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 ABXA030463Intercostal · crackedFORWARD LOWER CARGO DOOR INTERCOSTAL WEB CRACKED AT LOWER AFT SIDE BY DOOR STOP MARKED AS NR 6. REMOVED AND REPLACED INTERCOSTAL IAW DC-9 MM AND ON ABX NON ROUTINE CARD 0228.Nov 24, 2003 · N965AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA030464Angle · crackedEXTERIOR SURFACE OF VERTICAL STABILIZER AT FORWARD RIGHT FUSELAGE ATTACH POINT HAD CRACK. REMOVED AND REPLACED VERTICAL ATTACH ANGLE IAW DC-9 SRM.Nov 24, 2003 · N965AX · Doug DC941 · Vertical Stabilizer, Attach FittingsSDR ABXA030445Window · stiffCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. MAINTENANCE OPS CHECKED WINDOW ON GROUND. OPS CHECKED GOOD IAW DC9 MM 56-10-03.Nov 18, 2003 · N952AX · Doug DC941 · Flight Compartment WindowsSDR ABXA030434Angle · crackedVERTICAL ANGLE CRACKED AND HAD SHEARED RIVETS FS 696 RIGHT BUTTLINE 44. REMOVED AND REPLACED ANGLE IAW DC-9 SRM.Oct 28, 2003 · N978AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA030433Attach Angle · crackedVERTICAL STABILIZER RIGHT ATTACH ANGLE WAS CRACKED AT 99. REPAIRED CRACK ON VERTICAL STABILIZER RIGHT ATTACH ANGLE AND SEAM SEALED IAW DC-9 SRM.Oct 27, 2003 · N978AX · Doug DC941 · Vertical Stabilizer, Attach FittingsSDR ABXA030429Pan · crackedFORWARD LOWER CARGO DOOR OUTER PAN HAD CRACK INDICATION AROUND HI-LOK AT AFT LOWER STOP. REPLACED FORWARD LOWER CARGO DOOR ON JC 0314 IAW DC-9 MM.Oct 27, 2003 · N978AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA030427Pan · crackedFORWARD LOWER CARGO DOOR PAN WAS CRACKED AT AFT LOWER STOP. FORWARD LOWER CARGO DOOR WAS REPLACED ON JC 0314 IAW DC-9 MM.Oct 27, 2003 · N978AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA030426Pan · corrodedLEVEL 2 CORROSION ALONG BOTTOM OF FORWARD LOWER CARGO DOOR CUTOUT. REMOVED CORRODED AND CRACKED PAN SECTION. INSTALLED NEW PAN SECTION IAW DC-9 SRM 53-05.Oct 27, 2003 · N978AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA030428Pan · crackedFORWARD LOWER CARGO DOOR OUTER PAN HAD CRACK INDICATION AT FORWARD HINGE AREA. REPLACED FORWARD LOWER CARGO DOOR ON JC 0314 IAW DC-9 MM.Oct 27, 2003 · N978AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA030432Attach Angle · crackedVERTICAL STABILIZER LEFT ATTACH ANGLE WAS CRACKED AT 99. REPLACED LEFT VERTICAL STABILIZER ATTACH ANGLE IAW DC-9 SRM 53-05.Oct 27, 2003 · N978AX · Doug DC941 · Fuselage, Stabilizer Attach FittingsSDR ABXA030431Pan · crackedFORWARD LOWER CARGO DOOR WAS CRACKED IN OUTER PAN AROUND HI-LOK AT FORWARD LOWER STOP. REPLACED FORWARD LOWER CARGO DOOR ON JC 0314 IAW DC-9 MM.Oct 27, 2003 · N978AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA030430Pan · crackedFORWARD LOWER CARGO DOOR OUTER PAN HAD CRACK INDICATION IN RADIUS AT AFT LOWER STOP. REPLACED FORWARD LOWER CARGO DOOR ON JC 0314 IAW DC-9 MM.Oct 27, 2003 · N978AX · Doug DC941 · Cargo/Baggage DoorsSDR 0301969762Duct · damagedUPON SLAT EXTENSION DURING APPROACH, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED TO THE RIGHT. AS THE AIRCRAFT SLOWED TO BELOW 190 KTS, THE CREW HEARD A SLIGHT BANG AND THE DISAGREEMENT LIGHT EXTINGUISHED. NO MENTION OF COM PROCEDURES AND FOct 22, 2003 · N762NW · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA030407Longeron · crackedLONGERON 30 CRACKED LEFT AND RIGHT FLANGES SM 243 - 245. REPLACED LONGERON 30, STA 230 - 265 IAW REA D953-48386MR.Oct 13, 2003 · N979AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA030406Rib · crackedRIGHT WING LEADING EDGE NOSE RIB INBOARD SIDE OF NR 1 SLAT DRIVER HAD 2 CRACKS ON REPAIR MARKED, REA 43261, CRACKED IN FORWARD RADIUS AND AFT BETWEEN HI-LOKS. REPLACED LEADING EDGE RIB IAW DC-9 SRM 51-30-5 AND 51-30-2.Oct 13, 2003 · N979AX · Doug DC941 · Leading Edge DevicesSDR 0301919754Hose · separatedON DEPARTURE CLIMBOUT AT 13,000 FT, CREW HEARD A MUFFLED BOOM AND CABIN STARTED TO CLIMB AT 2000 FPM. FLIGHT CREW WAS UNABLE TO CONTROL CABIN PRESSURIZATION IN AUTO OR MANUAL. MASKS DID NOT DEPLOY AND COM PROCEDURES WERE COMPLIED WITH. FLIGHT DIVERTED TO DTOct 10, 2003 · N754NW · Doug DC941 · Humidity Control SystemSDR ABXA030364Odor · detectedINTERMITTENT BURNING ODOR UNDER FIRST OFFICER'S GLARESHIELD. ANTI-FOG C/B'S WERE PULLED FOR ENTIRE FLIGHT. INSPECTED WIRING UNDER GLARESHIELD, BEHIND FIRST OFFICER'S INSTRUMENT PANEL AND FORWARD ACCESSORY COMPARTMENT. ALL SYSTEMS WERE ON, ALL LIGHTS WERE FULLSep 19, 2003 · N972AX · Doug DC941 · Air Distribution SystemSDR ABXA030363Wire · brokenINTERMITTENT ODOR OF BURNING INSULATION UNDER THE GLARESHIELD ON FIRST OFFICER'S SIDE. FOUND BROKEN WIRE ON FIRST OFFICERS CLEARVIEW WINDOW ANTI-FOG WIRING. SUSPECT WIRE MAY HAVE BEEN ARCING CAUSING THE SMELL. REPAIRED BROKEN WIRE. FIRST OFFICER'S CLEARVIESep 18, 2003 · N972AX · Doug DC941 · Electrical Power System WiringSDR ABXA030372Channel · crackedLEFT MAIN LANDING GEAR INBOARD DOOR CRACKED AT FORWARD HINGE. REPLACED PAN SECTION AND REPAIRED AREA, REINSTALLED DOOR IAW DC-9 MM 32-12-01-2 AND SRM 52-05, 53-05, AND 51-30-1.Sep 12, 2003 · N951AX · Doug DC941 · Landing Gear DoorsSDR ABXA030373Beam · crackedAFT LOWER CARGO DOOR BEAM NR 2 END FITTING CRACKED ON AFT SIDE. REPLACED AFT LOWER CARGO DOOR BEAM NR 2 END FITTING IAW DC-9 SRM 51-30-5.Sep 9, 2003 · N951AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA030374Shear Tie · crackedSHEAR TIE CRACKED, FS 1021 AT LONGERON 14 RIGHT. REPLACED SECTION OF SHEAR TIE IAW DC-9 SRM.Sep 9, 2003 · N951AX · Doug DC941 · Fuselage Main, StructureSDR ABXA030361Odor · detectedA FAINT BURNING ODOR DETECTED ON DESCENT. INSPECTED ELECTRONIC COMPARTMENT, ENGINE CONTROL UNITS FOR LOOSE CONNECTOR AND ACCESSORIES FOR SECURITY. NO DEFECTS NOTED.Sep 6, 2003 · N954AX · Doug DC941 · Air Distribution SystemSDR ABXA030329Control Box · faultyUPON GEAR EXTENSION FOR LANDING, THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. COMPLIED WITH ABNORMAL PROCEDURES AND LANDED WITH THE LIGHT ILLUMINATED. REPLACED THE MAIN LANDING GEAR PROXIMITY SWITCH CONTROL BOX IAW DC9 MM. 32-60-03-2-0201.Aug 18, 2003 · N958AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA030326Radome · out of toleranceRADAR PAINTS STREAK OF GROUND RETURNS AT 60 DEGREES RIGHT OF NOSE ON COUNTER CLOCKWISE SWEEP. SOUNDS LIKE RADAR HITS DOME ON CLOCKWISE SWEEP. FOUND RADAR DRIVE PLATE BINDING AGAINST RADOME STATIC DISCHARGE STRIP PLASTIC NUT PLATES. REPLACED THE RADOME ASSEMBLYAug 12, 2003 · N964AX · Doug