Douglas DC-9-31

Service difficulty reports · 7,433

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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 ABXA020205Angle · damagedRIGHT DORSAL FIN ATTACH ANGLE HAD TOOLING DAMAGE IN THE RADIUS. REPLACED DORSAL FIN ATTACH ANGLE IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5, AND REA D953-44887.Aug 26, 2002 · N936AX · Doug DC931 · Fuselage Structure (General)SDR ABXA020204Skin · crackedFUSELAGE SKIN CRACKED AT UPPER/AFT STOP. REPAIRED UPPER AFT DOOR CUTOUT IAW DC-9 SRM 53-05.Aug 26, 2002 · N936AX · Doug DC931 · Fuselage Main, Plate/SkinSDR 0203079952Door · crackedDuring Hck in DHN, aft cargo door was found to be cracked at the #2 forward doorstop. Repaired per EA 99-191323.Aug 13, 2002 · N916RW · Doug DC931 · Fuselage Main, StructureSDR 0203049952Spar · crackedDuring HCK in DHN, the rear spar chord was found cracked. Repaired per EA 99-131324Aug 8, 2002 · N916RW · Doug DC931 · Wing Main, Frame StructureSDR 2003F00047Latch · wornAFTER T/O FROM PIE, THE LANDING GEAR LEVER WAS PLACED IN THE UP POSITION, CREW REPORTED NO RESPONSE TO GEAR HANDLE SELECTION, GEAR REMAINED DOWN AND LOCKED AND MLG DOORS OPEN. RECYCLED THE GEAR HANDLE, NO HELP. RETURNED TO PIE. DURING THE POST FLIGHT INSPECAug 2, 2002 · N932MJ · Doug DC931 · Landing Gear Door Retract SectionSDR A4J2002F00001Latch · wornAFTER TAKEOFF, LAND GR LVR WAS PLACED IN UP POSITION, FLT DECK CREW REPORTED NO RESPONSE TO GR HNDL (UP) SELECTION, WITH GR REMAINING IN DOWN AND LOCKED POS AND MN GR DOORS OPEN. RECYCLING OF THE GR HNDL WAS NO HELP. MAINT WAS NOTIFIED AND A/C RETURNED. MAIAug 2, 2002 · N932MJ · Doug DC931 · Landing Gear Retraction/Extension SystemSDR 0202459997Slide · malfunctionedTAIL CONE WAS DROPPED AT THE GATE AND THE SLIDE DID NOT DEPLOY AS DESIGNED. THE TAIL CONE DID NOT RECEIVE ANY DAMAGE AND WAS RE-ATTACHED BACK INTO POSITION AND THE AIRCRAFT WAS FERRIED TO ATL FOR SLIDE MAINTENANCE AND RIGGING. PERFORMED COMPLETE ADJUSTMENT AJul 26, 2002 · N8933E · Doug DC931 · Escape SlideSDR 0202489933Service difficultyDURING CLIMB, FLIGHT ATTENDANT NOTICED SMOKE IN CABIN AND FORWARD LAV ALARM SOUNDED. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND AN APU OIL LEAK. OIL LEAK WAS CORRECTED, CLEANED APU AREA, AND COMPJul 25, 2002 · N1334U · Doug DC931 · APU Oil SystemSDR 0202389937Controller · malfunctionedWHILE IN CRUISE AT FL250, THE CABIN ALTITUDE WENT TO 12,000 FEET. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO 9,000 FEET AND LEVELED OFF. MASKS DID NOT DEPLOY AND FLIGHT CONTINUED TO DESTINATION. LANDING AT BUF WAS UNEVENTFUL. CREW STATED THAT THE MANUAL SPRJul 19, 2002 · N908H · Doug DC931 · Cabin Pressure ControllerSDR 0203039931Skin · crackedDuring Hck in ATL, a .125 crack was found on the RH skin adjacent to the wiper cutout area. Repaired per EA 99-190551.Jul 18, 2002 · N90S · Doug DC931 · Fuselage Main, Plate/SkinSDR 