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 95ZZZM419Skin · damagedON C-CHECK FOUND, 9 INCHES BY 9.5 INCHES TEMP REPAIR AT FS 1300 L26R, UPPER AFT CORNER OF 'D' BELLY DOOR CUTOUT. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED DOUBLERS IAW DAC DWG SR 08530019. (M)SDR IXXA199559Csd · failedON DEPARTURE OUT OF NZAA, THE NR 3 CSD OIL LIGHT ILLUMINATED ACCOMPANIED BY LOSS OF VOLTAGE AND FREQUENCY. THE AIRCRAFT RETURNED TO NZAA FOR MAINTENANCE. MAINTENANCE DEFERRED THE NR 3 CSD. THE AIRCRAFT RETURNED TO SERVICE, AND THE NR 3 CSD WAS SCHEDULED FORSDR 95ZZZW709Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT LEFT WING LEADING EDGE LOWER SURFACE AT XFS 207.159. CORROSION FOUND IS BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER OF CLAD 7075-T6 .071 AND INSTALLED PER DER EO ARW 950037. FOUND LEVEL II CORROSSDR 95ZZZW708Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT LEFT WING LEADING EDGE LOWER SURFACE AT XFS 207.159. CORROSION FOUND IS BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER OF CLAD 7075-T6 .071 AND INSTALLED PER DER EO ARW 950037. FOUND LEVEL II CORROSSDR 95ZZZW703Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT LEFT WING LEADING EDGE LOWER SURFACE AT XFS 207.159. CORROSION FOUND IS BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER OF CLAD 7075-T6 .071 AND INSTALLED PER DER EO ARW 950037. FOUND LEVEL II CORROSSDR 95ZZZW702Skin · corrodedDURING PREFLIGHT FOUND EVIDENCE OF CORROSION AT LEFT WING LEADING EDGE LOWER SURFACE AT XFS 207.159. CORROSION FOUND IS BEYOND LIMITS. CUT OUT DAMAGED AREA. FABRICATED DOUBLER OF CLAD 7075-T6 .071 AND INSTALLED PER DER EO ARW 950037. FOUND LEVEL II CORROSISDR 95ZZZW707Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT RT LEADING EDGE AT XFS 291.500 TO 329. FOUND CORROSION BEYOND LIMIT. CUT OUT DAMAGED AREA. FABRICATED FILLER DOUBLER USING CLAD 7075-T6. PICKED UP EXISTING ATTACHMENTS WHERE POSSIBLE. ALL WORK DONE PER EO ARSDR 95ZZZW706Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT RIGHT LEADING EDGE AT XFS 291.500 TO 329.00. FOUND CORROSION BEYOND LIMIT. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER USING CLAD 7075-T6. PICKED UP EXISTING ATTACHMENTS WHERE POSSIBLE. ALL WORK DONSDR 95ZZZW705Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT RIGHT LEADING EDGE XFS 182.500. CORROSION FOUND IS BEYOND LIMIT. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER USING CLAD 7075-T6.071. PICKED UP EXISTING ATTACHMENT WHERE POSSIBLE. ALL WORK DONE PER EO SDR 95ZZZW701Skin · corrodedDURING PREFLIGHT, FOUND EVIDENCE OF CORROSION AT RIGHT LEADING EDGE XFS 182.500. CORROSION FOUND IS BEYOND LIMIT. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND FILLER USING CLAD 7075-T6.071. PICKED UP EXISTING ATTACHMENT WHERE POSSIBLE. ALL WORK DONE PER EO SDR 95ZZZZ222Doubler · corrodedLEVEL 2 CORROSION, RT SIDE FLOOR LEVEL FINGER DOUBLERS ATTACHED TO FRAME AT FS 225 TO 235 HAVE CORROSION. REMOVED DAMAGED AREA, CLEANED AND TREATED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-01-0.SDR 95ZZZZ221Aileron · corrodedLEVEL 2 CORROSION, LT WING I/B AILERON O/B TAB HAS BULGING CORROSION AT FASTENERS AT I/B END LOWER SURFACE. REMOVED CORROSION AND TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 51-1-9.SDR 95ZZZZ220Skin · corrodedLEVEL 2 CORROSION, RT WING O/B AILERON LOWER SURFACE SKIN AT I/B END HAS CORROSION BULGING AROUND RIVETS. REMOVED CORROSION, TREATED AREA FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR ABXA9500245O-Ring · defectiveDURING APPROACH AFTER THE FLAPS WERE SELECTED TO 35 DEGREES, THE HYDRAULIC FLUID LEVEL IN THE MAIN RESERVOIR WENT TO STANDPIPE