Douglas DC-8-71F
Service difficulty reports · 8,938
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 = 'DC871F' 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 = 'DC871F' 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 UPS02839482Door Frame · crackedINSPECTION TYPE:C1 R2 UPPER AFT DOOR JAMB CORNER HAS CRACKED INTERNAL DOUBLER APPROX 3 INCHES LONG FOUND BY RADIOGRAPHY. REPAIRED AREA IAW DC8 SRM 53-2-0 T/R 53-133.SDR UPS02839476Door Frame · crackedINSPECTION TYPE:C1 L2 LWR FWD DOOR JAMB CORNER CRACKED APPROX 1.5 INCHES LONG ABOVE TRIMOUT FOUND BY RADIOGRAPHY. REPAIRED AREA IAW DC8 SRM 53-2-0.SDR UPS02839458Intercostal · crackedINSPECTION TYPE:C1 L1 DOOR LWR FWD DOOR JAMB CORNER HAS A CRACKED CUSP LONGERON FOUND BY RADIOGRAPHY. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW DAC DWG 5797646.SDR UPS02839328Longeron · corrodedINSPECTION TYPE:C1 STA 1660 LONG 24L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW SRM 53-4-1 FIG 43, AND 53-2-2 FIG 8.SDR IXXA0200119SStructure · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED UNDER A TEMPORARY REPAIR OF THE FORWARD FUSELAGE, STATION 45 AT LONGERON 9L ADJACENT TO L-1 DOOR FRAME. REPAIR ACCOMPLISHED, REMOVAL OF THE TEMPORARY REPAIR AND DAMAGE, FABRICATION AND INSTALLATION OF REPSDR UPS02839452Frame · corrodedINSPECTION TYPE:C1 AFT PIT FRAME CORRODED AND CRACKED AT SCREW HOLE STA 1400 STRINGER 36. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER IAW SRM STD-5310-002. INSTALLED REPAIR DOUBLER IAW SRM STD-5310-002.SDR UPS02839439Attach Fitting · crackedINSPECTION TYPE:C1 STA 822 LONG 22L INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4753360, AND SRM 51-1-20D.SDR UPS02839349Skin · crackedINSPECTION TYPE:C1 RT T-1 DOOR AFT LOWER CORNER HAS A DOUBLER AT STA 440.000. REMOVED DOUBLER, NDT HFEC NO CRACK NOTED AROUND CUTOUT. FABRICATED DOUBLER, TRIPLER, AND FILLER IAW EO DC8-5330-17436-A AND SK-708-650. INSTALLED DOUBLER, TRIPLER, AND FILLER AT RSDR UPS02839325Skin · crackedINSPECTION TYPE:C1 LT WING L/E LOWER SKIN IS CRACKED AT XFS 347.75. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-4087 APPROX C.SDR UPS02839307Doubler · corrodedINSPECTION TYPE:C1 FINGER DOUBLER IS CORRODED BEYOND LIMITS STA 960-980 AT RBL 63. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 5646674, AND SRM 51-1-21.SDR UPS02839500Angle · corrodedINSPECTION TYPE:C1 MAIN CABIN STA 147 LONG 21R ANGLE HAS SHORT FASTENER IN DOUBLER DRILLED HOLE. REMOVED ANGLE, CORROSION FOUND, BLENDED, OUT OF LIMITS IAW DC8 SRM 5 1-1-8, 51-1-20D AND SRM 53-2-0. FABBED ANGLE IAW DC8 SRM 51-1-24, AND DAC DWG 2649940. INSTSDR UPS02839487Fitting · crackedINSPECTION TYPE:C1 STA 850 LONG 10R FWD SIDE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779658, AND UPS ENGINEERING FILE NUMBER DC8-53-20246, SAA SK 708-514, SRM 51-1-20D, 51-3-0, 53-2-1 FIG 7.SDR UPS02839417Fitting · crackedINSPECTION TYPE:C-1 LONG 10R END FITTING CRACKED AT STA 675. REMOVED CRACKED END FITTING AT LONG 10R, STA 675 IAW SRM 51-1-20 REPLACED IAW SRM 51-1-21 AND 51-1-20D.SDR UPS02839362Doubler · crackedINSPECTION TYPE:C1 LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 597.