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 ABXA050078Attach Angle · crackedNR 1 PYLON UPPER ATTACH ANGLE HAD 1 MISSING FASTENER AND CRACKED AT STA 1056. REPAIRED AREA IAW DC-9 SRM 54-04.Mar 21, 2005 · N975AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA050077Frame · corrodedAFT LOWER SECTION OF FRAME CORRODED FS 503, LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.Mar 21, 2005 · N975AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050076Cargo Track · corrodedCORROSION ON FLOOR TRACK STA 889 TO STA 1072, LEFT SIDE. REMOVED AND REPLACED TRACK IAW DC-9 SRM 51-30-1.Mar 21, 2005 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050079Skin · crackedAFT FUSELAGE HAD 7 EXTERNAL SKIN CRACKS FROM CANTED STA 1197 TO 1208, LONGERON 13 LEFT TO LONGERON 14 LEFT. CRACK LENGTHS FROM .5 TO .75 INCHES. REPAIRED AREA IAW DC-9 SRM 53-01 AND 53-10.Mar 21, 2005 · N975AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA050083Splice · crackedINBOARD FRAME FOOT ON AFT SIDE OF LEFT PYLON BULKHEAD WAS CRACKED. REPLACED CRACKED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.Mar 21, 2005 · N975AX · Doug DC941 · Nacelle/Pylon, Main FrameSDR ABXA050082Door Frame · crackedDOOR JAMB WAS CRACKED AT TOP LEFT STOP AT INBOARD RIVET. REPAIRED DOOR JAMB AT TOP LEFT IAW DC-9 SRM 53-05.Mar 21, 2005 · N975AX · Doug DC941 · Fuselage Main, StructureSDR ABXA050081Bulkhead · crackedWEB ON LEFT PYLON BULKHEAD WAS OIL CANNED AND CRACKED AT LOWER INBOARD LIGHTNING HOLE. REPAIRED AREA IAW DC-9 SRM 53-01.Mar 21, 2005 · N975AX · Doug DC941 · Nacelle/Pylon, Bulkhead/FirewallSDR ABXA050080Longeron · crackedLONGERON 17 RIGHT CRACKED AT PYLON BULKHEAD. SPLICED IN REPAIR ON LONGERON 17 RIGHT AT PYLON BULKHEAD IAW DC-9 DWG K05864 AND DC-9 SRM.Mar 21, 2005 · N975AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA050075Fitting · crackedBRACE FROM UPPER PRESSURE PANEL TO FUSELAGE CRACKED AT BOTTOM BOLT ATTACH POINT 56 INCHES LT BUTTLINE AND 19 INCHES AFT OF MAIN FRAME. REMOVED AND REPLACED BRACE IAW DC-9 SRM.Mar 18, 2005 · N975AX · Doug DC941 · Fuselage, Landing Gear Attach FittingsSDR ABXA050071Skin · corrodedDURING ROUTINE LINE MAINTENANCE AT ILN, FOUND THE FUSELAGE BELLY SKIN CORRODED BEYOND LIMITS AT STATION 596 AND LONGERON 30. CUT OUT CORRODED SKIN 3.5 BY 2.5 INCH AND REPAIRED IAW ABX AIR REA D953-51559.Mar 9, 2005 · N968AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA050067Structure · crackedCRACK IN SUBFLOOR STA 160 RBL 6. REPAIRED AREA IAW DC-9 SRM 53-01.Mar 4, 2005 · N969AX · Doug DC941 · Fuselage Main, StructureSDR ABXA050066Frame · crackedLEFT AFT MAIN FRAME HAD A CRACK APPROXIMATELY 1.5 INCH IN LENGTH AT POINT E FORWARD FLANGE. CRACK WAS WITHIN ALLOWABLE LIMITS IAW DC-9 SERVICE BULLETIN 53-131 AND ES00913.Mar 2, 2005 · N969AX · Doug DC941 · Fuselage Main, FrameSDR 0500429755Floorbeam · corrodedDURING H-CHECK FOUND CORROSION ON FLOORBEAM AT BS 794 RBL 57 TO RBL 60. REPAIRED PER EA 97-202515.Feb 28, 2005 · N755NW · Doug DC941 · Fuselage Main, Floor BeamSDR ABXA050065Support Fitting · crackedRIGHT OUTBOARD TORSION BAR OUTBOARD SUPPORT FITTING CRACKED AT UPPER FORWARD FASTENER. