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 ABXA040147Doubler · corrodedANTENNA SUPPORT CORRODED BETWEEN STA. 522 - 503, LONGERON 30 - 29 LT. REPLACED DOUBLERS AROUND THE ANTENNA IAW DC-9 SRM 51-30-2.SDR ABXA040146Doubler · corrodedANTENNA SUPPORT CORRODED BETWEEN STA. 465 - 446 LONGERON 30 - 29 LT. REPLACED DOUBLER 5911412-53 AND 5911412-55 AIW DC-9 SRM 51-30-2 AQND 51-30-5.SDR 0400509620Bulkhead · crackedDURING "H" CHECK FOUND CRACKS IN BULKHEAD WEB AT BS 756. REPAIRED PER EA 96-198613.SDR 0400409617Longeron · crackedDURING H-CHECK FOUND CRACK IN LONGERON AT FORWARD BULKHEAD BS 756. REPAIRED PER EA 96-197855.SDR MWEA040024Engine · vibrationLEFT ENGINE VIBRATION. COMPLIED WITH VIBRATON TEST, INLET HAS A VIBRATION OF 1.0 MILS, TEST 1 VIBRATION CHECKED OK FOR SERVICE.SDR ABXA040085Pump · inoperativeLEFT ENGINE HYDRAULIC PUMP FAILED IN FLIGHT INTO BTV. REPLACED LEFT ENGINE HYDRAULIC PUMP ON LEFT ENGINE IAW DC-9 AMM 29-10-05-2-0001. OPS AND LEAK CHECKED GOOD. ALSO INSPECTED FLUID IN PUMP, ALL CLEAN, '0' CONTAMINANTS. REPLACED LEFT ENGINE CASE DRAIN FILSDR MWEA040018Smoke Detector · false indicationLEFT LAVATORY SMOKE DETECTOR WENT OFF. INSPECTED LAVATORY COMPARTMENT, LIGHTING SOCKETS, LAVATORY TIMER, WATER HEATER, TRASH COMPARTMENT AND CYCLED LAVATORY MOTOR. REMOVED AND REPLACED SMOKE DETECTOR.SDR ABXA040061Connector · damagedABORTED APPROACH AND CYCLED THE GEAR ON A GO-AROUND. WHEN GEAR WAS EXTENDED, RIGHT MAIN GEAR UNSAFE LIGHT DID NOT COME ON. RIGHT LANDING GEAR GREEN LIGHT DID NOT COME ON. PROX INDICATION WAS NORMAL. PROBLEM VERIFIED. FOUND NR 5 PIN ON RIGHT MAIN LANDING GSDR MWEA040015Indicator · inoperativeFORWARD ENTRANCE DOOR SLIDE PRESSURE GAUGE IS INOPERATIVE. REMOVED AND REPLACED FORWARD EVACUATION SLIDE.SDR ABXA040060Attach Angle · corrodedAFT SIDE OF UPPER HORIZONTAL ATTACH ANGLE AT FS 996 EXFOLIATED AT LEFT BUTT LINE 6, RIGHT BUTT LINE 6, AND RIGHT BUTT LINE 10. REPAIRED ATTACH ANGLE IAW DC-9 SSRM, WITHIN LIMITS IAW DC-9 SRM 53-01.SDR ABXA040037Inverter · defectiveDURING PRE-FLIGHT, TURNED EMERGENCY POWER SWITCH ON AND AC EMERGENCY BUS OFF LIGHT CAME ON. REMOVED AND REPLACED EMERGENCY AC POWER INVERTER IAW DC-9 MM. OPS CHECKED GOOD.SDR 0400269605Skin · crackedDURING (L) CHECK FOUND CRACK IN SKIN AS BS 996 BETWEEN L7L AND L8L. REPAIRED IAW EA 96-197817.SDR ABXA040033Warning Light · illuminatedDURING PREFLIGHT, EMERGENCY POWER CHECK, A/C EMERGENCY BUSS POWER OFF LIGHT ILLUMINATED. RESET EMERGENCY BUS BREAKER B1-185 IAW DC-9 WD MANUAL 24-23-00. SYSTEM OPS CHECKED GOOD.SDR ABXA040003Odor · detectedAPPROXIMATELY 5 MINUTES AFTER TAKEOFF, NOTICED PRESSURIZATION BUMPS ON CLIMBOUT FOLLOWED BY LIGHT SMOKE AND ODOR IN COCKPIT. RETURNED TO ILN. INSPECTED AFT ACCESSORY COMPARTMENT DUCT WORK AND FLUID LINES. FOUND NO VISIBLE DAMAGE OR FLUID LEAKS AND FOUND NO SDR 0400259918Skin · crackedDURING L-CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 