Douglas DC-8-62
Service difficulty reports · 2,778
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 = 'DC862' 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 = 'DC862' 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 ABXA9900292Fitting · crackedDURING C-CHECK, FOUND FITTING CRACKED AT LONGERON 11 LEFT, STATION 680. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-3-0.SDR ABXA9900289Fitting · corrodedDURING C-CHECK, FOUND CORROSION ON CUSP FITTING AT STATION 1200 LT SIDE. REPLACED FITTING IAW DC8 SRM 51-30-0 AND 51-1-20D.SDR ABXA9900288Fitting · corrodedDURING C-CHECK, FOUND CORROSION ON STATION 1530 PRODUCTION SPLICE FITTING AT LONGERON 34 RIGHT. REPLACED FITTING IAW DC8 SRM 51-30-0 AND 51-1-20D.SDR ABXA9900287Fitting · corrodedDURING C-CHECK, FOUND CORROSION ON LONGERON FITTING, STATION 1540, LONGERON 32 RIGHT AT AFT PRESSURE BULKHEAD. REPLACED FITTING IAW DC8 SRM 51-3-0 AND 51-1-21.SDR ABXA9900279Fitting · crackedDURING C-CHECK, FOUND PRODUCTION SPLICE FITTING CRACKED AT STATION 1530, LONGERON 34 LEFT. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-3-0.SDR ABXA9900278Fitting · crackedDURING C-CHECK, FOUND 3 FITTINGS CRACKED AT BOTTOM OF KEEL BEAM BETWEEN MAIN LANDING GEAR DOORS, STATION 940 TO 960. REPLACED KEEL BEAM FITTINGS IAW DC8 SRM 51-3-0.SDR ABXA9900276Fitting · crackedDURING C-CHECK, FOUND PRODUCTION SPLICE FITTING AT STATION 1530 LONGERON 34 RIGHT CRACKED AND CORRODED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-21 AND 51-3-0.SDR ABXA9900275Link · crackedDURING C-CHECK, FOUND NR 2 PYLON OUTBOARD THRUST LINK CRACKED. REPLACED PYLON THRUST LINK IAW DC8 MM 71-20-1.SDR IXXA9900003Fan · failedEN ROUTE FROM AJK TO AVB, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT EMITTING FROM THE LEFT RECIRCULATION FAN. THE CREW TURNED OFF THE FAN AND THE ODOR DIMINISHED. MAINTENANCE INSPECTED AND FOUND THE FAN DEFECTIVE. MAINTENANCE DEFERRED THE LEFT RECIRCULASDR ARWA990203Light · malfunctionedMIA - LANDING GEAR DOOR NOT LATCHED. REMAINED ON, WARNING LIGHT ILLUMINATED. AFTER ALL ABNORMAL PROCEDURES WERE PERFORMED. RETURNED TO MIAMI WITHOUT INCIDENT. T/S FOUND DOOR NOT LATCHED WARNING LIGHT SOCKET DAMAGE. REMOVED AND REPLACED ELECTRICAL SOCKET ISDR 99T64R063ARFrame · corrodedFUSELAGE LONGERON 25L FRAME 119L FINGER DOUBLER AT FLOORBEAM COCKPIT SUB FLOOR CORROSION EXFOLIATION. REMOVED CORROSION BY CUTTING OUT DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND INSTALLED PER EO DRAWING NR 99-006 WITH 8110-3 DATED 0/21/99. (M)SDR 99T64R062ARFrame · corrodedFUSELAGE STATION 148 LEFT SIDE FUSELAGE SUB FLOOR FRAME ATTACH ANGLE CORRODED. REMOVED CORROSION, FABRICATED REPAIR ANGLE, AND INSTALLED PER EO DRAWING NR 99-009 AND 8110-3 DATED 01/12/99. (M)SDR ABXA9900038Latch · out of adjustDURING POSTFLIGHT CHECK, CABIN DOOR LOCK WAS STUCK IN LOCKED POSITION. FOUND OUTER LATCH ASSEMBLY MISADJUSTED 180 DEGREES. READJUSTED