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-2.Feb 28, 2005 · N969AX · Doug DC941 · Wing, Attach FittingsSDR ABXA050064Frame · crackedCRACKED FRAME AT STA 1152, LONGERON 15 LEFT, FORWARD OF LEFT EPR TRANSMITTER. REPAIRED AREA IAW DC-9 SRM.Feb 18, 2005 · N966AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050063Stop · corrodedFORWARD LOWER CARGO DOOR STOPS HAD EXTERNAL AND INTERNAL CORROSION. REPAIRED IAW REA D953-51511MR.Feb 17, 2005 · N966AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA050062Window Frame · crackedCRACK INDICATIONS ON LOWER LEFT WINDSHIELD ZEE. REMOVED AND INSTALLED NEW ZEE ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-8.Feb 17, 2005 · N966AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050061Window Frame · crackedCRACK INDICATIONS ON LOWER RIGHT WINDSHIELD ZEE. REMOVED AND REPLACED NEW ZEE ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-8.Feb 17, 2005 · N966AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050060Fitting · crackedLONGERON 26 RIGHT CRACKED AT STA 636 THROUGH KIDNEY PANEL. REPLACED LONGERON FITTING IAW DC-9 SRM 51-30-2 AND 51-30-5.Feb 16, 2005 · N966AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050059Fitting · crackedLONGERON 26 LEFT CRACKED AT STA 636 THROUGH KIDNEY PANEL. REMOVED AND REPLACED LONGERON END FITTING 26 LEFT AT STA 636 IAW DC-9 SRM 51-30-2 AND 51-30-5.Feb 16, 2005 · N966AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050058Frame · crackedSTRUCTURAL ANGLE LOCATED BENEATH FIRST OFFICER'S WINDOW CRACKED AT INBOARD END. REPAIRED AREA IAW REA D953-51500MR AND IAW DWG SR09530268.Feb 16, 2005 · N966AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050056Frame · crackedSTRUCTURAL ANGLE LOCATED BENEATH CAPTAIN'S WINDSHIELD WAS CRACKED AT INBOARD END. REPAIRED AREA IAW REA D953-51500MR AND IAW DWG SR09530268.Feb 16, 2005 · N966AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050057Frame · crackedBOTH ENDS OF STRUCTURAL ANGLE LOCATED BENEATH CENTER WINDSHIELD ARE CRACKED. REPAIRED AREA IAW REA D953-51500MR AND DWG SR09530268.Feb 16, 2005 · N966AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050028Floorbeam · corrodedFLOORBEAM CORRODED ON LOWER FLANGE STA 1013 AT CARGO DOOR UPLATCH BRACKET. REPAIRED IAW DC-9 SSRM K07411.Jan 31, 2005 · N971AX · Doug DC941 · Fuselage Main, Floor BeamSDR ABXA050023Limit Switch · malfunctionedALTERNATE TRIM (LONG) CIRCUIT BREAKER TRIPPED. PER FLIGHT CONTROL, CREW DECLARED AN INFLIGHT EMERGENCY. REPLACED ALT LIMIT SWITCH IAW DC-9 AMM 27-40-00. OPS CHECKED GOOD.Jan 21, 2005 · N974AX · Doug DC941 · Stabilizer Position IndicatingSDR ABXA050027Attach Angle · crackedLOWER LEFT PYLON ATTACH ANGLE WAS CRACKED INBOARD OF PYLON ACCESS PANEL 8101. REPAIRED AREA IAW DC-9 SRM 54-04.Jan 20, 2005 · N971AX · Doug DC941 · Nacelle/Pylon, Main FrameSDR ABXA050026Cusp Web · crackedCUSP WEB CRACKED AT FS 984, 1010, 1030 - 1040, LEFT BUTT LINE 54, UNDER SEAT TRACK. REPLACED CUSP WEB IAW DC-9 SRM 51-30-1 AND 51-30-2.Jan 17, 2005 · N971AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050021Pan · corrodedAFT LOWER CARGO DOOR CUTOUT LOWER PAN CORRODED AND FORWARD LOWER CORNER OF PAN BULGED WITH 3 RIVETS THROUGH