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 0201409754Hose · not seatedWHILE CRUISING AT ALTITUDE, THE AIRCRAFT HAD A LOSS OF PRESSURIZATION AND INITIATED AN EMERGENCY DESCENT TO 10,000 FEET. DURING DESCENT, COM REQUIRED THE CREW TO BE ON OXYGEN. THE CAPTAIN'S MASK WOULD NOT SUPPLY OXYGEN DURING THE EMERGENCY DESCENT. THE TESTApr 8, 2002 · N754NW · Doug DC941 · Crew Oxygen SystemSDR 0201129754Door Seal · missingCRUISING AT 24,000 FEET WITH WING AND ENGINE ANTI-ICE ON, THE CABIN BEGAN CLIMBING UNCONTROLLABLY. CREW FOLLOWED COM PROCEDURES AND PERFORMED AN EMERGENCY DESCENT. FLIGHT ATTENDANT REPORTED A LOUD SQUEAL IN THE AFT SECTION OF THE CABIN. FLIGHT CONTINUED TO DFWApr 8, 2002 · N754NW · Doug DC941 · Cabin Pressure Control SystemSDR ABXA010824Fitting · corrodedFRAME FOOT FITTING CORRODED AT FS 927 LEFT. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5.Apr 3, 2002 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA010823Angle · crackedCRACKED ANGLE AT STATION 775, RIGHT UPPER WHEEL WELL AT LONGERON 20. REPLACED ANGLE AND REPAIRED AREA IAW DC-9 SRM.Apr 3, 2002 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA010827Fitting · corrodedFRAME FOOT FITTING AT STATION 927 RIGHT WAS CORRODED. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5.Apr 3, 2002 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA010826Angle · crackedANGLE CRACKED ON AFT SIDE OF FRAME AT STATION 1021, BETWEEN LONGERON 15 LEFT AND LONGERON 16 LEFT. REPLACED ANGLE IAW DC-9 SRM 53-03.Apr 3, 2002 · N965AX · Doug DC941 · Fuselage Main, StructureSDR ABXA010825Fitting · corrodedFRAME FOOT FITTING CORRODED AT STATION 946 LEFT. REPLACED FRAME FOOT IAW DC-9 SRM 51-30-1 AND 51-30-5.Apr 3, 2002 · N965AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA010822Skin · crackedCRACK IN FUSELAGE EXTERIOR SKIN AT STATION 1222, LONGERON 15 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-01.Apr 1, 2002 · N965AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA010821Skin · crackedSKIN CRACKED AT RIGHT AFT NOSE GEAR DOOR AFT CUT-OUT. REPAIRED AREA IAW DC-9 SRM 53-05.Apr 1, 2002 · N965AX · Doug DC941 · Fuselage Main, StructureSDR ABXA010820Panel · delaminatedPANEL 1502 HAD 2 EACH AREAS OF DELAMINATION AND 1 SPOT OF LEVEL 1 CORROSION ON EXTERIOR SURFACE. REPLACED THE BUTE DOOR IAW DC-9 SRM 51-30-5.Apr 1, 2002 · N965AX · Doug DC941 · Wing, Plate/SkinSDR ABXA010780Odor · detectedNOTICED A BURNING SMELL IN THE COCKPIT, INTERMITTENT, NOT STRONG BUT NOTICEABLE. THE SOURCE WAS NEAR THE RIGHT CLEAR VIEW WINDOW HEAT SENSOR. INSPECTED WIRING AND TEMP. SENSOR AT FIRST OFFICER'S CLEAR VIEW WINDOW. CHECKED FORWARD ACCESSORY COMPARTMENT AND Mar 15, 2002 · N973AX · Doug DC941 · Air Distribution SystemSDR ABXA010764Switch · defectiveWHEN THE LEFT LANDING LIGHT SWITCH WAS SELECTED TO EXTEND, COCKPIT FILLED WITH SMOKE. REPLACED THE LEFT LANDING LIGHT SWITCH. OPS CHECKED GOOD IAW DC-9 MM.Mar 15, 2002 · N977AX · Doug DC941 · Exterior LightingSDR ABXA010763Wire · shortedWHILE ADJUSTING FIRST OFFICER'S OVERHEAD MAP LIGHT, SPARKING AND SMOKE CAME FROM BEHIND IT. MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPED. FOUND WIRE L453A24 BEHIND THE FIRST OFFICER'S MAP LIGHT CHAFED THROUGH