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 96ZZZM194Floor Beam · corrodedSTL - DURING OP-15, FOUND CORROSION AT TOP OF SCREW HOLE ON FLOOR BEAM OUTBOARD WALL OF RIGHT LAV, STATION 980. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER ARA 10024.SDR 96ZZZM191Skin · crackedSTL - DURING OP-15, FOUND A TWO INCH CRACK IN FUSELAGE SKIN, FORWARD OF FIRST OFFICERS WIPER BLADE POST. REPAIRED PER ARA 10023. (M)SDR 96ZZZM181Bulkhead · crackedSTL - DURING OP-15, FOUND .25 INCH CRACK IN AFT RIGHT LAVATORY FORWARD BULKHEAD, AT OUTBOARD CORNER AT FLOOR LINE. REPAIRED LAVATORY BULKHEAD PER SRM 53-03, FIGURE 31.SDR USAAD9500AHeat Controller · failedBOS - FLT 1204 - EN ROUTE PHL-PWM, THE OUTER PANE OF THE CAPTAIN'S WINDSHIELD BEGAN TO ARC AND CRACK. FLIGHT DIVERTED TO BOS AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD AND THE WINDSHIELD HEAT CONTROLLER. (X)SDR ABXA9600388Skin · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE LEFT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL THAT WAS NOT IAW THE DC-9 SRM. REPAIRED LEFT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL IAW ABX REA D955-13859-MR.SDR ABXA9600382Skin · gougedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE LEFT FORWARD FUSELAGE SKIN PANEL CREASED, DENTED AND GOUGED AT FS 229 AND LONGERON 19L. REPAIRED LEFT FORWARD FUSELAGE SKIN PANEL IAW ABX REA D953-13827-MR.SDR 9521909997Light · brokenDURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT BROKEN ON THE LEFT SIDE OF THE AFT FLIGHT ATTENDANT SEAT. REPLACED LIGHT ASSEMBLY AND OPERATIONAL CHECK GOOD.SDR 9521849936Door Jamb · corrodedDURING L-CHECK, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB PAN SPLICE JOINTS. REPAIRED PAN (P/N 5912494-501) PER EA 99-103354.SDR ABXA9600383Skin · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE FORWARD UPPER FUSELAGE SKIN AT LONGERON 1 FROM FS 250.0 TO 319.0 THAT WAS NOT PER THE DC-9 SRM. REPAIRED FUSELAGE SKIN IAW ABX REA D953-13828-MR.SDR ABXA9600376Floor Beam · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND A FLOOR BEAM AT FS 313 CORRODED AND BLENDED BEYOND LIMITS. REPAIRED FLOOR BEAM IAW ABX REA D953-13766-MR.SDR 96ZZZM197Door Pan · crackedDURING OP-15, FOUND THREE CRACKS, 1.5 INCH EACH, IN RIGHT FORWARD OVERWING EXIT DOOR PAN, UPPER AFT AND BOTH TOP CLIPS. INSTALLED DOUBLERS AND REPAIRED PER SRM 52-05, FIGURE 51 AND ARA 8897. (M)SDR ABXA9600390Blkhd Tee · reqd trimDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THAT WHEN REPLACING THE AFT PRESSURE BULKHEAD LOWER TEE, THERE WAS A REQUIREMENT TO TRIM 1.0 INCH FROM THE TEE SECTION VERTICAL LEG. REPAIRED THE AFT PRESSURE BULKHEAD LOWER TEE IAW ABX REA D953-13901-MR.SDR 9521719968Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERWING EMERGENCY EXIT LIGHTS VERY WEAK. REPLACED BATTERIES. OPERATIONAL CHECK GOOD.SDR 9521709936Slide · low batteryDURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED BATTERY CHECK. REPLACED SLIDE. OPERATIONAL CHECK GOOD.SDR USAA951363Skin · crackedPIT - WHILE ACCOMPLISHING X-RAY INSPECTION OF PYLON AREA IN BOS, MAINTENANCE DISCOVERED A .25 INCH CRACK IN SKIN AT STA 965, LONGERON 14L. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT FOR REPAIR. INTERIM EXTERNAL DOUBLER REPAIR INSTALLED PER USAIR EA NR 31838. ASDR ABXA9600405T-Cap · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 90-18-03; SB 57-98 OF THE LEFT WING MAIN FRAME T-CAP, FOUND NUMEROUS CORRODED FASTENERS, GOUGES AND CORROSION ON THE T-CAP BETWEEN AND UNDER STRINGERS 11 THROUGH 15, 16 TO 17, 19 TO 20, 20 TO SDR ABXA9600385T-Cap · corrodedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS WHILE COMPLYING WITH AD 90-18-03 AND SB 57-98 ON THE LEFT WING, FOUND CORROSION INSIDE BARREL NUT HOLE NR 14 