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 MWEA98181Web · crackedA CRACK WAS FOUND ON THE INTERIOR WEB IN THE AFT UPPER CORNER OF MAIN CABIN DOOR. FABRICATED REPAIR DOUBLER IAW SRM 52-00 AND 52-11.SDR MWEA98180Fitting · crackedMAIN CABIN DOOR THE NR 1 BEAM AFT SUPPORT FITTING WAS FOUND CRACKED. INSTALLED NEW FITTING IAW SRM 51-30.SDR MWEA98179Fitting · corrodedMAIN CABIN DOOR THE END FITTING ON THE FORWARD END OF BEAM NR 3 WAS FOUND EXFOLIATED. INSTALLED NEW FITTING IAW SRM 51-30.SDR MWEA98178Beam · crackedNR 1 HORIZONTAL BEAM OF THE MAIN CABIN ENTRANCE DOOR WAS FOUND CRACKED AT THE FORWARD AND AFT ENDS. INSTALLED NEW BEAM IAW SRM 51-30.SDR 9802959941Fitting · crackedDURING M-CHECK, FOUND CRACK IN LONGERON 28R END FITTING AT FS 567. REPLACED END FITTING PER DWG 5911412 AND SRM 53-02.SDR 9802949941Fitting · crackedDURING M-CHECK, FOUND CRACK IN LONGERON 27L END FITTING AT FS 455. REPLACED END FITTING PER DWG 5911412 AND SRM 53-02.SDR TWAA9802902Longeron · crackedSTL - DURING OP 9 MAINTENANCE CHECK, LONGERON 5L WAS FOUND CRACKED AT CABIN FUSELAGE STA 718. REPLACED LONGERON 5L CRACKED SECTION PER SRM 53-02 FIG 18. ACFT TT: 75,771 HOURS. ACFT TC: 82,773. (X)SDR TWAA9802901Longeron · crackedSTL - DURING OP 9 MAINTENANCE CHECK, LONGERON 5L WAS FOUND CRACKED AT CABIN FUSELAGE STA 756. REPLACED LONGERON 5L CRACKED SECTION PER SRM 53-02 FIG 18. ACFT TT: 75,771 HOURS. ACFT TC: 82,773. (X)SDR CALA9800276Latch Mechanism · inoperativeUPLATCH CHECK WAS UNSATISFACTORY. THE LEFT GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS WERE ILLUMINATED. THE GEAR WAS RECYCLED AND RECHECKED, BUT WAS STILL UNSATISFACTORY. OPERATION WAS CONTINUED AT BELOW .70 MACH WITH RIGHT ENGINE HYDRAULICS ON HIGH. MAINTENANCSDR CA980305013Control Valve · inoperative(CAN) AIRCRAFT RETURNED DUE TO PRESSSURIZATION FAULT. CABIN CONTINUED TO CLIMB PAST 11,000 FEET, OXYGEN MASKS DEPLOYED. LEFT PACK WATER SEPARATOR TEMPERATURE CONTROL VALVE FOUND INOPERATIVE WHEN PACK IN OPERATION. VALVE REPLACED AND CHECKED SERVICEABLE.SDR 9802889614Wire · shortedDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS FOR TAILCONE PULL HANDLE INOPERATIVE. REPAIRED SHORTED WIRES UNDER WALKWAY AND REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR TWAA9809403Jamb · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT FORWARD SERVICE DOOR JAMB PAN DAMAGED AT BAYONET PICK-UP BRACKET ON CENTER AFT EDGE OF DOOR. INSTALLED REPAIR DOUBLER PER SRM 53-05, FIG 42. (X)SDR TWAA9809109Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 17L CRACKED AT LOWER FLANGE AT LONGERON TO FORMER FRAME ATTACH FASTENER. REMOVED AND REPLACED LONGERONS PER SRM 51-01, STANDARD PRACTICES, AND PER SRM 53-02-00, FIG 18 AND 53-03. (M)SDR TWAA9809107Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON NR 17R CRACKED AT LOWER FLANGE AT LONGERON TO FS 945 FORMER FRAME ATTACH FASTENER. REPLACED LONGERON PER SRM 51-01, AND SRM 53-02, FIG 18 AND 53-03. (M)SDR TWAA9809105Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK IN FORWARD FUSELAGE INTERCOSTAL TO FS 69.550 FORMER ATTACH 'T' ANGLE AT RBL 12 INCH. REPLACED 'T' ANGLE PER SRM 51-01, PAGE 2. (M)SDR TWAA9809102Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 2L CRACKED AT STATION 200. REPAIRED PER SRM 53-02, PAGE 48. (M)SDR TWAA9807201Skin · dentedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENTED BEYOND LIMITS AT FS 503, BETWEEN L26R AND L26R, 3 INCH BY 2 INCH BY .145 DEEP. REPAIRED PER SRM 53.04, FIG 38 SHEET 22. (M)SDR TWAA9807102Firewall Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK FOUND ON NR 2 PYLON AFT FIREWALL A ONE INCH CRACK IN UPPER FLANGE, AT OTBD END APPROX 40 INCHES AFT OF AFT ENGINE MOUNT. REPAIRED CRACKED ANGLE UPPER FLANGE ON AFT FIREWALL PER SRM 53-01. (X)SDR TWAA9806911Floorbeam · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND FLOORBEAM CRACKED AT STATION 617, APPROX 58.6 RBL. INSTALLED NEW FLOORBEAM PER SRM 51-01, PAGE 1 ITEM C AND SRM 51-30-0. (M)SDR MWEA98190Skin · peelingDURING INSPECTION, FOUND THE LT WING OUTBOARD TRAILING EDGE PANEL TOP SKIN PEELING BACK. MTC REPLACED SKIN IAW EA NR 57-006.SDR 9802879614So Valve · leakingDURING CRUISE ALTITUDE AT 29,000 FEET, RUDDER CONTROL MANUAL LIGHT BEGAN FLICKERING AND RIGHT HYDRAULIC SYSTEM WENT TO ZERO. FLIGHT WAS CONTINUED TO DESTINATION. CREW DECLARED AN YELLOW EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RSDR CALA9800269Sensor · inoperativeTHE RT AIR CONDITIONING SUPPLY TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF WITH SMOKE IN THE CABIN. THE AIRFOIL ICE PROTECTION WAS ON. THE PACK WAS TURNED OFF AND THE SMOKE DISSIPATED. THE RT ICE PROTECTION HIGH TEMP SENSOR WAS REMOVED AND REPLACED IAW MM 30-SDR 9802859614Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ALONG CATWALK INOPERATIVE. REPLACED POWER SUPPLY AT FS 1133, OPERATIONAL CHECK NORMAL.SDR MWEA98166Bracket · crackedCORNER BRACKET JUST FORWARD OF THE NR 2 PYLON AFT UPPER SPAR STRAP WAS FOUND CRACKED. INSTALLED REPLACEMENT PART IAW SRM 51-30.SDR MWEA98165Longeron · crackedLONGERON 25 LEFT WAS FOUND CRACKED FROM FS 1087 TO 1121. FABRICATED REPLACEMENT SECTION PER PRINT NR 5914468.SDR MWEA98164Splice · crackedLONGERON SPLICE AT LONGERON 30 BETWEEN FS 945 AND 965 WAS FOUND CRACKED. FABRICATED REPAIR SPLICE IAW PRINT 3913291.SDR MWEA98163Splice · crackedSPLICE FITTING ON LONGERON 28L BETWEEN FS 813 AND 832 WAS FOUND CRACKED. FABRICATED REPLACEMENT SPLICE PER PRINT 3913291.SDR MWEA98162Frame · damagedFRAME AT FS 370 WAS FOUND TO HAVE A TOOLING MARK IN THE UPPER RADIUS BETWEEN LONGERON 29L AND 30. FABRICATED REPAIR ANGLE IAW SRM 53-01 FIG 1 AND FIG 2.SDR MWEA98161Intercostal · damagedINTERCOSTAL AT BS 511 FOUND HOLE AND TOOLING MARKS. FABRICATED REPAIR ANGLES IAW 53-01.SDR MWEA98160Frame · misrepairedPREVIOUS REPAIR WAS ON AT FS STA 389 BETWEEN LONGERON 28L AND 29R NOT IAW SRM. FABRICATED REPAIR FILLER AND DOUBLERS IAW SRM 53-03 FIG 2A.SDR MWEA98159Panel · corrodedLEFT HAND WING SLAT ACCESS PANEL NR 1136A FOUND PITTING CORROSION ON THE OUTER SURFACE. REPAIRED IAW SRM 57-01 FIG 3.SDR CALA9801208Longeron · crackedINSPECTION FOUND LONGERON 17L CRACKED OUT OF UPPER AND LOWER FRAME ATTACH HOLES AT FS 945. THE LONGERON WAS REMOVED IAW SRM 51-10-2. A NEW LONGERON WAS FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, 51-10-4, 51-10-3, AND 51-30-5.SDR ABXA9800088Battery · dischargedEMERGENCY EXIT LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHTS BATTERIES.SDR 9802699919Fuse · blownDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 11 AND 13 INOPERATIVE. REPLACED BLOWN FUSE. OPERATIONAL CHECK NORMAL.SDR VJ9800129Floor · corrodedBOTTOM FLOOR PANEL 4410 CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. FABRICATED AND BONDED NEW PART IAW DC9 SRM 51-10-2 AND 51-70-3.SDR 9803079941Fitting · crackedDURING M-CHECK, FOUND CRACK IN END FITTING FOR LONGERON 29R AT FS 680. REPLACED FITTING PER SRM 51-30-2.SDR VJ9800134Plating · crackedFWD EDGE OF AFT CARGO DOOR DAMAGED AT SEAL RETAINER. TRIMMED CRACK AND COLD WORKED WRINKLE IAW REA 98131. FABRICATED TWO DOUBLERS FROM .063 T3 AL AND ONE FROM .032 TITANIUM. INSTALLED IAW BOEING SKETCH 98-03-02-011, SHEET 1, AND DC9 SRM 52-03, FIG 8, SHEET SDR VJ9800128Angle · corrodedLT DOOR JAMB ANGLE, AFT PSGR DOOR, FS 996, BL 20L, CORRODED. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-2.SDR VJ9800069Bracket · corrodedCENTER OF END BRACKET AT FS 218 FROM LONGERON 28L TO 27R CORRODED. FABRICATED NEW BRACKET. HEAT TREATED, DRILLED AND INSTALLED IAW DC9 SRM 51-10-2A, PG 1-24 AND 51-10-1-4, PG 1-24.SDR VJ9800068Floor · corrodedCENTER FLOOR PANEL AT FS 351 TO FS 446 CORRODED BEYOND LIMITS AT TOP SIDE AND BOTTOM EDGES OF SCREW HOLES. FABRICATED NEW FLOOR PANEL IAW DC9 SRM 51-10-4 AND 53-05, FIG 1.SDR VJ9800027Skin · crackedAS A RESULT OF GROUND DAMAGE SUSTAINED TO THE LT O/B SECTION OF THE WING, A 1.25 INCH HOLE WAS PUNCTURED IN L/E SKIN ASSY PANEL AT WING STA XRS540. HOLE CUT OUT, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIRS IAW AEROCORP EO 98-792, REV 1R, DATED 02/10/9SDR MWEA98158Wire · brokenDURING INSPECTION, FOUND LT NACELLE EMERGENCY LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK RETURNED AC TO SERVICE.SDR MWEA98155Battery Pack · dischargedDURING INSPECTION, FOUND LT NACELLE EMERGENCY LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK RETURNED AC TO SERVICE.SDR MWEA98154Skin · delaminatedDURING INSPECTION, FOUND LT WING TRAILING EDGE PANEL NR 1504A IS DELAMINATED ON OUTBOARD EDGES. MAINTENANCE REPAIRED IAW DAC DRAWING NR 9957499 AND SRM 51-30 RETURNED TO SERVICE.SDR 9802489925Circuit Breaker · inoperativeDURING CLIMB-OUT, THE RIGHT WING FLAP WOULD NOT RETRACT FROM THE 15 DEGREE POSITION, THE WINDSHEAR ANNUNCIATOR LIGHT ILLUMINATED, THE FIRST OFFICER'S SPEED COMMAND FLAG WAS IN VIEW, AND THE NR 1 AND NR 2 VHF RADIOS BECAME INOPERATIVE (BOTH WORKED NORMALLY IN ESDR VJ9800127Angle · corrodedFLOORBOARD ATTACH ANGLES, FS 160 TO 220, BL 55L, CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. FABRICATED AND INSTALLED ATTACH ANGLE IAW DC9 SRM 51-10-2, 51-30-1, 51-30-2. TREATED AND PRIMED IAW DC9 SRM 51-10-3.SDR MWEA98149Seat Track · corrodedDURING INSPECTION, FOUND HEAVY CORROSION ON GALLEY SEAT TRACK NR 4 FROM STATION 200 TO 240. MTC REPAIRED IAW SRM 51-30-2 AND SRM 53-05 FIG 4F.SDR MWEA98148Bulkhead · corrodedDURING INSPECTION, FOUND LIGHT CORROSION ON FWD SIDE OF APB LEFT SIDE FROM APPROXIMATELY LONG 26L TO 28L. MTC REPAIRED IAW SRM 53-03 FIG 9 SHEET 1 AND 51-30-5.SDR MWEA98147Skin · corrodedDURING INSPECTION, FOUND LIGHT CORROSION ON EXTERIOR SURFACE OF LOWER SKIN ON RIGHT ELEVATOR XE 157.9. MTC REPAIRED IAW SRM 55-03 FIG 14 SHEET 2 AND SRM 51-30.SDR 9802349983Cable · wornDURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXTERNAL RELEASE HANDLE HANGS UP ON HINGED SPRING DOOR DURING PULL TEST OF THE EMERGENCY RELEASE. ALSO, FOUND THE INTERIOR TAILCONE RELEASE CABLE WORN AT THE HANDLE. RESHAPED HINGED SPRING DOOR AND REPLACED CABLE.
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