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 CALA9700196Longeron · corrodedINSPECTION FOUND LONGERON 28L CORRODED BETWEEN STA 230 TO 235. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.SDR CALA9700195Support · crackedINSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT FOR LEFT INBOARD FLOOR AT STA 680. THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-11-3.SDR CALA9700194Angle · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FLOOR ATTACH ANGLE AT STA 680. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-5.SDR CALA9700193Stiffener · crackedINSPECTION FOUND A .25 INCH CRACK IN STIFFENER BETWEEN LONGERON 2L AND 3L AT STA 996. THE CRACK WAS STOP DRILLED AND DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2.SDR CALA9700192Angle · crackedINSPECTION FOUND A .25 AND 1.5 INCH CRACK IN FLOOR SUPPORT ANGLE UNDER SEAT TRACK AT STA 658. THE FLOOR SUPPORT ANGLE WAS REPLACED IAW SRM 51-30-5.SDR CALA9700191Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 17R AT STA 960. A NEW LONGERON SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.SDR CALA9700190Longeron · crackedINSPECTION FOUND A .5 INCH CRACK IN LONGERON 17R AT STA 256. REPAIR SPLICES WERE INSTALLED IAW SRM 53-02, FIGURE 2.SDR ABXA9700733Floorbeam · gougedDURING C-CHECK, FOUND A CLIP AND FLOORBEAM GOUGED AT BL O AT FS 389. REPAIRED FLOORBEAM IAW ABX REA D953-17678-MR.SDR 97ZZZM238Latch Assembly · dirtyBOTH FORWARD SLIDES ARE HARD TO ARM AND DISARM. CLEANED UNDER LATCH ASSEMBLY ON SLIDE BAR. OPS CHECKED NORMAL. REFERENCE VJ970005.SDR 9701019924Batteries · dischargedDURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS AT TAILCONE, OVERWING EXITS, AND LEFT AFT AIRSTAIR AREA INOPERATIVE. CHARGED BATTERIES FOR TEN HOURS, OPERATIONAL CHECK NORMAL.SDR VJ970004Slide · low pressureR1 DOOR SLIDE BELOW PRESSURE RANGE. REPLACED DOOR SLIDE PER MM 25-62-0. (X)SDR VJ970003Power Supply · inoperativeEMERGENCY PATH LIGHTS FROM AFT OVERWING EXITS INOPERATIVE. REPLACED POWER SUPPLY PER MM 33-51-01 AND REPAIRED BROKEN WIRES. OPERATIONALLY CHECKED GOOD. (M)SDR ABXA9700790Angle · crackedDURING C-CHECK, FOUND FLOOR PANEL SUPPORT ANGLE CRACKED AT STA 639. REPLACED IAW DC9 SRM 51-30-2, DOUGLAS DWG. NR 5914617.SDR ABXA9700789Shear Tie · crackedDURING C-CHECK, FOUND CRACKED SHEAR TIE STA 890. REPLACED IAW DC9 SRM 51-30-2, 51-30-5, DOUGLAS DWG NR9915578.SDR 97ZZZM250Slide · malfunctionedCIT - FLT 851 - FORWARD CABIN DOOR SLIDE FELL OFF AND INFLATED WHEN DOOR WAS OPENED. REMOVED AND REPLACED FORWARD ENTRY DOOR SLIDE IAW MM 25-62. OK FOR SERVICE. INSPECTED INSTALLATION OF FORWARD ENTRY DOOR SLIDE PER MM 25-62-0. (M)SDR 97ZZZM227Trap Panel · crackedLEFT TRAP PANEL HAS CRACK INDICATIONS ALONG UPPER HORIZONTAL FLANGE BETWEEN AFT ATTACH BOLTS 3-4 AND 7-8 AND FORWARD BOLTS A-B AND AFT OF D. REF DC-9 SRM CHAPTER 57-09, FIG 6, SHEET 4. REPAIRED CRACKED PORTION OF LT FORWARD TRAP PANEL IAW DC-9 SRM 57-09, FIGSDR 9701219924Pressure Web · crackedDURING PERIODIC CHECK, FOUND PRESSURE PANEL IN NOSE WHEEL WELL CRACKED AT FS 106 UNDER OUTBOARD VERTICAL