Douglas DC-8-62
Service difficulty reports · 2,778
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 = 'DC862' 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 = 'DC862' 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 ARWA20030310HoseLOG PAGE 506081 & 506082. DISCREPANCY: ON LANDING AT FJDG, AIRCRAFT SUFFERED LOSS OF HYDRAULICS. EMERGENCY AIR BRAKE PRESSURE BOTTLE USED AFTER LANDING. CORRECTIVE ACTION: FOUND BROKEN HOSE IN RIGHT SIDE BOOGIE TRIM CYLINDER. REMOVED AND REPLACED HOSE IAWSDR IXXA0300023OWindshield · crackedDURING CLIMB OUT OF WRI COPILOTS WINDSHIELD CRACKED. CREW ELECTED TO RETURN TO WRI AND MADE AN UNEVENTFULL LANDING.SDR ARWA20030301Hose · leakingIN FLIGHT LOSS OF HYDRAULIC QUANTITY OF PRESSURE; PERFORMED APPROACH CHECKLIST. FOUND HYDRAULIC PRESSURE HOSE LEAKING AT NR 2 ENGINE. REMOVED AND REPLACED HYDRAULIC HOSE ON HYDRAULIC PUMP IN ACCORDANCE WITH MM 20-12-0. SERVICE HYDRAULIC RESERVOIR IAW MM 12SDR ARWA20030206Line · leakingIN FLIGHT ABOUT ONE HOUR OUT OF VTBU AFTER TAKE-OFF AIRCRAFT WAS LOSING HYDRAULIC FLUID. DID IN-FLIGHT TURNBACK, DUMPED FUEL AND LANDED BACK AT VTBU. RAN ALL APPROPIATE CHECK LISTS. FOUND NR 3 ENGINE HYDRAULIC PUMP SUPPLY LINE LEAKING. REMOVED AND REPLACESDR ARWA20030217Floorbeam · crackedDURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOOR BEAM SPLICE PLATES AT STATION 460 STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 460 IAW STC SA1063SO AND SA1377SO.SDR ARWA20030216Floorbeam · crackedDURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 440 STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 440 IAW STC SA1063SO AND SA1377SO.SDR ARWA20030215Floorbeam · crackedDURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 420 STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 420 IAW STC SA1063SO AND SA1377SO.SDR ARWA20030214Floorbeam · crackedDURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 400 STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 400 IAW STC SA1063SO AND SA1377SO.SDR ARWA20030213Floorbeam · crackedDURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 380, STRINGER 21. REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 380 IAW STC SA1063SO AND SA1377SO.SDR ARWA20030212Floorbeam · crackedDURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 360, STRINGER 21. CORRECTIVE ACTION: REMOVED AND REPLACED FLOORBEAM SPLICE PLATES AT STA 360 IAW STC SA1063SO AND SA1377SO.SDR ARWA20030210Floorbeam · crackedDURING AD INSPECTION (NOTE AD 2001-26-01/SID 53.08.FC4-10) FOUND CRACKS AT FLOORBEAM SPLICE PLATES AT STATION 340, STRINGER 21. REMOVED AND REPLACED