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 L1GA200000267Floor Support · corrodedA 1.5 INCH BY 20 INCH AREA CORRODED AT FS 160 BL 0 TO 20 LT. REMOVED AND REPLACED FLOOR SUPPORT.SDR L1GA200000266Floor Support · corrodedA 1.5 INCH BY 8 INCH CORRODED AREA AT FS 200 BL 44 TO 50 RT FLOOR SUPPORT. REMOVED AND REPLACED WITH IDENTICAL PART.SDR L1GA200000265Attach Angle · crackedA 1 INCH CRACK AFT FUSELAGE ABOVE APU ENCLOSER STEP STRUCTURE. FABRICATED REPAIR ANGLE.SDR L1GA200000264Support Bracket · crackedA 1 INCH CRACK AFT FUSELAGE ABOVE APU ENCLOSURE SUPPORT BRACKET. FABRICATED REPAIR ANGLE.SDR L1GA200000263Stiffener · cracked1 INCH CRACK AFT FUSELAGE ABOVE APU ENCLOSURE STEP STIFFENER. FABRICATED REPAIR ANGLE.SDR L1GA200000262Web · corrodedA 5 BY 7 INCH CORRODED AREA AT STATION 579 LT SIDE CUSP WEB. FABRICATED DOUBLER REPAIR.SDR L1GA200000261Angle · crackedA 1 INCH CRACK AFT PIT CEILING FS 990. FABRICATED REPAIR ANGLE.SDR L1GA200000260Skin · corrodedA 1 INCH LONG CRACK ON SKIN AT FS 82 LONGERON 20 TO 21 RT. INSTALLED REPAIR DOUBLER.SDR L1GA200000259Seat Track · corrodedA 1 BY 7 INCH CORRODED AREA RT OUTBOARD SEAT TRACK. REMOVED AND REPLACED SEAT TRACK.SDR L1GA200000258Seat Track · corrodedA 1 BY 7 INCH CORRODED AREA SEAT TRACK. REMOVED AND REPLACED TRACK.SDR L1GA200000257Seat Track · corrodedA 1 X 15 INCH CORRODED AREA RT OUTBOARD SEAT TRACK FS 670 - 685. REMOVED AND REPLACED SEAT TRACK.SDR L1GA200000256Seat Track · corrodedA 1 X 24 INCH CORRODED AREA AT RT OUTBOARD SEAT TRACK AT FS 642 - 666. REMOVED AND REPLACED TRACK.SDR L1GA200000255Floor Support · corrodedCORROSION AND DOUBLE DRILLED HOLES AT FS 160. FABRICATED NEW FLOOR SUPPORT.SDR L1GA200000254Web · crackedA 2 INCH CRACK AT STATION 960 BL 50 RT. INSTALLED DOUBLER REPAIR.SDR L1GA200000253Web · crackedA 1 INCH CRACK AT FS 598 - 610 LT SIDE CUSP WEB. FABRICATED DOUBLER REPAIR.SDR L1GA200000252Elbow · crackedA 3 INCH CRACK ON APU EXHAUST ELBOW. WELDED REPAIR.SDR L1GA200000251Frame · crackedFRAME CRACKED AT FS 180 LT BELOW LONGERON 5L. FABRICATED REPAIR ANGLE.SDR L1GA200000250Floor Panel · damagedHOLE IN FLOOR PANEL AT FS 560 - 580. INSTALLED REPAIR DOUBLER.SDR L1GA200000249Web · crackedA 3.5 INCH CRACKS AT FS 560 - 580 BL 0 TO 22 LT. FABRICATED WEB INSTALLED.SDR L1GA200000248Web · corrodedA 40 INCH X 8 INCH AREA OF CORROSION STATION 160 TO 218 RBL 46 TO 52. FABRICATED FLOOR WEB.SDR L1GA200000247Shroud · crackedCRACKED SHROUD LT SIDE OF APU COMPARTMENT. WELDED REPAIR.SDR TWAA0013607Longeron · crackedDURING OP 15 MAINT CHECK, LONGERON 30 WAS CRACKED AT STA 579. REPAIRED PER SRM 53-02, FIG 14.SDR CA001004017Motor · failed(CAN) PRIMARY LONGITUDINAL