THE SKIN POPPED. REMOVED DOOR PAN / SCUFF PLATE / WEB. REMOVED AND REPLACED -45 DOUBLER. CLEANED CORROSION ON DOOR PAN AND RE-INSTALLED DOOR PAN / WEJan 7, 2005 · N970AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050020Pan · crackedCRACK IN RADIUS OF INNER PAN AT AFT LATCH CAM. REPAIRED CRACKED PAN IAW DC-9 SRM 52-05.Jan 6, 2005 · N970AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA050019Frame · crackedFRAME CRACKED AT LONGERON 13 RIGHT, STA 1152. REPAIRED FRAME IAW DC-9 SRM 53-03 AND 51-30-5.Jan 6, 2005 · N970AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050018Frame · crackedFORWARD OVER WHEEL WELL FRAME RIGHT SIDE, REQUIRED REPLACEMENT PER JC NEA 53400100-002-40, FRAME CRACKED FORWARD AND AFT FLANGE. REMOVED AND RE-INSTALLED NEW FRAME AT STA 737 IAW EA 53400 322-001-3.Jan 6, 2005 · N970AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050017Fitting · crackedUPPER AFT STOP TEE FITTING CRACKED FORWARD LOWER CARGO DOOR. REPLACED FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-4.Jan 6, 2005 · N970AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA050016Support · damagedHORIZONTAL STAB JACKSCREW HAD DAMAGED THREAD NEAR THE SELF-LOCKING LOWER STOP NUT. REPLACED JACKSCREW IAW DC-9 MM.Jan 5, 2005 · N970AX · Doug DC941 · Horizontal Stabilizer StructureSDR ABXA050002Control Panel · defectiveON CLIMB-OUT FROM RIC, SMOKE OBSERVED COMING FROM CENTER CONSOLE. AIRCRAFT DIVERTED TO ROA. ISOLATED SMOKE TO PEDESTAL RED FILL LIGHT RHEOSTAT KNOB. DISCONNECTED PLUG TO PEDESTAL LIGHT CONTROL. REMOVED AND REPLACED PEDESTAL INSTRUMENT PANEL LIGHT CONTROL ADec 29, 2004 · N977AX · Doug DC941 · Flight Compartment LightingSDR 0402179750Engine · flamed outAFTER TAKEOFF, THE NR 1 ENGINE FLAMED OUT AT 3,300 FT, RELIGHT ATTEMPT WAS UNSUCCESSFUL. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 1 ENGINE DUE TO LOW OIL PRESSURE DURING ENGINE WINDMILLIDec 14, 2004 · N750NW · Doug DC941 · Engine (Turbine/Turboprop)SDR ABXA040390Downlock Switch · malfunctionedEN ROUTE, NOSE GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR, LIGHT REMAINED ON. REPLACED NOSE GEAR DOWNLOCK SWITCH IAW DC9 MM 32-60-01.Dec 6, 2004 · N955AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA040389Switch · defectiveRT MLG DOWN (GREEN) LIGHT DID NOT ILLUMINATE (ALTERNATE DOWN LIGHTS INDICATED DOWN), RECYCLED GEAR. ALL 3 DOWN LIGHTS CAME ON. REPLACED RIGHT MAIN LANDING GEAR DOWN LOCK SWITCH IAW PARA 3 OF DC9 AMM 32-60-01-2-0101, PARA 1D APPLIED, NO GEAR SWING REQUIRED.Dec 3, 2004 · N968AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA040391Shear Tie · crackedUPPER END OF SHEAR TIE CRACKED AT LONGERON 14 RIGHT, AFT OF FRAME 1056. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5.Nov 30, 2004 · N964AX · Doug DC941 · Fuselage Main, StructureSDR 0402129760Strap · missingA LINE CHECK INSPECTION FOUND THE AFT EVACUATION SLIDE MISSING THE DEPLOYMENT STRAPS. MAINTENANCE INSTALLED THE STRAPS PER ROUTINE WORK CARD 2560-4064M, STEP 3G, RII INSPECTION REQUIRED AND COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE.Nov 25, 2004 · N760NW · Doug DC941 · Escape SlideSDR ABXA040377Pressure Panel · leakingDESCENDING, PASSING