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.

SDR 99T64R003Nut Plate · strippedNR 3 PYLON REMOVEABLE PLANK HAS 5 SCREWS THAT WILL NOT TORQUE. OPENED HOLES TO .260 DIAMETER AND INSTALLED NAS 1670 PER EO DRAWING NR 98-026 ON 8110-3 DATED 10/27/98 UNDER WO NR 1308. (M)Jan 7, 1999 · N8969U · Doug DC862 · Nacelle/Pylon StructureSDR 99T64R002Skin · crackedRIGHT WING CENTER LEADING EDGE CRACKED ON OUTSIDE SEVERAL PLACES. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-036 ON 8110-3 DATED 11/09/98 UNDER WO NR 1308. (M)Jan 7, 1999 · N8969U · Doug DC862 · Wing, Plate/SkinSDR 99T64R001Skin · corrodedSTRIKE PLATE BULGING AROUND RIVETS AFT GALLEY DOOR R2. REMOVED CORROSION, FABRICATED DOUBLERS AND INSTALLED PER EO DRAWING NR 98-019 ON 8110-3 DATED 10/09/98 UNDER WO NR 1309. (M)Jan 7, 1999 · N8969U · Doug DC862 · Galley DoorsSDR ARWA981221Fcu · failedPNX - FLT 515 - BLOCK TURNBACK, ON RIGHT RUNUP, NR 1 ENGINE DIDN'T ACCELERATE. ALL INDICATIONS REMAINED IN IDLE. INDICATION WITH SLIGHTLY FLUCTUATING EPR NEEDLE. FELT ENGINE VIBRATING AND HEARD 'KNOCKING' NOISE. IMMEDIATELY BROUGHT THROTTLE BACK TO IDLE ADec 29, 1998 · N1804 · Doug DC862 · Fuel Control/Turbine EnginesSDR ARWA981219Gear Box · leakingMIA - FLT 941 - DURING CLIMB, FL 210, NR 4 ENGINE OIL PRESSURE DROPPED TO 35 PSI, PULLED POWER LEVEL BACK TO A LOWER POWER SETTING AND PRESSURE DROPPED TO 30 PSI OIL PRESSURE, LIGHT ILLUMINATED PULLED POWER LEVEL BACK TO IDLE, PRESSURE DROPPED DOWN TO 20 PSI ODec 23, 1998 · N8968U · Doug DC862 · Turbine Engine Reduction GearSDR ARWA981212Warning Light · illuminatedON TAXI, GENERATOR OVERLOAD LIGHT ILLUMINATED. ACCOMPLISHED OK LIST, LIGHT REMAINDED ON. AIRCRAFT RETURNED TO BLOCKS TRANSFERED TO DMI 9537 IAW MEL-24-24-CAT D.Dec 19, 1998 · N791AL · Doug DC862 · AC Indicating SystemSDR ARWA981211Pitot Tube · inopF/O PITOT HEAT INOP. REMOVED AND REPLACED CURRENT DETECTOR IAW DC-8 M/M 30-30-0. NO HELP. REMOVED AND REPLACED F/O PITOT TUBE IAW DC-8 M/M 30-30-0. PERFORMED PITOT STATIC LEAK CHECK IAW DC-8 M/M 34-12-0. OPERATION NORMAL.Dec 19, 1998 · N802BN · Doug DC862 · Pitot/Static Anti-Ice SystemSDR ARWA981206Switch · inopNR 1 ENGINE OIL PRESSURE LIGHT CAME ON IN FLIGHT, OIL PRESSURE AND QUANTITY OK, ENGINE SHUT DOWN AT 19:15 Z AS PER ARROW AIR ABNORMAL PROCEDURE, WINDMILLING PRESS, 17 PSI. REMOVED AND REPLACED NR 1 ENGINE OIL PRESS DIFF PRESS SWITCH, GROUND OPERATION CHECKED Dec 10, 1998 · N791AL · Doug DC862 · Engine Oil PressureSDR ARWA981203Pitot Syst · contaminatedDURING CLIMB-OUT, CAPT'S AIRSPEED INDICATOR READS 200 KTS AND F/O'S AIRSPEED INDICATOR READ 33O KTS. ACCOMPLISHED PITOT/STATIC LEAR TEST IAW MM 34-12-00. ALL PARAMETERS WITHIN LIMITS. PURGED SYSTEM PRECAUTIONARY MEASURE IAW 34-12-00 NR 1,2, ADC PITOT STACTIDec 8, 1998 · N8968U · Doug DC862 · Pitot/Static SystemSDR IH987518001Strut · damagedUPON DISASSEMBLY OF RT MLG STRUT FOR SEAL CHANGE, P/N 3598295 FOLLOWER FOUND TO BE FRACTURED CAUSING DAMAGE TO P/N 37673709-501 ADAPTER ASSY PACKING, P/N 3598375 SPACER. UPPER BEARING SPLIT, P/N 3598297 HEAD, PISTON, AND P/N 3598296 VALVE, REBOUND CHECK. VISDec 7, 1998 · N1804 · Doug DC862 · Main Landing Gear Strut/Axle/TruckSDR ARWA981204Wire · brokenGEAR DOOR NOT LATCHED, LIGHT ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE, LIGHT REMAINED ON. RETURNED TO MIAMI, NO FUEL DUMPED. FOUND BROKEN WIRE AT LT MLG DOOR UPLATCH SWITCH CANNON PLUG. REPAIRED SAME PER MM 20-50-00, OPS CHECK NORMAL PER MM 32-61-4.Dec 5, 1998 · N810BN · Doug