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 9810739961Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND ALL EMERGENCY LIGHTS IN TAIL COMPARTMENT AND ABOVE AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERY PACK AND BATTERIES. OPERATIONAL CHECK NORMAL.SDR TWAA9815903Seat Track · corrodedDURING OP 16 MAINT CHECK, FOUND NR 4 CABIN CHAIR TRACK CORRODED AT STA 218 TO 237. CORRODED SECTION OF TRACK REMOVED AND NEW SECTION INSTALLED WITH EXISTING HARDWARE.SDR TWAA9815902Panel · corrodedDURING OP 16 MAINT CHECK, FOUND PANEL ABOVE O/B END OF LT AILERON, 8 IN TO 17 IN FROM O/B END, WAS CORRODED AND DELAMINATED. INSTALLED NEW CORE AND ALUM SKIN PER SRM 51-70-2 HOT BOND PROCEDURE PER SERVICEABLE TAG.SDR USAAD98173Battery · dischargedDTW - THE AFT OVERHEAD EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD98166Power Supply · failedIND - THE COCKPIT EMERGENCY LIGHT WOULD NOT TURN OFF WHEN THE AIRCRAFT POWER WAS REMOVED FROM THE PLANE. MAINTENANCE REPLACED THE COCKPIT EMERGENCY LIGHT POWER SUPPLY. (M)SDR 9810509970Spar Cap · crackedDURING M-CHECK, A CRACK WAS FOUND IN THE REAR SPAR LOWER CAP AT FS XRS 353. REPAIRED PER EA 99-159317 (P/N 5911301-502).SDR TWAA9815802Pan · wornDURING OP 16 MAINT CHECK, FOUND PAN IN FWD ACCESSORY COMPT WITH INTERIM REPAIR INSTALLED PER ARA 11869 AND ARA 11870. REPLACED PAN AND REPAIRED PER ARA 15700, AND SRM 51-30-00 AND SRM 51-30-2.SDR 9810749959Fuse · blownDURING LINE MAINTENANCE INPSECTION, FOUND FIRST CLASS SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE. OPERATIONAL CHECK NORMAL.SDR TWAA9815801Support · corrodedDURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT, STA 218 TO 237, WAS CORRODED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-01.SDR USAAD98163Sensor · malfunctionedPIT-SDF - FLT 1805 - AFTER REACHING CRUISE ALTITUDE, THE LEFT MAIN GEAR RED UNSAFE ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GEAR UPLATCH SENSOR. SEVERAL GEAR RETRACTIONS WERE COMPLETED AND ALSDR USAA980427Longeron · crackedPIT - DURING C-6 CHECK, FOUND LONGEORN CRACKED ACROSS INTERSECTION .20 INCH AT STATION 639 LONGERON 4L. INSTALLED SPLICE PER SRM 53-02 PAGES 48-53. (M)SDR EISA98224Battery Pack · dischargedFORWARD EMERGENCY LIGHTS DIM. FOUND ON POST FLIGHT BY MECHANIC. REMOVED AND REPLACED BATTERY PACK IAW 33-53-0, OPS CHECK GOOD. (M)SDR USAAD98162Indicator · failedPIT - FLT 1572 - AFTER TAKEOFF, THE CAPTAINS FLIGHT DIRECTOR INDICATOR WINGS MOVED TO THE OFF POSITION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ADI. (M)SDR EISA98221Oxygen Panel · malfunctionedDURING CRUISE FLIGHT, BLUE OXYGEN LIGHTS AT FLIGHT ATTENDANT JUMPSEAT ILLUMINATED. AFTER TESTING COCKPIT ANNUNCIATOR. THE CABIN OXYGEN LIGHTS IN COCKPIT ILLUMINATED AIR TURN BACK TO ACY FOR MAINTENANCE. GENERATED FROM PILOT REPORT. PERFORMED OPS CHECK IAW 3SDR USAA980411Skin · crackedPIT - DURING RON, FOUND CRACKS RANGING FROM .125 INCH TO .75 INCH ON SKIN AT LT SIDE STATION 1132 BETWEEN LONGERONS 15L/16L. CRACKS AT 4 FASTENER HOLES RT SIDE STATION 1143 BETWEEN LONGERONS 12R/159 CRACKS AT 10 FASTENER HOLES. CLASSIFIED A MINOR REPAIR. CUSDR TWAA9816006Membrane · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE AT LONGERON 18R, STA 813. CORROSION WAS APPROX 0.008 DEEP AND 3 IN BY 3 IN. REMOVED CORROSION AND REPAIRED WITH ALUM 2024-T3, 0.032 IN PER SRM 53-01, PAGE 9 FIG 2.SDR TWAA9815312Stringer · corrodedDURING OP 16 MAINT CHECK, FOUND