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 MWEA96355Angle · corrodedDURING D-CHECK, SEVERE CORROSION WAS FOUND ON LT ELEVATOR T/E 'TEE' ATTACH ANGLE BRACKET AT STA XE 171.5. FABRICATED A NEW TEE AND INSTALLED IAW SRM 51-10 AND 51-30.SDR MWEA96354Shovel Clip · corrodedDURING D-CHECK, A SHOVEL CLIP WAS FOUND CORRODED AT STA 110, LONG 21R. INSTALLED A NEW CLIP IAW SRM 51-30-2 AND 51-30-5.SDR MWEA96353Frame · corrodedDURING D-CHECK, A-FRAME IN E AND E COMPT WAS FOUND WITH A 2 INCH AREA OF HEAVY CORROSION AT STA 120, LONGERON 25R. FABRICATED A REPAIR DOUBLER IAW SRM 53-03, FIG 5, SECTION AA AND INSTALLED IAW SRM 51-30-5.SDR MWEA96352Skin · dentedDURING D-CHECK, DEEP DENT IN FUSELAGE SKIN WAS FOUND AT APPROX STA 1155 ON AFT RT CANTED STATION AREA. FABRICATED AND INSTALLED A REPAIR IAW SRM 53-01, FIG 2 SHEET 3.SDR MWEA96351Skin · corrodedDURING D-CHECK, RT FUSELAGE SIDE SKIN FOUND CHAFED AND CORRODED FROM WING FILLET PANEL AT STA 813 AND LONG 26R. REPAIRED DAMAGED AREA IAW DAC TELEX SVC-MSP-0335/DLP DATED 6 MAY 96.SDR MWEA96350Fitting · oversize holeDURING D-CHECK, RT NR 2 SLAT CENTER FITTING FOUND WITH ENLARGED HOLE DIAMETER FOR THE ECCENTRIC ATTACH BOLT. REPAIRED OVERSIZED HOLE IAW DAC TELEX SVC-MSP-0451/PPS DATED 11 JUNE 96.SDR MWEA96349Fittings · corrodedDURING D-CHECK, NR 4 SLAT INBD FITTING FOUND WITH TWO PREVIOUSLY CORRODED SPOT FACES WHICH ARE PRESENTLY RECORRODED. REPAIRED FITTINGS IAW DAC TELEX SVC-MSP-0365/PDG DATED 17 MAY 96.SDR MWEA96348Ribs · crackedDURING D-CHECK, LT WING HAD TWO LEADING EDGE RIBS FOUND CRACKED AT NR 1 SLAT INBD AREA. REPLACED RIBS IAW SRM 57-01, PG 1, 2.SDR MWEA96347Frame · crackedDURING D-CHECK, AFT ACCESSORY COMPT FRAME WAS FOUND CRACKED AT STA 1076, LONG 3R. FABRICATED FRAME IAW SRM 53-01, PAGE 1. HEAT TREATED IAW SRM 51-10-2A AND INSTALLED IAW SRM 53-03, PG 131.SDR MWEA96346Longeron · crackedDURING D-CHECK, LONGERON 4L FOUND CRACKED IN FRAME AT STA 200. SPLICED IN NEW SECTION OF LONGERON IAW SRM 53-02 FIG 2.SDR MWEA96345Frame · crackedDURING D-CHECK, A-FRAME WAS FOUND CRACKED ABOVE PAX DOOR INTERCOSTAL AT STA 180 AT LONG 6L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-03, FIG 36. HEAT TREATED 7075-0 PARTS TO 7075-T6 IAW SRM 53-03 FIG 36.SDR MWEA96344Intercostal · crackedDURING D-CHECK, LT MAIN GEAR INNER DOOR PAN INTERCOSTAL 'Z' ATTACH ANGLE WAS CRACKED AT STA 737. INSTALLED A NEW INNER DOOR PAN INTERCOSTAL IAW SRM 51-30-2.SDR MWEA96343Skin · corrodedDURING