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 MWEA95481Fitting · crackedDURING D-CHECK, FOUND LT FLAP INBOARD FLAP HINGE FITTING INTERNAL FITTING FOR ATTACHMENT OF THE HINGE CRACKED. INSTALLED A NEW FITTING IAW SRM 57-09, PAR 14.SDR MWEA95480Angle · crackedDURING D-CHECK, FOUND TWO CRACKED ANGLES AT STA 160, LONGERON 28L AND 28R VISIBLE THROUGH INSP LIGHTENING HOLES IN E/E DOOR JAMB AFT CORNERS. INSTALLED TWO NEW SHEAR TIES IAW SRM 51-30.SDR MWEA95479Skin · crackedDURING D-CHECK, FOUND THE AFT FUSELAGE SKIN AT STA 996 AND LONGERON 23L CRACKED .3750 INCH FROM EDGE OF SKIN TO FASTENER HOLE. FABRICATED INTERNAL AND EXTERNAL DOUBLERS, A FILLER, CLEANED CORROSION AND INSTALLED IAW SRM 53-04 AND 53-01, PG 8.SDR MWEA95478Skin · creasedDURING D-CHECK, FOUND THAT THE FUSELAGE SKIN HAS A 40 INCH CREASE AT STA 190 - 229 NEAR LONGERON 24R. COLD FORMED THE DENT PER SRM 53-04, FIG 38, AND INSTALLED A DOUBLER IAW DAC TELEX.SDR MWEA95477Skin · crackedDURING D-CHECK, FOUND A TEMPORARY CLASS 3 REPAIR INSTALLED TO FUSELAGE SKIN CRACKED AT STA 167 AND 193 AT LONGERON 22L. FABRICATED A REPAIR AND INSTALLED PER SRO 9530219.SDR MWEA95476Skin · damagedDURING D-CHECK, FOUND A TEMPORARY EXTERNAL SKIN REPAIR AT STA 300 THRU 337, LONGERONS 24L-25L. INSTALLED A REPAIR PER ME DRAWING NR 53-149 AND DAC TELEX ORD-SVC-03001/JSS.SDR CAL951126Switch · inoperativeFLT NR 1512 - CLE - THE GEAR DOOR OPEN LIGHT REMAINED ON WITH GEAR UP AFTER TAKEOFF FROM CLE. CYCLING THE GEAR WAS OF NO HELP. WHEN THE GEAR WAS EXTENDED FOR RETURN TO CLE THE DOOR OPEN LIGHT EXTINGUISHED. MAINTENANCE FOUND THE LEFT MAIN DOOR INBOARD SWITCHSDR ABXA9501037Door Roller · out of adjustBWI - DURING INITIAL GEAR RETRACTION AFTER TAKEOFF, LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED LANDING GEAR WITH SAME INDICATION. UPLATCH CHECK YIELDED GEAR DOOR OPEN LIGHT AND LEFT GEAR UNSAFE LIGHT. ADJUSTED LEFT MAIN LANDING GEAR DOOR ROLLER ISDR 96ZZZX232Coaleser Sock · dirtySTL - FLT 363 - FOLLOWING AN ENGINE CHANGE, DURING TAKEOFF, FLIGHT ATTENDANTS REPORTED A BURNING SMELL AT MID-CABIN. REMOVED AND REPLACED RIGHT AND LEFT WATER SEPARATORS. OPERATIONAL CHECK NORMAL. CHECK C - 12-19-94 - STL.SDR 96ZZZM65Switch Unit · failedFLT NR 444 - ATL- AIR RETURN - ON TAKEOFF BOTH NAV SYSTEMS WERE INOP. NAV TRANSFER CIRCUIT BREAKER WOULD NOT RESET. REMOVED AND REPLACED NAV SWITCHING UNIT. OPS CHECK WITH T/C-30 IAW 34-10. (M)SDR CA960110506Oven · elect fault(CAN)AISLE TROLLEY (MEAL) POPPED CIRCUIT BREAKER & GAVE AN ELECTRICAL SHOCK TO FLIGHT ATTENDANT. MAINTENANCE ACTION INVOLVED CHECKING THREE PHASE POWER & GROUND