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 CAL951140Floor Web · crackedIAH - INSPECTION FOUND A 1 INCH CRACK IN COCKPIT FLOOR WEB AT BS 89.050 AND A 2 INCH CRACK FOUND AT BS 83.550. THE FLOOR WEB WAS REPAIRED IAW ECRA 5310-03193 AND ECRA 531003031. (X)SDR 9520069919Retract Mech · lack of lubeDURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BIL AND LANDED WITHOUT INCIDENT. REMOVED AND LUBRICATED APEX BOLT ON NOSE LANDING GEAR TRUNNION LINK. OPERATIONAL CHECK GOOD.SDR 9519889916Battery Pack · dischargedDURING LINE CHECK, FOUND NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. OPERATIONAL CHECK GOOD.SDR CAL951159Former · crackedHOU - INSPECTION FOUND A 1.5 INCH CRACK IN SKIN CLIP (FORMER) AT STA 980 BELOW LONGERON 14R. THE CRACK WAS STOP DRILLED. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 5301, FIGURE 2, SHEET 4. (X)SDR CAL951158Belt Frame · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN BELT FRAME AT STA 980, LONGERON 16R. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4. (X)SDR 9519859922Fitting · crackedDURING LINE CHECK, FOUND A CRACK IN THE LEFT INBOARD FLIGHT SPOILER SUPPORT FITTING. REPLACED FITTING.SDR 9519729903Latch Mech · out of adjustDURING CLIMB OF TEST FLIGHT (GDC), THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND THE LEFT AND RIGHT UNSAFE LIGHTS ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. ADJUSTED BOTH THE LEFT AND RIGHT SDR 9519719920Eel Connector · looseDURING LINE CHECK, FOUND LEFT EMERGENCY FLOOR LIGHTS, ROWS 1-4, INOPERATIVE. REPAIRED ELECTRICAL CONNECTOR ON SERVICE DOOR EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.SDR 9519589917Eel · inoperativeDURING LINE CHECK, FOUND RIGHT FORWARD DOOR AND CENTER AISLE LIGHTS MALFUNCTIONING. REPLACED LIGHT AT RIGHT FORWARD DOOR AND OPERATIONAL CHECK GOOD.SDR 9519449916Eel Power Supply · inoperativeDURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND OPERATIONAL CHECK GOOD.SDR MWEA95438Vert Gyro · inopMKE - DURING CLIMBOUT, VERTICAL GYRO FLAG INTERMITTENTLY COMING INTO VIEW ON FIRST OFFICER'S ADI. FLIGHT RETURNED TO MKE. MAINTENANCE VERIFIED, REMOVED AND REPLACED NR 2 VERTICAL GYRO. OPS CHECK GOOD AND RETURNED A/C TO SERVICE.SDR 9519459609Eel Power Supply · inoperativeDURING LINE CHECK, FOUND LEFT ENGINE NACELLE LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND OPERATIONAL CHECK GOOD.SDR 9519569983Fuel Control · moisture contamNR 1 ENGINE EPR AND N1 WERE FLUCTUATING ON POWER LEVER CHANGES AFTER DEPARTURE. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE DRAINED THE FCU MOISTURE TRAP. SUBSEQUENT RUNUP WAS SATISFACTORY.SDR 96ZZZM28Fuel Heat Vlv · inopON FLT NR 248 - ATL- AIRCRAFT RETURN, AFTER DEPARTURE THE LEFT FUEL HEAT CAME ON AND STAYED ON, DID NOT EXCEED OIL TEMP LIMITS. REMOVE AND REPLACE FUEL HEAT VALVE ON LEFT ENGINE PER MM 73-11-2, OPS CHECK NORMAL. (M)SDR 9519499609Battery · dischargedDURING LINE CHECK, FOUND BOTH AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND OPERATIONAL CHECK GOOD.SDR 9519629917Door · crackedDURING M-CHECK, FOUND A CRACK IN THE AFT CABIN DOOR, LOWER LEFT SIDE. REPAIRED DOOR PER EA 99-102790.SDR MWEA95435Ac Inverter · inoperativeWHEN EMERGENCY POWER IS TURNED ON, AC EMERGENCY BUS OFF LIGHT ILLUMINATED AND AC EMERGENCY BUS IS NOT POWERED. REMOVED AND REPLACED EMERGENCY POWER.SDR 9519419925Longeron · corrodedDURING L-CHECK, FOUND CORROSION IN THE LONGERON 23L END FITTING AT FS 996. REPLACED FITTING PER SRM 51-30.SDR 9518929940Eel Power Supply · inoperativeDURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS FORWARD OF ROW 6 AND THE TWO EMERGENCY EXIT SIGNS BY THE MAIN CABIN DOOR AND SERVICE DOOR INOPERATIVE. REPLACED THE POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK GOOD.SDR CAL951067Latch Spring · lack of lubeFLT NR 1090 - ATL - THE LT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND THE GEAR DOOR OPEN LIGHT ILLUMINATED DURING UPLATCH CHECK. THE RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT EXTINGUISHED AFTER UPLATCH CHECK. 'ABNORMAL' PROCEDURES WESDR CA960103528Access Panel · missing(CAN)DURING WALK AROUND, FOUND THE RIGHT WING TIP NAVIGATION LIGHT ACCESS PANEL MISSING. NEW PANEL FITTED.SDR 9518939926Battery Pack · dischargedDURING LINE CHECK, FOUND CATWALK AND TAILCONE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK, OPERATIONAL CHECK GOOD.SDR 96ZZZM71Connector · looseFLT NR 229 - ATL-DFW - UPON GEAR EXTENSION LEFT MAIN GEAR DOOR UNSAFE LIGHT AND GREEN DOWNLOCK LIGHTS WERE INTERMITTENT. FOUND CANNON PLUG ON LEFT DOWN LOCK SWITCH LOOSE. SECURED CANNON PLUG AND SAFTIED IAW VALUJET MAINTENANCE MANUAL. (M)SDR 96ZZZM68Ddor · not latchedFLT NR 580 - ATL - AIRCRAFT RETURNED, WAS UNABLE TO PRESSURIZE AFTER TAKEOFF. NO DOOR LIGHTS ON AIRCRAFT. AIRCRAFT RETURNED TO GATE FOUND E/E DOOR OPEN. FOUND DOOR LIGHT SWITCH INOP. DEFERRED DOOR SWITCH FOR REPAIR, CLOSED DOOR DISPATCHED AIRCRAFT. CONTROSDR 9519689613Windshield · crackedDURING CLIMB, GDC-MSP AT 3000 FEET, THE LEFT WINDSHIELD HEAT SYSTEM BEGAN ARCING. THE SYSTEM WAS SHUT OFF AT WHICH TIME THE WINDSHIELD CRACKED. THE AIRCRAFT RETURNED TO GDC WITHOUT FURTHER INCIDENT. REPLACED THE WINDSHIELD AND HEAT CONTROLLER.SDR CA960103526Service Door · missing(CAN)ON WALK AROUND, FOUND #2 ENGINE OIL SERVICING DOOR MISSING. NEW DOOR FITTED.SDR CA960103525Access Panel · missing(CAN)DURING WALK AROUND, RIGHT ENGINE CSD SERVICE DOOR WAS FOUND MISSING. NEW DOOR INSTALLED.SDR MWEA95434Seat Belt · brokenDURING AN INTERIOR EQUIPMENT CHECK, A SEAT BELT BUCKLE ON A PASSENGER SEAT FELL OFF OF THE STRAP. MAINTENANCE REPLACED THE SEAT BELT ASSY AND OPERATIONALLY CHECKED IT OK FOR SERVICE.SDR CAL951065Csd Washer · brokenFLT 1804 - CLE - THE NR 1 ENGINE EXPERIENCED AN UNCOMMANED SHUT DOWN ON FINAL APPROACH TO CLE. THE LANDING WAS UNEVENTFUL. THE NR 1 ENGINE WAS REMOVED AND REPLACED. LEAK CHECK AND POWER ASSURANCE RUN WERE GOOD. SHOP FINDINGS REVEALED CSD REAR BEARING SHAFTSDR GTIANK018Longeron · crackedDURING C-CHECK, FOUND THE FUSELAGE LONGERON 25 LEFT BETWEEN STATION Y446 TO Y465 CRACKED. REPAIRED THE LONGERON 25 IAW SRM 53-02 FIG 2A. (M)SDR GTIA96NK115Skin · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT SKIN WITH LIGHT CORROSION BETWEEN Y756 AND Y775, LONGERON 26 LEFT AND LONGERON 28 LEFT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3. AREAS WITHIN LIMITS IAW SRM 53-04 FIG 38. (M)SDR GTIA96NK114Support · corrodedDURING C-CHECK, FOUND AFT CARGO COMPT FITTING SUPPORT FLOOR PANELS WITH CORROSION IN Y815 BETWEEN LONGERON 27 RT AND 28 RT. REMOVED CORROSION AND TREATED METAL IAW SRM 51-10-3, AREAS WITHIN LIMITS IAW SRM 53-01 FIG 1. (M)SDR GTIA96NK113Floor Beam · corrodedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR BEAM Y965.09 WITH CORROSION BETWEEN XO AND PLUS X58. REPAIRED FLOOR BEAM LOWER CHORD AT Y965.09 BETWEEN PLUS X6.7 TO PLUS X 18 AND BETWEEN PLUS 21.5 TO PLUS X535 IAW EO NR COO-9-53-138-95. (M)SDR GTIA96NK074Longeron · crackedDURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION, P/N 592030350, IN BETWEEN STATION Y756 TO STATION Y802 CRACKED. REPLACED LONGERON 30 IAW SRM 51-01 PARA C, SRM 51-30-2. THE FRAMES AT STATION Y775 AND STATION Y794 WERE CUT FOR ACCESS AND REPAIRED IAW SRM 5SDR GTIA96NK019Floor Beam · corrodedDURING C-CHECK, FOUND THE PAX/FLOOR BEAM LOWER CHORD AT STATION Y965.09 BETWEEN PLUS X6.7 TO PLUS X18 AND BETWEEN PLUS X21.5 TO PLUS 53.5 CORRODED. REPAIRED PAX/FLOOR BEAM LOWER CHORD AT IAW COOPESA DWG NO HSE9-53-140 REV A DATED NOV 12, 1995 AND FAA FORM 811SDR GTIA96NK017Fitting · corrodedDURING C-CHECK, FOUND FUSELAGE LONGERON 20 RIGHT END FITTING AT STATION Y996 CORRODED. REPLACED LONGERON 20 END FITTING IAW SRM 51-01 PARAGRAPH C AND SRM 51-10-2. (M)SDR GTIA96NK016Longeron · corrodedDURING C-CHECK, FOUND FUSELAGE LONGERON 30 SECTION BETWEEN STATION Y356.7 TO STATION Y415 CORRODED. REPLACED LONGERON 30 SECTION IAW SRM 51-01 PARAGRAPH C, SRM 51-30-2, SRM 53-02 FIG 14, DATED NOV 13, 1995 AND FAA FORM 8110-3 DATED NOV 13, 1995. (M)SDR GTIA96NK015Frame · crackedDURING C-CHECK, FOUND RIGHT CENTER OVER WHEEL FRAME, P/N 9919618-2N, AT STATION Y718, CRACKED. REPLACED RIGHT CENTER FRAME IAW MD S/B 53-131 REV 3, DATED FEB 11, 