D-CHECK, NUMEROUS AREAS OF LT FLAP HAD CORROSION. REPLACED SKIN IN THESE AREAS IAW SRM 51-30-2.SDR MWEA96342Nose Rib · corrodedDURING D-CHECK, RT FLAP LDG EDGE NOSE CAP RIBS WERE FOUND CORRODED TO EXCESS AT STA XFLS198 AND XFLS210. INSTALLED TWO NEW NOSE CAP RIBS IAW SRM 51-30-2.SDR MWEA96341Web · corrodedDURING D-CHECK, FOUND CORROSION ON INBD AREA OF FLAP INSIDE ON AFT SPAR WEB. REPAIRED AFT SPAR WEB IAW SRM 57-01, FIG 2.SDR MWEA96340Skin · corrodedDURING D-CK, CORROSION FOUND ON LT FLAP INSIDE SURFACE OF UPPER AND LOWER SKINS STA XFLS 199-211 AND ADJOINING RIB AT STA XFLS 201. ALSO, ON LDG EDGE NOSE RIB SUPPORT AT STA XFLS201. REMOVED CORROSION, INSTALLED NEW RIBS IAW SRM 57-01 PG 1.SDR MWEA96339Clip · crackedDURING D-CHECK, AFT CARGO DOOR NR 4 BEAM END WAS FOUND CRACKED ON AFT END OF DOOR. REPLACED BEAM END CLIP WITH A NEW ONE IAW SRM 52-01.SDR MWEA96338Pan · crackedDURING D-CHECK, AFT CARGO DOOR WAS FOUND WITH CRACK IN DOOR PAN AT DOOR STOP BEAM NR 1 FWD SIDE OF DOOR. FABRICATED A NEW PAN SPLICE AND INSTALLED IAW DAC DRAWING 5934142.SDR MWEA96337Keel Beam · corrodedDURING D-CHECK, CORROSION FOUND ON RT MLG DOOR ATTACH BEAM AND ON A KEEL BEAM END FITTING. INSTALLED A NEW ATTACHING BEAM AND END FITTING IAW SRM 51-30-5.SDR MWEA96336Floor Beam · corrodedDURING D-CHECK, TWO CABIN FLOOR BEAMS WERE FOUND WITH CORROSION ON BEAM FROM CENTERLINE TO RT SIDE OF FUSELAGE AT STA 980 AND 996. INSTALLED REPAIR ANGLE AND FILLERS IAW SRM 53-04, FIG 20A.SDR MWEA96335Door Jamb · crackedDURING D-CHECK, VENTRAL DOOR JAMB WEB AT RT UPPER CORNER WAS FOUND CRACKED. FABRICATED REPAIR PARTS IAW SRM 53-05 AND INSTALLED IAW SRM 53-05, PG 63.SDR MWEA96334Blkhd Angles · crackedDURING D-CHECK, RT SIDE T-ANGLES WERE FOUND CRACKED AT NR 1, 2, 3 AND 4 POSITIONS AT STA 996 WHERE RT FUS SKIN MEETS AFT PRESSURE BULKHEAD. FABRICATED NEW ANGLES AND INSTALLED IAW DAC DRAWING J060110.SDR MWEA96333Floor Beam · corrodedDURING D-CHECK, CABIN FLOOR BEAM CAP AT STA 980 HAD CORROSION ON TOP OF BEAM; FLOOR BEAM UPPER CAP AT STA 996 HAD CORROSION ON TOP AND BOTTOM OF BEAM. REPAIRED AREAS IAW SRM 53-01, 53-05, FIG 20A PG 31.SDR MWEA96332Blkhd Angles · crackedDURING D-CHECK, LT SIDE NR 2, 3 AND 4 T-ANGLES WERE FOUND CRACKED WHERE AFT PRESSURE BULKHEAD MEETS FUS SKIN AT STA 996. FABRICATED AND INSTALLED NEW ANGLES IAW DAC DRAWING J060110.SDR MWEA96331Fitting · crackedDURING D-CHECK, VENTRAL DOOR JAMB LT SIDE FITTING 24 INCHES ABOVE FLOOR LINES WAS FOUND CRACKED. FABRICATED