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 RRXA991388Finger Dougler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, BLISTER AT FINGER DOUBLER AT STA 616 BETWEEN LONGERONS 32 RIGHT AND LONGERON 33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEWSDR DHL99806002Computer · malfunctionedON TAKEOFF ROLL, STICK SHAKER CAME ON AND STAYED ON, REJECTED TAKEOFF. REMOVED AND REPLACED LIFT COMPUTER, LIFT TRANSDUCEER, STALL WARNING MOD TRANSFER RELAY.SDR UPS99829853Battery Pack · dischargedINSPECTION TYPE:N/A, DURING CREW PREFLIGHT EMERGENCY EXIT LIGHTS FAILED TEST. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. LIGHTS CHECK GOOD.SDR RRXA991403Skin · crackedDURING A MAINTENANCE VISIT FOUND CRACK IN SKIN AT STA 55, LONGERON 34 RIGHT EXTERNAL. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED TENNESSEE TECHNICAL SESDR RRXA991395Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 31 LEFT AT STA 1220. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLATE DOUBLER IAW DC8 SRM 51-1-21 AND IAW FAA APPROVED TENNESDR RRXA991380Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, SKIN, BOTTOM OF FWD LAV SERVICE PANEL BETWEEN STA 75R AND STA 105R, AND BETWEEN LONGERONS 25 RIGHT AND LONGERON 28 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51SDR UPS99829970Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 2 MAIN O/B AT W/S 74.000 REAR SPAR HAS AFT FITTING CRACKED. REMOVED AND REPLACED END FITTING IAW DAC DAW 5613423 AND DC8 SRM 51-1-20 D.SDR UPS99829969Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN I/B AT W/S 74.000 REAR SPAR HAS FWD AND AFT FITTINGS CRACKED. REMOVED AND REPLACED FITTINGS W/SERVICABLE PART IAW DAC DWG 5613423 AND DC8 SRM 51-1-20D.SDR UPS99829968Fitting · crackedINSPECTION TYPE:C-1, STRINGER 51 NR 3 MAIN IB AT FS 74 REAR SPAR HAS TWO CRACKED FITTINGS. REMOVED AND REPLACED END FITTING IAW UPS DC8 SRM 51-2-20D AND DWG 3704 841.SDR UPS99829960Fitting · crackedINSPECTION TYPE:C-1 LONGERON END FITTING CRACKED L10L AFT SIDE OF FRAME 902. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-21.SDR RRXA991746Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1680 AND X=56. 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 RRXA991739Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A-2 BETWEEN Y=1000 TO Y=1300 AND X=50. 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 APPROVESDR RRXA991692Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT BEAM HAT CHANNEL BETWEEN AT Y=1766 AND LONGERON 35 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT CHANNELSDR RRXA991691Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL BETWEEN Y=1745 TO Y=1766 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT SDR RRXA991690Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL AT Y=1766 AND X=-10. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT CHANNEL IAW DC-8 SRM 51-3-SDR RRXA991689Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR SUPPORT FRAME HAT CHANNEL AT Y=1745 AND X=-10. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW HAT CHANNEL IAW DC-8 SRM 51-3-SDR RRXA991688Floorbeam · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM UPPER SURFACE AT Y=1700 BETWEEN LONGERONS 21 LEFT TO 21 RIGHT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 53-2-0.SDR RRXA991745Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1680 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 APPROVEDSDR RRXA991744Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL A BETWEEN Y=1300 TO Y=1620 AND X=50. 