Douglas DC-9-15F
Service difficulty reports · 851
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 = 'DC915F' 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 = 'DC915F' 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 EE4Y1003019Skin · corrodedDURING INSPECTION CARGO CABIN BETWEEN STA Y 370 AND STA Y 427 BETWEEN LONGERON 1R AND 3R FRAMES, LONGERONS AND SKIN WITH CORROSION.SDR EE4Y1003018Frame · corrodedDURING INSPECTION CARGO CABIN AT STA Y 218 LONGERON 4R FRAME WITH CORROSION.SDR EE4Y1003017Skin · corrodedDURING INSPECTION LOWER FUSELAGE STA 200 LONGERON 18L SKIN WITH LIGHT CORROSION.SDR EE4Y1003016Support · crackedDURING INSPECTION NR 2 ENGINE PYLON AT STA 817 CLOSING RIB HOSES SUPPORT CRACKED.SDR EE4Y1003015Frame · corrodedDURING INSPECTION UPPER FUSELAGE AFT ACCESSORY COMPARTMENT RT AT CANT-STA 925 OVER LONGERON 12 FRAME WITH CORROSION.SDR EE4Y1003014Longeron · corrodedCARGO CABIN BETWEEN STA Y 256 AND STA Y 275 LONGERON 8L WITH CORROSION.SDR EE4Y1003013Longeron · corrodedCARGO CABIN, BETWEEN STA Y 274 AND Y 294 LONGERON 2L WITH CORROSION.SDR EE4Y1003012Skin · corrodedDURING INSPECTION UPPER EXTERNAL FUSELAGE FROM STA 50 TO STA 70 BETWEEN +X28 AND -X28 SKIN WITH CORROSION IN SEVERAL PLACES.SDR EE4Y1003011Angle · corrodedDURING THE UPPER FUSELAGE AFT ACCESSORY COMPARTMENT INSPECTION COOPESA FOUND LT AT CAN STA 910 +Z50 +X50 ANGLE CORRODED.SDR EE4Y1003010Bulkhead · corrodedDURING THE LOWER FUSELAGE AFT COMPARTMENT INSPECTION COOPESA FOUND LT AFT PRESSURE BULKHEAD INNER SKIN CORRODED.SDR EE4Y100300Floor Support · corrodedDURING THE LOWER FUSELAGE FWD CARGO COMPARTMENT INSPECTION, FOUND AT STA 345 BETWEEN LONG 23 LT AND 24 LT FLOOR SUPPORT CORRODED.SDR EE4Y1003008Longeron · corrodedDURING THE LOWER FUSELAGE CARGO COMPARTMENT INSPECTION COOPESA FOUND LONG 30 AT STA 224 CORRODED.SDR EE4Y1003007Angle · corrodedDURING THE UPPER FUSELAGE AFT ACCESSORY COMPARTMENT RT INSPECTION COOPESA FOUND FROM CAN-STA 964 TO 976 -X15+Z2 ANGLE CORRODED.SDR EE4Y1003006Skin · corrodedDURING THE LOWER FUSELAGE INSPECTION COOPESA FOUND FROM STA 661 TO 680 BETWEEN LONG 29L AND 29R SKIN CORRODED.SDR EE4Y1003005Strap · corrodedDURING THE LOWER FUSELAGE FWD CARGO COMPARTMENT INSPECTION COOPESA FOUND AT STA 408 BETWEEN LONG 29L AND 30 STRAP CORRODED.SDR EE4Y1003004Floor Support · corrodedDURING LOWER FUSELAGE FWD CARGO COMPARTMENT INSPECTION COOPESA FOUND AT STA 408 BETWEEN LONG 28R AND LONG 27R FLOOR SUPPORT CORRODED.SDR EE4Y1003003Longeron · corrodedDURING LOWER FUSELAGE FWD CARGO COMPARTMENT INSPECTION COOPESA FOUND AT LONG 30 BETWEEN STA 427 AND 446 LONGERON CORRODED.SDR EE4Y1003002Angle · corrodedDURING INSPECTION UPPER FUSELAGE AFT ACCESSORY COMPARTMENT LT AT CANT STA 910+Z50+X50 COOPESA FOUND ANGLE CORRODED.SDR MJYA749T0912001Float Valve · stuckRIGHT WING TRAILING FUEL AFTER TAKEOFF, LEFT