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 CKSA98121Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1360, 5.5 ABOVE UPPER CUSP AREA. FABRICATED REPAIR ANGLE AND SHIMS DRILLED AND DEBURRED FRAME AND PARTS AND TRIMMED OUT DAMAGE IAW COTNEY DWG NR D93-R58. HEAT TREATED REPAIR ANGLSDR CKSA98120Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1160, 5.5 ABOVE UPPER CUSP AREA. FABRICATED PARTS, HEAT TREATED, AGED, FORMED, TREATED AND PRIMED AND INSTALLED PARTS IAW COTNEY DWG NR D93-R57. FORMED AND HEAT TREATED PARTS IAWSDR CKSA98119Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1140, 5.5 ABOVE UPPER CUSP AREA. PLUGGED SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1140, 5.5 ABOVE UPPER CUSP AREA. FABRICATED, LOCATED, DRILLED, ADDED FASTENERS AS REQUIRED, DEBSDR CKSA98118Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1020, 5.5 ABOVE UPPER CUSP AREA. FABRICATED REPAIR SHIM AND ANGLE AS REQUIRED BY COTNEY D93-R54 AT FS 1020. HEAT TREATED TO 7075.T6 FROM 7075.0 AGED, PRIMED AND INSTALLED IAW COTSDR CKSA98117Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1000, 5.5 ABOVE UPPER CUSP AREA. FABRICATED REPAIR IAW COTNEY D93-R46 FROM 7075.0 HEAT TREATED 7075-T6 .071. TREATED AND PRIMED REPAIR. INSTALLED SAME INSTALLED INTERCOSTAL SHIMSDR CKSA98116Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 980 5.5 ABOVE UPPER CUSP AREA. FABRICATED, DRILLED HOLES, PLUGGED HOLES, TREATED AND PRIMED AND INSTALLED DOUBLER IAW COTNEY DWG D93-R47. CORROSION TASK CARD NUMBER 573R-0551. NSDR CKSA98115Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 940, 5.5 ABOVE UPPER CUSP AREA. FABRICATED AND FORMED REPAIR ANGLES FOR REPAIR AT FS 940 RT 5.5 ABOVE UPPER CUSP AND HEAT TREATED IAW DC8 SRM 51-1-1 AND COTNEY DWG NR D93-R36. FASDR CKSA98114Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 940, 5.5 ABOVE UPPER CUSP AREA. FABRICATED AND FORMED REPAIR ANGLES FOR REPAIR AT FS 940 RT 5.5 ABOVE UPPER CUSP AND HEAT TREATED IAW DC8 SRM 51-1-1 AND COTNEY DWG NR D93-R36. FASDR CKSA98113Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 540, 5.5 ABOVE UPPER CUSP AREA. PLUGGED HOLES, FAB AND DRILLED ANGLE DOUBLER AND SHIM IAW COTNEY SKETCH NR D93-R14 AT FS 540 RT 5.5 ABOVE UPPER CUSP. TREATED, PRIMED AND INSTALLESDR CKSA98112Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 500, 5.5 ABOVE UPPER CUSP AREA. FAB AND INSTALLED REPAIR IAW COTNEY DWG NR D93-R10, FABRICATED REPAIR ANGLE, LOCATED, ADDED FAST ATTACHMENTS, PICK-UP EXISTING ATTACHMENTS. TREATESDR CKSA98111Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1580 AT UPPER CUSP AREA. PLUGGED MISDRILLED HOLES ON FS 1580 LT AT APPROX CUSP AREA. FABRICATED REPAIR DOUBLER IAW COTNEY DWG NR D93-R13. HEAT TREATED IAW DC8 SRM 51-1-1. TREATSDR CKSA98110Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1060 AT UPPER CUSP AREA. FABRICATED ANGLE AND SHIM IAW D93-R07 LT SIDE FRAME FS 1060 LT SIDE. INSTALLED ANGLE AND SHIM, FABRICATED FOR LT SIDE FRAME STA 1060 IAW COTNEY DWG D93-RSDR CKSA98109Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND PREVIOUS CORROSION BLEND ON RT FRAME AT FS 880 STILL SHOWS CORROSION. CORROSION BEYOND LIMITS. REMOVED AND REPLACED FRAME SEGMENT IAW DC8 SRM 53-3-0, 51-3-0 AND 51-1-20D. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTISDR CKSA98108Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, FOUND SUSPECTED CORROSION BULGE AT FS 350 BETWEEN LONG 26 TO 27 RT ON OUTER SKIN. REMOVED CORROSION IAW DC8 SRM 51-1-8. CORROSION REMOVAL BEYOND LIMITS. REMOVED DISCREPANT SKIN PLATING. CUT OUT DAMAGED AREA, FABRICATED, TSDR CKSA98107Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND CORROSION AND GOUGE ON LT FRAME AT FS 1040 AT UPPER CUSP AREA. REMOVED CORROSION IAW DC8 SRM 53-20-0 FIG 1F. REMOVAL IS WITHIN (.002) LIMITS IAW DC8 SRM 53-2-0 FIG 1F. TREATED AND PRIMED IAW DC8 SRM 51-1-8 AND FABRICATESDR CKSA98106Stringer · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON STRINGER FS 1100 ON TOP AT LONG 36. CORROSION REMOVAL OUT OF LIMITS IAW DC8 SRM 53-2-0, FIG 1F. FAB REPAIR AND INSTALLED ON FRAME STA 1100 IAW DC8 SRM 53-2-0 PAGE 5/6 FIG 2. FAB REPAIR ASDR CKSA98105Skin · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND 2 DENTS ON FUSE SKIN STA 130 TO 135 AT LONG 28 LT. SKIN DAMAGED LEFT SIDE STA 131 TO STA 158 JUST ABOVE LONG 28 LT HOLE 2.5 X 1.0 WITH GOUGE 27 EXTENDING AFT. REPAIRED TWO DENTS IAW COTNEY ENGINEERING DWG D99-R03 REV SDR CKSA98104Skin · damagedDURING ROUTINE C-CHECK INSPECTION, FOUND SKIN TORN AT FS 345 LONG 30RT. REMOVED DAMAGE, FABRICATED REPAIR FILLER AND DOUBLERS. LOCATED PICKUP EXISTING ATTACHMENTS. TRIM AND COUNTERSINK REPAIR DOUBLERS AND INSTALLED DOUBLERS IAW COTNEY DWG NBR D99-R02. NONSDR ABXA9800294Angle · crackedCOCKPIT SUB FLOOR AT STATION -25 RBL 8, INTERCOSTAL IS CRACKED AT FWD END (FLOOR SUPPORT ANGLE). REPAIRED IAW DWG 5613327 AND DC8 SRM 51-1-21.SDR ABXA9800225Tie Fitting · crackedFLOORBEAM STA 680 RBL-24 TO WING BOX TIE FITTING CRACKED. REPAIRED IAW DWG 4645517 AND DC8 SRM 51-1-8.SDR ABXA9800231Intercostal · crackedINTERCOSTAL CRACKED AT RBL 40 BETWEEN STATION 980 AND 1000. REPAIRED IAW DC8 SRM 53-2-0.SDR ABXA9800207Intercostal · crackedINTERCOSTAL ATTACH ANGLE CRACKED AT STATION 520 AND STATION 540, RBL 10. REPAIRED IAW SRM 51-1-21, SRM 53-2-0, AND SRM 51-1-20.SDR RRXA98147Skin · crackedDURING A MAINTENANCE VISIT, FOUND LEFT WING, LEADING EDGE, LOWER SKIN CRACKED AT XFS=326. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04378.SDR ABXA9800211Rib · crackedRIGHT WING LEADING EDGE RIB CRACKED AT STA XFS 697. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506.SDR ABXA9800143Fitting · crackedATTACH FITTING CRACKED OUTBOARD, AFT SIDE OF STRINGERS 10 AT XRS 74, LEFT WING. REPAIRED IAW ABX REA D828-21938MR.SDR ABXA9800142Frame · corrodedSTA 1000 AT LONGERON 36 ATTACH AREA, FRAME FLANGE AND HARDWARE IS CORRODED. REPAIRED IAW ABX REA D853-21904MR.SDR ABXA9800141Web · crackedSTA 270, LONGERON 33L TO LONGERON 34L WEBBING IS CRACKED UNDER Z-FITTING IN TORQUE BOX. REPAIRED IAW ABX REA D853-21920MR.SDR ABXA9800140Spar Cap · corrodedLEFT WING UPPER SKIN FRONT SPAR CAP CORRODED. REPAIRED IAW ABX REA D857-21941MR.SDR ABXA9800139Rib · crackedCRACK AT LEADING EDGE