FLOOR BEAM SPLICE PLATES AT STA 340 IAW STC SA1063SO AND SA1377SO.SDR IXXA0300012OO-Ring · leakingDURING CRUISE CREW NOTED HYD QTY DROPPING ABNORMALLY. CREW COMPLETED ABNORMAL CHECKLIST AND PROCEEDED TOWARDS QPG. WHILE ON FINAL APPROACH, AFTER ADVISING QPG ATC OF ABNORMAL CHECKLIST COMPLETION. QPG ATC DENIED LANDING CLEARANCE. CREW ELECTED TO PROCEED TSDR ARWA20030201Gyro · malfunctionedNR 2 RADIO MAGNETIC INDICATOR (RMI) HAS "OFF" FLAG AND CAPTAIN'S HORIZONTAL SITUATION INDICATOR (HSI) HAS "OFF" FLAG. FLAGS COME IN VIEW INTERMITTENTLY "CONTINOUSLY" AND IN TURNS. NO HEADING MOVEMENT WITH "OFF" FLAGS IN VIEW. REMOVED AND REPLACED NR 1 DIRECTSDR ARWA20030108Smoke Detector · malfunctionedLOWER CARGO SMOKE AND FIRE DETECTION MAINTENANCE LIGHT ON; CODE F15231: FALSE ALARM. LOWER CARGO AND FIRE DETECTOR MAINTENANCE LIGHT ON; ENTERED ON DMI 17416 IAW MEL 26-10-1-R-A CAT "C". REMOVED AND REPLACED SMOKE DETECTOR FORWARD CENTER; OPERATIONAL CHECK OSDR ARWA20030102Valve · inoperativeDURING TAXI, BEFORE TAKEOFF, ANTI SKID INOPERATIVE LIGHT ON WITH SWITCH IN (ON) POSITION. REMOVED AND REPLACED RT MAIN LANDING GEAR OUTBOARD ANTI SKID DUAL SERVO VALVE. BLED SYSTEM, OPS CHECKED AND FOUND NORMAL IAW MM.SDR IXXA030004OEngine · defectiveENROUTE FROM FJDG TO OBBI CREW NOTED #2 OIL QUANTITY DROPPED. CREW ELECTED TO FOLLOW ATI PROCEDURE AND SHUTDOWN THE #2 ENGINE. THE FLIGHT CONTINUED ON TO OBBI FOR AN UNEVENTFUL LANDING.OIL PRESSURE INDICATION ON #2 ENGINE REMAINED IN THE "POSITIVE"RANGE FOR DUSDR ARWA20021205O-Ring · leakingON FINAL APPROACH LOSS OF HYDRAULIC FLUID TO THE STAND PIPE. FOUND EMPENNAGE FILTER BOWL LEAKING AT MAGNETIC PLUG. REMOVED AND REPLACED O-RING LEAK CHECK NORMAL IAW MM.SDR ARWA20021204Limit Switch · faultyON UPLATCH CHECK RED DOORS LIGHT ILLUMINATED. FOUND NOSE LANDING GEAR DOWN LIMIT SWITCH FAULTY. REMOVED AND REPLACED LIMIT SWITCH IAW MM 32-60-0. ALL CONDITIONS ARE MET UNDER PARAGRAPH 1, ITEM B ON PAGE 201; SYSTEM OPERATIONS CHECK NORMAL ON GROUND IAW MM 3SDR IXXA0200140OGyro · faultyAFTER TAKEOFF FROM HIK CREW NOTED #2 "ADI" ATITUDE DIRECTIONAL INDICATOR ROLLING RANDOMLY. AS PRECAUTION CREW ELECTED TO RETURN TO HIK. AFTER AN UNEVENTFUL LANDING. MAINTENANCE TROUBLE SHOT AND REPLACED THE GYRO PER THE ATI DC-8 MAINTENANCE MANUAL AND E.O. 34-SDR ARWA20021203Hose · damagedLOST HYDRAULIC QUANTITY TOP OF DESCEND FOLLOWED BY ABNORMAL CHECKLIST AND PROCEDURES. CORRECTIVE ACTION: FOUND HYDRAULIC HOSE FROM PUMP ENGINE NR 2 DAMAGE. REMOVED AND REPLACED HOSE IAW MM, OPERATIONS CHECK OK IAW MM.SDR ARWA20021202Engine · malfunctionedPRECAUTIONARY NR 4 ENGINE