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 MWEA020495Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 18&19 ALSO EXTENDING UNDER STRINGER 18 FORWARD AND AFT. -- FABRICATED AND INSTALLED SHIM.SDR MWEA020483Stringer · damagedREPAIR CLIPS REQUIRED BETWEEN STRINGERS 15&14 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.SDR MWEA020484Stringer · damagedREPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGERS 14&13 ON THE INBOARD AND OUTBOARD SIDE OF XCW 58 WING.SDR MWEA020485Stringer · damagedREPAIR CLIP REQUIRED INSTALL BETWEEN STRINGERS 13&12 ON THE INBOARD AND OUTBOARD SIDES OF XCW 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.SDR MWEA02505Stringer · damagedREQUESTING BOEING AGREEMENT OF FASTENER PLACEMENT IN UPPER PORTION OF REPAIR CLIPS BETWEEN STRINGER 14,15&16 THERE ARE TWO CLIPS AND TWO FASTENERS PER CLIP. -- BOEING APPROVES OF THE PLACEMENT OF THE FASTENERS.SDR MWEA02504Stiffener · damaged1 EACH DOUBLE DRILLED HOLES ON AFT PRESSURE BULKHEAD BETWEEN RADIAL STIFFENER 18&20 LEFT. -- REAMED HOLES AND INSTALLED BUSHING.SDR MWEA020503Stiffener · damaged2 EACH DOUBLE DRILLED HOLES ON AFT PRESSURE BULKHEAD RADIAL STIFFNERS 2&6 LEFT. -- REAMED HOLE UP AND INSTALLED 2 EACH BUSHINGS.SDR MWEA020500Angle · crackedAFT PRESSURE BULKHEAD RIGHT HAND RADIAL #2 LOWER ANGLE THAT ATTACHES TO JAMB GUSSET HAS A CRACKED ATTACH HOLE. -- FABRICATED AND INSTALLED ANGLE.SDR MWEA020499Doubler · crackedAFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT UPPER RIGHT CORNER HAS A CRACK EMANATING FROM CUTOUT HOLE TO THE DOOR JAMB EDGE DOT 30. -- FABRICATED AND INSTALLED DOUBLER, FABRICATED AND INSTALLED 8 FASTENERS.SDR MWEA020492Doubler · crackedAFT PRESSURE BULKHEAD PLUG DOOR STOP RECEPTACLE AT LOWER LEFT CORNER HAS A CRACK EMANATING FROM CUT OUT HOLE TO DOOR JAMB EGDE DOT 31. -- FABRICATED AND INSTALLED DOUBLER.SDR MWEA020491Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 14&15 ALSO EXTENDING UNDER STRINGER 14&15 AND ONE SPOT ON VERTICAL LEG. -- FABRICATED AND INSTALLED SHIMSDR MWEA020482Clip · crackedREMOVED LEFT FUEL TANK SHEAR CLIP AT 69 BULKHEAD BETWEEN STRINGER 12 & 13. DRILLED UP CLIP AND INSTALLED FASTENERS.SDR MWEA020510Seal · crackedLEFT AND RIGHT AFT PRESSURE BULKHEAD SEAL RETAINERS ARE CRACKED. -- DRILLED UP AND INSTALLED SEAL RETAINERS.SDR MWEA020509Stringer · damagedREPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGER 17&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.SDR MWEA020508Stringer · damagedREPAIRED CLIPS REQUIRED INSTALL BETWEEN STRINGER 15&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.SDR MWEA020507Stringer · damagedTEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 11 AND AFT SPAR RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.SDR MWEA020494Stringer Clip · damagedTEMPORARY STRINGER CLIP INSTALLED AT XRS 111 BETWEEN STRINGER 21&22 RIGHT WING. -- DRILLED UP CLIP AND INSTALLED NEW CLIP.SDR MWEA020493Stiffener · crackedSTIFFENER AFT SIDE