76.55 RBL 16. REPAIRED PER EA 99-197447.SDR 0400069950Slat · malfunctionedDURING APPROACH INTO DCA, AIRCRAFT EXPERIENCED AN UNCOMMANDED LEFT ROLL WHEN SLATS WERE EXTENDED. THE SLAT DISAGREE LIGHT ILLUMINATED AND SLAT EXTEND DID NOT. COMPLIED WITH COM PROCEDURE AND SLATS WERE RETRACTED. A LONGER RUNWAY WAS NEEDED WITH SLATS RETRACSDR 0302229921Frame · crackedDURING (L) CHECK FOUND CRACK IN FUSELAGE FRAME AT BS 76 LBL 17. REPAIRED IAW EA 99-197446.SDR MWEA030500Bulkhead · crackedLOWER LT VENTRAL DOOR CORNER WEB IS CRACKED. INSTALLED DOUBLERS TO BOTH LOWER DOOR CORNERS OF THE AFT PRESSURE BULKHEAD.SDR ABXA040018Frame · corrodedFUSELAGE FRAME HAD LEVEL 2 CORROSION AT LONGERON 30, STA 813. REPAIRED AREA IAW DC-9 SRM 53-03.SDR ABXA040021Angle · crackedSUBFLOOR AND ANGLE CRACKED AT BUTTLINE 0, STA 160. REPAIRED SUBFLOOR IAW DC-9 SRM 53-01.SDR ABXA040017Beam · crackedFORWARD RIGHT SERVICE DOOR HAD A CRACK ON UPPER HORIZONTAL BEAM FORWARD END. REPAIRED UPPER BEAM OF SERVICE DOOR IAW DC-9 SRM 52-05.SDR ABXA040020Shear Tie · crackedSHEAR TIE CRACKED AT FS 947 BETWEEN LONGERON 15 AND 16 RT. REMOVED AND REPLACED SHEARTIE IAW DC-9 SRM.SDR ABXA040019Shear Tie · crackedSHEARTIE CRACKED AT FS 947, BETWEEN LONGERON 15 LT AND 16 LT. REMOVED AND REPLACED SHEAR TIE IAW SRM.SDR ABXA040015Shear Tie · crackedSHEAR TIE FS 622 WAS CRACKED, LONGERON 25 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.SDR ABXA040016Keelbeam · crackedKEELBEAM LONGERON 30 END CAP WAS CRACKED, LT SIDE FS 604. REPLACED KEELBEAM END CAP IAW DC-9 SRM.SDR MWEA030494Downlock Switch · inoperativeRT MLG GREEN LIGHT STAYED ON. REPLACED RT MLG DOWNLOCK SWITCH.SDR ABXA030483Skin · crackedCRACK IN FUSELAGE SKIN AT STA 996 ABOVE LONGERON 16 LEFT. REPAIRED CRACK IAW DC-9 SRM 53-04.SDR ABXA030482Fitting · corrodedSTA 604, LONGERON 28 LEFT END FITTING CORRODED. REPLACED END FITTING 28 LEFT, STA 604 IAW DC-9 SRM 51-10-4 AND 51-30-5.SDR ABXA030481Tee Fitting · crackedAFT PRESSURE BULKHEAD TEE NR 6 FORWARD SIDE HAD A 1.125 INCH CRACK AT APPROXIMATELY LONGERON 14 LEFT. REPLACED AFT PRESSURE BULKHEAD TEE NR 6 IAW JOB CARD EA 53120037 AND DC-9 MM.SDR ABXA030479Pan · crackedFORWARD LOWER CARGO DOOR CRACKED AT PAN EDGE UNDER AFT DOOR LATCH. REPLACED DOOR ON NON ROUTINE 0155 AND DC-9 SRM.SDR ABXA030480Intercostal · crackedINTERCOSTAL FS 756, LEFT BUTTLINE 22 WAS CRACKED. REPLACED INTERCOSTAL WEB IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.SDR MWEA030474Slat Track · brokenSLATS WERE RETRACTED, THE AMBER SLAT DISAGREEMENT LIGHT STAYED ON. FOUND SLAT TRACK DOOR AT NUMBER TWO AND NUMBER THREE SLAT JUNCTION BENT AND BROKEN. REMOVED AND REPLACED SLAT TRACK DOOR.SDR ABXA030446Wire · burnedWIRE BURNED ON PHASE C, GROUND SERVICE BUS POWER PANEL, WIRE HV X22810C. REMOVED BURNED AREA OF WIRE AND REPLACED WIRE END CONNECTOR. INSTALLED WIRE TO GROUND SERVICE BUS PHASE C IAW DC9 MM 20-50-01-2-0001. OPS CHECK