Douglas DC-8-62
Service difficulty reports · 2,778
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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 ARWA20011205EngineLOG PAGE 101856. DISCREPANCY: ON ADVANCING THROTTLE FOR TAKE OFF #4 ENGINE HUNG, CARRIED OUT ABNORMAL PROCEDURE FOR ENGINE HUNG WITH THRUST LEVER IN REVERSE ENGINE STARTED TO ACCELERATE. CANCELED REVERSE THRUST ENGINE CONTINUED TO ACCELERATE WITH THROTTLE CLOSSDR ARWA20011204Limiter · out of adjWHILE SETTING MAX POWER TAKEOFF, NR 4 ENGINE OIL PRESSURE MAXED OUT. PERFORMED ENGINE RUN IAW MM 71-00; FOUND OIL PRESSURE AT TAKEOFF 58 PSI WITHIN LIMITS IAW AA DC8 MM PAGES 5-35-90. ADJUSTED UPPER LIMIT TO 54 PSI IAW MM 79-20-5. OPS NORMAL, 41 PSI AT IDLESDR ARWA20011202Gyro · failedFIRST OFFICER'S COMPASS INOPERATIVE AFTER 1000 FEET. AIRCRAFT RETURNED TO KMIA AND PERFORMED OVERWEIGHT LANDING WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 PDI, INSTRUMENT AMPLIFIER AND DIRECTIONAL GYRO IAW MM 34-00. PERFORMED OPERATIONAL CHECK COMPASS SYSTSDR IXXA0100074OFan · defectiveENROUTE FROM KWA TO HIK, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT AND THE AFT PASSENGER COMPARTMENT WHEN THE RIGHT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDINSDR IXXA0100079SFloorbeam · crackedDURING ROUTINE C-CHECK INSPECTION A CRACK WAS DETECTED ON THE FLOORBEAM LEFT HAND FRAME ATTACHMENT PLATES AND CLIPS AT FS 320 TO 480. ACCOMPLISHED REMOVAL OF DAMAGED PLATES AND CLIPS. FABRICATED AND INSTALLED NEW ATTACHMENT PLATES AND CLIPS IN ACCORDANCE WITH SDR ARWA20011116Strap · crackedDURING C-CHECK INSPECTION, THE FOLLOWING WAS FOUND: NR 4 PYLON ACCESS DOOR 409 RT WITH TEMPORARY REPAIR, AFTER EVALUATION, FOUND CRACK ON OUTBOARD UPPER STRAP AT STA YUS 217. REPLACED STRAP IAW DC8 SRM 54-3-2,FIG 35, ITEM 5, NOTE 10. ACCOMPLISHED SB 54-70. SDR ARWA20011107Fitting · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: AFT CARGO COMPT STA 980 BULKHEAD LT STIFFENER WITH 1.5 INCH CRACK, NEAR MAIN CARGO DOOR COMPARTMENT FLOOR. REMOVED FITTING AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.SDR ARWA20011115StringerN/R 1080 - DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND: RH WING # 3 MAIN FUEL TANK INTERIOR BETWEEN STA. XRS 74 & SRS 107, STIFFENER 69 WITH 1.500" CRACK.CORRECTIVE ACTION: CUT-OUT DAMAGE SECTION OF STRINGER IAW DC8 SRM 57-2-2, PAGE 2, MADE SPLICE FITSDR ARWA20011114Floorbeam · crackedDURING "C" CHECK INSPECTION, STA 1120, X=10 RT SIDE, FLOORBEAM WEB WITH CORROSION. ACCOMPLISHED HFEC INSPECTION IAW DC-8 NDT MANUAL CHAPTER 06, FOUND CRACK OF 0.562 INCHES LENGTH DUE TO CORROSION & MATERIAL LOSS. TRIMMED OUT DAMAGED AREA; FABRICATED FILLER ASDR ARWA20011113Skin PanelN/R 1076 - DURING "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND: