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 ABXA9701113Fitting · crackedDURING C-CHECK, FOUND THE RIGHT ENGINE PYLON REAR SPAR UPPER FITTING CRACKED AT THE FWD INBD CORNER. REPLACED FITTING IAW DC9 SRM.Jun 6, 1997 · N955AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA9701112Fitting · corrodedDURING C-CHECK, FOUND THE LEFT FLAP INBOARD FWD HINGE FITTING CORRODED. REPLACED THE FWD HINGE FITTING IAW DC9 MM 57-40-01.Jun 6, 1997 · N955AX · Doug DC941 · Wing, Control Surface Attach FittingsSDR ABXA9701366Panel · delaminatedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE TRAILING EDGE PANEL JUST INBOARD OF LEFT AILERON SECTOR CORRODED AND DELAMINATED. REMOVED AND REPLACED PANEL IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-3.Jun 5, 1997 · N962AX · Doug DC941 · Wing, Plate/SkinSDR ABXA9701372Spar Cap · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT WING UPPER FRONT SPAR CAP CORRODED AT XOS240. REPAIRED FRONT SPAR UPPER CAP IAW ABX REA D957-19643.Jun 4, 1997 · N962AX · Doug DC941 · Wing SparSDR ABXA9701111Rib · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE 6TH RIB CRACKED. REPAIRED RIB IAW DC9 SRM 51-30-5.Jun 4, 1997 · N955AX · Doug DC941 · Vertical Stabilizer, Spar/RibSDR ABXA9701110Longeron · crackedDURING C-CHECK, FOUND LONGERON 13R AT STA 1152 CRACKED AND CORRODED. REPLACED LONGERON SECTION IAW DC9 51-30-2.Jun 4, 1997 · N955AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA9701109Rib · crackedDURING C-CHECK, FOUND 4TH RIB FROM THE BOTTOM INSIDE THE VERTICAL STABILIZER LEADING EDGE CRACKED. REPAIRED RIB IAW DC9 SRM 51-30-5.Jun 4, 1997 · N955AX · Doug DC941 · Vertical Stabilizer, Spar/RibSDR ABXA9701107Rib · crackedDURING C-CHECK, FOUND THE VERTICAL STABILIZER LEADING EDGE, 5TH RIB FROM BOTTOM CRACKED. REPAIRED RIB IAW DC9 SRM 51-30.Jun 4, 1997 · N955AX · Doug DC941 · Vertical Stabilizer, Spar/RibSDR ABXA9701375Skin · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND A FUSELAGE SKIN CRACK AT FS 58 ON RIGHT SIDE. REPAIRED CRACK IAW DC-9 SRM 53-01.Jun 3, 1997 · N962AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9701106Fitting · corrodedDURING COMPLIANCE WITH AD 82-06-02 AND 92-22-08, FOUND HORIZONTAL STABILIZER UPPER AFT FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-1.May 31, 1997 · N971AX · Doug DC941 · Horizontal Stabilizer StructureSDR ABXA9701104Frame · crackedDURING C-CHECK, FOUND THE LEFT MAIN FRAME STATION 737, CRACKED ON FWD AND AFT UPPER FLANGES. REPLACED FRAME IAW DC9 S/B 53-131.May 31, 1997 · N971AX · Doug DC941 · Fuselage Main, FrameSDR 9711589760Retract Mech · malfunctionedON APPROACH DURING GEAR EXTENSION, NOSE GEAR DID NOT COME DOWN. NO GREEN OR RED LIGHTS, HYDRAULIC PRESSURE AND QUANTITY WERE NORMAL. CYCLED GEAR AND NOSE GEAR CAME DOWN NORMALLY. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE JACKED AIRCRAFT AND CYCLED GEAR 8May 31, 1997 · N760NW · Doug DC941 · Landing Gear Retraction/Extension SystemSDR GTIA9700302Prox Sensor · failedACY - FLT 112 - LEFT RED GEAR UNSAFE LIGHT STAYED ON FOR ENTIRE FLIGHT. PERFORMED APPROPRIATE CHECK LISTS AND CONTINUED FLIGHT PER RESTRICTIONS IN FCOM. INSPECTED AND CLEANED ALL ASSOCIATED PROX SENSORS AND TARGETS ON LEFT MAIN LANDING GEAR. RELEASED FOR TEMay 29, 1997 · N130NK · Doug DC941 · Landing Gear Position and WarningSDR ABXA9701095Panel · crackedDURING C-CHECK, FOUND RIGHT WING PANEL NR 1220 CRACKED. REPAIRED PANEL IAW DC9 SRM 57-06.May 28, 1997 · N951AX · Doug DC941 · Wing, Plate/SkinSDR GTIA9700289Anti Skid System · malfunctionedMYR - DURING TAXI OUT, THE LT AND RT INBD ANTI-SKID ANNUNCIATOR ILLUMINATED. RETURNED TO GATE. TRANSFERRED TO DMI NR 00552 PER MEL 32-4. PLACARD INSTALLED, DISPATCH NOTIFIED. PERFORMED ANTI-SKID SYSTEM TEST IAW DC-9 MM 32-43-0. OPS CHECK GOOD. DISPATCH May 27, 1997 · N130NK · Doug DC941 · Brake Anti-Skid SectionSDR ABXA9701093Torsion Bar · corrodedDURING C-CHECK, FOUND RW INBD SPOILER TORSION BAR AT CAM ASSY IS CORRODED. REMOVED AND REPLACED INBD SPOILER TORSION BAR, CAM AND REACTION ARM IAW DC9 MM 27-61-6.May 24, 1997 · N951AX · Doug DC941 · Drag Control SystemSDR ABXA9701092Web · crackedDURING C-CHECK, FOUND THE RT CUSP WEB AT F/STA 1039 RBL 46 CRACKED. REPAIRED CUSP WEB IAW DC9 SRM 53-01, FIGURE 2 AND 51-30-1.May 24, 1997 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701091Torsion Bar · corrodedDURING C-CHECK, FOUND LW INBD SPOILER TORSION BAR AT CAM ASSY IS CORRODED. REMOVED AND REPLACED INBD SPOILER TORSION BAR, CAM AND REACTION ARM IAW DC9 TEMP REV 27-61-6 AND 27-453.May 24, 1997 · N951AX · Doug DC941 · Drag Control SystemSDR ABXA9701090Seat Track · corrodedDURING C-CHECK, FOUND THE SEAT TRACK AT F/STA 294 TO 484 BL 0 CORRODED. REMOVED AND REPLACED CORRODED SECTION OF SEAT TRACK IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5.May 24, 1997 · N951AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA9701089Floorbeam · crackedDURING C-CHECK, FOUND FLOORBEAM CRACKED AT F/STA 237, BL 0. REPAIRED IAW ABX REA D953-19459-MR.May 24, 1997 · N951AX · Doug DC941 · Fuselage Main, Floor BeamSDR ABXA9701088Panel · corrodedDURING C-CHECK, FOUND THE INTERIOR FUSELAGE FLANGE FOR THE LEFT KIDNEY PANEL NR 5115 CORRODED AROUND AND UNDER SEVERAL NUT PLATES. REPAIRED IAW ABX REA D953-19588.May 24, 1997 · N951AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9701087Jamb · corrodedDURING C-CHECK, FOUND THE DOOR JAMB WEB AT F/STA 965 TO 973 LONG 26R TO 27R CORRODED. REPAIRED IAW SBX DC9 SRM DWG K05485-7005.May 24, 1997 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701086Vane · delaminatedDURING C-CHECK, FOUND THE RW MOVEABLE VANE DELAMINATED UNDER THE CHAFE STRIP. