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 UPS08853998Doubler · misinstalledINSPECTION TYPE:SP 12-12 INCH REPAIR DOUBLER INSTALLED WITH BLIND FASTENERS FS 53-65 L31R TO 34R REPAIR SEQ 803-F1-32. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EA 81425920001.SDR UPS08853671Flap · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT BS XW5.0 I/B FLAP WEB REPAIR DOES NOT MEET CRITERIA FOR APPENDIX H. FLAP REPLACED ON NR 188423.SDR UPS08853670Flap · misrepairedINSPECTION TYPE:SV RT INBOARD FLAP LOWER I/B EDGE DOUBLER IN STA 0.00 NEEDS VALIDATION, FAILED APPENDIX H STEP 5. REMOVED DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-05 AND SRM 51-1-21.SDR UPS08853605Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-21 LT INBOARD FLAP EXTERIOR SURFACE AT STA XW1 05 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.SDR UPS08853603Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-20 LT INBOARD FLAP UPPER SURFACE AT STA XW89 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.SDR UPS08853565Structure · misrepairedINSPECTION TYPE:SV, L/E STATION XFS 88 DOUBLER DOES NOT MEET CRITERIA FOR APPENDIX H. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 57-2-1 FIG 2H CLASS B.SDR UPS08853553Skin · misrepairedINSPECTION TYPE:SV RT FLAP UPPER EXT SURFACE BOILER PANEL DOUBLER REPAIR NEEDS VALIDATION. UPON FURTHER INVESTIGATION REPAIR DOES MEET CRITERIA OF EO DC8-5100-304 18 APPENDIX H STEP 5, NO FURTHER ACTION REQUIRED.SDR UPS08853648Doubler · unknownINSPECTION TYPE:SV STA-53 TO -89 RBL TO RBL 42 DOUBLER NEEDS VALIDATION FOR REPAIR 894-F 3-11. REPAIRED BY SR08530026 AND SRM 53-2-1.SDR UPS08853651Doubler · damagedINSPECTION TYPE:SV EXT DOUBLER AFT LOWER DOOR CUTOUT BS 50.5 TO 55 L30L TO 1 INCH BELOW L 29L NEED VALIDATION FOR REPAIR. REPAIRED SRM 53-02-00 FIG 13.SDR UPS08853695Doubler · damagedINSPECTION TYPE:SV BS 659 TO 719.5 L35L TO L35R EXT DOUBLER LOWER BELLY NEED VALIDATION FOR REPAIR. REPAIRED IAW EO DC8-5300-3I587.SDR UPS08853682Doubler · damagedINSPECTION TYPE:SV EXT DOUBLER BS 1279.5 TO 1299.5 AT L35R CENTERLINE NEED VALIDATION FOR REPAIR REF SEQ 894-FA-57. REMOVED, FABBED AND REPLACED DOUBLER IAW BOEING ROD SKETCH 99-01-20-004 REV IR AND UPS EO DC8-53-20422.SDR UPS08853652Doubler · damagedINSPECTION TYPE:SV EXT WINDOW DOUBLER BS 1400 TO 1421 1.5 ABOVE L14R TO 1.5 BELOW L17R NEEDS VALIDATION FOR REPAIR. REPAIRED BY SRM 51-3-0 AND EO DC 5320-31585.SDR UPS08853599Cusp Web · crackedINSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR. EFN 8941997-55. ORIGINAL N/R 5 34204 LEFT CUSP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. REMOVED DOUBLER VERIFIED CRACK STOP DRILLED IAW SRM 53-02-00-0. REINSTALLED DOUBLER AND VERIFIED REPAIR CSDR UPS08853598Cusp Web · crackedINSPECTION TYPE:SV REMOVE AND REPLACE EFN 89419971055 ORGINIAL N/R 534204 LEFT CUP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. VERFIED