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 9519249603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING TANK FITTING, WS 69 AT STR 22. REPLACED FITTING PER SRM 51-00.SDR 9518739942Battery Pack · dischargedDURING LINE CHECK, FOUND ALL FLOOR EMERGENCY TRACK LIGHTS INOPERATIVE. REPLACED FORWARD POWER SUPPLY, ALL FOUR BATTERY PACKS AND OPERATIONAL CHECK GOOD.SDR 95ZZZM758Structure · damagedUPON ARRIVAL OF FLT 306, MIA-IAD, MX FOUND THE TAIL SKID AND SURROUNDING STRUCTURE DAMAGED APPARENTLY FROM GROUND CONTACT. INSPECTED AND FERRIED AIRCRAFT TO LACI, ID 7A1 FOR STRUCTURE REPAIR. PERFORMED NECESSARY REPAIRS TO STRUCTURE AND SKID IAW SRM 53-01, 5SDR 9518769922Battery Pack · dischargedDURING LINE CHECK, FOUND BOTH AFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK GOOD.SDR 9518539926Pressurization · malfunctionedDURING TAKEOFF, THE AIRCRAFT STARTED TO PRESSURIZE NEGATIVELY. PROBLEM CONTINUED DURING CLIMB AND COULD NOT CONTROL CABIN MANUALLY. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE DIFFERENTIAL PRESSURE SENSOR, OUTFLOW VALVE ACTUATOR, AND SDR CAL951060Angle · crackedIAH - INSPECTION FOUND A .75 INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE, LT SIDE. A REPAIR WAS PERFORMED IAW SRM 53-05, FIGURE 23A. (X)SDR CAL951050Connector · wiring pulledFLT NR 1401 - IAH - THE LEFT MLG HAD NO TRANSIT LIGHT OR GEAR DOWN LIGHT WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. THE CHECKLIST WAS COMPLIED WITH, A TOWER FLY-BY WAS PERFORMED, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WIRING PULLED OUT OSDR 9518709603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE BS 200 FLOORBEAM ATTACH FITTING AT LONGERON 18R. REPLACED FITTING PER SRM 51-30-0.SDR 9518469984Clips · out of adjustDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR TAILCONE HANDLE FROM THE CLIPS AND THAT THE TAILCONE DID NOT DROP. ALSO, FOUND A FRAYED RELEASE CABLE AND TWO WORN GUIDE PINS. REPLACED THE CABLE AND PINS, REMOVED THE SEALANT FROM SDR MWEA95432Slide Pin · fell outCREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE COVER RETAINING PIN FELL OUT. MAINTENANCE REPLACED EVACUATION SLIDE DOOR AND PIN, RETURNED A/C TO SERVICE.SDR ABXA9600165Intercostal · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND AN EXISTING REPAIR ON THE INTERCOSTAL AT FS 420, L19R CRACKED. REPAIRED IAW ABX REA D953-13439-MR.SDR 96ZZZM258Trap Frame · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY FL, FOUND CRACK AT BS 718 LEFT UPPER TRAPEZOIDAL FRAME. FAB AND INSTALLED PLATE IAW DC-9 SC 53-100 REV 5 AND DC-9 SRM 51-10-3. (M)SDR 9518699603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 30 END FITTING AT FS 756. REPLACED FITTING PER SRM 53-02, 51-30.SDR 9518689603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FS 603 FRAME TO TANK ATTACH FITTING, BETWEEN LONGERONS 19L TO 22L. REPLACED FITTING.SDR 9518679603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 25L AND 18R END FITTINGS AT THE FS 996 PRESSURE BULKHEAD. REPLACED FITTINGS PER SRM 51-30, 51-10-3, AND 53-02.SDR MWEA95430Frame · corrodedDURING D-CHECK, MAINTENANCE FOUND THE FRAME AT STA 446 FROM LONGERON 26R TO 26L HAS SEVERAL AREAS OF CORROSION. MAINTENANCE REPAIRED FRAME IAW SPLICE REPAIR PER SRM 53-03 FIG 2A.SDR MWEA95429Fitting · crackedDURING D-CHECK, MAINTENANCE FOUND LONGERON 28L HAS A CRACKED SPLICE FITTING AT STA 554. MAINTENANCE REMOVED AND REPLACED FITTING FROM STA 554 TO 579 PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95428Longeron · crackedDURING D-CHECK, MAINTENANCE FOUND LONGERON 29L IS CRACKED AT STA 415. MAINTENANCE REMOVED LONGERON FROM SPLICE AT STA 415 TO STA 