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 RRXA991717Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-2 BETWEEN Y=1330 TO Y=1500 AND X=30. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVSDR RRXA991716Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=1300 TO Y=1580. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGSDR RRXA991710Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=960 TO Y=1000. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGSDR RRXA991706Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=813 TO Y=990. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINSDR RRXA991705Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL B-3 BETWEEN Y=760 TO Y=1000 AND X=15. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVEDSDR RRXA991704Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=584 TO Y=600. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERISDR RRXA991703Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-2 BETWEEN Y=580 TO Y=435 AND X=24. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED SDR RRXA991697Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E BETWEEN Y=95 TO Y=110 AND BETWEEN X=-27 TO X=30. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAWSDR RRAX991706Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=880 TO Y=900. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINSDR UPS99830184Fitting · crackedINSPECTION TYPE:C123, THE RT STA 410 FLAP UP STOP FITTING IS CRACKED. REMOVED AND REPLACED STOP FITTING IAW SRM 51-3-0.SDR UPS99830159Fitting · crackedINSPECTION TYPE:C2, MAIN CARGO DOOR FTG CRACKED UPPER FWD CORNER NEAR ACTUATOR. INSTALLED NEW FITTING, ACTUATOR SUPPORT AND CORNER FITTING IAW UPS DC8 SRM 51-1-21 & 51-3-0, UPS DCI M/M 52-36-03 & 52-36-01.SDR RRXA991487Skin · damagedDURING A MAINTENANCE VISIT FOUND LEFT WING OUTBOARD SLOT LEADING EDGE I/B EDGE HAS SCREWS PULLING THROUGH SKIN AND MISSING. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW FAA SDR RRXA991485Skin · crackDURING A MAINTENANCE VISIT FOUND CRACKS, SKIN, LEFT WING O/B LEADING EDGE I/B SECTIONS LOWER SURFACE AT STA XFS 591.250, 1 TO 4 FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLSDR UPS99830183Skin · corrodedINSPECTION TYPE:C123, RT WING L/E LWR SKIN, AT THE L/E, STA XW 761.75 HAS INTERGRANNULAR CORROSION AROUND 2 SCREWS. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5720-4087B.SDR UPS99830182Skin · crackedINSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 422.75 IS CRACKED AT A FASTENER. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087B.SDR UPS99830181Rib · crackedINSPECTION TYPE:C123, RT WING OTBD SLOT, UPPER OTBD CLOSURE RIB AT XW 453 IS CRACKED AT THE AFT END. REMOVED AND REPLACED RIB IAW SRM 51-1-20D AND 51-3-0.SDR UPS99830180Skin · crackedINSPECTION TYPE:C123 RT WING L/E UPPER SKIN AT XFS 330, AT THE SPAR, HAS INTERGRANNULAR CORROSION AND IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.SDR UPS99830179Skin · crackedINSPECTION TYPE:C123, RT WING L/E UPPER SKIN AT XW 257.5, 33 FWD OF THE SPAR, IS CRACKED BETWEEN 2 FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1.SDR RRXA991732Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 AND X=-15. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVSDR RRXA991731Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 AND X=-10. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVSDR RRXA991714Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL C-3 BETWEEN Y=1000 TO Y=1300 AND X=15. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVSDR RRXA991702Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL AT Y=435 BETWEEN X=16 TO X=24. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENSDR RRXA991503Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, SEVERAL RIVET HEADS POPPED ON DOUBLER BETWEEN STA -52 TO STA -12, 20 RIGHT CENTER COCKPIT PRESSURE DECK AFT OF F/E TABLE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABSDR RRXA991486Skin · gougedDURING A MAINTENANCE VISIT, FOUND TWO SMALL GOUGES, LEFT WING CENTER LEADING EDGE LOWER SURFACE AT STA XS 478.897 AND STA XS 484.895 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALSDR RRXA991396Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FWD LAV SVC PANEL WELL AREA, ALSO RUSTED DOME NUTS BETWEEN STA 260 AND STA 280, AND BETWEEN LONGERONS 24 RIGHT AND LONGERON 26 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAWSDR RRXA991506Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RT WING, OUTBOARD LEADING EDGE O/B SECTION LWR. SURFACE I/B END, CORROSION CRACK AT STA XFS 710.000 AT FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATEDSDR UPS99829975Doubler · damagedINSPECTION TYPE:C-1, PERMANENT REPAIR TO AIRSTART CUTOUT (D161352) INCIDENT NR R598473 DATE OF OCCURANCE 10/22/98 ORIGINAL INCIDENT. AIRCART PULLED AWAY FROM AIRCRAFT WITH CART STILL CONNECTED. ACCOMPLISHED REPAIR IAW UPS EO DC8-5330-0793 AND UPS DC8 SRM 53-SDR RRXA991423Skin · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING O/B L/E I/B SECTION HAS CRACK AT DRIPLESS DRAIN AT STA 597.500. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REINSTALLED RIVET ACCEPTABLE TO RETURN TO SERVICE IAW FAA APPSDR RRXA991394Stiffener · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT CABIN BETWEEN STA 1745 AND STA 1766 FLOOR SUPPORT CHANNEL CROSS OVER STIFFENER HAS CORROSION EXFOLIATION EMANATING FROM FASTENERS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IASDR RRXA991387Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, LEADING EDGE CENTER SECTION I/B EDGE BETWEEN STA 291.5 TO 297.500, 15 TO 21 INCHES FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED SDR UPS99829954Battery Pack · dischargedINSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD.SDR UPS99829953Battery Pack · deadEMERGENCY LIGHTS INOP. FOUND EMERGENCY LIGHT SWITCH LEFT ON TURNED SWITCH OFF. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK, OPS CHECK GOOD.SDR RRXA991700Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-3 AT Y=360 BETWEEN X=16 TO X=24. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DSDR RRXA991695Angle · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO DOOR, SEAL ATTACHMENT ANGLE BETWEEN Y=213 TO Y=240. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW ATTACHMENT ANGLE AND INSTALLED SDR RRXA991694Angle · corrodedDURING MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CARGO DOOR, SEAL ATTACHMENT ANGLE BETWEEN SPOOLS 2 AND 3 AND BETWEEN Y=160 TO Y=180. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW ATTASDR RRXA991418Plenum · crackedDURING A MAINTENANCE VISIT, FOUND RT FWD PLENUM ASSY PRIMARY HEAT EXCHANGER HAS SEVERAL CRACKS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. STOPPED DRILLED CRACKS, WELDED IAW FAA APPROVED TENNESSEE TECHNICAL SERVISDR RRXA991419Door Panel · crackedDURING A MAINTENANCE VISIT, FOUND AFT LOWER CARGO COMPT STA 1540 AFT BULKHEAD DOOR BENT AND CRACKED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOOR IAW FAA APPROVED TENNESSEE TECHNICSDR RRXA991401Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BLISTER AND CRACK IN FINGER DOUBLER B PIT AT STA 506.000, LONGERON 30 RIGHT LOWER LEG, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CORROSION, CUT OUT DASDR UPS99829979Web · crackedINSPECTION TYPE:C-1, RUDDER STIFFENER INSIDE L/E AT STA ZR 110 IS CRACKED. FABRICATED AND INSTALLED NEW STIFFENER (WEB) IAW DAC DWG 5656229, DC 8 SRM 51-1-20D & 51-1-21.SDR UPS99829899Battery Pack · dischargedINSPECTION TYPE:PDC, AIRCRAFT EMERGENCY LIGHT WOULD NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01, OP CK GOOD.SDR RRXA991750Angle · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO VERTICAL STABILIZER FRONT SPAR ATTACHMENT ANGLE AT Y=1766 AND X=24. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SDR RRXA991410Skin · chafedDURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN RIGHT WING CENTER L/E STA 520.168, 30 TO 36 INCHES FWD OF FRONT SPAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT DOSDR UPS99829977Web · crackedINSPECTION TYPE:C-1, SUPPORT WEB BENEATH 2ND RUDDER DAMPENER CRACKED IN SEVERAL PLACES STA ZR155. REMOVED AND FABBED NEW 5656229-11 WEB IAW DAC DWG 5656229. REINSTALLED RIB, WEB AND SIDE SKIN IAW DC8 SRM 51-1-21 & 51-1-20D. REINSTALLED L/E SECTION IAW DC8 SSDR RRXA991620Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LEFT O/B AILERON I/B LWR ACCESS PANEL TOP PLATE AT XA 659. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW DC8 SRM 51-3-3. SDR RRXA991095Bulkhead · leakingAT APPROXIMATELY FLT LEVEL 230 CABIN PRESS WENT TO 10,000 FT, LEVEL OFF A FLT 220 TO MAINTAIN CABIN PRESSURIZATION. AIRCRAFT FERRIED TO EDDF FOR REPAIR. AFT PRESURE BULKHEAD REPAIRED PER BOEING ROD SKETCH 99-06-22-001, REF : EWA M/A NR AM-5312-01:00 AND WORKSDR UPS99829978Fitting · crackedINSPECTION TYPE:C-1, STRINGER-51 NR 2 MAIN O/B AT WS 74.00 REAR SPAR HAS FWD FITTING CRACKED. REPLACED CRACKED FITTING IAW DC8 SRM 51-1-20D.SDR RRXA991384Fitting · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, POPPED RIVET AND BULGE IN EXTERNAL SKIN, LONGERON FITTING END CORRODED INSIDE FWD ACCESSORY COMPARTMENT AT STA 8, LONGERON 32 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW SDR RRXA991686Bulkhead · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BULKHEAD MOUNT AT Y=1360 BETWEEN LONGERONS 34 LEFT TO 34 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED MOUNT, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW MOUNT IAW DCSDR RRXA991484Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766, BETWEEN LONGERONS 10 LEFT AND LONGERON 11 LEFT, APPROX 3-1/2 CRACK BETWEEN BL 35.0 RIGHT AND BL 35.750 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DCSDR RRXA991482Bulkhead · crackedDURING A MAINTENANCE VISIT FOUND CRACK, AFT PRESSURE BULKHEAD AT STA 1766 BETWEEN LONGERONS 10 RIGHT AND LONGERON 11 RIGHT, APPROX 3.75 INCH CRACK BETWEEN BL 33.50 LEFT AND BL 37.00 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW
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