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 DHL2003604710Skin · damagedD-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR IN IT (MAJOR REPAIR). PERFORMED MAJOR REAPAIR IAW SRM 52-1-0 PG 1, SRM 52-4-1 PG 5, DHL-CVG-00079H. REMOVED D-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW SSDR DHL2003604663Skin · crackedLT WING INBD. AILERON L/E UPPER PLATING HAS THREE CRACKS OF 0.750, 0.500, 0.500 AT STA. XA 487.000 - XA 569.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-8-1 FIG.1. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PG. 1. CLEANED, TREATED AND PRIMED AREA IAW SDR DHL2003604751Fastener · shearedLT WING NR 1 ALT TANK FWD LWR PART HI-LOK SHEARED. PERFORMED MAJOR REPAIR IAW BOEING TELEX SEUL-030613 AND SEULIM-03-00019H, FAR FORM 8110-3 DATED JUNE 16, 2003. REMOVED OLD SEALANT IAW EA-04923. CLEANED AND INSPECTED AREA IAW SEULIM-03-00019H, FAA FORM 811SDR DHL2003604786Longeron · corrodedAFT ACCESSORY COMPT L-30R CORRODED BETWEEN STA 1640.000 AND STA 1660.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG 8. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION FROM L-30R (STA 1640.000 - 1660.000) IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LISDR DHL2003604608Track · broken"D" BELLY DOOR AFT TRACK BROKEN, STA 1440.000. REMOVED BROKEN AFT TRACK IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW AFT TRACK ON "D" BELLY DOOR, STA 1440.000 IAW SRM 51-1-21 PG 1. FOR OPS CHECK SEE N/R 0530.SDR DHL2003873515Frame · crackedRT WING CENTER L/E FORMER CRACKED 0.250 AT XFS.404.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AT STA XFS.404.000 IAW SRM 57-2-0 PG 9-10. FABRICATED ANGLE DOUBLER IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLESDR UPS03840940Skin · crackedINSPECTION TYPE: C3 HFEC INSPECTION OF THE L-1 DOOR LOWER AFT CORNER DETECTED A CRACK APPROX. .750 INCHES SKIN, STATION 60 BETWEEN LONG. 20L-21L CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER,TRIPLER AND FILLER I.A.W. SRM.SDR UPS03840931Door Frame · mislocatedINSPECTION TYPE: C, MAIN CABIN AT STA 1660-R2 DOOR JAMB WEB HAS DOUBLE DRILLED HOLES. REM FASTENERS FROM DOOR JAMB WEB. REM AIR GRILL AND R2 DOOR DRAIN PAN. TRIMMED OUT DAMAGE FOUND TO BE OUT OF LIMITS IAW DC8 DWG DC8-53A-01 0 AND UPS EO DC8-5310-11728-ASDR UPS03840930Longeron · crackedINSPECTION TYPE: C LONGERON 17L AND FWD END FITTING CRACKED AT BS 1768 REMOVED LONGERON 17L AND END FITTING. LOCATED, DRILLED LONGERON AND END FITTING IAW SRM 51-1-24. REMOVED AND REINSTALLED HYDRAULIC CASE AND LINES AT STA 1768 IAW MM 20-12-00. INSSDR UPS03840916Rib · crackedINSPECTION TYPE: C, RT WING L/E LOWER RIB IS CRACKED AT XFS 741. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS03840915Rib · crackedINSPECTION TYPE: C, LEFT WING CENTER L/E UPPER RIBS ARE CRACKED AT XS 497.491 AND XS484.895. STOP DRILLED CRACKS. NDT VERIFIED CRACKS. STOPDRILL, FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.SDR UPS03840891Access Panel · crackedINSPECTION TYPE: C3, RIGHT WING IB. AILERON LOWER ACCESS PANEL NR 541 CUTOUT IS CRACKED. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED DOUBLER IAW SRM. 57-2-0 FIG. 2H.SDR UPS03840888Rib · crackedINSPECTION TYPE:C3 RIGHT WING OB. LE. LOWER RIB IS CRACKED AT XFS 728 STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 57-2-0 FIG. 2SDR UPS03840886Stiffener · crackedINSPECTION TYPE:C3 LEFT WING TE. VERTICLE STIFFNER IS CRACKED PAST STOPDRILL AT XW 0 REMOVED EXISTING DOUBLER,CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED FILLER AND REINSTALLED REPAIR DOUBLER I.A.W. DC8-5720-7767-ASDR UPS03840884Rib · crackedINSPECTION TYPE:C3 LEFT WING LE UPPER RIB IS CRACKED AT XFS 741.25. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 57-2-0 FIG. 2SDR UPS03840878Doubler · crackedINSPECTION TYPE: C3, RIGHT WING LE LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335 REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG.5769589,AND SRM. 51-1-20D,51-1-21SDR UPS03840877Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 747. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2SDR UPS03840875Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 797. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM. 57-2-0 FIG. 2SDR UPS03840871Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE UPPER RIB IS CRACKED AT XS448 STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2SDR UPS03840870Rib · crackedINSPECTION TYPE: C3, RT WING LE. UPPER RIB IS CRACKED AT XFS 297. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2SDR UPS03840868Rib · crackedINSPECTION TYPE: C3, LEFT WING LE UPPER RIBS ARE CRACKED AT XFS 826.75,XFS 847.5 AND XFS 822.5. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILL TERMINATES CRACKS, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2SDR UPS03840867Rib · crackedINSPECTION TYPE: C3, LEFT WING OB LE LOWER RIBS ARE CRACKED AT XFS 772.5 AND XFS 822.5. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM. 57-2-0 FIG. 2SDR UPS03840866Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 622. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2SDR UPS03840865Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE. UPPER RIB IS CRACKED AT XFS 872. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2SDR UPS03840864Rib · crackedINSPECTION TYPE: C3, LEFT WING LE. UPPER RIBS ARE CRACKED AT XFS 781.25,XFS 797.5, XFS 803.75. STOP DRILLED CRACKS,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLERS IAW SRM. 57-2-0 FIG. 2SDR UPS03840863Rib · crackedINSPECTION TYPE: C3, LEFT WING LE LOWER RIB IS CRACKED AT XFS 766.25 STOPDRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2SDR UPS03840862Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE. UPPER RIB IS CRACKED AT XFS 822. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2SDR UPS03840861Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 822. STOP DRILLED RIB,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2SDR UPS03840860Rib · crackedINSPECTION TYPE: C3, LEFT WING LE. OB. LOWER RIB IS CRACKED AT XFS 622.5 STOP DRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 57-2-0 FIG. 2SDR UPS03840859Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE LOWER RIB IS CRACKED AT XFS 785. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER I.A.W. SRM. 57-2-0 FIG.2SDR UPS03840858Rib · crackedINSPECTION TYPE: C3, RIGHT WING LE. LOWER RIB IS CRACKED AT XFS 791. STOP DRILLED CRACK,NDT VERIFIED STOP DRILL TERMINATED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM. 57-2-0 FIG. 2SDR UPS03840857Stiffener · crackedINSPECTION TYPE: C3, LEFT WING TE. VERTICLE STIFFNER IS CRACKED TWO PLACES AT XW 11.5 REMOVED,FABRICATED AND REPLACED STIFFNER I.A.W. DWG. 9887427 AND SRM 51-1-20D.SDR UPS03840856Rib · crackedINSPECTION TYPE: C3, LT WING LE LOWER RIB IS CRACKED AT XFS 385, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLERS I.A.W. SRM. 57-2-0 FIG.2SDR UPS03840855Rib · crackedINSPECTION TYPE: C3, LT WING CENTER L/E UPPER RIBS ARE CRACKED AT XFS 366.5 AND XFS 379. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILL TERMINATES CRACKS, FABRICATED AND INSTALLED REPAIR ANGLES IAW SRM 57-2-0 FIG 2.SDR UPS03840854Rib · crackedINSPECTION TYPE: C3, RT WING OUTBOARD LE LOWER RIB IS CRACKED AT XFS 816. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2.SDR UPS03840853Rib · crackedINSPECTION TYPE: C3, RT WING L/E UPPER RIB IS CRACKED AT XFS 304. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2.SDR DHL2003604697Tee Fitting · crackedRT AFT PRESSURE BULKHEAD TEE FITTING CRACKED 2.500 APPROX BETWEEN L-7 AND L-8R STA 1766.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 9, SRM 51-1-1. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED REPAIR ANGLE SDR DHL2003604734Plate · damagedLT INNER WING L/E AUX TANK UPPER PLATING SHOW HOLES FOR DOUBLER REMOVAL. PERFORMED MAJOR REPAIR IAW EODHL-030577, ED-3426. REMOVED ALL EVIDENCE OF CORROSION FROM REPAIRED AREA IAW SRM 51-1-8 PG 17-18. PLUGGED EXISTING HOLES WITH RIVETS IAW EODHL-030577, ED-SDR DHL2003604726Frame · crackedFWD ACCY COMPT FRAME CRACKED 1.500, STA 55.000, L-24R . TRIMMED OUT CRACKED FRAME SEGMENT IAW SRM 53-2-0 FIG 2, TR 53-125, TR 53-110. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FRAME SEGMENT (7075-T6 AL0.071) AND SPLICE ANGLES (02 EA) (707SDR DHL2003806010Lamp · inoperativeNR 6 UPPER DECK SMOKE DETECTOR WILL NOT TEST. DEFERRED NR 6 SMOKE DETECTOR IAW MEL 26-6-2 CAT C. DMI 13267 PLACARD IS INSTALLED. REF DMI 13267 NR 6 UPPER DECK SMOKE DETECTOR WILL NOT TEST. RELAMPED NR 6 MAIN CARGO COMPARTMENT SMOKE DETECTOR AS PER MM 26-10-SDR DHL2003604716Skin · damagedB-CARGO DOOR EXTERNAL SKIN WITH INTERIM REPAIR IN IT. PERFORMED MAJOR REPAIR IAW SRM 52-1-0 PG 1, SRM 52-4-1 PG 4, BOEING MESSAGE DHL-CVG-0079H. REMOVED EXTERNAL SKIN WITH INTERIM REPAIR IN IT IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1. FABRICATED NEW SKIN (7075SDR DHL2003604783Fitting · crackedAFT ACCY COMPT END FITTING CRACKED 1.500, STA 1640.000 - STA 1660.000, L-30R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-4-1 FIG 43A SHEET 2. REMOVED CRACKED END FITTING IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICSDR DHL2003604592Panel · damagedLT WING INBD AILERON UPPER PLATING SHOWS INTERIM REPAIRS BETWEEN STA XA 441.000 - XA 542.000. PERFORMED MAJOR REPAIR IAW EODHL-030570, ED-3398. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030570, ED-3398. CLEANED, TREATED ASDR DHL2003873505Frame · crackedLT HORIZONTAL STAB L/E INNER FORMER CRACKED 0.500 AT XFS 60.000 (UPPER/LOWER PART). REMOVED FASTENERS IAW SRM 51-1-20D PG 21. STOP DRILLED CRACK IAW SRM 55-2-0 PG 7,8. FABRICATED REINFORCING ANGLE IAW SRM 55-2-0 PG 7,8. CLEANED,TREATED AND PRIMED IAW SRM 51-1SDR DHL2003604765Attach Fitting · crackedMAIN CARGO COMPT FRAME FITTING CRACKED 4.500 AT STA 960.000 BETWEEN L-18L AND L-22L. PERFORMED MAJOR IAW SRM 53-1-0 PG 1, ATM PO201390, DWG 5646955. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATSDR DHL2003873500Skin · corrodedRT WING CTR L/E UPPER PLATING CORRODED STA XFS.460.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12. REMOVED CORROSION FROM RT WING CTR L/E UPPER SKIN IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11-12. REMOVED CORRODED SKIN SDR UPS03840927Skin · damagedINSPECTION TYPE: C, 8 PREVIOUS BLENDOUTS BELOW C-PIT DOOR BETWEEN LONG. 34R TO 30R FROM STA. 1220 TO 1260 CUT AND REMOVED SKIN SECTION FROM STATION 1190-1230 BETWEEN LONG 29R TO 34R,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED SKIN SECTION ANSDR DHL2003604767Skin · corrodedTAIL CONE EXTERNAL SKIN SHOWS INTERIM REPAIR AND SEVERAL CORROSION SPOTS BETWEEN STA.1916.000 AND STA.1951.000. PERFORMED MAJOR REPAIR IAW EODHL-030565, ED-3394. REMOVED FASTENERS AND INTERIM REPAIRS. REMOVED CORROSION. FOUND OUT OF LIMITS. TRIMMED OUT THE SDR DHL2003604597Tie · crackedFUSELAGE TAIL CONE INTERIOR - LT TIE 1.000 CRACKED AT STA. 1951.000. STOP DRILLED CRACK AND FABRICATED DOUBLER (2024-T3 AL0.040) IAW SRM 53-2-0 PG.1-2. CLEANED, TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-1-8B. INSTALLED NEW DOUBLER IAW SRM 51-1-21 PG.1, SRSDR DHL2003873504Frame · crackedRT WING CENTER L/E FORMER CRACKED 0.250 AT XFS 354.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK IAW SRM 57-2-0 PG 9,10. FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG 9,10. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED REINFORCING A
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