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 UPS96821108Shear Tie · crackedINSPECTION TYPE-CS2, SHEAR TIE CRACKED AT HOLE, FS 1100 LONGERON 11L. REPLACED SHEAR TIE SECTION PER SRM 51-1-20D.SDR UPS96821106Fitting · crackedINSPECTION TYPE-CS2, AFT SERVICE DOOR FITTING CRACKED INSIDE SECOND LIGHTENING HOLE FROM TOP ON FWD SIDE. REPLACED FITTING PER SRM 51-1-20D.SDR UPS96821061Fitting · crackedINSPECTION TYPE CS2, FITTING CRACKED ON FWD SIDE OF FS 857 AT LONGERON 18R. REPLACED FITTING PER SRM 51-1-20D.SDR UPS96821001Fitting · crackedRIGHT WING STA ZERO FLAP COVE FWD OF NR 1 FLAP DRIVE FWD PIVOT FITTING CRACKED ABOVE 90 DEGREE SPOILER CABLE BEND PULLEYS. REPLACED FITTING PER SRM 51-1-20D AND EO DC8-5310-8226D.SDR RRXA96150Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME CORRODED AND PAST LIMITATIONS IAW DC-8 SRM, AT Y=1120 AND LONGERN 36. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DER APPROVED ENGINEERING SKETCH B21-R25, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96148Scuff Plate · damagedDURING A MAINTENANCE VISIT, FOUND CARGO DOOR SCUFF PLATING DAMAGED PAST LIMITATIONS IAW DC-8 SRM, AT Y=200 TO Y=240. REMOVED SCUFF PLATE, FABRICATED NEW SCUFF PLATE AND INSTALLED IAW DC-8 SRM 51-1-20 AND RFTS 96-438.SDR RRXA96144Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATION IAW DC-8 SRM, AT Y=1100 AND LONGERON 36. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R02, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96143Skin · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT WING LEADING EDGE HAD 5 CRACKS AT MOUNT SCREW HOLES PAST LIMITATION IAW DC-8 SRM, AT XFS 485 TO XFS 603. INSTALLED DOUBLER REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R17, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96141Skin · crackedDURING A MAINTENANCE VISIT, FOUND 2 RIGHT WING LEADING EDGE MOUNT SCREW HOLES CRACKED, PAST LIMITATIONS IAW DC-8 SRM, AT XFS 385.250. INSTALLED FILLER AND DOUBLER IAW DER APPROVED ENGINEERING SKETCH B21-R18, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96140Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1120 AND LONGERON 36. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R05, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96128Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1280 BETWEEN LONGERON 27 RIGHT AND LONGERON 29 RIGHT. REPAIRED FRAME BY INSTALLING REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R07, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96127Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME CAP CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1040 BETWEEN LONGERON 35 LEFT AND LONGERON 36. REPAIRED FRAME CAP IAW DER APPROVED ENGINEERING SKETCH B21-R08, TREATED AREA IAW DC-8 SRM 51-1-8.SDR UPS96821241Skin · crackedINSPECTION TYPE-CS2, .5 INCH LONG CRACK AT NOSE GEAR WHEEL WELL CUTOUT. REPAIRED PER UPS EO AND SRM 51-1-21.SDR RRXA96142Skin · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING CRACKED IN SKIN PAST LIMITATIONS IAW DC-8 SRM, AT XS 520.168. INSTALLED DOUBLER REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R23, TREATED AREA IAW DC-8 SRM.SDR RRXA96135Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM PAST LIMITATIONS IAW DC-8 SRM, AT Y=1540 AND X=+58. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R14, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96133Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION DAMAGE TO FLOORBEAM PAST LIMITATIONS IAW DC-8 SRM, AT Y=1580 AND X-50. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R10, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96132Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION DAMAGE TO LONGERON 21R PAST LIMITATIONS IAW DC-8 SRM, AT Y=1640. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-11, TREATED AREA IAW DC-8 SRM 51-1-8.SDR UPS96821109Tab · delaminatedINSPECTION TYPE-CS2, LT AILERON GEAR TAB DELAMINATED. REPLACED TAB ASSY PER MM 27-13-01.SDR RRXA96149Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND EXFOLIATION ON FLOORBEAM AND WEB TORN PAST LIMITATIONS IAW DC-8 SRM, AT Y=1360. REPAIRED FLOORBEAM WEB BY REPAIR ANGLES AND WEB SPLICE IAW DER APPROVED ENGINEERING SKETCH B21-R22. REMOVED AND TREATED CORRODED AREA IAW DC-8 SSDR RRXA96145Skin · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING LEADING EDGE SKIN CRACKED PAST LIMITATIONS IAW DC-8 SRM, AT XFS 300. INSTALLED REPAIR IAW DER APPROVED ENGINEERING SKETCH B21-R01, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96131Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND EXFOLIATION DAMAGE ON FLOORBEAM PAST LIMITATION IAW DC-8 SRM, AT Y=1300 BETWEEN X-32 AND X-39. INSTALLED REPAIR DOUBLER AND FILLER IAW DER APPROVED ENGINEERING SKETCH B21-R21, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96130Floorbeam · corrodedDURING A MAINTENANCE VISIT, FOUND EXFOLIATION CORROSION ON RIGHT SIDE OF VERTICAL FLOORBEAM PAST LIMITATIONS IAW DC-8 SRM, AT Y=1360 AND X-47. INSTALLED SPLICE REPAIR TO FLOORBEAM WEB, IAW DER APPROVED ENGINEERING SKETCH, TREATED AREA IAW DC-8 SRM 51-1-8.SDR DHL9680201CTorque Tubes · corrodedAT C-CHECK, DURING X-RAY INSPECTION OF THE ELEVATOR BUS TORQUE TUBES, HEAVY INTERNAL CORROSION WAS FOUND. REMOVED AND REPLACED BOTH TORQUE TUBES PER M/M .SDR UPS96820926Doubler · crackedINSPECTION TYPE-SPEC, LT WING UPPER ACCESS PANEL DOUBLER HAS A 1.5 INCH LONG CRACK WS XRS 22.750 STRINGER NR 6. REPAIRED PER UPS EO.SDR RRXA96159Floor Panel · separatedDURING A MAINTENANCE VISIT, FOUND AFT LOWER FLOOR PANEL MODIFICATION SEPARATING FROM GILL BOARD ON BOTH SIDES OF PANEL, AT Y=1220 TO Y=1320. REPAIRED PANEL BY RESEALING PANEL TO GILL BOARD IAW DAC-DRW 2277-006 REV F, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96066Tee Fitting · failedSHUTDOWN HYDRAULIC SYSTEM DUE STEADY SLOW QTY LOSS, WITH SYSTEM SHUTDOWN QTY LOSS STOPPED. THEN RT GEAR DOOR LIGHT CAME ON WITH A LOUD RUMBLE FROM THE NOSE GEAR DOOR. ELECTED TO RETURN TO EINN, DUMPED FUEL TO MAX LANDING WEIGHT. REPOWERED HYDRAULIC SYSTEM FSDR UPS96820831Tail Cone · crackedINSPECTION TYPE DLY, 6 TO 8 INCH CRACK IN TAIL CONE BEHIND LEFT ELEVATOR. REPAIRED CRACK IN TAIL CONE PER EO DC-8-5350-7876-A.SDR RRXA96161Frame · corrodedDURING A MAINTENANCE VISIT, FOUND FRAME CORRODED PAST LIMITATIONS IAW DC-8 SRM 53-2-0, AT Y=1260 AND LONGERON 36. FABRICATED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-2-0 AND 51-3-0, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96160Angle · corrodedDURING A MAINTENANCE VISIT, FOUND FLOOR SUPPORT ANGLE CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=1220 TO Y=1140 AND BETWEEN LONGERONS 34 AND 35 RIGHT. FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE IAW DC-8 SRM 51-1-4 AND 51-1-24, TREATED AREA IAW SRM 51-SDR RRXA96158Intercostal · corrodedDURING A MAINTENANCE VISIT, FOUND INTERCOSTAL CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT LONGERON 35 LEFT AND Y=1000 TO Y=1060. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DAC DWG-5779936, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96153Fillet · delaminatedDURING A MAINTENANCE VISIT, FOUND CENTER WING FILLET PANEL DELAMINATED, DAMAGE PAST LIMITATION IAW DC-8 SRM, AT PANEL NR 162R. REPAIRED BY FABRICATING NEW FILLET PANEL AND INSTALLING IAW REO-02134 REV IR AND DOUGLAS DRAWING 566752 APPENDIX A, TREATED AREA IAWSDR RRXA96155Fillet · delaminatedDURING A MAINTENANCE VISIT, FOUND FILLET PANEL NR 162-W DELAMINATED, DAMAGE PAST LIMITATIONS IAW DC-8, AT Y=1058 TO Y=1078 LEFT SIDE. REPAIRED BY FABRICATING NEW FILLET PANEL IAW REO-02133 REV IR AND DOUGLAS DRAWING 