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN.May 24, 1997 · N951AX · Doug DC941 · Trailing Edge FlapsSDR ABXA9701085Splice Plate · corrodedDURING C-CHECK, FOUND THE FUSELAGE FRAME SPLICE PLATE F/STA 973, LONG 27L TO 29L CORRODED. REPLACED SPLICE PLATE IAW DC9 SRM 51-30-2 AND 51-10-3.May 24, 1997 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701365Door · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND LEFT MAIN GEAR FLYING DOOR CORRODED ON LOWER FORWARD CORNER. REMOVED AND REPLACED DOOR IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5 AND DC-9 MAINTENANCE MANUAL CHAPTER 32-12-1.May 22, 1997 · N962AX · Doug DC941 · Landing Gear DoorsSDR ABXA9701039Fitting · crackedDURING C-CHECK, FOUND VERTICAL FLOOR SUPPORT FITTING CRACKED AT F/STA 718 RBL 44. REPLACED FITTING (P/N 3925812-2) IAW DC9 MM 51-30-2.May 22, 1997 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701038Intercostal · crackedDURING C-CHECK, FOUND INTERCOSTAL AT LONG 29L F/STA 351 TO 370 CRACKED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2.May 22, 1997 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701037Longeron · corrodedDURING C-CHECK, FOUND LONGERON 23L AT STA 992 IS HEAVILY CORRODED. REMOVED AND REPLACED LONGERON IAW DC9 SRM 51-30-2.May 22, 1997 · N951AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA9701036Cusp Web · crackedDURING C-CHECK, FOUND CUSP WEB AT STA 1023 AND LBL 56 CRACKED. REPAIRED CUSP WEB IAW DC9 SRM 53-01.May 22, 1997 · N951AX · Doug DC941 · Elevator StructureSDR ABXA9701035Skin · corrodedDURING C-CHECK, FOUND SKIN BULGED AT NOSE LANDING GEAR DOOR AFT HINGE. REPAIRED IAW DC9 SRM 53-04.May 22, 1997 · N951AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9701034Skin · crackedDURING C-CHECK, FOUND SKIN CRACKED AT LONGERONS 27 AND 28 LT AT F/STA 110. REPAIRED CRACKED SKIN IAW DC9 SRM 53-04.May 22, 1997 · N951AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9701033Spar Cap · crackedDURING C-CHECK, FOUND LT HORIZONTAL STABILIZER UPPER REAR SPAR CAP CRACKED AT OUTBOARD END. REPAIRED SPAR CAP IAW DC9 SRM 55-02.May 22, 1997 · N951AX · Doug DC941 · Horizontal Stabilizer, Spar/RibSDR ABXA9701032Intercostal · crackedDURING C-CHECK, FOUND CRACKED INTERCOSTAL AT F/STA 851 AND RBL 02. REPAIRED IAW DC9 ABX SUPPLEMENTAL SRM DWG NR K05159.May 22, 1997 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701031Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN AT F/STA 619 AND LONGERON 30 BULGED AND CORRODED. REPAIRED IAW DC9 SRM 53-04.May 22, 1997 · N951AX · Doug DC941 · Fuselage Main, Plate/SkinSDR 9710059763Clips · out of adjustDURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO PULL THE EXTERIOR RELEASE HANDLE FROM THE RETAINING CLIPS. ALSO, FOUND THAT 6 ALIGNMENT PINS BOTTOM OUT. SHIMMED ALIGNMENT PINS AND ADJUSTED CLIPS, FUNCTIONAL CHECK OK.May 20, 1997 · N763NW · Doug DC941 · Aerodynamic FairingsSDR ABXA9701024Brake Hose · fracturedCOMPLETE LOSS OF HYDRAULIC FLUID OCCURED ON RIGHT SYSTEM WHEN LANDING GEAR WAS LOWERED. REPLACED NR 3 BRAKE HOSE, SERVICED, BLED AND LEAK CHECKED IAW DC9 MM 32-04-01.May 19, 1997 · N953AX · Doug DC941 · Landing Gear Brake SystemSDR ABXA9701045Panel · delaminatedDURING D-INSPECTION, FOUND THE LEFT WING OUTBOARD SPOILER PANEL DELAMINATED. *S/D* REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS.May 18, 1997 · N960AX · Doug DC941 · SpoilersSDR ABXA9701043Panel · delaminatedDURING D-INSPECTION, FOUND