579. FABRICATED SPLICE FROM 7074-T7351 AND LONGERON FROM 7075-T611. INSTALLED SPLICE AND LONGERON PER SRM 53-01 PG 1 AND AIRCRAFSDR MWEA95427Longeron · crackedDURING D-CHECK, MAINTENANCE FOUND LONGERON 30 IS CRACKED IN 3 PLACES. MAINTENANCE REMOVED AND REPLACED LONGERON FROM STA 229 TO 415 PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95426Skin · damagedDURING D-CHECK, MAINTENANCE REMOVED A TEMPORARY EXTERNAL SKIN REPAIR AT STA 300 TO 337 FROM LONGERON 24L TO 25L. INSTALLED A PERMANENT REPAIR FROM STA 287 TO 358 FROM LONGERON 24L TO 26L IAW ME53-149 SKETCH PER DAC TELEX ORD-SVC-0300/JSS.SDR MWEA95425Longeron · corrodedDURING D-CHECK, MAINTENANCE FOUND LONGERON 30 IS CORRODED IN SEVERAL AREAS FROM STA 415 TO 572. MAINTENANCE REMOVED AND REPLACED LONGERON PER SRM 51-30.SDR MWEA95424Intercostal · corrodedDURING D-CHECK, MAINTENANCE FOUND INTERCOSTAL AT LONGERON 29R BETWEEN STA 332 TO 351 HAS AREAS OF CORROSION. MAINTENANCE FABRICATED AND INSTALLED AN INTERCOSTAL OF 0.050 INCH 7075-T6 ALUMINUM PER SRM 51-30.SDR MWEA95423Longeron · corrodedDURING D-CHECK, MAINTENANCE FOUND LONGERON 29L IS CORRODED IN NUMEROUS AREAS FROM STA 229 TO 415. MAINTENANCE REMOVED AND REPLACED LONGERON PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95422Fitting · crackedDURING D-CHECK, MAINTENANCE FOUND END FITTING AT LONGERON 30 HAS A CRACK AT STA 571. MAINTENANCE REMOVED AND REPLACED FITTING FROM STA 571 TO 598 PER SRM 51-30.SDR MWEA95421Angle · corrodedDURING D-CHECK, MAINTENANCE FOUND TIP ANGLE OF LAVATORY FLOORBEAM AT STA 980 HAS A SMALL AREA OF CORROSION. MAINTENANCE INSTALLED REPAIR IAW SRM 53-05, FIG 2A.SDR GTIA96NK139Longeron · corrodedDURING C-CHECK, FOUND FORWARD CARGO COMPARTMENT LONGERON 30 WITH CORROSION BETWEEN Y359 AND Y389. REPLACED LONGERON 30 FROM Y356.7 TO Y415 IAW SRM 51-01, PARA C. INSTALLED TWO SPLICES IN LONGERON 30 FROM Y 356.7 TO Y415. INSTALLED RIVETS IAW SRM 51-30-2. (SDR CAL951114Longeron · crackedHOU - INSPECTION FOUND A .25 INCH CRACK IN LONGERON 17 AT RIGHT AFT LAV, STA 980. THE CRACKED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2A, SRM 51-30-2, AND SRM 51-30-5. (X)SDR ABXA9600164Skin · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FUSELAGE EXTERIOR SKIN CRACKED AT FS 160 AT THE MAIN ENTRY DOOR OPENING. REPAIRED FUSELAGE SKIN AT FS 160 IAW ABX REA D953-13277-MR.SDR 9518289601Eel Connector · looseDURING ROUTINE CHECK, FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE IN THE AFT FOUR ROWS OF THE AIRCRAFT. RECONNECTED CONNECTOR, OPERATIONAL CHECK GOOD.SDR MWEA95391Clips · crackedDURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY STA 980 ATTACH CLIPS ON FUSELAGE SKIN AT LONGERONS 14, 15 AND 16 HAVE .125 INCH CRACKS. MAINTENANCE FABRICATED AND INSTALLED CLIPS OF 0.050 INCH 2024-T3 ALUMINUM PER SRM 51-30. AIRCRAFT RETURNED TO SERSDR MWEA95390Clips · crackedDURING D-CHECK, MAINTENANCE FOUND THE RT LAVATORY STA 980 ATTACH CLIPS ON FUSELAGE SKIN AT LONGERONS 14, 15 AND 16 HAVE .125 INCH CRACKS. MAINTENANCE FABRICATED AND INSTALLED CLIPS OF 0.050 INCH 2024-T3 ALUMINUM PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95389Blkhd Clip · crackedDURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z34 CRACKED. MAINTENANCE FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95388Blkhd Clip · crackedDURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z-24 CRACKED. MAINTENANCE FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95387Blkhd Clip · crackedDURING D-CHECK, MAINTENANCE FOUND THE LEFT HAND LAVATORY PRESSURE BULKHEAD CLIP AT Z-14 CRACKED. FABRICATED AND INSTALLED A CLIP OF 0.032 INCH 2024-T3 ALUMINUM PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95386Floorbeam · corrodedDURING D-CHECK, MAINTENANCE FOUND THE FLOORBEAM TOP ANGLE IN AFT LAVATORY AREA AT STA 996 IS CORRODED. REPLACED TOP ANGLE PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95385Floorbeam · crackedDURING D-CHECK, MAINTENANCE FOUND THE FLOORBEAM AT STA 237 HAS A 4 INCH CRACK IN THE UPPER WEB 5 INCHES LEFT OF CENTERLINE. INSTALLED DOUBLER ON BEAM IAW SRM 53-05 FIG 73 PER DAC TELEX ORD-SVC-0218/PDG. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95384Longeron · corrodedDURING D-CHECK, MAINTENANCE FOUND LONGERON 25R AT STA 136 HAS AN AREA OF CORROSION BEYOND LIMITS. MAINTENANCE FABRICATED A DOUBLER SPLICE FROM 7637813-3 EXTRUSION AND INSTALLED PER SRM 53-01 PG 1. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95383Intercostal · corrodedDURING D-CHECK, MAINTENANCE FOUND THE INTERCOSTAL BETWEEN STA 218 AND 237, BETWEEN LONGERON 27R AND 28R CORRODED BEYOND LIMITS. MAINTENANCE FABRICATED AN INTERCOSTAL FROM .050 INCH 2024-T3 ALUMINUM AND INSTALLED PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95382Intercostal · corrodedDURING D-CHECK, MAINTENANCE FOUND THE INTERCOSTAL BETWEEN STA 218 AND 237 BETWEEN LONGERON 27L AND 28L CORRODED BEYOND LIMITS. MAINTENANCE FABRICATED AN INTERCOSTAL FROM .050 INCH 2024-T3 ALUMINUM AND INSTALLED PER SRM 51-30-2. AIRCRAFT RETURNED TO SERVICE.SDR MWEA95381Splice · crackedDURING D-CHECK, MAINTENANCE FOUND CRACKS IN LONGERON SPLICE AT LONGERON 2L AND 2R AT STA 1076. REMOVED AND INSTALLED SPLICE (P/N 3924814-501) PER SRM 51-30. AIRCRAFT RETURNED TO SERVICE.SDR CA960103519Receptacle · burnt(CAN)PRIOR TO DEPARTURE, BURNING SMELL DETECTED IN GALLEY AREA. CHECK OF AREA FOUND #18 OVEN RECEPTACLE BURNT. RECEPTACLE REPLACED.SDR 9518669940Fitting · crackedDURING MAINTENANCE CHECK, FOUND A CRACK IN THE LEFT WING FITTING STA 164 AT STR 20, OUTBOARD SIDE. REPLACED FITTING PER EA 99-10239.SDR 9518109613Bulb · missingDURING ROUTINE CHECK, FOUND TOP AND BOTTOM BULBS MISSING IN THE EMERGENCY EXIT LIGHT AT THE FORWARD ENTRANCE DOOR. INSTALLED BULBS AND OPERATIONAL CHECK GOOD.SDR 9518089987Eel Wire · brokenDURING LINE CHECK, FOUND FLOOR EMERGENCY LIGHTS INOPERATIVE IN AFT CABIN. REPAIRED WIRE AND OPERATIONAL CHECK GOOD.SDR CAL951119Blkhd Angle · crackedHOU - INSPECTION FOUND A .50 INCH CRACK IN OUTBOARD AFT PRESSURE BULKHEAD FORMER ATTACH ANGLE AT TEE CAP. THE CRACK WAS STOP DRILLED. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2. (X)SDR CAL951118Longeron · crackedHOU - INSPECTION FOUND A .50 INCH CRACK IN LONGERON 14L AT STA 965 BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 2. (X)SDR CAL951116Floor Beam · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN RIGHT SIDE FLOOR BEAM WEB AT STA 617. THE END OF WEB WAS CUT OFF AND A NEW WEB WAS SPLICED IAW SRM 53-01, FIGURE 4. (X)SDR CAL951115Skin · crackedHOU - INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN AT FORWARD SERVICE DOOR JAMB UPPER FORWARD CORNER AND A .25 INCH CRACK AT THE LOWER AFT CORNER. DOUBLER REPAIRS WERE INSTALLED IAW SRM 53-05, FIGURE 38. (X)SDR CAL951113Blkhd Stiffener · crackedHOU - INSPECTION FOUND A 1 INCH CRACK ON FORWARD BULKHEAD VERTICAL STIFFENER. THE CRACK WAS STOP DRILLED. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 4. (X)SDR CAL951042Downlock Switch · inoperativeAWS - FLT 0575 - WHEN THE GEAR WAS EXTENDED ON APPROACH TO AUS, THE RT REAR GREEN LIGHT AND RED UNSAFE LIGHT WERE BOTH ILLUMINATED. CYCLING THE GEAR WAS NO HELP. A TOWER FLY-BY WAS PERFORMED AND THE GEAR WAS VISUALLY CONFIRMED DOWN FOR A NORMAL LANDING. MAI
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