AT THE MAIN FRAME T-CAP AT STA XCW 58.5. REPAIRED LEFT WING T-CAP IAW ABX REA D957-13835-MR.SDR ABXA9600379Door Jamb · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE AFT LOWER CARGO DOOR JAMB PAN THAT WAS NOT IAW THE DC-9 SRM. REPAIRED IAW ABX REA D953-13785-MR.SDR ABXA9600378Frame · damagedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND AN EXISTING REPAIR ON THE AFT LOWER CARGO DOOR JAMB PAN THAT WAS NOT IAW THE DC-9 SRM. REPAIRED AFT LOWER CARGO DOOR JAMB PAN IAW ABX REA D953-13785-MR.SDR 9521729903Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.SDR 9521679970Strut · reqd serviceLANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF DUE TO GROUND SHIFT FAILURE. FLIGHT CONTINUED TO DESTINATION (MSP) AND LANDED WITHOUT INCIDENT. NOTE: EMERGENCY EQUIPMENT WAS CALLED OUT AS A PRECAUTIONARY MEASURE. CYCLED GEAR SEVERAL TIMES. ALL CHECKED NORMASDR 9521689903Green Light · malfunctionedON APPROACH INTO DTW, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. CYCLED GEAR SEVERAL TIMES. ALL CHECKED NORMAL. PROBLEM COULD NOT BE DUPLICATED.SDR 9521439944Nav Instruments · failedSEVERAL COCKPIT NAVIGATION INSTRUMENTS FAILED AFTER TAKEOFF FROM DTW. FLIGHT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. PERFORMED TEST OF INDIVIDUAL COMPONENTS AND ALL SYSTEMS CHECKED NORMAL. PROBLEM COULD NOT BE DUPLICATED AND AIRCRAFT RETURNED TO SERVICSDR 9521179909Pt7 Line · brokenNR 2 ENGINE EPR INDICATION WAS LOW ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE REPLACED A BROKEN PT7 LINE WITH A NEW PART.SDR GTIA96NK041Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y988 AND STATION Y996, LONGERONS 29 RIGHT TO 29 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04, FIG 9 PAGE 23. (M)SDR GTIA96NK040Skin · corrodedDURIGN C-CHECK, FOUND FUSELAGE SKIN SECTION FROM STATION Y667 TO STATION Y756, LONGERONS 28 LEFT TO 28 RIGHT CORRODED. REPLACED FUSELAGE SKIN SECTION IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2. (M)SDR GTIA96NK039Skin · corrodedDURIGN C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y576 AND STATION Y591, LONGERONS 28 RIGHT TO 28 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW COOPESA DWG HSE9-53-256 DATED DEC 4, 1995 AND FAA FORM DATED DEC 5, 1995. (M)SDR GTIA96NK038Frame · corrodedDURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y579 BETWEEN LONGERONS 27 RIGHT AND 27 LEFT CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEET 1 PAGE 4A. (M)SDR GTIA96NK037Door Pan · crackedDURING C-CHECK, FOUND LEFT WHEEL WELL DOOR PAN INBOARD AFT SECTION CRACKED. REPAIRED LEFT WHEEL WELL DOOR PAN INBOARD AFT IAW COOPESA DWG HSE9-52-261 DATED DEC 7, 1995. (M)SDR GTIA96NK036Bulkhead Web · corrodedDURING C-CHECK, FOUND FUSELAGE BULKHEAD WEB AT STATION Y996 FROM LONGERONS 23 RIGHT TO 23 LEFT AND BETWEEN -Z210 AND -Z240 CORRODED. REPLACED FUSELAGE BULKHEAD WEB IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2, SRM 51-30-5. (M)SDR GTIA96NK035Frame · crackedDURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y1038 AND LONGERON 13 LEFT CRACKED. REPAIRED FUSELAGE FRAME IAW SRM 53-01 FIG 2 SHEET 2. (M)SDR GTIA96NK034Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN SECTION FROM STATION Y667 TO STATION Y756, LONGERONS 28 RIGHT TO 28 LEFT CORRODED. REPLACED FUSELAGE SKIN SECTION IAW SRM 51-01 PARAGRAPH C AND SRM 51-30-2. (M)SDR GTIA96NK033Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y589 AND STATION Y607, LONGERONS 17 RIGHT TO 19 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW COOPESA HSE9-53-263 DATED DEC 11, 1995 AND FAA FORM 8110-3 DATED DEC 11, 1995. (M)SDR GTIA96NK032Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y432 AND STATION Y465, LONGERONS 28 LEFT TO 29 