BEAM. INSTALLED REPAIR DOUBLER PER EA 99-112006.SDR ABXA9700793Frame · corrodedDURING C-CHECK, FOUND CORRODED FRAME STA 237 AT LONGERON 30. REPAIRED IAW DC9 SRM 53-03, FIGURE 2A.SDR ABXA9700784Cusp · corrodedDURING C-CHECK, FOUND CORRODED CUSP WEB BETWEEN STA 218 - 256, LEFT SIDE. REPLACED IAW DC9 SRM 51-30-2, 51-30-5, 51-30-1.SDR ABXA9700782Cusp · corrodedDURING C-CHECK, FOUND CORRODED CUSP WEB AT STA 313 - 389. REPAIRED IAW DC9 SRM 53-01, FIGURE 1, SHEET 3.SDR 9700839924Web · crackedDURING PERIODIC CHECK, FOUND PRESSURE PANEL IN NOSE WHEEL WELL CRACKED ABOVE FRAME AT FS 83 OUTBOARD EDGE. REPAIRED PER EA 99-112007.SDR VJ970002Light · inoperativeEMERGENCY LIGHTS INOPERATIVE AT AFT AIR STAIR. CLEANED ELECTRICAL TERMINAL NR 5 AT LEFT AFT AIR STAIR. OPERATIONALLY CHECKED GOOD PER MM 33-50. (M)SDR CA970129005Receptacle · shorted(CAN) ELECTRICAL SMELL DETECTED IN FLIGHT DECK. MAINTENANCE TROUBLESHOOTING FOUND #4 OVEN RECEPTACLE BURNT. OVEN RECEPTACLE REPLACED AND CHECKED SERVICEABLE.SDR ABXA9700787Fitting · corrodedDURING C-CHECK, FOUND LEVEL 2 CORROSION ON FLOOR TO FRAME ATTACH FITTING STA 313. REPLACED IAW DC9 SRM 51-30-1, 51-30-5.SDR 9700779926Skin · crackedDURING PERIODIC CHECK, FOUND RIGHT WING FIXED LEADING EDGE SKIN CRACKED AT WS 242. ACCOMPLISHED INTERIM REPAIR PER EA 99-120700.SDR VJ970147Doubler · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE RIGHT WING CORRODED ON RIGHT UPPER LANDING GEAR SUPPORT DOUBLER. CORROSION FOUND TO BE OUT OF LIMITS (.080 INCH) IAW DC9 SRM 57-03 FIG 27. REMOVED DOUBLER IAW DC9 SRM 51-30-0. DRILLED ANSDR CA970129002Fuel Indicator · inoperative(CAN) ELECTRICAL SMELL DETECTED AND RH FUEL QUANTITY INDICATOR FAILED. TROUBLESHOOTING OF SNAG REVEALED RH INDICATOR CIRCUIT BREAKER HAD POPPED. DEFECTIVE INDICATOR REPLACED AND SYSTEM CHECKED SERVICEABLE.SDR ABXA9700795Shear Tie · crackedDURING C-CHECK, FOUND VERTICAL SHEAR TIE CRACKED AT STA 980. REPAIRED IAW ABX REA D953-17666.SDR ABXA9700792Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED AT STA 852, LEFT SIDE. REPAIRED IAW ABX REA D953-17673-MR.SDR ABXA9700731Doubler · corrodedDURING C-CHECK, THE AFT FUSELAGE SKIN DOUBLER CORRODED AT THE AFT LOWER CARGO DOOR CUTOUT. REPLACED DOUBLER IAW DC-9 SRM CHAPTER 51-30-1.SDR ABXA9700728Clip · crackedDURING C-CHECK, FOUND FLOORBEAM TO CUSP TEE CLIP TO BE CORRODED AND CRACKED AT STA 996 AND LONG 18R, (AD 92-22-08). REPLACED CLIP IAW DC-9 SRM CHAPTER 51-30-5.SDR ABXA9700715Drive Link · crackedDURING C-CHECK, FOUND LEFT WING INBOARD SPOILER DRIVE LINK CRACKED (AD 85-01-03, 90-18-03). REPLACED DRIVE LINK IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-61-2.SDR VJ970001Battery · dischargedEMERGENCY EXIT LIGHTS AT EXIT 15AB, ROW 15, WERE INOPERATIVE. INSTALLED NEW OVERHEAD BATTERY PACK, OPERATIONALLY CHECKED NORMAL. (M)SDR CA970129001Air Valve · leaking(CAN) ON TAKEOFF, UNABLE TO RAISE NOSE GEAR AND NOSE GEAR LIGHT CAME ON. QUICK REFERENCE HANDBOOK CHECK LIST CARRIED OUT. ON ARRIVAL FOUND NOSE GEAR OLEO FLAT. NOSE GEAR SERVICED AND SCHRADER VALVE REPLACED.SDR ABXA9700900Vane · delaminatedTHE