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 VJ9800583Structure · corrodedRT KEEL AREA AT FS 680 TO 756 CORRODED. Z ANGLE, L29R, LONGERON AND FITTING CORRODED BEYOND LIMIT. INSTALLED NEW PARTS IAW DC9 SRM 51-30-3, 51-10-4, 51-30-1, 51-30-2, 51-30-5 AND 53-01 FIG 1.SDR VJ9800582Skin · crackedDENT 1.5 INCHES BY .038 D/X=35 OUT LIMIT IAW DC9 SRM 53-04 FIG 38, SHEET 10, CONDITION 1B3. CUT OUT DENT, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04, FIG 38, 51-10-4, 51-30-2 AND AIRTRAN RES 981774. REINSTALLED ALL COMPONENTS REMOVED FOR ACCESSDR VJ9800581Skin · dentedDENT 1.5 INCHES BY .037 D/X=41 AT FS 410.5, L28-29R, AND FS 412.5, L28-29R, OF 1 INCH BY .018 D/X=56 OUT OF LIMIT IAW SRM 53-04, FIG 10. CUT OUT DENT, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC9 SRM 51-10-4, 53-01 FIG 4, 51-10-3, 51-30-2 AND -5 PLUSSDR VJ9800564Skin · creasedCREASE AT FS 522, L28R, APPROXIMATELY 3 BY 5 TIMES .070 INCHES OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. CUT OUT AREA, REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR AND FINGER DOUBLER IAW DC9 SRM 51-10-2, 53-04, FIG 12, 51-30-2, 51-30-5. 51-10-4 AND AIRTRAN SDR VJ9800563Skin · corrodedAFT CARGO SKIN AT FS 937, L28R, CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED NEW DOUBLER IAW DC9 SRM 53-01 FIG 4, 51-30-2 AND AIRTRAN RES 981737.SDR VJ9800541Floorbeam · corrodedFLOOR SUPPORT STRUCTURE LEFT OF CENTER LINE CORRODED BEYOND LIMIT IAW DC9 SRM 53-01 FIG 1 AT FS 965, LBL 30. CUT OUT CORRODED SECTION OF FLOORBEAM, FABRICATED AND INSTALLED NEW SECTION IAW DC9 SRM 53-05 FIG 20A.SDR VJ9800540Skin · corrodedA DENT, 11 INCHES BY 2.625 TIMES .084 WITH A DEPTH OF .098, FOUND AT FS 351 TO 362 L19 AND 20R. REMOVED AND FORMED NEW SKIN AND SPLICE. DRILLED, COUNTERSUNK, TREATED AND PRIMED. INSTALLED NEW SKIN AND SPLICE IAW DC9 SRM 51-30, 51-10-4, 51-10-3, RES 191745 ASDR VJ9800539Skin · dentedA DENT, 2 INCHES BY .016 AT FS 436, L27 AND 28R OUT OF LIMIT IAW DC9 SRM 53-04 FIG 38. CUT OUT DENTED AREA, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-01 FIG 4, 51-10-3, 51-30-2 AND RES 191736.SDR VJ9800530Skin · dentedCREASED OUT OF LIMITS DENT WAS FOUND AT FS 447 L26 & 27 L 1 1.5 X .068 IAW DC-9 SRM 53-04 FIG 38. FABRICATED AND INSTALLED REPAIR IAW SRM 53-04 FIG 38, 51-10-3 AND DAC NTSPM PART 8.SDR VJ9800529Angle · corrodedFLOOR SUPPORT STRUCTURE AT FS 996 APPROX 31 LT OF THE CENTER LINE WAS FOUND WITH CORROSION AROUND FASTENER HOLE. REMOVED THE UPPER L FLOORBEAM ANGLE IAW DC-9 SRM 53-01 FIG 1, 51-10-3, 51-30-2, 51-10-1.SDR VJ9800520Skin · dentedDENT .O45 INCHES IN DEPTH AT FS 206.25, L21 AND 22R, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. COLD WORKED AREA, FABRICATED, INSTALLED REPAIR IAW DC9 SRM 53-04, FIG 38 VIEW P, 51-10-3 AND MM 21-00.SDR VJ9800477Cover · looseGALLEY SLIDE COVER LOOSE. RESECURED IAW MM 25-61 AND PERFORMED REQUIRED INSPECTION.SDR VJ9800476Control Box · malfunctionedNO BRAKE PRESSURE INDICATION WHEN ANTI-SKID SELECTED ON, TAKING AIRCRAFT RUNWAY POSITION. MAINTENANCE INSPECTED ANTI-SKID AND BRAKE SYSTEM AND TROUBLE SHOT PROBLEM TO ANTI-SKID CONTROL BOX. .SDR VJ9800447Slide · dislodgedFWD ENTRY EMERGENCY DOOR SLIDE DISLODGED FROM CASING WHEN DOOR OPENED. SECURED SLIDE IAW MM 25-00.SDR VJ9800446Battery · dischargedEMERGENCY LIGHT AT MAIN CABIN PASSENGER DOOR INOP. REPLACED BATTERIES, OPS CHECKED