SHUTDOWN; OIL QUANTITY LOW. TIME: 0605Z, N1: 37 PERCENT. OIL PRESSURE 0-10 PSI. ACCOMPLISHED INFLIGHT ENGINE SHUTDOWN CHECKLIST. REMOVED AND REPLACED NR 4 ENGINE IAW ARROW AIR TASK CARD DC8 UN-003 AND MASTER TALLY UNDER W/O 601627SDR IXXA0200116OO-Ring · leakingEN ROUTE FROM NKW TO BAH. FLIGHT CREW NOTED MAIN HYDRAULIC SYSTEM FLUID QUANITY DECLINING. CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED WITHOUT INCIDENT TO BAH. MAINTENANCE DISCOVERED O-RING LEAKING AT MAIN HYDRAULIC SYSTEM SELECTOR VALVE. REPLACED O-RING ANSDR ARWA20021201WindshieldLOG PAGE # 109140. DISCREPANCY: APPROACHING FL350, CAPTAIN'S WINDSHIELD DEVELOPED MULTIPLE CRACKS. CORRECTIVE ACTION: REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-10-2; ALSO CAPTAIN'S WINDSHIELD CONTROLLER IAW MM 30-41-1. FOUND NORMAL OPS CHECK.SDR ARWA20021108Cylinder · inoperativeIN FLIGHT, AFTER NORMAL GEAR RETRACTION , RED GEAR LIGHT ON AFTER UP LATCH CHECK. FOLLOWED ABNORMAL CHECKLIST. REMOVED AND REPLACED LEFT GEAR UP LATCH CYLINDER IAW MM, REMOVED AND REPLACED LEFT GEAR ACTUATING CYLINDER IAW MM. PERFORMED CHECK, NO LEAK, GOOD.SDR IXXA0200115OBushing · defectiveAFTER TAKEOFF FROM WRI ENROUTE TO BWI LANDING GEAR NOT LATCHED LIGHT ILLUMINATED AFTER GEAR RETRACTION. CREW PERFORMED LANDING GEAR UPLATCH CHECK, LIGHT REMAINED ILLUMINATED WITH RUMBILING NOISE NOTED FROM NOSE LANDING GEAR AREA. AIRCRAFT RETURNED TO WRI FOR ASDR IXXA0200114OStriker · looseENROUTE KWA TO HIK, THE GEAR DOOR NOT LATCH LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE GEAR, PERFORMED AN GEAR UPLOCK CHECK AND THE WARNING INDICATION EXTINGUISHED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEASDR ARWA20021106Engine · failedAT 2130Z, NR 2 OIL QUANTITY RAPIDLY DROPPED TO 1 GALLON, SUBSEQUENTLY OIL PRESSURE DROPPED TO 5 PSI AND OIL PRESSURE LOW LIGHT ILLUMINATED. PERFORMED IN FLIGHT ENGINE SHUTDOWN PROCEDURE IAW ABNORMAL CHECKLIST, WINDMILLING OIL PRESSURE. REMAINED AT 5 PSI. INSSDR ARWA20021105Receiver · inoperativeNR 2 VHF FIRST OFFICER SIDE COURSE DEVIATION INDICATOR INOPERATIVE, RETURNED TO MIAMI. REMOVED & REPLACED NR 2 VOR INSTRUMENT LANDING SYSTEM RECEIVER. SYSTEM OPERATIONS NORMAL IAW MM 34-52-0. AIRCRAFT RETURNED TO SERVICE.SDR ARWA20021104Pin · brokenON GEAR EXTENSION RIGHT HAND MAIN LANDING GEAR DROPPED DOWN WITH A LOUD BANG. FOUND RT MAIN LANDING GEAR CYLINDER RETRACT PIN BROKEN. REMOVED RT MAIN LANDING GEAR. ROUTED TO AAR LANDING GEAR SERVICES FOR REPAIRS. REPAIRED PER DC8 OHM TAPE REVISION 46, DATSDR ARWA20021102Heat Exchanger · failedNR 1 ENGINE OIL TEMPERATURE INDICATED 140 DEGREES FOR 15 MINUTES; THEN WENT TO 150 DEGREES THROTTLE IDLE, ALL OTHER PARAMETERS NORMAL, PERFORMED IN FLIGHT ENGINE SHUTDOWN CHECKLIST. WITH NR 1 ENGINE SHUTDOWN, OIL PRESSURE AT 20 PSI AND TEMPERATURE 60 DEGREES SDR ARWA20021004Engine · malfunctionedDURING CRUISE NR 3 ENGINE IDLE PRESS. LIGHT ILLUMINATED. OIL PRESS. 