AND SHORTING TO GROUND. REPLACED A FIVE INCH SECTIOMar 13, 2002 · N977AX · Doug DC941 · Light System WiringSDR ABXA010762Odor · detectedTHROUGH 10,000 FT, 10 - 15 SECONDS AFTER EXTENDING WING LANDING LIGHTS THERE WAS A VERY NOTICEABLE ELECTRICAL BURNING ODOR THAT LASTED 30 SECONDS TO 1 MIN, THEN DISSIPATED AND DID NOT RECUR. ALL ELECTRICAL INDICATIONS WERE NORMAL. EXTENDED THE LIGHT AGAIN INMar 12, 2002 · N977AX · Doug DC941 · Air Distribution SystemSDR ABXA010760Sensor · faultyAFTER TAKEOFF, AIRCRAFT DID NOT HOLD PRESSURE AND FORWARD CARGO DOOR LIGHT CAME ON AND OFF IN FLIGHT. REPLACED THE CABIN/FLIGHT RATE OF CHANGE/HIGH LIMIT TEMPERATURE SENSOR IAW DC-9 MM 21-61-03-2.Mar 11, 2002 · N975AX · Doug DC941 · Cabin Temperature SensorSDR ABXA010769Frame · corrodedAFT LOWER CARGO FRAME AT F.S. 973, LONGERON 30, 29 LEFT AND 28 LEFT, HEAVILY CORRODED AND DOUBLE DRILLED HOLE. REPAIRED FUSELAGE FRAME IAW REA D953-43402-MR.Mar 7, 2002 · N978AX · Doug DC941 · Fuselage Structure (General)SDR ABXA010768Fitting · corrodedFLOORBEAM STATION 965, RIGHT END FITTING EXFOLIATED. REPLACED END FITTING IAW DC-9 SRM 1-30-5.Mar 4, 2002 · N978AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA010757Battery · dischargedCOCKPIT OVERHEAD EMERGENCY LIGHTS WOULD NOT TEST. REPLACED NICAD BATTERIES IN EMERGENCY LIGHTING BATTERY PACK IAW DC-9 MM 33-53-00-8. OPS CHECKED GOOD.Mar 4, 2002 · N954AX · Doug DC941 · Emergency LightingSDR ABXA010770Frame · crackedLONGERON 17 LEFT WAS CRACKED BEHIND FUSELAGE FRAMES AT STATION 256, 275, 408 AND 427. REPAIRED AREA IAW DC-9 SSRM K05864.Feb 28, 2002 · N978AX · Doug DC941 · Fuselage Structure (General)SDR ABXA010767Skin · crackedINBOARD WING UPPER TRAILING EDGE UPPER SKIN WAS CRACKED ALONG THE TRAILING EDGE NEXT TO INBOARD SPOILER. REPAIRED TRAILING EDGE IAW DC-9 SRM 57-01.Feb 25, 2002 · N978AX · Doug DC941 · Wing, Plate/SkinSDR ABXA010766Skin · crackedFOUND 2 CRACKS IN FUSELAGE SKIN AT UPPER AFT DOOR STOP HOLE FOR MAIN ENTRY DOOR. EACH CRACK IS APPROXIMATELY .350 INCHES LONG. REPAIRED CRACKED AREA OF FUSELAGE SKIN IAW E.A. 53100126-001.Feb 25, 2002 · N978AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA010765Panel · crackedFITTING OUTBOARD OF CANTED KEEL PANEL AT STATION 603, RIGHT SIDE CRACKED. REPLACED FITTING IAW DC-9 MM.Feb 19, 2002 · N978AX · Doug DC941 · Fuselage Structure (General)SDR 0200669608Doubler · crackedDuring HCK in DHN, the ground power access door doubler was noted as being cracked at sta 94.5 LBL 41 forward lower corner. The skin was not damaged. the Damaged area was trimmed out from the OEM doubler. Repaired per EA. 96-188359.Feb 15, 2002 · N608NW · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA010720Clip · defectiveSMOKE FROM FIRST OFFICER'S YOKE CLIPBOARD LIGHT. TRIPPED MAP AND BRIEFCASE LIGHT CIRCUIT BREAKER. REMOVED METAL CLIP FROM FIRST OFFICER'S CLIPBOARD IAW DC-9 MM 33-10-00.Feb 13, 2002 · N967AX · Doug DC941 · Flight Compartment LightingSDR ABXA010719Rheostat · malfunctionedBURNING SMELL FROM FIRST OFFICER'S YOKE FOLLOWED BY MAP AND BRIEFCASE CIRCUIT BREAKER TRIPPING. REPLACED FIRST OFFICER'S BRIEFCASE RHEOSTAT IAW DC-9 AMM 33-10-00-2.Feb 12, 2002 · N967AX · Doug DC941 · Flight Compartment LightingSDR