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 ABXA9801168Longeron · crackedDURING C-CHECK, FOUND LONGERON 30 CRACKED AT SPLICE BETWEEN STATION 794 TO 813. REPAIRED LONGERON IAW DC9 SRM 53-02.SDR ABXA9801167Longeron · crackedDURING C-CHECK, FOUND LONGERON 25L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC9 SRM 53-02.SDR ABXA9801166Longeron · crackedDURING C-CHECK, FOUND LONGERON 24L CRACKED AT STATION 200. REPAIRED IAW DC9 SRM 53-02.SDR ABXA9801165Longeron · crackedDURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 945. REPAIRED LONGERON IAW DC9 SRM 53-02.SDR ABXA9801164Longeron · crackedDURING C-CHECK, FOUND LONGERON 12R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM DWG K05864.SDR ABXA9801163Longeron · crackedDURING C-CHECK, FOUND LONGERON 2R CRACKED AT STATION 1076. REPAIRED LONGERON 2R IAW DC9 SRM 53-02.SDR ABXA9801148Bulkhead Web · corrodedDURING C-CHECK, FOUND LEFT PYLON BULKHEAD FORWARD LOWER SIDE CORRODED. REPLACED WEB ON PYLON BULKHEAD IAW DC9 SRM 51-30-2, 51-30-5, AND 51-30-1.SDR ABXA9801147Fitting · crackedDURING C-CHECK, FOUND CENTER WING FORWARD SPAR ATTACH FITTING AT STATION 600 AND LONGERON 24R CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9801146Angle · crackedDURING C-CHECK, FOUND VERTICAL STABILIZER ATTACH ANGLE RIGHT SIDE CRACKED AT LOWER AFT CORNER. REPAIRED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA9801145Blkhd Fitting · crackedDURING C-CHECK, FOUND RIGHT PYLON BULKHEAD AT STATION 965 INBOARD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.SDR ABXA9801144Fitting · crackedDURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE INTERNAL ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-2.SDR ABXA9801143Skin · crackedDURING C-CHECK, FOUND INTERNAL FUSELAGE SKIN AT STATION 1080 CRACKED BETWEEN LONGERON 1R AND 2R. REPAIRED IAW DC9 SRM 53-04.SDR ABXA9801142Skin · crackedDURING C-CHECK, FOUND SKIN CRACKED AT STATION 194, LONGERON 22L. REPAIRED SKIN IAW ABX EA 53300001-003.SDR ABX9801162Longeron · crackedDURING C-CHECK, FOUND LONGERON 2L CRACKED AT STATION 1076. REPAIRED LONGERON IAW DC9 SRM 53-02.SDR VJ9800629Fire Loop · malfunctionedFIRE DETECTION LOOP LIGHT ILLUMINATED WITH FIRE HANDLE LIGHT FLICKERING ON NR 1 ENGINE. PERFORMED LOOP TEST PER AOM AND FLIGHT CREW ELECTED TO SECURE NR 1 ENGINE. DECLARED EMERGENCY LANDING BUT LANDING WAS NORMAL AND NO EVACUATION WAS PERFORMED. REPLACED FISDR VJ9800622Retract Mech · malfunctionedNLG WOULD NOT RETRACT AFTER TAKEOFF. ALL GEAR INDICATIONS NORMAL WITH GEAR IN DOWN POSITION. CREW ELECTED TO RETURN TO DEPARTING STATION. INSPECTED GEAR FOR BROKEN, MISSING PARTS, AND LEAKS; NONE FOUND. PINNED GEAR AND FERRIED AIRCRAFT TO ATL MAINTENANCE BSDR VJ9800634Skin · crackedDURING SCHEDULED INSPECTION, THE FUSELAGE AT FS 965 L16R TO L17R WAS FOUND CRACKED. CUT OUT CRACK, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 51-10-3, 51-20-1, 51-10-4, 53-04 FIGURE 17 AND AIRTRAN RES 981976.SDR ABXA9801090Web · crackedDURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED UNDER FLOOR TRACK AT RBL 54, STATION 658. REPAIRED IAW DC9 SRM 53-01.SDR ABXA9801089Angle · crackedDURING C-CHECK, FOUND VERTICAL ANGLE/BRACKET CRACKED ON OUTBOARD SIDE OF NR 2 PYLON, UNDER THROTTLE CONDUIT JAM NUT. REPLACED BRACKET/ANGLE IAW DC9 SRM.SDR ABXA9801088Floorbeam · crackedDURING C-CHECK, FOUND FLOORBEAM AT STATION 680 AND LBL 54 CRACKED. REPLACED FLOORBEAM IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5.SDR ABXA9801087Support · crackedDURING C-CHECK, FOUND FLOORBEAM SUPPORT CRACKED STATION 680 AND RBL 44. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-1 AND 51-30-2.SDR ABXA9801086Bulkhead Fitting · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED JUST ABOVE DOOR WARNING SWITCH. REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ABXA9801085Floorbeam · corrodedDURING C-CHECK, FOUND FLOORBEAM AT STATION 965 CORRODED FROM LBL 22 TO LBL 44. REPAIRED FLOORBEAM IAW ABX REA D953-25565MR.SDR 9811429916Bulkhead Angle · crackedDURING M CHECK, FOUND T ANGLE CRACKED ON BULKHEAD FS 47 NEAR CENTER LINE. REPAIRED PER EA 99-159528.SDR 9811419926Spar Cap · crackedDURING M CHECK, FOUND CRACK ON RIGHT HORIZONTAL STABILIZER XRS 223 UPPER AFT SPAR OUTBOARD END. REPAIRED PER EA 99-159470.SDR VJ9800628Panel · leakingLT WING FUEL ACCESS PANEL LEAKING. FLIGHT CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE. INSPECTED AIRCRAFT AND FOUND NO RESIDUAL FLUID BUT INSTALLED DOME NUT ON FUEL INSPECTION PLATE IAW MM 28-00. LEAK CHECKED GOOD.SDR VJ9800621O-Riing · failedAFTER TAKEOFF FLIGHT CREW PERCEIVED THE ODOR OF FUMES IN COCKPIT AND ELECTED TO RETURN TO ATL MAINTENANCE BASE. INVESTIGATED BY MAINTENANCE AND FOUND FUEL SHROUD GOING TO APU TO NOT BE PROPERLY SEATED. REPLACED O-RING AND SEAL TO INSURE INTEGRITY OF FUEL LINSDR MWEA981090Structure · bird strikeON CLIMBOUT, AIRCRAFT TOOK MULTIPLE BIRD STRIKES AND RETURNED TO MKE. MKE MTC COMPLETED A BIRD STRIKE INSPECTION AND NO DAMAGE WAS FOUND. REMOVED TWO STRIKE MARKS.SDR VJ9800613Power Supply · inopEMERGENCY LIGHT AT AFT AIR STAIR ENTRY OUT. REPLACED POWER SUPPLY AND BATTERIES, OPS CHECKED GOOD IAW MM 33-00.SDR MWEA981089Longeron · crackedFOUND LONGERON 13L AT STATION 965 CRACKED. MTC SPLICED IN NEW SECTION OF LONGERON.SDR MWEA981088Longeron · crackedFOUND CRACKS ON LONGERON 16L AND 17L AT STATION 965. MTC SPLICED IN NEW SECTION OF LONGERON.SDR VJ9800630Panel · corrodedDURING SCHEDULED INSPECTION AT AERO CORP, FOUND THE R-1 FORWARD AND AFT GIRT BAR ATTACH FITTING IN THE FLOOR SPINNING. MECHANICALLY REMOVED THE CORROSION, TREATED AND PRIMED AREA. FABRICATED AND INSTALLED NEW TRANSITION PANEL IAW DC9 SRM 51-30-2, 51-10-5, 51-SDR VJ9800647Seat Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, THE SEAT TRACK AT FS 398 TO 740 RBL 44 WAS FOUND WITH CORROSION IN NUMEROUS PLACES. REMOVED AND REPLACED THE SEAT TRACK IAW DC9 SRM 53-05 FIG 4F.SDR VJ9800633Skin · dentedDURING A SCHEDULED INSPECTION, THE FUSELAGE SKIN AT FS 229 TO 399 L18R TO 26R WAS REMOVED AND REPLACED DUE TO NUMEROUS DENTS OUT OF LIMITS AND TWO LARGE EXISTING REPAIRS.SDR VJ9800594Valve · failedDURING INITIAL TAKEOFF ROLL AT APPROXIMATELY 40 KNOTS, FLIGHT CREW RECEIVED A MASTER CAUTION WARNING. FLIGHT CREW APPLIED BRAKES WITH ANTISKID SYSTEM ON AND THERE WAS NO BRAKE PRESSURE. TURNED ANTISKID SYSTEM OFF AND BRAKE PRESSURE WAS AVAILABLE. AIRCRAFT SSDR VJ9800636Seat Tracks · corrodedSCHEDULED INSPECTION, SEAT TRACKS WERE FOUND WITH CORROSION AND OUT OF LIMITS IN THE FOLLOWING LOCATIONS: LBL 22 BS 275 TO 589, LBL 44 BS 275 TO 589, RBL 