REPAIR COMPLIES WITH SRM 53-02-00 FIG 23.SDR UPS08853585Cusp Web · crackedINSPECTION TYPE:SV REMOVE REPAIR AND REPLACE WITH SRM REPAIR EFN 89419971080 ORIGINAL N/R 534358 CUSP MEMBRANE CRACKED BETWEEN LIGHTENING HOLES FS 80. UPON INVESTIGATION FOUND REPAIR MISSING ONE ROW OF FASTENERS, ADDED ROW 3 RIVETS AS IAW SRM 53-02-00. FOUNSDR UPS08853568Cusp Web · crackedINSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR ORGINIAL N/R 534146 RIGHT CUSP MEMBRANE CRACK EXTENDING FROM STOP DRILL TO AFT OF FS 1600. INSTALLED DOUBLER AS PER SRM 51-21-01.SDR UPS08853567Cusp Web · crackedINSPECTION TYPE:SV REMOVE AND REPLACE ORIGINAL N/R 534909 LEFT LOWER CUSP MEMBRANE CRACKED, DENTED AND CORRODED BETWEEN FS 400-420. UPON INVESTIGATION FOUND DAMAGE WAS REMOVED AND VALIDATED REPAIR WAS A ACCOMPLISHED REF DC8 SRM 53-02-00 FIG 25.SDR UPS08853550Rib · crackedINSPECTION TYPE:SV EVALUATION OF N/R 535858 LT WING L/E REPAIR BETWEEN NR 1 AND 2 PYLONS TENTH RIB FROM INBOARD END IS CRACKED. REPAIR WAS ACCOMPLISHED IAW DC8 SRM 57-2-0 SHEET 2 OF 2.SDR UPS08853586Fitting · crackedINSPECTION TYPE:SV BATH TUBE FITTINGG AT L33R-L34R IS CRACKED. REPAIR AS PER IAW DC8 SRM 51-03-02.SDR UPS08853552Skin · damagedINSPECTION TYPE:SV FLUSH SKIN REPAIR CUT BS 88 TO 14 BETWEEN L31L AND L27L NEEDS VALIDATION. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 53-02-01 FIG 007.SDR UPS08853411Retainer · brokenSLIDE CONTAINER IS OPEN. DEFERRED M385289 ASSIGNED. SLIDE CONTAINER RETAINER BROKEN DEFERRED MAIN ENTRY ESCAPE SLIDE PER MEL 52-7-4. SLIDE REMOVED AND ROUTED TO AMDC. COURIER SEATS NOT TO BE OCCUPIED. INSTALLED EVACUATION SLIDE PER AMM 25-60-01. PLACARDS SDR UPS08853664Skin · damagedINSPECTION TYPE:SV FUSELAGE EXTERIOR SKIN STA 50 L21R BULGING AND FASTENER HEAD SHEARED. REMOVED FASTENERS STA FS 70 TO FS 50 L19R TO L21R AND FS 50 TO FS 30 IAW DC 8 SRM 51-1-21. REMOVED DOUBLER FROM STA 7 TO STA 70 L20R-L21R. FABBED AND INSTALLED DOUBLER SDR UPS08853661Doubler · gougedINSPECTION TYPE:SV SURVEY SEQ 894-W4-23 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED INBOARD OF BOILER PANEL AT STA XF 211. REMOVED AND REPLACED DOUBLER IAW DC-8 SRM 57-02-05 FIG 2.SDR UPS08853660Doubler · gougedINSPECTION TYPE:SV SURVEY SEQ NO 894-W4-24 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 57-2-05 FIG 2.SDR UPS08853622Repair · corrodedINSPECTION TYPE:SV LOWER FUSE-INT, BATHTUB FITTING REPAIR ANGLE HAS CORROSION AT FS 1180, BETWEEN L33R-L34R JUST INBOARD OF AFT CARGO DOOR CUTOUT LOWER EDGE. REPLACED REPAIR ANGLE IAW DC8 SRM 51-30-00-0-1 AND 53-02-00-0 FIG 002D.SDR UPS08853563Skin · damagedINSPECTION TYPE:SV FLUSH REPAIR BS 151, 8 INCHES BELOW L21L HAS CLOSE FASTENER SPACING. ACCOMPLISHED IAW DALFORT AVIATION REPAIR XEA X8-53-706 AND REFERENCE DC8-73F SRM 53-2-0 FIG 1C PG 10 10 OF 14.SDR DHLA200800099Battery · dischargedEMERG LTS BATTERY DISCHARGED REPLACED BATTERY PACK FOR EMER