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 ABXA050250Skin · corrodedAREA OF BULGING AND DISHED RIVETS - FS 626 AT LONGERON 26 LEFT. EXFOLIATED DOUBLER ON THE INSIDE, ABOVE HAT CHANNEL. REPAIRED AREA IAW REA D953-52507.SDR 0501519623Duct · blownDURING CRUISE, CREW HAD TROUBLE REGULATING THE CABIN TEMPERATURE. THE CABIN STARTED TO CLIMB AT 1600 FPM AND THE RED (CABIN PRESS) WARNING LIGHT ILLUMINATED. CREW INITIATED A RAPID DESCENT AND COMPLIED WITH COM PROCEDURES BUT WAS NOT ABLE TO REGAIN CABIN PRESSSDR ABXA050248Frame · crackedFRAME 1152 CRACKED LONGERON 2 RIGHT. REPLACED CRACKED FRAME SECTION FS 1152 IAW DC-9 SRM 53-03.SDR ABXA050247Strut · corrodedNOSE LANDING GEAR STRUT BARREL HAD PITTING IN FIRST BEVEL OF BARREL HOUSING. REMOVED AND REPLACED STRUT BARREL IAW DC-9 SRM.SDR ABXA050246Skin · crackedFUSELAGE CRACKED AT STA 1135 LONGERON 4 LEFT. REPAIRED AREA IAW DC-9 SRM.SDR ABXA050235Engine · defectiveLEFT ENGINE WOULD NOT SPOOL UP DURING APPROACH. WHEN THROTTLE WAS ADVANCED, ENGINE WOULD NOT START, COMPRESSOR STALLED. EMERGENCY DECLARED. LANDED WITH ENGINE AT IDLE POWER. SERVICED FUEL CONTROL UNIT WITH 6 ML OF SILICON OIL IAW P&W JT8D-11 MM 73-21-01. SDR ABXA050217Control System · failedRAPID DECOMPRESSION AT TOP OF DESCENT WHEN POWER LEVERS RETARDED. UNRECOVERABLE IN MANUAL, POWER LEVELED AT IDLE, OXYGEN USED. PERFORMED PAR 3, DC-9 MM 21-31-09-2, ADJUST/TEST SINGLE ENGINE SECOND SEGMENT CLIMB SWITCHES. OPS CHECKED GOOD.SDR ABXA050212Wire · brokenWHEN CIRCUIT BREAKER FOR CLEARVIEW & EYEBROW WINDOWS WAS PUSHED IN DURING FLIGHT, CONSIDERABLE ARCHING AND SPARKS CAME FROM CAPTAIN'S CLEARVIEW WINDOW BUY THE TERMINAL BLOCK. REPAIRED A BROKEN WIRE AT THE TERMINAL BLOCK AND REPLACED THE TERMINAL BLOCK IAW DC9SDR ABXA050208Duct · looseAT FL 350 LOST CABIN PRESSURE. LT PACK WAS NOT PROVIDING PRESSURIZATION BUT WAS IN AUTO AND INDICATED 160 PSI. ONLY ABLE TO MAINTAIN FL 210 WITH RIGHT PAC AT 260 PSI. BOTH PAC TEMPS NORMAL. FOUND RIGHT ACM DISCHARGE DUCT LOOSE AND RESECURED. REMOVED AND REPLACSDR ABXA050203Control Box · defectiveGEAR DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. INSPECTED AIRCRAFT MAIN LANDING GEAR DOOR UPLATCHES AND MECHANISMS IAW DC-9 AMM 32-60-03-2. ALL OKAY, NO DEFECTS NOTED. INSPECTED PROX SENSORS FOR POSITIONING AND ATTACHMENT, NO DEFECTS NOTED. REMOVED AND REPLACESDR ABXA050215Pressure Panel · corrodedAREA OF EXFOLIATION ON UPPER PRESSURE PANEL, MAIN FRAME AREA. REMOVED AND REPLACED DOUBLERS IAW DC-9 SRM 51-30-5.SDR ABXA050214Stud · brokenRIGHT WING OUTBOARD FLAP HINGE, STA 333, INBOARD LOWER STUD BROKEN OFF. REMOVED AND REPLACED ALL 4 STUDS IAW JOB CARD 92410004 AND DC-9 SRM.SDR ABXA050213Floor Support · crackedLEFT VERTICAL FLOOR SUPPORT CRACKED AT FS 718, LEFT BUTT LINE 44. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-30-1.SDR ABXA050222Pan · crackedAFT UPPER CORNER OF MAIN ENTRY DOOR PAN WAS CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05.SDR ABXA050200Spar · crackedRIGHT AFT PYLON SPAR WEB WAS CRACKED AT LIGHTNING HOLE, LONGERON 13 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-01.SDR ABXA050196Window Frame · crackedTOP FORWARD CORNER OF WINDOW FRAME ON AFT SIDE OF STA 737 LEFT WAS CRACKED. REPAIRED AREA IAW DC-9 SSRM K07226.SDR ABXA050199Rib · crackedCRACKED RIB AT RIGHT WING TRAILING EDGE, STA XRS 133. REMOVED, REPAIRED AND REINSTALLED RIB AT RIGHT WING STA XRS 133 IAW DC-9 SSRM K05159 AND DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA050198Seat Track · crackedSEAT TRACK CRACKED AT STA 200, RIGHT BUTT LINE 10. REMOVED AND REPLACED SEAT TRACK RIGHT BUTT LINE 10, FS 200 TO FS 155 IAW DC-9 SRM 51-30-2 AND 51-30-1.SDR ABXA050197Window Frame · crackedTOP FORWARD CORNER OF WINDOW FRAME ON AFT SIDE OF STA 737 RIGHT HAD A SMALL CRACK. REPAIRED AREA IAW DC-9 SSRM K07226.SDR ABXA050183Relay · inoperativeLOST PRESSURIZATION AT FL 290. PRESSURE CONTROLLER WOULD NOT LOCK. DESCENDED TO 2000, GAINED MANUAL CONTROL. DECLARED AN EMERGENCY. TROUBLESHOOTING DISCOVERED R2-55 RELAY TO BE BAD, REPLACED RELAY. ALSO REPLACED R20227. REPLACED LEFT GROUND SHIFT RELAY R2-4. PSDR ABXA050194Seat Track · crackedSEAT TRACK RT BUTT LINE 9, FS 200, CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1.SDR ABXA050193Vane · crackedRIGHT FLAP INBOARD FIXED VANE SKIN CRACKED ADJACENT TO REPAIR. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM.SDR ABXA050192Skin · crackedFS 1114 RIGHT SKIN CRACKED 8 1/2 INCHES UP FROM ENGINE PYLON. REPAIRED AREA FS 1114 RIGHT IAW DC-9 SRM.SDR 0501009758Apu · leakingDURING CLIMB, AFT RT LAV SMOKE DETECTOR SOUNDED AND FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN AREA. NO FIRE DETECTED. FLIGHT CREW RETURNED A/C TO DEPARTURE AIRPORT. MAINTENANCE FOUND APU OIL LEAK AND REPLACED APU.SDR 0500979759Coalescer Bag · contaminatedSMOKE WAS REPORTED COMING OUT OF UPPER CABIN SIDEWALL DURING CLIMBOUT. THE AIRCRAFT RETURNED TO AN UNEVENTFUL LANDING BACK AT OMA. NO FIRE EXTINGUISHER ACTIVATED BUT ONE FLIGHT ATTENDANT DONNED PROTECTIVE BREATHING EQUIPMENT. CONTRACT MAINTENANCE AT OMA DISSDR ABXA050177Rib · crackedINNER RIB CRACKED ON LEFT MAIN LANDING GEAR DOOR. REPAIRED AREA IAW DC-9 SSRM NR K05159 AND DC-9 SRM 51-30-1.SDR ABXA050176Longeron · crackedCRACKED LONGERON STA 617, LONGERON 24 LEFT, THROUGH KIDNEY PANEL. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR ABXA050172Pan · crackedRIGHT FORWARD OVERWING EXIT DOOR HAD CRACKED DOOR PAN, LOWER AFT CORNER. REPLACED RIGHT FORWARD OVERWING EXIT DOOR IAW DC-9 SRM.SDR ABXA050171Door · crackedLEFT MAIN LANDING GEAR DOOR CRACKED JUST FORWARD OF ACTUATOR ATTACH POINT. REPAIRED CRACK IAW DC-9 SRM.SDR ABXA050175Pan · crackedLEFT AFT OVERWING EXIT DOOR HAD CRACKED DOOR PAN, LOWER AFT CORNER. REPLACED LEFT AFT OVERWING EXIT DOOR IAW DC-9 SRM.SDR ABXA050174Pan · crackedLEFT FORWARD OVER WING EXIT DOOR HAD CRACKED PAN, UPPER AFT CORNER. REPLACED LEFT FORWARD OVER WING EXIT DOOR IAW DC-9 SRM.SDR ABXA050173Pan · crackedRIGHT AFT OVERWING EXIT DOOR HAD CRACKED DOOR PAN, UPPER FORWARD CORNER. FABRICATED DOUBLER IAW DC-9 SSRM DWG K07390. INSTALLED IAW DC-9 SSRM DWG K07390. REINSTALLED WEB IAW DC-9 SRM 51-30-2.SDR