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 UPS03840027Skin · crackedINSPECTION TYPE:C2 REMOVE STEEL DOUBLER FROM L-2 DOOR LOWER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 18. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AROUND CUTOUT. FABRICATED AND INSTALLED DOUBLERS AND FILLER IAW SRM 53-2-0 FIG 18.SDR UPS03840032Aileron · crackedINSPECTION TYPE: C2, LT WING OUTBOARD AILERON L/E UPPER SKIN IS CRACKED AT XA 684. REMOVED, FABRICATED AND REPLACED SKIN SECTION IAW SRM 57-8-0 FIG 4.SDR UPS03840028Rib · crackedINSPECTION TYPE: C2, RT LEADING EDGE RIB REPAIR DOUBLER IS CRACKED AT XFS 385.25. REMOVED DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 57-2-0 FIG 2.SDR IXXA0200157OCylinder · leakingAFTER TAKEOFF FROM DEN, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC SYSTEM QUANTITY. THE FLIGHT CREW RETURNED TO DEN FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A LEAK AROUND THE LEFT AILERON PACK. MAINTENANCE REPLACED TSDR UPS03840062Longeron · crackedINSPECTION TYPE: C2, STA 70 LONGERON 30R IS CRACKED AT END FITTING. TRIMMED OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SAA SK 701-098.SDR IXXA0200156OLink · broken!DURING LANDING AT ANC FROM SEA, THE FLIGHT CREW HEARD A LOUD NOISE FOLLOWED BY AIRCRAFT ROLL THE FLIGHT CREW CONTINUED WITH AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED A BROKEN FLAP ACTUATOR ATTACH BRACKET ON THE LEFT WING. MAISDR UPS02839989Engine · flamed outNR 3 ENGINE FLAMED OUT IFSD AT 35000 FT N1 WINDMILLING AT 30 PERCENT N2 AT 15 PERCENT OIL PRESSURE = 1PSI, QUANTITY AND TEMP NORMAL TIME = 1235 TIME 1340 N1 = 14.5 PERCENT N2 = 0 OIL PRESSURE 0. PERFORMED T/S 71-00-00 PG 165-167, ADJUSTED GROUND AND FLIGHT IDSDR UPS02839983Smoke Detector · will not testINSPECTION TYPE: PFLT, MAIN CARGO DECK SMOKE DETECTORSPAA0200058S NR 1, 5, 6, 7 WILL NOT PROPERLY SELF TEST. REMOVED AND REPLACED SMOKE DETECTOR AMPLIFIER.SDR UPS02839967Web · bulgedINSPECTION TYPE: PFLT, LT W/W AREA HAS 3 POPPED RIVETS AND BULGE IN WEB. REMOVED 2 SECTIONS OF PRESSURE PANEL WEB IN LT WW AT STA 902. REMOVED CORROSION FROM FLOORBEAM FS 902 PER EO DC83107989 A-2. VERIFIED CORROSION REMOVAL & PERFORMED ULTRASOUND THICKNESS SDR UPS02839976Battery Pack · inoperativeINSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW MM 33-50-01.SDR UPS02839929Floorbeam · corrodedSTA 990, RT SIDE OUTBOARD FLOORBEAM LOWER FLANGE CORRODED POSSIBLE FERRY FOR REPAIR. FABBED REPAIR PARTS IAW REO G08940, ALODINED & PRIMED IAW DC8 SRM 51 -1-8 FABBED STIFFENER SPLICES AND STRAPS IAW DAC DWG SR08530029, INSTALLED REPAIR SPLICES AND STIFFENERSDR UPS02839928Pressure Panel · corrodedBULGE AND POPPED FASTENERS IN RT W/W PRESSURE PANEL POSSIBLE FERRY FOR REPAIR. FABBED REPAIR PARTS IAW REO G08940, ALODINED & PRIMED IAW DC8 SRM 51 -1-8 FABBED STIFFENER SPLICES AND STRAPS IAW DAC DWG SR08530029, INSTALLED REPAIR SPLICES AND STIFFENER IAW DC8SDR UPS02839923Battery Pack · dischargedINSPECTION TYPE:PFLT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CK OK.SDR UPS02839925Finger Doubler · corrodedINSPECTION TYPE: LNSV, RIVET POPPED ON RT FWD SECTION OF FUSELAGE NEXT TO D10 CONDITIONED AIR DOOR. REMOVED POPPED RIVET AT STA 8 AND FOUND FINGER DOUBLER SEVERLY CORRO DED. FABBED NEW FINGER DOUBLER IAW DAC DWG 5613862 MATERIAL ID 02570 75T6 PO 0349922 IAW SDR IXXA0200154SEngine · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DISCOVERED IN THE # 3 ENGINE INBOARD THRUST REVERSER HALF BLOCKER DOOR SUPPORT RING AT THE 11 O'CLOCK POSITION. REPAIR ACCOMPLISHED REMOVAL STOP DRILLED CRACK FABRICATION AND INSTALLATION OF REPAIR ANGLE IN ACCORDSDR UPS02839869Battery · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP WHEN SWITCH PLACED IN ARM POS AND BAT/EXT POWER SWITCH IN BAT FAILS TEST REF PS CHK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT, OPS CHK GOOD REF 33-50-02.SDR UPS02839853Control Cable · out of rigINSPECTION TYPE:N/A AFTER GEAR RETRACTION WITH GEAR HANDLE IN THE "UP" POSITION THE DOORS NOT LATCHED LIGHT IS ILLUMINATED. THE LT MLG DOOR ALTERNATE AMBER LIGHT IS ILLUMINATED. GEAR HAD TO BE CYCLED SEVERAL TIMES TO GET THE DOORS NOT LATCHED LIGHT. RIGGED SDR IXXA0200092OPitot Tube · cloggedAFTER TAKE OFF FROM BRO, THE FLIGHT CREW NOTED A DIFFERENCE BETWEEN THE NUMBER ONE AND NUMBER TWO AIRSPEED INDICATORS THAT INCREASED AS THE AIRCRAFTS ALTITUDE INCREASED. THE FLIGHT CREW ADVISED AND COORDINATED WITH ATC TO DETERMINE THE NUMBER TWO AIRSPEED INDSDR UPS02839890Strap · crackedINSPECTION TYPE: C2, RT WING HAS A CRACKED LONGERON 64 END FITTING-STRAP, AND LOWER SPAR IS CRACKED 1/2 INCH FROM EDGE OF SPAR TO FASTENER HOLE AT XRS 450. NDT VERIFIED 1/2 INCH CRACK AT XRS 450 FROM EDGE OF SPAR TO FASTENER HOLE, REMOVED, FABRICATED AND INSSDR UPS02839838Fitting · corrodedINSPECTION TYPE:C2 STA 300 BETWEEN LONG 35L TO 36 BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.SDR IXXA0200090ODuct · damagedAFTER TAKE OFF FROM ANC, THE FIRE WARNING LIGHT ILLUMINATED AND THE AUDIO WARNING SOUNDED FOR THE NUMBER THREE ENGINE. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SECURED THE ENGINE. THE FLIGHT RETURNED TO ANC FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPESDR IXXA0200153SDoor Actuator · damagedDURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED ON THE UPPER FORWARD L-1 DOOR JAMB STATION 25. REPAIR ACCOMPLISHED REMOVAL OF TEMPORARY REPAIR AND DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER AND TRIPLER IN ACCORDANCE WITH SDR IXXA0200152SDoor Frame · damagedDURING ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED IN THE LOWER FORWARD L-2 DOOR JAMB STATION 1620. REPAIR ACCOMPLISHED REMOVAL OF TEMPORARY REPAIR AND DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER AND TRIPLER IN ACCORDANCE WITSDR UPS02839844Longeron · corrodedINSPECTION TYPE:C2 STA 300-305 LONG 35L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON 35L SECTION BETWEEN STA 290 TO 330 IAW SRM 53-2-2 FIG 10.SDR UPS02839843Longeron · corrodedINSPECTION TYPE:C2 STA 300-305 LONGERON 35R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STA 290 TO 330 AT LONG 35R IAW SRM 53-2-2 FIG 10.SDR UPS02839832Fitting · crackedINSPECTION TYPE:C2 STATION 1040-1050 LONGERON 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257, AND SRM 51-1-20D.SDR UPS02839823Shear Tie · crackedINSPECTION TYPE:C-2 SHEAR TIE AT FS 1680 CRACKED AT LONG 18L. REMOVED AND REPLACED SHEAR TIE IAW DAC DWG 5640243-1.SDR UPS02839816Seat Track · wornINSPECTION TYPE:C-2 2ND OBSERVER'S FWD SEAT TRACK LOCK PIN HOLES WORN. REMOVED OLD SEAT TRACK IAW DC8 SRM 51-3-0. DRILLED NEW SEAT TRACK IAW DC8 SRM 51-1-24. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0.SDR UPS02839882Fitting · crackedINSPECTION TYPE:C-2 LT WING STR 51, O/B FWD STRINGER END FITTING IS CRACKED. RECEIVED NEW FITTING LOCATED & DRILLED FITTING IAW DC 8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0.SDR UPS02839847Fitting · crackedINSPECTION TYPE:C2 STA 70 LONG 22L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4611159, AND SRM 51-1-20D.SDR UPS02839840Fitting · corrodedINSPECTION TYPE:C2 STA 320 BETWEEN LONG 33L TO 34L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.SDR UPS02839839Fitting · corrodedINSPECTION TYPE:C2 STA 300 BETWEEN LONG 33L TO 34L BATHTUB FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755822, AND SRM 53-2-0 FIG 2D.SDR IXXA0200141SSupport · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE INBOARD AND OUTBOARD LOWER AREA OF THE NR 2 FLAP HINGE UPPER SUPPORT ON THE RIGHT WING. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA IN ACCORDANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL AND BOSDR UPS02839881Fitting · crackedINSPECTION TYPE:C-2 LT WING STR 51 I/B END, STR END FITTING CRACKED. RECEIVED NEW FITTING LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-3-0 & 51-1-20D.SDR IXXA0200089ORod End · strippedAFTER TAKE OFF FROM BFI, THE LANDING GEAR DOOR NOT LATCHED LIGHT AND THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR AND PERFORMED A SUCESSFUL UP LATCH CHECK, BUT THE LIGHTS REMAINED ILLUMINATED. SDR IXXA0200151SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED OF THE RIGHT AFT CORNER OF THE CARGO DOOR. REPAIR ACCOMPLISHED REMOVAL OF TEMPORARY REPAIR AND DAMAGED AREA. FABRICATION AND INSTALLATION OF DOUBLER AND TRIPLER IN ACCORDANCE WITH DOUGLASSDR IXXA0200150SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION, A CRACK WAS DISCOVERED ON THE LOWER FORWARD CORNER OF THE AFT RIGHT SERVICE DOOR STATION 1620. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION REPAIR OF DOUBLER AND TRIPLER IN ACCORDANCE WITH DOSDR UPS02839888Longeron · crackedINSPECTION TYPE:C-2 MAIN CABIN AT FS 1655 LONGERON 11R IS CRACKED. REMOVED AND REPLACED LONGERON PER DC8 SRM 51-1-21 AND 51-1-20D.SDR UPS02839880Floorbeam · corrodedINSPECTION TYPE:C-2 AFT ACCY COMPARTMENT FS 1680 AT LBL 48 LOWER SURFACE OF UPPER FLOORBEAM FLANGE IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, BEYOND LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR ANGLES AND FILLER IAW DC8 SRM 53-2-0 FIG 1B SHEETSDR UPS02839828Longeron · corrodedINSPECTION TYPE:C2 AFT ACCY COMPARTMENT LONG 33L CORRODED BEYOND LIMITS BETWEEN STATION 1540 TO 1545. REMOVED LONGERON SECTION FROM STA 1515 TO 1550 AT LONG 33L, FABRICATED AND INSTALLED LONGERON SECTION AND SPLICES IAW SRM 53-2-2, FIG 10, 53-4-1 FIG 43.SDR IXXA0200149SSkin · lightning strikeDURING A ROUTINE C-CHECK INSPECTION, EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 280 LONGERON 10R AND FUSELAGE STATION 340 LONGERON 9R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCSDR UPS02839879Skin · crackedINSPECTION TYPE: C-2, R-1 FORWARD SERVICE DOOR CUTOUT, UPPER FORWARD CORNER HAS CRACK INDICATION ON EXTERNAL SKIN. FABRICATED -23 FILLER, -15 AND -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 1 4. ALODINED AND PRIMED FILLER AND DOUBLERS IAW DC8 SRM 51-1-8. INSTALLED SDR UPS02839850Door Frame · crackedINSPECTION TYPE:C2 A-PIT DOOR FRAME IS CRACKED AFT SIDE OF 3RD UPPER HOOK FROM FWD END ON DOOR AT APPROX STA 300 AT LONG 23R ON DOOR. REMOVED FRAME SECTIONS, FABRICATED AND INSTALLED 2EA FRAME SECTIONS AND DOUBLERS IAW SRM 52-2-0 FIG 2 AND DWG 9754100.SDR UPS02839829Fitting · crackedINSPECTION TYPE:C2 RIGHT HORIZONTAL STAB LOWER PLANK FITTING IS CRACKED AT XFS 46. REMOVED AND REPLACED FITTING IAW DWG 3701427, AND SRM 51-1-21.SDR UPS02839817Skin · corrodedINSPECTION TYPE:C-2 LT WING LOWER WING SKIN, O/B OF FUEL VENT PANEL, FWD OF REAR SPAR, IS CORRODED ON EXTERIOR SURFACE. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER IAW REO G08852 AND DC8 SRM 57-2-0 FIG 2A, AND INSTALLED DOUBLER REPAIR IAW REO G08852 AND DC8SDR IXXA0200148SSkin · lightning strikeDURING A ROUTINE C-CHECK INSPECTION, EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 120 LONGERON 9R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL MANUAL AND DSDR IXXA0200147SSkin · lightning strikeDURING ROUTINE C-CHECK INSPECTION EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 600 LONGERON 7R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF INTERNAL FINGER DOUBLERS IN ACCORDANCE WITH DOUGLAS STRUCTURAL MANUASDR IXXA0200146SSkin · lightning strikeDURING ROUTINE C-CHECK INSPECTION, EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 460, 480 & 520 LONGERONS 7R-8R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURASDR IXXA0200145SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, A TEMPORARY REPAIR WAS DISCOVERED ON THE FORWARD SERVICE DOOR AT STATION 400. REPAIR ACCOMPLISHED REMOVAL OF TEMPORARY REPAIR AND DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCSDR IXXA0200144SSkin · lightning strikeDURING ROUTINE C-CHECK INSPECTION EVIDENCE OF LIGHTNING STRIKES WERE DETECTED ON FUSELAGE STATION 180 LONGERONS 9R. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL MANUAL AND DRA
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