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 UPS01837207Fitting · corrodedINSPECTION TYPE:C2 STA 340 LONG 33R BANANA FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755827,AND SRM 51-1-20D.SDR UPS01837180Rib · crackedINSPECTION TYPE:C2 RIGHT WING T/E UPPER RIB IS CRACKED AT XW 5. REMOVED FASTENERS, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS01837247Skin · crackedINSPECTION TYPE:C2 L-2 DOOR FWD LOWER CORNER FUSELAGE SKIN AND INTERNAL DOUBLER ARE CRACKED AT STA 1620 AT LONG 21L, AND EXISTING DOUBLER DOES NOT CONFORM TO THE SRM. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS. FABRICATED AND INSTALLED FILLERS, DOUBLER AND TRIPLSDR UPS01837224Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1723.076 LONG 15R. CUTOUT CRACKED AREA, NDT VERIFIED NO CRACKS AROUND CUTOUT, FABRICATED AND INSTALLED DOUBLER, FINGER DOUBLERS, AND FILLERS IAW SRM 53-2-1 FIG 7.SDR UPS01837205Angle · corrodedINSPECTION TYPE:C2 UPPER FUSELAGE RIGHT SIDE ANGLE AT BASE OF VERTICAL STAB IS CORRODED BEYOND LIMITS AT STA 1722. CUT OUT CORRODED AREA, NDT AT CUTOUT,NO CRACKS NOTED,FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW SRM 53-2-5 FIG 16A.SDR UPS01837202Angle · corrodedINSPECTION TYPE:C2 UPPER FUSELAGE ANGLE AT BASE OF VERTICAL STAB AT STA 1723.076 CANTED FRAME IS CORRODED BEYOND LIMITS CUT OUT CORRODED AREA,NDT CUTOUT,NO CRACKS NOTED FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-2-5 FIG 16A.SDR UPS01837233Skin · crackedINSPECTION TYPE:C2 NR 1 (A-PIT) CARGO DOOR SKIN IS DAMAGED AT LOWER AFT CORNER AT STA 330 LONG 32R. CUT OUT CRACKED AREA, NDT VERIFIED NO CRACKS AT CUT OUT, FABRICATED AND INSTALLED FILLER DOUBLER, AND SHIM IAW SRM 52-2-3 FIG 10A.SDR UPS01837035Heat Shield · crackedINSPECTION TYPE:IN NR 3 ENG RT TRUST REVERSER HALF STAINLESS SHIELD ON FWD FACE 4 O`CLOCK CRACKED AND PIECE MISSING. ACCOMPLISHED EO DC-8 7830-15530-B.SDR UPS01837131Skin · crackedINSPECTION TYPE:SV BOTTOM SKIN OF NR 4 MAIN I/B SIDE OF NR 3 PYLON BY PUMP HOUSING LOWER SKIN CRACKED AT FASTENER HOLE STA XCW 172.000 STR 58. COUNTERBORED HOLE TO .630 .003, FABRICATED BUSHING FOR SKIN, INSTALLED COUNTERSUNK BUSHING IAW REO G08431.SDR UPS01837130Stringer · crackedINSPECTION TYPE:SV FOUND CRACKED STRINGER IAW HFEC PER NDT SRM 06-10-01.003 AT STA APPROX 240.000 XLS STRINGER 58. REMOVED 80 INCHES OF STRINGER AND SPLICED IN NEW SECTION OF STRINGER IAW DC8 SRM 51-1-24, 57-2-2 AND 51-1-8.SDR UPS01837089Fitting · crackedINSPECTION TYPE:SV RIGHT WING NR 3 MAIN TANK STRINGER 51 END FITTING ON I/B SIDE IS CRACKED. REMOVED STRINGER 51 END FITTING ON I/B SIDE IAW DC8 SRM 51-3-2. LOCATED DRILLED AND INSTALLED NEW END FITTING IAW DAC DWG 5613423.SDR UPS01837088Fitting · crackedINSPECTION TYPE:SV RIGHT WING NR 3 ALT TANK STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 56SDR UPS01837062Fitting · crackedINSPECTION TYPE:SV LT WING NR 2 MAIN STRINGER 51 FWD I/B SIDE HAS A CRACKED STRINGER END FITTING. PERFORMED HFEC TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-001. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.SDR UPS01837061Fitting · crackedINSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED AND RPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.SDR UPS01837060Fitting · crackedINSPECTION TYPE:SV LT WING NR 2 MAIN STRINGER 51 AFT I/B STRINGER END FITTING IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.SDR UPS01837059Fitting · crackedINSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 060101. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 5613423. INSTALLESDR UPS01836855Wire · looseINSPECTION TYPE:N/A NR 1 BUS OFF LIGHT ILLUMINATED AND SMOKE IN COCKPIT. RESECURED WIRE TO TERMINAL X2 OF LMR R2-25 OF NR 1 AC BUS OPS CHECKS NORMAL OF NR 1 AC BUS.SDR UPS01836833Battery Pack · dischargedINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. R&R BATTERY PACK. OPS CHECKS GOOD PER DC8 MM 33-50-00.SDR UPS01836827Cover · damagedINSPECTION TYPE:IN EVAC SLIDE COVER IS DAMAGED. SLIDE CASE WILL NOT STAY CLOSED. GAPS OPEN AT THE BOTTOM. SLIDE COVER REMOVED AND ROUTED TO SHEETMETAL REPLACED SHEARED RIVETS ON COVER LATCH IAW 51-1-21 DC8 SRM 79657 9-15-01 INSTALLED SLIDE PER 25-60-01.SDR UPS01836726Relay · failedINSPECTION TYPE:IN EMERGENCY LIGHTS FAILED OPS CHECK, FOUND EMERGENCY LIGHT CONT RELAY STICKING. R&R EMERGENCY LIGHTING BATTERY AND RELAY UNIT AND PERFORMED OPS CK PER MM 33-50-01 PARA 2 & 4 OPS CKS NORMAL.SDR UPS01836721Relay · failedINSPECTION TYPE:ASE DURING MX INSPECTION FOUND EMERGENCY LIGHTS FAILING OPERATIONAL TEST. CAUSE FOUND TO BE A STICKING EMERGENCY LIGHT CONTROL RELAY. REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY AND RELAY UNITSDR UPS02839440Fitting · crackedINSPECTION TYPE:C1 STA 908 LONG 10R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779658, AND SRM 51-1-20D, 51-1-21, 51-3-0.SDR UPS01836682Battery Pack · dischargedINSPECTION TYPE:N/A EMERG LIGHTS INOP. REMOVED AND REPLACED EMERG LIGHT BATTERY PACK. OPS CHECKS GOOD.SDR UPS01836606Flap · crackedINSPECTION TYPE:PFLT LEFT WING INBOARD FLAP HAS A CRACK ON INBOARD TRAILING EDGE NEXT TO FUSELAGE AND BENT. REMOVED PREVIOUS SKIN REPAIR. REPAIRED IN REF SRM 57-20-0.SDR UPS01836607Battery Pack · dischargedINSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. R/R EMERGENCY LIGHTS BATTERY PACK. OPS CKS GOOD AT THIS TIME.SDR UPS01836560Sliding Window · leakingINSPECTION TYPE:IN FOUND F/O'S SLIDING WINDOW LEAKING AIR AT TOP APPROX MID POSITION OF SEAL. APPROX 1/2 PSID. REMOVED & REPLACED RT SLIDING WINDOW IAW MM 56-10-03.SDR UPS01836550Skin · crackedINSPECTION TYPE:IN PIT 33 DOOR LOWER SKIN CRACKED AFT LWR CARGO FWD DOOR BOTTOM EDGE OF SKIN DOUBLER, TORN & CRACKED IN 2 PLACES. FOUND PERVIOUS REPAIR FILLER DAMAGED, NO DAMAGE