ABXA010706Light · inoperativeEMERGENCY LAMP BY THE OVERHEAD FORWARD ATTENDANCE PANEL (THE AFT LAMP INOPERATIVE). REPOSITIONED CONTACT LEVEL POINT (DOOR CONTACT) AND RELAMPED IAW DC-9 AMM 33-55-00-4.Feb 10, 2002 · N975AX · Doug DC941 · Emergency LightingSDR ABXA010718Bulkhead · crackedRIGHT WING LEADING EDGE BULKHEAD CRACKED AT LOWER FASTENER ON INBOARD SIDE OF NR 2 SLAT TRACK. REPAIRED AREA IAW DC-9 REA D957-43261.Feb 6, 2002 · N979AX · Doug DC941 · Wing, Rib/BulkheadSDR ABXA010703Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED THE EMERGENCY EVACUATION LIGHTS BATTERY PACK IAW DC-9 MM 33-53-02.Feb 6, 2002 · N952AX · Doug DC941 · Emergency LightingSDR 0200189762Duct · malfunctionedSLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION DURING APPROACH INTO MSP ACCOMPANIED WITH A ROLL TO THE LEFT. COMPLIED WITH COM PROCEDURES AND AIRCRAFT LANDED SAFELY WITH SLATS RETRACTED. MAINTENANCE INITIALLY LUBRICATED THE 'T' DUCTS BUT HAVE SINCE Feb 3, 2002 · N762NW · Doug DC941 · Airfoil Anti/De-ice SystemSDR ABXA010717Longeron · crackedLONGERON 30 CRACKED AT LEFT FLANGE STATION 232 UNDER SPLICE. REPAIRED AREA IAW DC-9 REA D953-43229.Jan 30, 2002 · N979AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA010716Web · crackedCUSP WEB CRACKED AT STATION 239 RBL 56. REPAIRED AREA IAW DC-9 SRM 53-01.Jan 30, 2002 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA010715Stiffener · crackedUPPER HORIZONTAL STIFFENER CRACKED ON OUTBOARD END FORWARD FACE OF AFT PRESSURE BULKHEAD RIGHT SIDE. REPAIRED STIFFENER IAW DC-9 SSRM K05159.Jan 30, 2002 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR 0200239762Coupling · misalignedSLAT DISAGREEMENT LIGHT ILLUMINATED WITH A SLIGHT ROLLING TENDENCY TO THE LEFT ON APPROACH. REINSTALLED THE LEFT WING SLAT ANTI-ICE COUPLING BETWEEN NBR 1 AND NBR 2 SLATS. REPLACED THE LEFT NBR 1 SLAT INBOARD CUTOUT DOOR HINGES, TIGHTENED THE RIGHT 'T' DUCT OUJan 30, 2002 · N762NW · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA010714Door · crackedLEFT ENTRY DOOR LOWER AFT CORNER SKIN WAS CRACKED. REPAIRED ENTRY DOOR SKIN IAW DC-9 SRM 52-05.Jan 29, 2002 · N979AX · Doug DC941 · Passenger/Crew DoorsSDR ABXA010713Frame · crackedFUSELAGE FRAME STATION 1152 WAS CRACKED AT LONGERON 15 RIGHT. REPAIRED CRACKED SECTION OF FRAME AT STATION 1152 LONGERON 15 RIGHT IAW DC-9 SRM 53-03.Jan 29, 2002 · N979AX · Doug DC941 · Fuselage Structure (General)SDR ABXA010712Skin · crackedFORWARD LOWER CORNER CUTOUT HAD APPROXIMATELY .1250 INCH CRACK. REPAIRED DAMAGED AREA IAW DC-9 SRM 51-10-2.Jan 28, 2002 · N979AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA010711Doubler · crackedREPAIR CRACKED ON FORWARD UPPER CORNER OF INBOARD GEAR DOOR. REPAIRED AREA IAW DC-9 SRM 52-05. REINSTALLED INBOARD MAIN LANDING GEAR DOOR IAW DC-9 MM 32-12-01.Jan 28, 2002 · N979AX · Doug DC941 · Landing Gear DoorsSDR ABXA010710Skin · crackedSKIN CRACKED AT LEFT REAR CUTOUT FOR LEFT AFT NOSE GEAR DOOR. REPAIRED IAW DC-9 SRM 53-01. INSTALLED ROD IAW DC-9 MM 20-16-0.Jan 28, 2002 · N979AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA010709Fitting · crackedCRACK IN THE FORWARD SERVICE DOOR HOLD OPEN CUP. REPLACED THE FORWARD SERVICE DOOR HOLD OPEN CUP IAW DC-9 SRM 