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 VJ980022Power Supply · inoperativeEMERGENCY LIGHTS IN FWD GALLEY INOP. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW MM 33-50.SDR CALA9801241Longeron · crackedINSPECTION FOUND LONGERON 16R CRACKED AT UPPER FLANGE AND LONGERON 16L CRACKED OUT OF UPPER AND LOWER ATTACH CLIP FASTENERS, STA 965. THE CRACKED AREAS OF LONGERONS WERE REMOVED IAW SRM 51-30-2. LONGERONS AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 53-SDR CALA9801240Longeron · crackedINSPECTION FOUND THREE CRACKS IN LONGERON 17R AT FRAME ATTACH HOLES FROM STA 945 TO 980. THE CRACKS WERE .5 TO 1 INCH LONG. THE CRACKED AREAS OF LONGERON WERE REMOVED IAW SRM 53-02, FIGURE 18. LONGERON REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-02, FISDR CALA9801238Fitting · crackedINSPECTION FOUND A 7 INCH CRACK IN KEEL BEAM FITTING AT BS 756, LONGERON 30. THE FITTING WAS REMOVED AND A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-5 AND 51-30-1, PAGE 6.SDR TWAA9811906Skin · corrodedDURING OP 16 MAINTENANCE CHECK, FOUND SKIN PILLOWING AT FS 575 TO FS 604, L27R THROUGH LONGERON 27L. REMOVED FRAMES FROM FS 579 TO FS 604. REMOVED LONGERONS 26L TO 26R. REMOVED DOUBLERS, BLASTED PARTS PER SRM 51-10-03, ITEM 35D. REPLACED DOUBLER FROM STA 5SDR TWAA9811905Longeron · crackedDURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 30 CRACKED JUST FORWARD OF STA 578 FRAME. INSTALLED NEW LONGERON END PER INSTL DWG 592176 PER SRM 51-01, PG 1 ITEM C. INSTALLED WITH NEW FASTENERS PER SRM 51-60-0 AND INSTL DWG 592176. ACFT TT: 77,210 HOURS. ASDR TWAA9811904Longeron · crackedDURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29L CRACKED JUST FORWARD OF STA 578 FRAME. REMOVED AND REPLACED LONGERON END PER INSTL DWG 592176 PER SRM 51-01, ITEM C. INSTALLED NEW STRINGER PER INSTL DWG 592176 AND SRM 51-60-0. ACFT TT: 77,210 HOURS. ACFSDR CALA9801237Floor · corrodedINSPECTION FOUND FLOOR PANEL CORRODED AT STA 229 TO 294, BL 0. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 53-10-4, 51-20-2, 51-10-3, AND 51-30-2.SDR CALA9801236Doubler · bulgedINSPECTION FOUND DOUBLER BULGED WITH FASTENERS PULLING THROUGH AT STA 1019, LONGERON 19L. THE DOUBLER WAS REMOVED IAW SRM 51-10-2. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 53-04, FIGURE 12B.SDR CALA9801235Channel · crackedINSPECTION FOUND A .5 INCH CRACK AROUND FASTENER HOLE IN CHANNEL AT FORWARD CARGO DOOR FRAME STA 389, S18R, RBL 52. THE CHANNEL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2.SDR TWAA9811503Angle · corrodedDURING OP 16 MAINTENANCE CHECK, FOUND FLOOR ANGLE WITH EXFOLIATION AT FS 914, S29R. REMOVED EXFOLIATED SECTION OF ANGLE AND REPAIRED AREA PER SRM 53-01, FIG 2 SHEET 4. AFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)SDR MWEA98769Cover · detachedTHE GALLEY DOOR SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE COVER.SDR MWEA98768Slide · shiftedCAN'T READ GALLEY DOOR SLIDE PRESSURE GAUGE DUE TO SHIFT OF SLIDE. MAINTENANCE ADJUSTED GALLEY DOOR SLIDE.SDR CALA9801228Skin · corrodedINSPECTION FOUND SKIN CORRODED AT AFT CARGO COMPARTMENT FRAME STA 945 BETWEEN LONGERON 25R AND 26R. THE CORRODED AREA WAS CUT OUT. A REPAIR DOUBLER, FINGER DOUBLER, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-04, FIGURE 12, SHEESDR CALA9801227Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORROSION AT STA 980, LBL 34, STA 996, LBL 27, AND STA 965, LBL 16. L-ANGLES AND FILLERS WERE FABRICATED AND INSTALLED AT EACH LOCATION IAW SRM 53-05, FIGURE 20A AND 51-10-3.SDR VJ9800220Cover · dislodgedON ARRIVAL AT GATE, EMERGENCY SLIDE PACK COVER DISLODGED. REINSTALLED IAW MM 25-60. PERFORMED REQUIRED INSPECTIONS.SDR TWAA9811902Floor