WING FUEL LEVEL DROPPED 1000 POUNDS.SDR Y2PA200911260004Window · crackedAT CRUISE ALTITUDE (FL 340), AT NIGHT, CAPTAIN NOTED A REFLECTION OF THE MOON ABOVE HIS HEAD IN THE COCKPIT. UPON INVESTIGATION THE PILOT DISCOVERED THE LT AFT COCKPIT WINDOW HAD A SEMI-CIRCULAR CRACK APPROX 8" LONG BY APPROX ,5" WIDE. THE CREW DECLARED AN ESDR K11A2009100391501Heater · sparksFO'S WINDOW SPARKED AND OUTER GLASS CRACKED, EMERGENCY DESCENT WAS GIVEN TO 10,000 FT. TURNED OFF WINDSHIELD HEAT AND DONNED O2 MASKS RETURNED TO CYEG.SDR K11A2009021691503Skin · crackedSKIN CRACKED IN AREA OF RT AFT NOSE GEAR DOOR AFT HINGE CRACKED, 1 X 1 INCH.SDR K11A2009021191501Stiffener · crackedAFT EXIT PRESSURE DOOR FRAME HAS A CRACKED ANGLE STIFFENER AT 12 O'CLOCK CENTER FRAME.SDR K11A2009021691502Web · chafedUPLOCK ACTUATOR MOUNT WEB CHAFED 7 INCHES DOWN FROM MAIN DECK, 1 X 1 INCH.SDR K11A2009021691501Web · chafedUPLOCK ACTUATOR MOUNT WEB CHAFED 7 INCHES DOWN FROM MAIN DECK FLOOR, 1 X 1 INCH.SDR K11A2009020691501Bulb · burned outEMERGENCY LIGHT ASSY INOP AT L1 DOOR. REPLACED BULB, OPS CHECKED GOOD ALL WORK IAW MM 33-53-00.SDR K11A2008102291501Terminal Block · brokenTERMINAL BLOCK AT STA FS 146 FLOORBEAM BROKE, AFTER INVESTIGATION FOUND 2 WIRES DAMAGED. REPLACED WIRE FROM TERMINAL NR 1 TO THE T1 POSITION ON THE LEFT APU BUSS RELAY. ALSO REPLACED TERMINAL END ON THE SECOND ATTACHING IN THE NR 1 POSITION OF THE TERMINAL BSDR ABXR080173Longeron · crackedLONGERON 16 LEFT WAS CRACKED AT STA 801 FRAME UPPER ATTCH FASTENER. REMOVED AND REPLACE LONGERON IAW SRM 53-02, FIG 18, SHEET 1. (A)SDR ABXR080174Shear Tie · crackedSHEAR TIE CRACKED BELOW LONGERON 14 LEFT AT FRAME STA 801 REPAIRED SHEAR TIE IAW DWG K050159. (A)SDR ABXR080172Longeron · crackedLONGERON 3 LEFT CRACKED AT FRAME TO LONGERON ATTCH POINT STA 930. REMOVED LONGERON SECTION, SPLICED NEW LONGERON IAW DC9 SRM 53-02, FIG 18. (A)SDR ABXR080171Jackscrew · corrodedHORZ, STAB JACK SCREW THREADS PITTED/CORRODED. REMOVED AND REPLACED JACK SCREW IAW DC9 MM 27-40-1. (A)SDR ABXR080170Angle · crackedCENTER WING TO FUSELAGE ANGLE CRACKED AND SEPERATED ABOVE REPAIR STRAP FORWARD SPAR AREA AT APPROX. RIGHT BUTT LINE 48. REMOVED AND REPLACED FITTING IAW DC9 SRM. (A)SDR ABXR080169Support · crackedRIGHT WING OUTBOARD SPOILER HAD OUTBOARD ACTUATOR SUPPORT BRACE CRACKED, UPPER END. REMOVED AND REPLACED OUTBOARD ACTUATOR SUPPORT BRACE IAW DC0 SRM 51-30-1, 51-30-2 AND 51-30-5. (A)SDR ABXR080168Support · crackedLEFT WING OUTBOARD SPOILER HAD OUTBOARD ACTUATOR BRACE CRACKED. REMOVED AND REPLACED OUTBOARD ACTUATOR BRACE IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5. (A)SDR ABXR080034Skin · crackedRIGHT WING LOWER TRAILING EDGE SKIN AFT OF INBOARD BUTE DOOR WAS CRACKED. REPAIRED SKIN IAW DC9 SRM 57-01, FIGURE 3.SDR ABXR080033Bulkhead · crackedINBOARD KEEL BULKHEAD AT