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.

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.Oct 4, 2005 · N967AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 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 PRESSOct 2, 2005 · N623NW · Doug DC941 · Cabin Cooling SystemSDR ABXA050248Frame · crackedFRAME 1152 CRACKED LONGERON 2 RIGHT. REPLACED CRACKED FRAME SECTION FS 1152 IAW DC-9 SRM 53-03.Sep 29, 2005 · N955AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050247Strut · corrodedNOSE LANDING GEAR STRUT BARREL HAD PITTING IN FIRST BEVEL OF BARREL HOUSING. REMOVED AND REPLACED STRUT BARREL IAW DC-9 SRM.Sep 29, 2005 · N955AX · Doug DC941 · Main Landing Gear Strut/Axle/TruckSDR ABXA050246Skin · crackedFUSELAGE CRACKED AT STA 1135 LONGERON 4 LEFT. REPAIRED AREA IAW DC-9 SRM.Sep 27, 2005 · N955AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 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. Sep 22, 2005 · N960AX · Doug DC941 · Engine (Turbine/Turboprop)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.Sep 9, 2005 · N969AX · Doug DC941 · Cabin Pressure Control SystemSDR 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 DC9Sep 7, 2005 · N975AX · Doug DC941 · Light System WiringSDR 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 REPLACAug 31, 2005 · N964AX · Doug DC941 · Air Distribution SystemSDR 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 REPLACEAug 24, 2005 · N952AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA050215Pressure Panel · corrodedAREA OF EXFOLIATION ON UPPER PRESSURE PANEL, MAIN FRAME AREA. REMOVED AND REPLACED DOUBLERS IAW DC-9 SRM 51-30-5.Aug 22, 2005 · N956AX · Doug DC941 · Fuselage Main, BulkheadSDR 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.Aug 22, 2005 · N956AX · Doug DC941 · Trailing Edge FlapsSDR 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.Aug 21, 2005 · N960AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050222Pan · crackedAFT UPPER CORNER OF MAIN ENTRY DOOR PAN WAS CRACKED. REPAIRED AREA IAW DC-9 SRM 52-05.Aug 17, 2005 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050200Spar · crackedRIGHT AFT PYLON SPAR WEB WAS CRACKED AT LIGHTNING HOLE, LONGERON 13 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-01.Aug 9, 2005 · N965AX · Doug DC941 · Nacelle/Pylon, Frame/Spar/RibSDR ABXA050196Window Frame · crackedTOP FORWARD CORNER OF WINDOW FRAME ON AFT SIDE OF STA 737 LEFT WAS CRACKED. REPAIRED AREA IAW DC-9 SSRM K07226.Aug 8, 2005 · N965AX · Doug DC941 · Fuselage Main, StructureSDR 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.Aug 8, 2005 · N965AX · Doug DC941 · Wing, Rib/BulkheadSDR 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.Aug 8, 2005 · N965AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Aug 8, 2005 · N965AX · Doug DC941 · Fuselage Main, StructureSDR 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. PAug 8, 2005 · N990AX · Doug DC941 · Cabin Pressure ControllerSDR ABXA050194Seat Track · crackedSEAT TRACK RT BUTT LINE 9, FS 200, CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-9 SRM 51-30-1.Aug 5, 2005 · N965AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050193Vane · crackedRIGHT FLAP INBOARD FIXED VANE SKIN CRACKED ADJACENT TO REPAIR. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM.Aug 4, 2005 · N965AX · Doug DC941 · Trailing Edge FlapsSDR ABXA050192Skin · crackedFS 1114 RIGHT SKIN CRACKED 8 1/2 INCHES UP FROM ENGINE PYLON. REPAIRED AREA FS 1114 RIGHT IAW DC-9 SRM.Aug 4, 2005 · N965AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 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.Jul 12, 2005 · N758NW · Doug DC941 · APU Oil SystemSDR 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 DISJul 5, 2005 · N759NW · Doug DC941 · Humidity Control SystemSDR 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.Jun 