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 CA980608033Actuator · failed(CAN) UNABLE TO ARM GROUND SPOILERS ON APPROACH AND SPOILERS DID NOT DEPLOY MANUALLY ON LANDING. REPLACED SPOILER CONTROL ACTUATOR AND SPOILER CONTROL BOX. SPOILERS ADJUSTED AND CHECKED SERVICEABLE.SDR 9808029614Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR 9808019619Batteries · dischargedDURING PERIODIC CHECK, FOUND FORWARD FLIGHT ATTENDANT UPPER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL.SDR CA980608036Audio Panel · inoperative(CAN) LOSS OF VHF COMMUNICATION ON APPROACH TO AIRPORT, SOME TRANSMISSIONS TOO WEAK TO BE READ BY AIR TRAFFIC CONTROL CENTER. MAINTENANCE REPAIRED THREE BROKEN WIRES ON CAPTAIN'S AUDIO CONTROL PANEL CONNECTOR.SDR 9808139925Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9808129940Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND LEFT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9808059611Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR 9808039611Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR 9807939615Power Relay · failedCREW DETECTED ELECTRICAL BURNING SMELL IN COCKPIT DURING FINAL APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT AND POWER WAS SWITCHED TO EMERGENCY POWER ONLY. SMELL DISSIPATED. MAINTENANCE FOUND LOOSE HARDWARE AT TERMINAL STRIPS ON EITHER SIDE OF CROSSTIE RELAY SDR VJ9800176Battery Pack · dischargedEMERGENCY LIGHT OVER JUMPSEAT, L1 DOOR AND R1 DOOR INOP. REPLACED BATTERIES AND PACK, SYSTEM OPS CHECKS GOOD IAW MM 33-50-02.SDR TWAA9809303Fitting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT PYLON WITH CORROSION ON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 54-04, FIG 13, AND PLATED PER SRM 54-04, PAGE 53, ITSDR 9807989617Wire · brokenFLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 5 THRU 7 INOPERATIVE. REPAIRED BROKEN WIRES AT RIGHT FORWARD OVERWING EMERGENCY LIGHTS POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR 9807929983Circuit Breaker · damagedALL PHASES OF LEFT AC BUS CIRCUIT BREAKERS POPPED IN FLIGHT. FLIGHT WAS DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT AC C PHASE CIRCUIT BREAKER DAMAGED. REPLACED CIRCUIT BREAKER AND RESET ALL TRIPPED CIRCUIT BREAKERS ON AFT PANEL, OPESDR VJ9800318Skin · crackedMAIN CABIN SUPPORT STA 196 BL 0 - LBL 44 CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT, FABRICATED REPAIR SUPPORT FROM 2652479 EXTRUSION 42.50. LOCATED TRIM TO FIT, DRILLED, DEBURRED, TREATED, AND PRIMED IAW 51-30-2, 53-01-1 FIG 11, 51-10-2 AND SRM 51-10-4, SDR VJ9800235Strip · corrodedFWD PIT AFT RT FS 595 LWR FLOOR PANEL/GILLINER MOUNT STRIP CORRODED BETWEEN 28R AND 23R AND LWR LEG AT LONG 30. FWD PIT AFT RT FS 595 LWR FLOOR PANEL GILL MOUNT STRIP, MECH. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABBED 1EA ANGLE HEAT TREATED, DRILLEDSDR VJ9800162Skin · crackedDURING THE ACCOMPLISHMENT OF AD 88-24-08 INSP PER EO 12-5330-29-B1058 I/R, HFEC INDICATES EXTERNAL FUSELAGE SKIN CRACKED AT FS 617 RT LONG 1 SHEAR TIE. REMOVED 1 FASTENER IAW DC-9 SRM 51-30-2 HFEC VERIFIED CRACK IN SKIN AT COUNTERSINK IAW DC-9 STD PRACTICE PTSDR VJ9800146Battery Pack · dischargedSEVERAL EMERGENCY EXIT LIGHTS INOP IN FORWARD CABIN. REPLACED BATTERY PACK AND CHARGER.SDR MWEA98576Tip · erodedFOUND A HOLE ERODED IN THE LEFT HORIZONTAL STABILIZER LEADING EDGE TIP. MTC FABRICATED AND INSTALLED