FL 180, AUTOPILOT WITH HEADING MODE ENGAGED, NOTICED A/C DRIFTED 20 DEGREES LT OF COURSE WITH NOSE DOWN, SWITCHED TO TURN KNOB, A/C WOULD NOT RESPOND. DISENGAGED AUTOPILOT, YOKE STILL IN LT/FWD POSITION. WENT TO ROLL WINGS LEVEL BUT YOKE JANov 12, 2004 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA040376Structure · vibrationIN DESCENT, LEVELED OFF AT 300 KIAS, INCURRED VIBRATION, SLOWED TO 290 KIAS, VIBRATION WENT AWAY THEN CAME BACK AGAIN WHEN ACCELERATING THROUGH 295 KIAS. INSPECTED FOR GENERAL CONDITION & SECURITY OF THE FOLLOWING ITEMS: NOSE GEAR AREA, FUSELAGE, FLAPS, SLATSNov 7, 2004 · N971AX · Doug DC941 · Aircraft StructuresSDR ABXA040375Vane · damagedAIRFRAME RUMBLE/VIBRATION AT 285 KTS WITH AIRCRAFT CLEAN, VIBRATION CAN BE FELT THROUGH FLOOR AND RUDDER PEDALS. REPLACED RT FLAP FORWARD MOVABLE VANE IAW DC9 MM 27-51-02-4-0001. REPLACED BUSHING IN EYEBOLT ON RT WING T/E UPPER I/B PANEL SUPPORT. REPLACED SNov 5, 2004 · N971AX · Doug DC941 · Trailing Edge FlapsSDR 0402019760Strut · dischargedAT ABOUT 3,000 FEET DURING CLIMB-OUT, CREW COULD NOT COMPLETE THE UPLATCH CHECK. COM PROCEDURES COMPLIED WITH AND AFTER NUMEROUS GEAR OPERATION AND INDICATION PROBLEMS, THE AIRCRAFT LOST PRESSURIZATION AT 13,000 FEET. PER A FILED ASR, THE CREW DECLARED AN EMNov 4, 2004 · N760NW · Doug DC941 · Nose/Tail Landing Gear Strut/AxleSDR 0402139759Angle · crackedDURING H-CHECK FOUND CRACKED RT WING TO FUSELAGE ATTACH ANGLE AT BS 644. REPAIRED PER EA 97-201426.Nov 3, 2004 · N759NW · Doug DC941 · Wing, Fuselage Attach FittingsSDR ABXA040355Trunnion · corrodedBOTH FORWARD TRUNNIONS EARS INNER SURFACES PITTED AND CORRODED ON RIGHT MAIN LANDING GEAR TRUNNION. REPAIRED AREA IAW REA D932-50887MR.Oct 22, 2004 · N970AX · Doug DC941 · Main Landing GearSDR ABXA040353Attach Fitting · corrodedDURING ROUTINE GEAR CHANGE, FOUND CORROSION BEYOND LIMITS ON THE RIGHT MAIN LANDING GEAR ATTACH FITTING FORWARD LUG FORWARD FACE AND FORWARD LUG AFT FACE. REPAIRED ATTACH FITTING LUGS BY SPOT FACING AND INSTALLING WASHERS TO REGAIN BLUE PRINT DIMENSIONS IAW ROct 22, 2004 · N970AX · Doug DC941 · Wing, Landing Gear Attach FittingsSDR ABXA040345Fitting · crackedLONGERON END FITTING CRACKED AT RIGHT CANTED KEEL AREA, LONGERON 29 RIGHT. REMOVED AND REPLACED LONGERON END FITTING AT CANTED KEEL AREA IAW DC-9 SRM 51-30-5.Sep 28, 2004 · N990AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040344Vane · delaminatedRIGHT FLAP INBOARD FIXED VANE UPPER SURFACE AT XRS 164, LOCATED BETWEEN CHAFE STRIPS WAS DELAMINATED BEYOND LIMITS OF 15 SQ INCHES. REMOVED AND REPLACED INBOARD FIXED VANE IAW DC-9 SRM.Sep 25, 2004 · N990AX · Doug DC941 · Trailing Edge FlapsSDR ABXA040343Intercostal · crackedINTERCOSTAL END FITTING CRACKED AT STA 1072, LEFT SIDE. REPLACED FITTING IAW DC-9 SRM 51-30-5.Sep 23, 2004 · N990AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040342Spar Cap · crackedLEFT PYLON FORWARD UPPER SPAR CAP CRACKED AT SECOND FASTENER INBOARD OF FUSELAGE LOFT LINE. REPAIRED IAW JOB CARD EA 54100011-102 AND EA 54100011-001.Sep 22, 2004 · N990AX · Doug DC941 · Nacelle/Pylon, Frame/Spar/Rib
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