TO INTERNAL DOUBLER REMOVED AND REPLACED FILLER IAW SRM 51-2-0.SDR RRXA010064Indicator · failedNR 1 EGT REACHED 907 DEGREES C FOR APPROX 8 SEC ON MAX POWER T/O. 92 PERCENT N2 & 28 DEGREES C OAT AT DAY. FOUND NR 1 ENGINE EGT INDICATOR READS 24-34 DEGREES HIGH. NO DEFECTS ON HARNESS R&R NR 1 EGT INICATOR 077-20-1, CK GOOD WITH TEST SET, ENGINE RUN REQSDR RRXA010062Floor Panel · damagedUPPER DECK CARGO FLOOR AT STA 781, 30 AND TO THE RT HAS A HOLE. REPAIRED GOUGE IN FLOOR PANEL IAW DC-8 SRM 53-2-3 FIG 6.SDR IXXA0100050OFilter · dirtyEN ROUTE FROM LAX TO PDX, THE NUMBER THREE ENGINE FLAMED OUT DURING CLIMB. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURE AND PERFORMED A SUCCESSFUL RESTART AFTER TRANSFERRING TO AN ALTERNATE FUEL SOURCE. THE FLIGHT CONTINUED TO PDX FOR AN UNEVENTFUL LANDING. MSDR UPS01836522Fitting · crackedINSPECTION TYPE:C1/3 FWD BAG PIT Z FITTING CRACKED AT FS 300 LONGERON 27L. INSTALLED NEW Z FITTING P/N 3755822-515N IAW DC8 SRM 51-1-20DSDR IXXA0100049OControl Cable · brokenDURING TAXI AT ANU, BINDING OF THE ELEVATOR WAS EXPERIENCED WHILE THE FLIGHT CREW WAS PERFORMING THE FLIGHT CONTROL CHECK. THE AIRCRAFT RETURNED TO THE BLOCKS. MAINTENANCE INSPECTED THE AIRCRAFT FLIGHT CONTROLS WHICH REVEALED A DEFECTIVE RIGHT ELEVATOR CONTRSDR UPS01836431Window · out of adjINSPECTION TYPE:N/A CAPT SLIDE WINDOW WILL NOT OPEN. PERFORMED ADJUSTMENT OF CAPTS SLIDING WINDOW PER MM 56-10-03 OPS CK GOODSDR UPS01836409Cylinder · lack of lubeINSPECTION TYPE:N/A AIRCRAFT TURNS HARD LEFT DURING TAXI AND T/O. WHEN FLAPS ARE LOWERED ACFT BANKS LEFT 10 DEGREES. VISUALLY INSPECTED FLAP MECHANISM, NO DEFECTS NOTED T/S PER MM 27-50-00. FOUND OUTBOARD LOCK CYLINDER LOW, SERVICED AND BLED PER MM 27-51-10. FSDR RRXA010061Engine · flamed outNR 4 ENGINE IN FLIGHT FLAME OUT 35000. IAW UAL M/M 71-00-40 PGS 201-206 POWER LOSS/FLAME- OUT INVESTIGATED & CHECKED THE FOLLOWING: ENGINE INLET/ EXHAUST, CHIP DETECTORS, MAIN FUEL PUMP, FUEL CTRL.,NR 3 ENGINE FUEL BOOST PUMP, IGNITOR, FUEL QTY CHECKED LINE LSDR UPS01836481Fitting · crackedINSPECTION TYPE:C1/3 AFT PIT FS 1228 L35R-L34R Z FITTING IS CRACKED. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-24 & 51-1- 20DSDR IXXA0100040OElement · defectiveENROUTE FROM LAX TO TOL, DURING CRUISE THE NUMBER FOUR FIRE WARNING LIGHT ILLUMINATED ACCOMPANIED BY THE WARNING BELL. THE FLIGHT CREW FOLLOWED COMPANY EMERGENCY PROCEDURES, SECURED THE ENGINE AND DISCHARGED BOTH BOTTLES. THE FLIGHT RETURNED TO LAX FOR AN UNEVSDR UPS01836430Web · crackedINSPECTION TYPE:C1/3 SUBFLOOR WEB AT FS 15 RBL 40 IS CRACKED. CUT OUT DAMAGE IN WEB & FABBED NEW REPAIR DOUBLERS & FILLERS INSTALLED FILLER & DOUBLER IAW SRM.SDR UPS02839042Skin · corrodedINSPECTION TYPE:C2 EVIDENCE OF CORROSION UNDER NR 2 ADF ANTENNA, CORRODED BEYOND LIMITS STA 70 TO 190 LONG 31L TO 31R. REMOVED AND REPLACED SKIN BETWEEN STA 70 