NEW FITTING IAW DAC DRAWING 3917624 AND INSTALLED IAW SRM 51-30.SDR MWEA96330Floor Beam · gougedDURING D-CHECK, FWD CARGO COMPT CEILING LWR FLANGES OF CABIN FLOOR BEAM WERE GOUGED FROM CARGO DOOR HITTING AT STA 389 AND 408. INSTALLED REPAIR IAW SRM 53-05, FIG 86.SDR MWEA96329Hinge Fitting · crackedDURING D-CHECK, RT FLAP MOUNTED INBD HINGE FITTING WAS FOUND CRACKED AT ACTUATOR INBD LUG. INSTALLED NEW HINGE FITTING IAW LH MANUAL 27-50-1.SDR MWEA96328Hinge Fitting · crackedDURING D-CHECK, LT FLAP MOUNTED INBD HINGE FITTING WAS FOUND CRACKED AT ACTUATOR INBD LUG. INSTALLED A NEW HINGE FITTING IAW OH MANUAL 27-50-1.SDR MWEA96327Skin · crackedDURING D-CHECK, AFT FUS SKIN CRACKED AT LT PYLON UPPER ATTACH ANGLE, 1.5 INCH AT STA 991 UNDER LONGERON 15L. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW 53-04, PG 279 FIG 46.SDR MWEA96326Pan · crackedDURING D-CHECK, FWD CARGO DOOR WAS FOUND TO HAVE SMALL CRACK IN AFT OUTER PAN COMING FROM A BN FASTENER HOLE. INSTALLED A REPAIR IAW SRM 52-08, FIG 8 SHEET 1.SDR MWEA96325Spar · corrodedDURING D-CHECK, LT WING AFT SPAR UPPER AND LOWER CAPS WERE CORRODED FROM STA XRS 513 TO XRS 551. REPAIRED THE SPAR AND CAPS PER DAC TELEX SVC-MSP-0411/PDG DATED 30 MAY, 96 AND SRM 57-09, FIG 24.SDR MWEA96324Angle · crackedDURING D-CHECK, RT PYLON FRAME UPPER FLANGE FOUND CRACKED AT STA 1059 OUTBD OF FIREWALL. REPLACED ANGLE IAW SRM 51-302.SDR MWEA96323Firewall · crackedDURING D-CHECK, RT PYLON WAS FOUND TO HAVE SMALL CRACK IN LWR FWD CORNER OF ANGLED FIREWALL INBD OF AFT ENGINE ISOLATOR. FABRICATED A REPAIR AND INSTALLED IAW SRM 51-20-3 AND 54-01, FIG 2 SHEET 4.SDR MWEA96322Skin · dentedDURING D-CHECK, THE RT FLAP NR 5 TRAILING EDGE WAS FOUND WITH DENTED LOWER SKIN FROM THE 3RD THROUGH 5TH RIB FROM THE OUTBD EDGE. INSTALLED NEW SKIN IAW EA 57-004.SDR MWEA96321Longeron · crackedDURING D-CHECK, CRACKED LONGERONS WERE FOUND IN AFT ACCESSORY COMPT LONG 2L AND 2R AT STA 1076. FABRICATED LONGERONS IAW SRM 53-02, FIG 8 AND INSTALLED IAW SRM 53-01, PAGE 1.SDR MWEA96320Spar Cap · corrodedDURING D-CHECK, THE RT WING LEADING EDGE HAD MODERATE SURFACE CORROSION INSIDE BOTTOM SPAR CAP BETWEEN STATIONS XRS 506 TO XRS 545. COMPLETED REPAIR IAW DAC TELEX SVC-MSP-0427/RMK DATED 6/3/96.SDR MWEA96319Frame · crackedDURING D-CHECK, A FRAME WEB WAS FOUND CRACKED IN AFT ACCESSORY AT STA 1038 INBD OF LONGERON 13L. INSTALLED A REPAIR IAW SRM 53-01, FIG 2 SHEET 3.SDR MWEA96318Skin · corrodedDURING D-CHECK, FOUND