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 IXXA05SMN162SSkin · crackedDURING C CHECK INSPECTION, LT WING, UPPER SKIN HAS 03 CRACKS, XRS 74.000 S-9 S-10. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-2-1 FIG 17, EO SEMAN NR 20051135 DATE 08-10-05. REMOVED FASTENERS IAW DC-8 SRM 51-1-20D PAGE 21. REMOVED DAMAGED AREA IAW DC-8 SR, 57-2SDR IXXA05SMN161SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, LT WING NR 4 VANE FLAP LWR SKIN DELAMINATED. REMOVED AND REPLACED NR 4 FLAP VANE (LT WING) IN REPAIRED CONDITION IAW DC8 MM 27-51-14 PAGE 201-202.SDR IXXA05SMN163SAccess Door · crackedDURING ROUTINE C CHECK INSPECTION, LT WING, SLOT ACCESS DOOR CRACKED 1, XILD 7095 XS 250.089. REMOVED AND REPLACED INBD SLOT UPPER DOOR ON LT WING IAW DC-8 MM 27-80-02 PAGES 201-204.SDR IXXA05SMN160SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, RT WING, NR 3 VANE FLAP LWR. SKIN DELAMINATED. REMOVED AND REPLACED NR 3 FLAP VANE ON RT WING (REPAIRED CONDITION) IAW DC8 MM 27-51-14 PAGES 201-202.SDR UPS05845471Spar · crackedINSPECTION TYPE:C1 POSSIBLE CRACK ON LOWER SURFACE SKIN AFT CTR SPAR RT CTR AUX TANK. NDT VERIFIED 2 INCH CRACK AT RT CTR AUX TANK AFT CTR SPAR. REMOVED CRACKED SECTION OF CTR SPAR, FABRICATED REPLACEMENT SECTION OF CTR SPAR AND REPAIR PARTS, AND INSTALLED ISDR IXXA05SMN159SSkin · delaminatedDURING ROUTINE C CHECK INSPECTION, LT WING.- T/E UPPER PANEL EXTERNAL SKIN DELAMINATED, XW 0.000 XW 47.000. REMOVED DELAMINATED PANEL AND REPLACED ON LH WING T/E UPPER PANEL EXTERNAL SKIN, XW 0.000 – XW 47.000 IAW DC8 SRM 51-3-0SDR DHL2005806500Frame · crackedRUDDER L/E FORMER CRACKED 0.500" STA ZR 115.000. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.063") IAW SRM 55-2-0 PG 7, 8. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT IAW SRM 51-1-16. INSTASDR UPS05845394Doubler · crackedINSPECTION TYPE: C3, LT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE XFS 597.500. REMOVED, FABRICATED, AND INSTALLED INTERNAL DOUBLER IAW DC-8 SRM 57-3- 0, 51-1-20D, AND 51-1-21.SDR UPS05845196Pressure Panel · corrodedINSPECTION TYPE:C1 FOUND EXFOLIATION CORROSION AND CRACKS ON COCK PIT SUBFLOOR AT STA -67 RBL 60 INSIDE RIGHT NOSE TUNNEL. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR IAW DWG SRO8530 026 AND DC-8 SRM 51-1-20D.SDR UPS05845033Engine · shutdownNR 4 ENG SHUT DOWN IN FLT DUE TO OVER TEMP AND LOUD THUD. FROM LP 427064 ITEM 1 AND LP 427065 ITEM 3: PERFORMED THRUST LEVER STATIC TRIM IAW AMM 71-00-00 PG 595.23 TEST 9A. PERFORMED PART POWER TRIM AND INCREASED BY 10 CLICKS. PERFORMED ENG HIGH PWR RUN-UP.SDR UPS05845195Fitting · crackedINSPECTION TYPE:C1 -C- PIT STA 1240 L35R FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845194Fitting · crackedINSPECTION TYPE:C1 -C- PIT STA 1230 BETWEEN L34R TO L35R FITTING CRACKED AROUND FASTENERS . REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4758514 AND DC-8 SR M 51-1-20D.SDR UPS05845193Fitting · crackedINSPECTION TYPE:C1 -C- PIT CROSS SLIDE DOOR BANANA FITTING CRACKED AT BUMPER STOPS AT L27L STA 1180. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845162Fitting · corroded"C" PIT BATHTUB FITTING CORRODED AT STA 1200 BETWEEN L29L AND L28L. REMOVED AND REPLACED BATHTUB FITTING IAW DC-8 SRM 53-2-0 FIG 2D AND 51-1-20D.SDR UPS05845222Fitting · crackedA PIT STA 348 L31R ZEE FITTING CRACKED 3 INCHES LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845192Seal · corrodedINSPECTION TYPE:C1 HEAVY CORROSION AROUND EXTERNAL POWER CABLE PRESSURE SEAL BELOW EPC RA CK STA 20 RBL 60. REMOVED, FABRICATED, AND INSTALLED PRESSURE SEAL DOUBLER IAW DWG 56122 78 AND DC-8 SRM 51-1-20D.SDR UPS05845161Stiffener · corrodedHEAVY CORROSION ON BASE OF DIAGONAL STIFFENER IN COCKPIT SUB FLOOR BELOW PILOTS LT RUDDER PEDAL. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT GUSSET IAW DWG 5597992 AND SRM 51-1-20D.SDR UPS05845160Fitting · cracked"A" PIT STA 280 L29R ZEE FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED "Z" FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845000Bulkhead · crackedSTAB ACCESS COMPT FWD BULKHEAD LEDGE NR 3 CRACKED AT ANGLE ATTACH, LWR (MARKED). REMOVED LT AFT BULKHEAD WALL PANEL OF MAIN CARGO DECK TO FACILITATE SHEET METAL REPAIR. CONT. TO LP 414978 NR 2: REMOVED RIVETS AND BOLTS FROM PRESS BULKHEAD TO FACILITATE REPAIRSDR UPS05845159Fitting · crackedMAIN CABIN STA 834 L18R FRAME TO INTERCOSTAL FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845201Battery Pack · inoperativeINSPECTION TYPE:PNT EMERGENCY EXIT LIGHTS FAILED TEST REMOVED AND REPLACED BATTERY PACK. OPS CHECK NORMALSDR UPS05845146Fitting · crackedWHILE WORKING N/R 859104 FOUND LONG 31L END FITTING CRACKED. REMOVED AND REPLACED LONG END FITTING AT STA 106 IAW SRM 51-3-0 51-1-21, AND SRM 51-1-20D.SDR UPS05845112Frame · crackedINSPECTION TYPE:C1 WHILE ACCOMPLISHMENT OF MCD FWD HINGE REPLACEMENT AFTER REMOVAL OF THE ACTUATOR CLOSE OUT PNL FOUND A 1" CRACK ON THE FWD UPPER MAIN FRAME CRACK ON "Z" FRAME STOPPED AT EXISTING HOLE NDT HFEC CRACK TERMINATES AT EXISTING HOLE IAW NDTSPM06-10SDR UPS05845001Skin · damagedLT UPPER WING PANEL AT T/E IN FRONT OF NR 4 SPOILER HAS SKIN ROLLED UP APPROX 18 - 24 INCHES ALONG AFT EDGE W/APPROX 30 RIVETS PULLED. ROLLED APPX 1.5 - 2 INCHES FWD AT DEEPEST SPOT. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR DOUBLER & ANGLE & SEAL PER EO DC8SDR UPS05845158Finger Doubler · corrodedCENTER WING BOX AT STA 879 TO 902 LBL 65 FINGER DOUBLER HAS SEVERAL SHEARED FASTENER HEADS AND HEAVY CORROSION UNDER THE FINGER DOUBLER. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. AREA UNDER FINGER DOUBLER FOUND IN LIMITS IAW SDR UPS05845153Frame · crackedMAIN CABIN FRAME CRACKED 1" LONG AT STA 1700 L20L. TRIMMED OUT DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW EO DC8-5310 -11728-B AND DWG DC8-53A-011-A.SDR UPS05845381Fitting · crackedINSPECTION TYPE: C1, MAIN CABIN LONGERON SPLICE FITTING HAS 4 INCH CRACK STA 310 L18L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SAA SK 809- 850545 AND UPS ENGINEERING FILE NUMBER DC8-53-20487.SDR UPS05845157Fitting · crackedMAIN CABIN STA 1220 L20R FRAME ATTACH FITTING CRACKED 1/2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845156Fitting · crackedSTA 1160 L19R FITTING CRACKED 1" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR UPS05845155Fitting · crackedSTA 902 L5R LONGERON FITTING CRACKED 2" LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.SDR UPS05845154Fitting · crackedSTA 700 LONG 18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED APPROX 3" LONG. REMOVED AND REPLACED ATTACH FITTING IAW DC-8 SRM 51-1-20D.SDR DHL2005806001O-Ring · leakingDURING CLIMB OUT,HYD PRESS DROPPED TO ZERO AND HYD QTY DROPPED TO AUX LEVEL. DURING ABN PROC SYSTEM LEVEL DROPPED WELL BELLOW AUX LEVEL WHEN CONFIGURING TO LAND. FOUND WING SLOT CNTL VALVE IN R. W/W LEAKING AT RETAINING PLUG/STUD. R & R UPPER AND LOWER O-RINGSDR UPS05845151Skin · crackedR/W UPPER SURFACE 6" AFT OF FRONT SPAR AT FUEL PROBE NR 12 HAS A 1" CRACK AT FASTENER HOLE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57- 2-1 FIG 10.SDR UPS05845150Skin · crackedFUSELAGE EXTERIOR SKIN CRACKED 1/2" LONG AT STA 1746 L15R. REMOVED DAMAGED SECTION OF SKIN, FABRICATED, AND INSTALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7.SDR UPS05845149Skin · crackedFUSELAGE EXTERIOR SKIN CRACKED 1/2" LONG AT STA 1746 L15L. CUT OUT DAMAGED SECTION OF SKIN AT STA 1746 AND L15L. FABRICATED, AND IN STALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7.SDR UPS05845148Seat Track · corrodedFE'S AFT SEAT TRACK STOP HOLES WORN AND HEAVY CORROSION AROUND COUNTER SUNK ATTACH SCREWS. REMOVED AND REPLACED FE'S AFT SEAT TRACK IAW DC-8 SRM 51-1-21, 51-3-2, AND 51-3-0.SDR UPS05845003Fitting · corrodedA/C COMPT LONGERON END FITTING CORRODED AROUND FASTENER HOLE AT STA 70 L32R. REMOVED AND REPLACED LONG END FITTING AT STA 70 L32R IAW SRM 57-1-20D, AND 51-3-2.SDR UPS05844997Finger Doubler · corrodedINSPECTION TYPE: C1, SKIN SPLICE AT FS 1350 INTERIOR FINGER DOUBLER HAS PITTED CORROSION FROM L31R TO L31L. REMOVED FINGER DOUBLER AT FS 1350 IAW SRM 51-1-21 AND 51-1-20D. FABRICATED AND INSTALLED FINGER DOUBLER AT FS 1350 L31L TO 31R IAW SRM 51-1-21.SDR UPS05845188Hinge Pin · wornINSPECTION TYPE:C1 REMOVE MAIN CARGO DOOR HINGE TO ACCOMPLISH FWD HINGE REPLACEMENT, CRACKED, FOUND DURING DOUBLER REMOVAL. REMOVED MAIN CARGO DOOR AND HINGE, MAG PARTICAL, HFEC AND FPI INSPECT IONS