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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MWEA001252Thermostat · inoperativeDURING CLIMBOUT WITH CLIMB POWER, FULL ANTI-ICE "ON" RIGHT ICE PROTECT TEMP HIGH ANNUNCIATOR ILLUMINATED. QRH PROCEDURE TURNED OFF LIGHT IN ABOUT 1 MINUTE. -- PERFORMED RESISTANCE CHECK ON ELECTRONIC THERMO SWITCH NO DEFECTS NOTED. FOUND RIGHT ICE PROTECTIOSDR AT0100083Rib · crackedFOUND LEFT FLAP INNER SUPPORT RIBS CRACKED. INSTALLED 2 ANGLE REPAIRS IAW DC9 SRM 51-10, 57-01, AND 51-10-02.SDR CA010321010Turbine Blades · failed(CAN) AIRCRAFT REJECTED TAKEOFF ON ROLL DUE TO THE EPR INDICATION THAT WENT FROM 2.01 DOWN TO 1.6 (ENGINE PRESSURE RATIO). FLIGHT ATTENDANT REPORTED HEARING A LOUD BANG. ENGINE CONTAINED. MECHANIC FOUND EVIDENCE OF DAMAGE TO THE TURBINE SECTION. REPLACED LT ENSDR CA010201004Turbine · damaged(CAN) AIRCRAFT REJECTED TAKEOFF ON ROLL DUE TO THE EPR INDICATION THAT WENT FROM 2.01 DOWN TO 1.6 (ENGINE PRESSURE RATIO). FLIGHT ATTENDANT REPORTED HEARING A LOUD BANG. ENGINE CONTAINED.MECHANIC FOUND EVIDENCE OF DAMAGE TO THE TURBINE SECTION. REPLACED LT ENGSDR AT0000506Stringer · corrodedFOUND STRINGER 20R AND 21R BS 230 - 360 CORRODED BEYOND LIMITS. REMOVED AND REPLACED STRINGER 20R AND 21R BS 230 - 360 IAW DC9 SRM 51-10-03.SDR MWEA001244Shear Tie · crackedSHEAR CLIP CRACKED AT FUSELAGE STATION 945 BETWEEN LONGERON 15 RIGHT. -- REMOVED AND REPLACED SHEAR CLIP.SDR MWEA001254Fitting · crackedLEFT LAV AREA, AFT VENTRAL DOOR JAMB LEFT SIDE TWENTY INCHES ABOVE FLOOR, FOUND CRACKED FITTING. -- REMOVED, FABRICATED, AND INSTALLED FITTING.SDR MWEA001253Intercostal · damagedE&E BAY DOOR HAD TOOLING MARKS IN RADIUS OF STIFFNER(INTERCOSTAL) AND MISDRILLED HOLE. -- REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL.SDR MWEA001243Post · damagedFO'S CLEARVIEW WINDOW POST HOLE ELONGATED TO .358. -- REMOVED AND REPLACED WINDOW POST.SDR MWEA001242Seat Track · damagedCABIN FLOORBOARD B6 AT STATION 617 TO 639 LT, BETWEEN NR 1 & 2 SEAT TRACKS HAS HOLES CRACKED OUT. -- REMOVED AND REPLACED FLOORBOARD.SDR MWEA001251Acm · inoperativeAFTER TAKE OFF, CABIN CREW ADVISED OF STRONG BURNING ODOR, 3 LOUD THUDS FROM RIGHT AFT AREA WERE HEARD. -- REMOVED AND REPLACED WATER SEPERATOR SOCK, AIR CYCLE MACHINE, AND 35 DEGREE LEE VALVE.SDR AT0000504Smoke Detector · damagedFOUND JUST AFTER TAKE OFF 'A' LOOP SMOKE DETECTOR IN FORWARD CARGO COMPARTMENT LIGHT ILLUMINATED. RETURNED TO CAK AIRPORT LIGHT EXTINGUISHED AFTER LANDING. CORRECTIVE ACTION: MAINTENANCE