LEVEL. FOUND DEFECTIVE O-RING AT THE NR 3 ENGINE HYDRAULIC PUMP INLET ELBOW. REPLACED O-RING. SERVICED, LEAK, AND OPS CHECKED SYSTSDR MGMA950158Engine · failedPRIOR TO SETTING THE EPR BEFORE 80 KTS HEARD A LOUD BANG AND NR 1 ENGINE INDICATIONS READS AS FOLLOWS, EGT EQUALS 600, N2 EQUALS 0, FF EQUALS 0, N1 EQUALS 0, OIL PRESSURE EQUALS 0 AND OIL TEMP EQUALS 75, AND OIL QUANTITY READ 5.0 GALLONS. WE WERE ADVISED OF BASDR MGMA950148Switch · failedNR 3 ENGINE OIL PRESSURE LIGHT CAME ON WITH OIL PRESSURE TEMPERATURE NORMAL. ABNORMAL CHECKLIST PERFORMED, LIGHT STILL STAYED ON. DURING APPROACH INTO EWR, LIGHT WENT OFF. CLEANED OIL FILTER AND REMOVED AND REPLACED DIFFERENTIAL OIL PRESSURE SWITCH. RAN ENSDR MGMA950138Engine · stalledREJECTED TAKEOFF IN YIP DUE TO NR 1 ENGINE STALL. RAN UP ENGINE WITH NO OTHER INDICATIONS. TAKEOFF THEN NORMAL. INSPECTED INLET AND TAILPIPE ON NR 1 ENGINE. CHECKED BLEED VALVE SCHEDULING. ALL INDICATIONS NORMAL. TOTAL TIME: 43248.1 HOURS. TOTAL CYCLESSDR BUFA9507Hyd Line · leakingON CLIMB, LOST HYDRAULIC FLUID. FOUND LOOSE HYDRAULIC SLOT LEADING EDGE LINE IN NR 2 ENGINE PYLON. TIGHTENED AND LEAKED CHECKED SAME IAW DC8-MM 29-01. ACFT RETURNED TO SERVICE. (W)SDR 95ZZZW571Support · corrodedLEVEL 2 CORROSION, AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1574L AND BS 1540L 7 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. (W)SDR 95ZZZW570Longeron · corrodedLEVEL 2 CORROSION, LONGERON 30 LEFT IS CORRODED BETWEEN BS 1606 AND BS 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)SDR 95ZZZW569Skin · corrodedLEVEL 2 CORROSION, CORROSION BULGING OUT THROUGH FUSELAGE SKIN SURFACE AT AFT RIGHT SIDE OF FUSELAGE BS 1557R BETWEEN LONGERON 28R AND 26R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1. (W)SDR 95ZZZW568Support · corrodedLEVEL 2 CORROSION, AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1574L AND BS 1540L 12 INCHES LBL. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0. (W)SDR 95ZZZW535Skin · corrodedLEVEL 2 CORROSION, LEFT HORIZONTAL STABILIZER LOWER SURFACE SKI AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-1-2. (W)SDR 95ZZZW534Window Frame · corrodedLEVEL 2 CORROSION, WINDOW NR 23R HAS CORROSION INSIDE FRAME. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER RICH EO 9402289.SDR 95ZZZW533Skin · corrodedLEVEL 2 CORROSION, RT HORIZONTAL STAB UPPER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 55-3-0. (W)SDR 95ZZZW532Skin · corrodedLEVEL 2 CORROSION, FUSELAGE RT SIDE EXTERIOR SKIN FRAMES 670 TO FS 685 HAS SKIN CRACK AND BULGING AROUND FASTENER HEADS LGRN 21R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER RICH DWG RCH D85330-5018. (W)SDR 95ZZZW531Skin · corrodedLEVEL 2 CORROSION, RT HORIZONTAL STABILIZER LOWER SURFACE SKIN AT REAR SPAR CAP HAS BULGING CORROSION AROUND RIVETS FROM INBOARD END TO TIP. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 51-1-1. (W)SDR 95ZZZW530Spar Cap · corrodedLEVEL 2 CORROSION RT WING LEADING EDGE UPPER AT FRONT SPAR CAP ATTACH FLANGE HAS CORROSION AROUND SCREW HEADS OUTBOARD OF NR 4 PYLON FROM APPROXIMATELY XFS 503 TO XFS 710. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1.SDR 95ZZZW548Skin · corrodedLEVEL 2 CORROSION, AFT CABIN FUSELAGE SKIN IS CORRODED BETWEEN BS 1586L AND 1574, LONGERON 26L AND LONGERON 24L. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1.SDR 95ZZZW567Longeron · corrodedLEVEL 2 CORROSION, AFT FUSELAGE LONGERON 24R BETWEEN FS 1500 AND 1480 HAS SURFACE CORROSION AND BULGES. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)SDR 95ZZZW566Skin · corrodedLEVEL 2 CORROSION, FUSELAGE LOWER LOBE SKIN IS CORRODED AT CENTER PRESSURE BULKHEAD VERTICAL SUPPORT 4 INCHES LBL BETWEEN BS 1606 AND 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)SDR 95ZZZW565Window Frame · corrodedLEVEL 2 CORROSION, AFT FUSELAGE MAIN CABIN WINDOW FRAME FOR WINDOW 19R HAS CORROSION ON INSIDE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW RICH DRAWING 5164-6. (W)SDR 95ZZZW547Skin · corrodedLEVEL 2 CORROSION, AFT MAIN CABIN LOWER FUSELAGE SKIN IS CORRODED FROM BS 1530 TO BS 1606 LONGERON 35L TO 35R. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1.SDR 95ZZZW546Slot Door · corrodedLEVEL 2 CORROSION, LEFT WING NR 1 SLOT DOOR HAS DOUBLER REPAIR THAT IS SURROUNDED BY CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER DOUGLAS FILE NR 258324.SDR 95ZZZW545Flange · corrodedLEVEL 2 CORROSION, LEFT AUXILLARY TANK UPPER ATTACH FLANGE HAS INTERGRANULAR CORROSION. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1.SDR 95ZZZW544Support · corrodedLEVEL 2 CORROSION, AFT CABIN TRIANGLE FLOOR WEB SUPPORT IS CORRODED AT BS 1574 CENTER, CENTER LINE 12 INCHES LBL 12 INCHES RBL. REMOVED AND REPLACED TRIANGLE FLOOR WEB PER SRM 53-1-0.SDR 95ZZZW543Frame · corrodedLEVEL 2 CORROSION, AFT CABIN CIRCUMFERENTIAL FRAME IS CORRODED AT BS 1574L FROM LONGERON 24 TO 26L. REMOVED CORROSION AND REPLACED FRAME SECTION PER SRM 53-1-0.SDR 95ZZZW542Floor Beam · corrodedLEVEL 2 CORROSION, AFT CABIN FLOOR BEAM CAP AT BS 1540 IS CORRODED FROM 45 INCHES LBL TO 45 INCHES. REMOVED AND REPLACED FLOOR BEAM CAP PER SRM 53-1-0.SDR 95ZZZX2503Connector · dirtyDURING POST-FLIGHT, NR 2 ENGINE FIRE WARNING WOULD NOT TEST. FOUND NR 2 LOWER LOOP CONNECTOR OIL SOAKED, REMOVED AND CLEANED CONNECTOR, REINSTALLED, OPS CHECK GOOD IAW MM 26-10.SDR 95ZZZW212Slot Door · corrodedRT WING OUTBOARD SLOT DOOR HAS CORROSION LEVEL II AT L/E. REF N/R 1117 WO 950015.SDR 95ZZZW206Fire Loop · failedDURING POST FILGHT, NR 2 ENGINE FIRE WARNING TEST FOUND INOP. REMOVED AND REPLACED LOWER FIRE LOOP ASSY IAW MM 28-10. OPS CHECK GOOD.SDR 95ZZZW539Floor Beam · corrodedLEVEL 2 CORROSION, ENTIRE FLOOR BEAM CAP AT BS 1586 IS CORRODED FROM LEFT TO RIGHT SIDE OF CABIN. CLEANED CORROSION, FABRICATED, AND INSTALLED NEW FLOOR BEAM PER SRM 53-1-0.SDR 95ZZZW538Fitting · corrodedLEVEL 2 CORROSION, LONGERON 32 RIGHT END BATHTUB FITTING IS CORRODED AT PRESSURE BULKHEAD BS 1606R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZW537Fitting · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT BATHTUB FITTING IS CORRODED AT BS 1530R, LONGERON 30R. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZW536Skin · corrodedLEVEL 2 CORROSION, FUSELAGE SKIN CORRODED BETWEEN BS 1530 AND BS 1540 BETWEEN LONGERON 36 AND LONGERON 34 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)SDR 95ZZZZ153Support · corrodedLEVEL 2 CORROSION/AFT CABIN FLOOR PANEL SUPPORT IS CORRODED BETWEEN BS 1606 AND BS 1585, 9 INCHES LBL. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZZ152Longeron · corrodedLEVEL 2 CORROSION/LONGERON 26 LEFT END FITTING IS CORRODED AT BS 1530 LEFT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZZ151Support · corrodedLEVEL 2 CORROSION/AFT CABIN FLOOR SUPPORT IS CORRODED BETWEEN BS 1480L AND BS 1520L, 15 INCHES LBL. CLEANED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZZ150Fitting · corrodedLEVEL 2 CORROSION/LONGERON 30 RIGHT END FITTING IS CORRODED AT BS 1530 RIGHT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.SDR 95ZZZZ149Support · corrodedLEVEL 2 CORROSION/AFT CABIN FLOOR PANEL SUPPORT IS CORRODED BETWEEN BS 1606 AND BS 1585, 22 INCHES RBL. REMOVED CORROSION AND FABRICATED AND INSTALLED REPAIR PER SRM 53-1-0.
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