Douglas DC-9-41

Service difficulty reports · 2,671

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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 ABXA9500483Skin · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A REPAIR AT THE AFT LOWER CORNER OF THE LEFT FORWARD ENTRY DOOR NOT IAW DC-9 SRM. REPAIRED DOOR JAMB SKIN IAW ABX REA D953-11405-MR.Apr 18, 1995 · N990AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 9506859759Fitting · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE AFT CARGO DOOR BEAM END FITTINGS NR 3 AFT AND NR 4 FORWARD AND AFT. REPLACED FITTINGS PER SRM 51-30-2.Apr 18, 1995 · N759NW · Doug DC941 · Cargo/Baggage DoorsSDR ABXA9500471Trap Panel · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT TRAPEZOIDAL PANEL CRACKED AT THE MAIN LANDING GEAR UP STOP BUMPER. REPLACED LEFT TAPEZOIDAL PANEL IAW DC-9 SB 53-182.Apr 12, 1995 · N990AX · Doug DC941 · Fuselage Miscellaneous StructureSDR 9506139759Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN LEFT HALF OF LONGERON 30 END FITTING AT FS 642. REPLACED FITTING PER SRM 51-30-5.Apr 12, 1995 · N759NW · Doug DC941 · Fuselage Miscellaneous StructureSDR 9505609760Link · failedLOUD NOISE AND VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND THE RIGHT NOSE GEAR DOOR OPEN. REPLACED DOOR LINK. AIRCRAFT RETURNED TO SERVICE.Apr 12, 1995 · N760NW · Doug DC941 · Landing Gear Door Retract SectionSDR ABXA9500357Link · wornDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR WHERE ROD ASSEMBLIES MEET HAD EXCESSIVE PLAY. REPLACED LINK ASSEMBLY AND ATTACHING HARDWARE IAW DC-9 OVERHAUL MANUAL.Apr 11, 1995 · N971AX · Doug DC941 · Landing Gear Door Retract SectionSDR 9506089753Longeron · crackedDURING PERIODIC CHECK, FOUND (2) .5 INCH CRACKS RADIATING FROM LONGERON 17R TO FS 389 FRAME ATTACH FASTENERS. REPAIRED LONGERON PER SRM 53-02 FIG 4 AND EA 97-097460.Apr 11, 1995 · N753NW · Doug DC941 · Fuselage Main, Longeron/StringerSDR 9505569762Fuel Line · leakingON DESCENT, NR 2 ENGINE WOULD NOT RESPOND TO POWER LEVER MOVEMENT. FLIGHT LANDED IN PVD WITHOUT INCIDENT. THE ENGINE WAS SHUT DOWN WHILE TAXIING TO THE GATE. MAINTENANCE FOUND FUEL LEAKING FROM THE LINE CONNECTING THE P AND D VALVE TO THE FUEL OIL COOLER. Apr 11, 1995 · N762NW · Doug DC941 · Engine Fuel DistributionSDR 9506049753Support · crackedDURING PERIODIC CHECK, FOUND .5 INCH CRACK RADIATING FROM FS 408 VERTICAL FLOORBEAM SUPPORT ATTACH FASTENER, RIGHT OUTBOARD END OF BEAM. REPAIRED PER EA 97-097464.Apr 10, 1995 · N753NW · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500365Stringer · corrodedDURING C-CHECK INSPECTION DURING COMPLIANCE OF AD 90-18-03, SB 57-98, FOUND CORRODED HILOCKS ON FORWARD SIDES OF LEFT WING STRINGER 18, 19, 21 AND 22 AT STA XCW 58. REPLACED HILOCKS IAW DC-9 SRM 51-30-5.Apr 8, 1995 · N971AX · Doug DC941 · Wing, Longeron/StringerSDR ABXA9500364Stringer · corrodedDURING C-CHECK INSPECTION DURING COMPLIANCE OF AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER NR 18 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5.Apr 8, 1995 · N971AX · Doug DC941 · Wing, Longeron/StringerSDR ABXA9500363Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER NR 17 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5.Apr 8, 1995 · N971AX · Doug DC941 · Wing, Longeron/StringerSDR ABXA9500362Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON STRINGER NR 15 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5.Apr 8, 1995 · N971AX · Doug DC941 · Wing, Longeron/StringerSDR ABXA9500361Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER NR 13 AT XWC 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5.Apr 8, 1995 · N971AX · Doug DC941 · Wing, Longeron/StringerSDR ABXA9500360Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER 12 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5.Apr 8, 1995 · N971AX · Doug DC941 · Wing, Longeron/StringerSDR ABXA9500359Srtinger · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND CORRODED FASTENERS ON RIGHT WING STRINGER 11 AT XCW 58. REPLACED WITH HILOCKS IAW DC-9 SRM 51-30-5.Apr 8, 1995 · N971AX · Doug DC941 · Wing, Longeron/StringerSDR ABXA9500358Skin · dentedDURING C-CHECK INSPECTION, FOUND DENT AT FS 389R, LONGERON 18R AND 19R. REPAIRED DENT IAW ABX REA D953-11392-MR.Apr 7, 1995 · N971AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 