5656352, TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA96152Bulkhead Fillet · gougedDURING A MAINTENANCE VISIT, FOUND FILLET BULKHEAD PANEL LEFT SIDE DAMAGED WEB PAST LIMITATIONS IAW DC-8 SRM, AT Y=965 TO Y=990. FABRICATED NEW WEB AND DOUBLER, INSTALLED IAW REO-02128, TREATED REPAIR AREA IAW DC-8 SRM 51-1-8.SDR RRXA96065Retract Mech · brokenLANDING GEAR DOORS NOT LATCHED LIGHT STAYED ON AFTER GEAR RETRACTION. DID NOT GO OUT WITH UPLATCH CHECK, GEAR WAS CYCLED, LIGHT STAYED ON. ALTERNATE GEAR DOOR LIGHTS STAYED OUT. **CORRECTIVE ACTION** CHECKED LT AND RT PROXIMITY SWITCHES, CYCLED GEAR DOORS,SDR RRXA96156Plating · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT WING LOWER SKIN CRACKED PAST LIMITATIONS IAW DC-8 SRM, AT XRS 450. REPAIRED IAW REO-02129, REMOVED DAMAGE, FABRICATED DOUBLER IAW DOUGLAS DRAWING SRO8570013, TREATED AREA IAW DC-8 SRM 51-1-8.SDR DHL9680615CSkin · corrosionAT C-CHECK, FOUND RUDDER SKIN BULGED AND RIVETS POPPED RT SIDE ABOVE TRIM TAB STA ZR170. REPAIRED PER DACO ROD SKETCH 96-05-20-010 AND SRM 51-1-21. RE-BALANCED RUDDER.SDR DHL9680619CSkin · corrosionAT C-CHECK, LEFT WING TOP SURFACE BETWEEN NR 1 ENGINE AND NR 2 ENGINE BULGED BY CORROSION IN SEVERAL PLACES. REMOVED CORROSION AND REPAIRED PER SRM 57-2-1.SDR DHL9680618CFrame · crackedAT C- CHECK, FOUND FRAME CRACKED AT RIGHT SIDE STA 80. REPAIRED PER SRM 53-2-0.SDR DHL9680617CBulkhead · corrodedAT C-CHECK, RIGHT W/W BULKHEAD UPPER INBD SECT OTBD OF CONTROL PULLEY HAS CORROSION. REPAIRED BULKHEAD PER EA PD 08-53-001 AND SRM 51-1-20D.SDR DHL9680616CFrame · brokenAT C-CHECK, CABIN FRAME BROKEN AT FS 220 RIGHT BETWEEN STR 7R AND 8R. REMOVED AND REPAIRED BROKEN FRAME PER SRM 53-2-0.SDR DHL9680611CPress Panel · corrodedAT C-CHECK, COCKPIT HAD HEAVY CORROSION BETWEEN FINGER DOUBLER AND PRESSURE PANEL BELOW COCKPIT FLOOR LEFT SIDE OF LBL 60, FS 8-12. INSTALLED FRAME REPAIR PER ROD SKETCH 96-05-16-00.SDR DHL9680610CSkin · corrodedAT C-CHECK, COMPT AFT OF AFT BAGGAGE HAS CORROSION ON INTERIOR SKIN STA 1624 RBL 18 - LBL 18. REPLACED SKIN PER SRM 53-02-01.SDR DHL9680602CFrame · corrosionAT C-CHECK, FOUND EXFOLIATION CORRSOION ON FUSELAGE FRAME AT FLOOR BEAM ATTACH POINT, RIGHT SIDE OF CMPT FLOOR F.S.-52. REPAIRED FRAME IAW DOUGLAS FAX DATED 20 MAY 96 AND ROD SKETCH 96-05-001. REPAIRED FLOOR WEB PER SRM 51-1-21.SDR DHL9680601CStub Frame · corrodedAT C-CHECK, LEFT OUTBOARD SIDE STUB FRAME FOUND CORRODED AROUND NUTS AT STA 960. REPAIRED PER SRM 53-2-0.SDR UPS96820666Attach Stud · shearedINSPECTION TYPE: DLY. LEFT MLG DOWNLOCK ACTUATOR GEAR ATTACH STUD SHEARED (EXTEND-RETRACT) D113074. TRANSFERRED TO NRC 352009/009N. FABRICATED BUSHING AND INSTALLED BUSHING AND NEW STUD PER XEA-X8-32-1063. REINSTALLED ACTUATOR, ADJUSTED. OPS CK OK PER M/SDR RRXA96042Valve · malfunctionedKOAK - FLT 1 - AFTER GEAR RETRACTION, THREE GREEN LIGHTS EXTINGUISHED, DOORS NOT LATCHED AND GEAR NOT LATCHED RED LIGHTS ILLUMINATED. ON POST FLIGHT INSPECTION, FOUND TIRE MARKS ON DOOR. INDICATING RIGHT MLG DOOR IS NOT OPENING. RETURNED TO KOAK. MAINTENANSDR DHL9680614CTr Forging · crackedAT C-CHECK, NR 3 ENGINE OUTBOARD THRUST REVERSER UPPER HALF AFT END FORGING FOR SLIDE TUBE BRACKET CRACKED AT AFT END. REPAIRED CRACK PER HSLH REF 19-80059 AND G.E. FAX.SDR DHL9680613CSkin · damagedAT C-CHECK, PREVIOUS REPAIR RT SIDE FS 290 TO COMPLY WITH SRM. UPGRADED REPAIR PER SRM 53-2-1.SDR DHL9680612CSkin · crackedAT C-CHECK, LEFT WING/LOWER SIDE SKIN DENTED AND CRACKED THROUGH. INSTALLED HOT BOND REPAIR 250 DEGREES CURE PER SRM 51-1-9.SDR DHL9680609CFrame · damagedAT C-CHECK, CABIN STA 190, RT BOTTOM FRAME ATTACHMENT CLIPS DAMAGED. REPLACED ANGLES, INSTALLED WEB SPLICE, DOOR JAMB CLOSE-OUT SPLICE, AND FRAME REPAIR PER ROD SKETCH 96-06-04-005.
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