Douglas DC-9-32

Service difficulty reports · 12,755

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 = 'DC932'
  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 MWEA020412Shear Tie · crackedAFT ACCESSORY COMPARTMENT FRAME STATION 1019. DOUBLER HAS A CRACK LOCATED BELOW LONGERON 14 LEFT. FABRICATED AND INSTALLED FORMER.Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020408Longeron · crackedAFT ACCESSORY COMPARTMENT LONGERON 2 LEFT AND HAS A CRACK AT STATION 1076. REMOVED DAMAGED SECTION 2 LEFT, FABRICATED, INSTALLED LONGERON. INSTALLED REPAIR SPLICE.Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020416Longeron · dentedAT STATION 484 LONGERON 19 RIGHT HAS A DENT BEYOND LIMITS PER SRM 53-04. FABRICATED AND INSTALLED DOUBLER.Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020415Doubler · corrodedFUSELAGE INTERNAL SKIN DOUBLER SHOWS SIGNS OF EXFOLIATION CORROSION AT STATION 996 - 1019. REMOVED INTERNAL DOUBLER AND SKIN. FABRICATED AND INSTALLED INTERNAL DOUBLER AND INSTALLED NEW SKIN.Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020414Panel · corrodedCORROSION ON LEFT LOWER DIAMOND PANEL FORWARD OF MAIN LANDING GEAR. FABRICATED AND INSTALLED FILLER.Jun 17, 2002 · N501ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020420Controller · malfunctionedPRESSURIZATION INOP DURING CLIMB, SWITCHED TO MANUALLY CONTROLLED PRESSURIZATION AT CRUISE ABOUT 10 MINUTES. CABIN WENT TO FULL CLIMB BUT COULD NOT BE CONTROLLED MANUALLY. INITIATED EMERGENCY DESCENT, HAD NORMAL PACK PRESSURE. DEFERRED PER MEL 21-25 T FUNCTJun 8, 2002 · N301ME · Doug DC932 · Cabin Pressure ControllerSDR ABXA020040Frame · crackedCANTED FRAME 1137 HAD 2 EACH CRACKS COMMON TO STIFFENERS AT 11 AND 1 O'CLOCK POSITIONS. REPLACED LEFT AND RIGHT FRAMES IAW DC-9 SRM 51-30-2 AND 51-30-5.Jun 7, 2002 · N901AX · Doug DC932 · Wing StructureSDR ABXA020039Former · cracked3RD LEADING EDGE NOSE RIB, OUTBOARD OF #11 SLAT TRACK, WAS CRACKED AT FASTENER, LOWER FORWARD END. REPLACED LEFT WING LEADING EDGE RIB FORMER IAW DC-9 SRM 51-30-2, 51-30-5 AND 51-10-3.Jun 6, 2002 · N901AX · Doug DC932 · Wing StructureSDR ABXA020038Rib · cracked4 EACH LEADING EDGE NOSE RIBS BETWEEN TRACKS 10 AND 11, HAD CRACK INDICATIONS AT AFT EDGES. REPAIRED NOSE RIBS AT STATIONS XRS 466-473-479-491 IAW REA D957-44307-MR.Jun 6, 2002 · N901AX · Doug DC932 · Wing, Rib/BulkheadSDR ABXA020037Rib · crackedCRACK INDICATION ON AFT END OF LEADING EDGE NOSE RIB, INBOARD OF NR 10 SLAT TRACK. REPAIRED NOSE RIB IAW REA D957-44307-MR.Jun 6, 2002 · N901AX · Doug DC932 · Wing, Rib/BulkheadSDR 0201909951Duct · damagedUPON SLAT EXTENSION, THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED IN MSP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT -T- DUCT OUTER TOP FORWARD POSITION DAMAGED FRJun 5, 2002 · N9347 · Doug DC932 · Leading Edge Slat Control SystemSDR MWEA020418Transceiver · malfunctionedJUST AFTER DEPARTURE FROM MILWAUKEE RADAR INDICATOR BLANKED OUT. RECYCLED UNIT OFF AND ON DISPLAY CAME YELLOW ONLY AND FLICKERED DISPLAY WAS SAME ALL THE WAY TO GATE. RETURNED TO MILWAUKEE. REPAIRED AND REPLACED WEATHER RADAR TRANSCEIVER SYSTEM OPS CHECK OKJun 4, 2002 · N207ME · Doug DC932 · Weather Radar SystemSDR MWEA020391Stringer Clip · corrodedAFT ACCESSORY COMPARTMENT LONGERON 22 CLIP RIGHT HAS LIGHT CORROSION, LOCATED JUST FORWARD OF CANTED FRAME STATION 1121. REMOVED AND REPLACED END FITTING.