BUTT LINE '0', FS 604.00 VERTICAL ATTACH ANGLE ON AFT SIDE CRACKED. REPAIRED VERTICAL ATTACH ANGLE ON KEEL BULKHEAD STA 604 RIGHT IAW DC9 SSRM DWG K05159.SDR ABXR080032Skin · crackedFOUND FUSELAGE SKIN CRACKED AT MAIN ENTRY DOOR UPPER AFT DOOR STOP HOLE. REPAIRED FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER AFT DOOR STOP IAW DC9 SRM 53-05.SDR 0801001Light · inoperativeON APPROACH TO KGSO, RIGHT LANDING GEAR GREEN POSITION INDICATOR WOULD NOT ILLUMINATE. LANDING GEAR PHYSICALLY DOWN, VERIFIED WITH GEAR HORN. AFTER THE PROCEDURE, BOTTOM SOCKET LIGHT ILLUMINATED BEFORE LANDING. RELAMPED RIGHT LANDING GEAR GREEN INDICATOR ASSDR ABXR070251Gusset · crackedPASSENGER AFT ENTRANCE DOOR AFT PRESSURE BULKHEAD CUTOUT LOWER LEFT CORNER LEAKED AND SHOWED EVIDENCE OF A CRACK IN THE DOUBLERS. REPAIRED LOWER AFT PRESSURE BULKHEAD IAW REA D953-56099-MR. P/N'S: 5910130-85/87, CRACK LENGTHS: 2.250" AND 1.625".SDR ABXA070124Bulkhead · crackedCRACK OF UNKNOWN LENGTH AND DIRECTION IN DOUBLER UPPER LEFT AFT PRESSURE BULKHEAD DOOR CUTOUT CORNER. STOP DRILLED CRACK IN -13 DOUBLER, INSTALLED REPAIR IAW DC9 SRM J060088-543 AND DC9 SB 53-137.SDR ABXA070125Bulkhead · crackedAFT PRESSURE BULKHEAD SKIN CRACKED AT UPPER LEFT DOOR CUTOUT. REMOVED AND REPLACED SKIN IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA070121Spar · crackedX-RAY INSPECTION ON LEFT ELEVATOR REVEALED CRACKS AT STATIONS: XE 74(.750), XE 191(.600), XE 195(.750), XE 199 (.750), AND XE 219 (.400). REPAIRED CRACKS AT STATIONS: XE 191, XE 195, XE 199 AND XE 219. NO CRACKS DETECTED AT XE 74. REPAIRED IAW DC9 SRM 55-02SDR ABXA070123Bulkhead · crackedAFT PRESSURE BULKHEAD DOOR CUTOUT UPPER RIGHT CORNER DOUBLER HAD APPROXIMATELY 1.5" RADIUS CRACK. REPAIRED UPPER RIGHT CORNER OF AFT PRESSURE BULKHEAD IAW DC9 SRM J060088-543 REPAIR AND DC9 SB 53-137.SDR ABXA070122Tab · delaminatedRIGHT AILERON OUTBOARD TAB DELAMINATED 3 PLACES, 1 UPPER AND 2 LOWER APPROXIMATELY 3 BY 3, 3 BY1 1/2, OUTBOARD TIP REPAIR DISBOND. REMOVED AND REPLACED RIGHT AILERON TRIM TAB IAW DC9 MM 27-10-5.SDR K11A2008120391501Outflow Valve · malfunctionedCABIN WILL NOT PRESSURIZE.SDR K11A2008112091508Web · corrodedBS 646 APPROX RBL 55 WEB UNDER FLOOR BOARD CORRODED.SDR K11A2008112191505Floor Panel · damagedMAIN DECK FLOOR PANEL EDGE LIFTING BETWEEN BS 503 AND 566 AT LBL 21.SDR K11A2008112191506Door Frame · crackedGALLEY SERVICE DOOR INTERIOR HORIZONTAL FRAME CRACKED BEYOND STOP DRILL IN OUTBOARD RADIUS AT FORWARD SIDE OF DOOR APPROX BS 180 STRINGER 13R 1 INCH CRACK.SDR K11A2008112091503Stiffener · crackedHORIZONTAL STIFFENER CRACKED AT END FASTENER ON UPPER SKIN SURFACE INSIDE ACCESS PANEL 8204 18 INCHES OTBD OF FUSELAGE APPROX STA 860.SDR K11A2008112091501Floorbeam · corrodedFLOOR SUPPORT CORRODED AT STA 200 LBL 55.
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