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 TWAA0002511Intercostal · crackedDURING OP 16 MAINT CHECK, FOUND RT SIDE INTERCOSTAL CRACKED AT 2 CENTER NUT PLATE HOLES, STA 579 TO 598. REPLACED PART PER SPM 6-70-01, PAGE 1 ITEM 1, AND SRM 51-30-2 AND 51-10-4 AND DOUGLAS DRAWING 9915553.SDR 0000429979Roller · looseAFTER TAKEOFF FROM PHL DURING GEAR RETRACTION, THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FOLLOWED COM PROCEDURE BUT INDICATOR DID NOT EXTINGUISH. UPON ARRIVAL MSP, THE RIGHT GEAR DOOR OPEN LIGHT ANNUNCIATED. THE RIGHT GREEN SAFE LIGHT NEVER ILSDR TWAA0002401Wire · wornTHE EGRESS LIGHTING WAS INOPERATIVE FROM ROW 9 TO THE AFT CABIN. REPLACED FEEDER CABLE (P/N 5854-1) AND FLEX CABLE (P/N 5853-1). CHECK-C 1-14-00 STL.SDR ABXA000107Switch · failedON LANDING HAD TO RECYCLE GEAR BECAUSE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR WAS SELECTED DOWN AGAIN AND ALL THREE GREEN LIGHTS ILLUMINATED. REPLACED NLG DOWNLOCK POSITION SWITCH IAW DC9 SMM 32-60-00. OPS CHECKED GOOD.SDR ABXA000104Shear Tie · crackedSHEAR-TIE AT STA 996 AND LONGERON 18L IS CRACKED.. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-5 AND 51-30-2.SDR TWAA0002510Longeron · crackedDURING OP 16 MAINT CHECK, FOUND CABIN LONGERON 3L CRACKED AT STA 160. REPAIRED PER SRM 53-02, FIG 18.SDR 0000339967Seal · failedDURING FLIGHT, THE FLIGHT ATTENDANTS REPORTED THE FORWARD AND AFT LAVATORY SMOKE ALARMS SOUNDED AND HAZE IN THECABIN. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED AT MSP WITHOUT INCIDENT. MAINTENANCE FOUND OIL WITHIN THE NR 1 ENGINE COWLING AND REPLACEDSDR TWAA0002209Tail Cone · ejectedON THE GROUND, THE TAIL CONE WAS INADVERTANTLY DEPLOYED. REINSTALLED TAIL CONE ASSEMBLY PER MC8-5303. OP16 08-24-97 MCI..SDR TWAA0002201Power Supply · failedF/C EGRESS LIGHTS ON WITH SWITCH IN ARMED POSITION. REPLACED POWER SUPPLY. CHECK-C 01-14-00 STL.SDR USAAD000025Valve · failedPIT - MDT - FLT 1414 - AFTER TAKEOFF THE NOSE LANDING GEAR DID NOT FULLY RETRACT AND THE RED GEAR UNSAFE LIGHT REMAINED ON. WHEN THE LANDING GEAR WAS EXTENDED ALL THREE GREEN LIGHTS ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT.SDR TWAA0002410Fitting · crackedDURING OP 16 MAINT CHECK FOUND CRACK ON FITTING, O/B FLOOR SUPPORT BEAM AT STA 996, RBL 60 INCHES. INSTALLED NEW FITTING (P/N 5913700-24) WITH HI-LOKS PER SPM 6-70-01, PAGE 1 AND 3.SDR TWAA0002411Intercostal · crackedDURING OP 16 MAINT CHECK FOUND AT BL 0 JUST AFT OF CABIN FLOOR BEAM, STA 965, INTERCOSTAL WAS CRACKED AT UPPER FWD CORNER. INTERCOSTAL WAS FABRICATED AND INSTALLED WITH HARDWARE PER DOUGLAS DRAWING 9915585.SDR TWAA0002409Bulkhead · gougedDURING OP 16 MAINT CHECK FOUND GOUGE IN FWD SIDE OF AFT PRESSURE BULK HEAD SKIN BELOW LONGERON 2L. REMOVED FASTENER AND BLENDED GOUGE PER SRM 53-01 FIG 1 AND REINSTALLED FASTENER.SDR GTIA000068Light · inoperativeCLE - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE.. PLACED EXTERIOR EMERGENCY LIGHT ON DMI NR 51 REF MEL 33-20, CAT B. (M)SDR GTIA000066Lens · missingCLE - EMERGENCY PATHWAY LIGHTS ONE LENS COVER MISSING. REPLACED MISSING LENS COVER, OPS CHECK GOOD. (M)SDR USAAD00024Coalescer Bag · contaminatedDTW-PIT - FLT 2201 - ON APPROACH INTO PIT, AN OIL LIKE SMELL IN THE CABIN WAS REPORTED COMING FROM BOTH PACKS WITH SMOKE DETECTORS IN LAVATORY SOUNDING OFF. FLIGHT LANDED AT PIT WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED INTAKES AND TURBINES OF BOTH ENGSDR GTIA000067Light · inoperativeCLE - TWO FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRES AND INSTALL NEW SOCKET. OPS CHECK GOOD. (M)SDR TWAA0002408Longeron · crackedDURING OP 16 MAINT CHECK FOUND LONGERON 4L CRACKED AT STA 160. REMOVED AND REPLACED LONGERON PER DRAWING 5911406.SDR TWAA0002407Longeron · crackedDURING OP 16 MAINT CHECK FOUND LONGERON 4L CRACKED AT STA 200. REMOVED AND REPLACED LONGERON PER DRAWING 5911406.SDR ABXA000099Finger Doubler · crackedFINGER DOUBLER IS CRACKED AT STATION 239 JUST BELOW LONGERON 18 LEFT INSIDE FORWARD LOWER CARGO COMPARTMENT. REPAIRED FINGER DOUBLER IAW ABX REA D953-35352.SDR USAAD00021Battery · dischargedLGA - THE FORWARD ENTRY DOOR SLIDE ACTIVATED. EMERGENCY LIGHT WAS REMOVED FROM AIRCRAFT 830US. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (X)SDR USAA000100Keel Beam · chafedPIT - STA 917 A/C CENTERLINE. BEAM CAP HAD 1 INCH BY 2 INCH CHAFE MARK. KEEL BEEM FOUND CRACKED AT BS 917. BLENDED OUT WEAR MARKS AND INSTALLED .025 INCH SS WEAR STRIP PER SRM 53-05 FIG 20 PAGE 30A. (X)SDR GTIA000059Light · looseTPA - FLT 431 - EMERGENCY TRACK LIGHTING NEEDS TO BE SECURED IN AFT CABIN. PASSENGER PULLED LOOSE DURING FLIGHT. SECURED EMERGENCY TRACK LIGHTING IN AFT OF AIRCRAFT. OPERATIONAL CHECKS GOOD ON GROUND DC-9 MM 33-50. (M)SDR TWAA0002004Frame · crackedDURING OP 16 MAINT CHECK, FOUND CRACK ON TWO RIVETS ON MEMBRANE 2 IN AFT OF RT FORMER RING, STA 775 BELOW FLOOR. INSTALLED ALUMINUM ALLOY DOUBLER REPAIR PER SRM 53-01, PAGE 9 EXAMPLE C. TREATED, PRIMED, AND PAINTED DOUBLER PER 51-10-03.SDR GTIA000063Strap · missingDTW - AFT TAIL SLIDE HAS NO MANUAL DEPLOY STRAP.. OPENED TAIL SLIDE, FOUND MANUAL DEPLOY STRAP INSIDE, REROUTED STRAP IAW DC9 MM 25-61-01. (M)SDR GTIA000062Wire · exposedDTW - FLOOR PATH LIGHTING AT ROW 16 WIRES EXPOSED AND PINCHED. REINSTALLED TRACK AND REPOSITIONED WIRES UNDER TRACK IAW DC-9 MM 33-53-01. (M)SDR GTIA000061Wire · exposedDTW - FLOOR PATH LIGHTING AT ROW 2 HAS GAP IN TRACK AND WIRES EXPOSED. INSTALLED NEW TRACK AND CUT TO FIT IAW DC-9 MM 33-53-01. (M)SDR ABXA000098Angle · corrodedDURING C CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR FORWARD HINGE LOWER FUSELAGE SUPPORT BRACKET ATTACH ANGLE EXFOLIATED. REPLACED ANGLE IAW DC9 SRM 51-30-5.SDR ABXA000097Web · crackedDURING C CHECK, FOUND THE LEFT FORWARD EMERGENCY EXIT DOOR INTERIOR WEB CRACKED. REPAIRED WEB IAW DC9 SRM 52-01, FIGURE 2, SHEET 3.SDR ABXA000096Angle · crackedDURING C CHECK, FOUND STA 756 BULKHEAD CENTER VERTICAL SUPPORT ANGLE CRACKED. REPAIRED ANGLE IAW DC9 SRM DRAWING NR K05159.SDR ABXA000095Beam · crackedDURING C CHECK, FOUND NR 5 HORIZONTAL BEAM IN FORWARD ENTRY DOOR CRACKED AT THE BOLT HOLE AT THE CENTER OF THE BEAM. REPAIRED BEAM IAW SRM DRAWING NR K05159.SDR ABXA000094Rib · crackedDURING C CHECK, FOUND A RIGHT WING TRAILING EDGE RIB ABOVE THE INBOARD FIXED VANE CRACKED. REPAIRED RIB IAW ABX REA D957-35354.SDR ABXA000093Rib · crackedDURING C CHECK, FOUND A RIGHT WING TRAILING EDGE RIB ABOVE THE INBOARD FIXED VANE CRACKED. REPLACED RIB IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA000092Pan · crackedDURING C CHECK, FOUND THE SERVICE DOOR PAN CRACKED IN TWO PLACES AT THE FORWARD UPPER CORNER. REPAIRED DOOR PAN IAW DC9 SRM 52-03 FIGURE 3.SDR 0000269961Outflow Valve · malfunctionedLOSS OF PRESSURIZATION OCCURRED DURING CLIMB THROUGH 17,000 FEET. OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN AND FLIGHT WAS RETURNED TO RDU. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OUTFLOW NOZZLE VALVE RUBBING AGAINST HYDRAULIC SUPPLY LINE CLAMSDR TWAA0002003Vane · damagedDURING OP 16 MAINT CHECK ON THE RT WING FOUND REPAIR ON FLAP INBD FIXED VANE SEGMENT AT LE THAT NEEDED TO BE REPLACED. INSTALLED HOT BOND REPAIR PER SRM 51-70-2, PARA 18B AND 51-70-2 FIG 5 TABLE 6, TABLE 8 FIG 12. STRUCTURAL ADHESIVE BONDING MANUAL 5910041-1-SDR 0000209929Duct · lack of lubeON APPROACH INTO CLT, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ROLL TO THE LEFT ON SLAT EXTENSION. FLIGHT CREW DECLARED A YELLOW EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE LUBRICATED LEFT SLAT T DUCT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETSDR USAAD00017Battery · dischargedIND - THE TAILCONE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE TAIL CONE ACTIVATED EMERGENCY LIGHT BATTERY. (M)SDR TWAA0001811Skin · dentedDURING OP 16 MAINT CHECK, FOUND ON LT WING FLAP, A DENT IN LOWER SURFACE APPROX 65 IN FROM I/B END AND APPROX 37 IN FROM T/E APPROX 0.125 INCHES DEEP, LENGTH 5 IN, WIDTH 5 IN. REPLACED SKIN PANEL PER SRM 51-30-2 WITH RIVETS AND DAC DRAWING 5910134.SDR TWAA0001809Frame · crackedDURING OP 16 MAINT CHECK, FOUND MEMBRANE CRACKED AND CORRODED AROUND RIVETS ON AFT SIDE OF RT FORMER RING, STA 813. MADE ALUM ALLOY REPAIR PER SRM 53-01, PAGE 9. PAINTED DOUBLER PER 51-10-03, INSTALLED DOUBLER.SDR TWAA0001808Panel · damagedDURING OP 16 MAINT CHECK, ENGINEERING REQUESTED ACCOMPLISH PERMANENT REPAIR TO FIXED RT WING UPPER TRAILING EDGE PANEL ASSY (P/N 5920521-2). INSTALLED DOUBLER PER SRM 57-01 PAGE 15 FIG 5, AND PAGE 19 FIG 8.SDR TWAA0001807Panel · damagedDURING OP 16 MAINT CHECK, A PREVIOUS REPAIR WAS FOUND ON THE RT WING FIXED T/E PANEL ASSY (P/N 5920521-2) UPPER O/B SKIN PANEL INTERIOR. INSTALLED DOUBLER PER SRM 57-01, PAGE 15 FIG 5, AND PAGE 19 FIGURE 8.SDR TWAA0001810Frame · crackedDURING OP 16 MAINT CHECK, FOUND MEMBRANE CRACKED AND CORRODED 1.5 IN FWD OF RT FORMER RING, STA 813 BELOW FLOOR. MADE ALUM ALLOY REPAIR PER SRM 53-01, PAGE 9. TREATED AND PAINTED DOUBLER PER 51-10-03, INSTALLED DOUBLER.SDR TWAA0001806Skin · crackedDURING OP 16 MAINT CHECK, THE TOP NOSE SKIN WAS CRACKED AT RIVET RT STA 76.550, RBL 15. REMOVED DAMAGED AREA PER DOUGLAS DRAWING SRO 9530239 AND INSTALLED REPAIR PER SRO 9530239.SDR TWAA0001805Skin · crackedDURING OP 16 MAINT CHECK, FOUND LT TOP NOSE FUSELAGE SKIN WAS CRACKED AT 4 RIVETS STA 76.550, 16 IN LBL TO 20 IN LBL. TRIMMED DAMAGED AREA AND ADDED REPAIR DOUBLER AND FILLER PER SRO 9530239.SDR TWAA0001804Support · crackedDURING OP 16 MAINT CHECK, FOUND VERTICAL SUPPORT (P/N 9957860-6) WAS CRACKED AT STA 69.55. REMOVED DAMAGED VERTICAL SUPPORT AND INSTALLED NEW SUPPORT PER SRO 9530268.SDR TWAA0001803Skin · crackedDURING OP 16 MAINT CHECK, THE TOP NOSE SKIN WAS CRACKED AT RIVET RT STA 76.550, RBL 18. REMOVED DAMAGED AREA PER DOUGLAS DRAWING SRO 9530239. INSTALLED REPAIR PER SRO 9530239.SDR TWAA0001802Skin · crackedDURING OP 16 MAINT CHECK, THE LT TOP NOSE FUSELAGE SKIN WAS CRACKED AT 5 RIVETS, STA 69.550, 15 IN LBL TO 20 IN LBL. TRIMMED DAMAGED AREA AND ADDED REPAIR DOUBLER AND FILLER PER SRO 9530239.SDR 20000419AP001Battery · dischargedIND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT AND ONE SECTION OF PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD00015Battery · dischargedIND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT AND ONE SECTION OF PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
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