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 ABXA9600127Seal · bentDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR AFT METAL SEAL BENT AT THE BOTTOM OF DOOR. REPAIRED SEAL IAW DC-9 SRM 51-01.SDR MWEA95302Epr Wire · brokenCREW REPORTS AT START OF TAKEOFF ROLL, LEFT ENGINE EPR GAUGE FLUCTUATES ABOVE 1.8 EPR. AIRCRAFT RETURNED TO GATE. MAINTENANCE LEAK CHECKED PT2 AND PT7 LINES AND NO LEAK FOUND. WIRE 'D' FROM EPR TRANSMITTER WAS FOUND BROKEN JUST ABOVE RUDDER PEDALS. REPAIRESDR MWEA95301Evac Slide · fell offCREW REPORTS UPON ARRIVAL TO THE A/C IN THE MORNING, THEY FOUND THE FORWARD GALLEY SERVICE DOOR EVACUATION SLIDE HAD FALLEN OFF DOOR. MAINTENANCE REINSTALLED GALLEY DOOR EVACUATION SLIDE. RETURNED A/C TO SERVICE.SDR ABXA9600170Skin · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING LEADING EDGE SKIN SPLICE BETWEEN NR 3 AND NR 4 SLAT TRACKS CRACKED. REPLACED LEFT WING LEADING EDGE SKIN SPLICE IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9600141Floorbeam · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FLOORBEAM AT FS 160 HEAVILY CORRODED AT RBL 44 AND HAD A RIVET HOLE ELONGATED AT BL 22R. REPAIRED FLOORBEAM IAW ABX REA D953-12722-MR.SDR MWEA95300Angle · crackedDURING C-CHECK, FOUND RIGHT SIDE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED BETWEEN AND EXTENDING BEYOND TWO FASTENERS NEAR AFT SPAR OF VERTICAL STABILIZER.SDR MWEA95299Eel Sockets · dirtyDURING C-CHECK, FOUND EMERGENCY EXIT LIGHTS ABOVE AFT FLIGHT ATTENDANTS SEAT VERY DIM. MAINTENANCE CLEANED LIGHT SOCKETS AND LENS, OPS CHECK GOOD. RETURNED A/C TO SERVICE.SDR MWEA 95298Angle · crackedDURING C-CHECK, FOUND AFT ENTRANCE DOOR HAD 3 CRACKS INTERNALLY. THE FITTING ON RIGHT END FRAME APPROX 1 INCH LENGTH, THE RIGHT CENTER STOP AREA LOWER HORIZONTAL ATTACH ANGLE APPROX .75 INCH LENGTH, AND THE RIGHT HAND PAN STA Z35.0, .25 INCH AT ONE FASTENER. SDR CAL950833Angle · crackedHOU - INSPECTION FOUND A 3 INCH CRACK IN LEFT WHEEL WELL ATTACH ANGLE. A NEW ANGLE WAS INSTALLED IAW SRM 51-30. (M)SDR 9514189922Latches · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DROP THE TAILCONE. ALSO, FOUND THAT THE TAILCONE HUNG UP ON THE LOWER LATCHES. ADJUSTED THE TAILCONE RELEASE SYSTEM AND CHECKED OK.SDR CAL950843Bracket · crackedHOU - INSPECTION FOUND A .75 INCH CRACK IN NR 4 LEFT FLAP HINGE OUTBOARD BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5. (M)SDR CAL950839Cusp · corrodedHOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 165 JUST FORWARD OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE 55. (M)SDR CAL950838Cusp · corrodedHOU - INSPECTION FOUND CORROSION ON RIGHT CUSP AT STATION 200 JUST AFT OF DOOR JAMB. THE CUSP WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER SRM 53-05, FIGURE 55. (M)SDR CAL950834Bracket · crackedHOU - INSPECTION FOUND A .5 INCH CRACK IN THE RIGHT FLAP NR 4 FLAP HINGE INBOARD AND OUTBOARD BRACKETS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-5. (M)SDR ABXA9600174Press Panel · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT SLANT PRESSURE PANEL AT FS 699. REPLACED THE LEFT SLANT PRESSURE PANEL IAW DC-9 SRM 51-30-1.SDR ABXA9500687Switch · defectiveLEFT GEAR UNSAFE LIGHT INOP DURING RETRACTION AND EXTENTION. TESTED OK, RECYCLED GEAR AND PROBLEM REMAINED. REPLACED DOWNLOCK SWITCH ON LEFT GEAR. POSITION AND WARNING SYSTEM OPS CHECKED GOOD IAW DC-9 MM 32-60-00. PIN RETENTION POOR ON PINS 5 AND 7 OF PLUGSDR 95ZZZX5387Door · not latchedATL/DTW FLT 444 - ELECTRICAL COMPARTMENT DOOR CAME OPEN IN-FLIGHT, RETURNED TO GATE. SECURED E & E DOOR, OPS CHECKED ANNUNCIATOR LIGHT, OPS CHECKED OK.SDR 9515509609Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FUSELAGE SKIN FS 997 AT LONGERON 23R. REPAIRED SKIN (P/N 5911428-42), PER EA 99-97722.SDR MWEA95285Slide Cover · fell offCREW REPORTS, GALLEY DOOR EVACUATION SLIDE COVER FELL OFF. MAINTENANCE RESECURED GALLEY DOOR EVACUATION SLIDE COVER AND RETURNED A/C TO SERVICE.SDR CAL950832Jamb · corrodedHOU - INSPECTION FOUND CORROSION ON FORWARD BAGGAGE BIN DOOR JAMB. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 44, PAGE 105. (M)SDR ABXA9600171Blkhd Panel · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT SLANT PRESSURE PANEL CORRODED AT FS 699. REPLACED THE RIGHT SLANT PRESSURE PANEL IAW DC-9 SRM 51-30-1.SDR ABXA9500861Retainer · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03 AND SB 56-11 REV 3, FOUND EVIDENCE OF CRACKS ON TWO FASTENER HOLES ON THE LEFT EYEBROW WINDOW RETAINER, DURING X-RAY INSPECTION. REPLACED RETAINER IAW DC-9 SRM 51-30-2.SDR 95ZZZX5385Oil Temp Ind · malfunctionedATL/FLL - FLT 515 - FLIGHT MADE AN AIR RETURN TO ATL DUE TO NR 1 ENGINE HIGH OIL TEMP AT 150 DEGREES. ENGINE SHUT DOWN IN-FLIGHT AND CAPTAIN DECLARED EMERGENCY. RAN ENGINE AT POWER, OPS CHECK GOOD AFTER CHECKING ALL WIRING AND CONNECTORS. CHANGED OIL AND FISDR 95ZZZX5386Controller · malfunctionedJAN/ATL - FLT 494 - AUTOPILOT HEADING SELECT SWITCH SHORTED OUT WITH SMOKE IN-FLIGHT. REPLACED AUTOPILOT CONTROLLER, OPS CHECKED NORMAL PER MM 22-10.SDR 9513739603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FRAME TO FLOORBEAM LOWER ATTACH FITTING, FS 851. REPLACED FITTING PER SRM 51-10-3.SDR 9513729604Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FITTING LOCATED AT FS 700 IN THE RIGHT MAIN LANDING GEAR WHEEL WELL. REPLACED FITTING PER SRM 51-10-03.SDR CAL950783Fuel Coupling · leakingIAH - FLT 1230 - THE LEFT MAIN FUEL QUANTITY BEGAN TO DECREASE AS FUEL WAS TRANSFERRED FROM CENTER TANK AFTER TAKEOFF FROM IAH. THE LEFT FUEL QUANTITY STEADILY AND RAPIDLY DECREASED. THE CROSS-FEED WAS OPENED IN AN ATTEMPT TO BURN RT MAIN FUEL, BUT THE LT FUSDR 9513719604Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION TO THE LEFT MAIN LANDING GEAR RETRACT SUPPORT FITTING. REPLACED FITTING PER CITEXT 90-3211-1-9902.SDR ABXA9600179Web · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT CUSP WEB CRACKED AT FS 658. REPLACED RIGHT CUSP WEB IAW DC-9 SRM 51-30-2 AND ABX EA NR FS-53-3689.SDR 95ZZZM601Doublers · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, EVIDENCE OF CORROSION WAS FOUND ON THE TCAS ANTENNA AFT SIDE. REMOVED MOUNTING PLATE AND FINGER DOUBLERS. FABRICATED A NEW PLATE AND FINGER DOUBLERS AND INSTALLED ALL PARTS IAW DC9 SRM 53-04 FIGSDR 95ZZZM537Longeron · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND CORROSION ON LONGERON 23L FS 965 WHICH IS BEYOND THE SRM LIMITS 53-01. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR MEMBER AND SPLICES IAW DC9-SRM 53-02 FIG 5. (M)SDR 9513949922Frame · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 541 FLOOR SUPPORT FRAME BETWEEN LONGERON 29L TO 29R. REPAIRED FRAME PER EA 99-97124.SDR 9513939922Skin · cannedDURING H-CHECK, FOUND OIL CANNING IN THE FUSELAGE SKIN FS 1076 TO 1087 BETWEEN LONGERONS 17L TO 18L. REPAIRED SKIN (P/N 5912870-501), PER EA 99-94921.SDR ABXA9500873Skin · wornDURING C-CHECK INSPECTION, FOUND LEFT FLAP TOP SIDE SKIN HAD A WORN SPOT AFT OF THE INBOARD END OF THE NR 3 FIXED VANE. REPAIRED IAW ABX REA D957-12653-MR.SDR 95ZZZM600Frame · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, CORROSION WAS FUOND IN THE FORWARD PIT CRACKS, AT FS 218, ON THE LOWER FRAME. REMOVED DAMAGED