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600, AND SRM 51-1-20D, 51-1-21.SDR UPS02839324Attach Fitting · crackedINSPECTION TYPE:C1 STA 1220 LONG 19R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 4750418, AND SRM 51-1-20D.SDR UPS02839322Attach Fitting · crackedINSPECTION TYPE:C1 STA 781 FWD SIDE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978, AND SRM 51-1-20D.SDR UPS02839321Fitting · crackedINSPECTION TYPE:C1 STA 857 LONG 19R INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 4750422, AND SRM 51-1-20D.SDR UPS02839301Fitting · crackedINSPECTION TYPE:C1 STA 850 LONG 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.SDR UPS02839300Fitting · crackedINSPECTION TYPE:C1 STA 850 LONG 7R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.SDR UPS02839293Fitting · crackedINSPECTION TYPE:C1 STA 850 LONG 9R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.SDR UPS02839292Attach Fitting · crackedINSPECTION TYPE:C1 STA 700 LONG 18R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978, AND SRM 51-1-20D.SDR UPS02839291Fitting · crackedINSPECTION TYPE:C1 STA 857 LONG 3L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659, AND SRM 51-1-20D.SDR UPS02839477Longeron · crackedINSPECTION TYPE:C1 R2 DOOR UPPER AFT JAMB LONGERON 11 CRACKED. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D.SDR UPS02839408Skin · dentedINSPECTION TYPE:C1 DENT IN FUSELAGE SKIN AFT OF L4 DOOR. COLD WORKED AND BLENDED IAW DC-8 SRM 53-2-0, WITHIN LIMITS. NO CRACK NOTED IAW DAC NDT SRM 06-10-01.001. FABBED IAW DC-8 SRM 53-2-1 FIG 10. REPAIRED DENT IAW DC-8 SRM 53-2-1 FIG 10.SDR UPS02839391Skin · crackedINSPECTION TYPE:C1 AFT LOWER FUSELAGE SKIN IS CRACKED AT STA 1800 LONG 33. REMOVED AND REPLACED SKIN BETWEEN STA 1690 TO 1890 LONG 28L TO 28R IAW DWG 5649329, SRM 51-1-21, 51-1-20D, 53-1-0.SDR UPS02839290Skin · crackedINSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 610. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A.SDR UPS02839289Doubler · crackedINSPECTION TYPE:C1 RIGHT WING CENTER L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335.25. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21.SDR IXXA0200051OTank · uncalibratedAFTER TAKE OFF FROM LRD, THE FLIGHT CREW NOTICED A SIGNIFICANT AIRCRAFT ROLL TO THE RIGHT WHICH REQUIRED HALF LEFT AILERON TO MAINTAIN LEVEL FLIGHT. THE FLIGHT RETURNED TO LRD FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE #SDR UPS02839361Frame · crackedINSPECTION TYPE:C1 FRAME STA 55 CRACKED AT SUPPORT ROD BRACKET LONG 24L. CUT OUT DAMAGED AREA, REMOVED CRACKED SHEAR TIE AT STA 55 LONG 24L. FABRICATED AND INSTALLED FRAME REPAIR SECTION AND SHEAR TIE IAW SRM 53-2-0, SRM 53-2-0 FIG 2, AND SRM 53-3-1.SDR UPS02839357Frame · crackedINSPECTION TYPE:C1 FRAME STA 55 CRACKED AT SUPPORT ROD ATTACH FITTING LONG 24R. CUT OUT DAMAGED FRAME IAW SRM 53-2-0 FIG 2. FABRICATED FRAME AND ANGLE REPAIR IAW SRM 53-2-0 FIG2, INSTALLED FRAME ANGLE DOUBLER IAW SRM 51-1-20D.SDR UPS02839332Skin · crackedINSPECTION TYPE:C1 REMOVE DOUBLER ON THE L2 DOOR LWR AFT CORNER AND REPAIR PER DC8 SRM 53-2-0, FIG18 AT STA 1660 LONG 21L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACK AT CUT OUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRMSDR UPS02839331Skin · crackedINSPECTION TYPE:C1 REMOVE DOUBLER ON THE L2 DOOR LOWER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 18 AT LONG 21L. REMOVED EXISTING DOUBLER, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW DC8-5330-17427-SDR UPS02839327Doubler · corrodedINSPECTION TYPE:C1 EXTERIOR SKIN BULGING STA 190 BETWEEN LONG 35L TO 35R, INTERNAL DOUBLER IS CORRODED BEYOND LIMITS REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5779925 AND SRM 51-1-20D, 51-1-21.SDR UPS02839303Skin · crackedINSPECTION TYPE:C1 REMOVED DOUBLER ON R1 DOOR FWD UPPER CORNER AND REPAIR PER SRM 53-2-0 FIG 14 AT STA 160 LONG 