LTS PER MM 33-50-01 CHECKS SERV. N/A FLT NR. ACFT WAS GROUNDEDSDR DHLA200800098Battery Pack · dischargedEMERG LTS BATTERY DISCHARGED. REPLACED BATTERY PACK FOR EMER LTS PER MM 33-50-01 CHECKS SERV. NO FLT NR. ACFT WAS GROUNDED.SDR UPS08853667Fastener · looseINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-13 LT WING L/E ABOVE NR 2 PYLON AT XFS 275 SKIN REPAIR DOUBLER HAS 4 FASTENERS LOOSE AND 1 FASTENER PULLED THROUGH. REMOVED AND INSTALLED 5 NEW FASTENERS IAW DC8 SRM 51-3-0 FIG 52A.SDR UPS08853666Fastener · brokenINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-01 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER HAS 1EA FASTENER HEAD BROKEN AT XFS 404.000 BETWEEN NR 1 AND NR 2 ENG. REPLACED FASTENER IAW UPS DC8 SRM 51-03-00.SDR UPS08853665Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ NO 894-W3-03 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER A HAS 5EA FASTENER HEADS PROTRUDING AT XFS 462.000 AFT OF SLOT DOOR. RE-COUNTERSINK HOLES AND INSTALLED SCREWS IAW DC8 SRM 51-3-0.SDR UPS08853504Skin · damagedINSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR SURVEY SEQUENCE NR: 894-W4-09. RIGHT UPPER LEADING EDGE DOUBLER REPAIR STA XFS 512 MISSING 8 EACH FA FASTENERS. INSTALLED FASTENERS IAW DC-8 SRM 51-03-00.SDR UPS08853680Web · corrodedINSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89420061026. ORIG NR 994522 L33R STA 1 160 TO STA 1220 UPPER WEB HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABBED, AND INSTALLED NEW DOUBLER AND FASTENERS IAW REO G12470.SDR UPS08853668Doubler · corrodedINSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971256 ORIG NR 535436 PREVIOUS REPAIR DOUBLER AND TRIPLER ON LONG 33L ARE CORRODED STA 1185-1295. REMOVED AND INSTALLED REPAIR DOUBLER IAW ROD SKETCH 97-05-06-006 AND SRM 51-30-01-00. ACTUAL REPAIR FOUNDSDR UPS08853656Web · corrodedINSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89419911026. ORIGINAL NR 303033. CORROSION REPAIR TO WEB AND ANGLE AT AFT PASS DOOR FS 1615-1625. REPAIR SATISFIES INTENT AND GUIDELINES OF DC8 SRM 53-2-0 FIG 001D. RF TS 894UP-20-20265.SDR UPS08853655Door Frame · damagedINSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971106 ORIG NR 534710 R-1 DOOR AFT DOOR JAMB REPAIR FOR ELONGATED HOLES (FUSELAGE FRAME). EXISTING REPAIR ACCOMP IAW DWG UPS DC8-53A-011A. RFTS N894UP-12-2027.SDR UPS08853649Door Frame · damagedINSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 89419971107 ORGINIAL N/R 534711 R-1 DO OF FORWARD DOOR JAMB REPAIR FOR ELONGATED HOLES. REPAIRED BY ANGLE AND WEB REF DC8 51--21 EO DC8 5310-11728B AND DWG 53 DC8 53A-011-REV A.SDR UPS08853646Door Frame · damagedINSPECTION TYPE:SV EVALUATION ESN 89420041016 N/R 721564 FOWARD ENTRY DOOR AFT LOWER JAMB REPAIR FOR ELONGATED HOLES. FAB NEW WEB IAW DC8 SRM 53-02-00 FIG 25 AND DC8 SRM 51-3-0.SDR UPS08853635Door Frame · damagedINSPECTION TYPE:SV EVALUATION