Douglas DC-8-73

Service difficulty reports · 821

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 = 'DC873'
  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.

SDR DHL97801002Battery Pack · dischargedELECTRICAL BURNING SMELL NOTICED. FOUND EMERGENCY LIGHT BATTERY CHARGER CIRCUIT BREAKER TRIPPED. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD PER M/M 33-50-1.Mar 13, 1997 · N801DH · Doug DC873 · Emergency LightingSDR RRXA97050Longeron · crackedDURING C-CHECK, FOUND CRACK ON UPPER FLANGE ON LONGERON 26 LEFT AT, Y=200. REMOVED DAMAGE, FABRICATED INSERT REPAIR AND INSTALLED IAW TIMCO REO-02740 DTD 2/8/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).Feb 17, 1997 · N105WP · Doug DC873 · Fuselage Main, Longeron/StringerSDR RRXA97049Stringer Clip · crackedDURING C-CHECK, FOUND CRACK ON STRINGER CLIP ON RIGHT WING AT, XRS 22.730 AND BETWEEN STRINGERS 1R AND 2R. NEITHER REPLACEMENT PART NOR BLANK FORGING AVAILABLE FROM ACFT MFR. FABRICATED AND INSTALLED NEW CLIP IAW TIMCO REO-02751 DTD 2/11/97 AND FAA-DER APPROFeb 17, 1997 · N105WP · Doug DC873 · Wing Miscellaneous StructureSDR RRXA97048Longeron · corrosionDURING C-CHECK, FOUND CORROSION DAMAGE ON LONGERON 31R AT, Y=667 TO Y=671. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER REPAIR IAW TIMCO REO-02767 DTD 2/13/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).Feb 17, 1997 · N105WP · Doug DC873 · Fuselage Main, Longeron/StringerSDR RRXA97047Plating · dentedDURING C-CHECK, FOUND DENTS ON EXTERIOR SKIN AT, Y=160 AND BETWEEN LONGERONS 25L AND 27L. REMOVED DAMAGE, FABRICATED DOUBLER REPAIR AND INSTALLED IAW TIMCO REO-02717 DTD 2/5/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).Feb 17, 1997 · N105WP · Doug DC873 · Fuselage Main, Plate/SkinSDR RRXA97046Floorbeam · crackedDURING C-CHECK, FOUND 3 INCH CRACK ON FLOORBEAM UPPER FLANGE AT, Y=1600 AND X-45. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW TIMCO REO-02713 DTD 2/4/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).Feb 17, 1997 · N105WP · Doug DC873 · Fuselage Main, Floor BeamSDR RRXA97045Floorbeam · crackedDURING C-CHECK, FOUND 5 INCH CRACK IN FLOORBEAM UPPER FLANGE AT, Y=1580 AND X PLUS 45. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW TIMCO REO-02712 DTD 2/4/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).Feb 17, 1997 · N105WP · Doug DC873 · Fuselage Main, Floor BeamSDR DHL97801001Position Switch · failedRIGHT MAIN LND GEAR FAILED TO EXTEND NORMALLY. ABNORMAL PROCEDURES RUN. EXTENDED AFTER 2 CYCLES OF GEAR, NO INDICATION ON FORWARD GEAR IND AND SECONDARY IND, OK. REMOVED AND REPLACED RT POSITION INDICATING SWITCH IAW MM 32-60-0, OPS CHECK OK.Jan 18, 1997 · N801DH · Doug DC873 · Landing Gear Position and WarningSDR RRXA96165Light Ballast · failedDURING FLIGHT, THE FLT CREW OBSERVED AN INTERMITTENT SMELL OF HOT ELECTRICAL WIRING. MAINTENANCE TRANSFERRED THE GLARESHIELD LIGHTING BALLAST TO THE DMI LIST IAW MEL 33-1. MAINTENANCE REMOVED AND REPLACED THE FLUORESCENT BALLAST, OPERATIONAL CHECK OF LIGHTINNov 20, 1996 · N105WP · Doug DC873 · Flight Compartment LightingSDR RRXA96087Skin · crackedKMCN - DURING MAINTENANCE VISIT, FOUND CORROSION CRACK IN FUSELAGE SKIN AT Y=23 TO Y=55 BETWEEN LONGERONS 33R AND 34R. REMOVED DAMAGED AREA. FABRICATED FILLERS, DOUBLERS, AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH B31-R01. ACFT TT: 61,4Sep 19, 1996 · N105WP · Doug DC873 · Fuselage Main, Plate/SkinSDR DHL96801008Hose · rupturedAFTER DEPARTURE, NOTICED HYD QTY AT THE N OF NORMAL. COMPLETED ABNORMAL PROCEDURE AND COULDN'T DETECT ANY FURTHER LOSS. AFTER MONITORING QTY FOR 1 HOUR, NOTICED CONTINUING QTY LOSS. DECIDED ON PRECAUTIONARY LANDING AT DEN. AFTER LANDING AND TAXIING OFF RUNMar 15, 1996 · N801DH · Doug DC873 · Hydraulic System, MainSDR DHL96801007Press Switch · intermittentAILERON MANUAL CONTROL LIGHT ILLUMINATED AFTER TAKEOFF. ABNORMAL PROCEDURES FOLLOWED. REPLACED AILERON PCU PRESSURE SWITCH PER M/M 27-10 AND OPS CHECK OK.Jan 18, 1996 · N801DH · Doug DC873 · Aileron Control SystemSDR DHL95802004Brakes · grabbingREJECTED TAKEOFF, SUSPECTED FLAT TIRE OR BRAKE GRABBING. INSPECTED RIGHT TIRES AND BRAKE, NO FAULTS NOTED AND THE BRAKES OPERATE NORMALLY.Sep 20, 1995 · N802DH · Doug DC873 · Landing Gear Brake SystemSDR DHL95803002Coalescer Bag · serviceableCREW REPORTED STRONG ODOR OF CHLORINE IN CABIN. INSPECTED AIRCRAFT AND CARGO. REMOVED AND REPLACED COALESCER BAGS. PERFORMED ENGINE RUN, OPERATED HYDRAULIC, PNEUMATIC AND ELECTICAL SYSTEMS. COULD NOT DUPLICATE ODOR.May 11, 1995 · N803DH · Doug DC873 · Humidity Control SystemSDR 95ZZZW666Support Mlg · crackedDURING C-CHECK, FOUND RT MLG SUPPORT FITTING CRACKED. REPAIRED FITTING PER DOUGLAS S/B 53-61. TOTAL CYCLES 25,289.Mar 22, 1995 · N802DH · Doug DC873 · Wing, Landing Gear Attach FittingsSDR 95ZZZW665Support Fitting · crackedDURINK C-CHECK, RT INBOARD FLAP INBOARD SUPPORT FITTING FOUND CRACKED. REPLACED FITTING. TOTAL CYCLES 25,289.Mar 22, 1995 · N802DH · Doug DC873 · Wing, Control Surface Attach FittingsSDR 95ZZZW664Pylon Fitting · crackedDURING C-CHECK, NR 3 ENGINE PYLON SUPPORT FITTING FOUND CRACKED AT LOWER INBOARD RADIUS. REPLACED FITTING. TOTAL CYCLES 25,289.Mar 22, 1995 · N802DH · Doug DC873 · Wing, Nacelle/Pylon Attach FittingsSDR 95ZZZW663Skin · crackedDURING C-CHECK, FOUND NR 3 LOWER CARGO DOOR CUTOUT SKIN CRACKED FORWARD EDGE. REPAIRED PER DER DWG NR 239755124 DATED 3/14. TOTAL CYCLES 25,289.Mar 22, 1995 · N802DH · Doug DC873 · Fuselage Main, Plate/SkinSDR 95ZZZW662Corner Fitting · crackedDURING C-CHECK, NR 3 LOWER CARGO DOOR LOWER CORNER FITTINGS FOUND CRACKED. REPLACED FITTINGS. TOTAL CYCLES 25,289.Mar 22, 1995 · N802DH · Doug DC873 · Fuselage Miscellaneous StructureSDR 95ZZZW661Slot Door · puncturedDURING C-CHECK, FOUND LEFT INBOARD SLOT DOOR UPON SURFACE PUNCUTURED. REPAIRED PER DSRM 57-02-01 FIG 2A. TOTAL CYCLES 25,289.Mar 22, 1995 · N802DH · Doug DC873 · Leading Edge DevicesSDR 95ZZZX531Pump · lowSPOILER PUMP PRESSURE DROPPED TO 2450 PSI ON TAKEOFF ROLL. TAKEOFF REJECTED. SERVICED SPOILER RESERVOIR, SPOILER PUMP PRESSURE GOOD AT 3000 PSI.Jan 10, 1995 · N802DH · Doug DC873 · Drag Control System
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