Douglas DC-8-71F
Service difficulty reports · 8,938
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 = 'DC871F' 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 = 'DC871F' 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 UPS00831309Fitting · crackedINSPECTION TYPE:C1 FS 1230 AT LONGERON 18R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS00831308Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 442.185 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.SDR UPS00831307Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 467.232 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.SDR UPS00831306Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 227.335 IS CRACKED AT THE AFT UPPER END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.SDR UPS00831305Fitting · crackedINSPECTION TYPE:C1 FS 857 AT LONGERON 19R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DH SK702-997 AND SRM 51-1-20D.SDR UPS00831304Fitting · crackedINSPECTION TYPE:C1 FS 280, ABOVE LONGERON 27R, THE FLOORBEAM SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-1-21.SDR UPS00831302Fitting · crackedINSPECTION TYPE:C1 FS 1200 AT LONGERON 17R THE INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS00831301Longeron · crackedINSPECTION TYPE:C1 LONGERONG 24L IS CRACKED BETWEEN FS 920 AND 940. STOP DRILLED CRACK AND REPAIRED THE LONGERON IAW SRM 53-2-2, FIG 5.SDR UPS00831300Fitting · crackedINSPECTION TYPE:C1 FS 600 TO 620 AT LONGERON 31R, THE LONGERON SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS00831299Fitting · crackedINSPECTION TYPE:C1 FS 440 TO 460 AT LONGERON 31R, THE LONGERON SPLICE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS00831298Fitting · crackedINSPECTION TYPE:C1 FS 781 AT LONGERON 18R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS00831293Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XS 467.232 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.SDR UPS00831292Shear Tie · crackedINSPECTION TYPE:C1 THE SHEAR TIE AT FS 640 BETWEEN LONGERON 26R AND 27R IS CRACKED. CUT DAMAGED SHEAR TIE AND REPAIRED IAW SRM 53-2-0, FIG 2B.SDR UPS00831291Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 297 AND 304 ARE CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2.SDR UPS00831290Skin · crackedINSPECTION TYPE:C1 LT WING L/E LWR SKIN IS CRACKED AT THE FASTENER HOLE AT XFS 310.25. STOP DRILLED THE CRACK AND REPAIRED THE SKIN IAW EO DC8-5740-4087.SDR UPS00831289Rib · crackedINSPECTION TYPE:C1 LT WING L/E RIBS AT XFS 360.25 AND 366.5 ARE CRACKED AT THE AFT UPPER FASTENERS. STOP DRILLED THE CRACKS AND REPAIRED THE RIBS IAW SRM 57-2-0, FIG 2.SDR UPS00831283Fitting · crackedINSPECTION TYPE:C1 LONGERON 19R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AT FS 1260. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.SDR UPS00831282Skin · crackedINSPECTION TYPE:C1 LT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED THE SKIN IAW EO DC8-5740-4087.SDR UPS00831281Skin · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN INTERNAL DOUBLER IS CRACKED AT ACCESS PANEL 524B. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21.SDR UPS00831280Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 379.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.SDR UPS00831279Skin · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN, INTERNAL DOUBLER AT XS 429 IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769891 AND SRM 51-1-20D.SDR UPS00831278Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XILD .7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.SDR UPS00831276Rib · crackedINSPECTION TYPE:C1 RT WING L/E RIB AT XFS 597.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED THE CRACK AND REPAIRED THE RIB IAW SRM 57-2-0, FIG 2.SDR UPS00831275Skin · crackedINSPECTION TYPE:C1 RT WING L/E LWR SKIN AT XFS 598 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED THE CRACK AND REPAIRED THE SKIN IAW EO DC8-5720-4087.SDR UPS00831274Access Panel · corrodedINSPECTION TYPE:C1 RT WING L/E AT THE ACCESS PANEL 518A INTERNAL DOUBLER HAS HEAVY EXFOLIATION CORROSION UNDER THE NUTPLATE CHANNEL. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IWA DWG 3641257 AND SRM 51-1-21.SDR UPS99831236Slide · inoperativeINSPECTION TYPE:N/A, L-1 DOOR EVAC SLIDE INOP REF M183941.SDR UPS00831297Fitting · corrodedINSPECTION TYPE:C1 LT W/W FITTING AT FS 879 ABOVE LONGERON 24 HAS HEAVY CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0, FIG 8.SDR UPS00831288Skin · crackedINSPECTION TYPE:C1 LT WING L/E UPPER SKIN AT XFS 310.25 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED THE SKIN IAW SRM 57-2-1, FIG 38.SDR IXXA9900035Connector · failedAFTER TAKEOFF FROM GDL TO TOL, WHEN THE LANDING GEAR WAS RETRACTED THE LANDING GEAR DOOR UNSAFE LIGHT WAS INTERMITTENTLY FLASHING THEN EXTINGUISHED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTESDR UPS00831287Fitting · crackedINSPECTION TYPE:C1 FS 683 AT RBL 24, THE FLOOR SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE FITTING IAW DWG 5773275 AND SRM 51-1-20D.SDR IXXA9900034Wire · brokenEN ROUTE FROM ICT TO GDL, THE LANDING GEAR DOOR UNSAFE LIGHT ILLUMIATED AFTER A SUCCESSFUL LANDING GEAR UPLATCH CHECK WAS ACCOMPLISHED. THE FLIGHT CREW CYCLED THE GEAR WITH THE WARNING INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO GDL FOR AN UNEVENTSDR UPS99831233Battery Pack · dischargedINSPECTION TYPE:N/A, EMER EXIT LIGHTS FAILED TO DISARM. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01. SYSTEM OPS CHECKS NORMAL.SDR UPS99831231Light · intermittentEMERGENCY EXIT LIGHT DOES NOT REMAIN ILLUMINATED AFTER DISARM CHECK ON SHUTDOWN CHECKLIST. CYCLED EMERGENCY LIGHT SWITCH. LIGHT OPS CHECK NORMAL.SDR UPS99831209Rudder · out of rigINSPECTION TYPE:N/A, PILOT REPORT, RUDDER WENT FULL RT DEFLECTION ON APPROACH. COMPLETED ECA 04957 FOUND RUDDER CONTROL SYSTEM OUT OF RIG. RIGGED PER ECA. OPS CHECKS GOOD PER MM 22-10-00.SDR UPS99831196Unknown · smokeINSPECTION TYPE:N/A, DURING PREFLIGHT INSPECTION CREW REPORTED SMOKE IN COCKPIT.SDR UPS99831192Actuator · leakingINSPECTION TYPE:N/A, AFTER LANDING WHEN PULLING INTO PARKING RES PRESSURE LIGHT ILLUMINATED AND THEN FLIGHT CONTROL MANUAL LIGHTS. ONLY HAD ACCUMULATOR PRESSURE TO STOP AIRCRAFT. FLAPS DID NOT RETRACT. REMOVED AND REPLACED INBOARD LT FLAP ACTUATOR, OPS CK ASDR 2000ZZZX180Bolt · mismanufacturedDURING REPLACEMENT OF RT MLG ATTACH FITTING (TRUNNION) WHILE INSTALLING LOWER REAR AUXILIARY SPAR CAP TO TRUNNION, 'NEW CONDITION' BOLT, P/N NAS-638-39, CRACKED WHILE TURNING INTO POSITION. THIS BOLT WAS ONLY BEING RUN IN AT TIME OF FAILURE, NOT TORQUED. ACFSDR RRXA991590Relay · malfunctionedNO SPOILER PRESSURE WHEN GEAR EXTENDED OR SPOILER SW HELD IN OVERRIDE. WHEN SPOILER PUMP SWITCH WAS PLACED TO OVERRIDE A STRONG ODOR LIKE ELECTRICAL WIRING OVERHEATING WAS NOTICED. REMOVED AND REPLACED RELAY R2-217. SPOILER SYSTEM OP CHECKS NORMAL ON GROUNDSDR UPS99831148Cowl · damagedINSPECTION TYPE:N/A, UPON LANDING NUMBER 3 AND 4 ENGINE COWLS CONTACTED RUNWAY. *S/D* REMOVED AND REPLACED NUMBER 3 AND 4 ENGINE AND DAMAGED FAN COWLS PER MM 71-10-02 AND TC 9071-1, 9071-2. PERFORMED ENGINE RUNS PER TC 9071-2 AND 9071- 3. REFER TO LOG PAGESDR IXXA9900033Fuel Cell · contaminatedEN ROUTE FROM ONT TO SAN, THE NUMBER ONE ENGINE FLAMED OUT AT THE TOP OF CLIMB. THE FLIGHT CREW RELIT THE ENGINE FOLLOWING COMPANY PROCEDURES, THE FLIGHT CONTINUED TO SAN FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE IN ACCORDANCE WITH THE CFM SDR UPS99831146Light · inoperativeEMERGENCY EXIT LIGHTS FAILED TO COME ON DURING PREFLIGHT CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PN ON 5208458-503, PN OFF 570845 8-503 SN ON 976 SN OFF 2054, OPS CHECK GOOD.SDR UPS99831124#4 Pylon · leakingINSPECTION TYPE:SV FUEL LEAKING AT NR 4 PYLON AREA FROM FWD SPAR TO REAR SPAR, LOWER SURFACE OF WING. REMOVED I/B AND O/B SKATE ANGLES, T-DOUBLERS, L/E SKIN PANEL, INTERNAL FITTINGS LOCATED AT CANT BLKHDS STA 495 AND 508. INJECTED FRONT SPAR, CTR SPAR AND STSDR IXXA9900030Control Valve · out of adjustEN ROUTE FROM IAH TO DFW, DURING THE GEAR UPLATCH CHECK THE NOSE GEAR FAILED AND EXTENDED. THE FLIGHT CREW CYCLED THE GEAR TO PERFORM A SECOND CHECK WITH NO SUCCESS. THE FLIGHT CONTINUED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE NOSE LANDISDR RRXA991790Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 660 TO STA 750. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSIONSDR RRXA991789Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 750 TO STA 860. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSIONSDR RRXA991788Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 40 TO STA 80 AND BETWEEN BL 56L TO BL 68L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW SDR RRXA991787Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 1240 TO STA 1348 AND BETWEEN BL 48L TO BL 62L. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL SDR RRXA991786Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL BETWEEN STA 340 TO STA 346. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC-8 SRM 53-2-3. CORROSIONSDR RRXA991779Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT STA=-69 BETWEEN BL=0 TO BL=45L AND WL-9.5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED DER SDR UPS99830989Intercom · inopINSPECTION TYPE:N/A, F/O'S OXYGEN MASK INTERCOM DOES NOT WORK. REMOVED AND REPLACED F/O'S O2 MASK. PERFORMED LEAK CK AND OPS CK GOOD PER MM 35-00.
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