GOOD.SDR ABXA030436Controller · malfunctionedAFTER TAKEOFF 3000 FT, BOTH AUTO TEMP CONTROLLERS WERE SELECTED FULL HOT. ABOUT 14000 FT, AIRFLOW STOPPED & CABIN CLIMBED UNCONTROLLABLY AT 1400 FT FPM. LEFT PRESSURE GAUGE INDICATED '0' PSI, RIGHT GAUGE INDICATED '30' PSI, LEFT AND RIGHT DUCTS TEMPS PEGGED HOSDR ABXA030448Web · crackedCUSP WEB HAD 5 EACH CRACKS BETWEEN FS 945 AND 965. REMOVED AND REPLACED SECTION OF CUSP WEB IAW DC-9 SRM 51-30-2, 51-30-1 AND 50-01.SDR ABXA030447Structure · corrodedLEFT ELEVATOR OUTBOARD OF GEARED TAB HAD LEVEL II CORROSION WITH DISHED RIVETS AND BULGING SKIN. REPLACED LEFT ELEVATOR ON NON ROUTINE 0518, IAW DC-9 MM.SDR MWEA030437Light · looseEMERGENCY EXIT LIGHT FOR SERVICE DOOR AFT SIDE HAS COME LOOSE FROM TOP SIDE. REMOVED AND REPLACED EEPLS EXIT LIGHT FOR SERVICE DOOR.SDR 0301979940Controller · malfunctionedDURING CLIMBOUT, A BURNING ODOR AND LIGHT HAZE PERMEATED THE CABIN. THE LT PACK VALVE WAS PEGGED FULL RT AND THE LT DUCT TEMPERATURE REACHED 120 DEGREES. FLIGHT CREW SWITCHED THE LT PACK TO MANUAL CONTROL AND ODOR DISSIPATED. FLIGHT RETURNED TO CMH AND ON DESCSDR MWEA030435Wire · brokenEMERGENCY LIGHTS NOT WORKING. FOUND BROKEN WIRE AND REPAIRED.SDR 0301959987Engine · making metalDURING CRUISE FLIGHT, NR 2 ENGINE OIL QUANTITY WENT TO ZERO, OIL TEMP CLIMBED INTO THE RED ZONE. THE NR 2 ENGINE WAS SHUT DOWN. FLIGHT CREW DIVERTED AIRCRAFT TO MBS AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND METAL IN THE OIL FILTER AND ON THE CHIP SDR MWEA030431Skin · damagedRIGHT ELEVATOR HAS DAMAGE AT INBOARD TRAILING EDGE 1INCH X .5000 HOLE IN TOP SKIN. EXTERNAL SKIN REPAIR.SDR MWEA030430Skin · lightning strikeEXTERNAL FUSELAGE SKIN HAS SEVERAL LIGHTING STRIKES AT FRAME STATION 256 LONGERON 29 LEFT. CUT OUT DAMAGE AND INSTALLED FLUSH REPAIR.SDR MWEA030429Skin · damagedRIGHT ELEVATOR HAS DAMAGE TO OUTBOARD TRAILING EDGE 1INCH X .5 INCH. INSTALLED EXTERNAL DOUBLER.SDR MWEA030428Frame · crackedCRACK AT FUSELAGE FRAME STATION 718 LEFT OUTBOARD FORWARD FLANGE HAS GROWN FROM 6 INCHES TO 7.6250. -- INSTALLED DOUBLER.SDR ABXA030414Frame · crackedFRAME CRACKED AT FS 1076 AND LONGERON 19 LEFT. REPAIRED FRAME AT FS 1076 IAW DC-9 SRM 53-03.SDR ABXA030413Angle · crackedCRACK IN FRAME ATTACH ANGLE AT STA 1038 ABOVE LONGERON 18 LT. REPAIRED ANGLE IAW DC-9 SSRM DWG K05159.SDR ABXA030408Rib · crackedLEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB TOWARD THE TOP END OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.SDR ABXA030409Rib · crackedLEFT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.SDR ABXA030412Rib · crackedEND OF LEADING EDGE RIB RIGHT WING CRACKED AT STA 353. REPAIRED DAMAGED RIB IAW DC-9 SRM 57-06.SDR ABXA030411Rib · crackedRIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON RIB IN THE MIDDLE OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.
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