Douglas DC-9-41
Service difficulty reports · 2,671
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 = 'DC941' 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 = 'DC941' 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 ABXA030213Web · crackedRIGHT CUSP WEB JUST FORWARD OF FS 1041 CRACKED. REPAIRED CRACK IN CUSP IAW DC-9 SRM 53-01.SDR ABXA030212Fitting · corrodedCABIN FLOORBEAM END FITTINGS FS 973, RIGHT BUTTLINE 58, LEVEL I CORROSION. REPLACED FLOORBEAM END FITTINGS IAW DC-9 SRM.SDR ABXA030215Attach Angle · crackedNR 2 ENGINE LOWER PYLON ATTACH ANGLE WAS CRACKED AT STA 1030. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-1.SDR ABXA030211Seat Track · corrodedSEAT TRACK BUTT LINE '0' WAS CORRODED, FS 541 TO FS 619. REPAIRED SEAT TRACK, BUTTLINE '0', FROM STA 160 TO STA 645 IAW DC-9 SRM.SDR ABXA030210Skin · crackedFOSELAGE SKIN AT UPPER AFT MAIN ENTRY DOOR STOP CRACKED. REPAIRED AREA IAW DC-9 SRM 53-05.SDR ABXA030209Skin · crackedFORWARD LOWER CARGO DOOR EXTERIOR SKIN CRACKED ON LEADING EDGE. BLENDED CRACK IAW DC-9 SRM 52-01 AND REA D952-47410.SDR ABXA030144Stabilizer · vibrationSUSPECT FLIGHT CONTROL MALFUNCTION OF STABILIZER. DURING FLIGHT, THE AIRCRAFT EXHIBITED INCREASING TURBULANCE AND VIBRATION. THE AUTO PILOT WAS ENGAGED AND WORKING PROPERLY WITH NO NOTED PROBLEMS. FLIGHT LEVEL WAS AT 240, 330 KIAS. AS SOON AS AIRSPEED WAS REDUSDR ABXA030183Attach Angle · crackedVERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED, LEFT SIDE OF VERTICAL AFT END. REPAIRED ANGLE IAW DC-9 SRM 53-05.SDR ABXA030141Computer · malfunctionedWITH AUTOPILOT ON DURING TURNS, THERE WAS EXTREME AND EXCESSIVE UNCOMMANDED ELEVATOR INPUTS. VERIFIED. RERACKED PITCH AND ROLL COMPUTERS. VERSINE LIFT CHECKED GOOD IAW DC-9 AMM CHAPTER 22.SDR GTIA030274Slide · dislodgedPBI - FLT 330 - LEFT SIDE PACK FELL OFF. REINSTALLED SLIDE/COVER. (M)SDR GTIA030243Slide · dislodgedEMERGENCY SLIDE PACK FELL OFF. REINSTALLED LANYARD SLIDE CHECK OK. (M)SDR GTIA030241Liner · crackedFOUND RT ENGINE HAS A SECTION OF ACCOUSTIC LINER MISSING AND CRACKED TAILPIPE 2 O'CLOCK POSITION. REMOVED AND REPLACED THRUST REVERSER SPACER. OPS AND LEAK CHECK GOOD. (M)SDR ABXA030119Window · out of adjustCAPTAIN'S SIDE WINDOW WOULD NOT OPEN. ADJUSTED LOWER AFT WINDOW HOOK IAW DC-9 56-10-03-5-0002. OPS CHECKED GOOD.SDR ABXA030107Bracket · brokenSLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION. FLIGHT CREW VERIFIED THROUGH FLIGHT CONTROLS THAT THERE WAS AN ASSYMETRY PROBLEM. FLIGHT CREW RETRACTED SLATS AND MADE A NO SLAT LANDING. FOUND AT ILN, #1 AND #2 SLAT PULLEY BRACKETS BROKEN, AND 3 EACH LSDR ABXA030106Support · brokenSLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION. FLIGHT CREW VERIFIED THROUGH FLIGHT CONTROLS THAT THERE WAS AN ASSYMETRY PROBLEM. FLIGHT CREW RETRACTED SLATS AND MADE A NO SLAT LANDING. FOUND AT ILN, NR 1 AND NR 2 SLAT PULLEY BRACKETS BROKEN AND 3 EACSDR ABXA030113Flange · shearedFLAP INBOARD FIXED VANE CENTER TWO CAM ATTACH FITTINGS ON FLAP LEADING EDGE WERE SHEARED. REPLACED FITTINGS (9957536-13 AND 9957536-7) IAW DC-9 SRM 51-30-2.SDR GTIA030116Flashlight · inoperativeFORWARD