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 TWAA0002404Support · crackedDURING OP 16 MAINT CHECK FOUND AFT CABIN PRESSURE BULKHEAD DOOR INTERNAL CENTER SUPPORT WEB CRACKED, LT END WITH END SECTION MISSING. INSTALLED NEW SUPPORT WEB PER PRINT 9915565.SDR TWAA0002403Casting · crackedDURING OP 16 MAINT CHECK FOUND AFT CABIN PRESSURE BULKHEAD DOOR INTERNAL LT LOWER TOP CASTING CRACKED AT LOWER LEG. REPLACED WITH NEW CASTING PER SERVICE REWORK DRAWING JO60229.SDR TWAA0002402Fastener · looseDURING OP 16 MAINT CHECK FOUND NUMBER 1 PYLON TOP AFT SKIN HAD 4 ROWS OF BLIND FASTENERS LOOSE AND WORKING. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 9957742, 9915500, 9915501, 9915502, AND 9915503.SDR TWAA0002316Fastener · misinstalledDURING OP 16 MAINT CHECK ON NUMBER 2 PYLON, TOP OF PYLON SKIN INBD OF AFT ENGINE MOUNT HAD ROW OF SCREWS WITH SKIN WASHERS LOOSE AND IMPROPERLY INSTALLED. REPLACED UPPER SKIN AND FASTENERS PER DAC DRAWING 9957742, 9915500, 9915501, 9915502 AND 9915503.SDR AT0000074Door Pan · corrodedFOUND C1 CARGO DOOR CUTOUT PAN HAD SEVERAL AREAS OF CORROSION. REMOVED AND REPLACED CARGO DOOR PAN, FABRICATED AND INSTALLED PAN SPLICES IAW DC9 SRM 53-05 FIGURE 44, 51-30-2, 51-30-5, 51-10-4.SDR TWAA0002315Structure · corrodedDURING OP 16 MAINTENANCE CHECK, ON NUMBER 1 PYLON TOP AND BOTTOM OF PYLON FOR ENG MOUNT YOKE STRUCTURE HAD RUSTY SURFACES AT LE ATTACH. CHECKED MATERIAL THICKNESS PER SPM 04-00. REPAIRED PER ARA 16530 AND SRM 54-04 PAGE 77. SHOT PEENED PER DRS 4999.SDR TWAA0002313Skin · damagedDURING OP 16 MAINTENANCE, CHECK NECESSARY TO INSTALL UPPER WINDOW BELT STRIP FROM STA 699 TO 756 ON LT SIDE. REINSTALLED WINDOW BELT DOUBLER PER MO 71K21 AND EMLR 70533 A.SDR AT0000083Longeron · crackedFOUND LONGERON 25L CORRODED AT ATTACH POINT TO FRAME AT BS 150-170. CUT OUT LONGERON BETWEEN BS 150-170. INSTALLED LINGERON SPLICES IAW DC9 SRM 53-02 FIGURE 18.SDR AT0000076Frame · corrodedFOUND CORROSION ON FORWARD SIDE FRAME AT BS 980, LONGERON 26R -24R. REMOVED CORROSION, BEYOND LIMITS. REMOVED FRAME SECTION AT BS 980, LONGERON 26R - 24R, INSTALLED NEW FRAME AND REPAIR SPLICES IAW DC9 SRM 53-03 FIGURE 2A.SDR AT0000070Skin · crackedFOUND CRACK AT FORWARD ENTRY DOOR JAMB, FORWARD UPPER CORNER ON OUTER SKIN. CUT OUT CRACKED SKIN, FABRICATED DOUBLERS, AND INSTALLED IAW SRD 9530252.SDR MWEA00038Slide · dislodgedGALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE FELL OFF. MAINTENANCE REINSTALLED SLIDE PACK.SDR TWAA0002002Stringer · crackedDURING OP 16 MAINT CHECK, STRINGER 4L WAS CRACKED AT STA 200. REPLACED STRINGER 4L AT STA 155 TO 229 PER SRM 51-01, PAGE 1. FASTENERS PER SRM 51-30-02 AND 51-30-5.SDR