RH INBOARD FLAP LOWER SKIN WITH CRACK OF 0.500" BETWEEN STA. XW 92 & XW 104 FAIRING AREA.CORRECTIVE ACTION: REMOVED SKIN PANEL; FABRICATED NEW SKIN PANEL IAW AS ELEVEN INC. DWG # AS11321, SH 1 & SDR ARWA20011112PlateN/R 1068 - DURING "C" CHECK, THE FOLLOWING WAS FOUND: LH WING I/B FLAP LOWER SKIN WITH DENT AT STA. XW L7.CORRECTIVE ACTION: FOUND DENT OUT OF LIMITS IAW DC8 SRM 57-1-0; REMOVED DAMAGED AREA; FABRICATED NEW SOLID PLATING, FILLER & SPLICE STRAP IAW AS ELEVEN INSDR ARWA20011111Nozzle · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: NR 4 ENGINE EXHAUST NOZZLE SPLITTER WITH CRACK AT 2 O'CLOCK. REMOVED SPLITTER; FABRICATED NEW SPLITTER IAW DC8 SRM 78-3-2, FIG 8, ITEM C. PRIMED AND INSTALLED IAW DC8 SRM 51-1-8 & 51-1-21.SDR ARWA20011110FittingN/R 440 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH WING # 4 ALT. TANK INTERIOR STA. XRS 408.00 STRINGER # 58 END FITTING WITH CRACK.CORRECTIVE ACTION: OPENED FUEL TANK PLATE IAW DC8 MM 57-30-0; REMOVED & REPLACED FITTINGS IAW DC8 SRM 51-1-20D AND CSDR ARWA20011108PlateN/R 412 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: RH HORIZONTAL STABILIZER TIE STA. XE 77.000 AND 92.000 UPPER SKIN WITH INNER CORROSION.CORRECTIVE ACTION: REMOVED CORROSION IAW DC8 SRM 51-1-8; FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. REMOVED USDR ARWA20011106Skin · corrodedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: RT HORIZONTAL STABILIZER T/E BETWEEN STA 175.000 & STA 190.000 UPPER SKIN WITH INNER CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8; FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. REMOVED UPPER PLATING; FABRICSDR ARWA20011105PlateN/R 192 - DURING "C" CHECK INSPECTION, FOUND THE FOLLOWING: LH ELEVATOR LWR SKIN WITH CORRUGATION & OIL CANNING IN SEVERAL POINTS, BETWEEN STA. XE 28.343 AND XE 200.218.CORRECTIVE ACTION: REMOVED LH ELEVATOR LWR PLATING; FABRICATED NEW PLATING IAW AS ELEVEN, SDR IXXA0100080SClip · corrodedDURING ROUTINE C-CHECK INSPECTION CORROSION WAS DETECTED IN THE AFT CABIN FLOORBEAM AT STATION 1584. REMOVED DAMAGED FLOORBEAM AND INSTALLED NEW FLOOR SUPPORT AND CLIP NUTS IN ACCORDANCE WITH DOUGLAS STRUCTURAL MAINTENANCE MANUAL.SDR IXXA0100073OLine · looseENROUTE FROM AKJ TO AVB, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC QUANTITY SYSTEM. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO AVB FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECT THE AIRCRAFT LOCATING A LOOSE LINE ON THE RIGHT MASDR IXXA0100072OLinkage · dryDURING CLIMB FROM QPG TO DNA, THE FLIGHT CREW WAS UNABLE TO MAINTAING CABIN PRESSURIZATION. THE FLIGHT CREW DECLAIRED AND EMERGENCY AND FOLLOWED COMPANY PROCEDURES AND RETURNED TO QPG FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DISCRESDR