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 GTIA96NK186Battery · dischargedFORWARD CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSEMBLY. OPS NORMAL IAW DC-9 MM CHAP 33. (M)SDR CALA9601195Skin · crackedINSPECTION FOUND A 5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT STA XHS 86.0. AN EXTERNAL DOUBLER WAS INSTALLED IAW ECRA 5530-01174 AND SRM 55-03, FIGURE 13.SDR 9616649610Fuse · blownDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL.SDR 9616639609Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR MWEA96403Slide Cover · fell offDURING INSP, MAINT REPORTS GALLEY DOOR EVAC SLIDE COVER FELL OFF WHILE CLOSING DOOR. REINSTALLED GALLEY DOOR SLIDE COVER.SDR MWEA96400Longeron · corrodedDURING D-CHECK, LONGERONS 16L AND 17L WERE FOUND CRACKED AT STA 965 AND LONG 17L CRACKED AT STA 980. INSTALLED REPAIR IAW SRM 53-02, PAGE 2A.SDR MWEA96399Seal Pan · corrodedDURING D-CHECK, FOUND CORROSION ON RT AFT EMERGENCY EXIT DOOR SEAL PAN FWD AND AFT LOWER CORNERS. REPLACED SEAL PAN NEW IAW SRM 52-01.SDR MWEA96398Frame · corrodedDURING D-CHECK, FUSELAGE FRAME WAS EXFOLIATED AT STA 1104 BETWEEN LONGERONS 3L AND 4L. REPLACED FRAME NEW IAW SRM 53-01, PAGE 1 AND 2.SDR MWEA96397Seal Pan · corrodedDURING D-CHECK, CORROSION FOUND ON LT AFT EMERGENCY EXIT DOOR SEAL PAN FWD LOWER CORNER. REPLACED NEW LOWER SEAL PAN IAW SRM 52-01.SDR MWEA96396Support Strut · corrodedDURING D-CHECK, FOUND CORROSION ON FLOOR BEAM SUPPORT STRUT IN RT LAV AT STA 965. REMOVED CORROSION IAW SRM 51-10-3 AND INSTALLED SUPPORT AND CASTING IAW 51-30.SDR MWEA96395Intercostal · crackedDURING D-CHECK, FOUND INTERCOSTAL CRACKED AND CORRODED BETWEEN STA 446 TO 427 AT LONGERON 29LT. FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-10-2.SDR MWEA96394Longeron · corrodedDURING D-CHECK, LONGERON 29L WAS FOUND TO HAVE VARIOUS AREAS OF CORROSION STA 229 THROUGH 579. INSTALLED NEW LONGERON IAW SRM 53-01.SDR MWEA96393Longeron · crackedDURING D-CHECK, LONGERON 30 FOUND WITH MILD CORROSION FROM STA 417 T0 579. INSTALLED NEW LONGERON IAW SRM 53-01.SDR MWEA96392Rib · req'd repairDURING D-CHECK, TEMPORARY REPAIR NEEDED TO BE REPLACED ON FLAP AT STA XFLS 288.0. INSTALLED REPLACEMENT RIB IAW SRM 57-02, PAGE 1.SDR MWEA96391Rib · req'd repairDURING D-CHECK, DUE TO RECEIPT OF CORRECT PARTS, A TEMPORARY REPAIR NEEDED TO BE REPLACED ON FLAP AT STA XFLS 199.0. INSTALLED REPLACEMENT RIB IAW SRM 57-01, PAGE 1.SDR MWEA96390Recess Panels · crackedDURING D-CHECK, FOUND LT AND RT WINDSHIELD WIPER MOTOR CAVITIES HAVE CRACKS ON INNER RECESS PANELS. INSTALLED REPAIR IAW SRM 53-03, FIG 34 SHEET 1.SDR MWEA96389Skin · crackedDURING D-CHECK, RT MLG INBD DOOR TOP SKIN WAS FOUND CRACKED AT ACTUATOR FITTING APPROX .625 INCH LONG. FABRICATED A REPAIR IAW SRM 52-01 AND INSTALLED IAW SRM 52-01, FIG 2 SHEET 3.SDR MWEA96388Longeron · corrodedDURING D-CHECK, LONGERON 29R FOUND WITH CORROSION FROM STA 436 TO 522. FOUND CORROSION OUT OF LIMITS AND REPLACED WITH NEW LONGERON