29, 2005 · N978AX · Doug DC941 · Landing Gear DoorsSDR 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.Jun 28, 2005 · N978AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA050172Pan · crackedRIGHT FORWARD OVERWING EXIT DOOR HAD CRACKED DOOR PAN, LOWER AFT CORNER. REPLACED RIGHT FORWARD OVERWING EXIT DOOR IAW DC-9 SRM.Jun 27, 2005 · N978AX · Doug DC941 · Emergency ExitsSDR ABXA050171Door · crackedLEFT MAIN LANDING GEAR DOOR CRACKED JUST FORWARD OF ACTUATOR ATTACH POINT. REPAIRED CRACK IAW DC-9 SRM.Jun 27, 2005 · N978AX · Doug DC941 · Landing Gear DoorsSDR ABXA050175Pan · crackedLEFT AFT OVERWING EXIT DOOR HAD CRACKED DOOR PAN, LOWER AFT CORNER. REPLACED LEFT AFT OVERWING EXIT DOOR IAW DC-9 SRM.Jun 27, 2005 · N978AX · Doug DC941 · Emergency ExitsSDR ABXA050174Pan · crackedLEFT FORWARD OVER WING EXIT DOOR HAD CRACKED PAN, UPPER AFT CORNER. REPLACED LEFT FORWARD OVER WING EXIT DOOR IAW DC-9 SRM.Jun 27, 2005 · N978AX · Doug DC941 · Emergency ExitsSDR 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.Jun 27, 2005 · N978AX · Doug DC941 · Emergency ExitsSDR ABXA050169Frame · crackedFRAME CRACKED 3 PLACES - FS 1185 AT LONGERON 6 AND 7 LEFT. REMOVED AND REPLACED FRAME IAW DC-9 SRM 51-30-5.Jun 24, 2005 · N978AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050170Frame · crackedFRAME CRACKED - FS 1152 AT LONGERON 12 RIGHT. REPAIRED IAW DC-9 SRM 53-03.Jun 24, 2005 · N978AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050225Fitting · crackedLONGERON 25 LEFT, END FITTING CRACKED, STA 617. REMOVED AND REPLACED LONGERON 25 LEFT END FITTING IAW DC-9 SRM.Jun 13, 2005 · N979AX · Doug DC941 · Fuselage Main, Attach FittingsSDR 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.Jun 13, 2005 · N979AX · Doug DC941 · Fuselage Internal Mounting StructureSDR 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.Jun 13, 2005 · N979AX · Doug DC941 · Fuselage Main, Attach FittingsSDR 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.Jun 12, 2005 · N979AX · Doug DC941 · Cargo/Baggage DoorsSDR 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 Jun 6, 2005 · N754NW · Doug DC941 · Cabin Cooling SystemSDR ABXA050124Battery · inoperativeEMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERIES IAW DC-9 AMM 33-53-02-4. OPS CHECKED GOOD.May 9, 2005 · N963AX · Doug DC941 · Emergency LightingSDR 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.May 4, 2005 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050108Attach Angle · crackedUPPER PYLON ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED AREA IAW DC-9 SRM 54-04.May 3, 2005 · N951AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA050111Stop Fitting · crackedFORWARD UPPER STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.May 3, 2005 · N951AX · Doug DC941 · Cargo/Baggage DoorsSDR 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.May 3, 2005 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR 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.May 2, 2005 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050089Fitting · corrodedDURING ROUTINE LINE MAINTENANCE, FOUND THE AFT FUSELAGE JACK PAD FITTING CORRODED BEYOND LIMITS. REPLACED FITTING IAW DC-9 SRM 51-30-5.Apr 7, 2005 · N973AX · Doug DC941 · Fuselage Miscellaneous StructureSDR 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.Apr 7, 2005 · N973AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 0500849754Floor Support · crackedDURING H-CHECK, FOUND CRACKED VERTICAL FLOOR SUPPORT AT BS 794 LBL 22. REPAIRED PER EA 97-203199.Apr 5, 2005 · N754NW · Doug DC941 · Fuselage Miscellaneous StructureSDR 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.Mar 23, 2005 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 22, 2005 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach Fittings
Back to Douglas DC-9-41