THE LEFT WING INBOARD SPOILER PANEL DELAMINATED. *S/D* REPAIRED UNIT COMPLETE.May 18, 1997 · N960AX · Doug DC941 · SpoilersSDR 9709869754Valve · failedAS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE EIGHTH STAGE CHECK VALVE, OPERATIONAL CHECK OK.May 16, 1997 · N754NW · Doug DC941 · Compressor Bleed ControlSDR ABXA9700999Diode · failedDETECTED STRONG ELECTRICAL ODOR DURING CRUISE FLIGHT. AT FL 330 DECLARED EMERGENCY, MADE NON-SCHEDULED PRECAUTIONARY LANDING AT AMARILLO, TEXAS. CLEANED CORROSION FROM REVERSE CURRENT DIODES R7-48 AND R7-49, OPS CHECK NORMAL.May 15, 1997 · N968AX · Doug DC941 · DC Power Distribution SystemSDR ABXA9701046Door Assy · crackedDURING D-INSPECTION, FOUND THE RIGHT MAIN LANDING GEAR DOOR PAN CRACKED AT FORWARD SIDE OF ACTUATOR ATTACH BRACKET. REMOVED AND REPLACED RIGHT MLG DOOR IAW DC9 SUPPLEMENTAL MAINTENANCE MANUAL CHAPTER 32-12-01.May 12, 1997 · N960AX · Doug DC941 · Landing Gear DoorsSDR ABXA9701044Door · crackedDURING D-INSPECTION, FOUND THE LEFT MAIN LANDING GEAR WHEEL WELL DOOR CRACKED AT FORWARD UPPER CORNER OF ACTUATOR ATTACH FITTING. REPLACED LEFT MLG W/WELL DOOR IAW DC-9 SMM 32-12-01.May 12, 1997 · N960AX · Doug DC941 · Landing Gear DoorsSDR TWAA9756001Oil System · overservicedSTL - FLT 132 - DURING APPROACH WITH APU RUNNING, BOTH PACKS EMITTED SMOKE AND OILY ODOR. APU, MFG PN 5910050527, MANUFACTURED BY DOUGLAS AIRCRAFT CO., PLACARDED INOPERABLE DUE TO OIL LEAK. OPS CHECK NORMAL. CHECK C - 3-18-97. INVESTIGATION OF SMOKE AND OIMay 7, 1997 · N934L · Doug DC941 · APU Oil SystemSDR ABXA9701258Door · crackedOVERWING EXIT DOOR HAS PAN CRACKED AT STOP NR 14. REPAIRED IAW ABX REA D952-19963-MR AND SRM 51-10-3.May 7, 1997 · N962AX · Doug DC941 · Emergency ExitsSDR ABXA9701243Door · crackedOVERWING EMERGENCY DOOR HAD PAN CRACKED AT STOP NR 14. REPAIRED IAW ABX REA D952-19965-MR.May 7, 1997 · N962AX · Doug DC941 · Emergency ExitsSDR ABXA9701242Door · crackedOVERWING EMERGENCY DOOR HAD PAN CRACKED AT STOP NR 14. REPAIRED CRACK IAW ABX REA D952-19964-MR.May 7, 1997 · N962AX · Doug DC941 · Emergency ExitsSDR ABXA9701221Door · crackedDURING C-CHECK, FOUND OVERWING DOOR CRACKED AT STOPS NR 5, 8 AND 12. REPAIRED IAW DC-9 SRM 51-30-2 AND ABX REA D952-19962-MR.May 7, 1997 · N962AX · Doug DC941 · Emergency ExitsSDR ABXA9701053Keel Frame · crackedDURING D-INSPECTION, FOUND THE RIGHT LOWER KEEL FRAME CRACKED AT FS 675 IN CANTED KEEL AREA. REPLACED FRAME AND CLIP IAW DC9 SRM CHAPTERS 51-30-2 AND 51-30-5.May 7, 1997 · N960AX · Doug DC941 · Fuselage Main, KeelSDR ABXA9701058Fitting · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING NR 3 SLAT CENTER ATTACH FITTING CORRODED. *S/D* REPAIRED IAW DC-9 SRM 57-55-00.May 6, 1997 · N960AX · Doug DC941 · Leading Edge DevicesSDR ABXA9701057Slat · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING NR 4 SLAT CORRODED INBOARD OF CENTER ATTACH FITTING. *S/D* REPAIRED UNIT COMPLETE.May 6, 1997 · N960AX · Doug DC941 · Leading Edge Devices
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