F/A HANDHELD EMERGENCY LIGHT, INOPERATIVE. REMOVED AND REPLACED FWD HANDHELD EMERGENCY LIGHT. OPS CHECK GOOD.SDR GTIA030115Sign · inoperativeTAILCONE INTERIOR LUMINESCENT EXIT SIGN INOPERATIVE. REMOVED AND REPLACED TAILCONE INTERION LUMINESCENT EXIT SIGN. OPS CHECK GOOD.SDR ABXA030112Longeron · crackedLONGERON 17 RIGHT CRACKED AT STA. 389, APPROXIMATELY 1/4" LONG. INSTALLED NEW FABRICATED LONGERON (P/N 2777922-1) AND SPLICE (P/N 7637813-3) IAW DC-9 SRM 53-02.SDR ABXA030111Seat Track · corrodedSEAT TRACK AT BUTT LINE 22 LEFT HAD CORROSION ON UPPER SURFACE OF OUTBOARD LOWER LEG FROM STA. 1034 - 1041 AND LOWER SURFACE OF OUTBOARD UPPER LEG AT STA. 1009. REPLACED TRACK SECTION IAW DC-9 SRM 53-05.SDR ABXA030110Bulkhead · crackedAFT PRESSURE BULKHEAD NR 4 CRACKED AT OUTBOARD END. INSTALLED NEW ANGLE IAW DOUGLAS DWG J060110.SDR ABXA030083Sensor · failedAFTER LANDING GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ON. AFTER CYCLING GEAR, THE LIGHT REMAINED ON FOR ONE MINUTE, THEN WENT OUT. REMOVED AND REPLACED THE NOSE LANDING GEAR LOCK SENSOR IAW DC-9 MM 32-60-01-2.SDR ABXA030082Control Box · defectiveRED NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. GEAR RECYCLED. ABNORMAL COMPLIED WITH FOR RETURN FLIGHT TO ILN. REMOVED AND REPLACED PROX. CONTROL BOX. PERFORMED ADJUSTMENT TEST OF LANDING GEAR POSITION AND WARNING INDICATION SYSTEM IAW SDR ABXA030076Drain · frozenDEPLOYING SPOILERS CREATED A LT ROLL OF 5 DEGREES PER SECOND. AILERONS BINDED DURING APPROACH, AILERONS HEAVY DURING APPROACH. FOUND SLAT PANEL DRAINS BLOCKED BY ICE, WATER LEAKED OUT OF SLANT PANEL AND DOWN ONTO AILERON AND SPOILER CABLES, FREEZING THEM UP. TSDR GTIA030053Wire · brokenDURING LANDING GEAR RETRACTION (RT GEAR UNSAFE) LT REMAINED ILLUMINATED. C/W QRH PROC. UPLATCH CHECKS GOOD WITH GEAR EXTENDED FOR LANDING, ALL INDICATIONS NORMAL. FLT 262. FOUND BROKEN WIRE AT RT GER UP LOCK SENSOR, CONNECTOR NR P1-1150. REPINNED IAW STD SDR GTIA030052Proximity Sensor · malfunctionedLEFT GEAR UNSAFE LIGHT NEVER CAME ON EXTENTION. GROUND TESTS OK IAW MM 32-60-0. REMOVED AND REPLACED LEFT GEAR UP-LOCK PROXIMITY SENSOR AS PRECAUTIONARY.SDR ABXA030064Socket · wornON GEAR EXTENSION INTO PIE, GEAR DOOR OPEN LIGHT NEVER ILLUMINATED. BULB CHECKED GOOD. GEAR RECYCLED. ON NEXT EXTENSION IT DID NOT COME ON BUT ONLY FOR 1 SECOND, NOT THE NORMAL 30 SECONDS. VERIFIED, FOUND GEAR DOOR OPEN LAMP WORN WHICH CAUSED AN INTERMITTENT PSDR ABXA030073Intercostal · crackedINTERCOSTAL WAS CRACKED TWO PLACES, FS 180, LBL 22. REPAIRED AREA IAW DC-9 SRM 51-10-3, 51-10-3B, AND REA D953-46196.SDR ABXA030048Volt Regulator · burnedSMOKE IN UPPER CARGO COMPARTMENT AND COCKPIT. INSPECTED AND FOUND APU GENERATOR CONTROL PANEL AND APU VOLTAGE REGULATOR BURNED. INSPECTED WIRING FOR DAMAGE, NONE NOTED. INSPECTED AC BUS CONTROL FOR DAMAGE, NONE NOTED. INSPECTED FOR ANY CIRCUIT BREAKERS TRIPPEDSDR ABXA030047Proximity Sensor · dirtyRT GEAR UNSAFE LIGHT CAME ON DURING UPLATCH CHECK AFTER TAKE-OFF. FOLLOWED ABNORMAL PROCEDURE AND RECYCLED GEAR. UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE UP AND RT HYDRAULIC SYSTEM IN 'HIGH', RT