Douglas DC-8-73F
Service difficulty reports · 15,471
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 = 'DC873F' 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 = 'DC873F' 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 DHL2003604754Skin · damagedRT WING EXTENDED L/E OTBD VANE HAS SEVERAL ELONGATED HOLES AND INTERIM REPAIR AT STA XOLDI 67.000. REMOVED FASTENERS, REMOVED EXISTING INTERIM REPAIR. TRIMMED OUT ELONGATED HOLES SKIN AREA. PERFORMED EDDY CURRENT INSPECTION. CLEANED, TREATED AND PRIMED ARESDR DHL2003604703Fitting · crackedAFT ACCESSORY COMPT FITTING AT STA 660.000 WITH 7.000 CRACK IN IT BETWEEN L-35R AND L-36. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21, SRM 51-3-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IASDR DHL2003604706Skin · corrodedLT OUTER WING OTBD L/E SHOWS CORROSION AT STA XW 761.000. REMOVED FASTENERS, REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED OUT THE DAMAGED SKIN AREA IAW EODHL-030547, ED-3313. PERFORMED NDT INSPECTION, CLEASDR DHL2003604760Clip · crackedAFT ACCESSORY COMPT. CLIP ATTACHING FRAME TO SKIN AT STA. 660.000 L-22L WITH 1.500 CRACK IN IT. REMOVED CRACKED CLIP IAW SRM 51-1-20D PG.21. FABRICATED NEW CLIP (STEEL 0.500 H0.050) IAW SRM 53-1-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALSDR DHL2003604759Stringer Clip · crackedAFT ACCESSORY COMPT. CLIP ATTACHING FRAME TO SKIN AT STA.660.000 L-22R WITH 2.000 CRACK IN IT. REMOVED CRACKED CLIP IAW SRM 51-1-20D PG.21. FABRICATED NEW CLIP (STEEL 301 0.500 H0.050) IAW SRM 53-1-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTSDR DHL2003604755Skin · damagedLT WING EXTENDED L/E INBD. VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA. XS.247.000. PERFORMED MAJOR REPAIR IAW EODHL-030563, ED-3312. REMOVED FASTENERS AND EXISTING DOUBLER IAW SRM 51-1-21 PG.1. TRIMMED OUT DAMAGED AREA IAW EODHL-030563, ED-3312. PESDR DHL2003604570Track · brokenD-BELLY DOOR FWD TRACK BROKEN, STA 1400.000. REMOVED BROKEN TRACK IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK IAW SRM 51-1-21 PG 1. SEE N/R 0530 FOR OPS CK.SDR DHL2003604594Skin · corrodedLT OUTER WING OB L\E SHOWS CORROSION AT STA. XW.761.000. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED CORROSION ON LT OUTER WING OB. L\E IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS. TRIMMED OUT THE DAMAGED SKIN AREA IAW EODHL-030547, ED-3313. CLEANED, TRESDR DHL2003604604Vane · damagedRT WING EXTENDED LE OB VANE HAS SEVERAL ELONGATED HOLES AND INTERIM REPAIR AT STA XOLDO 67. REMOVED FASTENERS. REMOVED THE EXISTING INTERIM REPAIR IAW EO DHL 030558, ED-3351. CLEANED TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED AN EXTERNAL REPAIR DOUBSDR DHL2003604599Vane · damagedLT WING EXTENDED L/E INBD VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA XS.247.000. PERFORMED MAJOR REPAIR IAW EODHL-030563, ED-3312. REMOVED FASTENERS AND THE EXSISTING DOUBLER IAW SRM 51-1-21 PG 1. TRIMMED OUT THE ELONGATED HOLES SKIN AREA. CLEANED, SDR DHL2003604562Frame · crackedVERTICAL STAB L/E FORMER INNER SECTION CRACKED 0.500 AT STA ZFS 104.750 LT SIDE. STOP DRILLED CRACK AT ZFS 104.750 AND FABRICATED REINFORCEMENT IAW SRM 55-2-0 FIG 2. CLEANED, TREATED AND PRIMED AREA AND REINFORCEMENT IAW SRM 51-1-8B. INSTALLED REINFORCEMENT IASDR DHL2003604548Panel · delaminatedLT WING T/E UPPER PANEL EXTERNAL SKIN DELAMINATED AT XRS 436.000. REMOVED AND