ARWA0011015Uplock Switch · dirtyWHILE PERFORMING THE UPLATCH CHECK, LIGHT STAYED ILLUMINATED. COMPLETED ABNORMAL PROCEDURE AND RETURNED TO RODN. LUBRICATED LANDING GEARS AND UPLATCH MECHANISM, CLEANED AND SECURED LT MLG UPLATCH SWITCH IAW MM 32-60-0. OPERATION CHECK NORMAL. AIRCRAFT RETUSDR IXXA0100078SWing · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE AT STATION XW485 JUST OUTBOARD OF THE #4 PYLON. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL AND ENGINEERISDR ARWA0011014Pump · leakingIN CRUISE, HYDRAULIC QUANTITY DROPPED SLIGHTLY ABOVE EMERGENCY LEVEL. PERFORMED LOSS OF HYDRAULIC PRESSURE ABNORMAL EMERGENCY CHECKLIST. FLIGHT RESTRICTED TO MACH .65 AND 230 KIAS. CONTINUED WITHOUT INCIDENT. AFTER LANDING, MX FOUND AUX RUDDER PUMP LEAKINGSDR IXXA0100070OFan · defectiveENROUTE FROM RMS TO AVB, THE FLIGHT CREW SENSED AN ODOR IN THE COCKPIT WHEN THE LEFT RECIRCULATION FAN WAS OPERATING. THE FLIGHT CREW SECURED THE FAN AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO AVB FOR AN UNEVENTFUL LANDING. MAINTENACE INSPECT THE FAN WHICHSDR IXXA0100069OConnector · looseEN ROUTE FROM RMS TO AVB, AFTER THE LANDING GEAR WAS RETRACTED THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCSDR ARWA0011008Indicator · inoperativeCAPTAIN COMPASS INOP, RETURNED TO KMIA. REMOVED AND REPLACED PICTORIAL DEVIATION INDICATOR IAW MM 34-00. PERFORMED OPERATIONAL CHECK IAW 34-21-0, FOUND ALL SYSTEMS NORMAL.SDR ARWA0011007Sense Line · brokenNR 4 ENGINE LOW N1, N2, FF, HIGH EGT. INSPECTED NR 4 ENGINE FOUND PT7 LINE BROKEN. REMOVED AND REPLACED PT7 LINE IAW MM 70-30-2, PERFORMED ENGINE RUN UP AND FOUND NORMAL IAW DC8 MM 71-00.SDR ARWA0011005PinLOG PAGE 105745. DISCREPANCY:GEAR NOT LATCHED LIGHT ON, DOOR NOT LATCHED LIGHT ON, AIRCRAFT DIVERTED TO SJU AND ACCOMPLISHED AN UNEVENTFULL LANDING.AIRCRAFT PERFORMED AN OVERWEIGHT LANDING. CORRECTIVE ACTION:FOUND LEFT HAND MAIN GEAR RETRACT ACTUATOR PIN BROKESDR ARWA0011003Door · openAFTER GEAR RETRACTION LOUD NOISE AND VIBRATION COMING FROM NOSE WHEEL WELL. NOISE DISAPPEARED ON SHORT FINAL WITH GEAR DOWN. OVERWEIGHT LANDING AT PANC. UPON RETURN TO RAMP AFTER SPEAKING TO GROUND CREW FOUND NOSE GEAR DOORS WERE LEFT OPEN. RESET NOSE LANDSDR IXXA0100051OLine · defectiveDURING CRUISE FROM AVB TO RMS, THE FLIGHT CREW NOTICED THAT THE MAIN HYDRAULIC QUANTITY SYSTEM WAS DECLINEING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATE A DEFECTIVE SUPSDR ARWA0010902EngineLOG PAGE 106168. DISCREPANCY: ON CLIMB OUT OF KMIA NBR-3 ENG OIL PRESS LIGHT CAME ON AND OIL PRESS ERRATIC. PERFORMED PRECAUTIONARY SHUT DOWN. TOTAL WINDMILLING TIME 25 MIN. LANDING WT 240.0 LBS ENG SHUT DOWN AT 0536Z.AIRCRAFT LANDED WITHOUT INCIDENT. CORRECTISDR 