Douglas DC-9-31
Service difficulty reports · 7,433
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 = 'DC931' 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 = 'DC931' 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 USAA950244Eel Battery Pack · dischargedPIT - FLT 0541 - THE COCKPIT EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONS CHECKED GOOD. (W)SDR ABXA9500257Retainer · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND THE RIGHT COCKPIT OVERHEAD WINDOW RETAINER CRACKED. REPAIRED IAW DC-9 SRM 56-01, FIG. 3.SDR ABXA9500255Retainer · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING A.D. 90-18-03; S.B. 56-11, REV. 3, FOUND THE LEFT COCKPIT OVERHEAD WINDOW RETAINER CRACKED. REPAIRED IAW DC-9 SRM 56-01, FIG. 3.SDR 9504619956Hinge · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN RIGHT WING NR 2 FLAP HINGE FORWARD UPPER BORES. REPLACED FITTING PER CITEXT 09-5740-1-9800.SDR 9504529960Hinge · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN RIGHT NR 3 FLAP HINGE FORWARD SIDE FASTENER HOLES. REPLACED HINGE PER CITEXT 09-5740-9-9800.SDR 9504519996Angle · crackedDURING PERIODIC CHECK, FOUND CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE FS 1096 RIGHT SIDE. REPAIRED PER EA 99-097062, FIG.1.SDR USAA950310Skin · corrodedPIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION UNDER FWD BELLY AT MARKER BEACON ANTENNA. INSTALLED DOUBLER REPAIR PER USAIR EA 29959. (W)SDR EISA95054Eel Powre Supply · inopFORWARD EMERGENCY LIGHT POWER SUPPLY INOP. REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT POWER SUPPLY. (Z)SDR ABXA9500261Skin · dentedDURING C-CHECK INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN AT STATION 209 ABOVE LONGERON 18R. REPAIRED IAW ABX REA D953-11134-MR.SDR ABXA9500260Skin · dentedDURING C-CHECK INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN AT STA. 209 BELOW LONGERON 18R. REPAIRED IAW ABX REA D953-11134-MR.SDR ABXA9500256Support · damagedDURING C-CHECK INSPECTION, FOUND THE FLOOR PANEL SUPPORT TO HAVE A HOLE WITH SHORT EDGE DISTANCE, A DOUBLE DRILLED HOLE AND TWO HOLES WITH SHORT EDGE DISTANCE BETWEEN THEM, STA. 160 THROUGH 200, RBL 44. REPAIRED IAW ABX REA D953-11137-MR.SDR 9504119908Fitting · crackedDURING LINE CHECK FOUND 3 INCH CRACK IN LONGERON 20L END FITTING AT FS 585. REPLACED FITTING PER SRM 51-30-2.SDR ABXA9500263Cap · corrodedDURING C-CHECK INSPECTION, A PREVIOUS REPAIR TO THE LEFT VERTICAL STABILIZER WAS FOUND WITH LEVEL I CORROSION. REMOVAL OF THE REPAIR REVEALED THE REAR SPAR CAP HAD BEEN SPLICED. REPAIRED IAW ABX REA D955-1116-MR.SDR ABXA9500254Web · crackedDURING C-CHECK INSPECTION, FOUND A CUSP WEB AT STATION 960, LBL 48 CRACKED. REPAIRED IAW DC-9 SRM 51-30-2.SDR ABXA9500253Web · crackedDURING C-CHECK INSPECTION, FOUND A CUSP WEB AT STATION 960, RBL 48 CRACKED. REPAIRED IAW DC-9 SRM 51-30-2.SDR ABXA9500251Splice · crackedDURING C-CHECK INSPECTION, LONGERON 30 SPLICE WAS FOUND CRACKED AT STA. 955. REPLACED SPLICE IAW DC-9 SRM 53-02-147.SDR 96ZZZM790Longeron · crackedDURING OP-15, FOUND LONGERON 30 CRACKED APPROXIMATELY 10 INCHES FROM STATION 794, AFT TO SPLICE. REPLACED