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020403Frame · corrodedAFT CARGO COMPARTMENT FRAME STATION 870 HAS LIGHT CORROSION AROUND LONGERON 30 ATTACH BOLTS. CUT OUT DAMAGED AREA OF FRAME AND INSTALLED REPAIR PARTS.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020402Frame · corrodedLIGHT CORROSION ON AFT FACE OF FORWARD FRAME 237 FROM LONGERON 29 LEFT TO 26 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLERS.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020401Frame · corrodedMODERATE CORROSION ON AFT FACE OF FORWARD FRAME 332 AT LONGERON 30, 29, & 28 RIGHT. REMOVED AND REPLACED FRAME SECTION REPAIR.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020400Skin · corrodedAFT ACCESSORY COMPARTMENT SKIN HAS HEAVY CORROSION ON SKIN AT STATION 1009 BETWEEN LONGERON 18 AND 19 RIGHT. FABRICATED AND INSTALLED DOUBLER, FAIRING PLATE, AND SHIMS.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020399Web · tornWEB BELOW LEFT AFT OVERWING EMERGENCY EXIT DOOR HAS A LARGE HOLE/TEAR IN IT. -- REMOVED AND REPLACED WEB.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020398Shear Tie · crackedAFT ACCESSORY COMPARTMENT FRAME STATION 1059 SHEAR TIE IS CRACKED BELOW LONGERON 15 RIGHT. -- FABRICATED AND INSTALLED SHEAR TIE.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020397Longeron · dentedA SERIES OF SMALL DENTS BETWEEN STATION 851-889, LONGERONS 24 & 25 RIGHT. (REFERENCE CO #6277) -- FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020396Door Frame · chafedAFT RIGHT EMERGENCY EXIT DOOR JAMB IS CHAFED AT UPPER LATCH ASSY. LOCATED, DRILLED AND INSTALLED DOUBLER.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020395Door Frame · chafedRIGHT FORWARD EMERGENCY EXIT DOOR JAMB IS CHAFED AT THE TOP LATCH. LOCATED, DRILLED, AND INSTALLED DOUBLER.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020394Longeron · corrodedAFT ACCESSORY COMPARTMENT LONGERON 19 LEFT HAS AREAS OF LIGHT CORROSION UNDER FLANGES ON TOP AND BOTTOM SIDE FROM STATION 1080 TO CANTED FRAME 1121. MANUFACTURED AND INSTALLED LONGERON.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020393Longeron · corrodedAFT ACCESSORY COMPARTMENT LONGERON 21 LEFT HAS LIGHT CORROSION UNDER BOTTOM FLANGE AT STATION 1080. REMOVED AND REPLACED LONGERON SECTION.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020392Skin · corrodedAFT ACCESSORY COMPARTMENT, SKIN BELOW LONGERON 18 LEFT STATION 1086 TO CANTED FRAME 1121 HAS CORROSION ON INNER SURFACE. FABRICATED AND INSTALLED SKIN.