RIB, NR 3 PYLON. REPAIRED IAW ABX REA D857-21918MR.SDR ABXA9800138Doubler · crackedRIGHT WING LEADING EDGE INTERNAL DOUBLER CRACKED. REPAIRED IAW ABX REA D857-21919MR.SDR ABXA9800137Skin · corrodedCORROSION ON LOWER SKIN AT LEFT WING LEADING EDGE, JUST INBOARD OF NR 2 STUB WING, AFT OF SLOT DOOR. REPAIRED IAW ABX REA D857-21927MR.SDR ABXA9800232Tie Fitting · crackedFORWARD ACCESSORY COMPARTMENT STA 660 LEFT FRAME TO LONGERON 36, TIE FITTING IS CRACKED. REPAIRED IAW DOUGLAS DWG 3750497 AND DC8 SRM 51-1-20D.SDR ABXA9800293Doubler · crackedRIGHT WING LEADING EDGE SKIN INTERNAL DOUBLER BETWEEN STA XFS 597 AND XFS 603 IS CRACKED AT THE TAI EXHAUST HOLES. REPAIRED IAW DWG 5769600 AND DC8 SRM 51-1-21.SDR ABXA9800282Rib · crackedAT XFS 220.0, NR 2 STUB WING RIB (UPPER) IS CRACKED. REPAIRED IAW DWG K05056.SDR ABXA9800233Angle · crackedRIGHT WING LEADING EDGE STA XS 250.089 THE OUTBOARD AFT VERTICAL STIFFENER FOR THE INBOARD SLOT IS CRACKED AT THE LOWER END. REPAIRED IAW DWG 9753293 AND DC8 SRM 51-3-0.SDR ABXA9800286Rib · crackedNR 3 STUB WING RIB IS CRACKED AT STA 270 (UPPER RIB). REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D.SDR ABXA9800283Intercostal · crackedSTATION 520 RBL 10 ON CEILING INTERCOSTAL ATTACH ANGLE IS CRACKED. REPAIRED IAW DC8 SRM 53-7-7 AND 51-1-21D.SDR ABXA9800234Rib · crackedNR 2 STUB WING LOWER RIB CRACKED AT XFS 245.0. REPAIRED IAW DWG K05056-7005 AND DC8 SRM 51-1-21D.SDR ABXA980023Doubler · crackedRIGHT WING LEADING EDGE INTERNAL DOUBLER AT STA XFS 330 IS CRACKED. REPAIRED IAW DWG 5769589 AND DC8 SRM 51-1-8.SDR ABXA9800224Rib · crackedLEFT WING LEADING EDGE BETWEEN THE NR 1 AND NR 2 PYLONS HAS 3 UPPER RIBS CRACKED. REPAIRED IAW SRM 57-2-0.SDR ABXA980022Intercostal · crackedINTERCOSTAL UPPER FLANGE CRACKED AT LONGERON 33R JUST AFT OF FUSE STA 400. REPAIRED IAW DWG 5750726 AND DC8 SRM 51-1-21.SDR ABXA9800181Support · crackedNR 2 STUB WING INBOARD SUPPORT LEG CRACKED. REPAIRED IAW DWG 5769859 AND SRM 51-1-29.SDR ABXA9800308Longeron · corrodedLONGERON 32L CORRODED BEYOND LIMITS AT STATION 1746 TO 1756. REPAIRED IAW DC8 SRM 53-22.SDR ABXA9800227Rib · crackedLEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 647.5. REPAIRED IAW DWG K 05056 AND DC8 SRM 51-1-20D.SDR ABXA9800182Rib · crackedRIGHT WING LEADING EDGE RIB UPPER ARM CRACKED 7TH RIB INBOARD FROM OUTBOARD EDGE OF OUTBOARD SLOT. REPAIRED IAW SRM 57-20 AND DWG K05056.SDR ABXA9800190Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 722.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D.SDR ABXA9800189Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 820.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D.SDR ABXA9800188Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 826.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D.SDR ABXA9800187Rib · crackedLEFT WING LEADING EDGE RIB AT STATION XFS 7725 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D.SDR ABXA9800186Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 772.50 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0, 51-1-8 AND 51-1-21.
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