9505959755Panel · disbondingDURING FLIGHT DTW-ATL, FOUND THAT SHEET METAL WAS LOOSE AND FLAPPING UNDER THE LEFT INBOARD SPOILER PANEL. CONTINUED TO ATL WITHOUT FURTHER INCIDENT. FOUND PREVIOUS REPAIR DISBONDING. REPLACED SPOILER PER MM 27-60.Apr 5, 1995 · N755NW · Doug DC941 · SpoilersSDR ABXA9500505Spoiler Panel · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT OUTBOARD SPOILER PANEL DELAMINATED. REPLACED PANEL IAW DC-9 MM 27-61-1.Apr 4, 1995 · N990AX · Doug DC941 · SpoilersSDR ABXA9500496Frame · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND RIGHT MAIN FUSELAGE FRAME AT FS 737 CRACKED. REPAIRED RIGHT MAIN FRAME AT FS 737 IAW DC-9 SB 53-131.Apr 4, 1995 · N990AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9500460Skin · delaminatedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT OUTBOARD SPOILER PANEL DELAMINATED. REPLACED LEFT OUTBOARD SPOILER PANEL IAW DC-9 MM CHAPTER 27-61-1.Apr 4, 1995 · N990AX · Doug DC941 · SpoilersSDR ABXA9500459Skin · delaminatedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING INBOARD SPOILER TRAILING EDGE DELAMINATED. REPLACED RIGHT INBOARD SPOILER PANEL IAW DC-9 MM CHAPTER 27-61-1.Apr 4, 1995 · N990AX · Doug DC941 · SpoilersSDR ABXA9500497Frame · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND THE RIGHT FUSELAGE MAIN FRAME CRACKED AT FS 756. REPLACED RIGHT MAIN FRAME IAW DC-9 SRM 51-30-1, 51-30-2 AND SB 53-131.Mar 31, 1995 · N990AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9500482Channel · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A MOUNT CHANNEL CRACKED AT FS 1152 AND LONGERON 14R. REPAIRED CHANNEL IAW ABX REA D925-11297 AND RE-INSTALLED CHANNEL IAW DC-9 SRM 51-30-2.Mar 31, 1995 · N990AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500481Skin · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT WING LEADING EDGE CRACKED JUST INBOARD OF THE NR 5 SLAT OUTBOARD TRACK. REPAIRED CRACK IAW ABX REA D957-11284.Mar 31, 1995 · N990AX · Doug DC941 · Wing, Plate/SkinSDR ABXA9500476Skin · gougedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING LOWER SKIN GOUGED AND CHAFED AT TRAILING EDGE, OUTBOARD OF THE MAIN LANDING GEAR DOOR JAMB. REPAIRED RIGHT WING LOWER SKIN IAW ABX REA D957-11255-MR.Mar 31, 1995 · N990AX · Doug DC941 · Wing, Plate/SkinSDR ABXA9500461Doubler · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT WING UPPER MAIN LANDING GEAR DOUBLER CORRODED IN PREVIOUS BLENDOUTS. REPLACED RIGHT WING UPPER MAIN LANDING GEAR DOUBLER IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Mar 31, 1995 · N990AX · Doug DC941 · Wing Miscellaneous StructureSDR ABXA9500356Base · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT FLAP BASE FOR SPRING. REPLACED WITH NEW BASE FOR SPRING IAW DC-9 OVERHAUL MANUAL 27-50-1.Mar 31, 1995 · N990AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9500479Skin · gougedWHILE COMPLYING WITH C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A GOUGE AFT OF A PREVIOUS REPAIR AT FS 332 AND LONGERON 25R. REPAIRED SKIN IAW ABX REA D953-11278-MR.Mar 30, 1995 · N990AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9500462Blkdh · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT PRESSURE BULKHEAD LOWER TEE CAP AT FS 1072 CORRODED AT LONGERON 30. REPLACED AFT PRESSURE BULKHEAD LOWER TEE CAP SECTION IAW DC-9 SRM CHAPTER 51-30-2 AND 51-30-5.Mar 30, 1995 · N990AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9500480Door Jamb · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE WEB AROUND THE AFT BAG BIN DOOR JAMB CORRODED. REPAIRED WEB IN JAMB AREA IAW ABX REA D953-11279-MR.Mar 29, 1995 · N990AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500315Angle · crackedDURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 2 ENGINE LOWER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.Mar 29, 1995 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9500314Angle · crackedDURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 2 ENGINE UPPER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-112080-MR.Mar 29, 1995 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9500313Angle · crackedDURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND THE NR 1 ENGINE LOWER PYLON TO FUSELAGE ATTACH ANGLE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.Mar 29, 1995 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9500312Angle · crackedDURING COMPLIANCE OF CORROSION TASK 80-54300, FOUND NR 1 ENGINE UPPER PYLON TO FUSELAGE ATTACH ANGLE TO BE CRACKED. REPAIRED IAW ABX REA D954-11280-MR.Mar 29, 1995 · N975AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9500478Bulkhead · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A CRACK IN THE UPPER LEFT HORIZONTAL EDGE OF THE AFT VENTRAL STAIR DOOR. REPAIRED IAW ABX REA D953-11275-SB REV A.Mar 28, 1995 · N990AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9500474Skin · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A CRACK INDICATION COMING OUT OF AFT LOWER PRESSURE STOP HOLE ON THE FORWARD ENTRY DOOR JAMB. REPAIRED SKIN AT FORWARD ENTRY DOOR IAW ABX REA D953-11122-MR.Mar 28, 1995 · N990AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9500498Frame · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 78-07-05 AND SB 53-131, FOUND THE LEFT FUSELAGE MAIN FRAME AT FS 756 CRACKED. REPLACED MAIN FRAME AT FS 756 IAW DC-9 SB 53-131.Mar 27, 1995 · N990AX · Doug DC941 · Fuselage Main, FrameSDR ABXA9500477Skin · gougedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR BETWEEN FS 440 AND 462, FROM LONGERON 24L AND 25L WAS GOUGED AND DOUBLE DRILLED. REPAIRED FUSELAGE SKIN IAW ABX REA D953-11258-MR.Mar 27, 1995 · N990AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9500475Intercostal · gougedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN ANGLE GOUGED AT FS 184 AND LBL 56, ABOVE THE AIR STAIR DOOR SWITCH. REPAIRED INTERCOSTAL IAW ABX REA D953-11252-MR.Mar 25, 1995 · N990AX · Doug DC941 · Fuselage Miscellaneous StructureSDR 9505009760Line · crackedNR 1 ENGINE EPR INDICATION WAS LOW ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED A CRACKED PT7 LINE. THE SYSTEM CHECKED OK ON RUN-UP. THE AIRCRAFT RETURNED TO SERVICE.Mar 25, 1995 · N760NW · Doug DC941 · Engine Pressure Ratio (EPR)SDR 9504789762Fitting · crackedDURING LINE CHECK, FOUND CRACK IN LONGERON 30 END FITTING AT FS 642. REPLACED FITTING PER SRM 51-30-5.Mar 25, 1995 · N762NW · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500464Blkhd Former · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A RADIAL STIFFENER CRACKED ON FORWARD FACE OF AFT PRESSURE BULKHEAD FS 1072 AND LONGERON 14L. REPLACED STIFFENER IAW DC-9 SB 53-166 AND SRM 51-30-1, 51-30-2 AND 51-30-5.Mar 24, 1995 · N990AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9500463Support · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT VERTICAL FRAME SUPPORT CRACKED AT FS 908 IN AFT BAG BIN. REPLACED FRAME SUPPORT IAW DC-9 SRM 51-30-2 AND 51-30-5.Mar 24, 1995 · N990AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500466Blkhd Support · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL WALL SUPPORT FOR FORWARD BULKHEAD IN AFT BAG BIN CRACKED AT LONGERON 22 R. REPLACED SUPPORT IAW DC-9 SRM 51-30-2.Mar 23, 1995 · N990AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9500465Blkhd Support · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE HORIZONTAL WALL SUPPORT FOR FORWARD BULKHEAD IN AFT BAG BIN CRACKED AT 22R. REPLACED SUPPORT IAW DC-9 SRM 51-30-2.Mar 23, 1995 · N990AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9500470Panel · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE RIGHT TRAPEZOIDAL PANEL CRACKED AT THE MAIN LANDING GEAR UP STOP BUMPER PAD. REPLACED RIGHT TRAPEZOIDAL PANEL IAW DC-9 SB 53-182.Mar 22, 1995 · N990AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9500329Rib · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE ACCOMPLISHING DC-9 FLAP OFF WING INSPECTION, FOUND LEVEL II CORROSION ON THE RIGHT FLAP INBOARD RIB BEARING BORE. REPAIRED INBOARD RIB HOLE FOR BEARING IAW DC-9 SRM 57-02, FIGURE 7, PAGE 11.Mar 21, 1995 · N990AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9500467Skin · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE AFT FUSELAGE SKIN CORRODED ALONG LONGERON 20L BETWEEN FS 1197 AND FS 1208. REPLACED SKIN SECTION IAW DC-9 SRM 51-30-2.Mar 20, 1995 · N990AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9500243Bushing · wornDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING WORN IN THE ARM ASSEMBLY ON THE RIGHT OUTBOARD MAIN LANDING GEAR DOOR. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.Mar 19, 1995 · N956AX · Doug DC941 · Landing Gear Doors
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