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 RRXA98155Frame · corrosionDURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE AT STA 1020 BETWEEN LONGERONS 34 LEFT TO 34 RIGHT. REMOVED DAMAGE SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH RESDR RRXA98151Skin · gougedDURING A MAINTENANCE VISIT, FOUND RIGHT WING, FLAP SKIN GOUGED AT XRS=230.5. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04407.SDR RRXA98150Skin · corrosionDURING A MAINTENANCE VISIT, FOUND FUSELAGE, INTERNAL SKIN WITH CORROSION DAMAGE AT STA 450 BETWEEN LONGERONS 34 LEFT AND 35 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENSDR ABXA9800279Doubler · corrodedFINGER DOUBLER HAS HEAVY CORROSION AT FS 20 TO 25, STRINGER 31R. REPAIRED IAW DC8 SRM 53-1-0 AND 51-1-20.SDR RRXA98158Channel · crackedDURING A MAINTENANCE VISIT, FOUND EXHAUST NOZZEL AT 12 O'CLOCK POSITION HAD PREVIOUS REPAIR, AND INTERNAL CHANNEL CRACKED.SDR RRXA98157Fairing · chafedDURING A MAINTENANCE VISIT, FOUND RIGHT WING, FLAP TRAILING EDGE FAIRING CHAFED AT OUTBOARD SECTION. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER ENGINEERING SKETCH REO-04420.SDR ABXA9800313Fitting · crackedLEFT WHEEL WELL FITTING CRACKED AT STATION XCW 23 BELOW PRESSURE PANEL. REPAIRED IAW DC8 SRM 51-1-8.SDR ABXA9800213Frame · crackedFUSELAGE TO FRAME 540 FORMER BETWEEN LONG 35R-36R IS CRACKED. REPAIRED IAW DC8 SRM 53-2-0.SDR ABXA9800205Fitting · brokenLEADING EDGE OUTBOARD INTERNAL STRUCTURE FITTING BROKEN BETWEEN NR 1 AND NR 2 PYLON. REPAIRED IAW DC8 SRM 51-1-20D.SDR ABXA9800204Bulkhead Web · crackedFUSELAGE STA 857 LBL 16 THE MAIN LANDING GEAR FORWARD BULKHEAD WEB IS CRACKED AT THE ADF ANTENNA LEAD ACCESS PANEL. REPAIRED IAW DC8 SRM 51-3-0.SDR ABXA9800203Fitting · crackedSTATION 1260 TO 1280 STRINGER 36 SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D.SDR ABXA9800242Web · crackedWEB CRACKED AT STATION 510 - 520 RIGHT, JUST AFT OF SERVICE DOOR AT FLOOR LEVEL. REPLACED WEB IAW DC8 SRM 51-1-20 AND DOUG DWG 9755569.SDR ABXA9800247Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 816.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056.SDR ABXA9800246Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION XFS 785.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056.SDR ABXA9800245Rib · crackedRIGHT WING LEADING EDGE RIB AT STATION 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056.SDR ABXA9800244Fitting · crackedSTATION 1040 - 1060 STRINGER 31R SPLICE FITTING IS CRACKED. REPLACED FITTING IAW SRM 51-1-20D.SDR ABXA9800239Rib · crackedRIGHT WING LEADING EDGE RIB AT STA XFS 616.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 51-2-0 AND DWG K 05056.SDR ABXA9800220Rib · crackedRIGHT WING LEADING EDGE RIB AT STA XFS 728.25 IS CRACKED AT THE AFT UPPER END. REPAIRED CRACKED RIB IAW SRM 57-2-0.SDR ABXA9800215Rib · crackedRIGHT WING LEADING EDGE RIB AT STA XFS 635.