AT0000073Bulkhead · corrodedFOUND CANTED BULKHEAD AT BS 1143, LEFT HAND UNDER THE END OF LEFT HAND PYLON SKIN WAS CORRODED. REMOVED CORROSION, REPLACED SKIN AND DOUBLERS IAW DC9 SRM 53-01 FIGURE 4, 51-30-2, AND 51-30-3.SDR AT0000069Skin · crackedFOUND CARGO COMPARTMENT DOOR JAMB FORWARD LOWER CORNER HAS A .375 CRACK ON OUTER SKIN. CUT OUT CRACK, FABRICATED 2 REPAIR DOUBLERS. TREATED PRIMED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 51-10-03 AND EO 95310-29-E1410.SDR TWAA0002013Finger Doubler · corrodedDURING OP 16 MAINT CHECK, FOUND FUSELAGE CORROSION ON THE LOWER PRESSURE BULKHEAD FINGER DOUBLERS FROM LONGERON 24L TO L24R, STA 604. REPLACED WITH NEW FINGER DOUBLER PER DOUGLAS DRAWING 5914865.SDR TWAA0002012Tee · damagedDURING OP 16 MAINT CHECK, THE LOWER FUSELAGE LOWER BULKHEAD TEE AT STA 604 REQUIRED REPLACEMENT. CLEANED LOWER BULKHEAD TEE AREA STA 604. REPLACED WITH NEW TEE CORD PER DRAWING 5914865.SDR TWAA0002011Rib · crackedDURING OP 16 MAINT CHECK THE NUMBER 2 ENG PYLON, OTBD SUPPORT RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915502 AND INSTALLED RIB PN 9915501-502.SDR TWAA0002010Web · crackedDURING OP 16 MAINT CHECK, NR 2 PYLON HAD A CRACK IN THE WEB 9.5 INCHES OTBD OF THE FUSELAGE SKIN, TOP OF PYLON AT STA 1038. REPLACED PART PER DAC PRINT INSTALLATION 9915501, INSTALLED RIB 9915501-2.SDR TWAA0002009Rib · crackedDURING OP 16 MAINT CHECK, FOUND NR 2 ENGINE PYLON, INBD RIB WAS CRACKED AT THE FWD END. REPLACED PART PER DAC INSTALLATION PRINT 9915503 AND INSTALLED RIB 9915503-502.SDR MWEA00036Heater · malfunctionedFLIGHT CREW NOTICED SMOKE COMING FROM THE LEFT LAVATORY AT THE GATE. EVIDENCE OF ELECTRICAL FIRE. MTC REMOVED AND REPLACED LAV WATER HEATER, FLUSH TIMER, WATER HEATER CIRCUIT BREAKER, AND INSTALLED GROUNDING STRAP.SDR CA000215036Tire · failed(CAN) ON WALKAROUND NR 4 WHEEL TIRE CAP FAILED AND DAMAGED RT FIXED HINGE DOOR. WHEEL AND DOOR REPLACED.SDR MWEA00033Slide · dislodgedGALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE CAME LOOSE FROM COVER. MAINTENANCE RE-INSTALLED SLIDE.SDR AT0000087Bulb · failedFOUND AFT EMERGENCY SIGN, NEAR AFT DOOR, HAS BURNT BULBS. RELAMPED, IAW DC9 MM 33-50.SDR AT0000062Frame · crackedFOUND FRAME CRACKED AT RIGHT HAND SIDE NEAR THE ACTUATOR LOWER MOUNT (AIRSTAIRS) AT BS 1143. CUT OUT CRACKED FRAME SECTION FABRICATED L & Z DOUBLERS, HEAT TREATED AND INSTALLED NEW FRAME SECTION AND L & Z DOUBLERS IAW DC9 SRM 51-30-2, 51-10-3 AND EO L00024.SDR ABXA000079Warning System · malfunctionedON DEPARTURE OUT OF DSM, WHEN THE LANDING GEAR WAS RETRACTED, THREE GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. RECYCLED THE GEAR WITH NORMAL OPERATION. ON APPROACH