OUT, AIRCRAFT HAD A CABIN PRESSURE LOSS. THE CABIN FAILED TO MAINTAIN PRESSURE AT 14,000 FEET. THE FLIGHT CREW LOCKED THE SYSTEM INTO MANUAL, THEN TRIED THE AUTOSYSTEM AGAIN ON DESCENT AND THE SYSTEM WORKED NORMALLY. THE AIRCRAFSDR MWEA95141Door Jamb · crackedDURING ROUTINE INSPECTION IT WAS FOUND THAT FWD PAX ENTRANCE DOOR JAMB HAD A 1.25 INCH CRACK AT UPPER FWD CORNER. REPAIRED DOOR JAMB IAW SRM 53-05, FIG, 26. RETURNED A/C TO SERVICE.SDR ABXA9500145Barrel Nut · rustedDURING COMPLIANCE OF A.D. 82-06-02, FOUND HORIZONTAL STABILIZER CENTER BOX FRONT SPAR UPPER LEFT NR 2 BARREL NUT RUSTED. CLEANED AND TREATED BARREL NUT IAW DC-9 SRM 51-10-3.SDR ABXA9500144Retainer · looseDURING COMPLIANCE OF A.D. 82-06-02, FOUND HORIZONTAL STABILIZER CENTER BOX FRONT SPAR UPPER LEFT NR 2 BARREL NUT RETAINER LOOSE. SECURED BARREL NUT RETAINER AS REQUIRED IAW DC-9 SRM 51-10-3.SDR 9503069106Switch · malfunctionedDURING START OF TAKEOFF ROLL MEM-IND, THE AFT CABIN DOOR WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT AND THE AIRCRAFT RETURNED TO THE GATE. REPLACED THE DOOR WARNING SWITCH. CHECKED OK.SDR 9503119101Longeron · crackedDURING LINE CHECK, FOUND .5 INCH CRACK IN LONGERON 16R THROUGH LOWER LEG AT FS 370. REPAIRED PER EA 91-094932.SDR MWEA95139Evac Slide · fell offPILOT REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE FELL OFF DURING DESCENT. MECHANIC REINSTALLED GALLEY DOOR EVACUATION SLIDE AND RETURNED A/C TO SERVICE.SDR MWEA95135Latch Fitting · crackedDURING SERVICE CHECK, FOUND AFT PRESSURE BULKHEAD PLUG DOOR LOWER LATCH FITTING BROKEN. REMOVED DAMAGED FITTING, INSTALLED NEW FITTING. A/C RETURNED TO SERVICE.SDR GRAA9530Radio Alt Ind · failedRENO, NEVADA - UPON TAXI OUT FROM GATE B-10, AIRCRAFT N1068T HAD A RADIO ALTIMETER FAIL FLAG IN BOTH RADIO ALTIMETERS. THE AIRCRAFT RETURNED TO GATE. MAINTENANCE REPLACED THE CAPTAIN'S RADIO ALTIMETER INDICATOR AND THE SYSTEM CONTINUED TO FAIL. MAINTENANCE DSDR 9502929105Intercostal · crackedDURING LINE CHECK, FOUND ONE .5 INCH CRACK IN VERTICAL INTERCOSTAL, FORWARD CARGO DOOR JAMB FS 351. REPLACED INTERCOSTAL PER EA 91-096933.SDR MWEA95129Water Line · disconnectedPILOT REPORTED STIFF AILERONS IN FLIGHT. MECHANICS FOUND LINE FOR WATER SYSTEM DISCONNECTED WHICH CAUSED WATER TO DRAIN INTO WHEEL WELLS FORMING ICE ON AILERON PULLEY CLUSTERS. REMOVED ICE FROM PULLEYS. INSPECTED CABLES AND PERFOMRED OPS CHECK. RETURNED A/SDR MWEA95133Pan · crackedDURING INSPECTION PER DAC SB52-125, FOUND FORWARD CARGO DOOR HAD A .25 INCH CRACK IN THE OUTER PAN RADIUS. REPIARED IAW DAC SRM 52-03, FIG 8 (DOUBLER INSTALLATION).SDR 9502669105Dnlock Sw · malfunctionedDURING APPROACH INTO MSP, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED ON GEAR EXTENSION. CONFIRMED VISUALLY THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTION AND AIRCRAFT LANDED WITHOUT INCIDENT. REPSDR MWEA95124Evac Slide · detachedPILOT REPORTS MAIN ENTRANCE DOOR EVACUATION SLIDE FELL OFF. MECHANICS RESECURED EVACUATION SLIDE AND RETURNED A/C TO SERVICE.SDR 9502229138Studs · brokenDURING LINE CHECK, FOUND BROKEN ATTACH STUDS AT THE RIGHT WING NR 4 FLAP HINGE. REPLACED 4 STUDS AND THE HINGE PER CITEXT 09-5740-1-0004.SDR 9501919106Pt7 Line · frozenNR 2 ENGINE EPR INDICATOR DID NOT GIVE ACCEPTABLE READINGS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. FOUND FROZEN MOISTURE IN THE PT7 LINE. REMOVED LINE, CLEARED BLOCKAGE, AND REINSTALLED LINE. RAN ENGINE. SYSTEM OPERATION WAS NORMAL.SDR GRAA9528Hyd Pump · failedUPON DESCENDING INTO MISSOULA, MONTANA, ACFT N NR 1064T LOST ALL HYDRAULIC FLUID FROM THE RT SYSTEM. THE LANDING GEAR WAS EXTENDED BY USING THE FREE-FALL METHOD. THE AIRCRAFT LANDED AT MISSOULA AIRPORT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RT ENGISDR 9501629106Epr Indication · malfunctionedON TAKEOFF ROLL, THE NR 2 ENGINE HAD NO EPR INDICATION. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE. SYSTEM WAS INSPECTED AND THE INDICATORS WERE SWAPPED FOR TROUBLESHOOTING. THE PROBLEM COULD NOT BE DUPLICATED. SYSTEM FUNCTIONALLY TESTESDR MWEA95111Outer Pan · crackedDURING INSP OF AFT CARGO DOOR, A 2 INCH CRACK WAS FOUND IN THE OUTER PAN RADIUS IN THE UPPER FWD CORNER OF THE AFT DOOR. THE CRACK WAS STOP DRILLED, AND AN EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03 FIG 8. AREA WAS TREATED IAW SRM 51-10-3. SDR 95112Door Jamb Sill · corrodedDURING INSP OF AFT CARGO COMPARTMENT DOOR JAMB SILL AREA, CORROSION WAS FOUND ON ATTACHING INTERCOSTAL WEB 2 GUSSETS, AND 2 CLIPS, THAT ATTACH DOOR JAMB SILL AT STA 758.00 LONGERON 29 RIGHT. REMOVED CORRODED PARTS, FABRICATED NEW AND INSTALLED CLIPS, GUSSETS,SDR MWEA95110Evac Slide · fell off dorDURING ROUTINE MAINTENANCE, THE PAX DOOR EMERGENCY SLIDE FELL OUT. RESECURED EMERGENCY SLIDE IN DOOR SLIDE HOLDER. RETURNED A/C TO SERVICE.SDR 9500319102Pt7 Tube · brokenON TAKEOFF, THE NR 2 EPR WAS .2 BELOW NR 1 WITH OTHER PARAMETERS MATCHED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. THE EPR TRANSMITTER WAS REPLACED. A BROKEN PT7 TUBE WAS FOUND BETWEEN THE 2 O'CLOCK AND 4 O'CLOCK PROBES. REPLACED THE PT7 TUBE.
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