TO 190 LONG 31L TO 31R IAW DWG 5779925, SRM 53-1-0, 51-1-21, 51-1-20D.SDR IXXA0100039OAmplifier · defectiveENROUTE FROM TOL TO LAX, DURING CRUISE THE NUMBER FOUR ENGINE FIRE WARNING LIGHT ILLUMATED ACCOMPANIED BY THE WARNING BELL. THE FLIGHT CREW FOLLOW COMPANY EMERGENCY PROCEDURES, SECURED THE ENGINE AND DISCHARGED ONE BOTTLE. THE FLIGHT CONTINUED TO LAX FOR AN UNSDR UPS01836521Fitting · crackedINSPECTION TYPE:C1/3 LT WING FLAP HINGE SUPPORT FITTING XF 409.6673 INBOARD CRACKED AS MARKED. REMOVED FLAP LEADING EDGES I/B & O/B OF FLAP HINGE FITTING TO FOM. LOCATED & DRILLED NEW BASE FITTING. INSTALLED BUSHINGS, INSTALLED SPRING COVER, TRACK BASE FITTINGSDR RRXA010059Bottle · leakingAFTER SERVICING OXYGEN OF UPPER CREW BOTTLE - BOTTLE WAS INSTALLED & DURING TURN ON AT BOTTLE OXYGEN LINE & REGULATOR RUPTURED & CAUSED FLASH FIRE "A" PIT OXYGEN BOTTLE AREA. INSPECTED PURGED AND LEAK CHECKED CREW OXYGEN SYSTEM IAW OPS 4.901 AND TEST DRAWISDR UPS01836398Fitting · crackedINSPECTION TYPE:C1/3 FS 680 L10R LONGERON END FITTING CRACKED. REMOVED CRACKED 3779762-1 LONGERON END FITTING. INSTALLED NEW LONGERON END FITTING IAW DC8 SRM 51-3-0, 51-1-23 AND 51-1-24.SDR UPS01836396Bulkhead · crackedINSPECTION TYPE:C1,3 LT AFT PRESSURE BULKHEAD STA 1766 L11L IS CRACKED.SDR UPS01836569Frame · corrodedINSPECTION TYPE:C1/3 AFT PIT FS 1300 AT L36 FRAME IS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED -49 REPAIR STRAP IAW DC8 SRM 53-2-0. INSTALLED -49 REPAIR STRAP IAW DC8 SRM 51-1-20D.SDR UPS01836568Fitting · corrodedINSPECTION TYPE:C1/3 AFT CARGO CROSS SLIDE DOOR JAM T FITTING 3 (EA) HAS CORROSION UNDERNEATH CASTING. REMOVED CORROSION MAT'L OUT OF LIMITS IAW DC8 SRM 53-2-0. RECEIVED NEW FITTING (2 EACH) P/N 3755772-501 TORQUE BOX LATCH ASSY LOCATED AND DRILLED HOLES IAW DSDR UPS01836478Seat Track · corrodedINSPECTION TYPE:C1/3 MAIN CABIN AT STA 740-810 & LBL 47 SEAT TRACK HAS CORROSION INBD & OTBD SIDES OF SEAT TRACK AROUND FASTENER HOLES (UNDER SIDE). REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SEAT TR ACK, FABED NEW SEAT TRACK, AND INSTALLED NSDR UPS01836342Frame · crackedINSPECTION TYPE:C1,3 DAMAGED FRAME AT FASTENER HOLE AND MISSING MOUNT CLIP AT FRAME 180 26R. FOUND FRAME DAMAGE TO BE CRACKED FLANGE AT ATTACHMENT HOLE.SDR UPS01836603Skin · corrodedINSPECTION TYPE:C1/3 REPLACE FUSELAGE AFT CENTER SECTION EXTERIOR SKIN FROM FS 1050-1350 L31R-L31L DUE TO CORROSION. REMOVED AFT BELLY SKIN FROM FS 1050-1350. TRIM NEW SKIN LOCATE DRILL EXISTING FASTENER HOLES AND COUNTERSINK HOLES IAW DC8 SRM 51-1-24. INSSDR UPS01836564Doubler · corrodedINSPECTION TYPE:C1/3 REPLACE FUSELAGE AFT CENTER SECTION INTERNAL DOUBLER FROM FS 1100-1260 L27R-L33L (CORROSION). REMOVED INTERNAL DOUBLER IAW DC8 SRM 51-1-24. TRIM NEW DOUBLER LOCATE AND DRILL EXISTING FASTENER HOLES IAW DC8 SRM 51-1-24 AND INSTALL INTERNAL
Back to Douglas DC-8-71F