Douglas DC-8F-55
Service difficulty reports · 238
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 = 'DC8F55' 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 = 'DC8F55' 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 20001208AP007Longeron · crackedDURING B-CHECK INSPECTION, FOUND THE FOLLOWING, CRACKED LONGERON AT STATION 248, RECORDED ON NON-ROUTINE ITEM NR 3222. REPAIRED CRACKED LONGERON IAW SRM 53-2-2. (M)SDR 20001208AP005Fitting · corrodedDURING B-CHECK INSPECTION, FOUND THE FOLLOWING, CORRODED LONGERON FITTING AT BS 248, L-33R, RECORDED ON NON-ROUTINE ITEM NR 3257. REPLACED LONGERON SPLICE FITTING IAW SRM 51-1-20D, 51-3-0. (M)SDR 20001208AP004Door · openJUST AFTER TAKEOFF FROM KINGSTON CREW NOTICED THAT THE NLG DOOR STAYED OPEN. RETURNED FLIGHT BACK TO KINGSTON AND LANDED WITH A GROSS WEIGHT OF 190,000 LBS. UPON INSPECTION CONFIRMED OPEN DOOR. OPS CHECK NOSE GEAR DOOR LINKAGE IAW DC8 MM 32-2-6 FOUND OK. (SDR 2000ZZZX690Fitting · crackedLEFT HAND STA 98 FLAP ACTUATOR ATTACH FITTING (INSIDE PANEL 562L) HAS APPROXIMATELY 1 INCH CRACK IN IT. REMOVED AND REPLACED FITTING IAW DC-8 SRM'S 57-3-0, 51-3-2, AND 51-1-20D. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX684Door · damagedREPLACED COCKPIT DOOR. FABRICATED NEW COCKPIT DOOR PER EO 99-136 WITH APPROVED 8110-3 DATED 8-3-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX697Floor Panel · corrodedCORROSION EXISTS ON THE SURFACE OF ALL FLOOR PLANKS FROM STA 280 TO STA 1490 L21L TO L21R. REMOVED CORROSION BY CHEMICAL METHOD. TREATED AND PRIMED. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATSDR 2000ZZZX708Filler · missingDUE TO EXISTING REPAIR, DOUBLER ON LT FRONT SPAR (XRS 69.5) LOWER WING PLANK, TAPER FILLERS NEED TO BE FABRICATED TO COMPLETE SB 57-2OR5. FABRICATED FILLERS AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-22-99. REF: ZANTOP INTERNATIONAL AIRLINES,SDR 2000ZZZX676Skin · crackedDURING C-CHECK, FOUND .50 INCH LOWER L/E SURFACE AT INBOARD SLOT APPROXIMATELY XFS 213.5 LT WING. NDT TO ASSURE CRACK HAD BEEN STOPPED. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-11-99. REF: ZANTOP INTERNATIONAL SDR 2000ZZZX675Skin · crackedFOUND DURING C-CHECK. CRACK LOCATED AT INBOARD SLOT LOWER L/E, 1.50 INCHES LONG ON RT WING XFS 214.25. NDT CRACK TO ASSURE THAT CRACK HAD BEEN STOPPED. FABRICATED EXTERNAL DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 11-11-99. REF: ZANSDR 2000ZZZX694Spar · crackedLOWER FRONT SPAR HORIZONTAL LEG 10 INCH CRACK BS 680 - 26.5 INCHES TO 36.50 INCHES RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLER, DOUBLERS, AND INSTALLED IAW DC-8 SB 57-30R5. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX671Spar · crackedLOWER FRONT SPAR 1.50 INCH CRACK FS 680 LBL 34 INCHES Z AXIS -47 AND .50 INCH CRACK BS 680 LBL XCW 39 INCHES AND XCW 43 INCHES Z AXIS -47 INCH. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS, AND INSTALLED IAW DC-8 SB 57-30-R5. REF: ZANTOP INTERNATIONAL AISDR 2000ZZZM213Spar · crackedLOWER FRONT SPAR HORIZ LEG 10 INCHES CRACK FS 680 - 26.5 TO 36.5 INCH RBL CENTER WING TANK. CUT OUT DAMAGE. FABRICATED FILLERS, DOUBLERS AND INSTALLED IAW DC-8 S/B 57-30R5. (M)SDR 2000ZZZX681Fairing · damagedPANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX680Fairing · damagedPANEL 161V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX679Skin · damagedRT MLG DOOR CENTER STRUT/SEVERAL SCREWS STARTING TO PULL THROUGH SKIN. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZM260Skin · damagedSCREWS PULLING THROUGH SKIN L/E CENTER SECTION LOWER SURFACE XW454 LEFT WING. REPLACED SCREWS AND INSTALLED DIMPLE WASHERS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 11/05/99. (M)SDR 2000ZZZX670Tee · corrodedTHROUGH ACCESS HOLE 506C AND THROUGH INBOARD RIB CUT-OUT, INBOARD LOWER WING STR 63-72 AT STA XW.000 IN NR 3 MAIN TANK HAS CORROSION BETWEEN STRINGER. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FOUND T-CHORD OUT OF LIMITS IAW DC-8 SRM 57-2-0. REPLACED T-CHORD ISDR 2000ZZZX711Web · crackedFOUND DURING C-CHECK. RT FLAP EXHAUST GATE INBOARD END WEB CRACKED. CUT OUT INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 10-29-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX688Gilliner · damagedREPLACED MAIN CABIN GILLINER AND STRAPS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 7-24-99. REF: ZANTOP INTERNAL AIRLINES, INC. ZIAA.SDR 2000ZZZX682Fitting · corrodedPANEL 162V HAS SCREWS PULLING THROUGH. REPLACED SCREWS AND INSTALLED WITH DIMPLE WASHERS PER EO 99-136 WITH APPROVED 8110-3 DATED 11-5-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX677Skin · crackedINBOARD AILERON L/E PLATING AT STA XA 503.5 HAS A 2.5 INCH CRACK (EO). ROUTED OUT CRACK. FABRICATED DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 10-28-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZM215Web · crackedFOUND DURING C-CHECK, RIGHT FLAP EXHAUST GATE INBOARD END WEB CRACKED. CUT OUT CRACKED SECTION. FABRICATED NEW WEB AND INSTALLED PER EO NR 99-136 WITH APPROVED 8110-3, DATED 10/29/99. (M)SDR 2000ZZZX695Spar · crackedFOUND DURING C-CHECK. A 4.75 INCH CORROSION CRACK APPROXIMATE STA XCW 31.0 LT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. ROUTED OUT CRACK, BLENDED, NDT CONFIRMED CRACK, REMOVED. TREATED AND PRIMED. FILLED SEALER, CONTINUED THE INSTALLATION OF LOWER FRONT SPAR SDR 2000ZZZM214Spar · crackedFOUND DURING C-CHECK, A 4.75 INCH CORROSION CRACK APPROX STATION XCW 31 LEFT IN FRONT SPAR LOWER T-CAP VERTICAL LEG. ROUTED OUT CRACK, BLENDED, NDT CONFIRMED CRACK. REMOVED, TREATED AND PRIMED. FILLED SEALER CONTINUED THE INSTALLATION OF LOWER FRONG SPAR CASDR 2000ZZZX703Skin · crackedAFT LEFT COWL DOOR HAS 3 INCH CRACK OUTSIDE SKIN AT INLET SCOOP NR 3 ENGINE. STOP DRILLED, NDT CONFIRMED CRACK HAS BEEN STOPPED. WELDED CRACK AND NDT NO FLAWS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-8-99. REF: ZANSDR 2000ZZZX709Gear Tab · dentedRT ELEVATOR GEAR TAB DAMAGED DENT/CREASE. REPAIRED RT ELEVATOR GEAR TAB PER EO 99-136 WITH APPROVED 8110-3 DATED 