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 ABXA9500958Web · cutDURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.SDR ABXA9500957Web · cutDURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.SDR ABXA9500956Web · cutDURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.SDR 9522019601Frame · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE TAIL SECTION LEFT HAND FRAME FS 1168. REPAIRED FRAME (P/N 9911843-5), PER EA 12-5310-9-C0608.SDR 9521989601Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT AND RIGHT WING LOWER SKIN PANELS. REPAIRED SKIN (P/N 5910465), PER EA 12-5720-9-C0494.SDR 9515559601Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT FLAP INBOARD FIXED VANE TIE FITTING. REPLACED FITTING PER SRM 51-30-2.SDR ABXA9600153Spar Web · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING REAR SPAR LOWER VERTICAL LEG CORRODED JUST INBOARD OF THE OUTBOARD FLAP HINGE FITTING. REPAIRED LEFT WING REAR SPAR IAW ABX REA D957-13003-MR.SDR ABXA9500970Floorbeam · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON FLOORBEAM AT STA 389 AT RBL 44. REPAIRED IAW ABX REA D953-13029-MR.SDR ABXA9500969Skin · damagedDURING C-CHECK INSPECTION, FOUND A DENT WITH A GOUGE IN FUSELAGE SKIN STA 168, LONGERON 19R. REPAIRED IAW ABX REA D953-12980-MR.SDR ABXA9500967Skin · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON FUSELAGE SKIN IN AREA OF NR 2 ADF LOOP ANTENNA, STA 298.5, BETWEEN LONGERON 1 AND 2L. REPAIRED IAW ABX REA D953-12973-MR.SDR ABXA9500966Skin · damagedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED WITH A GOUGE AT STA 206, LONGERON 19R. REPAIRED IAW ABX REA D953-12989-MR.SDR 9515109984To Warning Sw · malfunctionedWHEN ADVANCING POWER FOR TAKEOFF, TAKEOFF WARNING HORN SOUNDED WITH FLIGHT SURFACES IN CORRECT POSITION. THE TAKEOFF WAS ABORTED. REPLACED THE TAKEOFF WARNING SWITCH, OPERATIONAL CHECK GOOD.SDR CAL950931Angle · corrodedHOU - INSPECTION FOUND CUSP ANGLE CORRODED ON LOWER FRAME AT FS 990, LEFT SIDE. THE CORRODED SECTION OF CUSP ANGLE WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-05, FIGURE 25. (M)SDR ABXA9500978Skin · dentedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 80, LONGERON 18. REPAIRED IAW ABX REA D953-12995-MR.SDR ABXA9500965Floorbeam · gougedDURING C-CHECK INSPECTION, FOUND FLOORBEAM STA 389, GOUGED. REPAIRED IAW ABX REA D953-13009-MR.SDR ABXA9500964Skin · damagedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DAMAGED AT THE FORWARD EDGE OF THE ALC DOOR CUTOUT. REPAIRED IAW ABX REA D953-13004-MR.SDR MWEA95348Slide Cover · fell offCREW REPORTED PASSENGER ENTRANCE DOOR SLIDE COVER FELL OFF. MAINTENANCE RESECURED SLIDE COVER. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95342Evac Slide · low preasureDURING SERVICE CHECK, THE TAIL EVACUATION SLIDE PRESSURE WAS FOUND LOW, 2400 PSI. MAINTENANCE REMOVED AND REPLACED TAIL EVACUATION SLIDE IAW DC9 MM, RETURNED A/C TO SERVICE.SDR ABXA9600139Fitting · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT ENGINE PYLON INTERIOR FITTING CRACKED AT FS 1038 ABOVE THE ELECTRICAL CONNECTORS. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR ABXA9600128Linkage · brokenDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINKAGE BROKEN. REPLACED ROD ASSEMBLY IAW DC-9 MM 21-10-6.SDR ABXA9500972Skin · damagedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED WITH A GOUGE AT STA 189, LONGERON 19R. REPAIRED IAW ABX REA D953-12988-MR.SDR ABXA9500968Skin · damagedDURING C-CHECK INSPECTION, FOUND FUSELAGE SKIN DENTED AND GOUGED AT STA 937, LONGERON 23. REPAIRED IAW ABX REA D953-12993-MR.SDR ABXA9500963Blkhd Skin · damagedDURING C-CHECK INSPECTION, FOUND DAMAGE AT FORWARD SIDE OF AFT PRESSURE BULKHEAD SKIN. REPAIRED IAW ABX REA D953-13005-MR.SDR MWEA95347Door Jamb · corrodedDURING C-CHECK INSPECTION, FOUND THE AFT CARGO DOOR JAMB LOWER PAN CRACKED WITH CORROSION NEAR CENTER STOP. MAINTENANCE REPLACED LOWER PAN PER SRM 53-05, FIG. 44. RETURNED A/C TO SERVICE.SDR MWEA95346Angle · crackedDURING C-CHECK INSPECTION, FOUND THE AFT VENTRAL STAIR DOOR HAS A SUPPORT ANGLE CRACKED AT THE MID-SPAN. MAINTENANCE REMOVED AND REPLACED ANGLE AS PER SRM 51-30-2 AND SRM 51-30-3. RETURNED A/C TO SERVICE.SDR MWEA95345Skin · chafedDURING C-CHECK INSPECTION, FOUND FORWARD CARGO DOOR HANDLE CHAFING ON DOOR SKIN AT CUTOUT. MAINTENANCE INSTALLED REPAIR DOUBLER ON SKIN PER SRM 52-05, FIG. 30. A/C RETURNED TO SERVICE.SDR MWEA95344Eel Power Supply · failedDURING C-CHECK INSPECTION, FOUND EMERGENCY LIGHTS OVER BOTH LT AND RT FWD EMERGENCY EXITS ARE INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95343Intercostal · corrodedDURING C-CHECK INSPECTION, FOUND THE AFT CARGO COMPARTMENT INTERCOSTAL BETWEEN STATION 897 AND 937 JUST INBD OF DOOR JAMB HAS CORROSION. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE.SDR ABXA9500977Blkhd Skin · gougedDURING C-CHECK INSPECTION, FOUND A GOUGE IN THE AFT SIDE OF THE AFT PRESSURE BULKHEAD. REPAIRED IAW ABX REA D953-12990-MR.SDR ABXA9500961Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT WING TO FUSELAGE GUSSET ANGLE AT STA 48 CRACKED. REPAIRED IAW DC-9 SB 57-103.SDR ABXA9500946Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING TO FUSELAGE GUSSET ANGLE AT STA 48 CRACKED. REPAIRED IAW DC-9 SB 57-103.SDR 9521919601Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN AT THE ATC TRANSPONDER ANTENNA FS 180. REPAIRED SKIN PER EA 12-5330-9-C0533.SDR CA951129505Oil Panel · missing(CAN)RIGHT ENGINE OIL ACCESS PANEL FOUND MISSING. NEW PANEL INSTALLED.SDR ABXA9500976Blkhd Skin · gougedDURING C-CHECK INSPECTION, FOUND THE INLET DUCT GOUGED THE BULKHEAD SKIN AT STA 1046. REPAIRED IAW ABX REA D953-12991-MR.SDR ABXA9500975Frame · crackedDURING C-CHECK INSPECTION, FOUND MAIN FRAME STA 718 CRACKED ON RIGHT SIDE. REPAIRED IAW ABX REA D953-12966-SB.SDR ABXA9500950Skin · damagedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LIGHTNING STRIKES FROM STA 110 TO 218, LONGERON 26R. REPAIRED IAW DC-9 SRM 53-04 FIG 38.SDR ABXA9500949Angle · missingDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND SERVICE BULLETIN FITTINGS MISSING FROM NOSE LANDING GEAR DOORS. REPAIRED FITTINGS IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-4 AND INSTALLED DOUBLERS IAW EA NR FS-53-03529-MA.SDR ABXA9500948Skin · dentedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND DENT IN THE FUSELAGE SKIN AT STA 115, LONGERON 21L. REPAIRED IAW DC-9 SRM 53-04 FIG 38 VIEW 1.SDR CAL950906Frame · crackedHOU - INSPECTION FOUND A 3 INCH CRACK IN LEFT OVERHEAD FRAME IN FORWARD ACCESSORY COMPARTMENT AT STATION 37. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-05. (M)SDR CA951129503Receptacle · burnt(CAN)A BURNING ELECTRICAL SMELL WAS DETECTED IN THE GALLEY AREA. INVESTIGATION REVEALED #1 OVEN RECEPTACLE WAS BURNT. DEFECTIVE ELECTRICAL RECEPTACLE REPLACED.SDR ABXA9500974Frame · crackedDURING C-CHECK INSPECTION, FOUND MAIN FRAME STA 718 CRACKED ON LEFT SIDE. REPAIRED IAW ABX REA D953-12966-SB.SDR ABXA9500973Skin · req'd repairDURING C-CHECK AND PSE INSPECTIONS, FOUND PREVIOUS REPAIR AT FORWARD UPPER CORNER OF ENTRY DOOR CUTOUT. REPAIRED IAW ABX REA D953-12981-MR.SDR ABXA9500951Te Panel · delaminatedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND WING TRAILING EDGE PANEL FORWARD OF RIGHT AILERON DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2.SDR 9515209613Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT FLAP NR 3 WEDGE INBOARD T-FITTING. REPLACED FITTING PER SRM 51-30, 51-10.SDR 9514999607Strut · reqd serviceDURING CLIMB, LANDING GEAR WOULD NOT RETRACT, CREW FOLLOWED PROCEDURE AND LANDING GEAR RETRACTED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. UPON INSPECTION FOUND NOSE STRUT FLAT. SERVICED NOSE STRUT AND AIRCRAFT APPROVED FOR SERVICE.SDR MWEA95324Skin · crackedWHILE ACCOMPLISHING A VISUAL INSPECTION OF THE LOWER FUSELAGE SKIN IAW AD 85-03-08, A 1.5 INCH CRACK WAS FOUND AT STA 465 AND LONGERON 30. INSTALLED TEMPORARY REPAIR IAW SB A53-188 AND DAC DRAWING SB 09530188.SDR CAL950882Spar Web · crackedHOU - INSPECTION FOUND A 1.25 INCH CRACK IN RT WING SPAR WEB AT STA XCW 58.1. THE CRACK WAS ROUTED OUT IAW EA 5761-01003. (X)SDR ABXA9600175Door Jamb · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE FORWARD SERVICE DOOR JAMB INTERIOR LOWER AFT CORNER. REPLACED UPPER CUSP IAW DC-9 SRM 53-05 FIG 55.SDR ABXA9500952Angle · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND PANEL 110 SUPPORT ANGLE CRACKED. FABRICATED AND INSTALLED NEW ANGLE IAW PFEA NR PFE-D953-10918 AND DC-9 SRM 51-30-5.SDR ABXA9500947Pan · crackedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND UPPER FORWARD END OF SERVICE DOOR HOLD OPEN LATCH PAN CRACKED AT WELD. REPLACED LATCH PAN IAW DC-9 SRM 51-30-2.
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