Douglas DC-9-31

Service difficulty reports · 7,433

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 = 'DC931'
  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 0400329969Annunciator · activatedTHE RED CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED AT FL240 DURING DESCENT. CABIN WAS APPROACHING 10,000 FT, OUTFLOW VALVE INDICATED CLOSED, AND NO ASSOCIATED NOISE IN COCKPIT OR CABIN. COMPLIED WITH COM PROCEDURES AND AIRCRAFT DESCENDED TO 10,000 FT MSL. Mar 2, 2004 · N9333 · Doug DC931 · Cabin Pressure Control SystemSDR ABXA040084Structure · crackedRIVET ROW FOUND CRACKED AT STA 76.550 UNDER CO-PILOT'S WINDSHIELD WIPER BETWEEN APPROXIMATELY LONGERON 3 AND 4 RIGHT. REPAIRED AREA IAW EA 53100075-003-2.Feb 18, 2004 · N908AX · Doug DC931 · Fuselage Main, StructureSDR ABXA040082Fitting · crackedSLANT PANEL INBOARD ANGLE FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-10-4, AND 51-30-1.Feb 17, 2004 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA040080Angle · crackedLEFT PYLON UPPER ATTACH ANGLE WAS CRACKED AT STA 1019. REPAIRED AREA IAW DC-9 SRM 54-04.Feb 17, 2004 · N908AX · Doug DC931 · Nacelle/Pylon Miscellaneous StructureSDR ABXA040083Actuator · crackedFITTING FORWARD OF DOOR ACTUATOR CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.Feb 17, 2004 · N908AX · Doug DC931 · Landing Gear Door ActuatorSDR ABXA040081Longeron · crackedLONGERON 17 RIGHT HAD 2 CRACKS AT EACH LOCATION, FS 389, FS 408 AND FS 427. REPAIRED LONGERON 17 RIGHT FROM STA 388 TO 446 IAW DC-9 SRM 53-02.Feb 17, 2004 · N908AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR 02340405WPBattery · out of toleranceEMERGENCY PORTABLE LIGHT AT FWD L1 DOOR INOPERATIVE. R&R RECHARGEABLE BATTERIES IAW 33-53-0. OPERATIONAL CHECK GOOD.Feb 16, 2004 · N934LK · Doug DC931 · Emergency LightingSDR 02240404WPLight · inoperativeL1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT IAW 33-53-0. OPERATIONAL CHECK GOOD.Feb 16, 2004 · N933JK · Doug DC931 · Emergency LightingSDR ABXA040062Door · obstructedPASSENGER ENTRY DOOR WOULD NOT OPEN FROM INSIDE, WORKED OKAY FROM OUTSIDE. FOUND DOUBLER PLATE INTERFERING WITH MOVEMENT OF OUTER DOOR HANDLE. FAIRED DOUBLER IAW DC-9 SRM 52-01. OPERATED DOOR SEVERAL TIMES. OPS CHECKED GOOD.Feb 10, 2004 · N946AX · Doug DC931 · Passenger/Crew DoorsSDR 0400199933Ballast · overheatedAT ABOUT 800 FOOT ALTITUDE DURING APPROACH INTO IND, THE FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN THE CABIN. OTHER PASSENGERS REPORTED SEEING WHAT LOOKED LIKE SMOKE AND SMELLING AN ELECTRICAL OZONE SCENT. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCIDENT, Feb 7, 2004 · N8986E · Doug DC931 · Passenger Compartment LightingSDR 02240403WPWarning Light · false indicationAFTER TAKEOFF, RT MLG UNSAFE LIGHT AND DOOR LIGHT ILLUMINATED. MAINTENANCE JACKED AIRCRAFT AND PERFORMED SEVERAL GEAR SWINGS AND 1 MANUAL EXTENSION. NO DEFECTS NOTED. AFTER RETURN TO SERVICE.Feb 5, 2004 · N932MJ · Doug DC931 · Landing Gear Position and WarningSDR 0400149915Relief Valve · failedAT ABOUT 100 MILES OUT FROM LANDING THE AIRCRAFT, PRODUCED SMOKE IN THE COCKPIT. ALSO NOTICED THE LOSS OF THE RT HYDRAULIC SYSTEM AS QUANTITY WENT TO ZERO ACCOMPANIED BY 'R HYD PRES LOW' LIGHT. FLIGHT CREW DECLARED AN EMERGENCY, REQUESTED CFR, AND