DC862 · Landing Gear System WiringSDR ARWA981201Switch · inopPRECAUTIONARY SHUT DOWN DUE ENGINE OIL PRESSURE LIGHT FOR NR 1 ENGINE. FOLLOWED ABNORMAL CHECKLIST FOR ENGINE OIL PRESS. LIGHT ON, OIL PRESS 48 PSI, OIL TEMPERATURE MAX 105 DEGREE AFTER THROTTLE RETARD DURING CLIMB 80 PSI, OIL PRESS WHEN ENGINE WINDMILLING, Dec 2, 1998 · N810BN · Doug DC862 · Engine Oil Indicating SystemSDR ARWA981130Control Cable · brokenLT MLG DOOR UPLOCK FOLLOW UP CABLE BROKEN. FABRICATED CABLE AS PER SAMPLE IAW DACO M/M 91-10-42. OPERATION CHECKED NORMAL IAW M/M 32-12-1.Nov 24, 1998 · N8968U · Doug DC862 · Landing Gear Door Retract SectionSDR ARWA981128Connector · looseNOSE GEAR DOWN LIGHT DID NOT COME ON WHEN GEAR WAS EXTENDED. T/S FOUND DOWNLOCK SWITCH CANNON PLUG NOT SECURED. SECURED CANNON PLUG ON DOWNLOCK SWITCH, OPS NORMAL WITH GEAR SWING IAW 32-60-00.Nov 23, 1998 · N8968U · Doug DC862 · Landing Gear Position and WarningSDR ARWA981125Skin · corrodedC-CHECK, CORROSION FOUND BETWEEN LOWER SKIN AND RIBS ON LT I/B AILERON. REMOVED DAMAGED LOWER SKIN, FABRICATED REPAIR SKIN PER EO DRAWING NR 98-0924-3, ON 8110-3, DATED SEPT 25, 1998 UNDER WORK ORDER NR 1299.Nov 19, 1998 · N810BN · Doug DC862 · AileronsSDR ARWA981124Fasteners · misinstalledC-CHECK, NR 1 AND NR 2 PYLON'S HAVE WRONG FASTENERS INSTALLED IN PLANKS. OPENED REPLACEMENT HOLES TO .260 DIA AND INSTALLED PER EO DRAWING NR 98-014 ON 8110-3, DATED SEPT 28, 1998 UNDER WORK NR 1299.Nov 19, 1998 · N810BN · Doug DC862 · Nacelle/Pylon StructureSDR ARWA981123Frame · misdrilledC-CHECK, FRAME 1340 AT LT CUSP ABOVE FLOOR FITTING HAS DRILLED HOLE AT EDGE OF ANGLE. REMOVED DAMAGED AREA AND INSTALLED DOUBLERS PER DRAWING NR 98-012 ON 8110-3 DATED SEPT 09, 1998 UNDER WORK ORDER NR 1392.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Main, FrameSDR ARWA981122Floorbeam · corrodedC-CHECK, CORROSION BLISTERS ON FLOORBEAM TOP FWD EDGE AT NUT PLATES STA 1140 BETWEEN NR 2 AND NR 4 SEAT TRACKS. REMOVED ENTIRE UPPER SECTION AND INSTALLED DOUBLER PER EO NR 98-924-04 0N 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Main, Floor BeamSDR ARWA981121Doubler · corrodedC-CHECK, FINGER DOUBLER CORRODED AT CUSP LINE RT O/B OF F/E POSITION SUBFLOOR PRESSURE PANEL STA 168 TO 188. REMOVED DAMAGED SKIN AND INSTALLED DOUBLERS PER EO NR 98-0924 ON 8110-3 DATED SEPT 24, 1998 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981120Skin · crackedC-CHECK, 1.75 INCH CRACK IN LEFT WING SKIN UPPER SURFACE AT STA 74.86. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 57-2-1 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Wing, Plate/SkinSDR ARWA981119Spar · crackedC-CHECK, CENTER WING REAR SPAR LOWER CAP CRACKED BETWEEN FASTENERS STA 857 LBL 37, 51, 61 LT W/W. STOP DRILLED CRACKS AND INSTALLED DOUBLERS PER DRAWING NR 98-013 ON 8110-3 DATED SEPT 22, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Wing SparSDR ARWA981118Spar · crackedC-CHECK, WING REAR SPAR LOWER CAP CRACKED BETWEEN FASTENERS 33 TO 35 RIGHT OF CENTER LINE AND 53 TO 54 STA 857 RT W/W. STOP DRILLED AND INSTALLED DOUBLERS PER DRAWING NR 98-015 ON 8110-3, DATED SEPT 30, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Wing SparSDR ARWA981117Angle · crackedC-CHECK, 4.5 INCH CRACK TOP O/B PYLON TO WING ATTACH ANGLE NR 3 ENGINE STA YN336. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER EO NR 98-0924-06 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Nacelle/Pylon StructureSDR ARWA981116Angle · crackedC-CHECK, 8 INCH CRACK IN RADIUS OF TOP O/B PYLON TO WING ATTACH ANGLE NR 3 ENGINE STA YN310. STOP DRILLED CRACK, INSTALLED DOUBLER PER EO NR 98-0926-06 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Nacelle/Pylon StructureSDR ARWA981115Longeron · crackedC-CHECK, CORROSION BLISTER/CRACK ON LONGERON 27R FUSELAGE FRAME 1060. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER DRAWING NR 98-012 ON 8110-3 DATED SEPT 04, 1998 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Main, Longeron/StringerSDR ARWA981114Skin · corrodedC-CHECK, FUSELAGE SKIN CORRODED AND SHEAR FOOT BULGED AFT SIDE FUSELAGE FRAME STA 1320 BETWEEN LONGERON 29L-31L. REMOVED DAMAGED SKIN, FABRICATED DOUBLERS AND INSTALLED PER SRM 53-2-1 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Main, Plate/SkinSDR ARWA981113Skin · corrodedC-CHECK, LT HORIZ STAB L/E I/B LITE CORROSION AT FASTENERS XFS 180. REMOVED CORROSION AND INSTALLED DOUBLERS PER EO NR 98-0924-02 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR ARWA981112Skin · corrodedC-CHECK, LT HORIZONTAL STAB L/E CORROSION AT SCREW HOLES O/B END UPPER SURFACE. REMOVED CORROSION AND INSTALLED DOUBLERS PER EO NR 98-0924-02 ON 8110-3 DATED SEPT 24, 1998 UNDER WORK NR 1300.Nov 19, 1998 · N810BN · Doug DC862 · Horizontal Stabilizer, Plate/SkinSDR ARWA981111Rib · crackedC-CHECK, 3.5 INCH CRACK IN RT WING L/E RIB STA XFS 422. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 57-2-0 UNDER WORK ORDER NR 1299.Nov 19, 1998 · N810BN · Doug DC862 · Wing, Rib/BulkheadSDR ARWA981110Fitting · crackedC-CHECK, 4.5 INCH CRACK IN LONGERON SPLICE FITTING 25R STA 1090. REPLACED LONGERON FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981109Fitting · crackedC-CHECK, LONGERON 22R END CAP 6.5 INCH CRACK STA 990. REPLACED END CAP FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981108Fitting · crackedC-CHECK, LONGERON 23R END CAP FITTING 5 INCH CRACK STA 990. REPLACED FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981107Fitting · crackedC-CHECK, 6 INCH CRACK IN LONGERON END CAP FITTING 22L STA 990. REPLACED FITTING PER SRM 51-1-20 UNDER WORK NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981106Fitting · crackedC-CHECK, 1.25 INCH CRACK IN LONGERON 28L END FITTING STA 1530. REPLACED FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302.Nov 19, 1998 · N810BN · Doug DC862 · Fuselage Miscellaneous StructureSDR ARWA981105Frame · crackedC-CHECK, 2.5 INCH CRACK NR 4 PIT DOOR BOTTOM FRAME JUST ABOVE BUMPER. STOP DRILLED CRACK, INSTALLED DOUBLERS PER SRM 52-2-0 UNDER WORK ORDER NR 1299.Nov 19, 1998 · N810BN · Doug DC862 · Cargo/Baggage DoorsSDR ABXA9801084Switch · wornON GEAR EXTENSION, DID NOT GET LEFT MAIN GEAR (GREEN) LIGHT. RED GEAR UNSAFE LIGHT DID NOT ILLUMINATE. RECYCLED GEAR AND ACCOMPLISHED TOWER FLY-BY. LANDING WAS UNEVENTFUL. COULD NOT DUPLICATE DISCREPANCY. INSPECTED WIRING AND REPLACED MAIN GEAR DOWN SWITCNov 19, 1998 · N801AX · Doug DC862 · Landing Gear Position and WarningSDR ARWA981104Connector · looseNR 1 EGT FLUCTUATING AT 300 DEGREES, ADVANCING THROTTLE ON T/O ROLL. ABORTED T/O AND RETURNED TO RAMP. TIGHTEN CANNON PLUG ON EGT INDICATOR, OPS CHECKED NORMAL IAW M/M 77-20-00.Nov 18, 1998 · N802BN · Doug DC862 · Engine EGT/TIT Indicating SystemSDR TC8A98081Generator · out of adjustNR 2 GENERATOR WILL NOT CARRY A NORMAL LOAD, NO VOLTS AND FREQS. ADJUSTED FREQS ON GENERATOR, ENGINE RUN CARRIED OUT, OPS CHECKS NORMAL IAW 24-20-1.Nov 12, 1998 · N181SK · Doug DC862 · AC Generator-AlternatorSDR CKSA98711Filter · dirtyNASI SYSTEM PRODUCES BURNT ODOR IN CRUISE FLIGHT WITH BLEEDS IN LOW BOTH NASI'S ON. CLEANED NASI SYSTEM FILTERS AS PER DC-8 MM NASI MM 21-00-0. OPS CHECK GOOD ON GROUND.Nov 12, 1998 · N818CK · Doug DC862 · Cabin Pressure Control SystemSDR ARWA981103Actuator · not securedUNABLE TO PRESSURIZE CABIN ALTITUDE REACHED 10,000 A/C ALTITUDE WAS 10,000 NO DOOR WARNING LIGHTS ILLUMINATED. T/S FOUND REC FAN AIR SELECTOR VALVE ACTUATOR NOT SECURED. SECURED AIR SELECTOR VALVE ACTUATOR IAW M/M 21-21-5, OPS NORMAL ON RUN UP.Nov 12, 1998 · N791AL · Doug DC862 · Air Distribution FanSDR RRXA98561O-Ring · leakingLOSS OF HYDRAULIC QUANTITY AND HYDRAULIC PRESSURE. PERFORMED CHECK LISTS TO LOWER FLAPS. FOUND FITTING ON LT GEAR TRIM FITTING LEAKING. REMOVED FITTING, REPLACED O-RING, REINSTALLED FITTING, SERVICED HYD RES. PERFORMED GROUND RUN ON NR 2 AND NR 3 ENGINES, Nov 10, 1998 · N995CF · Doug DC862 · Landing Gear Retraction/Extension SystemSDR TC8A98078Prbc · dirtyON T/O ROLL AT 110 KTS, NR 2 ENGINE COMPRESSOR STALLED, ABORTED TAKEOFF. CHECKED BRAKES PER GOM. CLEANED AND LUBED PRBC VALVE. PERFORMED FLAG CHECK IAW MM 75-30-3. PERFORMED VISUAL INSPECTION OF INTAKE EXHAUST, NO DEFECTS NOTED.Nov 7, 1998 · N181SK · Doug DC862 · Compressor Bleed ValveSDR RRXA98557Floorbeam · misdrilledDURING MAINTENANCE VISIT, FOUND FLOOR SUPPORT AT FS 660 WITH MISDRILLED HOLES IN THE UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW T-CAP IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R51, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, Floor BeamSDR RRXA98556Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 920 WITH MISDRILLED HOLES AT LONGERON 16 LEFT. PLUGGED HOLES, FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98242, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98555Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 640 CRACKED BETWEEN LONGERONS 9 AND 10 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED ACMI SKETCH SK98500, DC-8 SRM 51-1-20D, 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98554Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 822 WITH MISDRILLED HOLE AT LONGERON 3 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98298, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98553Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 759 WITH MISDRILLED HOLE AT LONGERON 15 LEFT. FABRICATED AND INSTALLED REPAIR STRAPS AND CLIPS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R87, DC-8 SRM 51-1-20D, 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98552Frame · misdrilledDURING MAINTENANCE VISIT, FOUND 540 WITH MISDRILLED HOLE AT LT CUSP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE, FILLER AND SHIM IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R67 AND DC-8 SRM 51-1-1A.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98551Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 940 WITH MISDRILLED HOLE AT LONGERON 14 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R109, DC-8 SRM 51-1-1, 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 7, 1998 · N995CF · Doug DC862 · Fuselage Main, FrameSDR RRXA98550Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME 280 WITH MISDRILLED HOLE AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER, TIE CLIPS AND SHIMS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R31, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.Nov 6, 1998 · N995CF · Doug DC862 · Fuselage Main, Frame
Back to Douglas DC-8-62