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 ABXA050334Clip · crackedRIGHT FORWARD PYLON HAD A CRACKED ATTACH BRACKET INBOARD AND AFT SIDE RIGHT BUTT LINE 30 APPROXIMATELY AT FLOOR SURFACE. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.Dec 3, 2005 · N954AX · Doug DC941 · Nacelle/Pylon, Main FrameSDR ABXA050321Pan · crackedFORWARD LOWER CARGO DOOR PAN CRACKED AT AFT HOLD OPEN FITTING. REPAIRED CRACKED DOOR PAN IAW SSRM K05159.Dec 2, 2005 · N963AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050320Retainer · crackedCRACKS NOTED ON X-RAY INSPECTION AT CAPTAIN'S OVERHEAD WINDOW RETAINER. REMOVED AND REPLACED CRACKED DOUBLER IAW SRM 51-30-2.Dec 1, 2005 · N963AX · Doug DC941 · Flight Compartment WindowsSDR 0501909753Frame · crackedDURING "H" CHECK, FOUND CRACK IN BULKHEAD FRAME AT BS 37. REPAIRED PER EA 97-204720.Nov 30, 2005 · N753NW · Doug DC941 · Fuselage Main, FrameSDR ABXA050333Fitting · crackedFOUND CRACKED END FITTING AFT SIDE OF PRESSURE BULKHEAD AT LONGERON 29 RIGHT. REPLACED END FITTING IAW DC9 SRM.Nov 30, 2005 · N954AX · Doug DC941 · Wing, Center BoxSDR ABXA050332Skin · crackedFOUND SKIN, FORWARD OF PANEL 1601, HAD A CRACK COMPLETELY ACROSS THE SKIN. MANUFACTURED NEW SKIN AND INSTALLED IAW DC9 51-30-5 AND 51-30-1.Nov 30, 2005 · N954AX · Doug DC941 · Wing, Plate/SkinSDR ABXA050331Skin · corrodedBROKEN FASTENER HEADS AND BULGE IN FUSELAGE SKIN FS 617, LONGERON 30 - LONGERON 29 RIGHT. REPAIRED AREA IAW DC9 SRM 53-04.Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA050330Fitting · corrodedBROKEN FASTENER HEAD AND BULGE IN FUSELAGE SKIN FS 1072. REMOVED AND REPLACED FITTING AT HING 23H, FS 1072 IAW DC9 SRM.Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050329Fitting · crackedRIGHT KEEL FS 675 LONGERON 29 RIGHT CRACKED FITTING. REMOVED AND REPLACED FITTING IAW DC9 SRM.Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050328Fitting · corrodedCORROSION RIGHT KEEL AFT OF PRESSURE BULKHEAD LONGERON 26 RIGHT END CAP. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050327Bulkhead · corrodedFORWARD LOWER CARGO STA 644 BULKHEAD SKIN WAS BULGED FROM LONGERON 30 TO LONGERON 29 LEFT, NUMEROUS RIVETS SHEARED. REMOVED AND REPLACED FINGER DOUBLER IAW DC9 SRM 51-30-1 AND 51-30-5.Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA050326Longeron · corrodedFOUND CORROSION LONGERON 30 END CAP AFT OF PRESSURE BULKHEAD TO FS 648 APPROXIMATELY LEFT KEEL AREA. REMOVED AND REPLACED END CAPS IAW DC9 SRM.Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA050325Bulkhead · corrodedFOUND CORROSION LONGERON 29 LEFT AND ADJACENT LONGERON PRESSURE BULKHEAD TO FS 675 LEFT KEEL AREA. REPAIRED AREA IAW DC9 SRM 53-01.Nov 28, 2005 · N954AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA050324Hinge Bracket · crackedCRACK AT FORWARD BOTTOM EDGE OF FORWARD ENTRY DOOR BELOW BOTTOM HINGE BRACKET. REPAIRED CRACK PAN WITH REPAIR IAW DC9 SRM 52-05.Nov 28, 2005 · N954AX · Doug DC941 · Fuselage, Door HingeSDR ABXA050319Fitting · crackedRT FORWARD OVERWING EXIT DOOR HAD A CRACKED FITTING AT FORWARD LOWER CORNER. REMOVED DAMAGED FITTING AND INSTALLED NEW FITTING IAW SRM 57-30-5 AND 51-30-2.Nov 28, 2005 · N963AX · Doug DC941 · Emergency ExitsSDR ABXA050323Door Frame · crackedAFT ENTRY DOOR JAMB CRACKED UNDER SEAL DEPRESSOR JUST BELOW UPPER RIGHT CORNER. REPAIRED AFT ENTRY DOOR JAMB UNDER SEAL DEPRESSOR BELOW UPPER RIGHT CORNER IAW DC9 SRM 53-01.Nov 23, 2005 · N954AX · Doug DC941 · Fuselage Main, StructureSDR ABXA050322Structure · crackedFOUND CORROSION AND CRACK IN SUBFLOOR, UNDER FIRST OFFICER'S INBOARD SEAT TRACK. CUT OUT CRACK AND CORROSION IN SUBFLOOR, INSTALLED DOUBLER IAW DC9 SRM 53.Nov 22, 2005 · N954AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050288Longeron · crackedLONGERON 28 RIGHT, STA 642 AND 660, CRACKED AND EXFOLIATED. REMOVED AND REPLACED LONGERON AND FRAME IAW DC-9 SRM 51-30-2 AND 51-30-5.Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA050287Fitting · crackedLONGERON END FITTING CRACKED AT FS 642, LONGERON 29 RIGHT. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-5.Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050284Frame · crackedRIGHT AFT OVER WHEEL WELL FRAME FS 775 FORWARD FLANGE CRACKED AT P & G. REPAIRED FRAME IAW JOB CARD EA 53400320-001-2.Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050283Support Fitting · crackedFRAME SUPPORT FITTING HAD CRACK INDICATIONS ON INBOARD SIDE FS 675 AT LONGERON 29 LEFT. REMOVED AND REPLACED SUPPORT FITTING FS 675, LONGERON 29 LEFT IAW DC-9 SRM 51-30-5.Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050282Fitting · crackedLONGERON END CRACKED FS 642 AT LONGERON 26 LEFT. REMOVED AND REPLACED LONGERON END FITTING FS 642, LONGERON 26 LEFT IAW DC-9 SRM 51-30-5.Nov 14, 2005 · N953AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050281Clip · crackedFRAME SUPPORT FITTING HAD CRACK INDICATIONS ON INBOARD SIDE. REMOVED AND REPLACED SUPPORT FITTING FS 675, LONGERON 29 LEFT IAW DC9 SRM 51-30-5.Nov 14, 2005 · N953AX · Doug DC941 · Wing, Attach FittingsSDR ABXA050285Controller · defectiveCABIN PRESSURIZATION LOSS AT TOP OF DESCENT. CABIN PRESSURE EMERGENCY LIGHT ILLUMINATED, EMERGENCY PROCEDURE COMPLETED. NO FURTHER INCIDENT. PERFORMED BITE TEST PROCEDURES AND THE FOWARD CABIN PRESSURE CONTROLLER FAILED TEST. REPLACED FORWARD CABIN PRESSUNov 5, 2005 · N964AX · Doug DC941 · Cabin Pressure Control SystemSDR ABXA050280Floorbeam · corrodedFOUND FLOORBEAM AT STA 1013, RIGHT BUTT LINE 15 AT DOOR UPLATCH BRACKET CORRODED ON LOWER FLANGE. REPAIRED DAMAGED FLOORBEAM IAW DC-9 SSRM DWG K07411.Nov 1, 2005 · N974AX · Doug DC941 · Fuselage Main, Floor BeamSDR ABXA050279Frame · corrodedFOUND FRAME EXFOLIATED AT FS 1041 AT LONGERON 29 LEFT. SPLICED IN NEW FRAME IAW DC-9 SRM.Oct 31, 2005 · N974AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050278Fitting · crackedFOUND LONGERON END CRACKED KEEL AREA 29 RIGHT AT FS 642. REMOVED AND REPLACED LONGERON END FITTING IAW DC-9 SRM.Oct 