RETURN, AIRCRAFT OVEN OUTLET. OVEN REPLACED.SDR 96ZZZM67Ducts · blown offFLT NR 515 - ATL - WHEN THE AIRCRAFT WAS PASSING THROUGH 17,000 FEET WHEN IT LOST CABIN PRESSURE AND WAS UNABLE TO CONTROL MANUALLY. AIR RETURN. FOUND LEFT AND RIGHT PACK DUCTS BLOWN OFF AT WATER SEPARATORS, REINSTALLED LEFT AND RIGHT DUCTS AND REPLACED LEFTSDR CAL951122Air Distr · smokeFLT NR 1589 - CMH - SMOKE APPEARED IN CABIN ON ROTATION AND INITIAL CLIMB-OUT AND THEN WENT AWAY ON DEPARTURE FROM CMH. THE AIRCRAFT WAS RETURNED TO CMH. THE PASSENGERS WERE EVACUATED VIA THE JETWAY, AS A PRECAUTIONARY MEASURE. THE AIR CONDITIONING SYSTEM WSDR 9520059919Retract Mech · out of adjustDURING CLIMB, THE LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED GEAR RETRACTION BY USING LANDING GEAR HANDLE RELEASE BUTTON. RECYCLED LANDING GEAR AND LANDING GEAR OPERATED NORMALLY. AIRCRAFT CONTINUED TO SLC AND LANDED WITHOUT INCIDENT. RIGGED GROUND SHIFTSDR 9519979986Uplock Switch · malfunctionedDURING APPROACH, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER THE LANDING GEAR WAS EXTENDED. APPROACH WAS ABORTED AND A GO-AROUND PERFORMED. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED UPLSDR MWEA95475Skin · dentedTEMPORARY EXTERNAL SKIN REPAIR LOCATED AT STA 285 THROUGH 323, LONGERONS 20 THROUGH 23 RT. INSTALLED A NEW SKIN PANEL IAW THE SRM 51-30.SDR MWEA95474Intercostal · crackedDURING D-CHECK, FOUND AN INTERCOSTAL CRACKED AT STA 84 AS VIEWED THROUGH THE CAPTAIN'S AND F/O'S WINDSHIELD WIPER MOTOR COVERS. FABRICATED A REPAIR IAW THE SRM 53-03, FIG 34 AND INSTALLED IAW SRM 51-30-5.SDR MWEA95472Bracket · crackedDURING D-CHECK, FOUND AN ATTACH BRACKET CRACKED AT STA 1038 IN THE PYLON UPPER INBOARD CORNER. FABRICATED A NEW BRACKET IAW DAC DWG 4919864 AND INSTALLED IAW THE SRM 51-30.SDR MWEA95471Bracket · crackedDURING D-CHECK, FOUND AN ATTACH BRACKET CRACKED AT STA 1038 IN THE LT PYLON UPPER INBOARD CORNER. FABRICATED A NEW BRACKET IAW DAC DWG 4919864 AND INSTALLED IAW THE SRM 51-30.SDR MWEA95470Fitting · crackedDURING D-CHECK, FOUND AN ATTACH FITTING AT THE BOTTOM LEFT OF THE KEEL BEAM CRACKED AT STA 699. FABRICATED A FITTING AND INSTALLED PER SRM 51-30.SDR MWEA95469Fitting · crackedDURING D-CHECK, FOUND LONGERON 25R END FITTING CRACKED AT STA 579. INSTALLED A NEW END FITTING IAW SRM 51-30.SDR MWEA95468Longeron · crackedDURING D-CHECK, FOUND LONGERON 24R CRACKED AT STA 455. REPLACED THE LONGERON WITH EXTRUSION P/N 27779225 IAW SRM 51-30.SDR MWEA95467Longeron · damagedDURING D-CHECK, FOUND LONGERON 25R DAMAGED AT STA 313. REPLACED THE LONGERON WITH EXTRUSION P/N 2777922-3 IAW