SECTION. FABRICATED REPAIR MEMBER AND INSTALLED IAW DC-9 SRM 51-10-3, 51-10-1 AND 51-10-2A. (M)SDR 9513929922Fitting · crackedDURING H-CHECK, FOUND CRACKS IN THE WING TO FUSELAGE ATTACH FITTING, RIGHT AND LEFT SIDES FS 604. REPAIRED FITTINGS (P/N 5910465-33, -34), PER EA 99-97123.SDR ABXA9500874Fitting · corrodedDURING C-CHECK INSPECTION, FOUND FITTING ON LEFT FUSELAGE SKIN THAT TIES INTO THE MAIN FRAME AND INTO LEFT TRAPEZOID PANEL HAD CORROSION IN THE BOLT HOLE. REPAIRED IAW ABX REA D953-12649-MR.SDR 95ZZZM538Frame · corrodedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FLORIDA, FOUND SEVERAL CORRODED SPOTS AROUND THE AFT CARGO DOOR LOWER FRAME. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED A NEW SECTION AND SPLICES IAW DC-9 SRM 53-30-2. NR 027N1-0064.SDR ABXA9500870Fairing · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT UPPER HORIZONTAL TO VERTICAL STABILIZER FAIRING CRACKED AT FORWARD END. REPAIRED FAIRING IAW DC-9 SRM 55-03 FIG 17.SDR ABXA9500864Blkhd Web · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 84-07-04 AND 90-18-03, AND SB 53-174 REV 3, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT FOUR HOLES AT THE TEE SPLICE PLATE ABOVE FRP, RIGHT SIDE. REPAIRED IAW DC-9 SB 53-174.SDR 9514579922Blkhd Web · cannedDURING H-CHECK, FOUND OIL CANNING IN THE PYLON BULKHEAD WEB, LEFT SIDE. REPAIRED PER EA 99-100864.SDR ABXA9600169Tie Strap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND MAIN CABIN INTERCOSTAL TIE STRAP AT FS 465 AND LONGERON 6R CORRODED AND BLENDED. REPLACED TIE STRAP IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500863Blkhd Web · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 81-26-03, 90-18-03 AND SB 53-147 REV 7, ASB 53-147 REV 4, FOUND CRACKS ON THE AFT PRESSURE BULKHEAD WEB AT SPLICE ABOVE LONGERON 13R AND 11R. REPAIRED IAW ABX REA D953-12628-SB.SDR 95ZZZX5201B-Nut · looseIAH - FLT 309 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 2123, DUE TO DECREASING OIL QUANTITY. FOUND OIL LINE B-NUT LOOSE ABOVE OIL FILTER. TORQUED B-NUT, SERVICED ENGINE OIL. ENGINE LEAK CHECKED AND OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 36,069 HOUSDR CAL950804Longeron · corrodedHOU - INSPECTION FOUND CORROSION ON LONGERON 26L BETWEEN STATION 945-960. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE INSTALLED IAW SRM 51-30-2. (M)SDR CAL950803Longeron · corrodedHOU - INSPECTION FOUND CORROSION ON LONGERONS 26L TO 28L IN AFT BAGGAGE BIN BETWEEN STATION 937-945. THE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3 AND RIVETS WERE REPLACED IAW SRM 51-30-2. (M)SDR CAL950761Anti-Retract Lvr · out of rigFLT NR 9873 - STA 31J - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM 31J (AERO CORP). THERE WAS NO GROUND SHIFT TO AIRBORNE. THE AIRCRAFT WAS RETURNED TO 31J WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RE-RIGGED THE GROUND SENSE AND ANTI-RETRACTISDR 9513409951Rmi Compass · malfunctionedLOSS OF NR 2 COMPASS INDICATOR OCCURRED DURING INITIAL SPOOL UP ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED NR 2 RMI. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE.SDR ABXA9500871Tab · dentedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND SEVERAL SMALL DENTS AND SCRATCHES ON LEFT SIDE OF RUDDER TAB. REPLACED RUDDER TAB IAW DC-9 MM 27-20-2.SDR ABXA9500862Retainer · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 90-18-03, SB 56-11 REV 3, FOUND CRACKS ON THE EYEBROW WINDOW RETAINER AT FASTENER HOLE ON THE RIGHT SIDE OF AIRCRAFT. REPLACED RETAINER IAW DC-9 SRM 51-30-2 AND 51-30-1.
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