THAT THE LT ELEVATOR HAD MODERATE CORROSION ON UPPER OUTBD SKIN FROM STA XE171.0 TO XHR 224.0. REPLACED AFFECTED SKIN IAW ME EA 55-002.SDR MWEA96317Fitting · crackedDURING D-CHECK, LT PYLON ATTACH FITTING WAS FOUND CRACKED IN AFT INBD CORNER OF THE CANNON PLUG COMPARTMENT. REPLACED CRACKED FITTING IAW SRM 51-01 AND 51-30-1.SDR MWEA96316Fitting · corrodedDURING D-CHECK, CORROSION AND POPPED RIVET FOUND IN END FITTING AT STA 1121, LONG 10R. INSTALLED A NEW FITTING IAW SRM 51-10-3 AND 51-30-5.SDR MWEA96315Fitting · crackedDURING D-CHECK, THE RT FWD VERTICAL STAB ATTACH FITTING WAS FOUND CRACKED BETWEEN BOLT HOLES AT STA 1087. INSTALLED A NEW ATTACH FITTING IAW SRM 55-01, PG 1.SDR MWEA96314Fitting · corrodedDURING D-CHECK, FITTING FOR FLOOR BEAM ATTACH TO CUSP STRUCTURE FOUND CORRODED/CRACKED AT STA 965. FABRICATED A NEW FITTING IAW SRM 51-10-2, INSTALLED IAW SRM 51-30.SDR MWEA96313Floor Beam · corrodedDURING D-CHECK, LIGHT CORROSION FOUND IN UPPER FLANGE OF CABIN FLOOR BEAM BETWEEN NUTPLATES AT STA 996 ABOVE WASTE DRAIN TUBE ON RT SIDE. REPLACED UPPER CAP ANGLE IAW SRM 53-1.SDR MWEA96312Fitting · corrodedDURING D-CHECK, EXFOLIATION CORRISION WAS FOUND IN ATTACH FITTING, FLOOR BEAM TO CUSP LINE STRUCTURE AT STA 980 LT. FABRICATED A NEW FITTING IAW SRM 51-10-2 AND INSTALLED IAW SRM 51-30.SDR MWEA96311Ribs · crackedDURING D-CHECK, THREE RIBS WERE FOUND CRACKED THROUGH THE AFT FASTENER HOLES IN THE VERTICAL STABILIZER LEADING EDGE. REPAIRED THE CRACKED RIBS WITH ANGLE DOUBLERS IAW SRM 55-01, FIG 2 SHEET 3.SDR MWEA96310Skin · corrodedDURING D-CHECK, FOUND CORROSION ON LOWER SKIN OF LT ELEVATOR 15 INCHES FROM OUTBD TIP. REPLACED SKIN IAW ME EA 55-003.SDR MWEA96309Stringers · crackedDURING D-CHECK, LOWER STRINGERS 5, 6 WERE FOUND CRACKED AT STATION XHS 50 IN LT HORIZ STAB. REPAIRED THE CRACKED STRINGERS IAW SRM 55-02, FIG 16.SDR MWEA96308Support Web · crackedDURING D-CHECK, CRACK FOUND IN THE NOSE LANDING GEAR DRAG BRACE SUPPORT WEB. REPAIRED DRAG BRACE SUPPORT BY INSTALLING A FILLER AND NESTED ANGLE PER DAC TELEX SVC MSP-0321/PDG DATED 7 MAY 96.SDR MWEA96307Fitting · crackedDURING D-CHECK, A CRACKED FITTING WAS FOUND IN RT PYLON. FABRICATED A NEW FITTING IAW DAC SWG 4919864, INSTALLED IAW SRM 51-30-1 AND 51-30-5.SDR MWEA96306Fitting · crackedDURING D-CHECK, LT AFT EMERGENCY EXIT OVERWING HAS TWO CRACKED PAN TO FRAME ATTACH FITTINGS. REPLACED THE TWO FITTINGS IAW SRM 52-01.
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