OF AFT PRESSURE BULKHEAD AT RADIAL 20 LEFT IS CRACKED AND DENTED. FABRICATED AND INSTALLED STIFFENER.SDR MWEA020488Fitting · crackedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 13 AND 14, ALSO EXTENDING UNDER STRINGER 14 AND 13. ALSO FOUND CRACK ON OUTBOARD LEG. BLENDED OUT CRACK AND REMOVED CORROSION AROUND AND UNDER STRINGER.SDR MWEA020487Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 12 AND 13 ALSO EXTENDING UNDER STRINGER 12 AND 13. -- FABRICATED SHIMS FOR STRINGER AND REMOVED CORROSION.SDR MWEA020478Angle · crackedANGLE AT RADIAL 6 LEFT IS CRACKED. -- DRILLED UP ANGLE AND INSTALLED ANGLE.SDR MWEA020486Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 11 AND 12 ALSO EXTENDING UNDER STRINGER 11. -- REMOVED CORRORION.SDR MWEA020480Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGERS 16 AND 17 ALSO EXTENDING UNDER STRINGERS 16 AND 17.SDR MWEA020476Bracket · damagedSUPPORT BRACKET 5910163-191 LOCATED ON LEFT SIDE OF APB AT RADIAL 6 INBOARD END DAMAGED. -- LOCATED AND DRILLED INBOARD AND OUTBOARD END OF NEW 191 AND REMOVED AND INSTALLED BRACKET.SDR MWEA020468Fastener · crackedSKIN CRACK INDICATION NOTED STATION 180 JUST RIGHT OF LONGERON ONE. -- REMOVED AND INSTALLED FASTENERS INTO FORMERS.SDR MWEA020465Fitting · oversizedFORWARD CARGO DOOR FITTINGS HAS OVERSIZED HOLES. -- REMOVED AND INSTALLED FITTINGS.SDR MWEA020464Angle · oversizedFORWARD CARGO DOOR ANGLE HAS OVERSIZED HOLES. -- REMOVED AND REPLACED ANGLE.SDR MWEA020470Doubler · crackedPER PCI 9274 FOUND SMALL SKIN CRACK INTO DOOR STOP ADJUST HOLE ON AFT SIDE OF DOOR 3RD HOLE FROM THE TOP (MARKED). -- FABRICATED AND INSTALLED DOUBLER.SDR MWEA020469Finger Doubler · crackedSKIN CRACKED INDICATION NOTED STATION 525 JUST RIGHT OF LONGERON ONE (MARKED). -- FABRICATED AND INSTALLED SKIN PLUG AND FINGER DOUBLER.SDR MWEA020467Angle · oversizedFORWARD CARGO DOOR ANGLE HAS OVERSIZED HOLES. -- REMOVED AND INSTALLED ANGLE.SDR MWEA020466Doubler · crackedFORWARD CARGO DOOR #2 OUTBOARD UPPER ATTACH HOLE IS CRACKED. -- FABRICATED AND INSTALLED DOUBLER.SDR MWEA020456Intercostal · crackedINTERCOSTAL IS CRACKED AROUND FASTENER HOLES FORWARD CARGO DOOR BELOW #1 BEAM FORWARD END OF DOOR (DOT JH 23). -- REMOVED AND INSTALLED INTERCOSTAL.SDR MWEA020455Clip · gougedSHOVEL CLIP JUST AFT OF APB LEFT 17 LONGERON IS GOUGED. -- REPAIRED GOUGE AND INSTALLED SHOVEL CLIP.SDR MWEA020454Clip · crackedAPB RADIAL NR 16 LEFT END CLIP HAS A CRACK AROUND END FASTENER HOLE. FABRICATED AND INSTALLED CLIP.SDR MWEA020451Splice Plate · crackedAFT PRESSURE BULKHEAD PLUG DOOR JAMB HAS A CRACK AT APPROXIMATELY THE 6 O'CLOCK POSITION IN THE SPLICE PLATE CONNECTION. REMOVED AND INSTALLED SPLICE PLATE.SDR MWEA020447Oil SystemON DEPARTURE OUT OF MILWUAKEE RIGHT ENGINE OIL QTY INDICATION DECREASED TO ZERO. -- DEFERRED RIGHT ENGINE OIL QTY PER MEL 79-3SDR 0202349150Pump · malfunctionedWHILE IN CRUISE FLIGHT WITH THE ENGINE DRIVEN HYDRAULIC PUMPS IN LOW, THE RIGHT HYDRAULIC SYSTEM