DC941 · Weather Radar SystemSDR ABXA030340Fitting · crackedFS 1152 LEFT SIDE OF AFT VENTRAL STAIR CUTOUT FRAME FITTING CRACKED. INSTALLED NEW FITTING IAW DC-9 SRM 51-30-5.Aug 11, 2003 · N975AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA030335Attach Fitting · crackedRIGHT ELEVATOR GEARED TAB ATTACH FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2.Aug 6, 2003 · N975AX · Doug DC941 · Elevator, Tab StructureSDR ABXA030338Shear Tie · crackedCRACKED SHEAR TIE FS 1021 JUST BELOW LONGERON 14 RIGHT. REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5.Aug 4, 2003 · N975AX · Doug DC941 · Fuselage Main, StructureSDR ABXA030339Web · crackedRIGHT CUSP WEB CRACKED JUST FORWARD OF FS 1041 BULKHEAD. REPAIRED RIGHT CUSP WEB JUST FORWARD OF FS 1041 IAW DC-9 SRM 53-01.Aug 4, 2003 · N975AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA030336Web · crackedMAIN ENTRY DOOR INTERIOR WEB JUST FORWARD OF DOOR HANDLE WAS CRACKED. REPLACED WEB IAW DC-9 SRM 51-30-2.Aug 1, 2003 · N975AX · Doug DC941 · Passenger/Crew DoorsSDR ABXA030333Skin · corrodedBULGE IN SKIN, CUPPED FASTENERS FLAP UNDER SURFACE NR 2 EXPANSION JOINT. REPLACED UPPER AND LOWER FLAP SEGMENT SKIN.Aug 1, 2003 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA030332Skin · corrodedBULGE IN SKIN, CUPPED FASTENERS, FLAP LOWER SURFACE AT NR 3 EXPANSION JOINT. REPLACED LOWER SKIN IAW DC-9 SRM 51-30-2.Aug 1, 2003 · N975AX · Doug DC941 · Trailing Edge FlapsSDR ABXA030337Seat Track · corrodedCORROSION ON SEAT TRACK AT STA 275, 294, 320, 351, 380 AND 408. REPLACED CENTER SEAT TRACK STA 160 - 588 IAW DC-9 SRM 51-30-1 AND SSRM K05406.Aug 1, 2003 · N975AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA030334Attach Fitting · corrodedLT ELEVATOR WAS CORRODED ON UPPER SURFACE AT OUTBOARD BALANCE HORN ATTACH FITTING. REPLACED LT ELEVATOR ATTACH FITTING CLIP.Aug 1, 2003 · N975AX · Doug DC941 · Elevator StructureSDR ABXA030319Pivot Assy · lack of lubeRIGHT MAIN LANDING GEAR CAME OUT ON UPLATCH CHECK. RECYCLED LANDING GEAR AND RECEIVED NORMAL INDICATION. FOUND UPLOCK PIVOT BOLT BOUND UP TO HOOK AND STRUCTURE IMPEDING MOVEMENT OF HOOK. PULLED, CLEANED AND LUBRICATED PIVOT BOLT AND BOSS. INSTALLED REMOTE Aug 1, 2003 · N951AX · Doug DC941 · Landing Gear Retraction/Extension SystemSDR ABXA030317Skin · crackedCRACKS IN SKIN JUST AFT OF CANTED FRAME 1197 BELOW LG 13 L. REPAIRED AREA IAW DC-9 SRM 53-01.Jul 21, 2003 · N969AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA030307Switch · faultyDURING CRUISE FLIGHT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. RIGHT HYDRAULIC SWITCH ON, 3000 PSI DID NOT RESOLVE THE PROBLEM. WHEN GEAR SELECTED DOWN, UNSAFE LIGHT REMAINED ILLUMINATED. GEAR DOWN LIGHT REMAINED OFF. DECLARED EMERGENCY. REPLACED THE NOSE GEARJul 21, 2003 · N956AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA030287Uplock Switch · failedRT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. LIGHT WENT OUT AFTER GEAR WAS RECYCLED. ALL INDICATIONS WERE NORMAL. REPLACED RIGHT GEAR UPLOCK SWITCH IAW MM 32-60-01-2. ALSO FOUND CANNON PLUG P1-1150 VERY CORRODED, REPLACED PLUG. OPS CHECKEJul 18, 2003 · N951AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA030284Pin · bentAFTER