Douglas DC-8-73F
Service difficulty reports · 15,471
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 = 'DC873F' 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 = 'DC873F' 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 UPS98825507Web · crackedINSPECTION TYPE-D, HEAVY CORROSION AND CRACK IN FLOOR WEB LT CUSP AREA EXTENDING UNDER FLOOR SUPPORT FITTING FROM FS 260 TO 280. REPAIRED WEB IAW SRM ADDN DC8-5330-2159-B.SDR UPS98825483Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT STA XFS 566.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-20-0.SDR UPS98825482Fitting · crackedINSPECTION TYPE-D, FS 1160 RT FLOORBEAM END FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3754946.SDR UPS98825432Doubler · corrodedINSPECTION TYPE-D, RT FINGER DOUBLER UNDER STR 31R IS CORRODED BETWEEN FS 200 TO 220 LWR FWD PIT. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-4-1 AND 51-1-21.SDR UPS98825431Support · corrodedINSPECTION TYPE-D, RT FLOORBEAM SUPPORT TO FRAME IS CORRODED OUT OF LIMITS AT FS 120 FWD LWR PIT. REMOVED AND REPLACED FITTING IAW SRM 51-01-20.SDR UPS98825428Skin · crackedINSPECTION TYPE-D, LT HORZ STAB I/B L/E SECTION EXTERIOR SURFACE AT STA XE29 CRACKED. REPAIRED IAW SRM 55-2-0.SDR UPS98825423Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT STA XFS 772.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.SDR UPS98825419Cusp · crackedINSPECTION TYPE-D, LT CUSP FROM FS 120 TO 130 IS CRACKED. REPAIRED IAW SRM 51-1-21 AND EO DC8-5330-2159-B.SDR UPS98825418Skin · crackedINSPECTION TYPE-D, LT HORIZ STAB I/B L/E SECTION SKIN EXTERNAL SURFACE AT APPROX STA XFS 293 HAS CRACK. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 55-3-1, 53-2-0, AND 51-1-20.SDR UPS98825415Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 828.750. REPAIRED IAW SRM 57-2-0.SDR UPS98825414Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER HOLE AT STA 778.750. ALSO LWR ARM CRACKED BY AFT FASTENER. REPAIRED IAW SRM 57-2-0.SDR UPS98825413Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 810.000. REPAIRED IAW SRM 57-2-0.SDR UPS98825412Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER HOLE AT STA 753.750. REPAIRED IAW SRM 57-2-0.SDR UPS98825411Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB CRACKED AT UPPER ARM BY AFT FASTENER HOLE AT STA 760.000. REPAIRED IAW SRM 57-2-0.SDR UPS98825410Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER HOLE AT STA 772.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825409Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 722.500. REPAIRED IAW SRM 57-2-0.SDR UPS98825408Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 728.750. REPAIRED IAW SRM 53-2-0 AND 57-2-0.SDR UPS98825407Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 728.750. REPAIRED IAW SRM 53-2-0.SDR UPS98825509Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT STA XOLDI 6.225 (ABOVE THE PNEU DUCT) IS CRACKED. THE CRACK IS OVER 2 INCHES LONG. REPAIRED IAW SRM 57-2-0.SDR UPS98825485Rib · crackedINSPECTION TYPE-D, RT WING L/E RIB UPPER ARM CRACKED BY AFT FSTA XS 454.976. REPAIRED IAW SRM 57-2-0.SDR UPS98825481Skin · crackedINSPECTION TYPE-D, LT WING L/E SKIN ABOVE THE NR 1 PYLON IS CRACKED. REPAIRED IAW SRM 57-2-1A.SDR UPS98825406Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT STA XS 435.788 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.SDR UPS98825405Rib · crackedINSPECTION TYPE-D, LT WING L/E RIB AT STA XFS 397.