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 MWEA97781Skin · crackedDURING C-CHECK, FOUND CRACK ON LEFT MLG INBOARD DOOR SKIN. REPAIRED IAW DC9 SRM 52-05 PAGE 25.SDR 9718449102Bulkhead · crackedDURING L CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE RIGHT OUTBOARD AND INBOARD FITTINGS FS 110. REPAIRED PER EA 91-151699.SDR 9718439102Bulkhead · crackedDURING L CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL LIGHT OUTBOARD FITTING FS 110. REPAIRED PER EA 91-151699.SDR 9717169138Strut · required serviceON START OF TAKEOFF ROLL, NOSE GEAR STARTED SEVERE SHIMMY. ABORTED TAKEOFF AT LOW SPEED AND RETURNED TO THE GATE. FOUND STRUT LOW AND LEFT NOSE TIRE SLIGHTLY OUT OF ROUND. SERVICED STRUT AND REPLACED THE LEFT NOSE WHEEL ASSEMBLY, OPERATIONAL CHECK OK.SDR TWAA9799004Valve · failedMCI - FLT 477 - DURING CLIMB, THE NR 2 ENGINE, FUEL HEAT VALVE STUCK IN THE OPEN POSITION CAUSING HIGH ENGINE OIL TEMPERATURE. SHUT DOWN ENGINE. REMOVED AND REPLACED THE FUEL HEAT VALVE, MFG P/N 3201115, MANUFACTURED BY WHITTAKER CONTROLS. OPERATIONAL CHECSDR MWEA97741Slide · defectiveDURING TRANS CHECK, FOUND EMERG GALLEY SLIDE PRESS LOW. MTC REMOVED AND REPLACED SLIDE.SDR 9715879101Battery · dischargedDURING INSPECTION, FOUND THE AFT SECTION OF THE FLOOR EMERGENCY ESCAPE LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY.SDR 9716559106Skin · corrodedDURING L-CHECK, FOUND CORROSION ON FUSELAGE SKIN BETWEEN LONGERONS 23R AND 26R AND BETWEEN FS 280 TO 315. REPAIRED PER EA 91-151615.SDR 9715649101Valve · malfunctionedDURING TAKEOFF ROLL, THE RIGHT ENGINE OIL PRESSURE INDICATION WAS ABNORMALLY HIGH. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED THE RIGHT ENGINE OIL PRESSURE REGULATOR VALVE, ENGINE OPERATIONAL CHECK OK.SDR MWEA97719Doubler · galledDURING C-CHK, FOUND AFT ADF UP ANTENNA MOUNT SURF AREA IS GALLING. MTC REPAIRED IAW SRM 53-04 FIG 29 SHT 1 / SRM 53-01.SDR MWEA97718Skin · crackedDURING C-CHK, FOUND CRACK ON APB PLUG DOOR LWR AFT SECTION. MTC REPAIRED IAW SRM 51-10-2A/52-05 FIG 21.SDR MWEA97703Angle · crackedDURING C-CHK, FOUND CRACKED MAIN ENTER DOOR INTERCOSTAL BETWEEN 6 AND 7 FWD SIDE. MTC REPAIRED IAW SRM 52-01/52-05.SDR MWEA97702Doubler · dentedDURING C-CHK, FOUND .5 INCH DENT FWD FUSE LT SIDE FS 133 ABOVE 20L. MTC REPAIRED IAW 53-04 FIG 38.SDR MWEA97701Doubler · corrodedDURING C-CHK, FOUND CORROSION GALLEY SERV DOOR AFT LWR ON ANGLE DOUBLER. MTC REPAIRED IAW SRM 51-30 AND 51-10-3.SDR MWEA97700Doubler · crackedDURING C-CHK, FOUND CRACKED INTERCOSTAL AT 29L BETWEEN STA 427 AND 446. MTC REPAIRED IAW 53-02 AND 51-30.SDR MWEA97699Angle · crackedDURING C-CHK, FOUND CRACK ON LT ENG PYLON ANGLE FLANGE. REPAIRED IAW SRM 54-01 FIG 2 SHT 3 AND 51-30.SDR MWEA97698Intercostal · crackedDURING CHK, CRACKS FOUND IN FWD CARGO DOOR INTERCOSTALS. MTC REPAIRED IAW SRM 52-01.SDR MWEA97697Spar · crackedDURING C-CHK, FOUND CRACK ON REAR SPAR OF HORIZ STAB. MTC REPAIRED IAW SRM 55-01 FIG 2 AND 51-10-3.SDR TWAA9782002Light · illuminatedSTL - FLT 416 - DURING CRUISE, EMERGENCY LIGHTS ILLUMINATED. PERFORMED SYSTEM OPERATIONAL CHECK WITH NO DEFECTS NOTED. UNABLE TO REPRODUCE MALFUNCTION. OP-15 - 6-2-96 - STL. (X)SDR 9713939106Fuel Control · malfunctionedDURING CLIMB, THE RIGHT ENGINE EPR, N1, N2, AND FUEL FLOW INDICATIONS BEGAN FLUCTUATING. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL CONTROL UNIT. ENGINE OPERATIONAL CHECKED OK.SDR 9715779104Skin · corrodedDURING LINE CHECK, FOUND CORROSION ON SKIN JUST AFT OF RIGHT BATTERY VENT DISCHARGE PORT. REPAIRED PER EA 91-151146.SDR 9715769104Doubler · corrodedDURING LINE CHECK, FOUND CORROSION ON INNER DOUBLER FORWARD OF E/E COMPARTMENT. REPAIRED PER EA 91-151146.SDR TWAA9769002Clamp · failedMCI - FLT 483 - DURING CRUISE, CABIN LOW PRESSURE LIGHT ILLUMINATED. REPLACED CLAMPS ON AIR CONDITIONING DUCT. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9766001Battery Pack · dischargedSTL - FLT 656 - DURING LANDING EMERGENCY EXIT LIGHTS FROM 14 AFT, ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS, INC. OPERATIONAL CHECK NORMAL. (M)SDR MWEA97446Slide · protrudingDURING TC, FOUND GALLEY EMERG SLIDE PROTRUDING BEHIND PLASTIC COVER. MTC REMOVED AND INSTALLED SLIDE IAW DAC MM 25-62-0.SDR 9709899104Vert Gyro · inoperativeNR 1 VERTICAL GYRO BECAME INOPERATIVE EN ROUTE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED NR 1 VERTICAL GYRO, OPERATIONAL CHECK OK.SDR ABXA9700927Spar Cap · corrodedDURING C-CHECK, FOUND THE CENTER WING SPAR AFT VERTICAL FACE OF THE SPAR CAP AT STA XCW -40 SEVERLY CORRODED. REPAIRED IAW ABX REA D957-19174-MR.SDR ABXA9700926Floorbeam · corrodedDURING C-CHECK, FOUND THE FLOORBEAM AT F/STA 786 CORRODED AT LBL 27 ON TOP SIDE. REPAIRED IAW ABX REA D953-19248-MR.SDR ABXA9700925Bulkhead Web · crackedDURING C-CHECK, FOUND THE UPPER CARGO BULKHEAD AT F/STA 786 LT WEB CRACKED. REPAIRED IAW ABX REA D953-19255-MR.SDR ABXA9700924Web · corrodedDURING C-CHECK, FOUND THE CUSP WEB AT F/STA 786 LT CORRODED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2.SDR ABXA9700923Fitting · crackedDURING C-CHECK, FOUND THE FLOORBEAM FITTING AT F/STA 786 LT CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5 AND 51-30-1.SDR ABXA9700922Rib · crackedDURING C-CHECK, FOUND THE RIGHT WING LEADING EDGE RIB AT STA 172 CRACKED. CUTOUT CRACKED SECTION OF RIB, AND REPAIRED IAW ABX REA D957-19252.SDR ABXA9700921Bulkhead Fitting · crackedDURING C-CHECK, FOUND THE RIGHT WING BULKHEAD FITTING AT W/STA XRS 69 BETWEEN STRINGERS 12 AND 13 INSIDE LT WING FUEL TANK CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-05.SDR ABXA9700920Door Pan · crackedDURING C-CHECK, FOUND THE FORWARD CARGO COMPARTMENT DOOR PAN CRACKED BOTH SIDES OF NR 1 PRESSURE