22 BS 398 TO 550 AND FS 936 TO 996. REMOVED AND REPLACED SEAT TRACKS IAW DC9 SRM 53-05 FIG 4F, 51-10-3 ASDR 9810369985Lamp · failedFLIGHT CREW NOTED THE RIGHT LANDING GEAR INDICATION (GREEN) DID NOT ILLUMINATE UPON LANDING GEAR EXTENSION. LANDING GEAR WAS RECYCLED WITH SIMILAR RESULTS. INDICATOR LAMP WAS REPLACED BY FLIGHT CREW. INDICATION CHECKED NORMAL AND AIRCRAFT LANDED AT DESTINATSDR VJ9800646Bulkhead Angle · corrodedSCHEDULED INSPECTION, THE ANGLE ON THE PRESSURE BULKHEAD WAS FOUND CORRODED AT L30 FS966. GAINED ACCESS TO AREA, REMOVED AND REPLACED ANGLE. REINSTALLED ALL PARTS REMOVED FOR ACCESS IAW DC9 SRM 51-10-4, 51-30-2, 51-30-1, 51-10-3, AND SB53-147 PG 44.SDR VJ9800588Battery Pack · dischargedEMERGENCY EXIT LIGHTS IN BUSINESS CLASS FAILED TO DISARM. REPLACED NICAD BATTERY, OPS CHECKED GOOD.SDR MWEA981051Slide · fell offTHE GALLEY DOOR SLIDE FELL OFF DOOR. MTC REINSTALLED SLIDE.SDR VJ9800645Skin · corrodedSCHEDULED INSPECTION, THE RIGHT WING UPPER SURFACE FIXED PANEL, FWD OF THE AILERON FROM XRS 445 TO XRS 400 APPROXIMATELY WAS FOUND WITH SURFACE CORROSION ON THE UNDERSIDE IN SEVERAL PLACES. CUT OUT CORROSION AND DELAMINATION IN THE SPECIFIED AREA. FABRICATEDSDR VJ9800639Skin · crackedDURING A SCHEDULED INSPECTION, THE COCKPIT FLOOR PANEL UNDER THE CO-PILOTS SEAT WAS FOUND CRACKED AND CORRODED AROUND THE SCREW HOLES. REMOVED THE UPPER SKIN, FABRICATED AND INSTALLED A NEW SKIN IAW DC9 SRM 51-30-2 AND 53-21-0 FIG 2D.SDR VJ9800587Fuel Pump · failedAFTER TAKEOFF AT 500 FEET ALTITUDE, NR 2 ENGINE FAILED, NO VIBRATION OR BANG EXPERIENCED. FOUND NR 2 ENGINE FUEL PUMP DRIVE SHAFT SHEARED. REPLACED FUEL PUMP IAW DC9 MM 73-10-1 AND FUEL CONTROL REPLACED IAW DC9 MM 73-20-1 AS PRECAUTIONARY MEASURE. OPS CHECKSDR CA981130013Actuator · failed(CAN) UNABLE TO ARM SPOILERS ON APPROACH, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT. REPLACED AUTO SPOILER ACTUATOR.SDR VJ9800584Cover · dislodgedFWD MAIN PASSENGER DOOR SLIDE COVER DISLODGED. REINSTALLED IAW MM 25-62-0 AND PERFORMED REQUIRED INSPECTION.SDR VJ9800638Seat Track · corrodedDURING A SCHEDULE INSPECTION, THE RT O/B SEAT TRACK RBL 44 FS 200 WAS FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF TRACK, FABRICATED AND INSTALLED REPAIR MEMBER IAW DC9 SRM 53-05 FIG 4F AND 51-10-3.SDR VJ9800579Cover · dislodgedFWD PASSENGER DOOR ESCAPE SLIDE COVER DISLODGED WHEN DOOR OPENED. REINSTALLED AND PERFORMED REQUIRED INSPECTION.SDR CA981230053Spacer · fractured(CAN) NR 2 ENGINE HAD HIGH VIBRATION AFTER TAKEOFF. ENGINE WAS SHUT DOWN AT 16,000 FEET. POST-FLIGHT INSPECTION FOUND THE SPACER BETWEEN THE 3-4 STAGE OF THE TURBINE WITH A 4 PIECE MISSING. THE DAMAGE INITIATED FROM A CRACK IN THE TIE ROD BOLT HOLE INNER THSDR VJ9800611Skin · dentedDENT AT FS 123L, L23-24. .035 X 1 DX=29, 124L, L23-24, .010 X .25 DX=25, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38, CONDITION 1B-3. NO FURTHER ACTION REQUIRED PER AIRTRAN RES 981872.SDR VJ9800610Skin · dentedDENT AT FS 211L, L15, .055 X 3 DX=55, 212L, L15-16, .052 X 3 DX=58, 213L, L15-16, .016 X 1/4 DX=16, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38, SHEET 38. COLD WORKED DENTS. VERIFIED NO CRACKS BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3,
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