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-3-3 AND SRM ADDN DC8-5720-4087.SDR UPS98825548Skin · crackedINSPECTION TYPE-D, SKIN CRACKED IN UPPER FWD CORNER OF FWD GALLEY DOOR. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SRM 53-2-0, 51-1-21, AND 51-1-20D.SDR UPS98825430Fitting · crackedINSPECTION TYPE-D, CARGO COMPARTMENT AFT LWR X SLIDE DOOR T-LATCH BRACKET CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.SDR UPS97825352Door Mechanism · inoperativeON LANDING ANC, UNABLE TO OPEN CREW ENTRANCE DOOR, HAD TO BE OPENED FROM THE OUTSIDE ADJUSTED DOOR PER MM 52-11-01. OK FOR SERVICE.SDR UPS97825348Tr Unit · inopINSPECTION TYPE-N/A, ON LANDING THRUST REVERSERS WOULD NOT DEPLOY. THRUST REVERSER HYDRAULIC VALVE C/B POPPED. REMOVED AND REPLACED T/R HYD S/O VALVE ASSY PER DC8 MM 78-37-03, SYS OPS CKS NORMALLY. INSPECTED TIRES AND BRAKES AND FOUND ALL TO BE OK FOR CONTISDR SRAA971210Hyd Line · failedDURING FLIGHT 082, APPROX 3 HRS INTO FLIGHT FOR BRU, HYD QTY INDICATOR DROPPED TO 5.5 GAL WITH SOME FLUCTUATION IN PRESSURE, CONTINUED FLIGHT IAW QRH AND LANDED SAFELY AT BRU. INSPECTED AIRCRAFT AND FOUND HYD LINE AT SWIVEL GLAND TOP ON LT MLG STRUT CRACKED ASDR UPS97825341Bungee Actuator · leakingINSPECTION TYPE-N/A, AIR TURNBACK DUE TO HYD LEAK SHORTLY AFTER TAKEOFF. LOST HYD DOWN TO AUX PUMP QUANTITY. FOUND LMLG BUNGEE ACTUATOR LEAKING. REPLACED ACTUATOR PER MM 32-32-03 AND SERVICE BULLETIN 32-133. PERFORMED GEAR SWING, OPS AND LEAK CHK GOOD.SDR SRAA971208Interlock Cable · inoperativeON CLIMB-OUT OF BRU FLIGHT 081, DURING GEAR RETRACTION, DOORS NOT LATCHED WARNING LIGHT CAME ON. ACCOMPLISHED AIR TURN BACK TO BRU AND LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FOUND THE RT MLG UPLOCK MICROSWITCH INOP. REPLACED THE RT UPLATCH INTERLOCSDR UPS97825331Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, OPS CK NORMAL.SDR SRAA971205Switch · brokenDURING POST FLIGHT INSPECTION, FOUND THE EMERGENCY EXIT LIGHT SWITCH BROKEN, IN ARMED POSITION. REPAIRED SWITCH AND OPS CHECKED GOOD PER MM CH 33-00 AT BRU.SDR SRAA971201Target · off targetAFTER TAKEOFF, DURING GEAR UPLATCH CHECK DOORS NOT LATCHED WARNING LIGHT CAME ON. RECYCLED GEARS SEVERAL TIMES WITH SAME RESULTS. CONTINUED FLIGHT AT 230 KNOTS AND LANDED WITHOUT INCIDENT. FOUND MLG DOOR TARGETS OUT OF ADJUSTMENT. ADJUSTED TARGETS AND CHECSDR DHL97802009Door · out of adjustBELLY DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. LIGHT WENT OUT WHEN DEPRESSURIZING AIRCRAFT TO CABIN ALT OF 4,500 FEET. REPRESSURIZING, LIGHT CAME BACK ON. RERIGGED DOOR PER M/M 52.SDR DHL97802008Inu · failedNR 1 INS DRIFTED OFF 20 MILES WITHIN 1 HOUR OF DEPARTURE. UPDATED WAS INITIATED WITHIN 5 MIN. BOTH INS BEGAN FLASHING, BOTH ALERT AND WARNING LIGHTS ILLUMINATED, THEN EXTINGUISHED. MALFUNCTION CODES WERE 8010301 