TAKEOFF, RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER INITIAL RETRACTION. THERE WAS NO ASSOCIATED YAW OR NOISE. AFTER RECYCLING GEAR, ALL INDICATIONS WERE NROMAL. FOUND PIN A BENT ON R5-1150. STRAIGHTENED PIN. OPS CHECKED GOOD IAW DC-9 AMM 32-60-0Jul 15, 2003 · N951AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA030286Window · unsecureEN ROUTE, CREW REPORTED LOUD AIR NOISE IN COCKPIT. NOISE WAS SO LOUD CREW COULD NOT HEAR. DESCENDED TO 10K AND CONTINUED UNPRESSURIZED. RESECURED AND RESEALED CAPTAIN'S EYEBROW WINDOW IAW DC-9 AMM. PRESSURIZED TO 4 PSID AND NO LEAKS NOTED.Jul 7, 2003 · N969AX · Doug DC941 · Flight Compartment WindowsSDR ABXA030291Support Fitting · crackedLEFT INBOARD SPOILER TORSION BAR SUPPORT FITTING CRACKED AT UPPER END. REPLACED FITTING IAW DC-9 SRM 51-30-1, 51-30-2, AND 51-30-5.Jul 4, 2003 · N971AX · Doug DC941 · Wing, Attach FittingsSDR ABXA030290Support Bracket · crackedLEFT INBOARD SPOILER TORSION BAR SUPPORT BRACKET CRACKED AT UPPER END. REPLACED SUPPORT IAW SRM 51-30-1 AND 51-30-5.Jul 4, 2003 · N971AX · Doug DC941 · SpoilersSDR ABXA030289Support Bracket · crackedLEFT OUTBOARD SPOILER TORSION BAR OUTBOARD SUPPORT BRACKET CRACKED AT UPPER END. REPLACED SUPPORT BRACKET FOR LEFT OUTBOARD SPOILER TORSION BAR IAW DC-9 SRM.Jul 2, 2003 · N971AX · Doug DC941 · SpoilersSDR ABXA030306Attach Angle · crackedRIGHT PYLON LEADING EDGE INBOARD ATTACH MOUNT HAD CRACKED REPAIR ANGLES. REMOVED, FABRICATED NEW ANGLE AND INSTALLED IAW DC-9 SSRM DWG K05159.Jun 19, 2003 · N966AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA030305Pan · crackedRIGHT FORWARD EMERGENCY OVERWING EXIT DOOR HAD CRACKED PAN AT AFT SIDE LOWER JAMB SUPPORT FITTING. REPAIRED AREA IAW DC-9 SRM 52-51.Jun 18, 2003 · N966AX · Doug DC941 · Emergency ExitsSDR ABXA030304Pan · crackedRIGHT AFT EMERGENCY OVERWING EXIT DOOR PAN CRACKED AT AFT UPPER JAMB SUPPORT FITTING. REPAIRED AREA IAW DC-9 SRM 52-51 AND SSRM K07390.Jun 18, 2003 · N966AX · Doug DC941 · Emergency ExitsSDR ABXA030303Pan · damagedRIGHT AFT EMERGENCY OVERWING DOOR HAD FIBERGLASS REPAIR ON DOOR PAN UPPER FORWARD CORNER OF DOOR. REPAIRED AREA IAW DC-9 SRM 52-51 AND SSRM K07390.Jun 18, 2003 · N966AX · Doug DC941 · Emergency ExitsSDR ABXA030302Skin · crackedCRACK IN SKIN .25 INCH IN LENGTH FROM RIVET HOLE BETWEEN LONGERON 12 LEFT AND LONGERON 13 LEFT AT STA 1114. REPAIRED DAMAGED AREA IAW DC-9 SRM 53-01.Jun 17, 2003 · N966AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA030234Blade · damagedTURBINE DAMAGE (T-1) ON NR 1 ENGINE. BLADE TIP MISSING. REPLACED THE NR 1 ENGINE IAW DC-9 MM.Jun 13, 2003 · N969AX · Doug DC941 · Turbine SectionSDR ABXA030189Handle · bindingMAIN CABIN LEFT FORWARD ENTRY DOOR WOULD NOT OPEN. FOUND DOUBLER ON EXTERIOR DOOR BINDING EXTERIOR HANDLE, CHAMFERRED DOUBLE ON MAIN CABIN LEFT FORWARD ENTRY DOOR, NO BINDING NOTED. DOOR OPEN/CLOSED OKAY IAW DC-9 AMM 52-11-00.Jun 4, 2003 · N972AX · Doug DC941 · Passenger/Crew DoorsSDR ABXA030214Frame · corrodedFRAME FS 446 WAS CORRODED LONGERON 29 LEFT TO LONGERON 29 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.May 28, 2003 · N970AX · Doug DC941 · Fuselage Main, Frame
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