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05056.SDR ABXA980021Fitting · crackedFLOORBEAM END FITTING IS CRACKED AT STA 1220 AND STR 21R. REPAIRED IAW DWG 3754946 AND DC8 SRM 51-1-20.SDR CKSA98201Skin · corrodedDURING ROUTINE C-2 CHECK INSPECTION, FOUND B-PIT DOOR HAS CORROSION ON LOWER SEAL CHANNEL FWD LOWER TO AFT LOWER. REMOVED MINOR SURFACE CORROSION ON LOWER AFT CORNER AND AREA BETWEEN FWD AND AFT CORNER. .002 METAL REMOVED IS WITHIN LIMITS IAW DC8 SRM 52-2-0 SDR CKSA98200Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON FWD FACE OF FRAME AT FS Y180 ABOVE LONGERON 34R. CORROSION REMOVAL BEYOND DC8 SRM LIMITS IAW DC8 SRM 51-1-8 AND 53-2-0 FIG 7. HEAT TREATED AND AGED DOUBLER IAW DC8 SRM 51-1-1. LOCATED ANSDR CKSA98199Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. NR 1 T-BOLT BACK-UP FITTING CORRODED STA Y288. REMOVED NR 1 T BOLT BACK UP FITTING AT STA Y288. CLEANED AND PRIMED AREA IAW DC8 SRM 51-1-8. DRILLED NEW FITTING AND FABRICATED REPAIR SPLICES IAW DC8 SSDR CKSA98198Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON FITTING AT FS 340 BETWEEN LONGERON 34R AND 35R. CORROSION IS OUT OF LIMITS. REMOVED FITTING FROM STA 340 BETWEEN L34R AND 35R. CUT NEW FITTING, FABRICATED SPLICES IAW DC8 SRM 53-2-0 FIG 2SDR CKSA98197Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON FRAME TO SPAR FITTING CENTER WING UPPER SKIN UNDER CUSP RIGHT SIDE STA680 X=-64. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED FITTING AND REPLACED WITH NSDR CKSA98196Seat Track · corrodedDURING ROUTINE C-2 CHECK INSPECTION, FOUND COCKPIT FLOOR TRACK SECOND OBSERVERS SEAT AFT TRACK HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED AFT FLOOR TRACK AT SECOND OBSERVERS SEAT IAW DC8 SRM 51-1-21. SEAT TRACK DRILLED IAW DAC DWG NR 3657504. PRIMSDR CKSA98195Seat Track · corrodedDURING ROUTINE C-2 CHECK INSPECTION, FOUND COCKPIT FLOOR TRACK SECOND OBSERVERS SEAT FWD TRACK HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED FWD FLOOR TRACK AT SECOND OBSERVERS SEAT IAW DC8 SRM 51-1-21. SEAT TRACK DRILLED IAW DAC DWG NR 3657504. PRIMSDR CKSA98194Frame · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION OF FLOOR FRAME STA 240 ABOVE LONGERON 35L A PIT. AFTER REMOVAL OF CORROSION FLOOR FRAME OUT OF LIMITS. FABRICATED REPAIR FILLER AND DOUBLERS IAW DC8 SRM 53-2-0 FIG 2. HEAT TREATED AND AGED SDR CKSA98193Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON UPPER CUSP FITTING AT FS 580 LT. REMOVED UPPER CUSP FITTING AT STA 580 LT. CORROSION EVALUATION BEYOND LIMITS IAW DC8 SRM 53-2-0. TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8. INSTALLED NSDR CKSA98192Fitting · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION AND GOUGE MARK ON LT UPPER CUSP FITTING AT FS 1000. REMOVED OLD FITTING IAW DC8 SRM 53-1-0. DRILLED UP NEW FITTING ON LT UPPER CUSP AT FS 1000 IAW DC8 SRM 