28, 2005 · N974AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050277Pan · crackedAFT LEFT OVERWING EXIT DOOR HAD CRACK AT LOWER AFT STOP ON DOOR PAN. REMOVED AND REPLACED DOOR ON JC 9542005.Oct 28, 2005 · N974AX · Doug DC941 · Emergency ExitsSDR ABXA050276Door · crackedRIGHT FORWARD OVERWING EXIT DOOR HAD CRACKS AROUND 2 EACH STOPS ON LOWER AFT CORNER DOOR PAN. REPAIRED LOWER AFT CORNER IAW DC-9 SSRM DWG K07390. RE-INSTALLED DOOR STOPS IAW DC-9 SRM 51-30-1 AND 51-30-2. HEAT TREATED IAW DC-9 SRM 51-10-2A.Oct 28, 2005 · N974AX · Doug DC941 · Emergency ExitsSDR ABXA050275Shear Tie · crackedFOUND CRACK IN SHEAR TIE AT STA 1021 BELOW LONGERON 15 RIGHT. REMOVED AND REPLACED SHEAR TIE AT STA 1021 BELOW LONGERON 15 RIGHT IAW DC-9 SRM 51-30-5.Oct 28, 2005 · N974AX · Doug DC941 · Fuselage Internal Mounting StructureSDR ABXA050274Frame · crackedFOUND CRACK ON FRAME AT FASTENER FS 1152 AT LONGERON 15 RIGHT. REPAIRED AREA IAW DC-9 SRM 53-03.Oct 27, 2005 · N974AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050273Skin · crackedTWO 1/4" CRACKS IN FUSELAGE SKIN COMING OUT OF FASTENER HOLE AT FORWARD LOWER CARGO DOOR CUT-OUT UPPER FORWARD CORNER. REPAIRED AREA IAW SR 09530117.Oct 27, 2005 · N974AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA050269Stop Fitting · crackedAFT P DOME DOOR JAMB UPPER RIGHT DOOR STOP FITTING CRACKED. REMOVED AND REPLACED AFT P DOME DOOR JAMB UPPER RIGHT DOOR STOP FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.Oct 23, 2005 · N952AX · Doug DC941 · Fuselage Main, StructureSDR ABXA050266Fitting · corrodedEND FITTING CORRODED JUST INBOARD OF LONGERON 29 RIGHT IN KEEL BEAM AREA LOWER WING CENTER SECTION FS 649. REMOVED AND REPLACED END FITTING IAW DC-9 SRM 51-30-5.Oct 20, 2005 · N952AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050268Keelbeam · crackedEND FITTING SIDE SUPPORT CRACKED ON LEFT SIDE OF KEEL BEAM CENTER SUPPORT LONGERON 30, FS 646 APPROXIMATELY. REMOVED AND REPLACED END FITTING AT STA 646, LONGERON 30 IAW DC-9 SRM 51-30-5.Oct 20, 2005 · N952AX · Doug DC941 · Fuselage Main, KeelSDR ABXA050267Fitting · corrodedEND FITTING CORRODED LONGERON 29 LEFT APPROXIMATELY STA FS 649, LOWER WING CENTER SECTION IN KEEL BEAM AREA. REMOVED AND REPLACED LONGERON END FITTING IAW DC-9 SRM 51-30-5.Oct 20, 2005 · N952AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050265Shear Tie · crackedSHEAR TIE CRACKED AT STA 1021 BETWEEN LONGERON 15 RIGHT AND LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5 AND 51-30-2.Oct 19, 2005 · N952AX · Doug DC941 · Fuselage Internal Mounting StructureSDR ABXA050264Attach Bracket · crackedATTACH BRACKET ON AFT SIDE OF PYLON BULKHEAD AT LONGERON 17 RIGHT WAS CRACKED. REMOVED AND REPLACED BRACKET IAW DC9 SRM 51-30-2.Oct 19, 2005 · N952AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050249Battery · defectiveDURING PRE-DEPARTURE CHECK FOUND EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00.Oct 17, 2005 · N990AX · Doug DC941 · Emergency LightingSDR