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 UPS04842391Fitting · crackedINSPECTION TYPE:C1 STATION 850 LONGERON 5R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D, AND M/M 20-14-00.SDR UPS04842376Strap · crackedINSPECTION TYPE:C1 FRAME INTERCOSTAL STRAP IS CRACKED AT STATION 940 LONG 14R. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5895045 AND SRM 51-1-21.SDR UPS04842375Strap · crackedINSPECTION TYPE:C1 FRAME INTERCOSTAL STRAP IS CRACKED AT STATION 940 LONG 14L. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5895045 AND SRM 51-1-21.SDR UPS04842368Fitting · crackedINSPECTION TYPE:C1 STATION 680 AFT SIDE LONG 3L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D & 51-3-0.SDR IXXA0400079SDoor · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND AN INTERIM REPAIR ON THE UPPER AFT CORNER OF AFT PASSENGER DOOR STA 1660.000 L-9L TO L-11L. REPAIR WAS ACCOMPLISHED. THE INTERIM REPAIR WAS REMOVED IAW DC8 SRM 51-1-21 PG 1, FABRICATED A NEW DOUBLER, TRIPLER AND FILLSDR IXXA0400077SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION A CRACK (1 INCH) WAS FOUND ON FUSELAGE EXTERIOR STA 174.000-1745.000, L-16R TO L-17R. REPAIR WAS ACCOMPLISHED. FASTENERS AND EXISTING EXTERNAL DOUBLER WERE REMOVED IAW DC8 SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN IAW DC8 SRSDR IXXA0400071SSkin Panel · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CTR LE UPPER SURFACE CORRODED AT STA XFS 341.500. REPAIR WAS ACCOMPLISHED, REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-8 PG 17-18 AND 57-2-1 PG 11. TOOK OUT DAMAGED SECTION IAW SRM 57-2-1 FIG. 38, SDR IXXA0400070SPanel · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WIND IB LE SLANT PANEL UPPER CAP CORRODED AT SEVERAL AREAS. STA XW.0 - XFS 164.000. REPAIR WAS ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITSDR IXXA0400069SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CENTER LE HAS REPAIR ON UPPER SURFACE, STATION XFS 304.000. THIS REPAIR WAS ACCOMPLISHED IAW SRM 57-2-1 FIG 38 TR NR 57-85, 51-1-21, 51-1-20D. REMOVED DOUBLER AND FABRICATED FILLER AND DOUBLER. CLEANED TREATESDR IXXA0400068SSkin · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT OB WING LE OB SECTION CORRODED AT STA XFS 710.000. THIS REPAIR WAS ACCOMPLISHED IAW DWG V82-R02 AND N/R 0652. REMOVED FASTENERS IAW SRM 51-1-21 PG1. REMOVED CORROSION IAW SRM 51-1-8 PGS. 17-18. FOUND OUT OF LIMITS.SDR IXXA0400067SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING OB LE LOWER SKIN CRACKED .5000 INCH. REPAIR ACCOMPLISHED. REMOVED FASTENERS WITHIN REPAIR AREA IAW SRM 51-1-21 AND 51-1-20D PG1. REMOVED DAMAGED AREA IAW DWG V82-R01. PERFORMED NDT INSPECTION IAW NDT SPM PSDR IXXA0400094SSpar · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND LT WING REAR SPAR DOUBLER UPPER SIDE HAS CRACK DAMAGE AT STA XCW 69.500. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS, ALONG WITH THE DAMAGED AREA IAW DC8 SRM 51-1-20D PG 21 AND DC8 SRM 57-2-6 FIG 15. FABRICATED FILSDR IXXA0400066SSkin · dentedDURING A ROUTINE C-CHECK INSPECTION, FOUND DENTS ON RT WING STATION 660. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1 ALSO REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER 57-2-1 FIG 24 PG 15. CLEANED, TREATED AND PRIMED AREA IAW SRM 51SDR UPS04842340Seat Track · corrodedINSPECTION TYPE: C-1, MAIN CABIN SEAT TRACK G & H AT FS 418 HAS EXFOLIATION. SEAT TRACK AREA DAMAGED RMVD LOCATED AND DRILLED NEW SEAT TRACK SPLICE FITTING AND SPLICE CHANNEL IAW EO DC8 5320-8309-D. INSTALLED IAW EO DC 8 5320-8309D.SDR UPS04842330Fitting · crackedINSPECTION TYPE:C-1 CORROSION AROUND FASTENER HOLE ON L35 RT STA 1040-1060 INTERNAL AFT PIT, REMOVED INTERCOSTAL & CLIP AT STA 1040 - 1060 RT L35 RT IAW DC8 SRM 51-1- 20D. FILLET PANELS 1924 & 191CC IAW DC8 SRM 51-3-1 EVOL LONGERON SPLIC E 51-1-20D, FOUND TO SDR IXXA0400021OComputer · malfunctionedAT V1, 121 KNOTS STALL WARING (SHAKER STICK) WENT OFF. HIGH SPEED ABORT 122 KNOTS BRAKE CHART 28 MILLION FT. LBS. 2.5 HOURS COOLING TIME REQUIRED. CREW RETURNED TO BLOCKS. AN INSPECTION IS ON GOING. AS SOON INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENSDR UPS04842245Connector · inoperativeEMERGENCY LIGHTS INOPERATIVE. FOUND CONNECTOR LOOSE ON BATTERY PACK. RE INSTALLED SAME, SYSTEM TEST OKSDR UPS04842331Seat Track · gougedINSPECTION TYPE: C-1, SEAT TRACK C/H STA 1120-1140 GOUGED, REMOVED GOUGES IAW DC8 SRM 53-2-0 & FOUND TO BE OUT OF LIMITS REMOVED FLOOR PANEL F90 & F94 FOR ACCESS. LOCATE NEW SEAT TRACK DRILLED EXISTING FASTENER HOLES ALODINE & PRIME IAW 51-1-8. LOCATE SEAT TSDR UPS04842312Seat Track · corrodedINSPECTION TYPE: C-1, UPPER CARGO PIT BETWEEN STA 822 TO 837 FLOORBEAM AT STA 822 AT SEAT TRACK (E) IS CORRODED. CUT SEAT TRACK REPAIR FLOORBEAM INSTALLED NEW SEAT TRACK AND 4 EACH FITTING SPLICE.SDR UPS04842329Skin · crackedINSPECTION TYPE: C-1, LEFT HORIZONTAL STAB LEADING EDGE INBD OF CENTER 3 EACH POPPED RIVETS REMOVED & INSTALLED LT HORIZONTAL STAP L/E 331F TO FOM IAW DC8 SRM 51-3 -0. RMVD FASTENERS IAW DC8 SRM 51-1-21A. FOUND SKIN TO BE CRACKED. CUT OUT DAMAGE & FAB REPAISDR UPS04842354Fitting · crackedINSPECTION TYPE: C1, LONGERON FITTING IS CRACKED. REMOVED FITTING, RECEIVED, LOCATED, AND DRILLED FITTING, INSTALLED FIT TING; ALL IAW DC8 SRM 51-1-20D, 51-1-24.SDR UPS04842105Battery · dischargedINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY, OP CHECKED GOOD.SDR UPS04842345Longeron · gougedINSPECTION TYPE: C1, LT MLG WW L34 BOTTOM SIDE GOUGED FWD STA 980. REMOVED ADF PANEL AND LONGERON IAW DC8 SRM 51-3-0 AND 51-1-20D. FABRIC ATED LONG -503 IAW DAC DWG 3750347. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED -503 LONGERON IAW DC8 SRM 51-1-SDR UPS04842347Doubler · corrodedINSPECTION TYPE: C1, FWD LWR CARGO STA 300 TO 308 L33R DOUBLER WITHIN TORQUE BOX CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0 . FABRICATED NEW DOUBLER FROM 7075-T6 .063 IAW DC8 SRM 51-1-24 AND DAC DWG 3254065. ALODINED ANDSDR UPS04842332Fitting · crackedINSPECTION TYPE: C-1, 680 LONGERON 11 LT LOWER AFT FITTING IS CRACKED, REMOVED CRACKED FITTING P/N 4751625-1 IAW DC8 SRM 51-3-0,51-1-20D & 51-1- 21 LOCATED AND DRILLED NEW FITTING IAW DAC DWG 4751625 AND DC8 SRM 51- 1-24 AND INSTALLED IAW DC8 SRM 51-1-20D, 51SDR UPS04842324Doubler · corrodedINSPECTION TYPE:C-1 FWD LWR CARGO STA 300 TC 308 L33R TO L34R DOUBLER HAS CORROSION. REMOVED CORR IAW DC8 SRM 51-1-8. ORIG THICKNESS WAS .063 IAW DAC DWG 3754065. MATERIAL RMVD WAS .020 AND IS OUT OF LIMITS IAW DC8 SRM 53-2-0 FAB NEW DOUBLER FROM 7075-T6 .0SDR UPS04842194Stiffener · crackedINSPECTION TYPE:C1 2 EA DIAGONAL