0202299907Psu · defectiveFLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE SMELL AIRBORNE AND FELT IT WAS ASSOCIATED WITH SEAT 21AB CALL LIGHT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED SEAT 21AB PSU. OPERATIONAL CHECK OK.Jul 17, 2002 · N957N · Doug DC931 · Passenger Compartment EquipmentSDR 0203029975Angle · crackedDuring Hck in ATL Maintenance Base, the LH side of the verticle stabilizer attach angle (aft) was found cracked at station 1100. Repaired per EA 99-190557.Jul 15, 2002 · N90S · Doug DC931 · Fuselage Main, StructureSDR 0202329943Slide · malfunctionedTAIL CONE WAS ACCIDENTALLY DROPPED AND THE EVACUATION SLIDE DID NOT DEPLOY. MAINTENANCE REINSTALLED THE SLIDE AND CHECKED THE INSTALLATION. ALSO, THE DAMAGE TO THE TAIL CONE WAS TEMPORARILY REPAIRED TO ALLOW THE AIRCRAFT TO BE FERRIED TO MEM.Jul 13, 2002 · N1308T · Doug DC931 · Escape SlideSDR 0202339995Switch · defectiveWHEN THE NOSE TAXI LIGHTS WERE TURNED ON AFTER POWERBACK, SPARKS AND SMOKE CAME OUT FROM UNDER THE NOSE LIGHT SWITCH PANEL. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NOSE TAXI LIGHT SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.Jul 11, 2002 · N8978E · Doug DC931 · Exterior LightingSDR 0203019975Bulkhead · crackedDuring HCK in ATL, a crack was found on the LH portion of the APB Door cutout upper jamb. A repair of the upper jamb area was extended to incorporate the the cracked area. Repaired per EA 99-190542.Jul 9, 2002 · N9339 · Doug DC931 · Fuselage Main, StructureSDR 0203009931Frame · crackedDuring HCK in ATL, frames station 389 and 408 were found cracked at longeron 17. Repaired per EA 99-190536.Jul 9, 2002 · N90S · Doug DC931 · Fuselage Main, FrameSDR ABXA020046Warning System · malfunctionedUPON SELECTING GEAR DOWN, NOSE GEAR UNSAFE LIGHT ILLUMINATED AND NOSE GEAR GREEN LIGHT DID NOT COME ON. GEAR WARNING HORN SOUNDED. RECYCLED GEAR, ALL INDICATIONS NORMAL. OPS CHECKED GOOD IAW DC-9 MM 32-60.Jul 9, 2002 · N945AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA020155Doubler · crackedCRACK IN FUSELAGE SKIN AT STATION 994, LONGERON 12 RIGHT, BETWEEN 2 RIVETS AND EXTENDING 1/4" PAST BOTH RIVETS. REPAIRED CRACK IAW DC-9 DWG SR09530151 AND E.A. 5311005-034.Jul 8, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)SDR 0202229954Controller · malfunctionedWHILE LEVEL AT FL290, THE CABIN PRESSURE ALTITUDE WOULD FLUCTUATE BETWEEN A 2000 FPM CLIMB TO ZERO. AS THE ACTUAL CABIN ALTITUDE REACHED 10,000 FEET, THE CREW MANUALLY DEPLOYED THE PASSENGER MASKS AND AN EMERGENCY DESCENT WAS INITIATED. CABIN ALTITUDE REACHEJul 8, 2002 · N621RW · Doug DC931 · Cabin Pressure ControllerSDR ABXA020160Cap · crackedLONGERON END CAP CRACKED NR 11 RIGHT. INSTALLED NEW END CAP NR 11 RIGHT IAW DC-9 SRM 51-30-2 AND 51-30-5.Jul 6, 2002 · N908AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA020165Angle · corrodedBOTTOM OF SERVICE DOOR CUTOUT, INNER JAMB