AND DISPOSITION REPAIR EFN 89419971107 ORIGINAL NRC 534711 R1 DOOR FORWARD DOOR JAB (FUSELAGE FRAME) REPAIR FOR ELONGATED HOLES. FABRICATED NEW INTERCOSTAL PER DAC DWG 561575700 REV EC, FABRICATED NEW FRAME DOUBLERS AND INSTALLEDSDR UPS08853533Seat Track · gougedINSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR EFN 89420081074. ORIGINAL N/R 14 7772 SEAT TRACK PLUG GOUGED FS 1470 RBL 46. REPAIR FOUND TO BE IAW SRM DC-8 53-2-3 FIGURE 60.SDR UPS08853529Rib · crackedINSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR EFN89419911115. ORIGINAL N/R 480 775. VERTICAL STABILIZER L/E LOWER SECTION NR 25 RIB CRACKED AFT LT FLANGE. RFTS N894UP-9-20284 RIVETS INSTALLED IN FREE STANDING LEG OF REPAIR. REMOVED RIVETS AND INSTALSDR UPS08853551Rib · crackedINSPECTION TYPE:SV EVALUATION OF N/R 534213 RIGHT HAND LEADING EDGE AT STA XFS 804.00 UPPER LEFT RIB HAS A CRACK AFT END. REPAIR IS ACCOMPLISHED IAW DC8 SRM 57-2-0 FIG 2.SDR UPS08853383Doubler · damagedINSPECTION TYPE:N/A REPAIR DOUBLER AT FUSELAGE FRAME 50 AND STRINGER 24L REQUIRED REPLACEM MENT D385232. REMOVED DOUBLER, ACCOMPLISHED STEPS APPENDIX-A (1) THRU (6). PER PRELIMINARY EO DC8-5330-30623-A. DAMAGE REMOVAL VERIFIED OK TO INSTALL FABRICATED DOUBLESDR UPS08853382Doubler · damagedINSPECTION TYPE:N/A DOUBLER AT FUSELAGE STATION 902, LT SIDE OF FUSELAGE REQUIRES REPLACEMENT. REMOVED EXISTING DOUBLER AND SHIM PER SRM 51-1-00, C/W EO DC8-5330-3 9 UP TO STEP 6. INSTALLED 28 1/4" HI-LOKS IN REPAIR DOUBLER PER PRELIMINARY EO DC8 5330-30619-SDR UPS08853658Flange · crackedINSPECTION TYPE:SV RT WING LEADING EDGE AUX TANK AFT INBOARD SIDE VENT TUBE FLANGE CRACKED. REMOVED, REPAIRED, REINSTALLED FLANGE IAW DCI MM 20-12-00-2.SDR UPS08853318Slide · unwanted deployINSPECTION TYPE:N/A JUMP SEATER OPENED DOOR WITH RAFT ATTACHED. REPACKED EMERGENCY DOOR SLIDE AND SECURED. CHECK OK.SDR UPS08853324Clamp · disconnectedINSPECTION TYPE:N/A UNABLE TO MAINTAIN PRESSURIZATION. FOUND LEFT CLAMP PACK DISCONNECTED PERFORMED DECAY CHECK PER AMM 21-31-00-2. ALSO PERFORMED COOLING PACK ADJUSTMENT TEST 21-55-00-5.SDR UPS08853242Seal · leakingCREW EXPERIENCED SLOW LOSS OF HYDRAULIC FLUID DURING FLIGHT. COMPLETED LOSS OF HYDRAULIC FLUID CHECKLIST AND WERE ABLE TO STOP THE LOSS. CREW DECLARED AN EMERGENCY & CONTINUED TO SDF WHERE AIRCRAFT LANDED SAFELY. REPLACED HYD QTY TRANSMITTER SEAL REF MM 29-SDR UPS08853136Angle · damagedSIDE WALL STRUCTURAL DAMAGE IN POSITION 2/3 AREA, ATTACHED Z-ANGLE DAMAGED. *SUPPLEMENTAL SDR* FABRICATED AND INSTALLED Z-ANGLE ON 3RD FROM FLOOR AT POS 2/3 PER SRM 57-1-21.SDR DHL200800093Connector · malfunctionedFIRE WARNING LIGHT ON AND FIRE BELL RINGING NR 3 ENG. SWITCHED TO B LOOP LIGHT AND BELL WENT OUT. DEFERRED NR 3 ENG A LOOP PER EML 26-2-3 CAT C PLACARD ISN`T DMI 33371. A/C WAS GROUNDED FLIGHT 445. P/N CHANGED CONNECTOR 878238-02.
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