CHECKED DETECTION SYSTEM, FOUND DETECTORS DAMAGED FOSDR ABXA000530Bracket · bentAT FL 230, CABIN PRESSURE LIGHT ILLUMINATED. THE CREW PERFORMED EMERGENCY CHECKLIST AND DESCENDED TO 22,000 FT. AT 22,000 FT, CABIN PRESSURIZATION WAS MAINTAINED. MAINTENANCE INSPECTED AND FOUND THE FORWARD MAIN ENTRY DOOR LEAKING DURING PRESSURIZATION CHECKSDR MWEA001248Apu · contaminatedDURING PUSH-BACK, AFT RIGHT AND LEFT LAV SMOKE DETECTORS SOUNDED. -- SUSPECT EXTERNAL OIL LEAK FROM APU. RAN APU FOR 30 MINUTES. NO OIL LEAKS NOTED.SDR MWEA001245Fairing · crackedRH VERTICAL STAB SKIN UNDER AFT LOWER HORIZONTAL STAB FAIRING IS CRACKED. -- REPLACED SKIN.SDR AT0000513Fitting · crackedFOUND RIGHT AFT KEEL BEAM FITTING CRACKED AT BS 738 - 756. REMOVED AND REPLACED FITTING ON RIGHT MLG WHEEL WELL, REMOVED AND REINSTALLED HYDRAULIC RESERVIOR AND HYDRAULIC LINES IAW DC9 MM 29-00-01 AND SRM 51-10-6, 51-30-1.SDR MWEA001238Pump · inoperativeDURING TAKE-OFF RIGHT HYDRAULIC TEMP HIGH LIGHT CAME ON. TAKE-OFF ABORTED. -- REPLACED ELECTRIC HYDRAULIC PUMP.SDR AT0000486Controller · inoperativeAUTO PRESSURIZATION FAILED IN FLIGHT. CABIN PRESSURE WAS CONTROLLED IN MANUAL. STOWED ALL MASK, PERFORMED OPERATIONAL CHECK OF MASK DROP SYSTEM. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. IAW DC9 MM 21-32.SDR AT0000508Floor Support · crackedFOUND AFT CRAGO COMPARTMENT FRAME 813 LONGERON 29R CARGO FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT, WELD REPAIR FLOOR SUPPORT, REINSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-4, 51-30-2, EA 12-5321-29-C1362, 51-30-2, 51-30-5.SDR MWEA001231Longeron · crackedLONGERON 17 LEFT CRACKED AT STATION 980. -- FABRICATED AND INSTALLED SPLICE HAT SECTION.SDR MWEA001230Longeron · crackedLONGERON 16 RIGHT CRACKED AT STATION 965. -- FABRICATED AND INSTALLED LONGERON REPAIR.SDR MWEA001234Seat Track · corrodedNR 4 SEAT TRACK AT STATION 376 HAS CORROSION IN UPPER CHANNEL AND LUGS. -- FABRICATED AND INSTALLED SEAT TRACK REPAIR.SDR MWEA001233Shear Tie · crackedSHEAR TIE JUST UNDER LONGERON 14 LEFT CRACKED AT STATION 980. -- REMOVED AND REPLACED SHEAR TIE.SDR MWEA001232Shear Tie · crackedSHEAR TIE JUST UNDER LONGERON 14 RIGHT CRACKED AT STATION 980. -- REMOVED AND REPLACED SHEAR TIE.SDR AT0000511Pylon · crackedFOUND NR 2 ENGINE PYLON LOWER AND UPPER TRAILING EDGE PANEL HAS LOOSE AND MISSING FASTENERS. REMOVED AND REPLACED NR 2 ENGINE TRAILING EDGE PANEL UPPER AND LOWER SKINS. REMOVED AND REPLACED WEDGE, REMOVED AND REINSTALLED NR 2 ENGINE PYLON TRAILING EDGE