ANGLE EXFOLIATED, LONGERON 18 RIGHT. REPLACED JAM ANGLE AND REPAIRED AREA IAW DC-9 SRM 51-30-5 AND 51-10-3.Jul 2, 2002 · N943AX · Doug DC931 · Fuselage Main, StructureSDR ABXA020164Web · crackedRIGHT CUSP CRACKED AT STATION 937. REPAIRED AREA IAW DC-9 SRM 53-01.Jul 2, 2002 · N943AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA020163Splice · crackedBULKHEAD 965 CABIN FLOOR, LOWER FITTING WAS CRACKED AT LEFT BUTT LINE 33. REPLACED FITTING IAW DC-9 SRM 51-30-5.Jul 2, 2002 · N943AX · Doug DC931 · Fuselage Main, Floor BeamSDR ABXA020162Skin · crackedFUSELAGE SKIN CRACKED AT UPPER AFT CORNER OF MAIN ENTRY DOOR CUTOUT. LOCATED AT UPPER AFT DOOR STOP. REPAIRED CRACKED FUSELAGE SKIN AT UPPER AFT CORNER OF MAIN ENTRY DOOR CUTOUT IAW DC-9 REWORK DWG SR0953252-7001.Jul 2, 2002 · N943AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA020161Angle · crackedLONGERON 18L CUSP ANGLE FS 980, CORRODED AND CRACKED. REPAIRED CUSP ANGLE IAW REA D953-44535.Jul 2, 2002 · N943AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 0301069952Oil Cooler · leakingDURING CLIMB FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN CABIN. FLIGHT ATTENDANT DISCHARGED A HALON FIRE EXTINGUISHER IN THE AFT RIGHT LAV. FLIGHT CREW RETURNED AC TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. NO EVIDENCE OF A FIRE WAS FOUND. MAINJul 1, 2002 · N916RW · Doug DC931 · APU Oil SystemSDR 0202119952Smoke · detectedSMOKE WAS REPORTED IN THE CABIN SHORTLY AFTER TAKEOFF. SMOKE CLEARED PRIOR TO LANDING A FEW MINUTES LATER. AFT LAV SMOKE DETECTOR SOUNDED. FLIGHT LANDED BACK AT RAP SAFELY. MAINTENANCE RAN PACKS AND APU, CHECKED FOR WIRING FAULTS OR HOT BALLAST. NO TROUBLJun 28, 2002 · N916RW · Doug DC931 · Air Distribution SystemSDR ABXA020008SwitchWHEN CENTER FORWARD BOOST PUMP WAS TURNED ON, SPARKS CAME OUT OF THE PANEL AND TWO CIRCUIT BREAKERS TRIPPED.REPLACED THE FORWARD CENTER BOOST PUMP ON/OFF SWITCH.Jun 28, 2002 · N924AX · Doug DC931 · Fuel Boost PumpSDR 0202159975Cap · corrodedDuring an MCK in ATL, corrosion was found in the upper flange of the center wing upper skin cap. The cap is located at sta 681. The corrosion was blended out and at three locations was determined to be ouit of limits. Repaired per EA 99-190532.Jun 27, 2002 · N9339 · Doug DC931 · Wing Main, Frame StructureSDR 0202149975Cap · corrodedDuring Mck in Atl, corrosion was found in the upper flange of the center wing upper skin cap. The cap is located at sta 681. The corrosion was blended out and at one location was determined to be out of limit. Repaired per EA 99-190519.Jun 27, 2002 · N9339 · Doug DC931 · Wing Main, Frame StructureSDR ABXA020159Bulkhead · damagedAFT PRESSURE BULKHEAD SIDE SKIN SPLICED AT Z 14.00. SPLICE NOT IAW DOUGLAS AFT PRESSURE BULKHEAD RE-WORK. SPLICED NEW SECTION (LOWER) OF RIGHT AFT PRESSURE BULKHEAD WEB IAW REA D953-44534-MR AND DOUGLAS DWG J060088.Jun 25, 2002 · N908AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA020158Doubler · crackedANGLED DOUBLER COMMON TO #7 SLAT TRACK RIB INBOARD AND FRONT SPAR CRACKED. REPAIRED AREA IAW DC-9 SRM 57-09.Jun 24, 2002 · N908AX · Doug DC931 · Wing StructureSDR ABXA020157Rib · crackedNR 8 SLAT TRACK INBOARD LEADING EDGE RIB ANGLE COMMON TO ROLLERS CRACKED AT AFT LOWER VERTICAL LEG. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5.Jun 24, 2002 · N908AX · Doug DC931 · Wing, Rib/BulkheadSDR 0202079976O-Ring · damagedLEFT HYDRAULIC PRESSURE AND QUANTITY WENT TO ZERO. COMPLIED WITH COM PROCEDURES AND THE LEFT QUANTITY RETURNED TO 5 QUARTS BUT PRESSURE REMAINED AT ZERO. FLIGHT RETURNED TO A SAFE UNEVENTFUL LANDING BACK TO DTW. MAINTENANCE FOUND THE RESERVOIR EMPTY AND FOUJun 22, 2002 · N9340 · Doug DC931 · Hydraulic System, MainSDR ABXA020156Doubler · cracked5" CRACK TOP OF FUSELAGE AT #1 LONGERON IN AFT PRESSURE BULKHEAD AREA. REPAIRED CRACK IAW DC-9 DWG SR0953151 AND E.A. 5311005-034.Jun 21, 2002 · N908AX · Doug DC931 · Fuselage Structure (General)SDR 0202139975Frame · crackedDuring H-CK at ATL base MTC. a 1/2" crack was found at sta 1132 on the forward side of the 9911839-19 doubler. The crack extended from the upper pulley bracket hole for NAS 1105 on the LH side of the aircraft in the outboard direction. Repaired per EA 99-19051Jun 21, 2002 · N9339 · Doug DC931 · Fuselage Main, StructureSDR 0202019963Service difficultyDURING CLIMB, THE LEFT AFT SMOKE DETECTOR SOUNDED AND FLIGHT ATTENDANTS REPORTED ODOR IN THE CABIN. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED COALESCER SOCKS AND PERFORMED A PACK BURNOUT. APU ON MEL.Jun 12, 2002 · N913RW · Doug DC931 · APU Oil SystemSDR 0201759955Oxygen Mask · malfunctionedTHE EMERGENCY OXYGEN MASK FOR THE FLIGHT ATTENDANT'S AFT JUMPSEAT DID NOT DEPLOY WHEN ALL OTHER PASSENGER MASKS DID DURING AN EMERGENCY DESCENT DUE TO LOSS OF CABIN PRESSURIZATION. THE MASK FINALLY DEPLOYED AFTER THE AIRCRAFT LEVELED OFF AT 10,000 FEET. MAINJun 4, 2002 · N922RW · Doug DC931 · Crew Oxygen SystemSDR 0201749955Warning System · false indicationUPON DESCENT FROM FL290 TO FL270, THE CABIN PRESSURE LIGHT AND THE MASTER WARNING LIGHT ILLUMINATED. CREW INITIATED AN EMERGENCY DESCENT AND DONNED OXYGEN MASKS. ALL CABIN OXYGEN MASKS DEPLOYED. THE AIRCRAFT LEVELED OFF AT 10,000 FEET AND CONTINUED TO DFW. Jun 4, 2002 · N922RW · Doug DC931 · Cabin Pressure IndicatorSDR 0201739993Landing Gear · collapsedLANDING GEAR COLLAPSED DURING LANDING ROLL. SPECIFICS UNKNOWN AT THIS TIME DUE TO THE LOG PAGES BEING SECURED FOR INVESTIGATION.Jun 3, 2002 · N8986E · Doug DC931 · Main Landing GearSDR ABXA010903Rheostat · failedCAPTAIN'S OVERHEAD MAP LIGHT WAS SPARKING AND SMOKING. REPLACED THE CAPTAIN'S OVERHEAD MAP LIGHT RHEOSTAT. OPS CHECKED GOOD IAW DC-9 MM.Jun 1, 2002 · N937AX · Doug DC931 · Flight Compartment LightingSDR 0201659906Seal · out of positionDURING CLIMBOUT, THE