Douglas DC-9-14
Service difficulty reports · 1,736
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 = 'DC914' 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 = 'DC914' 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 MWEA95256Skin · gougedDURING ROUTINE INSPECTION, THE SKIN WAS FOUND GOUGED AT STA 756 AND LONGERON 12L. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 53-04 FIG 38 VIEW G. RETURNED A/C TO SERVICE.SDR MWEA95238Connector · corrodedDURING CRUISE, TAIL CONE MISSING LIGHTS WENT ON AND OFF INTERMITTENTLY. THE TAILCONE SWITCH CONNECTORS WERE FOUND CORRODED. CLEANED CORROSION AND OPS CHECKED GOOD.SDR MWEA95237Cover · off hingeDURING ROUTINE INSPECTION, THE TAIL EMERGENCY SLIDE COVER WAS FOUND NOT INSTALLED ON HINGE. MAINTENANCE RESECURED TAIL SLIDE COVER. RETURNED A/C TO SERVICE.SDR MWEA95255Skin · crackedDURING ROUTINE INSPECTION, THE SKIN WAS FOUND CRACKED APPROXIMATELY .75 IN LENGTH AT STA 756, LONGERON 7R. MAINTENANCE INSTALLED PLUG REPAIR IAW SRM 53-04 FIG 38 VIEW 1. RETURNED A/C TO SERVICE.SDR 9512299160Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE LEFT MAIN LANDING GEAR SIDE BRACE ATTACH FITTING LUG. REPAIRED FITTING (P/N 5919289-521) PER EA 91-97104.SDR 9511939150Skin · crackedDURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN FS 200 BETWEEN LONGERONS 14L TO 15L. REPAIRED SKIN (P/N 5911406-7), PER EA 91-100820.SDR MWEA95254Longeron · crackedDURING ROUTINE INSPECTION, LONGERON 17R WAS FOUND CRACKED AT STA 786. MAINTENANCE REPLACED SECTION OF LONGERON IAW SRM 53-02. RETURNED A/C TO SERVICE.SDR MWEA95253Longeron · crackedDURING ROUTINE MAINTENANCE, LONGERON 16R WAS FOUND CRACKED AT STA 786. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 53-02. RETURNED A/C TO SERVICE.SDR MWEA95252Longeron · crackedDURING ROUTINE INSPECTION, LONGERON 14L WAS FOUND CRACKED AT STA 766. MAINTENANCE REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 53-02. RETURNED A/C TO SERVICE.SDR MWEA95251Longeron · crackedDURING ROUTINE INSPECTION, LONGERON 13R WAS FOUND CRACKED AT STA 786. MAINTENANCE REPLACED LONGERON SECTION IAW SRM 53-02. RETURNED A/C TO SERVICE.SDR MWEA95250Longeron · crackedDURING ROUTINE INSPECTION, LONGERON 17L WAS FOUND CRACKED AT STA 786. MAINTENANCE REMOVED AND REPLACED LONGERON SECTION IAW SRM 53-02 FIG 2 PAGE 2A. RETURNED A/C TO SERVICE.SDR 9511239150Handle · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE INTERIOR TAILCONE HANDLE AND DROP THE TAILCONE. RERIGGED THE TAILCONE, CHECKED OK.SDR MWEA 95249Skin · gougedDURING ROUTINE INSPECTION, FOUND GOUGE IN BELLY SKIN .040 DEEP JUST RIGHT OF LONGERON 30 STA 737. MAINTENANCE REPAIRED SKIN IAW SRM 53-05 FIG 38 VIEW H. RETURNED A/C TO SERVICE.SDR 9511899150Support · corrodedDURING H-CHECK, FOUND CORROSION ON THE CENTER FLOOR SUPPORT BETWEEN FS 229 TO 296. REPAIRED SUPPORT (P/N 5910137-9) PER EA 91-100826.SDR 9511889150Skin · oil cannedDURING H-CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 942 TO 964 LONGERONS 20L TO 20R. REPAIRED SKIN (P/N 5910228-19), PER EA 91-100809.SDR MWEA95248Angle · corrodedDURING ROUTINE INSPECTION, THE CUSP ANGLE AT STA 210 LONGERON 18R WAS FOUND CORRODED BEYOND LIMITS. MAINTENANCE REPAIRED ANGLE IAW SRM 53-05 FIG 55 AND DAC DRAWING 9910078. REPAIR ANGLE FABRICATED FROM 7075-T6. RETURNED A/C TO SERVICE.SDR 9510709150Fitting · crackedDURING H-CHECK, FOUND A 1 INCH CRACK IN THE LONGERON 27R END FITTING AT FS 472. REPLACED FITTING PER SRM 51-30-2.SDR 9510289150Support · crackedDURING H-CHECK, FOUND A 1 INCH CRACK IN THE FORWARD GALLEY DOOR