LATCH TO PROPER POSITION, OPS CHECKED GOOD.SDR ABXA9900039Latch · out of adjustDURING POSTFLIGHT, FOUND COCKPIT DOOR KNOB STUCK. ADJUSTED AND LUBRICATED INTERNAL MECHANISM IAW DC8 SRM.SDR ABXA9900023Controls · fodDURING DESCENT, AIRCRAFT WOULD NOT TURN TO THE LEFT. PILOT REPORTED FEELING SOMETHING 'SNAP'. AFTERWARDS, AIRCRAFT WAS VERY SLUGGISH TURNING TO THE LEFT. TURNED OK TO RIGHT. CREW DECLARED EMERGENCY, LANDING WAS UNEVENTFUL. *S/D* VISUALLY INSPECTED LEFT ASDR RRXA99004Rod End · failedUPON LANDING GEAR EXTENSION THE RIGHT MAIN LANDING GEAR FREE FELL INTO THE DOWN AND LOCKED POSITION. AFTER LANDING THE GEAR WAS PINNED AS A PRECAUTION, TAXIED TO RAMP. ACFT FERRIED TO KMCN FOR REMOVAL AND REPLACEMENT OF RT MLG BOSS PIN IAW DC-8 SB 32-102 PG SDR ARWA990107Uplock · lack of lubeMIA - FLT 1628 - AFTER TAKEOF IN SEGU, GEAR NOT LATCHED LIGHT ILLUMINATED, RECYCLED GEAR SEVERAL TIMES. COULD NOT GET SATISFACTORY UPLATCH CHECK, DOOR NOT LATCHED, LIGHT DID NOT ILLUMINATE, PROCEEDED TO DESTINATION IN ACCORDANCE OF ABNORMAL CHECKLIST. CHECKESDR ARWA990106Engine · leakingMIA - FLT 1628 - FL310, OIL QTY NR 1 ENGINE DROPPED TO .5 GALLON, OK OIL AND SUBSEQUENT ENGINE DAMAGE. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN AS EPR ABNORMAL CHECKLIST. AFTER SHUTDOWN, N1 25 PERCENT, N2 40 PERCENT, OIL PRESS 21 PSI. REMOVED OIL SCREEN AND SDR ARWA990105Bolt · wornMIA - FLT 9627 - ON PRE-FLIGHT, FOUND RT AILERON INBD TO OTBD SECTION 2 INCH SPLIT. TROUBLESHOT, FOUND EYE BOLT ATTACHING INBD/OTBD AILERON LOOSE AND WORN. REPLACED SAME IAW 211-11-02. OPERATIONAL PER MM 27-11-02. (X)SDR 99T64R034Skin · corrodedLEFT HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS EXFOLIATED CORROSION AROUND ATTACH SCREW HOLES. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED PER EO DRAWING NR 98-047 ON 8110-3 DATED 11/16/98 UNDER WOR 1308. (M)SDR 99T64R033Skin · corrodedRIGHT WING LEADING EDGE SECTION BETWEEN 3 AND 4 PYLONS CORROSION AT FASTENER ATTACH HOLES CENTER OF LEADING EDGE UPPER SURFACE. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-037 ON 8110-3 DATED 11/12/98 UNDER WO 1347. (M)SDR 99T64R032Skin · corrodedRIGHT WING LEADING EDGE 2ND SECTION OUTBOARD NR 4 PYLON CORROSION AT FASTENER ATTACH HOLES UPPER SURFACE. REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED PER EO DRAWING NR 98-054 ON 8110-3 DATED 11/23/98 UNDER WO 1347. (M)SDR 99T64R031Skin · corrodedLEFT WING OUTBOARD END AT LEADING EDGE CORROSION ATTACH HOLE AND FOUND CRACK SAME AREA. REMOVED CORROSION PER SRM 51-1-8 AND INSTALLED DOUBLER PER SRM 57-2-1. (M)SDR 99T64R030Frame · crackedFOUND A 4.5 INCH CRACK IN FUSELAGE FRAME STATION 759 BETWEEN RL 17 AND 18. STOP DRILL CRACK, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-055 ON 8110-3 DATED 12/03/98 UNDER WO NR 1347. (M)SDR 99T64R029Skin · corrodedLEFT WING FIRST LEADING EDGE SECTION OUTBOARD NR 1 PYLON HAS CORROSION AT FASTENER HOLES MOST INBOARD AFT XFS 578.750. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-035 ON 8110-3 DATED 11/09/98 UNDER WO 1347. (M)SDR 99T64R028Skin · corrodedFOUND CORROSION AT SCREW HOLES NR 4 STUBWING UPPER SURFACE. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-049 ON 8110-3 DATED 11/17/98 UNDER WO 1347. (M)SDR 99T64R027Fitting · corrodedW/W RIGHT VERTICAL FITTING FROM LONGERON 24 TO FLOORBEAM AT 879 IS CORRODED. REPLACED FITTING PER 51-1-20 AND EO DRAWING NR 98-032 ON 8110-3 DATED 11/01/98 UNDER WO 1300. (M)SDR 99T64R026Skin · corrodedRIGHT WING LEADING EDGE HAS CORROSION ON BOTTOM SKIN TRAILING EDGE AT WING STATION XFS 341.5. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-038 ON 8110-3 DATED 11/12/98 UNDER WO 1310. (M)SDR 99T64R025Skin · corrodedRIGHT WING LEADING EDGE HAS CORROSION ON BOTTOM SKIN TRAILING EDGE APPROX WING STATION XFS 422.750. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-038 ON 8110-3 DATED 11/12/98 UNDER WO 1310. (M)SDR 99T64R024Skin · corrodedNR 3 STUBWING FORWARD AND INBOARD SLOT WS XS 213 CORROSION REMOVAL BEYOND LIMITS. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-031 ON 8110-3 DATED 10/31/98 UNDER WO 1309. (M)SDR 99T64R023Skin · corrodedNR 3 STUBWING INBOARD TOP TRAILING EDGE STATION XS 220.190 CORROSION BEYOND LIMITS. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-030 ON 8110-3 DATED 10/30/98 UNDER WO 1309. (M)SDR 99T64R022Longeron · crackedAFT ACCESSORY COMPARTMENT RIGHT LONERON 24 AT STATION 1400 HAS .875 INCH CRACK IN RADIUS. FABRICATED REPAIR CHANNEL AND INSTALLED PER EO DRAWING NR 98-024 ON 8110-3 DATED 10/22/98 UNDER WO 1310. (M)SDR 99T64R021Skin · corrodedLEFT WING LEADING EDGE CORRODED AT FASTENER HOLE AFT OF INBOARD SLOT DOOR APPROX WS 250. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-029 ON 8110-3 DATED 10/30/98 UNDER WO 1309. (M)SDR 99T64R020Skin · corrodedRIGHT WING LEADING EDGE UPPER SURFACE PANEL HAS .5 INCH CRACK BEHIND NR 3 SLOT AND SMALL BULGE XFS 240.126. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-030 ON 8110-3 DATED 10/30/98 UNDER WO 1310. (M)SDR 99T64R019Skin · corrodedLEFT WING LEADING EDGE CORROSION AT SCREW OUTBOARD NR 2 PYLON APPROX WS 250 TOP OF WING XFS 335.25. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-039 ON 8110-3, DATED 11/12/98 UNDER WO NR 1310. (M)SDR 99T64R018Skin · corrodedLEFT WING CORROSION AT SEAM OF LEADING EDGE AFT NR 2 PYLON WS 260 TOP OF WING BETWEEN XFS 291.5 AND 304. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-040 ON 8110-3 DATED 11/18/98 UNDER WO 1310. (M)SDR 99T64R017Skin · corrodedLEFT WING LEADING EDGE PANEL AF TNR 1 PYLON SURFACE CORROSION WS 560 TOP OF WING. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-028 ON 8110-3 DATED 10/30/98 UNDER W/O 1310. (M)SDR 99T64R016Skin · corrodedFOUND LEFT WING LEADING EDGE PANEL OUTBOARD NR 1 PYLON WS 580 TOP OF WING SURFACE CORROSION XFS 641.250. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-035 ON 8110-3 DATED 11/09/98 UNDER WO NR 1309. (M)SDR 99T64R015Skin · corrodedFOUND LEFT WING OUTBOARD LEADING EDGE PANEL RUSTY FASTENERS WS 710-880 TOP OF WING. FOUND CORROSION IN SCREW HOLES, REMOVED CORROSION. FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-027 ON 8110-3 DATED 10/29/98 UNDER WO NR 1309. (M)SDR 99T64R014Fitting · corrodedRIGHT W/W LONGERON FITTING STATION 920 CORRODED ABOVE LANDING GEAR UPLOCK CYLINDER. REMOVED CORRODED FITTING AND REPLACED WITH NEW FITTING PER SRM 57-3-2 AND SRM 51-1-20 UNDER WO NR 1310. (M)SDR 99T64R013Skin · corrodedSKIN BULGED RIGHT WING CENTER SECTION UPPER SURFACE INBOARD OF OUTBOARD SLOT XFS 520 .168. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-037 ON 8110-3 DATED 11/12/98 UNDER WO 1309. (M)SDR 99T64R012Nut Plate · missingMISSING FASTENERS RIGHT WING LEADING EDGE. OPENED HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-058 ON 8110-3 DATED 12/13/98 UNDER WO NR 1308. (M)SDR 99T64R011Nut Plate · missingMISSING FASTENERS LEFT WING LEADING EDGE SECTION. OPEN HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-057 ON 8110-3 DATED 12/13/98 UNDER WO 1308. (M)SDR 99T64R010Skin · corrodedLEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS EXFOLIATED CORROSION AT BOTTOM ATTACH SCREW HOLES. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-046 ON 8110-3 DATED 11/17/98 UNDER WO 1308. (M)SDR 99T64R009Longeron · damagedFOUND STATION 400-420 STRINGER 19R LOWER FLANGE REMOVED. INSTALLED REPAIR CHANNEL PER EO DRAWING NR 98-056 ON 8110-3 DATED 12/04/98 UNDER WO 1347. (M)SDR 99T64R008Angle · corrodedCENTER FUEL TANK TOP SIDE AT STATION 857 UNDER NR 4 FLOOR PANEL SURFACE CORROSION AFT TANK ANGLE. REMOVED CORROSION, FLAP PEEN BLENDED AREA PROTECT REWORKED AREA PER EO DRAWING NR 98-025 ON 8110-3 DATED 10/27/98 WO 1308. (M)SDR 99T64R007Skin · corrodedLEFT HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS EXFOLIATED CORROSION AT TOP ATTACH SCREW HOLES. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-045 ON 8110-3 DATED 11/16/98 WO NR 1308. (M)SDR 99T64R006Skin · corrodedRIGHT HORIZ STABILIZER OUTBOARD LEADING EDGE EXFOLIATED CORROSION TOP ATTACH SCREW HOLES. REMOVED CORROSION FABRICATED DOUBLERS AND INSTALLED PER EO NR 98-044 ON 8110-3 DATED 11/23/98 UNDER WO NR 1308. (M)SDR 99T64R005Skin · corrodedRIGHT WING LEADING EDGE FROM XRS 697 TO XRS 885 HAS SCREW HEADS WORKING DUE TO EXFOLIATED CORROSION UPPER SURFACE. REMOVED CORROSION FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-054 ON 8110-3 DATED 11/23/98 UNDER WO NR 1308. (M)SDR 99T64R004Nut Plate · loose/missingNR 2 PYLON REMOVEABLE PLANK HAS ONE NUT PLATE MISSING AND ONE NUT PLATE LOOSE. OPENED HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-026 ON 8110-3 DATED 10/27/98 UNDER WO NR 1308. (M)
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