WENT TO ZERO PRESSURE FOR 3-5 SECONDS THEN RETURNED TO NORMAL 1500 PSI. THIS OCCURRED TWICE AND THE RIGHT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MANUAL LIGHTS SDR 0202359140Duct · disconnectedAT 14,000 FEET, THE CABIN PRESSURE ANNUNCIATOR ILLUMINATED. CABIN ALTITUDE WAS 10,000 FEET. VERY SOON AFTER THE WARNING LIGHT CAME ON AND CABIN WENT TO 15,000 FEET AND MASKS DEPLOYED. COMPLIED WITH COM PROCEDURES AND PRESSURE CONTROLLER WAS FULL FORWARD. FLIGHSDR 0201579150Indicator · malfunctionedRIGHT HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. RIGHT HYDRAULIC QUANTITY WENT TO 10 QUARTS FROM 7-8 THAT WAS SHOWING AT TAKEOFF. COMPLIED WITH COM AND LANDED AT MSP WITHOUT INCIDENT. THE AIRCRAFT WAS TOWED TO THE GATE FROM THE TAXIWAY. MAINTENANCE TESTED THESDR MWEA020321Oven · shortedF/A REPORTED SEEING AN ORANGE FLASH ABOVE AND BEHIND GALLEY OVEN. -- NWA MTC INSPECTED LEFT AND RIGHT OVENS. FOUND OVEN GROUND WIRE SHORTED. PULLED AND COLLARD LEFT AND RIGHT OVEN CIRCUIT BREAKERS. DEFERRED OVENS PER MEL 25-12. REMOVED AND REPLACED OVENS DMISDR MWEA020290Arm · failedPASSENGER DOOR HAS STRUCTURAL DAMAGE (CRACK) TO INTERCOSTAL LOCATED WHERE CRANK ARM PASSES THROUGH. DAMAGED CAUSED BY CRANK ARM FAILURE. REMOVED AND REPLACED INTERCOSTAL.SDR MWEA020292Beam · elongatedREMOVED DAMAGED INTERCOSTAL AND SUPPORT AND FOUND PAX DOOR BEAM #5 TO HAVE AN ELONGATED HOLE. -- FABRICATED AND INSTALLED REPAIR DOUBLER.SDR MWEA020291Support · elongatedINTERCOSTAL SUPPORT WAS REMOVED TO FACILITATE OTHER MAINTENANCE AND WAS FOUND TO HAVE ELONGATED HOLES AFTER REMOVAL. -- REPLACED WITH NEW SUPPORT.SDR 0201189152Insulation · out of positionJUST PRIOR TO THE FLIGHT LEVELING OFF AT FL290, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED. CABIN ALTITUDE WAS 10,500 FEET WITH THE DIFFERENTIAL AT 5 PSI. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET AND RETURNED TO DTW. NO MENTION OF COM COMPLIANCESDR 0201309151Door · crackedDuring shop visit in ATL, the 2 aft cargo door assy webs were found cracked at aft end. Repaired per EA 99-189648.SDR MWEA020207Stiffener · elongatedVERTICAL STIFFENER IN FORWARD ELECTONIC POWER CENTER HAS ELONGATED HOLES. -- REPAIRED VERTICAL STIFFENER IAW SRM 53-01 FIGURE SHEET 4.SDR ABXA010776Stiffener · crackedOUTBOARD STATION 91.00, FRONT SPAR VERTICAL STIFFENER, UPPER PORTION WAS CRACKED. REPLACED STIFFENER IAW DC-9 SRM.SDR MWEA020158Stiffener · crackedLEFT ENGINE PYLON AFT VERITCAL STIFFENER IS CRACKED LOCATED BETWEEN UPPER AND LOWER AFT PYLON SPARS. -- FABRICATED AND INSTALLED STIFFENER.SDR ABXA010775Skin · crackedRIGHT MAIN LANDING GEAR DOOR INNER SKIN CRACKED JUST AFT OF THE FORWARD HINGE FITTING. REPAIRED CRACKED AREA IAW DC-9 SRM 52-01.SDR ABXA010774Frame · crackedAUXILIARY SUPPORT FRAME CRACKED IN AFT ACCESSORY COMPARTMENT FLOOR SUPPORT, FORWARD OF MAIN FRAME AT STATION 908. REPLACED FRAME IAW DC-9 SRM DWG 505159 AND DC-9 SRM 51-30-2.
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