SRM 51-30.SDR MWEA95466Longeron · crackedDURING D-CHECK, FOUND LONGERON 25R CRACKED AT FS 455. REPLACED THE LONGERON WITH EXTRUSION P/N 2777922-5 IAW SRM 51-10-4.SDR MWEA95465Longeron · oversized holesDURING D-CHECK, FOUND NUMEROUS LARGE HOLES IN LONGERON THAT WERE LEFT OVER FROM A PREVIOUS REPAIR AT FS 313-332 ON LONGERON 22R. REPLACED THE LONGERON SECTION IAW SRM 51-30 FROM FS 229 TO 370.SDR MWEA95464Longeron · oversized holesDURING D-CHECK, FOUND NUMEROUS LARGE HOLES IN LONGERON THAT WERE LEFT OVER FROM A PREVIOUS REPAIR AT FS 313-332 ON LONGERON 21R. REPLACED THE LONGERON SECTION IAW SRM 51-30.SDR MWEA95463Spar Splice · corrodedDURING D-CHECK, FOUND LT FLAP FORWARD SPAR SPLICE PLATE WAS CORRODED TO EXCESS AT STA XFLS 154.5. FABRICATED A NEW SPLICE PLATE AND INSTALLED IAW SRM 57-09, PARA 14.SDR MWEA95462Fitting · corrodedDURING D-CHECK, FOUND LT FITTING WITH CORROSION OUT OF LIMITS IN A BARREL NUT HOLE AT STA 718 JUST BELOW LONGERON 18. REPLACED THE FITTING IAW SRM 51-30-1.SDR MWEA95461Fitting · corrodedDURING D-CHECK, FOUND RT FITTING WITH CORROSION OUT OF LIMITS IN A BARREL NUT HOLE AT STA 718 JUST BELOW LONGERON 18. REMOVED AND REPLACED THE FITTING IAW SRM 51-30-1.SDR MWEA95460Skin · oversize holesDURING D-CHECK, FOUND 6 OVERSIZE HOLES IN SKIN AT STA 570, LONGERON 26L. REPAIRED THE OVERSIZE HOLES IAW SRM 53-04, FIG 37 PER DAC TELEX SVC-ORD-0230/DME.SDR MWEA95459Support · corrodedDURING D-CHECK, FOUND THE UPPER CAP AT FLOOR SUPPORT STRUCTURE AT STA 160 AT X 44.5 IS EXFOLIATED. FABRICATED AND INSTALLED A NEW FLOOR SUPPORT SECTION IAW DOUGLAS TELEX SVC-ORD-0240/AJC.SDR MWEA95458Skin · corrodedDURING D-CHECK, FOUND THE BELLY SKIN AT FORWARD KEEL STA 588 TO STA 667 HAS SEVERAL AREAS OF CORROSION UNDER LONGERONS. CORRODED SKIN REPLACED IAW SRM 51.30.SDR MWEA95457Angle · crackedDURING D-CHECK, FOUND THE LT CANTED KEEL BOTTOM ANGLE HAS A CRACK IN THE RADIUS. INSTALLED A NEW ANGLE IAW THE SRM 51-30.SDR MWEA95456Angle · corrodedDURING D-CHECK, FOUND IN THE RT WHEELWELL THE ATTACH Z-ANGLE FOR INBOARD DOOR HINGE CORRODED BEYOND LIMITS. INSTALLED A NEW Z-ANGLE IAW SRM 51-30.SDR MWEA95455Angle · crackedDURING D-CHECK, FOUND IN THE LT KEEL A CANTED ANGLE SUPPORT CRACKED IN THE RADIUS AS STA 604, LONGERON 24L. FABRICATED A NEW FITTING IAW DAC DWG 4956771 AND INSTALLED THAT ANGLE IAW THE SRM 51-30.SDR MWEA95454Doubler · corrosionDURING D-CHECK, FOUND LT WHEELWELL KEEL WEB DOUBLER AT STA 699 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-01, FIG 2, SHEET 3.SDR MWEA95453Splice · crackedDURING D-CHECK, FOUND LONGERON 27R SPLICE WAS CRACKED AT STA 794-STA 