STIFFENERS FOR STA 8 BULKHEAD HAVE PREVIOUSLY CUTOUT DAMAGE ON LOWER ENDS. FABBED REPAIR ANGLE DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D.SDR UPS04842334Seat Track · wornINSPECTION TYPE: C-1, ENGINEERS SEAT TRACKS HAVE ELONGATED HOLES. REMOVED FWD F/E'S SEAT TRACK IAW DC8 SRM 51-3-0 LOCATED AND DRILLED SE AT TRACK IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-3-1SDR UPS04842333Seat Track · wornINSPECTION TYPE: C-1, ENGINEER SEAT TRACKS HAVE ELONGATED HOLES. REMOVED F/E SEAT TRACKS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED FWD AND AFT TRACKS P/N 3657504-1 IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SR M 51-3-1SDR UPS04842328Frame · gougedINSPECTION TYPE: C-1, NLG RT CTR TUNNEL AREA (ACCESS THUR AFT PRESS PAL) FRAME & BRKT GOUGED JUST FWD OF PWR RECP BOX BLEND GOUGE IAW DC8 SRM 53-2-0, FIG 1F ORINGINAL THICKNESS .050 REMAIN ING MATERIAL OF .036 OUT OF LIMITS. ROUNDED GOUGE ON BRAKETT EDGESDR UPS04842336Seat Track · corrodedINSPECTION TYPE: C-1, CORROSION AROUND NUTPLATES & FASTENER FROM STH 1480 TO 1540 AT CUSP LT SIDE OF AFT CARGO COMPT PUT A7763. REMOVED AIR GRILLS CUSP CLOSEOUT & FLOOR TO FOM REMOVED SEAT TRACK ORIG THICKNESS .090 IAW 51-2-0. REMOVED CORR IAW 51-1-8 AFTER BLESDR UPS04842335Intercostal · dentedINSPECTION TYPE: C-1, STA 1240-1260 L35L INTERCOSTAL DENTED. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21 & 51-1-20D MATERIAL ID & FAB OF NEW PART IAW DAC DWG 49758507, HEAT TREATED PART REF LOAD HT041904 -3. ALODINE & PRIMED INTERCOSTAL IAW DC8 SRM 51-1-8. INSTALSDR UPS04842322Channel · crackedINSPECTION TYPE:C-1 RIGHT WING I/B FLAP O/B TRAILING EDGE IS CRACKED. REMOVED CRACKED CHANNEL. FAB NEW CHANNEL IAW DC8 SRM 57-7-1. ALODINED AND PRIMED CHANNEL IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW DC8 SRM 51-3-O,51-3-1,51-1-21 AND 51-1-21ASDR UPS04842351Floorboard · corrodedINSPECTION TYPE: C1, MAIN DECK FLOOR PANEL CORRODED STA 50 LBL 14. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS. FABBED SPLICE PLATES IAW DC8 SRM 53-2-3; LOCATED, DRILLED, AND COUNTERSUNK NEW FLOOR PANEL SECTION IAW DC8 SRM 51-1-24. ALOD & PRIMED IASDR UPS04842338Longeron · corrodedINSPECTION TYPE:C-1 FWD PIT BETWEEN STA 200-300 LONGERON 34R CORRODED RMVD FASTENERS L34R FS 190-300 & FROM SHEARTIES & FRAMES AT FS 200& 220 AT L34R TO FOM. RMVD CORR FROM L34R AT FS 205-217. ORIG THICKNESS IS .092 MAT RMVD .030 MAT REMAINING.062 & IS OUTSDR UPS04842337Fitting · corrodedINSPECTION TYPE: C-1C, FWD PIT- FWD SIDE OF TORQUE BOX (APPROX STA 275) BETWEEN LONGERONS 33R -34 RT ZEE ANGLE CORRODED. REMOVED OLD FITTING PN 3755824-1 IAW DC8 SRM 51-1-20D. RECIVED NEW FITT ING PN 3755824-1 TAG 00702413 DRILLED UP FITTING IAW DC8 SRM 51-1SDR UPS04842352Angle · corrodedINSPECTION TYPE: C1, AFT PIT RT CUSP EXTRUSION CORRODED BETWEEN STA 1000 AND 1020 LONG 21 RT. REMOVED DAMAGED CUSP SECTION IAW TR53-179 STA 990-1030 L21 RT. IAW DC8 SRM 51-1-20D. REC'ED, LOCATED AND DRILLED -3 & -5 REPAIR ANGLES, -7 D OUBLER AND -9 CUSP SECSDR UPS04842350Angle · gougedINSPECTION TYPE: C1, STA 1560-1580 L21L CUSP MEMBRANE GOUGED. REMOVED GOUGE ON CUSP TONGUE IAW DC8 SRM 53-2-0. OUT OF LIMITS. FABRICATED CUSP IAW DAD DWG 9750448. FABRICATED SPLICES IAW REO G09789. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW CUSP SECTSDR UPS04842339Seat Track · brokenINSPECTION TYPE: C-1, SEAT TRACK STA 1700 LOBES BROKEN OFF. SEAT TRACK FOUND OUT OF LIMITS IAW DC8 SRM & UPS EO 5340-12053. REMOVED SEAT TRACK IAW 51-1-200 & 51-30 MAT ID SEAT TRACK P/N 3772660 IAW 53-7-1 LACATED & DRILLED HOLE IN SEAT TRACK F STA 1670-1710 ISDR UPS04842198Bracket · crackedINSPECTION TYPE:C1 RIGHT WING NR 2 SPOILER O/B MOUNT BRACKET CRACKED. REMOVED AND REPLACED RIGHT WING 32 SPOILER O/B MOUNT BRACKET IAW UPS DC8 SRM 51-1-21, 51-1-20D, AND 51-3-1.SDR UPS04842349Fitting · crackedINSPECTION TYPE: C1, MAIN CABIN, FRAME FITTING CRACKED ON BOTH SIDES FS 427 L11L (DOT 6603). REMOVED TEE FITTING TO GAIN ACCESS TO CRACKED FITTING, REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING P/N 3755820- 1 IAW DC8 SRM 51-1-2SDR UPS04842197Longeron · crackedINSPECTION TYPE:C1 AT APPROX STA 20, L34R CRACKED AT LOWER RADIUS. FAB, LONGERON LOCATED, DRILLED AND DEBURRED, ALODINED AND PRIMED NEW LONGERON IAW DC8 SRM 51-1-24, 51-1-8, AND DAC DWG 4615293.SDR UPS04842196Skin · crackedINSPECTION TYPE:C1 EXT FUSELAGE AT FS 1700 APPROX BETWEEN L16R AND L17R FASTENER HOLE CRACKED RUNNING FWD. CUT OUT DAMAGED AREA IAW DC8 SRM 53-2-1. FABBED DOUBLER, FINGER DOUBLER, AND FILLER IAW DC8 SRM 53-2-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTASDR IXXA0400016OUplock · corrodedDURING UPLATCH CHECK AFTER TAKE OFF, GEAR DOORS AND GEAR UNSAFE LIGHTS CAME ON. CREW PERFORMED UNSATISFACTORY UPLATCH CHECK (WARNING LIGHTS ON) CHECK WAS STILL UNSATISFACTORY. CREW RETURNED AIRCRAFT AND LANDED WITHOUT INCIDENT. AN INVESTIGATION IS ON GOING. ASSDR IXXA0400015OCylinder · leakingAFTER DEPARTURE FROM VTBU TO RJTY NOTED HYD FLUID AND PRESSURE LOSS. CREW FOLLOWED ABNORMAL CHECKLIST, PROCEEDED TO RJTY FOR AN UNEVENTFUL LANDING. MX DISCOVERED LEFT MLG BOGIE TRIM CYLINDER LEAKING AND REPLACED THIS COMPONENT. SYSTEM LEAKS AND OPS CHECKS GSDR UPS04842195Floorbeam · corrodedINSPECTION TYPE: C1, MAIN CABIN FS 1727 FLOORBEAM AT RBL 34 & FLOOR SUPPORT CORRODED. REMVOED CORROSION FROM FLOORBEAM IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED TEE & L ANGLES IAW DAC DWG 575503. LOCATED AND DRILLED PARTS IAW DC8 SRM SDR IXXA0400014OControl Cable · looseDURING CLIMB FROM KLAX TO KTOL, AT LOW SPEEDS, CREW HAD ELEVATOR VIBRATION. VIBRATION WENT AWAY WHEN AIRCRAFT REACHED 280 KTS SPEED. CREW CONTINUED FLIGHT TO KTOL. AN INVESTIGATION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. LEFT SDR UPS04842193Floorbeam · corrodedINSPECTION TYPE:C1 MAIN CABIN FS 1660 FLOORBEAM AT LBL 20-LBL 30 HAS CORROSION ON UPPER SURFACE. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND PRE-EXISTING PLUG AT SEAT TRACK ATTACH HOLE OUT OF LIMITS. ROUTED OUT DAMAGE & FAB REPAIR ANGLE AND FILLER IAW DC8 SSDR UPS04842182Fitting · crackedINSPECTION TYPE: C1, LONGERON 6L BATHTUB FITTING CRACKED AT STA 857. REMOVED CRACKED FITTING, LOCATED & DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D AND MM DC8 20-14-00.SDR IXXA0400013OCoupler · corrodedDURING CRUISE HF SYS WAS NOT RECEIVING, ELECTED TO RETURN. MX FOUND INCORRECT P/N'S INSTALLED FOR ACCESS COUPLER & TUNER COUPLERS. REMOVED & REPLACED COUPLERS. MX FOUND RECEIVE LINES FOR HF 1 & 2 FROM LIGHT ARRESTOR TO ACCESS COUPLERS CORRODED & SHORTED TO
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