1988 OPTION 2, GROUP III, FIG 4. (M)SDR GTIA96NK014Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN SECTION AT PITOT STATIC PORT AREA BETWEEN STATION Y451 TO STATION Y465, LONGERONS 23 LEFT TO 26 LEFT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-04, FIG 31, SHEET 1. (M)SDR GTIA96NK013Longeron · corrodedDURING C-CHECK, FOUND FUSELAGE LONGERON 14 LEFT BETWEEN STATION Y1109 TO STATION Y1114 CORRODED. REPAIRED LONGERON 14 LEFT IAW SRM 53-02, FIG 2A. (M)SDR GTIA96NK012Frame · crackedDURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104 BETWEEN LONGERONS 10 LEFT TO 23 LEFT CRACKED. REPLACED FUSELAGE CANTED FRAME SECTION IAW ARM 51-01, PARAGRAPH C. (M)SDR GTIA96NK011Frame · crackedDURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104.937 BETWEEN LONGERON 10 RIGHT TO 16 RIGHT CRACKED. REPLACED FUSELAGE CANTED FRAME SECTION IAW SRM 51-01, PARAGRAPH C. (M)SDR GTIA96NK010Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN BETWEEN STATION Y1121 TO STATION Y1136, LONGERONS 20 RIGHT TO 21 RIGHT CORRODED. REPAIRED FUSELAGE SKIN IAW SRM 53-01, FIG 2, PAGE 8, SRM 51-30-2. (M)SDR GTIA96NK009Frame · crackedDURING C-CHECK, FOUND FUSELAGE CANTED FRAME SECTION AT STATION Y1104, LONGERON 4 LEFT CRACKED. REPAIRED FUSELAGE CANTED FRAME SECTION IAW SRM 53-01, FIG 2. (M)SDR GTIA96NK008Spar · corrodedDURING C-CHECK, FOUND LEFT AND RIGHT WING UPPER REAR SPAR CAP FLANGES AT RIGHT STATION XRS129 AND LEFT STATION XRS127.5 CORRODED. REWORKED LEFT AND RIGHT UPPER REAR SPAR CAP FLANGES IAW MCDONNELL DOUGLAS INSTRUCTION ON FILE 95-11-06-014/AJC00146 DATED NOV 8, SDR GTIA96NK007Panel · crackedDURING C-CHECK, FOUND RIGHT WING TRAILING EDGE FLAP CENTER PANEL OUTBOARD ATTACH FITTING AT XFS187 CRACKED. REPLACED RIGHT WING TRAILING EDGE FLAP CENTER PANEL OUTBOARD ATTACH FITTING IAW SRM 51-01, PARAGRAPH C AND SRM 51-30-2 AND FAA FORM 8110-3 DATED NOV 9,SDR GTIA96NK006Support · crackedDURING C-CHECK, FOUND RIGHT WING TRAILING EDGE FLAP LOWER FITTING SUPPORT AT XRS324.00 CRACKED. REPLACED RIGHT WING TRAILING EDGE FLAP LOWER FITTING SUPPORT IAW COOPESA DWG HSE9-57-242 DATED NOV 14, 1995 AND FAA FORM 8110-3 DATED NOV 14, 1995. (M)SDR CA960103521Elect Socket · shorted(CAN)STRONG ELECTRICAL BURNING ODOR DETECTED IN CABIN. INVESTIGATION REVEALED FLOURESCENT LIGHT SOCKET AT 1AB SIDEWALL HAD SHORTED. DEFECTIVE SOCKET REPLACED.SDR 9518729942Eel · inoperativeDURING LINE CHECK, FOUND FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. REPLACED DEFECTIVE EMERGENCY LIGHT ASSEMBLY AT FORWARD LEFT DOOR, OPERATIONAL CHECK GOOD.SDR 9522119608Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 813 AT LONGERON 26L. REPAIRED SKIN PER EA 99-103144.
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