LANDED UNEVEJan 28, 2004 · N965N · Doug DC931 · Hydraulic System, MainSDR ABXA040029Amplifier · failedCARGO SMOKE LIGHT ON IN FLT. COULD NOT DUPLICATE. INSPECTED WIRING, TAPPED ON DETECTORS & AMPLIFIER, LIGHT REMAINED OUT. FOR PRECAUTION, R & R BOTH SMOKE DETECTORS & SMOKE DETECTOR AMP. PERFORMED CHECK USING LIQUID SMOKE. SYSTEM OPS CHECKED GOOD IAW DC-9 Jan 15, 2004 · N908AX · Doug DC931 · Smoke DetectionSDR ABXA040030Charger · defectiveIN FLIGHT, BATTERY CHARGER WAS CHARGING BATTERY CONTINUALLY AT 20 AMPS, THE BATTERY WAS AT 38 TO 39 VOLTS. REMOVED AND REPLACED BOTH MAIN BATTERIES, BATTERY CHARGER, AND BATTERY SENSOR IAW DC-9 AMM 24-30-01-4-0001 AND 24-30-02-2-001. OPS CHECKED GOOD.Jan 15, 2004 · N942AX · Doug DC931 · Battery/Charger SystemSDR 0400449988Clip · crackedDURING H-CHECK, FOUND CRACK IN FRAME SHEAR CLIP AT BS 1038 L14R. REPAIRED PER EA 99-197375.Jan 9, 2004 · N8944E · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA040032Light · misinstalledBLUE ELECTRICAL ARCING BEHIND LT OVERHEAD MAP LIGHT. BREAKER TRIPPED (T-42). FOUND GROUND POST HAVING WRONG HARDWARE. INSTALLED CORRECT HARDWARE AND RESET CIRCUIT BREAKER. OPS CHECKED GOOD IAW MM.Jan 7, 2004 · N946AX · Doug DC931 · Flight Compartment LightingSDR ABXA040001Uplock · out of adjustAFTER TAKEOFF, LT GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. PERFORMED THE UPLATCH CHECK ABNORMAL AND GEAR UNSAFE ABNORMAL. THIS DID NOT SOLVE THE PROBLEM. FOUND UPLATCH OUT OF ADJUSTMENT. ADJUSTED UPLATCH IAW DC-9 MM 32-31-04-2-0103. OPS CHECKED GOOD. POSIJan 6, 2004 · N944AX · Doug DC931 · Landing Gear Position and WarningSDR 0400109906Channel · crackedDURING L-CHECK FOUND CRACK IN AFT PRESSURE BULKHEAD CHANNEL. REPAIRED IAW EA 99-197419.Jan 5, 2004 · N956N · Doug DC931 · Fuselage Main, BulkheadSDR 0400039905Compressor · stalledDURING TAKEOFF, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL. TAKEOFF ABORTED AT 110 KNOTS. FLIGHT CREW INDICATED SNOW AND SLUSH ON RUNWAY. MAINTENANCE INSPECTED THE INLET AND EXHAUST, PS3 FILTER, AND SADDLE DUCTS; NO TROUBLE FOUND. ENGINE GROUND RUN TO Jan 4, 2004 · N955N · Doug DC931 · Turbine Engine Compressor SectionSDR 0302219935Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON FLOORBEAM WEB AT BS 996 RBL 50. REPAIRED PER EA 99-197352.Dec 27, 2003 · N1332U · Doug DC931 · Fuselage Main, Floor BeamSDR 0400029935Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON FLOORBEAM WEB AT BS 996 RBL 50. REPAIRED PER EA 99-197352.Dec 27, 2003 · N1332U · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA030452Proximity Switch · out of adjustUPON FIRST GEAR EXTENSION, NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE AND RED GEAR UNSAFE LIGHT WAS LIT. CYCLED GEAR AND RECEIVED 3 GREEN. FOUND GAP AT NOSE GEAR DOWNLOCK PROX SWITCH EXCESSIVE. ADDED SHIMS AS NEEDED IAW DC-9 MM 32-60-01-2-0201. OPS CHECKED GNov 26, 2003 · N943AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA030457Intercostal · crackedINTERCOSTAL CRACKED AT STA 389 BUTTLINE XERO AT FLOORBEAM ATTACH POINT. REPAIRED IAW DC-9 SSRM DWG K05159.Nov 19, 2003 · N907AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA030456Fitting · crackedLONGERON 29 LEFT END FITTING CRACKED ON OUTBOARD SIDE FS 756. REPAIRED LONGERON 29 LEFT AT STA 756 IAW DC-9 SRM 