INTO CIA, WHEN THE GEAR WAS LOWERED, THE NOSE LANDING GEAR TOOK LONGER THAN NORMAL TO LOCK DOWN.SDR TWAA0101702Longeron · crackedDURING CHECK-C MAINT LONGERON 4L WAS FOUND CRACKED IN 2 PLACES AT BELT RING, STA 1087. REMOVED AND REPLACED LONGERON PER SRM 53-02, FIG 18.SDR TWAA0001801Skin · crackedDURING OP 16 MAINT CHECK AT STA 200, THE FIRST FASTENER ABOVE STRINGER 4L HAD CRACK IN FUSELAGE SKIN 0.250 IN LONG. CRACK STOP DRILLED AND CONTAINMENT CONFIRMED BY NDT PER PART 6-51-00-03. SKIN WAS REPAIRED PER SRM 53-04 FIG 38.SDR AT0000085Light · inoperativeFOUND R1 DOOR OVERHEAD EMERGENCY LIGHT WILL NOT ILLUMINATE. RELAMPED, IAW DC9 MM 33-50.SDR AT0000084Bulb · failedFOUND 1 BULB BURNT ON TAILCONE HANDLE EMERGENCY LIGHT ASSEMBLY. RELAMPED BULB IAW DC9 MM 33-50.SDR AT0000060Longeron · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND LONGERON IN E&E COMPARTMENT BETWEEN BS 200-218 LONGERON 28 CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA AND SPLICED IN NEW REPAIR AT BS 200-218 LONGERON 28 IAW DC9 SRM 53-02 FIG 18, 55-01 FIG 1, 51SDR MWEA00035Oven · smokeRIGHT HAND GALLEY STARTED TO SMOKE DURING FLIGHT. FLIGHT ATTENDANT TURNED OFF OVEN AND SMOKE IMMEDIATELY STOPPED. MTC CHECKED AND RAN OVENS FOR SEVERAL MINUTES, NO SMOKE OR SMELLS OF SMOKE WERE NOTED.SDR TWAA0002008Keel Beam · corrodedDURING OP 16 MAINT CHECK, FOUND FUSELAGE STA 607 TO 667 HAD CORROSION ON THE KEEL BEAM. REMOVED CORROSION PER SRM 6-80-01, PAGE 1.SDR MWEA00031Unknown · odorAFTER TAKEOFF, NOTICED UNUSUAL ODOR IN COCKPIT. MTC THROUGHLY INSPECTED ALL AREAS AND COMPONENTS WITH NO ODORS OR DEFECT NOTED.SDR AT0000071Skin · corrodedFOUND RIGHT HAND AFT VANITY CLOSE TO ANGLE SKIN WAS CORRODED OUT OF LIMITS. FABRICATED UPPER SKIN, FILLERS, HEAT TREATED AND INSTALLED IAW DC9 SRM 51-30-1, 51-10-3, 53-01 FIGURE 2, 51-7 0-1. DC9 MM 20-20-0, WEBER OVERHAUL MANUAL, 25-42-50, DPS 4901 AND DPS 1SDR AT0000065Frame · crackedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND RIGHT MAIN FRAME AT BS 699 IN AFT POCKET POINT F TO D, POINT M-B-A, AND POINT G-H CRACKED. REMOVED AND REPLACED RIGHT MAINFRAME AT BS 699 IAW DC9 SRM 51-30-01, 51-30-02, AND 51-30-05.SDR AT0000061Door Jamb · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON FORWARD CARGO LOWER DOOR JAMB. REMOVED AND REPLACED LOWER CARGO DOOR JAMB IAW DC9 SRM 51-10-04, 51-10-03, AND 53-05 FIG 4A.SDR AT0000059Longeron · corrodedFOUND LONGERON 24R HAD CORROSION AT BS 935 FROM END CAP ALONG UPPER CHANNEL TO BS 945. REMOVED LONGERON 24R, END CLIP, END FITTING. INSTALLED NEW SKIN PATCH AT BS 945, LONGERON 24R, END CLIP AND END FITTING IAW DC9 SRM 53-04 FIGURE 38, 52-02 FIGURE 18.SDR ABXA000090Doubler · corrodedWHILE COMPLYING WITH A C CHECK INSPECTION, FOUND LEFT SIDE STATIC PORT INTERNAL DOUBLER CORRODED. REPLACED INTERNAL DOUBLER IAW DC9 SRM 51-30-2.SDR ABXA000089Column · crackedWHILE COMPLYING WITH A C CHECK INSPECTION, FOUND FIRST OFFICER'S CONTROL COLUMN CRACKED. REPLACED FIRST OFFICER'S CONTROL COLUMN REF DOUGLAS SERVICE BULLETIN.SDR ABXA000088Fairing · corrodedWHILE COMPLYING WITH A C-CHECK INSPECTION, FOUND LOWER RIGHT SIDE HORSE COLLAR CORRODED. REPLACED LOWER RIGHT SIDE HORSE COLLAR IAW DC9 MM 55-10-0 AND DC9 SRM 51-30-1.SDR 0000529614Hinge · crackedCRACK IN NOSE WHEEL WELL SUPPORT FITTING BS 50 ABOVE FORWARD HINGE OF LEFT FORWARD DOOR 1.5 INCH LONG. CRACKED LOWER SURFACE FRONT END THROUGH FASTENER HOLE. REPAIRED, REMOVED AND REPLACED NOSE GEAR DEFLECTOR STOP PER EA 96-172125 AND SRM 51-30-5 SB 32-124RLSDR TWAA0002312Fastener · wrong partDURING OP 16 MAINTENANCE CHECK, FOUND SEVERAL CHERRY FASTENERS IN UPSIDE DOWN HAT SECTION FROM STA 606 TO 659 AND BETWEEN KEEL AND STRINGER 29R. RE-INSTALLED MS20470AD6 RIVETS PER DRAWING 5911418. INSTALLED RIVETS PER SRM 51-30-2. SUBSTITUTED HL326-6 FOR NASDR AT0000057Light · failedFOUND TAIL CONE LEFT STAIR EMERGENCY LIGHT WOULD NOT ILLUMINATE. RELAMPED UNIT IAW DC9 MM 33-50.SDR AT0000052Frame · corrodedDURING A SCHEDULED INSPECTION AT TIMCO IN LAKE CITY FL, FOUND CORROSION ON FRAME AT BS 237 LONGERON 30. AFTER REMOVAL OF CORROSION, FOUND FRAMEOUT OF LIMITS. REMOVED AND REPLACED DAMAGED SECTION OF FRAME AT BS 237 LONGERON 30 IAW DC9 SRM 5 3-01 FIG 1, 53-03 SDR ABXA000073Battery · dischargedEMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES.SDR AT0000046Frame · corrodedFOUND AFT PIT LONGERON CORRODED AT BS 832 ALONG FRAME. REMOVED CORROSION, TREATED, ALODINED AND PRIMED IAW DC9 SRM 53-01 FIGURE 1, TABLE 2, 51-10-3.SDR AT0000038Strut · dischargedFOUND LANDING GEAR UPLATCH RELEASE OR GROUND SHIFT DID NOT WORK AND WOULD NOT RAISE. ON FINAL AT BUF (BUFFALO). GROUND SHIFT OR THE UPLATCH RELEASE WAS HEARD TO HAVE RELEASED. PERFORMED GEAR SWING. NOSE LANDING GEAR FOUND TO BE UNDER SERVICED WITH FLUID ANSDR AT0000036Gcu · inoperativeFOUND LEFT GENERATOR FAILED AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED SMELL OF SMOKE IN CABIN AFTER TAKEOFF. REMOVED AND REPLACED GENERATOR CONTROL UNIT. RAN ENGINE PACKS, COULD NOT DUPLICATE SMOKE SMELL..SDR MWEA00030Slide · dislodgedGALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE CAME LOOSE. MAINTENANCE REINSTALLED EVACUATION SLIDE.SDR MWEA00026Slide · dislodgedMAIN CABIN DOOR EMERGENCY EVACUATION SLIDE FELL OUT OF COVER. MAINTENANCE REINSTALLED SLIDE PACK INTO COVER.
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