Panel · crackedDURING OP 16 MAINTENANCE CHECK, FOUND FORWARD CABIN FLOOR PANEL NR 40 WITH HAT SECTIONS CRACKED IN SEVERAL PLACES. REPLACED CRACKED HAT SECTIONS IN FLOOR PANEL NR 40 PER SRM 53-00-104, PAGE 201 FIG 201. (M)SDR MWEA98771Control Box · malfunctionedTHREE RED UNSAFE LIGHTS STAYED ON UPON GEAR RETRACTION CYCLED GEAR DOWN AND RED LIGHTS STAYED ON WITHOUT ANY GREEN LIGHTS ON. REMOVED AND REPLACED PROX SWITCH CONTROL CIRCUIT BREAKER AND PROX SWITCH CONTROL BOX.SDR CALA9801225Frame · crackedINSPECTION FOUND A .5 INCH CRACK IN RADIUS OF FORWARD CARGO COMPARTMENT FLOOR FRAME AT STA 256, S27L. THE CRACK WAS STOP DRILLED. AN L-ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263 AND SRM 51-10-3.SDR CALA9801224Rib · crackedINSPECTION FOUND A 3.5 INCH CRACK IN LT WING LEADING EDGE RIB AT HI-LOK IN UNDERSIDE OF LEADING EDGE AT XOS 516. THE RIB WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED ON RIB IAW SRM 57-02, FIGURE 6 AND 51-10-3. THE RIB WAS REINSTASDR CALA9801223Doubler · corrodedINSPECTION FOUND DOUBLER CORRODED WITH FASTENERS PULLING THROUGH AT STA 351, LONGERON 30. A FINGER DOUBLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR CALA9801222Angle · crackedINSPECTION FOUND NR 2 ENGINE PYLON INBOARD VERTICAL ATTACH ANGLE FORWARD OF WIRE BUNDLE CRACKED AT LOWER END. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30-5, 54-04, FIGURE 10, AND MM 51-20-11.SDR CALA9801221Support · crackedINSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT STRIP AT STA 332, S27L. THE CRACK WAS STOP DRILLED. AN L-ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.SDR CALA9801220Support · crackedINSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT AT STA 294, S28R, FORWARD CARGO COMPARTMENT. THE CRACK WAS STOP DRILLED. AN L-ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.SDR VJ9800219Bumper · wornUNSATISFACTORY GEAR UPLATCH CHECK OF LT MLG; DOOR OPEN AND GEAR UNSAFE INDICATION. FLIGHT CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE AS A PRECAUTIONARY MEASURE. REPLACED LT MAIN TORQUE LINK BUMPER; GEAR SWING PERFORMED AND CHECKED GOOD.SDR VJ9800218Cover · dislodgedEMERGENCY EVACUATION SLIDE COVER ON GALLEY DOOR BECAME DISLODGED. REINSTALLED IAW MM 25-00 AND PERFORMED REQUIRED INSPECTION.SDR TWAA9811005Skin · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WING SKIN WITH HOLE WORN THROUGH SKIN INBD OF NR 1 SLAT TRACK, L.E. OF WING TO END OF WING TO NR 3 SLAT TRACK HAD WORN SKIN. BLENDED WEAR AREA OTBD OF CENTER TRACK CUT-OUT PER SRM 57-01 PAGE 5, FIG 1. INSDR TWAA9811003Rib · bentMCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING FLAP, TWO RIBS INSIDE LOWER INBD ACCESS PLATE WERE BENT. INSTALLED REPAIR DOUBLER PER ARA 15361. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR CALA9801226Shear Tie · crackedINSPECTION FOUND A .5 INCH CRACK IN SHEAR TIE ON MAIN FRAME AT FS 945 BETWEEN LONGERON 14R AND 15R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-10-4, AND 51-10-3.SDR VJ9800217Control Panel · repairableNR 2 GENERATOR WENT OFF LINE EN ROUTE TO PHL FROM ATL. VOLTS AND FREQUENCY CHECKED NORMAL; GENERATOR WOULD NOT RESET. TAIL COMPARTMENT HI LIGHT ILLUMINATED AFTER APU STARTED AS BACK UP FOR ELECTRICAL POWER. AS PRECAUTIONARY MEASURE, FLIGHT CREW ELECTED TO RESDR VJ9800216Cover · dislodgedEMERGENCY SLIDE COVER ON MAIN PASSENGER DOOR BECAME DISLODGED. REINSTALLED SLIDE PACK.SDR MWEA98763Slide · inoperableTHE GALLEY SERVICE DOOR ESCAPE SLIDE PRESSURE GAUGE IS IN RED AREA. MAINTENANCE REPLACED GALLEY DOOR SLIDE.SDR CALA9801210Skin · crackedINSPECTION FOUND A 1 CRACK IN FUSELAGE SKIN AT STA 935, LONGERON 25R, AFT OF CARGO DOOR OPENING. THE CRACKED AREA WAS REMOVED IAW SRM 53-05, FIGURE 80. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 53-05, FIGURE 80, 51-10-3, 51-30-2, AND 51-30-5.SDR VJ9800213Window · out of adjustCAPTAIN'S SLIDING WINDOW JAMMED; WON'T OPEN. REINSTALLED UPPER HINGE IAW MM 56-10. OPS CHECKS GOOD.SDR VJ9800212Battery · dischargedFWD AFT CABIN OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERIES; OPS CHECKED GOOD IAW MM 33-00.SDR TWAA9810602Battery Pack · dischargedSTL - DURING MAINTENANCE CHECK, FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS INOP IN CABIN AISLE, AND RT AFT OVERWING EXIT LIGHT INOP. REPLACED CELL PACK B5-25. CHECK-C, 8-6-97 MCI. (M)SDR MWEA98762Slide · not installedTHE MAIN CABIN DOOR SLIDE PACK IS REMOVED. MAINTENANCE REINSTALL DOOR SLIDE.SDR CALA9801209Support · crackedINSPECTION FOUND A 2 INCH CRACK EXTENDING FROM RADIUS TO FASTENER HOLE IN CABIN FLOOR SUPPORT AT STA 3113, BL 0. THE CRACK WAS STOP DRILLED. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30-2.SDR ABXA9800602Power Supply · inoperativeEMERGENCY LIGHTING WOULD NOT TEST. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY.SDR 9809749942Line · leakingRIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WENT TO ZERO AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE LEAKING. REPLACED LINE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR 9809739986Boot · looseLOSS OF CABIN PRESSURIZATION OCCURRED AT 31,000 FEET EN ROUTE. CREW ACCOMPLISHED EMERGENCY DESCENT TO 10,000 FEET. FLIGHT WAS CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE RUBBER BOOT BETWEEN LEFT AIR CYCLE MACHINE AND HEAT ESDR VJ9800224Jamb · damagedFWD AND AFT LOWER DOOR JAMB IN FWD CARGO COMPARTMENT REQUIRES REPAIR AT FWD AND AFT CORNER. FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW RES 1-06013 AND DC9 SRM 53005, FIG 44.SDR VJ9800215Oxygen Mask · deployedWITH PRESSURIZATION IN MANUAL MODE, OXYGEN MASKS DEPLOYED IN BUSINESS CLASS SECTION, FLT ATTENDANT STATIONS AND 8 POSITIONS IN COACH CLASS ON DESCENT FOR LANDING. REPACKED OXYGEN MASKS AND FLEW AIRCRAFT BELOW FL100 FROM MEM TO ATL. INSPECTED AIRCRAFT AND NO SDR TWAA9810805Web · crackedMCI- DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR MEMBRANE CRACKED AT FS 744, RBL 50. REPLACED MEMBRANE WITH NEW PART PER SRM 51-01 PAGE 04. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)SDR CALA9801207Skin · crackedINSPECTION FOUND A 1.25 CRACK IN FUSELAGE SKIN AT STA 560, STRINGER 18L. THE CRACKED SKIN WAS REMOVED AND A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5330-02481.SDR CALA9801206Floor · corrodedINSPECTION FOUND CABIN FLOOR PANEL CORRODED AND PUNCTURED AT STA 960-965, BL 0 TO RBL 21.5. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-70-1 AND 53-05, PAGE 122B.SDR TWAA9810712Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOND FORMER FOOT STA 980 CRCKED BELOW LONGEORN 14R AND ABOVE 16R. REPLACED FORMER PER MO 72J14. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)SDR TWAA9810711Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LOWER SURFACE AT DAMPER CUT OUT LOWER RIB CAP CRACKED ON LT ELEVATOR. REPLACED LOWER RIB CAP PER DAC DWG 9918535. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X)SDR GTIA9800079Slide · looseMAIN CABIN DOOR ESCAPE SLIDE FELL OUT DUE TO JET BLAST. REINSTALLED ESCAPE SLIDE AS REQUIRED. NO DEFECTS NOTED AT THIS TIME IAW DC9 MM 25-61-0. ALL ACCOMPLISHED. (M)SDR CALA9801203Support · crackedINSPECTION FOUND TWO .5 INCH CRACKS IN FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 294, STRINGER 27L. THE CRACKS WERE STOP DRILLED IAW ECRA 5320-01263. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.
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