51-1-20D. INSTALLED NEW FITTING ATSDR CKSA98191Longeron · corrodedDURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION SPOT ON LT SIDE OF LONG 34 RT AT FS Y298 INSIDE DOOR CUT OUT. CORROSION REMOVAL IS BEYOND LIMITS OF DC8 SRM 53-2-0 FIG 1F. REMOVED SECTION OF LONG 34R FROM FS 285 TO 315 INSIDE DOOR CUTOUT. SDR CKSA98190Bulkhead Web · puncturedDURING ROUTINE C-2 CHECK INSPECTION, FOUND NUMEROUS PUNCTURES ON LOWER END OF 9G BULKHEAD. FABRICATED REPAIR DOUBLERS TO REPAIR PUNCTURES ON LOWER END OF 9G BULKHEAD, DRILLED AND DEBURRED DOUBLERS AND BULKHEAD, TREATED, PRIMED AND INSTALLED DOUBLERS IAW DC8 SSDR CKSA98189Bulkhead Angle · brokenDURING ROUTINE CPCP INSPECTION, FOUND BULKHEAD ATTACH ANGLE RT SIDE BETWEEN C AND D PITS FS 1320 HAS AREA BROKEN OUT AT TWO HOLES WHERE ATTACH ANGLE ATTACHES TO FRAME. REPAIRED BROKEN BULKHEAD ATTACH ANGLE RT SIDE BETWEEN C AND D PITS IAW DC8 SRM 53-2-0 FIG 1SDR CKSA98188Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND CAPT'S UPPER SEAT TRACKS WORN. REMOVED AND REPLACED BOTH FWD SEAT TRACK T'S AT CAPT'S POSITION IAW DC8 SRM 53-1-0 AND 51-1-20D. INSTALLATION OK. AFTER CAPT'S SEAT INSTALLATION SEAT TRACK AND SEAT OPERATES GOOD AT ASDR CKSA98187Skin · damagedDURING ROUTINE CPCP INSPECTION, FOUND SKIN TORN DAMAGE TOP OF DOOR CUT OUT BOX FS 320 TO 330 ABOVE LONGERON 35 RT. ROUTED OUT DAMAGED AREA AT FS 320 TO 330 LONGERON 35 RT. FABRICATED FILLER AND REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D. TREATED AND PRIMED PASDR CKSA98186Flange · crackedDURING ROUTINE CPCP INSPECTION, FOUND FRAME FLANGE CRACKED STA Y420 ABOVE LONGERON 36. REMOVED INTERCOSTAL AT FS 420 TO ACCESS DAMAGE AREA FROM LONGERON 35 TO 36RT. REMOVED DAMAGE, FABRICATED PLUG AND 2 REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 2. HEAT TREATEDSDR CKSA98185Skin · corrodedDURING ROUTINE C-2 CHECK INSPECTION, FOUND LEFT WHEEL WELL BARE METAL WITH SLIGHT CORROSION ON TOP OF LONGERON 24 STA 980 AROUND 2 AFT BOLT HEADS. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND CRACK AT FS 980 ON LONGERON. STOP DRILLED CRACK, FABRICATED REPAIRSDR CKSA98184Fitting · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND HOLES DRILLED INTO RT UPPER CUSP FITTING AT FS 1000. REMOVED AND REPLACED CUSP FITTING AT FS 1000 IAW DC8 SRM 51-1-20D AND 51-3-0. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04793 TASK NR Y1252.SDR CKSA98183Frame · crackedDURING ROUTINE CPCP INSPECTION, FOUND LT FRAME CRACKED AT FS 1560. REMOVED CUSP FITTING AND CUT OUT CRACKED FRAME SEGMENT ON LT FRAME STA 1560. FABRICATED NEW FRAME SEGMENT AND DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0 FIG 2 SHEET 4 VIEW J. HEAT TREATED 7075-SDR CKSA98182Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 480, 5.5 ABOVE UPPER CUSP AREA. PLUGGED HOLES, FABED SHIM, ANGLE AND DRILLED RT FRAME AT FS 480 IAW COTNEY DWG NR D93-R15 AND