STOP FITTING SUPPORT AT THE NR 3 BEAM AFT END. REPLACED THE SUPPORT PER SRM 51-30-1.SDR 9510429162Press Controller · malfunctionedAUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED CABIN PRESSURE CONTROLLER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR 9510029150Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON RIGHT CUSP FITTING AT FS 786. REPLACED FITTING (P/N9912243-68) PER SRM 51-30-1.SDR MWEA95218Girt Bar Latch · lack of lubeCREW REPORTS GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR LATCH IS VERY HARD TO LATCH. MAINTENANCE CLEANED AND LUBRICATED GIRT BAR LATCHES. OPS CHECK GOOD. RETURNED A/C TO SERVICE.SDR 9509969139Connector · dirtyTAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. ABORTED AT 20 KNOTS AND RETURNED TO GATE. CLEANED CONNECTOR P10-1009. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE.SDR 9509589178Flange · crackedDURING LINE CHECK, FOUND A 4 INCH CRACK IN THE AFT CABIN DOOR LOWER LEFT FLANGE. REPLACED DOOR PER MM.SDR 9508709153Nav/Comm Panel · not seatedLOSS OF NR 1 NAV RECEIVER OCCURRED AFTER TAKEOFF. VOR/LOC FLAG WAS IN VIEW AND NO BEARING WAS AVAILABLE. PULLED AND RESET NAV CIRCUIT BREAKER WITH NO HELP. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND NR 1 NAV/COMM CONTROL PANEL NOT SEATED PROSDR 9508769140Release Mech · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND RELEASE THE TAILCONE. RE-RIGGED THE TAILCONE, CHECKED OK.SDR MWEA95206Duct · rupturedEN ROUTE TO DCA FROM OMA AT 33,000 FT, NOTICED CABIN ALT INCREASE 100 FPM PLUS DIFFERENTIAL DECREASE. UNABLE TO CONTROL IN AUTO AND MANUAL, DIVERTED TO MKE. REPLACED RUPTURED DUCT DOWNSTREAM OF TEMP CONTROL VALVE. CONTINUED FLIGHT TO DCA.SDR 9508429140Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE KEEL TO MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING FS 585. REPLACED FITTING P/N 9915511-5 PER DWG 9910164.SDR 9508399140Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE LEFT SIDE KEEL FITTING FS 525. REPLACED FITTING PER SRM 51-30-5.SDR 9508189140Fitting · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE LEFT WHEEL WELL KEEL FITTING LONGERON 29L AT FS 629. REPLACED FITTING PER SRM 51-30-1 AND SRM 51-30-5.SDR 9508179140Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN THE LEFT WHEEL WELL LONGERON 30 END FITTING AT FS 629. REPLACED FITTING PER SRM 51-30-1 AND SRM 51-30-5.SDR 9508169140Fitting · crackedDURING PERIODIC CHECK, FOUND A .25 CRACK IN THE AFT CARGO DOOR NR 2 BEAM AFT END FITTING. REPLACED FITTING.SDR 9508079162Guide Tube · out of positionDURING LINE CHECK, FOUND THAT THE TAILCONE WOULD NOT DROP. FURTHER INVESTIGATION REVEALED THAT THE TURNBUCKLE WAS STICKING IN THE CABLE GUIDE TUBE (BETWEEN THE INNER AND OUTER HANDLE) PREVENTING THE UPPER LATCHES FROM COMPLETELY RELEASING. ALSO, FOUND 3 WORNSDR MWEA95199Wire · brokenWHEN GEAR LOWERED RIGHT MLG UNSAFE LIGHT DID NOT LIGHT DURING TRANSIT UNLESS THROTTLES RETARDED. FERRIED A/C TO MKE. FOUND WIRE 2G204E24 OPEN BETWEEN RT UPLOCK CONNECTOR AND TERMINAL STRIP S3-66. REPLACED WIRE. PERFORMED GEAR SWING. SYSTEM PERFORMS O.K. SDR MWEA95198Skin · crackedDURING ROUTINE INSPECTION THE SKIN WAS FOUND CRACKED 1.50 INCHES IN LENGTH AT FASTENER HOLE STA 786 LONGERON 14L. MAINTENANCE REPAIRED SKIN BY CUTTING OUT CRACKED SKIN, INSTALLING FINGER DOUBLER AND SKIN FILLER TO REMAIN FLUSH IAW DOUGLAS TELEX SYS-ENG-DAC-02SDR 9507579160Release Mech · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ADJUSTED THE CLIPS AND RE-RIGGED THE LATCHES. CHECKED OK.SDR MWEA95195Antenna · inopON TAKEOFF