GEAR LIGHT REMAINED ILLUMINATED. ON DESCENT AT FL 250, RT GEAR SDR ABXA030072Web · crackedFORWARD LOWER CARGO DOOR UPPER AFT HINGE INTERCOSTAL WEB CRACKED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA030071Web · crackedCUSP WEB CRACKED, LONGERON 18 LT, FS 1021 - 1041. REPLACED CUSP IAW DC-9 SRM 51-30-2.SDR ABXA030070Fitting · crackedFLOOR BEAM TO KEEL FITTING, STA. 775 WAS CRACKED. REPLACED FITTING, STA. 775, IAW DC-9 SRM 51-30-5 AND 51-30-1.SDR ABXA030069Rib · crackedNR 2 SLAT TRACK CUT-OUT INBOARD LEADING EDGE RIB LOWER HORIZONTAL FLANGE HAD A 3.5 INCH CRACK. REPAIRED AREA IAW DC-9 REA D957-46167.SDR GTIA030003Skin · crackedDTW - FOUND CRACK/PUNCTURE IN SKIN AT STATION NR 1012 LONGERON STATION NR 26R JUST AFT OF CARGO PIT DOOR. REPAIRED CRACK/PUNCTURE IN SKIN AT STATION1012 LONGERON NR 26R JUST AFT OF CARGO PIT DOOR. (M)SDR ABXA030044Floorbeam · crackedF.S. 1072 FLOORBEAM UPPER ANGLE CRACKED, RBL 54. REPAIRED FS 1072 FLOORBEAM UPPER ANGLE AT RBL 54 IAW DC-9 SRM.SDR ABXA030043Intercostal · corrodedLEVEL I CORROSION BETWEEN FS 218 - 200 AT FLOOR SUPPORT INTERCOSTAL, JUST INBOARD FROM 29 RT LONGERON. REPLACED INTERCOSTAL IAW DC-9 SRM.SDR ABXA030042Skin · corrodedRT FORWARD NOSE LANDING GEAR DOOR EXTERIOR SKIN WAS CORRODED AROUND AFT DOUBLER. REPLACED RT NOSE LANDING GEAR DOOR IAW DC-9 MM 32-22-01-2.SDR GTIA030019Oil System · fluctuatesACY - FLT 277 - GATE RETURN, NR 2 OIL PRESSURE FLUCTUATING. UNSCHEDULED CHANGE OF A/C EN ROUTE. (M)SDR ABXA020366Battery · dischargedEMERGENCY LIGHTING DIM. REMOVED AND REPLACED BATTERIES. OPS CHECKED GOOD IAW MM.SDR ABXA020353Link · crackedNR 1 ENGINE UPPER RIGHT LINK THRUST REVERSER CRACKED. REPLACED IAW MM.SDR ABXA020351Intercostal · crackedINTERCOSTAL CRACKED AT STA. 973, LONGERON 28 RIGHT. REPLACED INTERCOSTAL IAW DC-9 SRM.SDR ABXA020307Controller · malfunctionedELEVATOR OSCILLATES VIOLENTLY WHEN AUTO PILOT WAS ENGAGED. COULD NOT DUPLICATE. REPLACED THE AUTO PILOT CONTROLLER IAW DC9 M.M. 22-10-00-5. AUTO PILOT SYSTEM OPS CHECK GOOD.SDR ABXA020280Link · crackedWHILE COMPLYING WITH AD 96-10-11, FOUND CRACK INDICATION ON UPPER LEFT THRUST REVERSER DRIVER LINK. INSTALLED SERVICEABLE DRIVER LINK IAW DC-9 MM 78-31-05-2-0001.SDR ABXA020275Latch · out of adjustCOCKPIT DOOR MECHANISM JAMMED. WOULD NOT ALLOW DOOR TO CLOSE OR OPEN. ADJUSTED COCKPIT DOOR LATCH MECHANISM IAW DC-9 AMM 25-32-0.SDR ABXA020283Shear Tie · crackedSHEAR TIES CRACKED ABOVE AND BELOW LONGERON 15 LEFT AT FS 1024. REPLACED CRACKED SECTION IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA020282Web · crackedCRACK IN LT CUSP WEB AT FS 1039 AND LONGERON 18. REPAIRED CUSP IAW DC-9 SRM 53-01.SDR ABXA020281Intercostal · crackedCORRODED AND CRACKED INTERCOSTAL BETWEEN STA. 1056 - 1072, BELOW THE LEFT GILLINER FLOOR SUPPORT. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR GTIA021070Floor Panel · cracked6 TO 8 INCH CRACK IN FLOOR WEBBING STA 807, RT SIDE. REPLACED FLOOR WEBBING.SDR GTIA021069Floor Panel · crackedTHE 04BD RT FLOOR PANEL AT ROWS 12 THROUGH 15 HAS CRACK. REPAIRED FLOOR PANEL (CLOSED 10/15/02).
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