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 UPS04843018Frame · damagedINSPECTION TYPE: C2, STATION 1280 LONG 35R FWD UPPER FLANGE OF FRAME HAS A HOLE AT RADIUS. FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER AND FILLER IAW EO DC8-5310-11728-A.SDR UPS04843017Skin · corrodedINSPECTION TYPE: C2, FUSELAGE SKIN IS CORRODED BEYOND LIMITS STATION 120-160 UNDER ADF ANTENNA MOUNTING LOCATION AT LONG 36. REMOVED EXISTING DOUBLER AT NR 1 ADF ANTENNA, CUT OUT DAMAGE AT NR 2 ADF ANTENNA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSSDR IXXA0400101OSmoke Detector · brokenDURING ROUTINE TAKEOFF FROM MIAMI LOWER CARGO COMPT FIRE LIGHT ILLUMINATED. AFTER SHUTDOWN, MECHANIC DISPLAY SHOWED FALSE ALARM. FIRE DEPARTMENT VERIFIED NO HEAT IN (D) PIT. DOOR OPENED AND NOTHING FOUND. OVERWEIGHT INSPECTION REQUIRED. T/S SMOKE SYSTEM AND SDR UPS04842831Structure · corrodedCORROSION IN RIGHT MLG WHEEL WELL. REMOVED CORROSION FROM RMLG W/2 PANEL. UT AREA FOUND MIN MATERIAL TO BE .048" THICK. PERFORMED HFEC INSP NO CRACKS FOUND. ACCOMPLISHED INTERIM REPAIR PER EO DC8-5330-20826. DEFERRAL D285269 ASSIGNED AWAITING CLOSING LP AND CLSDR IXXA0400100OWire · brokenDURING CRUISE FROM KTOL, RADAR HAD A TENUATION NOISE BAND AT 20 MILE MARKER RUNNING COMPLETELY ACROSS DISPLAY IN ANY RANGE SELECTED. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED DEFECTIVE SPLICES BEHIND PLUG D10-61 IN RADISDR UPS04843054Web · corrodedINSPECTION TYPE:C3 CUT OUT WEB ON RIGHT STA 3 AT RIVET AREA AND CHECK FOR CRACKS. REMOVED AND REPLACED RIGHT STA 3 FITTING.SDR UPS04843056Web · corrodedINSPECTION TYPE: C3, LEFT MAIN LANDING GEAR WHEEL WELL, AFT AND BEHIND FLAP CABLE DRUM WEB IS CORRODED. REMOVED AND REPLACED LEFT STA 3 FLAP SUPPORT FITTING AND REPAIRED CORRODED WEB.SDR UPS04842886Fitting · gougedINSPECTION TYPE: C3, C-1 DOOR AFT LOWER GUIDE PIN FITTING WORN GOUGED. REMOVED DAMAGED FITTING IAW UPS SRM 51-3-0. DAC DWG NR 5754075. FOUND TO BE OUT OF LIMITS IAW UPS SRM 53-2-0. RECEIVED NEW FITTINGS P/N NR SP 003923. LOCATED AND DRILLED AND DEBURRED FITSDR IXXA0400099OLink · brokenDURING TAKE OFF, ON GEAR RETRACTION, CREW HEARD NOISE AND VIBRATION IN NOSE GEAR AREA UNTIL GEAR WAS LOWERED. CREW CYCLED GEAR, RETURNED AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ONGOING. AS SOON AS INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTSDR IXXA0400098OSeal · damagedDURING TAKE OFF, ON GEAR RETRACTION, CREW HEARD NOISE AND VIBRATION IN THE NOSE GEAR AREA UNTIL GEAR WAS LOWERED. CREW CYCLED GEAR, RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LT NOSE LANDING GEAR DOOR SEAL PARTIALLY HANGING OUT. THE DAMAGED SEAL SDR UPS04842885Seat Track · crackedINSPECTION TYPE: C3 STA 65-75 RBL 36 SEAT TRACK LOBES OBLONGED. REMOVED FLOOR PANELS FS 70-170 FOM. REMOVED SEAT TRACK,DAMAGED OUT OF LIMITS IAW SRM 53-2-3. DRILLED NEW SEAT TRACK AND TRACK SPLICE TO FIT. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED FLOORSDR UPS04843057First Aid Kit · wornINSPECTION TYPE: C3, C-1 DOOR FWD LOWER GUIDE PIN FITTING WORN. REMOVED FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. ORIG MAT .250 IAW DAC DWG 5754075 MAT REMAINING .130, LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D.SDR UPS04842718Battery Pack · inoperativeINSPECTION TYPE:N/A, COCKPIT AND ENTRY EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHECKED GOOD PER MM 33-50-01-2.SDR IXA04000970Actuator · crackedAIR RETURN, AFTER T/O SLOT LIGHT REMAINED ON AFTER FLAP RETRACTED. CYCLED, SLOT LIGHT OUT WHEN EXTENDED, ON WHEN RETRACTED. THEN 10 MIN INTO FLT SLOT LIGHT WENT OUT WITH FLAPS RETRACTED. NEVER EXCEEDED 230 KTS, LIGHT CAME BACK ON WHEN ON THE GROUND, WHILE TSDR UPS04842892Floorbeam · crackedINSPECTION TYPE: C3, CABIN OVERWING AREA FS 960 FLOORBEAM CRACKED UNDER CUSP LOWER SIDE OF LIGHTENING HOLE RT. REMOVED DOUBLE SEAT TRACK & SPLICES. REMOVED WEB, GRILL & FASTENERS FROM FLOORBEAM. CUT OUT DAMAGED FLOORBEAM IAW DC8 REO GO9893 MAT ID FOR SPLICESDR UPS04842661Link · brokenNR 4 BRAKE COMPENSATING LINK BROKE AND BRAKE SPUN. REMOVED AND REPLACED COMPENSATING LINK IAW MM 32-42-04-4, 32-33-00-2 ATTACHED LINK TO MLG 29046. SECURED LINK TO BRAKE IAW M/M 32-42-01-4 AND 32-33-002SDR UPS04842868Bracket · gougedINSPECTION TYPE: C-3, B-PIT DOOR LINK HINGES ARE GOUGED/ WORN PORTION ON AIRFRAME (NOT DOOR). REMOVED 2 EACH EXISTING C2 DOOR LINK HINGE FITTINGS. RECEIVED NEW FITTING 2 EACH PN 4654281. LOCATED AND DRILLED TRANSFER HOLES FOR NEW HINGE FITTINGS IAW SRM 51-1-2SDR UPS04842880Seat Track · wornINSPECTION TYPE: C3 SEAT TRACK E HAS WORN SCALLOPS AND LUGS BETWEEN FS 1400 AND 1410. BLEND AREA IAW UPS SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3, CUT OUT DAMAGE ON SEAT TRACK IAW EO 5340-7779B. ALODINED AND PRIMED CUT AREA, MAT ID PLUG SEAT TSDR UPS04842879Seat Track · wornINSPECTION TYPE: C3, SEAT TRACK (D) HAS WORN SCALLOPS AND LUGS BETWEEN FS 1560-1580 DOT NR D 973. BLENDED SEAT TRACK LUGS AND SCALLOPS, FOUND OUT OF LIMITS. OPEN FLOORBOARDS FROM FS 1495 TO 1690 LBL 16 TO LBL 32 IAW DC8 SRM 51-3-0 TO FOM, REMOVED SEAT TRACK SDR UPS04842878Seat Track · gougedINSPECTION TYPE: C3, STA 1580 RBL 18 SEAT TRACK LOBES GOUGED AND OBLONGED. BLENDED OUT DAMAGED LOBES AND FOUND OUT OF LIMITS. REMOVED 4 HOLES SEAT TRACK PLUG P/N DC8-53B-007-002 PO NR SP0906208 AND INSTALLED IAW EO NR 5340-7779-B. ALL IAW SRM 53-2-0, 53-2-3, ASDR UPS04842877Floorboard · corrodedINSPECTION TYPE: C3, STA 235 RBL 8 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORRODED FLOORBOARD. LOCATED NEW FLOORBOARD AND SPLICE PLATES. ALODINED AND PRIMED. INSTALLED FLOORBOARDS. ALL IAW SRM 51-3-0, 51-3-1, 51-1-8, AND 5SDR UPS04842876Floorboard · corrodedINSPECTION TYPE: C3, STA 280 RBL 1 FLOORBOARD CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED CORROSION SECTION OF FLOORBOARD FAB SPLICE PLATES. ALODINED AND PRIMED. INSTALLED SPLICE PLATES AND SECTION OF FLOORBOARD IAW SRM 51-3-0, 51-3-1, 5SDR UPS04842874Seat Track · wornINSPECTION TYPE: C3, STA 595-600 RBL 36 SEAT TRACK LOBES ELONGATED/OBLONGED. DAMAGE FOUND OUT OF LIMITS IAW SRM 53-2-3. REMOVED SEAT TRACK SECTION IAW SRM 51-3-0, DRILLED NEW SEAT TRACK SECTION TO FIT IAW SRM 51-1-24. INSTALLED IAW SRM 51-3-0 AND 51-3-1.SDR UPS04842869Door Frame · crackedINSPECTION TYPE: C3 B- PIT DOOR FRAME AFT SIDE CRACKED DOT NR Y52Y. MAT ID 2024-0 .071 PO 4255761 IAW SRM 52-2-0 AND 52-4-1. RECEIVED MATERIAL USED FOR REPAIR DOUBLER FROM HEAT TREAT. HEAT TREATED FROM 2024-T4 IAW TPS 1003 REV A. FABRICATED REPAIR DOUBLER ISDR UPS04842866Seat Track · wornINSPECTION TYPE: C3, SEAT TRACK-C HAS WORN LUGS AND SCALLOPS BETWEEN FS 1300-1315 (DOT D976). BLENDED OUT OF LIMITS IAW DC8 SRM 53-2-3. DIMENSION AFTER BLEND OUT OUT OF LIMITS. REMOVED DAMAGE FROM SEAT TRACK MAT ID FOR PLUG 7452952 -3 MAT ID FOR SEAT TRACK SDR UPS04842893Fitting · wornINSPECTION TYPE: C3, A PIT DOOR FWD UPPER LOCK PIN GUIDE FITTING WORN. REMOVED DAMAGED GUIDE FITTING IAW DC8 SRM 51-3-0. ORIG THICKNESS IS .250 REMAINING MAT .108 IAW DAC DWG 5754075. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 52-2-0. REC'D, LOCATED, DRILLED NESDR UPS04842891Fitting · wornINSPECTION TYPE: C3, A PIT DOOR AFT UPPER LOCK PIN GUIDE WORN. REMOVED DAMAGED FITTING DC8 SRM 51-3-0. ORIG MAT IS .250 IAW DAC DWG 5 754075. MAT REMAINING IS.104 AND FOUND TO BE WITHIN LIMITS IAW DC8 SRM 52-2-0. LOCATED AND DRILLED IAW DC8 SRM 51-1-24. ISDR UPS04842881Longeron · crackedINSPECTION TYPE: C3, FUSELAGE INTERIOR L 17 RT CRACKED FROM FS 1770 TO FS 1774. REMOVED L17R AT STA 1766 IAW SRM 51-1-20D. RECIEVED NEW LONGERON PN 5 649327-43. ALODINED AND PRIMED IAW SRM 51-1-8. INSTALLED LONGERON IAW SRM 51-1-21 AND 51-1-20D.SDR UPS04842883Web · corrodedINSPECTION TYPE: C3, AFT PIT WEB CORRODED BETWEEN FS 1200 L35R. REMOVED WEB FROM STA 1160 TO 1220, MAT ID FOR WEB AND SPLICES 7075T6 .125 PO NR 424554.3 IAW DWG NR 3753772, FAB WEB AND SPLICES. ALODINED AND PRIMED IAW SRM 51-1-8, INSTALLED WEB FROM STA 1160SDR UPS04842882Frame · corrodedINSPECTION TYPE: C3, FLC BILGE FRAME HAS CORROSION AT FS 600 RBL 12. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. CUT PART OF FRAME WITH CORROSION FAB NEW FRAME SECTION IAW DWG 5750886. SECTION HEAT TREATED TO 17075+6 FAB SPLICES AND STAPS. SPLICES HEAT TRESDR UPS04842867Skin · bentINSPECTION TYPE: C3, CABIN FWD LOWER CORNER OF L2 DOOR BENT AND TURN METAL. FAB ANGLE DOUBLER, Z-ANGLE SHIM, INNER SKIN SHIM, AND DOUBLER SKIN. ALODINED 2 SHIMS, DOUBLER INNER, PRIMED 2 SHIMS & DOUBLER INNER SKIN. RECEIVED HEAT TREAT. LOCATED & DRILLED. ASDR UPS04842578Lamp · inoperativeINSPECTION TYPE: AS, EMERGENCY LIGHT IN COURIER AREA INOP. RELAMPED EMERGENCY LIGHT.SDR IXXA0400081SPlate · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE AFT CENTER SECTION LWR PLATING CRACKED 1 INCH BETWEEN STA 1555.00 AND SB 1560.00. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8-53-2-1 FIG 7. REMOVED FASTENERS IAW DC8 SRM 51-1-21, PAGE 1. RSDR UPS04842549Battery Pack · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHTS INOP WHILE PERFORMING EMERGENCY LIGHT CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK. LIGHTS OPS CHECKED NORMAL REFERENCE MM 33-50-01-2.SDR IXXA0400088SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT WING OTBD FLAP LWR PART SKIN HAS INTERIM REPAIR AT XF 320.00. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 4 PAGE 2 OF 2. REMOVED LOWER PLATING WITH SDR IXXA0400084SFitting · crackedDURING A ROUTINE A-CHECK INSPECTION, FOUND ALT. CARGO COMPT FITTING CRACKED AT STA 1260.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW SRM 53-1-0 PAGE, PAIR SPECIFICATION NR 2003-05M DWG NR 3350223, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, TRSDR IXXA0400082SSkin · dentedDURING A ROUTINE A-CHECK INSPECTION FOUND B-CARGO DOOR HAS REPAIRS & DENTS ON EXTERIOR SKIN AND .2500 INCH BROKEN AT RT SIDE EDGE. REPAIRS WERE ACCOMPLISHED BY PERFORMING REPAIR IAW SRM 52-10 PG. 1, SRM 52-4-1 PG. 2 FIG. 1, REMOVED DAMAGED EXTERIOR SKIN IAW SSDR IXXA0400092SSkin Panel · damagedDURING ROUTINE C CHECK INSPECTION, FOUND LT INBD FLAP HAS INTERIM REPAIR ON UPPER PLATING, STA XW 89.