DOUBLER.SDR MWEA98575Skin · gougedFOUND A DEEP GOUGE IN RIGHT SIDE VERTICAL STABILIZER UPPER AFT CANOE SKIN. MTC FABRICATED AND INSTALLED SKIN.SDR 9807679951Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR VJ9800321Skin · crackedDURING ACCOMPLISHMENT OF AD 88-24-08 INSP PER EO 12-5330-29-B1058I/R, HFEC INDICATES EXTERNAL FUSELAGE SKIN CRACK .100 AT COUNTERSINK FASTENER HOLE COMMON TO FS 639 RT LONG 5 LOWER SHEAR TIE. REMOVED FASTENER, NDT VERIFIED CRACK AT COUNTERSINK. CUT OUT 2 .12SDR VJ9800161Skin · crackedDURING ACCOMPLISHMENT OF AD 88-24-08 INSPECTION PER EO-12-5330-29-B1058I/R, HFEC INDICATES EXTERNAL FUSELAGE SKIN CRACK .100 AT COUNTERSINK FASTENER HOLE CONDTO FS 639 RT LONGERON 5 LOWER SHEAR TIE. REMOVED 1 FASTENER, NDT VERIFIED CRACK IN SKIN AT COUNTERSINSDR VJ9800159Floorbeam · corrodedDURING C-CHECK, FOUND CORROSION ON STA 996 FLOORBEAM RT BL 44 UNDER NUT PLATE. REMOVED CORRODED SECTION OF THE BEAM, FABBED NEW SECTION FROM 60-15273 EXTRUSION 1 BY 40 BY 1 DRILLED DEBURRES, TREATED AND PRIMED IAW DC-9 SRM 51-10-4, 51-10-3 AND EO 98=863, INSSDR VJ9800145Frame · corrodedAFT FRAME CORRODED, LT SIDE 6 INCHES ABOVE FLOOR, AT FS 996. FABRICATED SPLICE, 15 BY 2 BY 1 INCHES IAW DC9 SRM 53-03, FIG 14 AND FRAME, 15 BY 2 BY 1 INCHES, IAW DAC DWG 5910163 AND RES 1 05439. INSTALLED REPAIR PARTS IAW DC9 SRM 51-30-5.SDR MWEA98241Fitting · corrodedTHE CUSP SPLICE FITTING AT FS 218 TO FS 237 WERE FOUND CORRODED. REMOVED AND REPLACED DAMAGED FITTING.SDR CA980608018Spacer · cracked(CAN) THE NR 2 ENGINE WAS REMOVED FROM THE AIRCRAFT DUE TO METAL CONTAMINATION IN THE OIL FILTER. ON DISASSEMBLY, THE SPACER BETWEEN THE THIRD AND FOURTH STAGE ON THE LOW PRESSURE COMPRESSOR WAS FOUND CRACKED IN SEVERAL PLACES. THE LARGEST CRACK EXTENDED RADSDR CA980512014Spacer · cracked(CAN) DURING DISASSEMBLY OF THE ENGINE TO INSPECT FOR METAL CONTAMINATION, THE FRONT COMPRESSOR ROTOR THIRD (TO FOURTH) STAGE SPACER WAS FOUND CRACKED. THE PART WAS REMOVED FROM SERVICE AND A FURTHER EVALUATION WILL BE DONE WITH ANOTHER SDR REPORT TO FOLLOW. SDR ABXA9800400Shear Tie · crackedDURING C-CHECK, FOUND SHEAR-TIE CRACKED BETWEEN LONGERONS 14R AND 16R AT FRAME 945. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2.SDR ABXA9800399Shear Tie · crackedDURING C-CHECK, FOUND SHEAR-TIE CRACKED BETWEEN LONGERONS 14L AND 16L AT FRAME 945. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2.SDR ABXA9800398Fitting · corrodedDURING C-CHECK, FOUND FRAME MOUNT FITTING AT STATION 313, RIGHT SIDE CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9800397Fitting · crackedDURING C-CHECK, FOUND AFT LOWER CARGO DOOR FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9800396Fitting · crackedDURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT DOOR INTERIOR FITTING P/N 3914025-2 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9800395Fitting · crackedDURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT DOOR INTERIOR FITTING P/N 3914025-502 CRACKED AT DOOR LEADING EDGE NEXT TO UPLATCH MECHANISM. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9800374Angle · crackedDURING C-CHECK, FOUND THE RIGHT PYLON INTERIOR ATTACH ANGLE CRACKED AT THE AFT ENGINE MOUNT UPPER SPAR LUG. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5.SDR VJ9800323Frame · crackedCANTED FRAME STA 1132 BETWEEN LONGERON 13R AND 14R CANTED FRAME WEB CRACK 2. REMOVED HAT STIFFENER, DOUBLER AND ANGLE TO GAIN ACCESS TO CORROSION BETWEEN OVERLAPING WEBS REMOVED CORRODED SECTION OF WEB IAW DC-9 SRM 53-10 FIG 1. FABBED DOUBLER REPAIR FROM 707SDR MWEA98561Apu · defectiveAFTER COMPLETING BEFORE START CHECKLIST EXTERNAL POWER WENT OFF LINE AND CABIN FILLED WITH SMOKE. MTC DEFERRED ENTIRE APU.SDR MWEA98560Fairing · chafedFOUND THE BLEND OUT OF CHAFING ON UPPER VERTICAL STABILIZER FAIRING OUT OF LIMITS. MTC REPAIRED WITH DOUBLER.SDR MWEA98559Skin · chafedFOUND VERTICAL STABILIZER CANOE SKIN ON RIGHT AFT SIDE CHAFED BEYOND LIMITS. MTC REPAIRED WITH DOUBLER.SDR 9807359918Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT TAIL CONE HANDLE INOPERATIVE. SOCKET WAS CORRODED THROUGH LEGS OF LAMP. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.SDR 9807349921Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERIES IN POWER SUPPLY AT FS 984, OPERATIONAL CHECK NORMAL.SDR MWEA98558Clip · crackedFOUND CRACKED BEAM END CLIP AT FS 69 IN UPPER LEFT HAND SIDE OF FORWARD ACCESSORY. MTC REMOVED AND REPLACED BEAM END CLIP.SDR MWEA98557Angle · crackedFOUND CRACKED AFT ACCESSORY COMPARTMENT CANTED FRAME 1168 RIGHT SIDE LOWER SUPPORT ANGLE. MTC REMOVED AND REPLACED ANGLE.SDR VJ9800164Skin · corrodedIN AFT CARGO COMPARTMENT, FOUND CORROSION OF SKIN ADJACENT TO STR 28 L I/B SIDE AT STA 944. MECH REMOVED CORROSION, FOUND AREA TO BE OUT OF LIMITS MORE THAN 50 PERCENT MATERIAL LOSS IAW DC-9 53-01 FIG. FABBED DOUBLER, DRILLED AND COUNTERSUNK, DEBURRED HOLES,SDR 9807329983Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 12 THRU 14 INOPERATIVE. REPLACED BATTERY PACK AND BATTERIES, OPERATIONAL CHECK NORMAL.SDR VJ9800169Doubler · corrodedLEFT WING LOWER MLG DOUBLER HAS SEVERAL BLEND OUTS BEYOND LIMITS. REMOVED LEFT 1WR MLG DOUBLER IAW DC-9 SRM 51-30-5. RECEIVED NEW DOUBLER, DRILLED, COUNTERSUNK, AND DEBURRED NEW MLG DOUBLER IAW DC-9 SRM 51-10-3, INSTALLED AND SEALED NEW MLS DOUBLER IAW DC-9SDR VJ9800168Stringer · corrodedFWD CARGO PIT AT STA 380 28L IS CORRODED BETWEEN STA 370-389. REMOVED CORROSION IAW DC-9 51-10-3, FOUND TO BE BEYOND LIMITS MATERIAL LOSS 75 PERCENT. REMOVED LONGERON 28L FROM STA 345-398. DRILLED AND DEBURRED NEW LONGERON 28L. TREATED, PRIMED AND INSTALLESDR VJ9800167Skin · corrodedMATERIAL THICKNESS OF FUSELAGE SKIN AT ADF ANTENNA IS BEYOND LIMITS SRM 51-01 LIMITS AFTER CORROSION REMOVAL. REMOVED OVERHEAD CEILING PANELS, A/C DUCTS FOR ACCESS TO THE ANTENNA AREA. REPAIRED CORRODED SKIN AREA UNDER AFT ADF LOOP ANTENNA IAW DC-9 53-04 FIGSDR VJ9800163Support · corrodedCABIN STA 218 FLOOR SUPPORT HAS CORROSION AT FASTENER HOLE. REMOVED CORROSION IAW DC-9 SRM 51-10-3, MATERIAL LOSS 50 PERCENT OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1 GAUGE NR 4782-01. FABBED REPAIR FLOOR SUPPORT OUT OF 7075 T6 511 ANGLE 18 X 2 IAW DC-9 SRM 51-1SDR VJ9800144Doubler · corrodedLT WING LOWER MAIN LANDING GEAR DOUBLER HAS SEVERAL BLEND OUTS BEYOND LIMIT. REMOVED, REPLACED, DRILLED, COUNTER SUNK AND DEBURRED NEW DOUBLER. TREATED AND PRIMED IAW DC9 SRM 51-30-5.SDR VJ9800143Skin · corrodedFUSELAGE SKIN AT ADF ANTENNA CORRODED BEYOND LIMIT AFTER REMOVAL OF CORROSION IAW SRM 51-01. REMOVED OVERHEAD CEILING PANELS AND AIR CONDITIONING DUCTS FOR ACCESS. REPAIRED FUSELAGE SKIN IAW DC9 SRM 53-04, FIG 29, REINSTALLED DUCTS AND PANELS IAW DC9 MM 25-2
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