ASSEMSDR AT0000507Spar Cap · corrodedFOUND CORROSION ON FORWARD FLANGE OF LEFT HORIZONTAL UPPER REAR SPAR. REMOVED UPPER LEFT HAND HORIZONTAL SPAR CAP FROM SPAR CAP AT XRS 100. FORMED REPAIR ANGLE AND SPLICES, HEAT TREATED, DRILLED, PRIMED AND INSTALLED IAW DC9 SRM 55-02 FIGURE 21, 51-30-2, 51-SDR AT0000485Regulator · inoperativePASSING THROUGH 260FL, FIRST OFFICER HEARD SURGE FROM PAX O2 SYSTEM. ALL MASKS DEPLOYED. CABIN ALTITUDE WAS AT 7000FT. REMOVED AND REPLACED PAX O2 CYLINDER REGULATOR. IAW DC9 MM35-20SDR AT0000484Door · disengagedNOSE GEAR DOOR NOT CLOSED, DID NOT CLOSE AT GEAR RETRACTION. RESECURED DOOR ON NOSE GEAR. IAW DC9 MM32-20SDR MWEA001235A/C Pack · failedAFTER DEPARTURE FROM MCI AT 6800 FT THE LEFT PACK SHUTDOWN. JUST PRIOR TO SHUTDOWN CREW NOTED EXTREMELY WARM AIR IN COCKPIT. RETURNED TO MCI. -- DEFERRED LEFT PACK PER DMI 12-29, MEL 21-1A CH C.SDR AT0000512Skin · damagedFOUND AT BS 498R ONE STATIC DISCHARGE SPOT ON AFT SIDE OF WINDOW CUTOUT. REPAIRED STATIC DISCHARGE SPOT ON WINDOW CUTOUT IAW REO L00335.SDR AT0000509Tail Cone · corrodedFOUND VERTICAL STAB TAIL CONE HAS SURFACE CORROSION ON THE RIGHT AFT SIDE AND UNDER AFT SIDE. REMOVED CORROSION ON VERTICAL STAB. FABRICATED, TREATED AND INSTALLED DOUBLER IAW DC9 51-10-3, 51-30-1, 51-10-4.SDR AT0000510Skin · corrodedFOUND FUSELAGE SKIN BULGING AROUND FASTENERS AT BS 889 LONGERON 29R. REMOVED CORRODED SKIN, REMOVED AND REPLACED AFT CARGO DOOR FRAME INTERNAL DOUBLER, TREATED AND INSTALLED REPLACEMENT SKIN IAW REO L00337, DC9 SRM 53-04 FIGURE C12, 51-10-4, 51-10-3, 51-30-2,SDR MWEA001229Engine · lack of lubeRIGHT ENGINE OIL QUANTITY DROPPED TO 6 QUARTS IN CRUISE. -- MCI MAINTENANCE FOUND RIGHT ENGINE OIL CAP OFF. REINSTALLED CAP AND SERVICED OIL QUANTITY TO "FULL".SDR ABXA000519Separator · contaminatedDURING TAKEOFF ROLL BETWEEN V1 AND VR THE COCKPIT FILLED WITH A STRONG BURNING ODER. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCK. MAINTENANCE INSPECTED THE NUMBER ONE AND NUMBER TWO ENGINE INLETS, OUTLETS AND PNEUMATIC DUCTS FOR RESIDUES. MAINTENANCE INSPECSDR TWAA0018803Power Supply · defectiveTHE EGRESS LIGHTS WERE INTERMITTENTLY GOING ON AND OFF DURING FLIGHT. REPLACED THE EGRESS LIGHT POWER SUPPLY. CHECK-C 7-4-00 MCI.SDR TWAA0018802Connector · looseTHE LAST 4 ROWS OF EGRESS LIGHTS FLICKERED IN CLIMB. RESEATED THE CONNECTION OF THE EGRESS LIGHTING. CHECK-C 7-4-00 MCI.SDR AT0000483Wire · brokenFOUND EMERGENCY LIGHT AT AFT DOOR TO VERTICAL STAIRS WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE ON BATTERY PACK R88. IAW DC9 MM 20-50SDR MWEA001216Light · inoperativeAFT ACCESSORY EMERGENCY LIGHTS INOP. -- REPLACED LIGHT ASSEMBLY ABOVE TAILCONE RELEASE HANDLE.SDR AT0000482Circuit Breaker · trippedDURING CLIMB, CIRCUIT BREAKERS POPPED AND EMERGENCY LANDING WAS PERFORMED FOLLOWED BY AN EMERGENCY EVACUATION. TROUBLE SHOOTING IN PROGRESS.SDR L1GA200000552Release System · wornCOMPLY WITH SB DC9-53-257 TAIL CONE EMERGENCY RELEASE MOD ON LEGEND AIRLINES EO DC9-53-00-025 & 026-COMPLIED WITH AS REQUIRED-REF AD97-22-05SDR L1GA200000551Release System · wornCOMPLY WITH SB DC9-53-257 TAIL CONE EMERGENCY RELEASE MOD ON LEGEND AIRLINES EO DC9-53-00-025 & 026-COMPLIED WITH AS REQUIRED-REF AD97-22-05SDR AT0100027Spar · corrodedFOUND RIGHT HORIZONTAL STABILIZER FORWARD SPAR XFS 161-163 EXFOLIATED CORROSION. FABRICATED AND INSTALLED FILLER AND NUT PLATE STRIP IAW REO-L00320.SDR AT0100022Floor Panel · corrodedFOUND COCKPIT FLOORPANEL 4416 CORRODED BEYOND LIMITS. REPLACED SKIN ON FLOOR PANEL 4416 IAW DC9 SRM 53-01, 53-21, AND 51-10-03.SDR TWAA0018301Socket · crackedAIRCRAFT RETURNED FROM TAXI DUE TO ELECTRICAL SMELL IN AREA OF CABIN ROW 20 AND 21, LEFT SIDE. REPLACED BURNED LIGHT BULB SOCKET AT ROW 20ABC FOR LOWER SIDEWALL LIGHTS. CHECK-C 3-29-00 MCI.SDR ABXA000513Lock · jammedFLIGHT DECK DOOR LOCK JAMMED IN THE LOCKED AND CLOSED POSITION. MAINTENANCE INSPECTED TIGHTENED, AND LUBRICATED THE DOOR LOCK, IAW DC9 MM 52-00-00. OPS CHECKED GOOD.SDR ABXA000512Battery · dischargedEMERGENCY LIGHTS FAILED TO OPERATE DURING PREFLIGHT INSPECTION. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY IAW DC9 MM 33-53-00. OPS CHECKED GOOD.SDR MWEA001194Battery Pack · inoperativeAFTER ENGINE START FLIGHT ATTENDENT COMPLAINED OF STRONG ELECTRICAL SMOKE SMELL AROUND OVERWING EXITS. EMERGENCY AND FORWARD EXIT LIGHTS WOULD NOT STAY ON. FOUND BATTERY PACK HAD BURNT SMELL. REMOVED AND REPLACED EMERGENCY CEILING BATTERY PACK.SDR L1GA200000550Release System · wornCOMPLY WITH SB DC9-53-257 TAIL CONE EMERGENCY RELEASE MOD ON LEGEND AIRLINES EO DC9-53-00-025 & 026-COMPLIED WITH AS REQUIRED-REF AD97-22-05,SDR AT0100031Skin · chafedFOUND CHAFE MARKS OUT OF LIMITS IN VERTICAL STABILIZER LEADING EDGE. REPLACED LEADING EDGE OF VERTICAL STABILIZER IAW DC9 SRM 55-01 FIG 1.SDR MWEA001195Starter · inoperativeSTARTED RIGHT ENGINE ON DELAYED ENGINE START, N2 ACCELERATED TO 19 PERCENT THEN BEGAN TO DECREASE RAPIDLY AT WHICH TIME START WAS TERMINATED. REPLACED STARTER.
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