RIGHT WING CENTER FLAP VANE HAD DELAMINATION ON THE UPPER MID SURFACE BETWEEN RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9700881Vane · gougedTHE RIGHT WING INBOARD FLAPS VANE WAS GOUGED AT THE MID RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9700879Spoiler · corrodedTHE LEFT INBOARD SPOILER HAD SCATTERED AREAS OF CORROSION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR ABXA9700724Skin · bulgedDURING C-CHECK, FOUND FUSELAGE SKIN BULGED STA 980 LONGERON 26L, (AD 92-22-08). REPLACED LOWER FUSELAGE SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.SDR ABXA9700723Skin · bulgedDURING C-CHECK, FOUND FUSELAGE SKIN BULGED AT STA 996 LONGERON 23L, (AD 92-22-08). REPLACED LOWER FUSELAGE SKIN PANEL IAW DC-9 SRM CHAPTERS 51-30-1, 51-30-2 AND 51-30-5.SDR 97ZZZX1069Water Line · failedDURING FLIGHT, THE AIRCRAFT'S AILERONS MOMENTARILY BECAME JAMMED. UPON LANDING, THE LEFT WING SPOILERS DID NOT DEPLOY. INSPECTION REVEALED THE CABIN POTABLE WATER LINE BURST DUE TO BEING PREVIOUSLY FROZEN, LEAKING WATER ACCUMULATED AT THE SLANT BULKHEAD AREASDR TWAA9708002Bulbs · failedSTL - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LEFT MAIN LANDING GEAR DID NOT INDICATED DOWN AND LOCKED. USED VISUAL GEAR CHECK. FOUND LIGHT BULBS BURNED OUT, MFG P/N MS25231-313. REPLACED LIGHT BULBS. LANDING GEAR INDICATION THEN CHECKED NORMAL. (SDR 9700579942Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON LOWER RIGHT WING BETWEEN WS 111.5 AND 164, STR 15. MADE INTERIM REPAIR PER EA 99-112008.SDR 9700529610Strut · reqd serviceLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NOSE GEAR STRUT LOW. SERVICED STRUT TO PROPER LEVELS, OPERAITONAL CHECK NORMAL.SDR 9700519917Retract Mech · lack of lubeLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF AND CABIN DID NOT PRESSURIZE. GROUND SHIFT FAILED TO SHIFT TO FLIGHT MODE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SEVERAL TIMES ON GROUND. DISCREPANCY COULD NOT BE DUPLICATEDSDR TWAA9707002Battery Pack · dischargedSTL - DURING LANDING CAPTAINS EMERGENCY LIGHT WAS INOP. REMOVED AND REPLACED BATTERY PACK, MFG P/N 5956904-1B062. OPERATIONAL CHECK NORMAL. (M)SDR ABXA9700799Floor Support · corrodedDURING C-CHECK, FOUND CORRODED FLOOR SUPPORT AT STA 218. REPLACED FLOOR SUPPORT IAW DC9 SRM 51-30-5.SDR ABXA9700796Panel · delaminatedDURING C-CHECK, FOUND BONDED PANEL BELOW ANTI-SKID VALVES DELAMINATED. REPLACED PANEL IAW DC9 SRM 51-30-1.SDR 9700739940Epr Transmitter · malfunctionedAS TAKEOFF POWER WAS APPLIED, BOTH ENGINE EPR INDICATIONS FROZE AT 1.60. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTERS FOR BOTH ENGINES. OPERATIONAL CHECK OK.SDR 9700729940Pt7 Line · water contamAS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE EPR INDICAITON DID NOT RESPOND. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED MOISTURE FROM THE PT7 LINES, OPERATIONAL CHECK OK.SDR 9700499608Slide · low pressureDURING PERIODIC CHECK, FOUND FORWARD GALLEY DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE.
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