25 PSI, QTY, 1 GALLON. TEMP 135 DEGREES. ENGINE SHUT DOWN AT 1421Z. WINDMILLING OIL PRESSURE ZERO. REMOVED ENGINE, AND REPLACE WITH SERVICEABLE ENGINE. FUNCTIONAL TEST AND GROUND RUN-SDR ARWA20020914Splice · crackedDURING C-CHECK, MAIN CARGO COMPARTMENT FLOORBEAM SPLICES CRACKED AT STA 320, 340, 360, 380, 400, 420, 440 & 460 L-21 LONGITUDE.SDR ARWA20020903Transceiver · failedNR 2 RADAR ON CAPTAIN'S SIDE WILL NOT PAINT GROUND RETURNS OR WEATHER. NR 2 RADAR ON FIRST OFFICER'S SIDE WILL NOT PAINT GROUND RETURN OR WEATHER AND RADAR SPIKES. AIRCRAFT RETURNED TO DEPARTING BASE. REMOVED AND REPLACED NR 2 RADAR TRANSCEIVER IAW MM 34-0SDR ARWA20020902Bleed ValveLOG PAGE # 112879. DISCREPANCY: DURING TAXI NOTICED # 3 ENGINE COMPRESSOR STALLING ACCELERATION OF ENGINE. CORRECTIVE ACTION: REMOVED AND REPLACED # 3 ENGINE SURGE BLEED VALVE IAW DC-8 MM 75-30-3. OPERATIONS CHECKED OK; RUNUP FOUND NORMAL IAW DC-8 MM 71-00SDR ARWA20020901Cylinder · leakingAFTER LANDING IN SKCL LOSS OF HYDRAULICS PRESSURE AND QUANTITY. FOUND HYDRAULIC LEAK IN LEFT BOGIE TRIM CYLINDER. REMOVED AND REPLACED LEFT HYDRAULIC BOGIE TRIM CYLINDER AS PER ALTERNATE METHOD MM REF 32-33-1. SERVICED HYDRAULIC IAW MM 12-30-1 AND BLEED SYSSDR ARWA20020905Hinge · crackedDURING C-CHECK, MAIN CARGO COMPARTMENT DOOR HINGE LOBE WITH CRACK STA 460.SDR ARWA20020907Doubler · corrodedDURING C-CHECK, COCKPIT STA 133 - STA 148 RBL 63 SUB FLOOR FILLER DOUBLER WITH CORROSION & SHEARED RIVET. REMOVED CORROSION IAW DC-8 SRM 51-1-8, FOUND TO BE WITHIN LIMITS IAW DC-8 SRM 53-2-0; REMOVED AND REPLACED RIVET IAW DC-8 SRM 51-1-21.SDR ARWA20020908Fitting · crackedDURING C-CHECK, MAIN CARGO COMPARTMENT STA 840, L-22R, FITTING WITH CRACK. REMOVED AND REPLACED FITTING OF MAIN CARGO COMPARTMENT IAW DC-8 SRM 51-1-20D AND DC-8 SRM 53-1-0.SDR ARWA20020909Fitting · crackedDURING C-CHECK, MAIN CARGO COMPARTMENT STA 840, L-22L, FITTING WITH CRACK. REMOVED AND REPLACED FITTINGS OF MAIN CARGO COMPARTMENT STA 840, L-22L IAW DC-8 SRM 51-1-20D AND DC-8 SRM 53-1-0.SDR ARWA20020910Support Fitting · crackedDURING C-CHECK, RT WING L/E INTERIOR STA XW 239.743 INBOARD PYLON FRONT SPAR SUPPORT FITTING (FOOT STOOL) WITH CRACK. REMOVED AND REPLACED FOOT STOOL FITTING IAW BOEING MESSAGE INSTRUCTIONS ARW-MIA-02-00020H DATED 08/21/02, S/B DC8-57-84, DC8-A57-84 