CABIN PRESSURE WARNING LIGHT ILLUMINATED. CABIN PRESSURE CLIMBED THROUGH 10,000 FEET TO 12,500 FEET WHEN CREW ACCOMPLISHED AN EMERGENCY DESCENT TO 10,000 FEET AND DIVERTED TO MKE. NO MENTION OF COM OR OF MANUAL PRESSURE CONTROL. LANDINGMay 22, 2002 · N956N · Doug DC931 · Entrance StairsSDR 0201649911Apu · leakingDURING GROUND COOLING IN CLT, THE FLIGHT ATTENDANT NOTED A TRACE OF SMOKE IN THE CABIN. PACK WAS ADJUSTED TO WARMER TEMP AND PROBLEM ENDED. ON TAKEOFF, THE SMOKE RETURNED AND CAUSED THE FORWARD LAV SMOKE DETECTOR TO ALARM FOR ABOUT 3 MINUTES THEN CEASED. THMay 20, 2002 · N961N · Doug DC931 · APU Oil SystemSDR ABXA010886Switch · defectiveDURING INITIAL GEAR EXTENSION, THE NOSE LANDING GEAR LIGHT FLICKERED ON AND OFF AND CONTINUED TO DO SO UNTIL THE GEAR WAS RAISED. FOUND NOSE LANDING GEAR DOWN LOCK SWITCH TO BE STICKING. REPLACED SWITCH IAW DC-9 MM 32-60-01. PERFORMED A GEAR SWING. ALL INDICATMay 20, 2002 · N907AX · Doug DC931 · Landing Gear Position and WarningSDR 0201609981Flex Line · leakingINBOUND TO VPS, THE AIRCRAFT LOST THE HYDRAULIC FLUID FROM THE RIGHT SYSTEM. CREW FOLLOWED COM PROCEDURES AND WAS ABLE TO LAND WITHOUT FURTHER INCIDENT IN VPS. MAINTENANCE FOUND A PREVIOUSLY INSTALLED TEMP FLEX LINE LEAKING. REPLACED THE FLEX LINE WITH TWO NEWMay 14, 2002 · N994Z · Doug DC931 · Hydraulic System, MainSDR 0201599969Valve · leakingDURING START WHEN THE CREW ATTEMPTED TO PRESSURIZE THE RIGHT HYDRAULIC SYSTEM, THE HYDRAULIC PRESSURE INDICATION DID NOT RISE AND THE HYDRAULIC QUANTITY INDICATION DROPPED TO ZERO. FLIGHT ABORTED THE START AND RETURNED TO THE GATE. MAINTENANCE FOUND THE RIGHMay 14, 2002 · N9333 · Doug DC931 · Brake Anti-Skid SectionSDR 0201569972Valve · failedDURING CLIMBOUT WITH THE ENGINE AND AIRFOIL ANTI-ICE SYSTEM ACTIVATED, THE FORWARD AND LEFT REAR LAV SMOKE DETECTOR ALARMS SOUNDED. THE RIGHT AIR CONDITION SUPPLY TEMP HIGH LIGHT ILLUMINATED FOR ABOUT 10-15 MINUTES AND THEN EXTINGUISHED. THE LAV SMOKE DETECTMay 12, 2002 · N9336 · Doug DC931 · Cabin Cooling SystemSDR ABXA010874Rheostat · defectiveCAPTAIN'S MAP LIGHT SPARKED WHEN MOVED LENS BALL. REPLACED RHEOSTAT ON CAPTAIN'S MAP LIGHT IAW DC-9 MM 33-10-00.May 11, 2002 · N937AX · Doug DC931 · Flight Compartment LightingSDR 0201399944Duct · bindingDURING APPROACH FOR LANDING WHEN SLATS EXTENDED, THE SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED. FOLLOWED COM PROCEDURES AND THE FLIGHT ATTENDANT VERIFIED THE RIGHT SLAT DID NOT DEPLOY. FLAP ONLY LANDING AT MSP WAS UNEVENTFUL. MAINTENANCE DMay 4, 2002 · N1309T · Doug DC931 · Airfoil Anti/De-ice SystemSDR 0201529954Door Frame · crackedWhile in MSP during line operations a crack was found on the Non-ventral APB door jamb. The crack is located at the end of the LH side #2 radial.Repaired per EA 99-189338.May 2, 2002 · N921RW · Doug DC931 · Fuselage Main, Structure
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