SECTION IAW SRM 53-01.SDR MWEA96387Angle · corrodedDURING D-CHECK, A T/E PANEL RIB UPPER ANGLE CORRODED, RT WING STA XRS 380. FABRICATED AND INSTALLED A NEW ANGLE WITH RIB IAW SRM 51-40-0.SDR MWEA96386Spar · corrodedDURING D-CHECK, RT WING REAR SPAR UPPER TANG WAS FOUND CORRODED AT STA XRS 380.0 JSUT ABOVE OUTBD FLAP HINGE. FABRICATED AND INSTALLED REPAIR IAW SRM 57-09, FIG 12.SDR MWEA96385Intercostal · crackedDURING D-CHECK, INTERCOSTAL FOUND CRACKED ABOVE FWD CARGO DOOR JAMB AT STA 408 ABOVE LONG 19R. FABRICATED NEW INTERCOSTAL AND INSTALLED IAW SRM 51-30-2.SDR MWEA96384Skin · damagedDURING D-CHECK, FWD CARGO COMPT DOOR JAMB AREA EXTERIOR SKIN CORNER FOUND DAMAGED AT STA 370, LONG 26L. REPAIRED SKIN PER SRM 53-04, FIG 38 SHEET 20.SDR MWEA96383Skin · dentedDURING D-CHECK, FWD FUSELAGE LOWER RT SKIN HAD SEVERAL DENTS AND CREASES AT STA 332, LONG 24R. FABRICATED AND INSTALLED REPAIR IAW SRM 53-04, FIG 38 SHEET 18.SDR MWEA96382Skin · creasesDURING D-CHECK, FWD FUSELAGE LOWER RT SKIN HAD SEVERAL CREASES IN CORNER BETWEEN STA 218 TO 256 AND LONG 24R TO 26R. INSTALLED A REPAIR IAW SRM 53-04, FIG 38 VIEW P.SDR MWEA96381Skin · blendedDURING D-CHECK, LT WING LEADING EDGE WAS FOUND WITH TWO SMALL BLENDED AREAS AT STA XIS 82.0. REPAIRED BLENDED AREAS IAW SRM 57-06A, FIG 4.SDR MWEA96380Skin · corrodedDURING D-CHECK, LT WING LEADING EDGE FOUND CORRODED EXCESSIVELY AT STA XIS 84.0. INSTALLED REPAIR DOUBLERS IAW SRM 57-06A, FIG 4.SDR MWEA96379Tee · corrodedDURING D-CHECK, LT GEAR WELL TEE HAD DEEP CORROSION PITTING AT STA 756, LONG 29L AND 30. FABRICATED REPAIR AND INSTALLED IAW SRM 53-03 AND 51-30-5.SDR MWEA96378Angle · gougedDURING D-CHECK, VHF ANTENNA SUPPORT L-ANGLE FOUND GOUGED TO EXCESS AT STA 325, LONG 29L AND 30. REPLACED THE ANGLE IAW SRM 53-01 PAGE 1.SDR MWEA96377Skin · damagedDURING D-CHECK, PREVIOUS REPAIR ON FUSELAGE SKIN WAS REEVALUATED ON FWD LOWER SKIN AT STA 288 AT LONG 20R. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED NEW REPAIR IAW SRM 53-04, FIG 12B SHEET 5.SDR MWEA96376Skin · damagedDURING D-CHECK, A PREVIOUS SKIN REPAIR DOUBLER REQUIRED REMOVAL FOR FURTHER EVALUATION AT STA 150 BETWEEN LONG 17R AND 18R. COMPLETED REPAIR IAW SRM 53-04, FIG 47.SDR MWEA96375Splice · crackedDURING D-CHECK, LT KEEL SPLICE FOUND CRACKED AT STA 700. INSTALLED NEW KEEL SPLICE IAW SRM 51-30-5.SDR MWEA96374Floor Beam · corrodedDURING D-CHECK, FLOOR BEAM UPPER CAP FOUND EXFOLIATED 15.5 INCHES INBD OF THE CUSP ANGLE AT STA 160. SPLICED IN A NEW SECTION OF CAP IAW DAC TELEX SVC-SMP-0420/SBT.SDR MWEA96373Skin · corrodedDURING D-CHECK, FUSELAGE SKIN FOUND CORRODED FROM STA 803 TO 818 LONG 27L TO 27R. FABRICATED NEW SKIN PANEL AND INSTALLED IAW DAC TELEX SVC-MSP-0320/AJC, DATED 7 MAY 96.SDR MWEA96372Skin · corrodedDURING D-CHECK, A SKIN PANEL WAS FOUND CORRODED FROM STA 986 TO 996 LONG 29L TO 29R. INSTALLED EXTERNAL DOUBLER REPAIR IAW 53-04, FIG 9.SDR MWEA96371Frame · improper repairDURING D-CHECK, FUSELAGE FRAME FOUND