0109Stop · looseAUTO PILOT PORPOSING IN LEVEL FLIGHT. DURING RT ELEVATOR CABLE ADJUSTMENT CHECKED TRAVEL TAB IN BOTH DIRECTION. WITH STICK FULL FORWARD THE LEFT ELEVATOR TAB ONLY GOES UP. THE RIGHT ELEVATOR TAB STAYS AT THE SAME POSITION. AFTER TROUBLE SHOOTING WE FOUND THESDR ARWA0010808Boot · out of adjDURING UPLATCH CK DOORS NOT LATCHED LIGHT ILUMINATED. ACCOMPLISHED ABNORMAL CK LIST AND NO HELP. SLIGHT VIBRATION ON COCKPIT FLOOR DURING ENTIRE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. CHECK ADJUSTMENT LT MAIN DOOR UPLATCH MECHANISM IAW MM 32-31-4, OPS CSDR ARWA0010803SealLOG PAGE 53334. DISCREPANCY: ON FINAL APPROACH SHUT DOWN #3 ENGINE DUE TO RAPID DROP IN OIL QUANTITY AND PRESSURE. CORRECTIVE ACTION: REMOVED HOUSING AND SEAL FROM FUEL BOOST PUMP DRIVE ON # 3 ENGINE GEAR BOX. INSTALLED SEAL (SEAL P/N 730376) AND HOUSING SDR ARWA0010720Bolt · shearedDURING FL 350 AND AS CRUISE ALTITUDE, THE NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND THE EGT BECAME ERRATIC. PERFORM CHECKLIST, SHUT DOWN ENGINE AT 0819Z, OIL PRESSURE READING 45 PSI. ON LANDING SMELLED BURNING SMELL IN COCKPIT. LANDED WITHOUT INCIDENT.SDR IXXA0100067SFloorbeam · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE FLOOR BEAM AT FUSELAGE STATION 879, LBL-61. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A BEAM FILLER AND REPAIR SPLICE ANGLES IN ACCORDANCE WITH DOUGLAS STRUCTURALSDR IXXA0100068SLongeron · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED AT FUSELAGE STATION 902 BETWEEN LONGERONS LONGERON 21R AND LONGERONS 20R. REPAIR ACCOMPLISHED REOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION REPAIR FILLERS AN EXTERNAL DOUBLERS IN ACCORDANCE WITHSDR IXXA0100038Uplock · lack of lubeEN ROUTE FROM HIK TO SUU, THE LANDING GEAR NOT LATCH LIGHT ILLUMINATED DURING THE LANDING GEAR UPLATCH CHECK. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO SUU FOR AN UNEVENTFUL LANDING. MAINTESDR ARWA0010605Engine · malfunctionedDURING TAKEOFF ROLL LOSS POWER ON NR 1 ENGINE. ABORTED TAKEOFF AT 70 KNOTS. REFERRED TO PERFORMANCE MANUAL BRAKE ENERGY CHART OK TO TAXI. CHECKED ALL TANK CROSSFEED VALVES AND SELECTOR VALVES FOR OPERATION FOUND NORMAL IAW MM 28-22-2,3. INSPECTED FUEL FILTSDR ARWA0010603Link Rod · defectiveAFTER TAKEOFF OUT OF KMIA AND RAISED THE LANDING GEAR EXPERIENCED HEAVY NOSE VIBRATION. RECYCLED LANDING GEAR, BUT DID NOT HELP. DECLARED EMERGENCY AND LANDED OVERWEIGHT WITH FULL FLAPS. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NLG DOOR LT FWSDR ARWA0010602Selector Valve · leakingHYDRAULIC PRESS LOST OUT OF SLLP. AILERON AND RUDDER POWER LIGHTS CAME ON, CHECKLISTS WERE COMPLETED AND DIVERTED TO SPIM. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HYDRAULIC SYSTEM SELECTOR VALVE IAW MM 29-10-18. OPERATIONAL CHECKED OK, NO LESDR ARWA0010601Oil Cooler · failedNR 4 ENGINE OIL TEMP ROSE TO 145 DEGREES, COMPLETED IN FLIGHT SHUT DOWN CHECKLIST, ENGINE WAS SHUT DOWN AT 22:45ZULU, WINDMILLING OIL PRESS 20 PSI. AIRCRAFT LANDED WITHOUT INCIDENTS. REMOVED AND REPLACED NR 4 OIL TEMP. INDICATOR FOR T/S. REMOVED AND REPLACESDR ARWA0010503O-Ring · failedON APPROACH TO TNCC (CURAZAO) LOSS OF HYDRAULIC FLUID. PERFORMED EMERGENCY CHECKLIST AS PER ARROW AIR PROCEDURE. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED O-RING FROM NR 3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE ELBOW IAW MM 29-10-12, LEAK CKD OK, OPERASDR IXXA0100025Belt · looseEN ROUTE FROM KWA TO HIK, AN ODOR WAS SENSED IN THE COCKPIT EMITTING FROM THE COCKPIT AIR CONDITIONING UNIT. THE FLIGHT CREW SECURED THE AIR CONDITIONER AND THE ODOR SUBSIDED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE SDR IXXA0100018Fan · defectiveEN ROUTE FROM HIK TO JON, THE FLIGHT CREW EXPERIENCED SMOKE IN THE AIRCRAFT. THE FLIGHT CREW SECURED THE RIGHT RECIRULATION FAN, THE SMOKE SUBSIDED. THE FLIGHT CONTINUED TO JON FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THESDR ARWA0010403Generator · malfunctionedNR 2 GENERATOR FIELD RELAY TRIPS AND WILL NOT RESET.CORRECTIVE ACTION: REMOVED AND REPLACED NR 2 GENERATOR OPERATIONAL CHECK NORMAL DURING RUN UP IAW MM 24-20-1 & 71-00SDR ARWA0010310Guide · looseRADAR WILL NOT PAINT WEATHER. AIRCRAFT DIVERTED TO MIAMI AND LANDED WITHOUT INCIDENT. TIGHTENED WAVE GUIDE; OPS CHECK NORMAL IAW MM 34-41-0.SDR IXXA0100010Hydraulic Line · defectiveDURING CLIMBOUT FROM AVB, THE FLIGHT CREW NOTICED A DECLINE IN THE MAIN HYDRAULIC QUANTITY AND PRESSURE INDICATION SYSTEMS. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURNED TO AVB FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT LOCATINGSDR ARWA0010307O-Ring · leakingAT TOP OF DESCENT NR 3 ENGINE OIL PRESSURE GAUGE FLICKERS FULL SCALE HIGH AND LOW AND NR 3 ENGINE OIL PRESSURE LIGHT FLICKERS ON AND OFF. ALL OTHER ENGINE PARAMETERS NORMAL. PRECAUTIONARY ENGINE SHUTDOWN. ON INSPECTION OF ENGINE, FOUND TOWER SHAFT SEAL LEAKSDR ARWA0010303Tire · separatedAFTER TAKEOFF FROM KATL ATC ADVISED FLIGHT 509 THAT A TIRE WAS LEFT ON THE RUNWAY, FLIGHT CREW REPORTED THE INCIDENT TO MIAMI MX AND CONTINUE TO TJSJ. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT TJSJ. ON POST FLIGHT INSPECTION IT WAS CSDR ARWA1000204O-Ring · tornHYDRAULIC SYSTEM LOSS DOWN TO STADPIPE, EMERGENCY CHECK, LIST C/W. RETURNED TO STATION. FOUND O-RING FROM RT AILERON ACTUATOR TUBING FITTING LEAKING. REPLACED O-RING IAW MM 20-60-0, OPS CHECK NORMAL. NO LEAKS NOTED, SYSTEM CHECK SATISFACTORY.
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