10-15-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX669Ring · missingFOUND DURING C-CHECK. DOUBLER AROUND CIRCUMFERENCE OF FORWARD SIDE OF WIND SOCK HAS SECTION MISSING. NR 4 ENGINE. FABRICATED NEW SECTION, WELDED IN PLACE NDT WELD (NO FLAWS) PER EO NR 99-136 WITH APPROVED 8110-3 DATED 10-19-99. REF: ZANTOP INTERNATIONAL SDR 2000ZZZX704Duct · crackedNR 2 ENGINE INBOARD SIDE 1 O'CLOCK POSITION. FIRE EXTINGUISHER DUCT CRACKED AT ATTACH ANGLE. REMOVED DUCT, REPAIRED PER BOEING MEMO 99-00006 H AND EO 99-136 WITH APPROVED 8110-3 DATED 8-23-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZM235Drain · crackedFOUND DURING C-CHECK, LEFT MAIN GEAR WELL FORWARD DRAIN SPOUT CRACKED. NDT TO DETERMINE END OF CRACK, STOP DRILLED AND WELDED PER MIL-STD-2219. NDT NO FLAWS PER EO NR 99-136 WITH APPROVED 8110-3 DATED 10/01/99. (M)SDR 2000ZZZX696Skin · misrepairedLEFT HAND AFT ENTRY DOOR FUSELAGE SKIN CUT-OUT, PREVIOUS REPAIR IMPROPER STA 1400 - L21L. REMOVED EXISTING DOUBLER. FABRICATED NEW DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-4-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX689Frame · crackedFUSELAGE STATION 460 LONGERON 21R FRAME BENT AND FRAME CAP CRACKED. REMOVED DAMAGED SECTION OF FRAME. FABRICATED FRAME SPLICES IAW DC-8 SRM 53-2-0. TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW DC-8 SRM 51-1-20D. REF: ZANTOP INTERNATIONAL AIRLISDR 2000ZZZX702Rivet · shearedNR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR PNEUMATIC HEAT EXCHANGER. IT IS ACCEPTABLE TO USE AS IS, IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-9-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX699Heat Shield · crackedNR 1 ENGINE HEAT SHIELD FOR MAIN FUEL LINE CRACKED. STOP DRILLED CRACK, NDT TO ASSURE CRACK HAD BEEN STOPPED. WELDED ACCORDING TO MIL-STD-2219. NDT WELD NO FLAWS PER EO 99-136 WITH APPROVED 8110-3 DATED 8-25-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC.,SDR 2000ZZZX687Pipe · chafedFOUND DURING C-CHECK. NR 3 PYLON VENTILATION PIPE CHAFED. FABRICATED DOUBLERS AND WELDED IN PLACE IAW BOEING MESSAGE M-7200-99-07969 WITH APPROVED 8110-3 DATED 10-22-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX678Skin · crackedLEFT WING OUTBOARD FLAP SKIN JUST BELOW HINGE FITTING IS CRACKED STA XR 219. STOP DRILLED CRACKS, NDT TO ASSURE CRACKS HAD BEEN STOPPED. FABRICATED DOUBLER AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 9-15-99. REF: ZANTOP INTERNATIONAL AIRLINESSDR 2000ZZZX672Fitting · crackedRIGHT ELEVATOR NR 2 A-FRAME CRACKED. REMOVED AND REPLACED NR 2 POSITION A-FRAME RT ELEVATOR IAW DC-8 OHM 27-30-1. (X)SDR 2000ZZZX691Longeron · corrodedLONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AND REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60 PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIASDR 2000ZZZM210Longeron · corrodedLONGERON 6R STATION 1490 TO 1600 HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED AND REPAIR PER DC-8 SRM 53-2-2 PAGE 59/60 PER EO NR 99-136 WITH APPROVED 8110-3 DATED 8/11/99. (M)SDR 2000ZZZX700Spinner · crackedNOSE