AND 0001. REMOVED AND REPLACED NR 1 INU, OPSSDR UPS97825316Battery Pack · dischargedINSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK LIGHTS.SDR SRAA971110Switch · failedON CLIMBOUT, DURING GEAR RETRACTION THE LEFT HAND MAIN GEAR DOOR HAD UNSAFE WARNING LIGHT. RECYCLED GEAR SEVERAL TIMES LIGHT WOULD NOT GO OUT. DUMPED FUEL AND ACCOMPLISHED AIR TURNBACK TO HRE WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FOUND LT MLG DOOR SWITCHSDR UPS97825321Transformer · failedINSPECTION TYPE-N/A, ON DESCENT TO ONTARIO NOTICED SPARKS AND SMOKE FOR A SHORT MOMENT IN OVERHEAD PANEL BEHIND THE FIRE HANDLES. FOUND RED OVERHEAD SWITCH PANEL INTRAL LIGHTS C/B OUT. NO FURTHER SMOKE WAS DEVELOPED. CONNECTOR DC 26F-10-6SW BURNT. REMOVED SDR RRXA97316Switch · malfunctionedRT MAIN LANDING GEAR DIDN'T EXTEND ON FINAL, RECYCLED GEAR 3 TIMES, GEAR FINALLY DOWN. REMOVED AND REPLACED RT DOWNLOCK SWITCH. RT MAIN LANDING GEAR DOWN IND GREEN LIGHT, OPS CHECKS GOOD.SDR UPS97825244Fitting · crackedDURING D CHECK INSPECTION, FOUND T BOLT BACKUP FITTING CRACKED AT F/S 332. REMOVED CRACKED FITTING, DRILLED, TREATED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 53-1-0, 51-1-20D.SDR RRXA97314Current Detector · failedON ROTATION, PITOT HEAT SENSING BOX AND CAPT'S PITOT HEAT C/B AND ALT PITOT HEAT C/B POPPED. COCKPIT FILLED WITH SMOKE. REMOVED AND REPLACED CURRENT SENSING DET IAW DC8 MM 30-30-1. REMOVED AND REPLACED STALL TRANSDUCER IAW DC8 MM 34-16-1. CHECKED GOOD IAW SDR DHL9780264CSkin · damagedAT C-CHECK, NR 1 ENGINE RT FAN COWLS OUTER SKIN DAMAGED AT LOWER CORNER. TRIMMED DAMAGED AREA AND FABRICATED REPAIR DOUBLER 31.5 X 1 PER DC-8 -70 SRM 71-2-8.SDR DHL9780258CTr Sleeve · wornAT C-CHECK, ENG NR 1 ON RT REV SLEEVE INTERIOR SKIN 30 AFT OF FWD TOP HOLE WORN THROUGH. CUT OUT DAMAGED AREA AND FABRICATED REPAIR PER CFM 56 MM 78-31-10. INSTALLED REPAIR PER SRM 51-1-21A, 3 X 3.SDR DHL9780250CVane · delaminatedAT C-CHECK, RT WING I/B FLAP VANE DELAMINATED. REMOVED VANE, REPAIRED AND REINSTALLED PER M/M 27-51-14.SDR DHL9780248CPanel · delaminatedAT C-CHECK, RIGHT WING LOWER SURFACE STA 130 TO 219 PANEL DELAMINATED. REMOVED, REPAIRED PANEL AND INSTALLED PER SRM 51-1-15.SDR DHL9780211CSkin · delaminatedAT C-CHECK, RT WING LOWER T/E O/B AILERON HINGE PANEL INNER SKIN DELAMINATED. INSTALLED REPAIRED PANEL PER SRM 51-1-15.SDR DHL9780208CSkin · dentedAT C-CHECK, RT WING I/B T/E PANEL AFT OF MLG OUTER SKIN HAS TEMP REPAIR, DENTS AND SKIN SURFACE CORR. REMOVED, REPAIRED AND INSTALLED PANEL PER SRM 56-1-21.SDR DHL9780206CPanel · delaminatedAT C-CHECK, LT WING T/E PANEL BETWEEN XRS 172 AND 255 HAS DELAMINATION AND LOWER SURFACE HAS INTERM REPAIR. REMOVED DAMAGED PANEL, REPAIRED AND INSTALLED PER SRM 51-3-0.SDR DHL9780260CSkin · damagedAT C-CHECK, LEFT WING UPPER T/E PANEL ABOVE AT I/B GROUND SPOILER HOLE. TRIMMED DAMAGED AREA OF SKIN AND FABRICATED REPAIR DOUBLER PER SRM 57-2-1, 7.2 X 5.0.SDR DHL9780247CPanel · delaminatedAT C-CHECK, RT WING T/E LOWER SURFACE DELAMINATED FROM STA 97 TO 130. REMOVED DELAMINATED PANEL AND REPAIRED PER SRM 51-3-0.
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