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA020390Fitting · worn#5 SLAT INBOARD SADDLE FITTING BUSHINGS WORN. -- REMOVED AND REPLACED RIB.Jun 4, 2002 · N501ME · Doug DC932 · Leading Edge DevicesSDR MWEA020389Web · puncturedCOCKPIT SUBFLOOR AT STATION 134 APPROXIMATELY 24 INCHES RIGHT OF THE AIRCRAFT CENTERLINE IS PUNCTURED. FABRICATED AND INSTALLED REPAIR DOUBLER.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020388Doubler · chafedFORWARD PASSENGER DOOR HANDLE CHAFING ON DOUBLER AROUND HANDLE CUTOUT. REMOVED AND REPLACED DOUBLER.Jun 4, 2002 · N501ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA020387Longeron · corrodedAFT ACCESSORY COMPARTMENT LONGERON 15 LEFT HAS LIGHT CORROSION UNDER TOP FLANGE AT STATION 1076. REMOVED AND REPLACED LONGERON SECTION AND SPLICE.Jun 4, 2002 · N501ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR GTIA020580Servo · faultyTPA - FLT 276 - AUTO PILOT AILERON SERVO IS ERRATIC IN ALL REQUIRES OF FLIGHT 276. REMOVED AND REPLACED SERVO AUTO DRIVE. OPS CHECK OK. BITE CHECK FOR SERVO PORTION OF CHECK ON ROLL COMP. NO DEFECTS NOTED. (M)Jun 3, 2002 · N12536 · Doug DC932 · Autopilot Main ServoSDR AT0200068Acm · lowAFT LAVATORY SMOKE DETECTORS ACTIVATED ON TAKEOFF. FOUND RIGHT AIR CYCLE MACHINE GIVING OFF AN OIL SMELL. REMOVED AND REPLACED COALESCER BAG AND SERVICED AIR CYCLE MACHINE TO PROPER LEVEL.Jun 3, 2002 · N837AT · Doug DC932 · Cabin Cooling SystemSDR GTIA020663Wire · damagedDTW - REF M-22 35589 AFT TAIL COMP WALKWAY EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRE FOR WALKWAY LIGHTS, OPS CHECK NORMAL IAW DC9 MM 33-51-00. (M)Jun 2, 2002 · N133NK · Doug DC932 · Light System WiringSDR GTIA020662Power Supply · dischargedDTW - AFT FLIGHT EMERGENCY LIGHT STAY ON ALL THE TIME AND TAIL COMP EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED AFT LEFT LAVATORY BATTERY POWER SUPPLY FOR AFT FLIGHT EMERGENCY LIGHT. OPS CHECK GOOD. (M)Jun 2, 2002 · N133NK · Doug DC932 · Emergency LightingSDR GTIA020661Power Supply · dischargedDTW - FOUND OVERWING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY AT B5-25. OPS CHECK GOOD. (M)Jun 2, 2002 · N133NK · Doug DC932 · Emergency LightingSDR MWEA020385Proximity Sensor · faultyTHE AMBER GEAR DOOR OPEN LIGHT CAME ON AND STAYED ON EVEN WITH ALL HYDRAULIC PUMPS ON. ON START OF DESCENT THE LIGHT WENT OUT. WHEN SELECTING GEAR DOWN FOR LANDING ALL LIGHTS WORKED NORMAL. REMOVED AND REPLACED RIGHT GEAR DOOR PROXIMITY SENSOR AND PERFORMEDJun 1, 2002 · N205ME · Doug DC932 · Landing Gear Position and WarningSDR 0201919951Door · damagedDURING APPROACH FOR LANDING WHEN SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE LEFT. THE SLAT DISAGREEMENT LIGHT WAS ON AND THE SLATS RETRACTED LIGHT WAS OUT. CREW CYCLED THE SLAT EXTENSION PROCEDURES AND THE SLATS AGREED AND NO TENDENCY TO ROLL. ALL INDICATIOMay 25, 2002 · N9347 · Doug DC932 · Leading Edge DevicesSDR MWEA020384Slat · puncturedLEFT WING HIT DELTA BAG CART PUNCTURING LEFT OUTBOARD SLAT PANEL. -- REMOVED AND REPLACED SLAT. OPS CHECK GOOD.May 25, 2002 · N602ME · Doug DC932 · Leading Edge Slat Control SystemSDR AT0200064Engine#1 ENGINE FAILED AT