COWL CRACKED AT 6:00 O'CLOCK POSITION NR 4 ENGINE. CUT OUT PREVIOUS WELD, NDT TO ASSURE ALL CRACKS STOPPED. FABRICATED PLUG AND WELDED IN PLACE. NDT WELD NO FLAWS FOUND PER EO 99-136 WITH APPROVED 8110-3 DATED 8-31-99. REF: ZANTOP INTERNATIONAL AIRLSDR 2000ZZZX692Ring · crackedLONGERON 6R STA 1490 TO STA 1600, HAS AREAS OF EXFOLIATION. REMOVED CORROSION IAW DC-8 SRM 51-1-8. TREATED, PRIMED, AND REPAIRED PER DC-8 SRM 53-2-2 PAGES 59/60 PER EO 99-136 WITH APPROVED 8110-3 DATED 8-11-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIASDR 2000ZZZX683Leg · brokenLEFT MAIN W/W SAFETY NET LEG BROKEN OFF. WELDED NEW SECTION OF TUBING PER MIL-STD-2219. NDT WELD NO FLAWS FOUND PER EO 99-136 WITH APPROVED 8110-3 DATED 9-10-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZM211Ring · crackedINBOARD TOP SIDE OF TRANSLATING RING HAS CRACK NR 4 ENGINE. STOP DRILLED CRACK, NDT TO ASSURE CRACK STOPPED. FABRICATED DOUBLER AND INSTALLED PER EO NR 99-136 WITH APPROVED 8110-3 DATED 9/2/99. (M)SDR 2000ZZZX673Longeron · corrodedLONGERON 30, 31 RIGHT AT STA 320 HAD CORROSION. REMOVED CORROSION. FABRICATED FILLER, DOUBLER, AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 9-1-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX686Panel · corrodedLEFT OUTBOARD MOST UPPER SLOT DOOR BOTTOM INBOARD OF INBOARD ADJ SCREW HAS CORROSION XS 503.789. BLENDED OUT CORROSION, TREATED AND PRIMED. MAXIMUM UNDER CUT IN RIB IS DOWN .078 INCHES. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-SDR 2000ZZZX701Rivet · shearedNR 1 ENGINE RIVET HEAD SHEARED IN INTAKE FOR OIL COOLER. IT IS ACCEPTABLE TO USE AS IS. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO 99-136 WITH APPROVED 8110-3 DATED 9-9-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX706Outflow Valve · corrodedSUGAR SCOOP CORRODED (OUTFLOW VALVE) STA 1323. REMOVED CORROSION IAW DC-8 SRM 51-1-8. WELDED AREA, NDT TO ASSURE NO FLAWS (NONE FOUND) BLEND SMOOTH AND FINISHED PER FACTORY SPECS PER EO 99-136 WITH APPROVED 8110-3 DATED 8-14-99. REF: ZANTOP INTERNATIONAL ASDR 2000ZZZM229Fitting · crackedDURING B-CHECK INSPECTION, FOUND 20 INCH CRACK AT LEFT INBOARD CANOE FITTING AT STATION 98. REPLACED FITTING AT LEFT CANOE IAW MM 27-27-7. (M)SDR 2000ZZZM245Skin · corrodedDURING D-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION DAMAGE AT LEFT AND RIGHT RUDDER SKIN. REPAIRED CORROSION DAMAGE IAW FINE AIR EO NR 9808131, SRM 51-1-21. (M)SDR 2000ZZZX685Panel · corrodedOUTBOARD SLOT LEFT WING L/E HAS AREA OF EXFOLIATION XW 454. CUT OUT AREA OF EXFOLIATION. FABRICATED FILLER, DOUBLER, AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-13-99. REF: ZANTOP INTERNATIONAL AIRLINES, INC., ZIAA. (X)SDR 2000ZZZX674Skin · crackedLEFT WING CENTER L/E OTBD EDGE XFS 291.500 FWD VERTICAL PLATE CRACKED APPROXIMATELY 3 INCHES. REMOVED OUTBOARD END WEB. FABRICATED NEW SECTION AND SPLICE PLATE AND INSTALLED PER EO 99-136 WITH APPROVED 8110-3 DATED 8-20-99. REF: ZANTOP INTERNATIONAL AIRL
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