53-02.Nov 14, 2003 · N907AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA030455Fitting · crackedLONGERON 29 RIGHT END FITTING CRACKED ON OUTBOARD SIDE FS 756. REPAIRED LONGERON 29 RIGHT AT STA 756 IAW DC-9 SRM 53-02.Nov 14, 2003 · N907AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA030454Frame · corrodedLEVEL II CORROSION OF FRAME FS 218, LONGERON 28 LT. REMOVED DAMAGED FRAME AND INSTALLED NEW SECTION OF FRAME STA 218, LONGERON 26 LT LONGERON 26 RT IAW DC-9 SRM 53-03.Nov 14, 2003 · N907AX · Doug DC931 · Fuselage Main, FrameSDR ABXA030453Fitting · crackedLT MLG WW OUTBOARD APPROXIMATELY FS 730 SUPPORT BRACKET CRACKED FOR UPPER INBOARD BONDED PANEL LINK. REPLACED FITTING IAW DC-9 SRM 51-30-1.Nov 14, 2003 · N907AX · Doug DC931 · Wing, Attach FittingsSDR 0302069994Odor · detectedAFTER TAKEOFF, THERE WAS A SMOKE ODOR IN THE AIRCRAFT AND THE SMOKE DETECTORS WERE SOUNDING. FLIGHT CREW DECLARED AN EMERGENCY, RETURNED TO DTW, AND LANDED WITHOUT FURTHER INCIDENT. FIRE RESCUE MET AND INSPECTED THE AIRCRAFT BUT FOUND NO EVIDENCE OF FIRE. MNov 14, 2003 · N8979E · Doug DC931 · Air Distribution SystemSDR ABXA030416Switch · defectiveFUMES IN COCKPIT, UNABLE TO DETERMINE EXACT SOURCE. INSPECTED BOTH LEFT AND RIGHT AMC'S AND LEFT AND RIGHT DUCTING. INSPECTED E&E COMPARTMENT FOR GENERAL CONDITION AND OBVIOUS DEFECTS. INSPECTED FORWARD ACCESSORY COMPARTMENT FOR GENERAL CONDITION AND OBVIOUNov 6, 2003 · N937AX · Doug DC931 · Windshield/Door Rain/Ice RemovalSDR ABXA030415Battery Pack · dischargedEMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHT POWER PACK IAW DC-9 MM 32-53-02.Nov 6, 2003 · N929AX · Doug DC931 · Emergency LightingSDR 0302109945Skin · corrodedDURING M-CHECK FOUND CRACK IN SKIN AT NR 6 FORWARD STOP OF DOOR 1L. REPAIRED PER EA 99-196420.Oct 30, 2003 · N8925E · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA030393Warning Switch · defectiveON FINAL APPROACH, GEAR WENT DOWN AND GEAR DOOR OPEN LIGHT WENT OUT. AT 400 AGL, GEAR DOOR OPEN LIGHT CAME BACK ON. DID MISSED APPROACH. CYCLED THE GEAR EARLY FOR SECOND APPROACH. ON FINAL FOR SECOND APPROACH, GEAR DOOR OPEN LIGHT CAME BACK ON. FOLLOWED ABNORMOct 13, 2003 · N946AX · Doug DC931 · Landing Gear Position and WarningSDR 0301949992Line · brokenDURING CRUISE FLIGHT, BOTH THE LEFT HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED TO ZERO INDICATION. CREW APPLIED COM PROCEDURES, VERIFIED COMPLETE LOSS OF SYSTEM, AND LANDED UNEVENTFULLY AT MSP. MAINTENANCE FOUND A BROKEN ELEVATOR PRESSURE LINE AND REPLACOct 11, 2003 · N896OE · Doug DC931 · Hydraulic System, MainSDR ABXA030404Fitting · crackedFITTING IN LEFT WHEEL WELL STA 699, LEFT BUTT LINE '10' CRACKED. REPLACED FITTING IAW DC-9 SRM.Oct 10, 2003 · N947AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA030403Skin · crackedFUSELAGE SKIN CRACKED AT MAIN ENTRY DOOR UPPER/AFT STOP. REPAIRED AREA IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.Oct 9, 2003 · N947AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA030402Web · crackedCUSP WEB CRACKED AT RIGHT BUTT LINE 54 BETWEEN FS 945 - 965. REPAIRED CRACK IAW DC-9 53-01.Oct 9, 2003 · N947AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA030400Door · crackedAFT PRESSURE BULKHEAD DOOR CRACKED AT LOWER HINGE. REPLACED AREA NOTED