STOP. REPAIRED UPPER CRACK IAW DC9 SRM 52-05, FIGURE 50 AND LOWER CRACK IAW DC9 SRM 52-03, FIGURE 1.SDR ABXA9700919Skin · crackedDURING C-CHECK, FOUND THE FUSELAGE SKIN CRACKED 4 INCHES LONG AT LONGERON 18R, FS 544. REPAIRED CRACKED SKIN IAW DC9 SRM 53-04, FIGURE 12B.SDR ABXA9700914Trapezoidal Pnl · crackedDURING C-CHECK, FOUND THE RT TRAPEZOIDAL PANEL CRACKED JUST ABOVE THE RT MLG FIXED STRUT ATTACH POINT. REPLACED TRAPEZOIDAL PANEL IAW DC9 SRM 57-09, FIGURE 34 AND DACO SB 53-182.SDR ABXA9700913Fitting · crackedDURING C-CHECK, FOUND FORWARD INTERCOSTAL FS 218 BETWEEN LONG 27 AND 28 L CRACKED. REPLACED ATTACH ANGLE (FITTING) P/N 5956034-527 PER DC9 SRM 51-30-2.SDR ABXA9700912Skin · damagedDURING C-CHECK, FOUND FUSELAGE SKIN DAMAGED AT STA 408, LONGERON 21L. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 38, SHT 20.SDR ABXA9700911Floorbeam · crackedDURING C-CHECK, FOUND FLOORBEAM AT FS 503 AND LBL 57 CRACKED. REPLACED FLOORBEAM IAW DC9 SRM.SDR ABXA9700910Frame · crackedDURING C-CHECK, FOUND FUSELAGE FRAME STA 801 CRACKED AT LONGERON 17R. REMOVED AND REPLACED CRACKED SECTION OF FRAME IAW DC9 SRM 53-03, FIGURE 32.SDR ABXA9700908Fitting · crackedDURING C-CHECK, FOUND THE RT FLOORBEAM TO KEEL WEB ATTACH FITTING AT FS 585 CRACKED. REPLACED RT FLOORBEAM ATTACH FITTING IAW ABX REA D953-19152-MR, DC9 SRM 51-30-5.SDR TWAA975003Battery Pack · dischargedSTL - FLT 416 - DURING CRUISE, AFT EMERGENCY ESCAPE LIGHTING ILLUMINATED. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5822-2, MANUFACTURED BY LUMINESCENT SYSTEMS, INC. OPERATIONAL CHECK NORMAL. (M)SDR ABXA9701119Skin · corrodedRIGHT INBOARD FIXED VANE HAS HOLE IN SKIN AND CORRODED. REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN.SDR ABXA9700909Longeron · crackedDURING THE C-CHECK INSPECTION, FOUND THE FORWARD END OF LONGERON 20R CRACKED. REPAIRED LONG 20R IAW DC9 SRM, FIGURE 9.SDR ABXA9700918Door · crackedDURING C-CHECK, FOUND DOOR PAN CRACKED. REPAIRED CRACK PER DC9 SRM.SDR ABXA9700907Subfloor · crackedDURING C-CHECK, FOUND THE FORWARD SUBFLOOR MEMBRANE CRACKED AT FS 207 AND LBL 26. REPAIRED FORWARD SUBFLOOR MEMBRANE IAW DC9 SRM 53-01, FIGURE 1.SDR ABXA9700906Skin · dentedDURING C-CHECK, FOUND EXTERIOR FUSELAGE SKIN DENTED AT FS 165 AND LONG 21R - 22R. REPAIRED DENT IAW DC9 SRM 53-04, FIGURE 38, VIEW F.SDR ABXA9700749Hinge · crackedDURING C-CHECK, FOUND MLG INBOARD DOOR HINGE AFT LUG CRACKED. REPLACED MLG DOOR HINGE HALF IAW DC9 SRM 51-30-1.SDR ABXA9700748Fitting · crackedDURING C-CHECK, FOUND FLOORBEAM FITTING ATTACHED TO LEFT PYLON BULKHEAD AT FS 786 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9700747Angle · crackedDURING C-CHECK, FOUND ANGLE AT LONGERON 20 RT AND FORWARD END OF TRAPEZIODAL PANEL IS CRACKED AND CORRODED. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-1.
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