ABXA050258Cargo Track · corrodedFORWARD LOWER CARGO LEFT TRACK HAD EXFOLIATED CORROSION AT TWO ATTACH FASTENERS BETWEEN STA 218 AND 237. REPLACED BAD SECTION OF TRACK IAW DC-9 SSRM K05159 DRAWING.Oct 12, 2005 · N962AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050261Bulkhead · crackedAFT PRESSURE BULKHEAD DOOR UPPER LT CORNER 13 DOUBLER HAD RADIAL CRACK EXTENDING FROM STOP DRILL. CRACK EXCEEDED APPLICABILITY AND CRACK REPAIR LIMITS FOR PREVIOUS J060088-1 ANGLE REPAIR. STOP DRILLED CRACKS AND REPAIRED IAW SRM.Oct 11, 2005 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA050257Intercostal · crackedAFT ASSY COMPARTMENT INTERCOSTAL BETWEEN FS 1114 AND FS 1133, LONGERON 17 RIGHT AND LONGERON 16 RIGHT HAD A CRACK ON BOTTOM FORWARD SIDE. FABRICATED AND INSTALLED REPAIR ANGLE AS REQUIRED IAW DC-9 SRM K05159 DRAWING.Oct 11, 2005 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050260Skin · corrodedFUSELAGE SKIN BULGED AT STA 579, LONERON 30, EVIDENCE OF CORROSION INTERNAL. REMOVED INTERNAL CORRODED DOUBLER / INSTALLED NEW DOUBLER IAW SRM.Oct 10, 2005 · N962AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA050256Skin · crackedFUSELAGE CRACK AT STA. 1087, LONGERON 2 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.Oct 10, 2005 · N962AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA050254Frame · crackedADDITIONAL CRACK FOUND IN LEFT AFT MAIN FRAME FORWARD FLANGE. FRAME IS OUT OF REPAIR LIMITS IAW ES00916 DUE TO CRACKS IN BOTH FLANGES. REPLACED MAIN FRAME ON EA 53400325-001-5.Oct 7, 2005 · N967AX · Doug DC941 · Fuselage Main, FrameSDR ABXA050245Pushrod · damagedUNABLE TO RAISE GEAR HANDLE PAST UPLATCH POSITION. NOSEWHEEL STEERING STILL ENGAGED AFTER TAKEOFF. FOUND GROUND SHIFT LOWER SECTOR PUSH ROD BOLT WITH MISSING HARDWARE. REMOVED AND REPLACED GROUND SHIFT LOWER SECTOR PUSH ROD BOLT AND HARDWARE IAW DC9 MM 20-1Oct 7, 2005 · N969AX · Doug DC941 · Nose/Tail Landing GearSDR ABXA050243Fitting · leakingAT FLIGHT LEVEL 350, NOTICED CREW 02 BOTTLE WAS LOSING PRESSURE. DESCENDED TO LOWER ALTITUDE (170). REMAINDER OF FLIGHT, PRESSURE REMAINED AT 1000 PSI. SERVICED CREW 02 BOTTLE TO 1800 (WAS 1000) PSI. FOUND LINE FROM BOTTLE TO VALVE FITTING ON BULKHEAD LEAKOct 7, 2005 · N964AX · Doug DC941 · Crew Oxygen SystemSDR ABXA050253Support Fitting · crackedLEFT SUPPORT FITTING CRACKED CANTED BULKHEAD 1219, LT OF RUDDER TORQUE TUBE MECHANISM. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-2.Oct 6, 2005 · N967AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050252Seat Track · crackedSEAT TRACK WAS CRACKED 2 PLACES BETWEEN FS 160 AND 200 AT LEFT BUTT LINE 41.5. REPAIRED DAMAGED AREAS (2 EA) IAW DC-9 SSRM DWG K05159.Oct 6, 2005 · N967AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050251Fitting · crackedLEFT INBOARD SPOILER HAD AN APPROXIMATE .1562 INCH CRACK IN THE CENTER DOUBLER ABOVE THE CENTER DRIVE FITTING. BLENDED CRACK IAW REA D957-52510.Oct 6, 2005 · N967AX · Doug DC941 · Spoilers
Back to Douglas DC-9-41