813. FABRICATED A NEW SPLICE FITTING AND INSTALLED IAW SRM 51-30-5.SDR MWEA95452Keel Web · corrodedDURING D-CHECK, FOUND LT GEAR KEEL WEB HAD A SMALL AREA OF CORROSION THAT WAS BEYOND LIMITS AT STA 744 TO STA 756. FABRICATED A REPAIR WEB AND INSTALLED IAW SRM 53-01, FIG 2, SHEET 3.SDR MWEA95451Skin · crackedDURING D-CHECK, FOUND FUSELAGE SKIN AT STA 917 AT CARGO DOOR CUT-OUT AT LONGERON 27R HAS A 2.50 INCH CRACK. FABRICATED A DOUBLER AND INSTALLED IT IAW ROD SKETCH 95-11-06-007.SDR MWEA95450Longeron · oversize holeDURING D-CHECK, FOUND ONE LONGERON WITH OVERSIZED HOLES IN SEVERAL PLACES AT STA 570, LONGERON 26L. REPLACED THE LONGERON AND SPLICE IAW SRM 53-04, FIG 2, FROM STA 551 TO STA 579.SDR MWEA95449Intercostal · crackedDURING D-CHECK, FOUND THE INTERCOSTAL BELOW THE CUSP ANGLE AT STA 408 CRACKED. INSTALLED A FABRICATED INTERCOSTAL IAW SRM 53-01, PG 1.SDR MWEA95448Doubler · wornDURING D-CHECK, FOUND BOTH CAPTAIN'S AFT SEAT RAILS REMOVED TO FACILITATE STRAP REPAIR. INSTALLED DOUBLER ON SEAT TRACKS AND MACHINED LOCKPIN HOLES PER SRM 53-05, FIGURE 28. INSTALLED SEAT TRACKS IAW MM 53-40.SDR MWEA95447Beam · crackedDURING D-CHECK, FOUND FORWARD PASSENGER DOOR HAS A 2 INCH CRACK IN A REPAIR ON THE TOP DOOR BEAM ON THE AFT BOTTOM SIDE. REPAIRED CRACKED BEAM IAW SRM 52-05, FIGURE 31.SDR MWEA95446Fitting · crackedDURING D-CHECK, FOUND A CRACK IN RT GEAR DOOR ACTUATOR ATTACH FITTING AT BOTTOM OF KEEL AREA COMING OUT OF THE AFT OUTBOARD FASTENER HOLE AT STA 699. REPAIRED THE CRACK AS PER DAC TELEX ORD-SVC-0311/JSS, 27 OCT 95.SDR MWEA95445Keel Web · corrodedDURING D-CHECK, FOUND A 1 INCH DIAMETER CORROSION HOLE IN THE FORWARD KEEL AREA SECONDARY WEB AT LONGERON 30 FROM STA 604 TO STA 639. REPLACED THE FORWARD KEEL WEB PLATING IAW SRM 51-30.SDR MWEA95444Fitting · corrodedDURING D-CHECK, FOUND LT AFT KEEL AT STA 756, LONGERON 30L HAS A CORRODED END FITTING.SDR MWEA95443Fitting · corrodedDURING D-CHECK, FOUND RT AFT KEEL AT STA 756, LONGERON 30R, HAS A CORRODED END FITTING. DRILLED UP AND INSTALLED NEW FITTING PER SRM 51-30-1.SDR MWEA95442Fitting · crackedDURING D-CHECK, FOUND RIGHT AFT KEEL AT STA 756, LONGERON 29R HAD A CRACKED END FITTING. MAINTENANCE INSTALLED A NEW END FITTING IAW SRM 51-30-1, SRM 51-30-5.SDR MWEA 95473Longeron · corrodedDURING D-CHECK, FOUND CORROSION IN LONGERON 20 IN RT MLG WHEELWELL WHERE FS FRAME 718 MEETS LONGERON 20. REPLACED LONGERON 20 AS PER THE SRM 51-30.SDR MWEA 95444Fitting · corrodedDURING D-CHECK, FOUND LT AFT KEEL AT STA 756, LONGERON 30L HAS A CORRODED END FITTING.
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