STRINGER 2L CRACKED AT BOTH SIDE FLANGES AT STA 200. REPLACED LONGERON MFG PART NR 5911406-13, USING FASTENERS PER SRM 51-30-0.SDR TWAA9815311Floor · corrodedDURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 20 WAS CORRODED THROUGH AND HAD BROKEN SUPPORT CHANNELS. FABRICATED NEW FLOOR PANEL PER SRM 53-00-64, FIG 201 PAGE 201.SDR TWAA9815307Spar · crackedDURING CHECK-C MAINT, FOUND LT WING AFT SPAR WITH EDDY CURRENT INDICATION OF 1.25 INCH CRACK IN AFT SPAR WEB, .75 INCH BELOW O/B LOWER BOLT HOLE FOR O/B FLAP HINGE CASTING. INSTALLED REPAIR PER ROD DRAWING 95-12-06-018, AND ARA 15388.SDR TWAA9815306Skin · corrodedDURING CHECK-C MAINT, FOUND ON VERT STAB LT SIDE, A GROOVE BLENDED BEYOND LIMITS PER SRM 53-01, PG 6 FIG 1, IN SKIN BELOW LT HORIZ STAB. ACCOMP EDDY CURRENT OF AREA PER 51-00-03 AND NO CRACKS FOUND. REPAIRED PER ARA 15375.SDR TWAA9815305Angle · damagedDURING CHECK-C MAINT, FOUND RT MAIN LANDING GEAR I/B DOOR DAMAGE WITH CRACK IN FWD Z' ANGLE UPPER FLANGE AND THE BUMPER PUSHED IN. REPAIRED PER SRM 52-05, FIG 14 PAGE 25. ALSO REF DRAWING 5910161, HIGH FREQ EDDY CURRENT AND CRACK CONTAINED PER 51-00-03 PAGE SDR TWAA9815310Support · brokenDURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 34 WITH BROKEN SUPPORT CHANNELS. REMOVED AND INSTALLED NEW SUPPORT CHANNELS.SDR TWAA9815309Floor · corrodedDURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 19 WITH CORROSION AND SEVERAL BROKEN SUPPORT CHANNELS. REPLACED CABIN FLOOR PANEL SHEET/HAT SECTION PER SRM 53-00-14, PAGE 201.SDR TWAA9815308Support · corrodedDURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT BEAM WITH CORROSION, STA 237 TO 313. REPLACED SUPPORT ANGLE STA 237 TO 258. REMOVED CORROSION FROM STA 258 TO 313.SDR TWAA9815304Former · crackedDURING CHECK-C MAINT, IN AFT ACCY COMPT FOUND FORMER CRACKED AT ATTACH POINT TO LONGER 2L AT STA 1076. REMOVED DAMAGED SECTION AND INSTALLED DOUBLERS PER DC9 SRM 53-03, FIG 32.SDR TWAA9815303Bulkhead Web · crackedDURING CHECK-C MAINT, FOUND AFT FUSELAGE STA 1121 WITH 2 INCH CRACK IN CANTED BULKHEAD WEB BELOW LOUVERS ON LT SIDE. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01, FIG 2 PAGE 9.SDR TWAA9815302Support · crackedDURING CHECK-C MAINT, FOUND IN RT GEAR WHEEL WELL LOWER RT FWD KEEL BEAM SELF SUPPORT CRACKED 60 PERCENT THRU, HAD ONLY BEEN STOP DRILLED. CRACK LOCATED FWD OF WHEEL WELL DOOR ACTUATOR.SDR USAAD98161Slide · failedPIT - THE AFT ESCAPE SLIDE MECHANISM FAILED TO DEPLOY THE SLIDE DURING FUNCTIONAL TEST. MAINTENANCE REPLACED THE SLIDE ASSY. (M)SDR 9810259998Angle · crackedDURING M CHECK, WING TO FUSELAGE ATTACH ANGLE WAS FOUND TO HAVE A 1.25 CRACK. REPAIRED PER EA 99-159285.SDR USAA980409Skin · crackedPIT - DURING C-5 CHECK, FOUND 1 INCH CRACK AT RADIUS OF -9 DOUBLER UPPER LT CORNER OF VENTRAL DOOR OPENING. ROUTED OUT CRACK AND INSTALLED DOUBLER PER EA 50476. (M)SDR USAA980396Skin · crackedPIT - DURING C-5 CHECK, FOUND 1 INCH CRACK JUST AFT OF STATION 465, LONGERON 20 (NEAR VHF ANTENNA) IN FUSELAGE SKIN. DETECTED VISUALLY AND BY EDDY CURRENT. REPAIRED PER EO NR 5385X016 AND EA NR 50475. (M)SDR USAA980395Longeron · crackedPIT - DURING C5 CHECK, FOUND CRACK .5 INCH LONG AT STATION 617, 8 RT LONGERON. DETECTED BY EDDY CURRENT. SPLICED IN NEW SECTION LONGERON PER 53-02 FIG 18. (M)SDR TWAA9814904Longeron · crackedDURING CHECK-C MAINT, FOUND .125 INCH CRACK IN LONGERON 4L AT STA 200. SPLICED IN NEW SECTION OF