Douglas DC-8-63F
Service difficulty reports · 1,883
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 = 'DC863F' 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 = 'DC863F' 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 ABXA9800530Angle · crackedLEFT INBOARD STUB WING AT STATION XS 250 CRACKED AT BOTTOM. INSTALLED REPAIR ANGLE STIFFENER IAW DWG 9753203 AND DC8 SRM 51-1-20.SDR ABXA9800491Fitting · crackedLONGERON 31L SPLICE BETWEEN STATION 440 TO 460 IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D.SDR ABXA9800529Intercostal · crackedINTERCOSTAL CRACKED AT STATION 1440 AND LONGERON 34R. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5616674.SDR ABXA9800528Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION XS 466.651 IS CRACKED AT THE AFT LWR END. REPAIRED IAW ABX DWG K05056 AND DC8 SRM 51-1-20D.SDR ABXA9800652Fitting · crackedSTATION 600-620, STRINGER 31R SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DWG 3750257 AND DC8 SRM 51-3-0.SDR IXXA9800106Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT VERTICAL STABILIZER PANEL BETWEEN STATIONS ZR 253 AND ZR 297. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWINSDR ABXA9800654Angle · crackedFORWARD AND AFT SIDES OF STATION 380 FLOORBEAM LBL 11 AND RBL 11. THE INTERCOSTAL ATTACH ANGLES ARE CRACKED. REMOVED, FABRICATED AND REPLACED ANGLES IAW DWG 5610326 AND SRM 51-1-21.SDR ABXA9800513Angle · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 785.0 IS CRACKED AT THE AFT LWR END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800512Angle · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 672.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800511Angle · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 778.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG NR K05056 AND DC8 SRM 51-1-8.SDR ABXA9800510Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 747.5 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056.SDR ABXA9800509Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XS 442.185 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056.SDR ABXA9800508Angle · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 603.75 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800507Angle · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 585.00 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800506Angle · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800504Angle · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 803.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800503Angle · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 822.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800502Angle · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 585.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800501Angle · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 772.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800500Angle · crackedRIGHT WING LEADING EDGE RIB AT STATION XS 448.501 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR ABXA9800492Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XS 448.50 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056.SDR ABXA9800490Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 347.75 IS CRACKED AT THE AFT LOWER END. REPAIRED RIB IAW DRAWING KO5056.SDR ABXA9800495Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XS 466.651 IS CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056.SDR ABXA9800494Angle · crackedTHE LEFT OUTBOARD SLOT BOX, OUTBOARD AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM END. REPAIRED IAW DC8 SRM 51-1-21 AND 57-3-3.SDR ABXA9800493Bulkhead Fitting · corrodedSTATION 70 BULKHEAD FORWARD SIDE LONGERON 31R INBOARD FITTING HAS HEAVY CORROSION ON LOWER FLANGE BELOW BOLT HEAD. REPLACED FITTING IAW SRM 51-1-21 AND DWG 4614397.SDR ABXA9800408Mount · shearedDURING C-CHECK, FOUND NR 3 ENGINE REAR INBOARD MOUNT ARM SHEARED AT THREADED PORTION. *S/D* REPLACED NR 3 LEFT AFT ENGINE MOUNT IAW DC8 MM 71-20-02.SDR CKSA98301Skin · damagedDURING ROUTINE B CHECK INSPECTION, FOUND RIVET PULLED FS 70 STRINGER 23R. REPAIRED SKIN IAW DC-8 SRM 53-2-1 FIG 7. CLASS II REPAIR INSTALLED. REPAIR MUST BE RE-INSPECTED EVERY 4000 LANDINGS (INITIAL INSPECTION OF 12,000 LANDINGS) AND REPLACED WITH CLASS I RSDR CKSA98300Skin · crackedDURING ROUTINE B CHECK INSPECTION, FOUND FS 100 AT STR 33L SKIN HAS CRACK. REPAIRED SKIN IAW DC-8 SRM 53-2-1 FIG 7. CLASS II REPAIR INSTALLED. REPAIR MUST BE RE-INSPECTED EVERY 4000 LANDINGS AND REPLACED WITHIN 24,000 LANDINGS IAW DC8 SRM 53-2-1 PARAGRAPH 16SDR CKSA98299Seat Track · corrodedDURING ROUTINE B CHECK INSPECTION, FOUND SEAT TRACK STA 490 RBL25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER DC-8 SRM 53-02-3. NON ROUTINE TASK CARD NUMBER 23625.SDR ABXA9800653Rib · crackedLEFT WING LEADING EDGE AT STATION XFS 716.250. THE UPPER RIB IS CRACKED AT THE AFT END. REPAIRED IAW ABX DWG K05056.SDR ABXA9800505Angle · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 791.