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04 FIG 44 SHEET 1. (M)SDR GTIA96NK031Bulkhead Tee · corrodedDURING C-CHECK, FOUND FUSELAGE BULKHEAD T-CHORD SECTION AT Y604 BETWEEN LONGERONS 28 RIGHT AND 28 LEFT CORRODED. REPAIRED FUSELAGE T-CHORD SECTION IAW DOUGLAS FAX ACTION NR 284374 DATED DEC 6, 1995 AND MD DWG 5934768 VIEW 'C' ZONE 3 AND VIEW 'B' ZONES 8 AND 9SDR GTIA96NK030Frame · corrodedDURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y1132.6 AND LONGERON 16 LEFT CORRODED AND WORN. REPAIRED FUSELAGE FRAME IAW SRM 53-01 FIG 2 SHEET 4 PAGE 9. (M)SDR GTIA96NK029Seat Track · corrodedDURING C-CHECK, FOUND PAX SEAT TRACKS FROM FS Y200 TO FS Y256 AT PLUS X23 AND -X47 CORRODED. REPAIRED PAX SEAT TRACKS IAW SRM 53-05 FIG 4 SHEET 1. (M)SDR GTIA96NK028Door Beam · crackedDURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 6 REAR SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 6 REAR SECTION IAW SRM 52-05 FIG 31 SHEET 13 SECTION AC-AC PAGE 185. (M)SDR GTIA96NK027Door Beam · crackedDURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 6 FORWARD SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 6 FORWARD SECTION IAW SRM 52-05 FIG 31 SHEET 7 SECTION MM PAGE 193. (M)SDR GTIA96NK026Jamb · crackedDURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR JAMB AT UPPER AFT CORNER CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR JAMB AT UPPER AFT CORNER IAW SRM 53-05 FIG 26A PAGE 62A. (M)SDR GTIA96NK025Frame · crackedDURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y408 BETWEEN LONGERONS 25 LEFT AND 30 CRACKED AND CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEETS 1 TO 5. (M)SDR GTIA96NK024Fairing · delaminatedDURING C-CHECK, FOUND FORWARD ADF LEFT ANTENNA FAIRING DEFECTIVE DUE TO DELAMINATION. REPAIRED FORWARD ADF LEFT ANTENNA IAW COOPESA DWG HSE-9-53-270 DATED DEC 15, 1995 AND FAA FORM 8110-3 DATED DEC 15, 1995. (M)SDR GTIA96NK023Frame · corrodedDURING C-CHECK, FOUND FUSELAGE FRAME AT STATION Y917 BETWEEN LONGERONS 26 LEFT AND 29 RIGHT CORRODED. REPAIRED FUSELAGE FRAME IAW SRM 53-03 FIG 2A SHEET 1 PAGE 4A. (M)SDR GTIA96NK022Fairing · delaminatedDURING C-CHECK, FOUND FORWARD RIGHT ADF ANTENNA FAIRING DEFECTIVE DUE TO DELAMINATION. REPAIRED FORWARD RIGHT ADF ANTENNA IAW COOPESA DWG HSE9-53-262 DATED DEC 8, 1995 AND FAA FORM 8110-3 DATED DEC 11, 1995. (M)SDR GTIA96NK021Door Beam · crackedDURING C-CHECK, FOUND PAX CABIN MAIN ENTRY DOOR BEAM NR 2 AFT SECTION CRACKED. REPAIRED PAX CABIN MAIN ENTRY DOOR BEAM NR 2 AFT SECTION IAW SRM 52-05 FIG 31 SHEET 13 SECTION AA-AA PAGE 185. (M)SDR GTIA96NK020Longeron · corrodedDURING C-CHECK, FOUND FUSELAGE 30 LONGERON SECTION FROM STATION Y563 TO STATION Y604 CORRODED. REPLACED FUSELAGE 30 LONGERON SECTION IAW COOPESA DWG HSE9-53-247, FAA FORM 8110-3 NR 95113 DATED NOV 30, 1995, AND FAA FORM 8110-3 NR 95112 DATED NOVE 30, 1995. (SDR 9521489956Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND OPERATIONAL CHECK NORMAL.SDR 9521429991Uplock Switch · malfunctionedDURING CLIMBOUT, NOSE LANDING GEAR GREEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR WITH NO CHANGE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR UPLOCK SWITCH. ALSO, REPLACED NOSE GEAR GREEN SAFE AND RED UNSAFE LIGHSDR 9521229947Wire · brokenDURING APPROACH, THE NOSE LANDING GEAR SAFE LIGHT DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. A DOWNLOCK CHECK WAS PERFORMED WHICH VERIFIED THE NOSE LANDING GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED BROKEN WIRE FROM DOWNLOCK SDR ABXA9600412Angle · crackedDURING C AND D-CHECK ACCEPTANCE INSPECTIONS, FOUND THE FLOOR BEAM ATTACH ANGLE AT FS 69L CRACKED. REPLACED THE ATTACH ANGLE AT FS 69 IAW DC-9 SRM CHAPTER 51-30-5.
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