AND DC8-SDR IXXA0200050OO-Ring · damagedAFTER TAKEOFF FROM COF, THE FLIGHT CREW NOTICED A DROP IN THE HYDRAULIC QUANTITY AND THE OIL LOW LIGHT ILLUMINATED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO COF FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND LOCATED A DASDR ARWA20020906Hinge · crackedDURING C-CHECK, FORWARD ENTRANCE DOOR UPPER HINGE WITH 2 INCH CRACK. REMOVED FORWARD ENTRANCE DOOR IAW DC-8 MM 52-11-1, REMOVED AND REPLACED HINGE AND REINSTALLED FORWARD ENTRANCE DOOR IAW DC-8 MM 52-11-1. OPS CHECK NORMAL IAW DC-8 MM 52-10-0. NO LEAKS NOTESDR ARWA20020911Frame · crackedDURING C-CHECK, MAIN CARGO COMPARTMENT 980, L-18R FRAME WITH A 1.75 INCH CRACK. REMOVED AND REPLACED AREA, FABRICATED FILLERS ANGLES AND DOUBLER IAW AS ELEVEN INC DRAWING AS11451 SH 1 & 2, DATED 09/10/02; PRIMED FILLERS, ANGLES & DOUBLER IAW DC-8 SRM 51-1-/ ASDR ARWA20020704Duct · looseAFTER TAKEOFF, HEAVY VIBRATION / NOISE FELT COMING FROM THE COCKPIT FLOOR AREA, CAPTAIN'S SIDE. INSPECTED NOSE WHEEL WELL AREA AND FOUND LT AIR DUCT BOOT LOOSE FOR FLOW CONTROL SYSTEM; REINSTALLED BOOT AND SECURED CLAMPS AND CHECK RT SIDE TOO FOR CONDITION FOSDR ARWA20020604Cylinder · faultyAFTER T/O, HYD TEMP CLIMBED TO 83 DEG C, PERFORMED ABNORMAL CHECKLIST, NO CHANGE. RETURNED TO RAMP. REMOVED & REPLACED NR 3 ENG HYD DRIVEN PUMP, PERFORMED OPERATIONS CHECK, CHECKED NORMAL IAW MM 29-30-0. DURING TAXI FOR T/O, HYDRAULIC OIL TEMP CLIMBED TO 8SDR IXXA0200073SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE STATION XFS 178 TO XFS 285. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL FILLER AND REPAIR DOUBLER IN ACCOURDSDR IXXA0200072SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 857 TO 902 BETWEEN LONGERONS 10L TO 21L. REPAIR ACCOMPLISHED CORROSION REMOVAL AND FOUND TO BE WITHIN LIMITATIONS. CORROSION REMOVAL AT FUSELAGESDR IXXA0200028OFan · defectiveENROUTE FROM KWI TO AVB, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN BOTH RECIRCULATION FANS WERE OPERATING. THE FLIGHT CREW SECURED THE FANS AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT ANSDR IXXA0200071SWing · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING UPPER LEADING EDGE OUTBOARD OF NUMBER FOUR PYLON. REPAIR ACCOMPLISHED REOMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERMAL DOUBLER IN ACCORDANCE WISDR IXXA0200070SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 902, LONGERONS 14,17 AND 18 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL AND DETERMINED TO BE WITH LIMITATION IN ACCORDANCE WITH THE DOUGLAS STRUCTUR
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