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 RRXA991742Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-3 BETWEEN Y=1300 TO Y=1680 AND X=-20. 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 RRXA991741Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D-3 BETWEEN Y=1300 TO Y=1680 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 RRXA991738Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=1000 TO Y=1300 AND 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 IAW FAA APPROVESDR RRXA991737Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL E-1 BETWEEN Y=1000 TO Y=1300 AND 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 IAW FAA APPROVSDR RRXA991736Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL F BETWEEN Y=1000 TO Y=1300 AND X=-50. 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 RRXA991709Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL D AT Y=907 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 APPROVED DER ENGINEERINGSDR RRXA991693Doubler · corrodedDURING FOUND CORROSION DAMAGE TO L-1 DOOR WINDOW EXTERNAL DOUBLER AT Y=160 LT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED DOUBLER, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW DC-8 SRM 51-1-20.SDR RRXA991424Frame · crackedDURING A MAINTENANCE VISIT, FOUND MAIN CARGO DOOR UPPER JAM 2 AREAS CRACKED OUT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLERS IAW FAA APPROVED TENNESSEE TECHNICAL SERVICESDR UPS99829967Fitting · crackedINSPECTION TYPE:C-1 SPLICE FITTING FS 1050 AT LONGERON 35 RT IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-3-2 AND 51-1-20D.SDR UPS99829966Intercostal · crackedINSPECTION TYPE:C-1 INTERCOSTAL CRACKED AT LONGERON 35L BETWEEN FS 1080-1100. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DAC DWG 9758507 AND DC8 SRM 51-1-20D.SDR UPS99829961Splice · crackedINSPECTION TYPE:C-1 STA 1700 LONG 24 LEFT FRAME SPLICE IS CRACKED. REMOVED FABRICATED AND INSTALLED FRAME SPLICE IAW DC8 SRM 51-1-20D, 53-5-3, DAC DWG 612142, 51-1-8 AND 51-1-20D.SDR RRXA991751Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO EXTERIOR SKIN PANEL AT Y=718 AND LONGERON 35 RIGHT. 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 DERSDR RRXA991701Floor Panel · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO UPPER FLOOR PANEL BETWEEN Y=409 TO Y=417 AND LONGERON 21 LEFT. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SDR UPS99829963Floor · corrodedINSPECTION TYPE:C-1, CORROSION ON FLOOR PANEL AT RBL 35 AT FS 350. REMOVED CORROSION, FABRICATED REPAIR DOUBLER IAW DC8 SRM 53-2-3 AND INSTALLED REPAIR.SDR UPS99829965Frame · corrodedINSPECTION TYPE:C-1, CORROSION EMITTING FROM AROUND AND UNDER NUT PLATES ON BOTTOM SIDE OF FRAME FLANGE AT STA 100 BETWEEN LONG 34R TO 36. REMOVED CORRODED MATERIAL OUT OF LIMITS. REPAIRED WITH FILLER/DOUBLER REPAIR IAW DAC DWG 9753784, 53-2-0, 51-1-8, 51-1-SDR UPS99829800Girt Bar · inoperativeCREW ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT BAR INOP. REPOSITIONED GIRT BAR LOCKING CLIPS ON FLOOR, GIRT BAR LOCK CKS GOOD.SDR RRXA991412Plate · chafedDURING A MAINTENANCE VISIT FOUND SCREW PULLING THROUGH SKIN LEFT WING CENTER L/E LWR SURFACE STA XFS 304, 2 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 DOUBLER IAW FAA ASDR RRXA991411Skin · chafedDURING A MAINTENANCE VISIT, FOUND CRACK EMANATING FROM RIVET LT WING CENTER L/E STA XFS 304, 15 FWD OF FRONT SPAR ON LWR SURFACE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW FASDR RRXA991390Cargo Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT BETWEEN STA 980 AND STA 1100 TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK IAW DC8 SRM 51-1SDR RRXA991389Cargo Track · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, AFT LOWER CARGO COMPARTMENT BETWEEN STA 1020 AND STA 1140, FLOOR TRACK. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW TRACK IAW DC8 SDR RRXA991379Doubler · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, AFT LOWER CARGO COMPARTMENT AT STA 1220, BL 45 RIGHT FLOOR STRUT DOUBLER NEXT TO FLOORBEAM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED DOUBLER IAW SDR UPS99829964Seat Track · corrodedINSPECTION TYPE:C-1, SEAT TRACK AT STA 870, BL O.O CORR DOT E560. REMOVED CORROSION IAW DC8 SRM 51-1-8 NOT WITHIN LIMITS IAW DC8 SRM 5 3-2-3. REMOVED DAMAGED SECTION OF TRACK STA 850-890 IAW DC8 SRM 53- 2-3. INSTALLED NEW TRACK SECTION IAW DC8 SRM 53-2-3.SDR UPS99829962Floor · corrodedINSPECTION TYPE:C-1 FLOOR PNL 58-880 ROW A IS CRACKED AT ATTACH HOLE, HAS 2 EACH GOUGES, NUMEROUS AREAS OF BARE METAL AND CORROSION, AND MISSING/DAMAGED NON- SKID. FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0 FIG LF. INSTALLED NON-SKID TAPE AS NECESSARY IAW SDR UPS99829957Floor Panel · corrodedINSPECTION TYPE:C-1 FLOORBOARD CORRODED ROW-C FS880-1000. REMOVED CORROSION IAW DC8 SRM 51-1-8, REPAIR CORRODED AREA IAW DC8 SRM 53-2-3. ALODINE AND PRIME IAW DC8 SRM 51-1-8, INSTALL REPAIR DOUBLER IAW DC8 SRM 51-1-21.SDR UPS99829956Floorboard · corrodedINSPECTION TYPE:C-1 FLOOR PANEL FS 1470 LBL 35 HAS CORROSION BULGE AROUND INSERT. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0, FAB DOUBLER IAW DC8 SRM 53-2-3, INSTALL DOUBLER IAW DC8 SRM 51-1-8.SDR UPS99829955Floorboard · corrodedINSPECTION TYPE:C-1 FLOORBOARD CORRODED AROUND INSERT FS 1420 LBL 10. REMOVED CORROSION IAW DC8 SRM 51-1-8, CUT OUT DAMAGE AND REPAIR IAW DC 8 SRM 53-2-3 ALODINE AND PRIME REPAIR DOUBLER IAW DC8 SRM 51-1-8. INSTALLED ALL REPAIR DOUBLER IAW DC8 SRM 51-1-21A.SDR UPS99829928Floorbeam · corrodedINSPECTION TYPE:C-1, MAIN CABIN RT SIDE FS 1680 BL 24 THRU 34 FLOORBEAM T-CAP CORRODED ON UNDERSIDE OF NUT PLATE. FAB NEW ANGLE IAW DOUGLAS DWG 5892151, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-3-0.SDR UPS99829890Doubler · crackedINSPECTION TYPE: C1, RT W/W INBOARD DOOR, AFT CORNER OF TONGUE REPAIR. DOUBLER GOUGED AND CRACKED. REPAIRED BY FABRICATION AND INSTALLATION OF DOUBLER IAW DC 8 SRM 52- 2-0 AND DC 8 SRM 51-1-21, 51-1-20A, 51-3-0. SEALED REPAIR IAW DC8 SRM 51-1-16.SDR RRXA991621Splice · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LWR FWD CARGO COMPT AT STA 616 AND LONGERON 31 RIGHT, SPLICE CRACKED AND HAS CORROSION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SSDR RRXA991382Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION, WING, LEFT WING I/B L/E UPPER SURFACE AT STA XFS 54.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLERS IAW FAA APPROVED TENNESDR UPS99829773Switch · failedINSPECTION TYPE:ASN, CABIN DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. ACARS SENSORS (MAIN CREW) CONFIRMED DOOR. AIRCRAFT MAINTAINED DIFFERENTIAL PRESSURIZATION. DOOR APPEARS CLOSED AND SECURE. REPLACED LEFT AFT SERVICE DOOR MICROSWITCH AND CHECKED PER 52-70.
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