ROLL, GPWS 'PULL UP' SQUAWKED SEVERAL TIMES, CAPT REPORTED SPEED UNDER 60 KNOTS. PULLED OFF TO DEFER (34-29A) AND SILENCE GPWS COMPUTER. MAINTENANCE VERIFIED BAD RADIO ALTIMETER ANTENNA. REPLACED ANTENNA, OPS CHECK GOOD. RETURNED A/C TO SERVICE.SDR 9507349161Dnlock Switch · malfunctionedDURING CLIMBOUT FROM DTW, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND LIGHT EXTINGUISHED AFTER APPROXIMATELY ONE MINUTE. FLIGHT CONTINUED TO DESTINATION (IAD) AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GSDR 9507329160Temp Sensor · malfunctionedRIGHT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED ON CLIMBOUT AT 14,000 FEET. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT HIGH TEMPERATURE SENSOR AND THERMAL CONTROL BOX. ALSO, TIGHTENED LINE AT RIGHT AUGMENTATION VSDR MWEA95188Eel Bulb · failedDURING ROUTINE INSPECTION, THE FWD ENTRANCE EMERGENCY FLASHLIGHT WAS FOUND INOP. MAINTENANCE REPLACED LIGHT BULB OPS CHECK GOOD. RETURNED A/C TO SERVICE.SDR 9507269163Handle · out of adjustDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ALSO, FOUND THAT THE TAILCONE DID NOT DROP USING THE INTERIOR HANDLE. ADJUSTED BOTH THE CLIPS AND THE LATCHES. CHECKED OK.SDR MWEA95186Inlet Cowl · crackedDURING ROUTINE INSPECTION A .5 INCH CRACK WAS FOUND ON LEFT ENGINE INLET LEADING EDGE SKIN. REPLACED LEFT ENGINE INLET. RETURNED AIRCRAFT TO SERVICE.SDR MWEA95181Oven · inopCREW REPORTS, 3 OVEN CIRCUIT BREAKER POPPED IN FLIGHT AND F/A SMELLED BURNING ODOR IN CABIN. MAINTENANCE REMOVED AND REPLACED OVEN. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.SDR MWEA95179Eel Power Supply · dischargedCREW REPORTS, THAT EMERGENCY FLOOR TRACK LIGHTS CAME ON DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY FOR SECTION OF TRACK LIGHTING AFFECTED. OPS CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.SDR 9506489152Uplock Switch · malfunctionedDURING APPROACH INTO DTW, GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED FOR LANDING. EXECUTED GO-AROUND PROCEDURES AND PERFORMED EMERGENCY EXTENSION PROCEDURES. REPLACED LEFT MAIN GEAR DOOR UPLOCK SWITCH. ALSO, REPLACED THE LEFT AND RIGHT GEAR DOSDR 9506479152Door Switches · contaminatedDURING APPROACH INTO RIC, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. RECYCLED GEAR AND LIGHT STAYED ON. PERFORMED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. CLEANED MAIN GEAR DOOR SWITCHES. ALSO, CHECKED WSDR 9505579151Adc · malfunctionedCAPTAIN'S ALTIMETER AND ALTITUDE ALERTER FLAGGED DURING CLIMBOUT. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED CAPTAIN'S AIR DATA COMPUTER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95197Angle · corrodedDURING ROUTINE INSPECTION FOUND ANGLE CORRODED SEVERELY IN LEFT WHEELWELL FWD OUTBD CORNER STA 586. REPLACED ANGLE WITH FACTORY PART IAW SRM 51-30-5. RETURNED A/C TO SERVICE.SDR 9506099163Te Panel · crackedDURING LINE CHECK, FOUND THAT THE RIGHT SIDE TRIPLE SLOTTED FLAP ARM BECAME DISCONNECTED RESULTING IN A 5 INCH CRACK IN THE TRAILING EDGE PANEL XEF 111.250, 2 FEET FORWARD OF THE TRAILING EDGE. ALSO, FOUND A CRACK IN THE -12R ANGLE. REPLACED PANEL AND REPAIRSDR 9505999162Fitting · corrodedDURING LINE CHECK, FOUND CORROSION AND PREVIOUS REWORK ON THE LEFT MAIN LANDING GEAR SIDE BRACE ATTACH LUG FACES. REWORKED PER EA 91-64916, SEC 1.SDR MWEA95166Eel Socket · inopEMERGENCY FLOOR MACH LIGHT INOP AT ROW 1C (DEFERRED). REMOVED AND REPLACED FLOOR TRACK LIGHT SOCKET. OPS CHECK GOOD. CLEARED DMI, RETURNED AIRCRAFT TO SERVICE.
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