DC8 SRM 51-1-21 AND 51-1-8. CORROSION TASK CARD NUMBSDR CKSA98181Frame · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 560, 5.5 ABOVE UPPER CUSP AREA. FABRICATED REPAIR ANGLE IAW COTNEY DWG NR D93-R02. HEAT TREATED AND AGED IAW DC8 SRM 51-1-1. PERFORMED CONDUCTIVITY TEST ON HEAT TREATED ANGLE ITSDR CKSA98180Skin · damagedDURING ROUTINE C-2 CHECK INSPECTION, FOUND RT WING L/E STA XFS710 LOWER SEAM SCREW HEADS PULLED THROUGH L/E SKIN. FABRICATED FILLER PLATE FROM 7075-T6 .063 IAW SRM 57-2-1 FIG 2H PG 15 AND INSTALLED REPAIR ON RT WING L/E STA XFS710 LOWER SEAM SCREWS IAW SRM 57SDR CKSA98179Fitting · misdrilledDURING ROUTINE CPCP INSPECTION, FOUND LT UPPER CUSP FITTING AT FS 600 DRILLED INTO. REMOVED LT UPPER CUSP FITTING AT FS 600. POSITION AND FITTED NEW CUSP FITTING IAW DC8 SRM 53-1-0. INSTALLED FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. CORROSION TASK CARD NUMSDR CKSA98178Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND FITTING CRACKED ON STA 857 FRAME RT SIDE 20 INCHES ABOVE CUSP. REMOVED FITTING FROM STA 857 FRAME, FABRICATED FITTING IAW DAC DWG NR 3779498. LOCATE AND PICKED UP ALL ATTACHMENT LOCATIONS IAW DC8 SRM 51-1-20D. TREATED ASDR CKSA98177Fitting · crackedDURING ROUTINE CPCP INSPECTION, FOUND FITTING CRACKED ON STA 902 FRAME RT SIDE 20 INCHES ABOVE CUSP. REMOVED DAMAGED FITTING, FABRICATED NEW FITTING IAW DAC DWG NR 3779498. DRILLED UP NEW FITTING PER DC8 SRM 53-1-0 AND 51-1-20D. TREATED AND PRIMED IAW DC8 SSDR CKSA98176Skin · crackedDURING ROUTINE C-2 CHECK INSPECTION, FOUND A PIT DOOR INNER SKIN CRACKED 2 PLACES UPPER FWD CORNER. STOP DRILLED CRACK AND FABRICATED, HEAT-TREATED, TREATED AND PRIMED AND INSTALLED DOUBLER ON CRACK A-PIT DOOR INNER SKIN IAW DC8 SRM 51-1-1, 51-1-21, 52-4-1 PGSDR CKSA98175Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1400, BL 45RT. CUT OUT DAMAGED AREA 2 PLACES FOR PLUG REPAIR AT STA 1400 BL 45RT IAW DC8 SRM 53-2-3. TREATED AND PRIMED AREA OF REPAIR IAW DC8 SRM 51-1-8. INSTALLED PLUG REPAIRS IAW DC8 SRM 51-SDR CKSA98174Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 860, BL 45RT. REMOVED THE DAMAGED CARGO TRACK AT STA 860, BL 45RT. CORROSION TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNELS AND PLUGS ON CARGO TRACK AT STA 860 BL 45RT IAW DC8 SRM 53SDR CKSA98173Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 770 BL 24RT. CUT WORN OUT SEAT TRACK AT STA 770, BL 24RT. INSTALLED CHANNELS AND SEAT TRACK IAW DC8 SRM 53-2-3 FIG DG. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 04472 TASK NR Y1583.SDR CKSA98172Seat Track · wornDURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1130, BL 24RT. CUT THE DAMAGED SEAT TRACK AT STA 1130 BL 24RT TO FIT PLUGS AND CHANNELS. INSTALLED THE PLUGS AND CHANNELS FIT IN TRACK STA 1130, BL 24RT IAW DC8 SRM 53-2-3 FIG 6D. C-CHECK WORK
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