WITH PREVIOUS IMPROPER REPAIR AT STA 503, LONGERON 28L TO 28R. INSTALLED REPAIR PER SRM 53-03, FIG 2A SHEET 1.SDR MWEA96370Longeron · corrodedDURING D-CHECK, LONG 30 END FITTING WAS FOUND CORRODED FROM STA 579 TO 604. FABRICATED SPLICE FITTING IAW DAC DWG 3924809 AND INSTALLED IAW SRM 53-01.SDR MWEA96369Door Jamb · corrodedDURING D-CHECK, GALLEY DOOR JAMB 'T' FITTING WAS FOUND WITH CORROSION AT STA 200 FWD OF LONG 17R. FABRICATED NEW FITTING AND INSTALLED IAW SRM 51-10-2 AND 51-30-2.SDR MWEA96368Rib · crackedDURING D-CHECK, RT WING NR 1 SLAT INBD IDLER TRACK OUTBD RIB WAS FOUND CRACKED. REPLACED RIB SET IAW SRM 57-01, PAGE 1 AND 2.SDR MWEA96367Frame · corrodedDURING D-CHECK, FRAME LOWER FLANGE WAS FOUND CORRODED AT STA 218 IN E AND E COMPT FROM LONG 27L TO 27R. INSTALLED FRAME REPAIR IAW SRM 53-03-4A.SDR MWEA96366Doubler · corrodedDURING D-CHECK, DOUBLER PLATE FOUND CORRODED AT STA 996 FWD OF APB ABOVE LONGERON 30. FABRICATED A NEW DOUBLER IAW SRM 53-03 AND INSTALLED IAW 51-30-5.SDR MWEA96365Rib · crackedDURING D-CHECK, RT FLAP NOSE RIB FOUND CRACKED AT STA 207. FABRICATED A TEMPORARY REPAIR IAW SRM 57-01, FIG 3 SHEET 3 AND INSTALLED IAW SRM 51-30-2.SDR MWEA96364Fitting · crackedDURING D-CHECK, RT SIDE KEEL FITTING FOUND CRACKED AT STA 699. FABRICATED A NEW FITTING IAW DAC DWG 4915126 AND INSTALLED IAW SRM 51-30-5.SDR MWEA96363Fitting · corrodedDURING D-CHECK, LT KEEL HORSESHOE BRACKET FOUND CORRODED AT STA 680, LONG 29 LT. FABRICATED A NEW FITTING IAW DAC DWG 4916270 AND INSTALLED IAW SRM 51-30-03.SDR MWEA96362Longeron · crackedDURING D-CHECK, LONGERON UPPER FLANGE FOUND CRACKED AT STA 313 TO 332 AT LONG 29L. FABRICATED A LONG SECTION AND REPAIR SPLICES AND INSTALLED IAW SRM 53-02 AND 53-02, FIG 14.SDR MWEA96361Angle · crackedDURING D-CHECK, LT WING TRAP PANEL AFT OUTBD FLANGE REPAIR HAD AN ANGLE CRACK AT THE AFT FLANGE. INSTALLED ANGLE REPAIR IAW SRM 57-09, FIG 71 SHEET 2.SDR MWEA96360Spar Web · corrodedDURING D-CHECK, A 2 INCH AREA OF CORROSION FOUND ON RT HORIZONTAL STAB AFT SPAR WEB AT STA XMS 32.0. COMPLETED REPAIR IAW DAC TELEX SVC/MSP/0407/SBT.SDR MWEA96359Skin · corrodedDURING D-CHECK, LT AILERON UPPER SKIN FOUND WITH NUMEROUS AREAS OF LIGHT CORROSION. FABRICATED NEW SKIN AND DOUBLER IAW ME EA 57-002, TREATED AND PRIMED IAW SRM 51-10-3 AND INSTALLED IAW EA 57-002.SDR MWEA96358Fitting · crackedDURING D-CHECK, TWO SEAT TRACK FITTINGS WERE FOUND CRACKED AT STA 680, ONE UNDER NR 1 AND ONE UNDER NR 4 TRACK. INSTALLED NEW FITTINGS IAW SRM 51-10-4 AND 51-30-5.SDR MWEA96357Rib · crackedDURING D-CHECK, RT WING HAD SIX NOSE RIBS CORRODED AND ONE CRACKED ON LOWER FLANGE. REMOVED CORROSION IAW SRM 51-10-3, REPAIRED DAMAGED RIB IAW SRM 57-01, REINSTALLED REPAIR IAW SRM 51-30.SDR MWEA96356Rib · crackedDURING D-CHECK, RT WING NR 4 SLAT OUTBD DRIVE FITTING RIB ASSY WAS FOUND CRACKED BETWEEN 2 FASTENERS ON LOWER FLANGE. REPLACED RIB SET IAW SRM 57-02 PAGE 1, 2.
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