TRIM DID NOT WORK SHORTLY AFTER TAKEOFF. NEITHER SUITCASE HANDLES OR THUMB SWITCHES WORKED. ALTERNATE TRIM WORKED AND SHORTLY THEREAFTER THE PRIMARY TRIM BEGAN TO WORK. PRIMARY STABILIZER TRIM MOTOR REPLACED AS PER MAINTENANCE MANUALSDR AT0000433Frame · crackedFOUND FRAME AT BS 737 WAS CRACKED. REPAIRED FRAME AT BS 737 IAW SERVICE BULLETIN 53-131 DRAWING 5935650.SDR AT0000436Frame · lightning strikeFOUND LIGHTNING STRIKE ON WINDOW NR 50 LOWER AFT CORNER ON FRAME. BLENDED OUT LIGHTNING STRIKE, FABRICATED AND INSTALLED REPAIR IAW SRO 9530053 AND REO L-00265.SDR AT0000435Fitting · corrodedFOUND STRINGER 30 END CAP FITTING AT WING SPAR HAS CORROSION. REMOVED AND REPLACED STRINGER END CAP FITTING AT BS 540 - 580 IAW DC9 SRM 51-01 FIGURE 1, 51-30-0, 51-10-3.SDR AT0000432Skin · dentedFOUND DENT AT BS 350, LONGERON 26R, 27L. DENT OUT OF LIMITS. PERFORMED HFEC INSPECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04 FIGURE 3B.SDR AT0000427Bracket · crackedFOUND CRACKED SUPPORT BRACKETS FOR CABIN FLOOR PANEL AT BS 725 - 832. REMOVED AND REPLACED SUPPORT BRACKETS IAW TIMCO SERVICE ORDER 151080-20463.SDR AT0000394Frame · corrodedFOUND FRAME SEGMENT AT BS 598 CORRODED. REMOVED AND REPLACED FRAME SEGMENT IAW DC9 SRM 51-30-2, 51-30-2, 51-30-5.SDR TWAA0013503Channel · corrodedDURING OP 15 MAINT CHECK, FOUND FLOOR ATTACH ANGLE HAD CORROSION. REPLACED J-CHANNEL PER SRM 51-30-2, PAGE 1.SDR TWAA0104906Skin · crackedDURING OP 15 MAINT CHECK FOUND RT WING L/E DOUBLER OUTBOARD OF LOWER VORTILION CRACKED INSIDE THE L/E. REPLACED DOUBLER. INSTALLED RIVETS PER SRM 51-30-0. INSTALLED HI-LOKS PER SRM 51-6-0.SDR TWAA0104905Angle · crackedDURING OP 15 MAINTENANCE CHECK ON RIGHT WING LEADING EDGE THE WING LEADING EDGE ANGLE AFT OF DOUBLER OUTBOARD OF LOWER VORTILION, WAS CRACKED. REPLACED ANGLE AND INSTALLED FASTENERS.SDR AT0000439Skin · lightning strikeFOUND LIGHTNING STRIKE ON WINDOW FRAME NR 24. BLENDED STRIKE AND INSTALLED DOUBLER IAW REO-L000256 AND DC9 SRM 53-05 FIGURE 11.SDR AT0000385Spar Cap · mismanufacturedFOUND RIGHT HAND SPAR LOWER SPAR CAP REQUIRED TRIMMING PER EO 9-5510-29-1514. COMPLIED WITH EO 9-5510-29-1514.SDR AT0000384Spar Cap · mismanufacturedFOUND LEFT HAND LOWER SPAR CAP REQUIRES TRIMMING PER EO 9-5510-29-E1514 REV A. COMPLIED WITH EO 9-5510-29-E1514 REV A.SDR TWAA0013502Stringer · crackedDURING OP 15 MAINT CHECK, FOUND STRINGER 17R, STA 965, WAS CRACKED ALL AROUND THE TOP HOLE. REPLACED LONGERON 17R FROM STA 954 TO 996 PER SRM 53-02, FIG 18, PAGES 48 TO 53.SDR TWAA0101503Longeron · corrodedDURING OP 15 MAINT CHECK LONGERON 22L, STA 996, HAD CORROSION ON LONGERON TIE CLIP, AFT OF PRESSURE BULKHEAD. INSTALLED NEW PART PER DRAWING 5911428.SDR AT0000425Lanyard · frayedFOUND FORWARD AND AFT ESCAPE LINE OVER RIGHT WING WERE FRAYED. REMOVED AND REPLACED FORWARD AND AFT EMERGENCY ESCAPE LINES IAW DC9 MM 25-61-0.SDR AT0000392Skin · gougedFOUND FUSELAGE SKIN HAS 2 GOUGES AT BS 342. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04 FIGURE 38.SDR AT0000399Web · corrodedFOUND CABIN FLOOR WEB CORRODED AROUND BUTTON HEAD AT BS 170 - 180. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3, 53-01 FIGURE 1, 51-10-4, 53-11-1 FIGURE 11, 51-30-2.SDR AT0000389Longeron · dentedFOUND DENT IN LEFT LONGERON 17 - 18 AT BS 226. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04 FIGURE 38.SDR AT0000388Skin · dentedFOUND DENT AT BS 251 LEFT LONGERON. DENT OUT OF LIMITS, INSPECTED, FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DC9 SRM 53-04 FIGURE 38, 51-10-3, 51-30-2.SDR AT0000379Bulb · failedFOUND L-1 EMERGENCY POST LIGHT INOPERATIVE. RELAMPED.SDR AT0000400Trunnion · corrodedFOUND RIGHT MAIN LANDING GEAR SIDE BRACE TRUNNION LUG HAS CORROSION ON FORWARD AND AFT FACE. REMOVED BUSHING FROM RIGHT TRUNNION, REMOVED CORROSION BY SPOT FACING LUG, FABRICATED NEW BUSHING AND SHIMS AND INSTALLED IAW DC9 OHC 20-10-3, 57-40-1 AND TIMCO REO-LSDR AT0000390Frame · corrodedFOUND FRAME AT BS 148R EXFOLIATED CORROSION BEYOND LIMITS AND CUSP T-FITTING CORRODED AND CRACKED. REMOVED CUSP TO FRAME T-ATTACH FITTING, FABRICATED Z-DOUBLER, HEAT TREATED, PRIMED AND INSTALLED IAW TIMCO REO - L00250, DC9 SRM 51-10-2, 51-10-5, 51-10-4.SDR AT0000386Floor Panel · corrodedFOUND FORWARD CARGO COMPARTMENT FLOOR PANEL CORRODED. TRIMMED, DRILLED AND DEBURRED REPLACEMENT FLOOR PANEL AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-4, 51-10-3.SDR 0003159925Frame · corrodedCORROSION AT THE FWD B/B LOWER FLANGE OF DOOR OPENING. REMOVED CORROSION AND REPAIRED ARE IAW EA 99-177196 LOG PAGE 1480766.SDR TWAA0013111Shear Tie · crackedDURING OP 15 MAINT CHECK, FOUND FORMER FOOT (SHEAR TIE) CRACKED AT STA 943, LONGERON 14R. REPLACED FORMER FOOT IN CONJUNCTION WITH MO 72J14.SDR CA000918006Wire · damaged(CAN) STALL INDICATION FAILURE LIGHT ON TRAINING FLIGHT, AIRCRAFT RETURNED TO BASE. FOUND LT GENERATOR TRIPPED, ATTEMPTED RESET, NIL FIX, FOUND DAMAGED WIRING.REPLACED WIRE X4A2N, SYSTEM CHECK SERVICEABLE.SDR MWEA00750Line · leakingMXI - FLT 009 - AT CRUISE FLIGHT, CREW NOTICED RIGHT HYDRAULIC SYSTEM QUANTITY WAS DOWN TO 1 QUART. RIGHT HYDRAULIC PRESSURE DROPPED AND PRESSURE LOW LIGHT AND RUDDER CONTROL MANUAL LIGHTS CAME ON. LANDED AT MCI WITHOUT INCIDENT AFTER PERFORMING QRH PROCEDUR
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