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 1. REMOVED UPPER PLATING IAW DC8 SRM 51-1SDR IXXA0400087SDoor Frame · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND FWD ACCY COMPT FRAME CRACKED 1" AT STA 55.000, 1-24R. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 53-2-0 FIG 2. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PAGES 1, 2. REMOVED DAMAGED FRAME IAW DC8 SDR IXXA0400096SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE FORWARD CENTER SECTION INTERIM REPAIR AROUND STA FS 356.00, L-25L. REPAIR WAS ACCOMPLISHED. REMOVED EXTERNAL CIRCULAR DOUBLER IAW DC8 SRM 51-1-20D PG 21. FABRICATED NEW DOUBLER AND FINGER DOUBLER IAW DCSDR IXXA0400089SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT WING OTBD FLAP L/E UPPER PART HAS INTERIM REPAIR AT XE 415.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIG 4. REMOVED PLATING WITH INTERIM REPAIR IAW DC8 SSDR IXXA0400091SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND FWD FUSELAGE EXTERNAL AC POWER RECEPTACLE EXTERNAL SKIN HAS INTERIM REPAIR AT FS 32.000, L-31R TO L-32R. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIR IAW DC8 SRM 51-1-21 PAGES 1, 2. REMOVED DAMAGED ASDR IXXA0400090SAccess Door · damagedDURING ROUTINE C CHECK INSPECTION, FOUND FWD FUSELAGE (02 EA) INTERIM REPAIRS ON EXHAUST DOOR SYSTEM CORNERS AT STA 40,000 L-31L. REPAIRS WERE ACCOMPLISHED BY PERFORMING THE FOLLOWING REPAIRS IAW DC8 SRM 53-2-0 FIG 13. REMOVED INTERIM REPAIR IAW DC8 SRM 51-1SDR IXXA0400080SSkin · damagedDURING A ROUTINE A-CHECK INSPECTION, FOUND AFT SERVICE DOOR HAS INTERIM REPAIR ON UPPER AFT CORNER, STA 1660.000 L-11R TD L-98. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW SRM 53-2-0, FIG 76, TR NR 53-197 MAR 26/04 REMOVED INTERIM REPAIR IAW SRM 5SDR IXXA0400085SPlate · wornDURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBD FLAP L/E UPPER PLATING WEAR AT STA XF 211.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, DC8 SRM 57-7-1 PG 2 FIG 4. REMOVED WORN PLATING IAW DC8 SRM 51-1-21 PG 1 FABRICATSDR IXXA0400086SSkin · wornDURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBD FLAP UPPER SKIN HAS INTERIM REPAIR AT STA XF 282.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW DC8 SRM 51-1-0 PG 1 DC8 SRM 57-7-1 PG 2 FIG 4. REMOVED RT OUTBD FLAP FWD UPPER PLATING WITH ISDR UPS04842442Shear Tie · crackedINSPECTION TYPE:C1 STATION 1320 SHEAR TIE IS CRACKED BELOW LONG 21L. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 9755510 AND SRM 51-1-20D, 51-1-21.SDR UPS04842411Fitting · crackedINSPECTION TYPE:C1 LT WING FLAP LINK SUPPORT ASSY IS CRACKED AT FLAP HINGE 3. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM. 51-1-20D, 51-3-0.SDR UPS04842441Splice Plate · corrodedINSPECTION TYPE:C1 STATION 210 FINGER DOUBLER AND SPLICE PLATE ARE CORRODED BEYOND LIMITS BETWEEN LONG 21L TO 31L AND STATION 210 LONG 25R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER, SPLICE PLATE AND SPLICE FITTING IAW DWG 5779SDR UPS04842413Strap · brokenINSPECTION TYPE:C1 STATION 440 AT LBL 12 HAS STRAP BROKEN ON FLOOR WEB. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5633853 AND SRM. 51-1-21.
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