REPLACED UPPER PANEL ON LT WING T/E AT XRS 436.000 IAW SRM 51-3-0 PG 1.SDR DHL2003604578Seat Track · damagedNAVIGATOR FWD SEAT TRACK WITH ELONGATED HOLES. REMOVED NAVIGATOR FWD. SEAT TRACK WITH ELONGATED HOLES IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW NAVIGATOR FWD. SEAT TRACK IAW SRM 51-3-0 PG.1SDR DHL2003604723Skin · corrodedRT INNER WING UPPER SKIN CORRODED AROUND STA XRS 184.000 BETWEEN CTR SPAR AND S-9R. REMOVED FASTENERS, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENDED OUT DAMAGED SKIN AREA IAW EODHL-030534, ED-3356. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-SDR DHL2003604775Skin · corrodedUPPER EXTERNAL FUSE SKIN CORRODED AT STA 1050.000 BETWEEN L-2R - L-2L. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. PERFORMED EDDY CURRENT INSPECTION IAW DC8 NDT SPM PART 06-10SDR DHL2003604595Skin · corrodedRT INNER WING UPPER SKIN CORRODED AROUND STA XRS 184.000 BETWEEN CTR SPAR AND S-9R (MAJOR REPAIR). REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENDED OUT DAMAGED SKIN AREA IAWSDR DHL2003604598Skin · corrodedLT OUTER WING OTBD EXTENDED L/E OUTER PLATING LOWER SURFACE CORRODED AROUND STA XFS 710.000. REMOVED FASTENERS, REMOVED CORROSION, FOUND OUT OF LIMITS. TRIMMED OUT DAMAGED SKIN AREA. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREASDR DHL2003604602Skin · damagedLT WING EXTENDED L/E OTBD. VANE SHOWS ELONGATED HOLES AND INTERIM REPAIR AT STA. XOLDI 67.000 PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. REMOVED EXISTING INTERIM REPAIR AND FILLER. TRIMMED OUT DAMAGED SKIN AREA IAW EODHL-030545, ED-3302. PSDR DHL2003604549Skin · damagedLT WING INBD FLAP UPPER PLATING SHOWS INTERIM REPAIR, XW 104.000 - XW 122.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-7-1 FIG 1. REMOVED UPPER PLATING WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1. FABRICATED NEW UPPER PLATING IAW SRM SDR DHL2003604568Angle · crackedLT HORIZ STAB INNER ANGLE CRACKED 1.000 AT XFS.30.500. REMOVED CRACKED ANGLE IAW SRM 51-1-21 PG 1. FABRICATED NEW ANGLE IAW SRM 55-1-0 PG 1. PERFORMED HEAT TREATMENT TO NEW ANGLE IAW SRM 51-1-1 PG 11,13. CLEANED, TREATED AND PRIMED AREA AND NEW ANGLE IAW SRM SDR DHL2003873009Lamp · inoperativeEMERGENCY EXIT LIGHT DISARM LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT DISARM LIGHT IAW M/M 33-10-1, OPS CHECKED NORMAL.SDR DHL2003604718Skin · crackedLT OUTER WING INBD L/E LOWER PLATING CRACKED 1.000, AROUND STA XFS 597.500. PERFORMED MAJOR REPAIR IAW EODHL-030527, ED-3290. REMOVED FASTENERS, PERFORMED STOP HOLE ON CRACK END USING 0.250 DIA DRILL IAW EODHL-030527, ED-3290. PERFORMED NDT INSPECTION IAW DSDR DHL2003604601Skin · corrodedRT. WING OB L/E UPPER SKIN CORRODED STA. XFS.710.000 PERFORMED MAJOR REPAIR IAW EODHL-030517, ED-3306. REMOVED FASTENERS AND EXISTING DOUBLER AND FILLER IAW SRM 51-1-21 PG.1. REMOVED CORROSION IAW SRM. FOUND OUT OF LIMITS. TRIMMED OUT THE CORRODED SKIN AREA. SDR DHL2003604629Vane · elongatedLT WING CTR L/E VANE SLOT HOLES ELONGATED AT XOLDI 6.224. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. TRIMMED OUT THE ELONGATED HOLES SKIN AREA. CLEANED, TREATED AND PRIMED AREA. FABRICATED A REPAIR EXTERNAL DOUBLER (7075-T6 AL0.071), A FILSDR DHL2003604581Floor Panel · corrodedMAIN CARGO COMPT, CORROSION ON FLOOR PANEL SKIN STA 1160.000 TRACK NR 6. REMOVED CORROSION IAW SRM 51-1-8 PG 17,18 FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED DOUBLER IAW SRM 53-2-3 FIG 10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B.SDR DHL2003604731Frame · damagedMAIN CARGO COMPT FRAME SHOWS INTERIM REPAIR AT STA 1580.000, L-21R TO L-19R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110, SRM 51-1-1, DPS 7.00-01. TRIMMED OUT DAMAGED FRAME AND FABRICATED NEW FRAME SEGMENT AND SPLICE ANGLES 2 EA WITH IASDR DHL2003604779Frame · crackedMAIN CARGO COMPT FRAME FLANGE WITH 2.000 CRACK, STA 1580.000, L-21L - L-20L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110, SRM 51-1-1. TRIMMED OUT DAMAGED FRAME AND FABRICATED NEW FRAME SEGMENT AND SPLICE ANGLES (02 EA) IASDR DHL2003604656Plate · corrodedRT OUTER WING OUTBD L/E UPPER PLATING CORRODED AT STA XW 761.000. PERFORMED MAJOR REPAIR IAW EODHL-030529, ED-3305. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. TRIMMED ANDSDR DHL2003604749Skin · damagedLT OUTER WING CTR. EXTENDED L/E SLOT HAS ELONGATED HOLES AT STA. XFS.526.000. (MAJOR REPAIR) PERFORMED MAJOR REPAIR IAW EODHL-030550, ED-3353. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. BLENDED OUT THE ELONGATED HOLES SKIN AREA IAW EODHL-030550, ED-3353. PEFORMEDSDR IXXA0300036Connector · looseDURING CRUISE FROM TOL ENROUTE TO DFW NR 4 EGT ROSE ABNORMALLY, THEN DROPPED TO "0". AS A PRECAUTIONARY MEASURE FLIGHT CREW ELECTED TO SHUTDOWN NR 4 ENGINE. AN UNEVENTFUL LANDING WAS MADE IN DFW. UPON INSPECTION MAINTENANCE DISCOVERED LOOSE CONNECTOR ON HARNESSDR DHL2003604752Doubler · crackedRT OUTER WING CTR EXTENDED L/E SLOT INNER DOUBLER CRACKED (0.063) AT STA. XFS. 526.000. PERFORMED MAJOR REPAIR IAW EODHL-030532, ED-3350. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. STOP DRILLED ON CRACK END (0.250 DIA) IAW EODHL-030532, ED-3350. PERFORMED EDDY SDR DHL2003604647Skin · corrodedLT HORIZONTAL STAB. LE EXTERNAL SKIN SHOWS CORROSION ON SEVERAL SPOTS AT STA. XFS.178.750. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED CORROSION ON LT HORIZ. STAB. L/E EXTERNAL SKIN IAW SRM 51-1-8 PG.17-18. FOUND OUT OF LIMITS IAW SRM 55-2-1 FIG.3. TSDR DHL2003604689Skin · crackedRT OUTER WING INBD EXTENDED L/E LOWER PLATING CRACKED 1.650 AROUND STA XFS 597.500. REMOVED FASTENERS IAW SRM 51-1-21 PG 21. PERFORMED STOP HOLE ON CRACK END USING 0.250 DIA DRILL IAW EODHL-030520, ED-3352. PERFORMED EDDY CURRENT INSPECTION IAW NDT SPM PARTSDR DHL2003604606Doubler · crackedRT OUTER WING CTR EXTENDED L/E SLOT INNER DOUBLER CRACKED 0.630 AT STA XFS 526.000. PERFORMED MAJOR REPAIR IAW EODHL-030532, ED-3350. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED THE CRACK END 0.250 DIA IAW EODHL-030532, ED-3350. CLEANED, TREATED ASDR DHL2003604553Skin · damagedINTERIM REPAIR ON TOP SURFACE OF LT WING L/E (STA XS 246.518-250.089) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38, TR NR 57-85. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1SDR DHL2003604560Frame · crackedRT WING CENTER L/E FRAME CRACKED 1.000, XFS.366.500 (UPPER INNER). STOP DRILLED CRACK AT XFS.366.500 AND FABRICATED ANGLE DOUBLER (2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBSDR DHL2003807008Position Switch · malfunctionedAT FL 370 BELLY DOOR OPEN LIGHT ILLUMINATED AIRPLANE WAS PRESSURIZING NORMALLY RAN ABNORMAL PROCEDURE DESCENDED TO FL 290. REMOVED AND REPLACED A PIT DOOR POSITION SWITCH PER M/M 52-31-1, OPS CHECKED GOOD.SDR DHL2003604545Intercostal · crackedFWD CARGO COMPT PRESSURE BULKHEAD INTERCOSTAL 1.000 AT L-31L, STA 70.000. STOP DRILLED CRACK AT L-31L, STA 70.000 AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21 PG 1.SDR DHL2003604554Skin · crackedLT WING OUTBOARD L/E UPPER SKIN CRACKED 1.500 AT XFS.207.