ACCOMPLISHED, NO CRACKS NOTED. REINSTALLED HINGE, REPLACED SDR DHLA200587302Bolt · corrodedDURING B-CHECK INSPECTED NOSE LANDING GEAR REMOVED RED SEAL PER NON-ROUNTINE 009836 FOUND BOLT RUSTED THROUGH AND FELL OFF. LOG PAGE OF B-CHECK 057634SDR UPS05845121Skin · corrodedINSPECTION TYPE:C1 UPON REMOVAL OF D-PIT SCUFF PLATE TO FOM FOR NDT INSPECTION TO COMPLY WITH EO DC8-5330-20206 FOUND CORROSION ON FUSELAGE SKIN FS 1395 TO 1445 L34R-L32R. REMOVED AND REPLACED FUSELAGE SKIN AT STA 1395-1445 L34R-L32R IAW SRM 51-1-21, 51-1-20DSDR UPS05844965Longeron · corrodedINSPECTION TYPE:C1 AFTER REMOVAL OF INTERCOSTAL ON N/R 858794 FS 1473 L34R FOUND CORROSION AT LONGERON UNDER STRAP REMOVED LONGERON 34R STA 1350 TO 1490 IAW DC8 SRM 53-2-2 FABRICATED AND INSTALLED LONGERON 34R AT STA 1350-1490 IAW DRWG 3646937SDR UPS05845183Skin · crackedREPLACE SKIN PANEL AT STA 70 TO -21.92 LONG 31R-L31L. REMOVED AND REPLACED FWD BELLY SKIN AT STA -21.92 TO STA LONG 31L TO LONG 31R IAW EO DC8-5330-8942-D.SDR UPS05845182Plate · crackedMAIN CARGO DOOR LWR AFT CORNER, THE DOOR JAMB CORNER INTERNAL SUPPORT PLATE IS CRACKED. REMOVED FILLET IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT FILLET AT THE MAIN CARGO DOOR LWR AFT DOOR JAMB INTERNAL SUPPORT PLATE IAW DWG 5772786 AND SRM 51-3-0SDR UPS05845120Fitting · crackedINSPECTION TYPE:C1 LONG 31R SPLICE FITTING CRACKED FROM 1040-1060. REMOVED AND REPLACED LONG SPLICE FITTING IAW SRM 53-1-0 AND 51-1-20 AT STA 1040-1060 LONG 31R.SDR UPS05845115Fitting · crackedINSPECTION TYPE:C1 BATHTUB FITTING CRACKED AT C-PIT DOOR JAMB STA 1200 L33R-L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 53-2-0 AND SRM 53-2-0 FIG 02G.SDR UPS05845046Floorbeam · crackedF/S 960 LBL 60 FLOORBEAM AT LIGHTING HOLE ON VERT FLANGE AT CENTER OF HOLE HAS A 5" CRACK GOING AT HORIZ ANGLE. STOP DRILLED CRACKED FLOORBEAM, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SAA SK 807-858978 AND UPS EODC8-53-20486.SDR UPS05844966Fitting · crackedINSPECTION TYPE:C1 SPLICE FITTING CRACKED AT STA 610, L35L REMOVED CRACKED SPLICE FITTING AT STA 610, LONG 35L IAW SRM 51-1-20D. FABRICATED REPLACEMENT FITTING AND INSTALLED FITTING IAW DRWG 3750330SDR UPS05844880Control Valve · closedBTB DUE TO SMOKE IN COCKPIT DURING PUSHBACK. SUSPECT LEFT PACK OPEN DUE TO DMI ON LEFT PACK. LEFT PACK SWITCH WAS IN THE OFF POSITION. FOUND LEFT PACK FLOW CONTROL VLV OPEN CLOSE VLV PER MEL ITEM 7 STEP 1 OPS CK LEFT AND RIGHT PACKS ON GROUND LEFT PACK IS CSDR UPS05845145Fitting · corrodedA-PIT CENTER TORQUE BOX BATHTUB FITTING AT FS 360 BETWEEN TORQUE BOX FRAME AND LONGERON34R HAS CORROSION. REMOVED CORROSION FROM BATH TUB FITTING AT STA 360 LONG 34R AND FOUND OUT OF LIMITS IAW SRM 51-1-8. REPLACED BATHTUB FITTING AT STA 360, 34R IAW 53-02-0
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