LONGERON 30 FROM STATION 756 TO 813 PER SRM 51-30 AND TWA STANDARD PRACTICES.SDR 95ZZZX1768Frame · crackONE INCH LONG CRACK ON CANT FRAME FS 074, LONGERON 4L. REPAIRED FRAME PER SRM 53-01, FIGURE 2. AIRCRAFT TT, 54,495 HRS.SDR 95ZZZX1767Doubler · crackFS 990, BETWEEN LONGERONS 15R-16R, INNER SKIN DOUBLER HAS A 1 INCH LONG CRACK INSIDE RT LAV. REPAIRED INNER DOUBLER PER SRM 53-04, FIGURE 41. AIRCRAFT TT, 54,495 HRS.SDR 95ZZZX1766Angle · corrosionHEAVY CORROSION ON ANGLE FRAME TEE CAP, FS 110 BETWEEN LONGERONS 26R-27R. REPAIRED ANGLE PER DALFORT AVIATON XEA NR X9-53-74. AIRCRAFT TT, 54,495 HRS.SDR 95ZZZX1765Skin · crackFUSELAGE SKIN HAS A 5 EACH 1 INCH CRACK ON CANT FRAME, STA 1132 AT LONGERON 20R. REPAIRED SKIN PER SRM 53-01, FIGURE 2. AIRCRAFT TT, 4,495 HRS.SDR 95ZZZX1764Shear Tie · crackSHEAR TIE HAS CORROSION AND .5 INCH CRACK, FS 1089 BETWEEN LONGERONS 16L-17L. REPLACED SHEAR TIE PER SRM 53-30-5. AIRCRAFT TT, 54,495 HRS.SDR 95ZZZX1763Fitting · corrosionMODERATE CORROSION DAMAGE AT LONGERON 36 END FITTING, FS 760. REPLACED FITTING PER SRM 53-02, FIGURE 12. AIRCRAFT TT, 54,495 HRS.SDR 9504099936Skin · crackedDURING LINE CHECK, FOUND CRACKS AND LOOSE RIVETS IN THE LEFT SIDE RUDDER SKIN. REPLACED RUDDER PER CITEXT 90-2720-1-9801.SDR 9504029996Release Mech · out of adjustDURING PERIODIC CHECK FOUND THAT INADEQUATE FORCE WAS REQUIRED TO RELEASE THE HANDLE FROM THE CLIPS AND DROP THE TAILCONE. ADJUSTED THE LATCHES AND THE CLIPS. CHECKED OK.SDR 9503979996Fitting · corrodedDURING PERIODIC CHECK FOUND CORROSION IN LONGERON 30 END FITTING AT FS 598. REPLACED PER SRM 51-30-0.SDR 9503969996Fitting · corrodedDURING PERIODIC CHECK FOUND CORROSION IN LONGERON 29R END FITTING AT FS 604. REPLACED PER SRM 51-30-3.SDR 9503959996Fitting · crackedDURING PERIODIC CHECK FOUND CRACK IN LONGERON 27L END FITTING AT FS 579. REPLACED PER SRM 51-30-0.SDR ABXA9500250Fitting · crackedDURING C-CHECK INSPECTION, A VERTICAL CABIN FLOOR SUPPORT FITTING WAS FOUND CRACKED AT STA. 965, LBL 34. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.SDR 9504249902Mosture Trap · contaminatedCLIMBING OUT OF MEM, THE CREW NOTED SMALL FLUCTUATIONS IN NR 2 ENGINE INDICATOR. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. UPON INSPECTION, WATER WAS FOUND IN THE FCU MOISTURE TRAP. THE TRAP AND DRAIN HOLE WERE CLEANED. ENGINE RUNUP WAS PERFORMSDR 9503939996Fitting · corrodedDURING PERIODIC CHECK FOUND CORROSION IN THE RIGHT SIDE KEEL FITTING AT FS 756. REPLACED FITTING PER 51-30-0 AND SB 53-75.SDR USAA950239Eel Lights · malfunctionCLT - FLT 0845 - THE FLOOR TRACK LIGHTING MALFUNCTION AT DEPARTURE TIME. (W)SDR USAA950238Actuator · inoperativePIT - FLT 0757 - FLIGHT DIVERTED TO PIT DUE TO A PRESSURIZATION PROBLEM. MAINTENANCE REPLACED THE OUTFLOW DOOR AFT MOTOR AND GEAR BOX. OPERATIONS CHECKED GOOD. (W)SDR 9504299958Switch · brokenGEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS EXTENDED ON APPROACH. ACCOMPLISHED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LEFT GEAR DOOR SWITCH ARM BROKEN. REPLACED SWITCH, OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SDR USAA950236Transmitter · out of limitsCLT - FLT 8027 - AFTER TAKEOFF, THE STALL INDICATION FAIL AND WINDSHEAR WARNING LIGHTS ILLUMINATED. FLIGHT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT FLAP TRANSMITTER. OPERATIONS CHECKED GOOD. (X)SDR 9504039998Clips · out of adjustDURING LINE CHECK FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR HANDLE FROM THE CLIPS. ADJUSTED AND LUBRICATED THE CLIPS. CHECKED OK.SDR USAA950235Link · damagedPIT - FLT 0590 - UPON GEAR RETRACTION, CREW HEARD A LOUD BANG FROM THE NOSE GEAR. THE RED UNSAFE LIGHT ILLUMINATED. THE GEAR WAS PUT DOWN, BUT THE LIGHT REMAINED. FLIGHT RETURNED TO PIT WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT NOSE GEAR FORWARD LINKSDR 95ZZZX1762Angle · crackRIGHT PYLON ANGLE RIB HAS 1 INCH LONG CRACK UNDER PANEL NR 8206. REPLACED ANGLE RIB PER SRM 51-30-02. AIRCRAFT TT. 54,495 HRS.SDR 95ZZZX1761Fitting · crackFS 986 - FS 996, RBL 15, 54 INCHES AND 18 INCHES ABOVE FLOOR, 2 EACH FITTINGS CRACKED AROUND FASTENERS. REPLACED FITTINGS PER SRM 51-3-5, AND SRM 51-30-2. AIRCRAFT TT, 54,495 HRS.SDR 95ZZZX1760Doubler · corrosionHEAVY CORROSION ON INNER DOUBLER FS 1132 - FS 1143, BETWEEN LONGERONS 18L-20L. REPLACED DOUBLER PER SRM 51-30-02. AIRCRAFT TT, 54,495 HRS.SDR 95ZZZX1759Angle · crackRIGHT PYLON ANGLE RIB HAS A .75 INCH CRACK UNDER PANEL NR 8204. REPAIRED ANGLE PER SRM 54-01, FIGURE 2. AIRCRAFT TT, 54,495 HRS.SDR 95ZZZX1758Skin · corrosionHEAVY CORROSION ON INNER SKIN FS 950 AT LONGERON 29R. REPAIRED SKIN PER DALFORT AVIATION XEA NR X9-53-80. AIRCRAFT TT, 54,495 HRS.SDR 95ZZZX1757Doubler · corrosionHEAVY CORROSION AND CRACK ON INNER SKIN DOUBLER FS 1121 - FS 1132, BETWEEN LONGERONS 17L-18L. REPAIRED DOUBLER PER SRM 53-01, FIGURE 2. AIRCRAFT TT, 54,495 HRS.SDR 9504509996Doubler · brokenDURING PERIODIC CHECK, FOUND BROKEN DOUBLER AT FS 1084, LONGERON 18L. REPAIRED PER EA 99-097155.SDR 9504289971Slats Mech · lack of lubeSLAT DISAGREEMENT LIGHT ILLUMINATED WITH SLATS EXTENDED, FLAPS AT 5 DEGREES, AND SPEED AT 220 KNOTS. RETRACTED SLATS AND AIRCRAFT ROLLED TO THE RIGHT. EXTENDED SLATS AGAIN WITH FLAPS SET AT 15 DEGREES. NORMAL SLAT CONFIGURATION WAS ACHIEVED. INSPECTED AND SDR 9504089945Bracket · crackedDURING LINE CHECK, FOUND CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE REPAIR, RIGHT SIDE ABOVE THE RUDDER LEADING EDGE. REPAIRED PER XEA X9-53-82.SDR 9503929996Fitting · crackedDURING PERIODIC CHECK FOUND CRACK IN FLOOR SUPPORT FITTING, LONGERON 28R AT FS 996. REPLACED FITTING PER SRM 51-30-0.SDR 9503919996Fitting · crackedDURING PERIODIC CHECK FOUND CRACK IN LONGERON 28R END FITTING AT FS 984. REPLACED FITTING PER SRM 51-30-0.SDR USAA950237Control Cable · frozenDTW - FLT 1698 - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE FOUND LANDING GEAR CONTROL CABLE IN THE RIGHT WHEEL WELL FROZEN. THE OBSTRUCTION WAS CLEANED. AIRCRAFT OKAY FOR SERVICE. (X)SDR 9503789906Generators · malfunctionedLEFT AND RIGHT GENERATORS DROPPED OFF LINE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. RAN OPERATIONAL CHECK WITH NO PROBLEMS FOUND. AIRCRAFT RETURNED TO SERVICE.
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