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38, TR 57-85. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. CUT OUT DAMAGED AREA AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 38, TR 57-SDR DHL2003604546Frame · crackedRT OUTBD STUB WING FORMER AT STA XS. 512.000 WITH 1.000 CRACK IN IT. STOP DRILLED CRACK AND FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D PG 9, SSDR UPS03840743Seat Track · crackedINSPECTION TYPE: C-2, AFT PIT FS 1127 AT RBL 49 LOWER FLANGE OF SEAT TRACK IS CRACKED. REMOVED DAMAGED SEAT TRACK. REC'D NEW SEAT TRACK, DRILLED IAW DC8 SRM 51-1-24. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0.SDR DHL2003807007Line · leakingAFTER T/O UPON GEAR RETRACTION HYD SYS PX WENT TO ZERO , HYD QTY WENT TO HALF FULL. AILERON CONTROL MANUAL LIGHT ILLUMINATED. COMPLETED HYD PX ABNORMAL. ABNORM PROCEDURE, PX DID NOT INCREASE HYD QTY DECREASED TO AUX LEVEL. COMPLETED HYD QTY LOSS ABNORMAL PROCESDR DHL2003604596Skin · crackedUPPER FUSELAGE EXTERIOR SKIN WITH 1.000 CRACK AT STA. 1745.000, L-16R - L-17R. CORR.: PERFORMED MAJOR REPAIR IAW SRM 53-2-1 PG.99-100. TRIMMED OUT DAMAGED AREA IAW SRM 53-2-1 PG.99-100. FABRICATED FILLER (7075-T6 0.063) AND INTERNAL DOUBLER (7075-T6 0.040) ANDSDR DHL2003604686Door Frame · crackedAFT LOWER CORNER OF AFT PASSENGER DOOR JAMB WITH 1.000 CRACK IN IT. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 18 SHEET 1, TR 53-134, TR 53-135, DWG 5750776, DWG SR08530021. CUT OUT DAMAGED AREA AND FABRICATED FILLER (7075-T6 AL0.080) AND (2) DOUBLERS (7075-TSDR DHL2003604558Frame · crackedRT. HORIZONTAL STABILIZER L/E INNER FRAME CRACKED 0.500 AT XFS. 47.500. (INNER PART). REMOVED FASTENERS IAW SRM 51-1-21 PG.1. STOP DRILLED CRACK AT XFS.47.500 AND FABRICATED ANGLE DOUBLER (2024-T3 0.032) IAW SRM 55-2-0 PG.7,8. CLEANED, TREATED AND PRIMED AREA SDR DHL2003805009Lamp · burned outNR 4 SMOKE DETECTOR WILL NOT TEST. RE-LAMPED NR 4 SMOKE DETECTOR OPS CHECKED GOOD AS PER M/M 26-10-5.SDR DHL2003604728Splice · crackedMAIN CARGO COMPT AFT SPLICE FITTING WITH 1.000 CRACK IN IT (STA 1690.000 A 1700.000, L-30L). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 51-1-20D PG 9, 21. REMOVED CRACKED SPLICE FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 5SDR DHL2003604743Skin · dentedLWR FUSELAGE SKIN WITH TWO DENTS BETWEEN STA 25.000 AND 45.000, L-24L - L-25L. PERFORMED MAJOR REPAIR IAW EODHL-030513, ED-3285. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. BLENDED OUT DAMAGED AREA IAW EODHL-030513, ED-3285. PERFORMED EDDY CURRENT INSPECTION ISDR DHL2003604563Flap · dentedRT WING OB FLAP T/E DENTED FROM STA XF 304.000 - XF 310.000. REMOVED DAMAGED T/E IAW SRM 51-1-21A PG. 4, FABRICATED NEW T/E IAW SRM 57-1-0 PG 7,SRM 57-7-1 FIG 4. CLEANED, TREATED AND PRIMED AREA AND T/E LOWER SURFACE IAW SRM 51-1-8B. INSTALLED NEW T/E IAW SRM SDR UPS03840745Cap · crackedINSPECTION TYPE:C-2 LT HORIZ STAB INBOARD LOWER CAP CRACKED. REMOVED LT HORIZ L/E CAP, PERFORMED HEFC IAW NDT SPM 06-10-001.01. LOCATED & DRILLED IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21/51-1-20D.
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