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8.SDR IXXA9800107Panel · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT VERTICAL STABILIZER EXTERNAL PANEL BETWEEN STATIONS ZR 253 AND ZV 297. REPAIR ACCOMPLISHED REMOVAL OF AFFECTED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPRSDR ABXA9800371Up Latch Switch · out of adjustIN CRUISE FLIGHT, LANDING GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED LANDING GEAR. LANDING GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. SLOW FLEW AIRCRAFT AT 220 KNOTS. ADJUSTED LEFT GEAR DOOR UPLATCH IAW DC8 MM 32-31-4.SDR ABXA9800367Door Spring · out of adjustLANDING GEAR UNSAFE LIGHT ILLUMINATED DURING CRUISE FLIGHT WITH LEFT MAIN LANDING GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. RECYCLED GEAR, NO CHANGE. ADJUSTED LEFT MAIN LANDING GEAR PROXIMITY SWITCH TARGET STOP. REPLACED LEFT GEAR DOOR SPRING IAW DC8 MM 32SDR CKSA98267Stringer · crackedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS 1700 STRINGER 29R CRACKED AT END. STRESS CRACK (CORROSION) .0625 TO END OF STRINGER 29R FROM LAST FASTENER. REPAIRED STRINGER IAW EDR NO D805818 AND AIA/E/2808 DTD APRIL 18, 1998. CORROSION TASK CASDR CKSA98266Stringer · crackedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. STRINGER 26 POSSIBLE INDICATION OF CRACK. COMPLIED WITH HFEC INSPECTION, DETERMINED CRACK TO RUN FWD TO APPROX .0625 FROM 2ND FASTENER. FITTING CRACKED DUE TO CORROSION STRESS AT BOLT ATTACH POINT. RSDR ARWA980408Skin · corrodedON PREFLIGHT, FOUND EVIDENCE OF CORROSION AT APPROXIMATELY FS 640 L 33R AND 34R. REMOVED CORROSION, FOUND BEYOND LIMITS IAW SRM 53-2-0. REFER TO DOUGLAS MESSAGE MISC 546/JCT.SDR ABXA9800357Switch · defectiveLANDING GEAR UPLATCH CHECK FAILED. RED GEAR UNSAFE LIGHT AND LEFT MAIN\NGEAR DOOR UNLATCHED LIGHT ILLUMINATED. RECYCLED GEAR, NO CHANGE. PERFORMED ALTERNATE UPLATCH CHECK. REPLACED LEFT MAIN LANDING GEAR PROXIMITY SWITCH IAW DC8 MM 32-60-0, OPS CHECKED GOOSDR RRXA98177Cowling · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO NR 1 ENGINE RIGHT SIDE FAN COWLING, ZEE CLOSE-OUT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-0448SDR RRXA98166Cowling · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO NR 4 ENGINE, RIGHT SIDE AFT FAN COWLING, ZEE CLOSE-OUT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REOSDR RRXA98153Cowl · wornDURING A MAINTENANCE VISIT, FOUND NR 1 ENGINE FAN COWLING, ZEE CLOSE-OUT WORN. FABRICATED AND INSTALLED NEW ZEE CLOSE-OUT, (P/N 575716-503), IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04413.SDR CKSA98259Transformer · malfunctionON LANDING F/E'S PANEL BEHIND LIGHT SWITCH'S BEGAN TO ARC AND SMOKE. ON INSPECTION OF LIGHT SWITCHES FOUND DAMAGE ON FLOOD LIGHT SWITCHES PULLED BREAKERS AS REQUIRED AND TIED OFF CONTINUE DMI NR 8230998 IAW DC8 MM 33-1. REMOVED AND REPLACED RHEOSTAT TRANSFORSDR RRXA98179Skin · dentedDURING A MAINTENANCE VISIT, FOUND DENT TO FUSELAGE SKIN AT STA 114 AND LONGERON 23 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04496.SDR RRXA98172Fillet · corrosionDURING A MAINTENANCE VISIT, FOUND FILLET PANEL CORRODED RIGHT WING. FILLET PANEL DAMAGED BEYOND SRM REPAIR, FABRICATED AND INSTALLED NEW FILLET PANEL IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04463.SDR RRXA98159Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO FRAME FLANGE AT STA 1140 AND LONGERON 36. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04425.SDR RRXA98154Plank · corrosionDURING A MAINTENANCE VISIT, FOUND FLOOR PLANK EDGE CORRODED BEYOND LIMITATIONS IAW DC-8 SRM, AT STA 1580 TO 1689. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCHSDR RRXA98152Frame · damagedDURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO FRAME FLANGE RADIUS, AT STA 272 BETWEEN LONGERONS 32 RIGHT AND 33 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH REO-04411.SDR RRXA98185Fillet · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT WING FILLET PANEL, NR 162. REMOVED FILLET PANEL FOR REPLACEMENT, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FILLET PANEL IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04608.SDR RRXA98184Floorbeam · corrosionDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1726.656 AND BL 20 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04549.SDR RRXA98173Spar Cap · crackedDURING A MAINTENANCE VISIT FOUND RIGHT WING, FORWARD SPAR CAP LOWER CRACKED AT XFS=519. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04464.
Back to Douglas DC-8-63F