V2 ALL ENGINE PARAMETERS NORMAL EXCEPT EGT AT RED LINE 70% N1 1.4. NO OTHER ASSOCIATED LIGHTS, OIL PRESSURE, AND TEMPERATURE NORMAL. CORRECTIVE ACTION: REMOVED AND REPLACED #1 ENGINE.May 25, 2002 · N845AT · Doug DC932 · Engine Temperature Indicating SystemSDR MWEA020383Retainer · crackedRIGHT WINDOW RETAINER HAS A CRACK INDICATION IN THE TITANIUM DOUBLER. FABRICATED AND INSTALLED DOUBLER.May 24, 2002 · N501ME · Doug DC932 · Flight Compartment WindowsSDR MWEA020382Attach Fitting · crackedRIGHT FLAP #3 TRAILING EDGE PANEL UPPER INBOARD ATTACH FITTING CRACKED. -- REMOVED AND REPLACED FITTING.May 24, 2002 · N501ME · Doug DC932 · Trailing Edge FlapsSDR MWEA020381Skin · damagedLEFT SIDE OF RUDDER 5 INCHES AFT OF FORWARD SPAR BETWEEN ZR 117 AND ZR 113 HAS CREASE 2.5 INCHES LONG. FABRICATED AND INSTALLED REPAIR DOUBLER.May 24, 2002 · N501ME · Doug DC932 · Rudder, Plate/SkinSDR MWEA020380Pressure Panel · gougedCENTER WING FORWARD LOWER BULKHEAD WEB HAS 1 VERY DEEP GOUGE ON FORWARD SURFACE AT STATION 606 & LONGERON 25 LEFT. FABRICATED AND INSTALLED DOUBLER.May 24, 2002 · N501ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA020370Pan · crackedAFT CARGO DOOR INNER PAN CRACKED AT AFT LOCKING CAM. -- FABRICATED AND INSTALLED REPAIR DOUBLER.May 21, 2002 · N501ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020375Fitting · crackedCENTER WING FORWARD LOWER BULKHEAD FITTING CRACKED AT STATION 606 AND LONGERON 24 LEFT. REMOVED AND REPLACED FITTING.May 21, 2002 · N501ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020369Longeron · crackedLONGERON 17 RIGHT IS CRACKED UNDER FRAME 484. -- FABRICATED AND INSTALLED LONGERON SECTION AND REPAIR SPLICE.May 21, 2002 · N501ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020368Pan · chafedAFT CARGO DOOR INNER PAN HAS A DEEP CHAFE NEXT TO AFT LOCK CAM. FABRICATED AND INSTALLED REPAIR DOUBLER.May 21, 2002 · N501ME · Doug DC932 · Cargo/Baggage DoorsSDR MWEA020367Fitting · crackedCENTER WING FORWARD LOWER BULKHEAD FITTING CRACKED AT STATION 606 AND LONGERON 24 RIGHT. -- REMOVED AND INSTALLED FITTING.May 21, 2002 · N501ME · Doug DC932 · Wing, Rib/BulkheadSDR MWEA020365Web · crackedAFT ACCESSORY COMPARTMENT BULKHEAD WEB AT FRAME STATION 1038 IS CRACKED AT LIGHTNING HOLE AT LONGERON 12 LEFT. -- FABRICATED AND INSTALLED REPAIR DOUBLER.May 21, 2002 · N501ME · Doug DC932 · Fuselage Main, BulkheadSDR 0201949605Skin · crackedDuring Hck in DHN, a crack was found in the skin common to the fasteners picking up the APB tee cap. Repaired per EA 96-190036.May 20, 2002 · N605NW · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA010887Light · looseWHEN LANDING GEAR EXTENDED, NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE RED INTRANSIT LIGHT WAS EXTINGUISHED ALONG WITH THE UNSAFE LIGHT. THE PROBLEM CORRECTED BY ITSELF. THE NOSE LANDING GEAR UNSAFE BULB WAS LOOSE IN THE SOCKET. REPLACED BULB AND PERFORMED A May 20, 2002 · N900AX · Doug DC932 · Landing Gear Position and Warning
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