LONGERON PER DC9 SRM 53-02, FIG 18.SDR TWAA9814708Seat Track · corrodedCHAIR TRACK GROUND BEYOND LIMITS TO REMOVE CORROSION AT STA 200 TO 237, RBL 23 IN. REMOVED CHAIR TRACK AND REPLACED WITH NEW TRACK. INSTALLED WITH FASTENERS PER SRM 51-30-0.SDR TWAA9814707Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON 4L CRACKED AT STA 200. REPLACED LONGERON USING FASTENERS PER SRM 51-30-0.SDR EISA98216Fire Loop · failedRIGHT ENGINE LOOP 'A' FAILS TO TEST, LOOP 'B' CHECK OK. FOUND ON PREFLIGHT. GENERATED FROM PILOT REPORT. FOUND CONTACTS ON CONNECTOR TO BE DIRTY. CLEANED AND RESEATED CONTACTS. CHECK GOOD. (M)SDR EISA98215Switch · inoperativeRIGHT SIDE A/C PACK SHUT DOWN AT 35,000 FT, CABIN PRESSURE WARNING LIGHT CAME ON, PRESSURE ALTITUDE INDICATED 7000 FT IN THE CABIN. RETURNED TO EL PASO. GENERATED FROM PILOT REPORT. DETERMINED 2 SWITCHES BAD ON A/C SYSTEM REMOVED AND REPLACED 190 DEGREES SWSDR 98ZZZM785Switch · inoperativeRIGHT SIDE A/C PACK SHUT DOWN AT 35,000 FT, CABIN PRESSURE WARNING LIGHT CAME ON, PRESSURE ALTITUDE INDICATED 7000 FT IN THE CABIN. RETURNED TO EL PASO. GENERATED FROM PILOT REPORT. DETERMINED 2 SWITCHES BAD ON A/C SYSTEM REMOVED AND REPLACED 190 DEGREES SWSDR USAAD98142Apu · leakingCLT - FLT 1604 - DURING APPROACH, THE CREW NOTICED THE SMELL OF OIL APPARENTLY COMING FROM THE AIR CONDITION SYSTEM. THE SMELL BECAME MORE INTENSE AFTER LANDING. MAINTENANCE FOUND THE APU DROPPING OIL FROM THE INTERNAL CORE. THE APU WAS MEL'D AND SCHEDULED SDR ABXA9800818Latch · bindingCOCKPIT DOOR LATCHING MECHANISM BINDING AND STICKS IN CLOSED POSITION. DISASSEMBLED, CLEANED, LUBRICATED AND REASSEMBLED LATCH ASSEMBLY. OPS CHECKED GOOD.SDR ABXA9800817Longeron · crackedDURING C-CHECK, FOUND LONGERON 17L CRACKED FS 965. REPLACED SECTION OF LONGERON 17L FS 965 IAW DC9 SRM 53-02.SDR ABXA9800816Frame · crackedDURING C-CHECK, FOUND LEFT MAIN FRAME FS 718 CRACKED. REPAIRED LEFT FUSELAGE MAIN FRAME FS 718 IAW ABX REA D953- 24732-SB.SDR ABXA9800815Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN CORRODED FS 946-950 LONGERON 27R - LONGERON 29R. REPLACED DOUBLERS FS 945-980 LONGERON 27R TO LONGERON 29R, IAW DC9 MM 51-30-2.SDR ABXA9800814Skin · corrodedDURING C-CHECK, FOUND CORROSION ON LONGERON 30 AND ADJACENT FUSELAGE SKIN LONGERON 29R TO LONGERON 30R, FS 756-760. REPAIRED FUSELAGE SKIN IAW ABX REA D953 24724.SDR ABXA9800813Web · corrodedDURING C-CHECK, FOUND CUSP WEB CORRODED FS 945, LBL 50-54. REPLACED SECTION OF LEFT CUSP WEB 945L IAW ABX REA 953 24 702 MR.SDR ABXA9800812Longeron · crackedDURING C-CHECK, FOUND LONGERON 4 LEFT AT FS 160 CRACKED. REPLACED NEW SECTION OF LONGERON IAW DC9 SRM 53-02.SDR ABXA900811Frame · corrodedDURING C-CHECK, FOUND CORROSION ON FRAME 917 AT LONGERON 29L-LONGERON 29R. REPAIRED IAW DC9 SRM 53-03.SDR 9810069998Frame · crackedDURING PERIODIC CHECK, FOUND HOLE PUNCHED IN FRAME AND CRACK SURROUNDING HOLE AT FS 908, LONGERON 11R. INSTALLED REPAIR DOUBLER PER SRM 51-30-5 AND EA 99-159316.SDR USAAD98159Battery · dischargedPIT - THE EMERGENCY LIGHT MOUNTED ON THE FORWARD ENTRY DOOR WAS DIM. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGENCY LIGHT BATTERY. (M)SDR USAAD98158Battery · dischargedDTW - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 9 AND 13 WERE DIM. MAINTENANCE REPLACED THE BATTERIES FOR THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 9 AND 13. (M)
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