51-30-5.Jan 28, 2002 · N979AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA010708Rod End · corrodedRIGHT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ROD (FROM CRANK TO DOOR) CORRODED AT DOOR END. RIVET WAS CORRODED, RUST BLEEDING FROM ROD END, PLAY WHERE ROD END ATTACHES TO ROD. REPLACED DOOR ROD PANEL IAW DC-9 AMM.Jan 28, 2002 · N979AX · Doug DC941 · Landing Gear Door Retract SectionSDR 0200229754ExciterDURING RIGHT ENGINE START, THE EGT WOULD NOT RISE. TAKEOFF WAS ABORTED. AFTER ENGINE RESTART, THE TOWER REPORTED SMOKE AND FIRE IN THE RIGHT ENGINE TAILPIPE. CREW SHUT DOWN THE RIGHT ENGINE, DISCHARGED TWO FIRE BOTTLES, AND AN EMERGENCY PASSENGER EVACUATION OFJan 24, 2002 · N754NW · Doug DC941 · Powerplant SystemSDR ABXA010681Wire · brokenWHEN EXTENDING GEAR, LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT COME ON. THREE MISSED APPROACHES INTO RIC. THE CREW USED THE ALTERNATE GEAR EXTENSION AND HAD TO HOLD ON THE RUNWAY FOR MAINTENANCE UPON LANDING. FOUND BROKEN WIRE 1G13B24N AT CONNECTOR P1-431.Jan 24, 2002 · N973AX · Doug DC941 · Landing Gear System WiringSDR 0200209762Guide · wornON SLAT EXTENSION, THE SLAT DISAGREEMENT LIGHT ILLUMINATED ACCOMPANIED WITH A ROLL TO THE RT. CREW RECYCLED THE SLATS AND DISCREPANCY REPEATED INCLUDING ROLL TO THE RT. IN PROCESS OF APPLYING COM PROCEDURES, LIGHT WENT OUT AND LANDING WAS NORMAL. MAINTENANCE FJan 22, 2002 · N762NW · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA010678Battery · dischargedEMERGENCY LIGHTS BATTERIES LOW. REPLACED THE EMERGENCY LIGHTS BATTERIES IAW DC-9 AMM 33-53-00-8. OPS CHECKED GOOD.Jan 21, 2002 · N959AX · Doug DC941 · Emergency LightingSDR 0200059752Seal · damagedAIRCRAFT ROLLS SHARPLY TO THE LEFT WHEN SLAT EXTENDED. A LOUD BANG WAS HEARD AFTER 5 DEGREES OF FLAP SELECTED AND ROLLING MOVEMENT STOPPED. THERE WERE NO ABNORMAL ANNUNCIATOR INDICATIONS. THE FLIGHT LANDED SAFELY AT DTW. MAINTENANCE STATED THAT SLAT EXTENSJan 5, 2002 · N752NW · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA010674Panel · corrodedRIGHT SLANT PANEL HAD CORROSION AROUND NUT PLATES, LOWER EDGE FROM INBOARD TO OUTBOARD. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-2, 51-10-4, 51-30-1 AND 51-20-6.Jan 4, 2002 · N951AX · Doug DC941 · Fuselage Main, StructureSDR ABXA010673Panel · corrodedLEFT SLANT PANEL CORRODED AROUND NUTPLATES. REPLACED SLANT PANEL IAW DC-9 SRM 51-30-1.Jan 3, 2002 · N951AX · Doug DC941 · Fuselage Structure (General)SDR ABXA010672Attach Angle · corrodedLEFT WHEEL WELL OUTBOARD SLANT PANEL ATTACH ANGLE EXFOLIATED AT LOWER FASTENER. LOCATED AND DRILLED SLANT PANEL ATTACH ANGLE IAW DC-9 SRM 51-30-5.Jan 3, 2002 · N951AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA010671Angle · crackedLEFT WHEEL WELL ATTACH ANGLE CRACKED IN RADIUS, JUST OUTBOARD OF THE TRAP PANEL, ABOVE THE HYDRAULIC SERVICE ACCESS. REPLACED ANGLE IAW DC-9 SRM.Jan 3, 2002 · N951AX · Doug DC941 · Fuselage Main, StructureSDR ABXA010657Battery · dischargedEMERGENCY LIGHTS FAILED TEST. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-02-4-001. OPS CHECKED GOOD IAW DC-9 MM 33-53-00.Dec 30, 2001 · N952AX · Doug DC941 · Emergency Lighting
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