IAW DC-9 SRM 52-05, 51-30-5 AND 51-30-1.Oct 8, 2003 · N947AX · Doug DC931 · DoorsSDR ABXA030399Skin · crackedFUSELAGE SKIN HAD 1.5 INCH TEAR/CRACK IN SKIN FORWARD ENTRANCE DOOR CUTOUT FORWARD SIDE BETWEEN STOP F4 AND F5. REPAIRED AREA IAW REA D953-48357MR.Oct 8, 2003 · N947AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA030401Channel · crackedAFT PRESSURE BULKHEAD DOOR CRACKED AT UPPER HINGE. REPAIRED DOOR IAW DC-9 SRM 52-05.Oct 8, 2003 · N947AX · Doug DC931 · Passenger/Crew DoorsSDR ABXA030398Intercostal · crackedLEFT AFT OVERWING DOOR HAD CRACKED INTERCOSTAL AT LATCH HANDLE. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 7, 2003 · N947AX · Doug DC931 · Emergency ExitsSDR ABXA030397Pan · crackedLEFT AFT OVERWING DOOR HAD CRACKED DOOR PAN AT STOP NR 6. REPAIRED AREA IAW DC-9 SRM 52-05.Oct 7, 2003 · N947AX · Doug DC931 · Emergency ExitsSDR 0302029959Skin Panel · corrodedDURING SPECIAL VISIT FOR INSPECTION OF BELLY SKINS CORROSION WAS FOUND ON SKIN PANEL BETWEEN BS 110-134 L27L TO L29R. REPAIRED PER EA 99-196522.Oct 6, 2003 · N919RW · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA030396Spar Cap · crackedCRACK ON UPPER SPAR CAP REAR SPAR XCW '0' TO XCW '10' RIGHT. REPAIRED AREA IAW DC-9 SRM.Oct 6, 2003 · N947AX · Doug DC931 · Wing SparSDR ABXA030371Uplock · out of adjustCYCLED MAIN LANDING GEAR AT 210 KNOTS, 3000 FT, CLEAN UPON RETRACT. RIGHT MAIN LANDING GEAR UNSAFE LIGHT STAYED ON. ADJUSTED RIGHT MAIN LANDING GEAR DOOR UPLATCH IAW DC-9 MM AND WORK ACCOMPLISHED ON W.O. NR 2003908. OPS CHECKED GOOD.Sep 30, 2003 · N908AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA030395Attach Fitting · crackedINBOARD RIB OF NR 5 SLAT DRIVE LINK HAD AN AFT ATTACH FITTING ATTACHED VERTICALLY TO SPAR AND RIB CRACKED IN 3 PLACES. REPAIRED ATTACH FITTING IAW DC-9 SRM 57-09.Sep 27, 2003 · N906AX · Doug DC931 · Wing Miscellaneous StructureSDR 0301809927Slide · malfunctionedPER MAINTENANCE CONTROL ORDER 4721, AN OPERATIONAL CHECK OF THE TAIL CONE DEPLOYMENT WAS PERFORMED. FOUND SLIDE PACK DEPLOY STRAP DID NOT SNAP ON THE SLIDE ASSEMBLY AS DESIGNED. SLIDE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Sep 18, 2003 · N8920E · Doug DC931 · Escape SlideSDR ABXA030376Cap · crackedCRACK IN LONGERON 16 LEFT END CAP AT FS 994. REPLACED END CAP IAW DC-9 SRM 51-30-5.Sep 17, 2003 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA030377Stop Fitting · crackedMAIN ENTRY DOOR AFT UPPER DOOR STOP A3, HAD CRACK FROM STOP HOLE TOWARDS DOOR OPENING APPROXIMATELY .1875 INCH LONG. REPAIRED AREA IAW DC-9 SRM AND EA 53100131-001.Sep 17, 2003 · N946AX · Doug DC931 · Fuselage Main, StructureSDR ABXA030375Web · corrodedCUSP WEB STA 908 - 965, LEFT BUTT LINE 44 - 54, LIGHT HOLES CORRODED LOWER SURFACE. REPLACED CUSP WEB IAW DC-9 SRM 51-30-2 AND 51-30-1.Sep 16, 2003 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 0301769937Duct · damagedRT LEADING EDGE SLAT DID NOT EXTEND DURING APPROACH FOR LANDING. THE SLAT DISAGREEMENT LIGHT DID ILLUMINATE AND THE SLAT EXTEND LIGHT DID NOT. THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL TO THE RIGHT UNTIL SLATS WERE RETRACTED. LANDING WAS UNEVENTFUL. MAINTSep 15, 2003 · N908H · Doug DC931 · Leading Edge Slat Control System
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