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 DHL2001806520Floor Support · crackedC-CHECK - FWD. CARGO COMPARTMENT FLOOR PANEL SUPPORTING ANGLE CRACKED 3 INCHES, STA. 220.00 L-33 R.REMOVED DAMAGED AREA IAW SRM 53-2-0 PAGE 11. FABRICATED DOUBLER IAW SRM 53-2-0 PAGE 11. INSTALLED DOUBLER IAW SRM 53-2-0 PAGE 11. STATUS-CLOSED.SDR RRXA11040Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING CENTER LE UPPER SKIN AT STA XOLDI 6.225 TO XFS422.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSSDR RRXA11039Spar Cap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT STA XFS32.5-XFS142, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-SDR DHL2001806638Diffuser · crackedC-CHECK, LT WING L/E ANTI-ICE DIFFUSER 1 INCH CRACK AT LOWER PART STA AFS 766.500 - XFS 766.950.SDR DHL2001806600Fitting · crackedC-CHECK - RT REAR PRESSURE BULKHEAD TEE FITTING SHOWS CRACK OF 3 INCH WITH STOP DRILL. FABRICATED REINFORCEMENT ANGLE IAW SRM 51-1-8B FIG 1B. TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCEMENT ANGLE IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED.SDR DHL2001806581Diffuser · crackedC-CHECK - LT WING ANTI-ICE DIFFUSER UPPER PART HAS A 1 INCH CRACK AT STA XFS 728.720. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. SDR DHL2001806575Diffuser · crackedC-CHECK - LT WING L/E ANTI-ICE DIFFUSER HAS A 1/2 INCH CRACK AT LWR PART STA XFS 747.500. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806574Diffuser · crackedC-CHECK - LT WING L/E ANTI-ICE DIFFUSER 1 INCH CRACK AT LWR. PART STA XFS 728.750. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806570Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 860. PERFORMED STOP DRILL AND FABRICATED DOUBLERS IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806569Rib · crackedC-CHECK - LH WING L/E RIB UPPER PART 1/2 INCH CRACK AT STA XFS 822. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8, PAGES 12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806566Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1/2 INCH CRACK AT STA XFS 803.730. PERFORMED STOP HOLE AND FABRICATED DOUBLERS IAW SRM 57-2-0 PAGE 9, 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 PAGE 9/10. STATUS-CLOSEDSDR DHL2001806565Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LOWER PART 1-1/2 INCH CRACK AT STA XFS 728. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806564Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LOWER PART 1/2 INCH CRACK AT STA XFS 760-250. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806563Rib · crackedC-CHECK - LH WING L/E RIB UPPER PART 1 INCH CRACK AT STA XFS 766.500. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 PAGES 9. 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 PAGES 9, 10. STATUS-CLOSSDR DHL2001806562Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSERS 1-1/2 INCH CRACK AT UPPER PART STA XFS 745.950. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUSDR DHL2001806561Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER LWR PART 1/2 INCH CRACK AT STA XFS 766.250. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSDR DHL2001806557Diffuser · crackedC-CHECK - LT WING LE ANTI-ICE DIFFUSER, 1 INCH CRACK AT UPPER PART STA XFS 766.500 - XFS 766.950. PERFORMED STOP HOLE. AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-SDR DHL2001806555Rib · crackedC-CHECK - WING LE RIB UPPER PART 1 INCH CRACK AT STA 803.730. PERFORMED STOP HOLE AND FABRICATED DOUBLERS IAW SRM 57-2-0 P1, 9, 10. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLERS IAW SRM 57-2-0 PAGE 10. STATUS-CLOSEDSDR DHL2001806549Floor Support · crackedC-CHECKED - MAIN CARGO 2 INCH CRACK IN CENTRAL WING FLOOR D STA 866.00. CUT OUT DAMAGED AREA OF FLOOR PANEL D AT STA 866.00, FABRICATED FILLER & DOUBLER ANGLES IAW SRM 53-2-3 PAGE 39, 40. CLEANED, TREATED, & PRIMED IAW SRM 51-1-8B. INSTALLED FILLER & DOUBSDR DHL2001806545Angle · corrodedC-CHECK - AFT FUSELAGE EXTERIOR-UPPER PART VERTICAL STABILIZER TO FUSELAGE ANGLE SHOWS CORROSION, STA FS 000 RT SIDE.CORRECTIVE ACTION - REMOVED LEVEL I CORROSION FROM AFT FUSELAGE EXTERIOR UPPER PART VERTICAL STABILIZER TO FUSELAGE ANGLE STA FS 000 RH IAW SRMSDR DHL2001806503Fitting · crackedRT HORIZONTAL STABILIZER, LE INTERIOR LWR FITTING CRACKED 1 IN AT STA XFS 60.REMOVED CRACKED FITTING AT STA. XFS.60 OF RT HORIZONTAL STAB LE INTERIOR IAW SRM 51-1-20D PAGE 21. CLEANED, TREATED, & PRIMED AREA IAW SRM 51-1-8 PAGE 12-13. INSTALLED NEW FITTING ISDR RRXA010019Inu · failedNR 1 INS FAILED WENT ATT MODE. TRANSFERRED TO DMI LIST AS CONTROL D-9272201-1175 CAT: D MEL 3420 ATA 3410 DUE DATE 11JUL01 PLACARD INSTALLED. REMOVED AND REPLACED NR 1 INU PERFORMED OPERATIONAL CHECK IAW SUPPLEMENTAL MANUAL CHECK GOOD. THIS CLEARS DMI D9SDR DHL2001806603Skin · crackedC-CHECKED - LT WING L/E LWR SKIN SURFACE CRACKED 1/2 INCH AT STA XFS 585. CUT OUT DAMAGED AREA OF LT WING L/E LWR SKIN XFS 585 AND FABRICATED FILLER AND DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FILLER AND DOUBLESDR DHL2001806573Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART 1/2 INCH CRACK AT STA XFS 660. PERFORMED STOP DRILL AND FAVRICATE REINFORCING ANGLE IAW SRM 53-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806568Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 822.500. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806558Rib · crackedC-CHECK - LT WING LE RIB 1 INCH CRACK AT UPPER PART STA XFS 822.500. PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGES 1-12, 13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806547Floor Support · crackedC-CHECK - MAIN CARGO 1 INCH CRACK IN CENTRAL WING FLOOR ''D'' STA 878.000. CUT OUT DAMAGED AREA OF FLOOR PANEL ''D'' AT STA 878 FABRICATED FILLER AND DOUBLER IAW SRM 53-2-3 PAGE 39/40 CLEANED, TREATED & PRIMED IAW SRM 51-1-8B PAGE 1-12. INSTALLED FILLER ANDSDR DHL2001806535Floor Support · crackedC-CHECK - FWD CARGO COMPART. FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA 600. L-35LT. PERFORMED STOP DRILL IAW SRM 53-1-0 FIG 1B. FABRICATED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. INSTALLED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. STATUS-CLOSED.SDR RRXA11023Door Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT WW DOOR FRAME AT STA 883, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2B, DWG 5616306, DC-8 SRM 53-1-01SDR DHL2001806637Rib · crackedC-CHECK, LT WING L/E RIB LWR PORT .5 INCH CRACK AT STA XFS 642 - 250.SDR DHL2001806609Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 747.000. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2 CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INBSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATSDR DHL2001806580Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 041.950.PERFORMED STOP DRILL AND FABRICATED DOUBLER IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806579Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1 INCH CRACK AT STA XFS 841.250. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CSDR DHL2001806578Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1 INCH CRACK AT STA XFS 822.950. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CSDR DHL2001806577Rib · crackedC-CHECK - LT WING L/E RIB UPPER PART HAS A 1/2 INCH CRACK AT STA XFS 785.250. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUSSDR DHL2001806576Rib · crackedC-CHECK, LT WING L/E RIB LOWER PART HAS A 1/2 INCH CRACK AT STA XFS 803.750.PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CSDR DHL2001806567Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 785.800. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED & PRIMED IAW SRM 51-1-8B, AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. STATUS-CLOSED.SDR DHL2001806556Rib · crackedC-CHECK - LT WING LE RIB UPPER PART 1 INCH CRACK AT STA XFS 785.800. PERFORMED STOP DRILL AND FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B AND INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 FIG2. STATUS-CLOSEDSDR UPS01835408Floorboard · corrodedINSPECTION TYPE:C2 FLOORBOARD STA 1040 BETWEEN RAILS E & F CORRODED REPAIRED AREA IAW DC8 SRM 53-2-3SDR RRXA010018Tire · blownON LANDING, TOWER REPORTED SMOKE OF RIGHT MLG NR 8 TIRE BLEW, NR 3 TIRE DAMAGED UPON LANDING. NO SECONDARY CAUTION LIGHT OR ANTI SKID LIGHT ILLUMINATED. TRANSFERRED TO DMI LIST AS CONTROL C-9272181-1171 CAT: C MEL 3101 ATA 3245 DUE DATE 23MAR01 PLACARD INSTASDR RRXA11031Longeron · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 35-55 AND L26R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-SDR DHL2001806536Floor Support · crackedC-CHECK - FWD CARGO COMPARTMENT LT FLOOR SUPPORT ANGLE CRACKED 3 INCH AT STA 520.00 L-33L TO L34L. STOP DRILLED AND FABRICATED DOUBLER AND INSTALLED IAW SRM 53-2-5 PAGE 6M. STATUS-CLOSED.SDR DHL2001806533Angle · crackedC-CHECK - VERT. STAB. LE INNER RIB REINFORCING ANGLE CRACKED 1/2 INCH ZF 86.000 RT. REMOVED CRACK REINFORCING ANGLE IAW SRM 51-1-21 PAGE 1. FABRICATED ANGLE IAW SRM 55-1-1 FIG 2. CLEANED, TREATED AND PRIMED IAW SRM 5-1-8B. INSTALLED ANGLE IAW SRM 51-1-21 PAGSDR DHL2001806506Floor Support · crackedC-CHECK - FWD CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED 1 INCH AT STA. 220 L-35 LT CORRECTIVE ACTION: PERFORMED STOP HOLE. FABRICATED REINFORCING ANGLE AND INSTALLED IAW SRM 53-2-3 FIG 10. STATUS-CLOSED.SDR RRXA010017Engine · failedAFTER 1 HR INFLT NOTICED N2 DROPPED +0 2 PERCENT N1 EGT FUEL FLOW NORMAL QTS CKD OTHER GAUGES OIL QTY AT 6 QTS AND DROPPING OIL PRESS 40 PSI, RETARDED THE THROTTLE AND PERFORMED A PRECAUTIONARY SHUTDOWN AS PER QRH. WHEN OIL QTY DROP TO 20 PRESS BETWEEN 20-25 SDR DHL2001806607Control Valve · misinstalledC-CHECK - RT FWD TANK, LEVEL CONTROL VALVE ELECTRICAL PLUG IMPROPERLY SAFETIED. SAFETIED PROPERLY LEVEL CONTROL VALVE ELECT PLUG (RT FWD TANK) IAW MM 20-18-0 PAGE 201-215. STATUS-CLOSED.SDR DHL2001806590Floor Panel · crackedC-CHECK - COCKPIT - 682 FLOOR PANEL SUPPORT ANGLES LWR EDGE CRACKED 1/2 INCH AT STA -12.000. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRICATED REINFORCING ANGLE IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING ANSDR DHL2001806544Structure · crackedC-CHECK 0- TAIL CONE INTERIOR PART, SIDE, RT AT STA 1920, SHOWS 1/2 INCH CRACK AND RIVETS LOOSE IN ELEVATOR TORQUE TUBE PROTECTOR. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1. PERFORMED STOP HOLE IAW SRM 53-2-0 FIG 1B. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1SDR DHL2001806543Floor Panel · crackedC-CHECKED - FLIGHT COMPARTMENT #676B FLOOR PANEL SKIN CRACKED. PERFORMED STOP HOLE IAW SRM 53-2-3 FIG 10. FABRICATED DOUBLER IAW SRM 53-2-3 FIG 10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER USING NEW FASTNERS IAW SRM 51-1-21 PAGE 1. SDR DHL2001806542Floor Panel · crackedC-CHECK - FLIGHT COMPARTMENT 676C FLOOR PANEL SKIN CRACKED. PERFORMED STOP HOLE IAW SRM 53-2-3 FIG 10. FABRICATED DOUBLER IAW SRM 53-2-3 FIG 10, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 53-2-3 FIG 10. STATUS-CLOSED.
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