10R. REMOVED EXISTING REPAIR, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FILLER IAW SRM 53-2-0SDR UPS02839144Fitting · crackedINSPECTION TYPE:C1 INT CABIN CRACKED FRAME TO FORMER FITTING STA 12 RT STA 220. REMOVED AND REPLACED CRACKED FITTING.SDR UPS02839134Skin · crackedINSPECTION TYPE:C1 NR 1 PYLON O/B SIDE AT PNL 199A UPPER SKIN IS CRACKED. FABBED DOUBLER IAW DC8 SRM 54-2-0, INSTALLED DOUBLER IAW DC8 SRM 51-1-20D.SDR UPS02839106Bulkhead · damagedINSPECTION TYPE:LNSV NLG BULKHEAD DAMAGED. TRIMMED OUT DAMAGE ON BULKHEAD IAW REO G08732. DYE PENETRANT CHECKED FOR CRACKS, NONE NOTED. FABRICATED NEW STIFFENER, FILLERS, TRIPLER, AND FINGER DOUBLER PER DAC DWG 5615530 & REO G08732. INSTALLED IAW REO G0873SDR UPS02839075Mount · brokenINSPECTION TYPE:N/A ATB - NLG RETRACT CYLINDER AFT MOUNT ASSY BROKE CAUSING DAMAGE TO FUSELAGE SKIN. A/C FERRIED TO TCO FOR REPAIR 9150. TRIMMED DAMAGE ON BULKHEAD IAW REO G08732 STEP NR 1, DYE PENETRATE INSP IAW MIL-271F, NO CRACK NOTED IN CUTOUT. FABBED, SDR UPS02839044Light · inoperativeINSPECTION TYPE:N/A, ENTRY DOOR EMERGENCY EXIT LIGHTS INOP. OPS CHECK NORMAL, NO DEFECTS NOTED.SDR UPS02839155Doubler · crackedINSPECTION TYPE:C1 L1 LWR FWD DOOR JAMB CORNER CRACKED AT FASTENER HOLE. INTERNAL DOUBLER CRACKED PER X-RAY INSP FOUND OX AND DOUBLE DRILLED HOLES, INSTALLED BUSHINGS IAW DAC DWG 47099818, FABBED REPAIR BUSHINGS IAW DAC DWG 4709987B, BLENDED GOUGES WITHIN LIMSDR UPS02839135Fitting · crackedINSPECTION TYPE:C1 RT WING STR 51 I/B SIDE AT STA 74 IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, TORQUED BOLT IAW DC8 SRM 51-1-23.SDR UPS02839123Fitting · crackedINSPECTION TYPE:C1 RT WING STR 51 I/B SIDE STA 74 IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, TORQUED BOLT IAW DC8 SRM 51-1-23.SDR UPS02839090Skin · crackedINSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1746 AT LONG 35R AND 34R. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, FILLER, AND FINGER DOUBLERS IAW SRM 53-2-1 FIG 7.SDR UPS02839136Web · crackedINSPECTION TYPE:C1 RT MLG DOOR CUTOUT AREA AFT WEB PNL OF UPLATCH CUTOUT IS CRACKED. FABBED NEW WEB IAW DAC DWG 5651021 & NEW ATTACH ANGLE IAW DAC DWG 56 51221. INSTALLED ASSY IAW DC8 SRM 51-1-21 & 51-3-0 AND 51-120D.SDR UPS02839129Web · crackedINSPECTION TYPE:C1 RT MLG DOOR CUTOUT AREA AFT WEB PNL OF UPLATCH CUTOUT IS CRACKED. FABBED NEW WEB IAW DAC DWG 5651021 & NEW ATTACH ANGLE IAW DAC DWG 56 51221. INSTALLED ASSY IAW DC8 SRM 51-1-21, 51-3-0 & 51-1-20D.SDR UPS02839037Fitting · crackedINSPECTION TYPE:C2 STA 780 LONG 35R END FITTING CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 5755058 AND SRM 51-1-21.SDR IXXA0200117SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK ALONG WITH CORROSION WAS DETECTED ON THE LT WING UPPER AFT SKIN ABOVE THE LT GEAR TRUNNION AREA. REAPIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUSDR IXXA0200049OOil Cap · looseEN ROUTE FROM PDX TO BFI, THE FLIGHT CREW NOTICED THE NUMBER ONE ENGINE OIL QUANTITY DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND SECURED THE ENGINE AND CONTINUED TO BFI FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE LOCATING THE SSDR UPS02839036Rib · crackedINSPECTION TYPE:C2 RUDDER RIB CRACKED STA ZR 135. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5656223 AND SRM 51-1-21.SDR UPS02839035Rib · crackedINSPECTION TYPE:C2 RUDDER RIB CRACKED AT STA ZR 140. REMOVED, FABRICATED, AND REPLACED RIB IAW DWG 5656223 AND SRM 51-1-21.
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