NORMAL.SDR VJ9800580Angle · crackedAFT ENTRANCE DOOR LT SIDE WALL SUPPORT ANGLE CRACKED AND CORRODED. FABRICATED AND INSTALLED NEW ANGLE IAW DC9 SRM 51-30-2, 51-30-4, 52-11-0, FIG 2, 51-20-2A AND AIRTRAN RES 981705.SDR VJ9800562Longeron · corrodedLT WHEEL WELL IN KEEL BEAM AREA AT FS 718-737 CORRODED BEYOND LIMIT IAW DC9 SRM 53-01 FIG 1. REMOVED AND REPLACED LONGERON IAW DC9 SRM 51-30-2, 51-30-5, 51-30-1 AND 51-30-3. KEEL BEAM DETERMINED TO BE WITHIN LIMIT IAW AIRTRAN RES 981746.SDR VJ9800533Actuator · corrodedRT MLG RETRACT ACTUATOR AND CORRODED AND SUPPORT BUSHING TRUNNION IS WORN AND CORRODED. REMOVED AND REPLACED RT MLG RETRACT ACTUATOR AND BUSHINGS TRUNNION IAW DC9 32-32-2 AND 57-40-2.SDR VJ9800528Skin · corrodedLEFT HAND AFT GALLEY PAN WAS FOUND WITH CORROSION ON THE I/B EDGE. REMOVED CORRODED SKIN. FABRICATED AND INSTALLED NEW SKIN IAW DC-9 SRM 51-30-2, 51-10-4, 51-10-3 AND RES 981704.SDR VJ9800527Support · corrodedAFT CARGO COMPARTMENT FLOOR TRACK WAS FOUND WITH CORROSION ON THE INNER AND OUTER SURFACES AT FS 756 TO 851 LT. FABRICATED AND INSTALLED NEW REPAIR MEMBER IAW SRM 51-10-3 AND 53-21-0 FIG 10.SDR VJ9800526Floor · corrodedFS 218 TO 332 THE LT FWD FLOOR PANEL AND TIE DOWN TRACK WAS FOUND WITH CORROSION. REMOVED FLOOR PANEL AND TIE DOWN TRACK IAW DC-9 SRM 53-21-0 FIG 8, 51-10-3 AND RES 981748.SDR VJ9800525Floor · corrodedFWD CARGO FLOOR PANEL AT FS 218 TO 351 WAS FOUND WITH CORROSION AROUND EDGES. REMOVED PANEL, FABRICATED AND INSTALLED NEW PANEL IAW DC-9 SRM 51-10-3, 53-21-0 AND 53-01 PG 6.SDR VJ9800514Skin · chafedVERTICAL SKIN ON LT AND RT UPPER AND LOWER BANANA FAIRING CHAFED. RT UPPER BANANA FAIRING SKIN CHAFED OUT OF LIMIT IAW DC9 SRM 55-01. REMOVED SKIN, FABRICATED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2 AND 55-01.SDR VJ9800434Power Supply · inoperativeIN EMERGENCY POSITION, LH NACELLE LIGHT WON'T WORK. REPLACED BATTERY POWER SUPPLY IAW MM 33-50.SDR MWEA98980Battery Pack · dischargedTHE LEFT ENGINE NACELLE LIGHT WILL NOT TEST WITH EMERGENCY LIGHTING. MTC REMOVED AND REPLACED BATTERY PACK.SDR CA981019025Combustion Case · cracked(CAN) DURING ENGINE DISASSEMBLY THE COMBUSTION OUTER CASE WAS FOUND CRACKED IN THE REAR FLANGE AT THREE DIFFERENT LOCATIONS. THE CRACKS WERE FROM THE HOLES AT THE INNER DIAMETER AND CONTINUED TOWARDS THE OUTER CASE WALL. THE COMBUSTION OUTER CASE WAS REPLACESDR 9810159619Control Cable · brokenAFTER TAKEOFF, THE FLIGHT CREW NOTICED A LOUD BANG AND STRONG FLUTTER FROM THE NOSE LANDING GEAR DOOR AREA. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR STOP CABLE AND NOSE LANDING GEAR DOOR. OPERATIONAL CHESDR VJ9800445Skin · gougedGOUGE IN FUSELAGE SKIN AT FS 967, L21-22R, BEYOND LIMIT IAW DC9 SRM 53-04, FIG 8. BLENDED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC9 SRM 51-10-3, 53-31-0 FIG 8 AND 53-04 FIG 38.SDR VJ9800433Actuator · failedNOSE GEAR WOULD NOT RETRACT. FERRIED AIRCRAFT FROM IAD TO MAIN MAINTENANCE BASE IN ATL FOR CONVENIENCE. REPLACED NLG ACTUATING CYLINDER IAW MM 32-32-6, PG 204 - 206. LEAK AND OPS CHECKED GOOD.SDR 9810729609Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT AND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.SDR 9810149606Roller · out of adjustAFTER LANDING GEAR EXTENSION, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RECYCLED THE LANDING GEAR SYSTEM, AND LANDED AT DTW WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT LANDING GEAR DOOR LOCK ROLLER ASSDR VJ9800420Battery · dischargedAFT STAIRS EMERGENCY LIGHTING BATTERIES WON'T HOLD A CHARGE. REPLACED NICAD BATTERIES IAW MM 33-50, OPS CHECKED GOOD.SDR VJ9800419Battery Pack · dischargedAFT STAIRS EMERGENCY LIGHT INOP. REPLACED BATTERY POWER SUPPLY IAW MM 3350, OPS CHECKED GOOD.SDR TWAA9815502Engine · failedTHE LT ENG FILTER CLOG LIGHT ILLUMINATED AND EGT INCREASED. RETARDED THROTTLE AND DIVERTED TO BNA. FOUND METAL IN MAIN OIL SCREEN. ENGINE WAS CHANGED. CHECK-C 11-15-97 MCI. *S/D* ANALYSIS OF MATERIAL IN OIL SCREEN FOUND EVIDENCE OF M-50 BEARING MATERIAL.SDR CALA9801962Battery · dischargedLEFT EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS TURNED ON. REMOVED AND REPLACED AFT BATTERY PACK IN AFT BAG BIN OVERHEAD PER MM 33-53-0.SDR CA981019028Controller · failed(CAN) AIRCRAFT RETURNED TO AIRPORT WITH RIGHT PACK OVERHEAT AND SMOKE AND BURNING SMELL. RIGHT PACK TEMP CONTROL VALVE WENT TO FULL HOT, WHEN COLD SELECTED VALVE RESPONDED CORRECTLY. TEMPERATURE CONTROLLER REPLACED.SDR VJ9800482Spar · magnetizedREPAIR ON AFT SIDE REAR SPAR LWR CAP XRS 525 DETERMINED TO BE MAGNETIC WITHIN 5 FEET FLUX VALVE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-10-4 AND AIRTRAN RES 981625.SDR VJ9800418Hub Cap · wornSMOKE ODOR IN CABIN. AIRCRAFT RETURNED TO MCO. FOUND EVIDENCE OF NR 4 TIRE SPINNING IN WHEEL WELL. REPLACED RUBBER HUB CAP.SDR 9810499942Frame · crackedDURING M-CHECK, FOUND CRACK ON FRAME WEB AT FS 1038, INBOARD OF LONGERON 14R, EMITTING FROM UNDER STIFFENER. REPAIRED PER EA 99-162759.SDR VJ9800518Support · corrodedFLOOR SUPPORT AT FS 160, RBL 0-45, CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-30-2, 51-10-4, 51-10-2.SDR VJ9800417Control Box · failedNO BRAKE PRESSURE DURING TAXI WITH ANTISKID SYSTEM ON. REPLACED ANTISKID CONTROL BOX AND OPS CHECKED GOOD IAW MM 32-43.SDR MWEA98971Cover · detachedFORWARD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE COVER.SDR MWEA98970Light · inoperativeFORWARD ENTRANCE PORTABLE EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FOWARD ENTRY EMERGENCY FLASHLIGHT.SDR CALA9801853Vane · gougedINSPECTION FOUND RT WING UPPER MOVEABLE VANE LEADING EDGE GOUGED. A REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 1, 51-10-4, 51-10-3, 51-30-2, AND 51-10-2.SDR CA981019029Controller · failed(CAN) ON DEPARTURE AT 2,500 FEET, THE RIGHT AIR CONDITION PACK OVERHEATED THEN FORWARD FIRE DETECTORS ANNUNCIATED, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, DECLARED EMERGENCY AND RETURNED TO BLOCKS . REPLACED AUTOMATIC CABIN TEMPERATURE CONTROLLER.SDR VJ9800412Slide · looseFWD ENTRY DOOR EVAC SLIDE LOOSE FROM CASE. RESECURED SLIDE PACK LATCH AND COVER PER MM 25-51.SDR VJ9800411R1Uplock Latch · inoperativeGEAR DOOR OPEN LIGHT ON WITH LANDING GEAR INDICATING DOWN AND LOCKED. REMOVED AND REPLACED THE LT MLG UPLOCK LATCH ASSY IAW D MM 32-31-4.SDR VJ9800411Indication · malfunctionedGEAR DOOR OPEN LIGHT ON WITH LANDING GEAR INDICATING DOWN AND LOCKED.SDR VJ9800513Tab · corrodedRT ELEVATOR GEAR TAB HAS 1 INCH DIAMETER CORROSION SPOT. CUT OUT CORROSION, CLEANED AREA, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-70-2.SDR VJ9800416Slide · contaminatedTAIL CONE EVAC SLIDE ASSY SATURATED WITH FOREIGN MATERIALS. REMOVED AND REPLACED TAIL CONE SLIDE ASSY.
Back to Douglas DC-9-32