ABXA050169Frame · crackedFRAME CRACKED 3 PLACES - FS 1185 AT LONGERON 6 AND 7 LEFT. REMOVED AND REPLACED FRAME IAW DC-9 SRM 51-30-5.SDR ABXA050170Frame · crackedFRAME CRACKED - FS 1152 AT LONGERON 12 RIGHT. REPAIRED IAW DC-9 SRM 53-03.SDR ABXA050225Fitting · crackedLONGERON 25 LEFT, END FITTING CRACKED, STA 617. REMOVED AND REPLACED LONGERON 25 LEFT END FITTING IAW DC-9 SRM.SDR ABXA050156Shear Tie · crackedSHEAR TIE CRACKED AT LONGERON 27 LEFT, FS 695. REPAIRED IAW DC-9 SSRM DWG K05159 AND DC-9 SRM 51-30-5.SDR ABXA050157Fitting · crackedEND FITTING LONGERON 30, CRACKED FS 644, LEFT SIDE. REMOVED AND REPLACED END FITTING AT LONGERON 30, FS 644 IAW DC-9 SRM 51-30-5.SDR ABXA050155Pan · crackedAFT LOWER CARGO DOOR CRACK INDICATION IN RADIUS OF OUTER, ADJACENT TO TOP MOST STOP. REPAIRED DOOR IAW DC-9 SRM 52-03, 51-30-7, 51-30-1, 51-20-0 AND 51-30-5.SDR 0500939754Duct · blownLEVEL AT FL 290 WITH ENGINE AND AIRFOIL ANTI-ICE ON, CREW FELT A PRESSURE BUMP AND NOTICED CABIN ALTITUDE CLIMBING AT 1500 FPM. CYCLED PRESSURE CONTROLLERS FROM AUTO TO MANUAL AND BACK, ANTI-ICE SWITCHED OFF, BUT CABIN STILL CLIMBED. INITIATED RAPID DESCENT SDR ABXA050124Battery · inoperativeEMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERIES IAW DC-9 AMM 33-53-02-4. OPS CHECKED GOOD.SDR ABXA050112Cusp Web · crackedRIGHT CUSP WEB CRACKED AT EXISTING REPAIR, STA 1021 - 1041, RIGHT BUTT LINE 50. REMOVED AND REPLACED CUSP AT STA 1021 - 1041 IAW DC-9 SRM 53-03 AND 51-30-4.SDR ABXA050108Attach Angle · crackedUPPER PYLON ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED AREA IAW DC-9 SRM 54-04.SDR ABXA050111Stop Fitting · crackedFORWARD UPPER STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.SDR ABXA050110Stiffener · crackedAFT PRESSURE BULKHEAD RIGHT SIDE DOOR JAMB STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA050109Floor Support · corrodedFLOOR SUPPORT AT STA 1072 WAS CORRODED TOP AND BOTTOM SIDE LONGERON 28 LEFT - LONGERON 28 RIGHT. REMOVED AND REPLACED FLOOR SUPPORT SECTIONS IAW DC-9 SRM 51-30-2, 51-30-5, AND SSRM DRAWING K05159.SDR ABXA050089Fitting · corrodedDURING ROUTINE LINE MAINTENANCE, FOUND THE AFT FUSELAGE JACK PAD FITTING CORRODED BEYOND LIMITS. REPLACED FITTING IAW DC-9 SRM 51-30-5.SDR ABXA050088Doubler · corrodedDURING ROUTINE LINE MAINTENANCE, FOUND THE FUSELAGE DOUBLER BETWEEN EXTERIOR SKIN AND JACK PAD FITTING AT STA 1072, LONGERON 30, CORRODED BEYOND LIMITS. REPLACED DOUBLER IAW DC-9 SRM 51-30-3 AND 51-30-2.SDR 0500849754Floor Support · crackedDURING H-CHECK, FOUND CRACKED VERTICAL FLOOR SUPPORT AT BS 794 LBL 22. REPAIRED PER EA 97-203199.SDR ABXA050085Seat Track · corrodedUPPER CARGO LEFT SIDE BUTT LINE 44 HAD FLOOR PANEL BULGED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK AT STA 973 - 1071, LEFT BUTT LINE 44 ON JOB CARD 0349 IAW DC-9 SRM.SDR ABXA050084Seat Track · brokenSEAT TRACK BROKEN IN UPPER CARGO COMPARTMENT AT FS 1041 AND LEFT BUTT LINE 44.5. SPLICED IN NEW SECTION OF SEAT TRACK AT FS 1041 - 965, LEFT BUTT LINE 44.5 IAW DC-9 SRM 53-05.
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