Douglas DC-9-41
Service difficulty reports · 2,671
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 = 'DC941' 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 = 'DC941' 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 GTIA010047Tail Cone · dislodgedMYR - FLT 303 - TAILCONE CAME OFF ON LANDING. TAILCONE RELEASE SYSTEM EVACUATED AND REPAIRED BY BOEING. REPLACED EXTERIOR CABLE FITTING AND RIGHT LOWER LOCKING PIN. TAILCONE WAS FIT FOR CLEARANCES AND DROP CHECK PERFORMED AS PER DC-9 MM 53-50-3. (M)SDR ABXA010063Battery Pack · dirtyEMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND CLEANED EMERGENCY LIGHT BATTERY PACK AT FSD AND RETURNED THE A/C TO SERVICE. UPON ARRIVAL AT ILN, MAINTENANCE REPLACED EMERGENCY LIGHT PACK AS A RELIABILITY PRECAUTION IAW DC9 MM 33-02-4.SDR GTIA010043Tail Cone · separatedDCA - FLT 72 - TAILCONE FELL OFF DURING LANDING. REMOVED AND REPLACED TAILCONE IAW MM 53-50-3, OPS CHECK NORMAL. (M)SDR ABXA010061Door Frame · crackedUPPER LEFT CORNER VENTRAL DOOR JAMB WAS CRACKED AND WAS PROPAGATING FROM STOP DRILL. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW ABX REA D953-39998-MR.SDR ABXA010060Fitting · crackedLOWER FRAME ATTACH FITTING AT FUSELAGE STATION 677R WAS CRACKED APPROX 3 INCHES. VERIFIED WITH DYE PEN AND EDDY CURRENT INSPECTION.SDR ABXA010059Fitting · crackedFLOORBEAM TO PYLON BULKHEAD ATTACH FITTING AT APPROX RBL 44.0 WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE ATTACH FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.SDR ABXA010058Rib · corrodedLEFT WING TRAILING EDGE RIB AT STATION 140 WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE RIB IAW ABX REA D957-40000.SDR ABXA010057Aileron · corrodedLEFT AILERON WAS CORRODED. MAINTENANCE INSPECTED AND REPLACED THE AILERON IAW DC-9 MAINTENANCE MANUAL.SDR ABXA010056Skin · crackedFUSELAGE SKIN LOCATED AT STA 61 LONGERON 19R WAS CRACKED. MAINTENANCE INSPECTED AND REPAIRED THE CRACK IAW DC-9 SRM 53-01 FIG 2.SDR ABXA010055Mount · corrodedRIGHT FLAP CARRIAGE MOUNT ANGLE WAS CORRODED. MAINTENANCE INSPECTED AND MANUFACTURED NEW FLAP MOUNT ANGLE PER DOUGLAS DRAWING 9923445 AND INSTALLED IAW DC-9 SRM 51-30-5.SDR ABXA010053Downlock Switch · defectiveA NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED WHEN LOWERING THE LANDING GEAR. THE CREW PERFORMED A MANUAL GEAR EXTENSION. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH IAW DC-9 MM 32-60-01. THE AIRCRAFT WAS INSPECTED FOR STRUCTURALSDR ABXA010054Control Unit · contaminatedTHE WHEEL BRAKES FAILED TO OPERATE ON LANDING AT JAN. WHEN ANTI-SKID WAS SELECTED OFF, BRAKES WORKED NORMALLY. MAINTENANCE INSPECTED AND REPLACED THE ANTI-SKID CONTROL UNIT DUE TO WATER INTRUSION IAW DC-9 MM. MAINTENANCE DEFERRED THE ANTI-SKID SYSTEM IAW DCSDR ABXA010050Battery · dischargedTHE COCKPIT EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-00. LATER ON 02/13/01 MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AS A RELIABILITY PRECAUTION IAW DC-9 MM 33-53-SDR ABXA010049Electrical Box · odorA HOT ELECTRICAL ODOR WAS NOTED COMING FROM THE FORWARD CENTER CONSOLE AREA. WHEN THE FORWARD CONSOLE CIRCUIT BREAKER WAS PULLED, THE ODOR SUBSIDED. MAINTENANCE INSPECTED THE PEDESTAL LIGHTS SWITCH BOX AND CONSOLE AREA WIRING. NO DEFECTS WERE NOTED. MAINTESDR ABXA010033Longeron · crackedLONGERON 30 AT FUSELAGE STATION 617 - 642 WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.SDR ABXA010032Longeron · corrodedLONGERON AT STRINGER 29L WAS EXFOLIATED ON THE HORIZONTAL FLANGE AT APPROX FUSELAGE STATION 675. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30.SDR ABXA010031Vane · corrodedFIXED VANE ON LEFT WING WAS CORRODED INTERNALLY. MAINTENANCE INSPECTED AND REPLACED THE LEFT FIXED VANE IAW DC-9 MM.SDR ABXA010030Longeron · crackedFUSELAGE LONGERON 28L WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON AT 28L IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA010029Latch · crackedREPAIR NEAR THE AFT BAG BIN AFT LATCH WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE BAG BIN DOOR IAW DC-9 SRM AND ABX NEA52300001-005.SDR ABXA010028Doubler · corrodedINTERNAL FUSELAGE DOUBLER AT STA 642 L30 WAS CORRODED FORWARD OF THE KIDNEY PANEL. MAINTENANCE INSPECTED AND REPLACED THE DOUBLER IAW DC-9 SRM 51-30-1 AND DRAWING 9923434.SDR ABXA010037Longeron · crackedLONGERON 26R WAS CRACKED FROM FUSELAGE STATION 617 TO 642. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-2.SDR ABXA010036Shear Tie · corrodedFUSELAGE SHEAR TIE AT FRAME 675 WAS CORRODED ON LEFT SIDE AT KEEL AREA. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM.SDR ABXA010035Frame · corrodedFUSELAGE FRAME AT STATION 560 LONGERON 29R WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW DC-9 SRM 53-03 PAGE 4E FIG 2A.SDR ABXA010034Longeron · corrodedCORROSION WAS FOUND ON LONGERON 29L, FUSELAGE STATION 617 - 642. MAINTENANCE REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.SDR ABXA0100037Longeron · crackedLONGERON 26R WAS CRACKED FROM FUSELAGE STATION 617 TO 642. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-2.SDR ABXA0100036Shear Tie · corrodedFUSELAGE SHEAR TIE AT FRAME 675 WAS CORRODED ON LEFT SIDE AT KEEL AREA. MAINTENANCE REPLACED THE SHEAR TIE IAW DC-9 SRM.SDR ABXA0100035Frame · corrodedFUSELAGE FRAME AT STATION 560 LONGERON 29R WAS CORRODED. MAINTENANCE INSPECTED AND REPAIRED THE FRAME IAW DC-9 SRM 53-03 PAGE 4E FIG 2A.SDR ABXA0100033Longeron · crackedLONGERON 30 AT FUSELAGE STATION 617 - 642 WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.SDR ABXA0100032Longeron · corrodedLONGERON AT STRINGER 29L WAS EXFOLIATED ON THE HORIZONTAL FLANGE AT APPROX FUSELAGE STATION 675. MAINTENANCE INSPECTED AND REPLACED THE LONGERON IAW DC-9 SRM 51-30.SDR ABXA0100031Vane · corrodedFIXED VANE ON LEFT WING WAS CORRODED INTERNALLY. MAINTENANCE INSPECTED AND REPLACED THE LEFT FIXED VANE IAW DC-9 MM.SDR ABXA0100030Longeron · crackedFUSELAGE LONGERON 28L WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE LONGERON AT 28L IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA0100029Latch · crackedREPAIR NEAR THE AFT BAG BIN AFT LATCH WAS CRACKED. MAINTENANCE INSPECTED AND REPLACED THE BAG BIN DOOR IAW DC-9 SRM AND ABX NEA52300001-005.SDR ABXA0100028Doubler · corrodedINTERNAL FUSELAGE DOUBLER AT STA 642 L30 WAS CORRODED FORWARD OF THE KIDNEY PANEL. MAINTENANCE INSPECTED AND REPLACED THE DOUBLER IAW DC-9 SRM 51-30-1 AND DRAWING 9923434.SDR ABXA0100034Longeron · corrodedCORROSION WAS FOUND ON LONGERON 29L, FUSELAGE STATION 617 - 642. MAINTENANCE REPLACED THE LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.SDR ABXA010039Latch · defectiveCOCKPIT DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT DOOR LATCH IAW DC-9 MM.SDR ABXA0100039Latch · defectiveCOCKPIT DOOR WOULD NOT OPEN FROM THE OUTSIDE. MAINTENANCE INSPECTED AND REPLACED THE COCKPIT DOOR LATCH IAW DC-9 MM.SDR ABXA010026Switch · failedDURING APPROACH WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE LANDING GEAR DOWN (GREEN) LIGHT FAILED TO ILLUMINATE. MISSED APPROACH, PROCEDURES WERE COMPLIED. THE CREW REPLACED THE NOSE LANDING GEAR DOWN INDICATOR LIGHT BULBS AND RECYCLED THE LANDING GEAR. SDR ABXA0100026Proximity Switch · failedDURING APPROACH WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE LANDING GEAR DOWN (GREEN) LIGHT FAILED TO ILLUMINATE. MISSED APPROACH PROCEDURES WERE COMPLIED WITH. THE CREW REPLACED THE NOSE LANDING GEAR DOWN INDICATOR LIGHT BULBS AND RECYCLED THE LANDING GEASDR ABXA010025Power Supply · dischargedEMERGENCY LIGHTS WOULD NOT ILLUMINATE ON PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY IAW DC-9 MM 33-53-02.SDR ABXA0100025Power Supply · dischargedEMERGENCY LIGHTS WOULD NOT ILLUMINATE ON PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY IAW DC-9 MM 33-53-02.SDR ABXA0100016Battery · dischargedEMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE EMERGENCY LIGHTS POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-02-4-0001.SDR ABXA0100021Skin · crackedFUSELAGE SKIN WAS CRACKED FORWARD OF STATION 1072, BELOW LONGERON 14R. MAINTENANCE INSPECTED AND REPAIRED THE CRACKED AREA IAW ABX REA D953-39613.SDR ABXA0100020Fitting · crackedINBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS FOUND CRACKED. MAINTENANCE INSPECTED AND REPLACED THE FITTING IAW DC-9 SRM 51-30-5.SDR ABXA0100019Fairing · delaminatedLEFT UPPER HORSECOLLAR WAS FOUND DELAMINATED. MAINTENANCE INSPECTED AND REPLACED THE HORSECOLLAR IAW DC-9 SRM 51-30-1.SDR ABXA0100018Fairing · corrodedRIGHT UPPER HORSECOLLAR HORIZONTAL FAIRING FOUND WORN AND CORRODED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT UPPER HORSECOLLAR FAIRING IAW DC-9 MM 55-10-00.SDR ABXA0100017Jackscrew · corrodedCORROSION WAS LOCATED ON THE STABILIZER JACKSCREW THREADS, RIGHT HAND SIDE. MAINTENANCE INSPECTED AND REPLACED THE JACKSCREW ASSY AND ACME NUT IAW DC-9 MM 27-40-01.SDR ABXA010134Jackscrew · corrodedTHE HORIZONTAL STABILIZER JACKSCREW THREADS WERE FOUND TO HAVE PITTING CORROSION. MAINTENANCE REPLACED THE JACKSCREW ASSY IAW DC-9 MM 27-40-01.SDR ABXA0100011Strap · crackedUPPER RIGHT PYLON TO FUSELAGE ATTACH ANGLE AT STATION 1095 WAS REPORTED TO BE CRACKED. MAINTENANCE REMOVED SPLICE STRAP AND DYE CHECKED THE AREA. NO CRACKS WERE NOTED IAW ABX GMM CHAPTER 3 SECTION 5.01.SDR ABXA0100010Doubler · crackedFORWARD UPPER ROTATING BEACON DOUBLER WAS CRACKED AT MOUNTING HOLE. MAINTENANCE REPLACED THE DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA0100009Frame · crackedLEFT FUSELAGE FRAME 677 WAS CRACKED AT LOWER END BELOW CUSP, IN THE RADIOUS. MAINTENANCE REPAIRED CRACKED FRAME IAW DC-9 SRM 53-03 FIG 16.
Back to Douglas DC-9-41