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.

SDR ABXA9600369Sill · crackedDURING C-CHECK INSPECTION, DISCOVERED THE GROUND PNEUMATIC AIR CONNECTOR DOOR SILL CRACKED. FABRICATED DOUBLER FOR THE GROUND PNEUMATIC ACCESS DOOR THAT WAS CRACKED IAW ABX REA D853-13606MR.Mar 21, 1996 · N808AX · Doug DC862 · Fuselage Miscellaneous StructureSDR TC8A96009Ps4 Line · looseNR 2 ENGINE WILL NOT ACCELERATE PAST IDLE POWER WHEN THROTTLE IS ADVANCED. FOUND PS4 LINE LOOSE, TIGHTENED. ALSO, CLEANED PS4 FILTER, OPS CHECKED ON RUN UP AS PER MM 71-00 NORMAL. (M)Mar 20, 1996 · N803MG · Doug DC862 · Fuel Controlling SystemSDR 96ZZZM765Moisture Trap · fullON TAKEOFF ROLL AT 95 KNOTS NR 2 ENGINE COMPRESSOR STALLED THREE. ABORTED TAKEOFF WITHOUT INCIDENT. INSPECTED NR 2 ENGINE BLEED SYSTEM OK, PBRC OK. OK ENG EXHAUST AND INLET CHECK OK. FOUND MOISTURE TRAP FULL ON FCU. CLEANED AS REQUIRED, PERFORMED ENGINE GMar 20, 1996 · N802MG · Doug DC862 · Fuel Control/Turbine EnginesSDR IXXA9638Fuel Pump · leakingON DESCENT INTO SJU, THE NR 4 ENGINE WAS PRECAUTIONARILY SHUT DOWN DUE TO LOW OIL QUANTITY. ON THE GROUND IN SJU, MAINTENANCE DETERMINED THAT THE ENGINE FUEL PUMP GEARBOX DRIVE SEAL WAS LEAKING INTO ITS SPLINE CAVITY. THE DRIVE WAS RESEALED, AND THE ENGINE LMar 18, 1996 · N51CX · Doug DC862 · Engine Fuel PumpSDR 96ZZZX1631Bearing · brokenBEARING ON FLAP ACTUATOR CYLINDER BARREL RECEIVED BROKEN. SUSPECT DUE TO HIGH STRESS IN THIS AREA AS WELL AS POSSIBLE METAL FATIGUE.Mar 15, 1996 · Doug DC862 · Trailing Edge Flap ActuatorSDR ABXA9600309Bulkhead Fitting · leakingHYDRAULIC QUANTITY GAUGE INDICATION BEGAN DECREASING DURING DESCENT. EMERGENCY CHECKLIST WAS ACCOMPLISHED. HYDRAULIC FLUID QUANTITY STABILIZED AT THE STANDPIPE LEVEL. REPLACED NR 2 ENGINE HYDRAULIC PRESSURE LINE BULKHEAD FITTING. GROUND RAN ENGINE AND LEAMar 13, 1996 · N801AX · Doug DC862 · Hydraulic System, MainSDR IXXA9636Prox Switch · dirtyON TAKEOFF OUT OF BGTL, THE MLG 'NOT LATCHED' LIGHT CAME ON AFTER GEAR RETRACTION. THE GEAR WAS CYCLED, WITH NO CHANGE IN THE INDICATION. THE UPLATCH CHECK WAS NORMAL. AT KWRI, MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE PROBLEM TO BE CAUSED BY DIMar 12, 1996 · N21CX · Doug DC862 · Entrance StairsSDR ABXA9600272Retract Mech · malfunctionedLANDING GEAR UNSAFE LIGHT ILLUMINATED WHEN LANDING GEAR RETRACTED DURING CLIMBOUT. INDICATION CONFIRMED THAT THE RIGHT MAIN LANDING GEAR DOOR WAS NOT LATCHED. RECYCLED LANDING GEAR TWICE WITHOUT CHANGE. CHECKED WIRING FROM RIGHT PROXIMITY SWITCH TO PROXIMITMar 12, 1996 · N804AX · Doug DC862 · Landing Gear Door Retract SectionSDR ABXA9600249Retract Mech · lack of lubeDURING GEAR RETRACTION AFTER TAKEOFF, A LOUD NOISE WAS HEARD FROM THE NOSE GEAR AREA. THE LANDING GEAR RETRACTED AND THE LIGHTS WENT OUT. RECYCLED GEAR AND CONDITION REMAINED. FOUND LEFT NOSE LANDING GEAR DOOR UNLATCHED. CLEANED AND LUBED THE ACTUATOR MECHMar 11, 1996 · N805AX · Doug DC862 · Landing Gear Door Retract SectionSDR C1HA960011Engine · malfunctionedDURING TAKEOFF ROLLOUT AT APPROX 70 KTS, NOTED EPR DROP ON NR 1 ENGINE, FELT A SLIGHT YAW AT THE SAME TIME. ELECTED TO REJECT TAKEOFF COMPLETED THE SAME WITHOUT INCIDENT. INSPECTED NR 1 EPR IND. FOUND NO DEFECTS PERFORMED 1.84 POWER SETTING ON NR 1 AND NR 4Mar 9, 1996 · N802MG · Doug DC862 · Engine (Turbine/Turboprop)SDR TC8A96006Hyd System · req'd servON TAXI, FOUND HYDRAULIC QUANTITY INDICATOR TO STANDPIPE LEVEL. SERVICED HYDRAULIC RESERVOIR, CHECKED ALL SYSTEMS FOR LEAKAGE, NO LEAKS FOUND. (M)Mar 8, 1996 · N803MG · Doug DC862 · Hydraulic System, MainSDR TC8A96005Hydraulic Line · leakingSCDA/KMIA - FLT 06603 - LOSS OF HYDRAULIC QUANTITY, PRESSURE NORMAL. FOUND NR 3 ENGINE HYDRAULIC PUMP CASE DRAIN LINE LEAKING. REPLACED LINE, RUN-UP CHECKS NORMAL. SERVICED HYDRAULICS. (X)Mar 7, 1996 · N803MG · Doug DC862 · Hydraulic System, MainSDR ARWA9603005Skin · crackedRUDDER BOTTOM SURFACE, INSPECTION PANEL CUT OUT SKIN IS CRACKED. REMOVED AND REPLACED CRACKED SECTION IAW DER JOSSAIR, CO DRAWING ARW 950163-0014.Mar 5, 1996 · N810BN · Doug DC862 · Rudder, Plate/SkinSDR ARWA9603004Skin · corrodedCORROSION ON RT WING LOWER SURFACE AT WING STA XFS 472.750. REMOVED CORRODED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DER JOSSAIR, CO EO ARW 960051-0024.Mar 5, 1996 · N810BN · Doug DC862 · Wing, Plate/SkinSDR ARWA9603003Panel · corrodedRT WING UPPER SURFACE BETWEEN WING STA XRS 659.000 AND XRS 727.000 HAS CORROSION AROUND FASTENERS' HEADS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DAC 96-02-26-003 AND 96-03-01-002.Mar 5, 1996 · N810BN · Doug DC862 · Wing, Plate/SkinSDR ARWA9603002Skin · corrodedLT WING UPPER SURFACE BETWEEN WING STA XRS 624.000 AND XRS 693.000 CENTER SKIN AREA HAS CORROSION. BLENDED OUT CORROSION, INSTALLED DOUBLER IAW DAC FAX 96-02-29-010 AND 96-02-06-004.Mar 5, 1996 · N810BN · Doug DC862 · Wing, Plate/SkinSDR ARWA9602001Computer · malfunctionedYAW DAMPER SWERVED AIRCRAFT, RETURNED TO MIAMI. YAW DAMPER AT 37,000, SEVERE INFLIGHT UPSET, LEFT DEFLECTION. ACCOMPLISHED WIRING CONTINUITY AND INTEGRITY CHECK OF THE TRANSFER VALVE AND POSITION SENSOR FROM YAW CHANNEL TO RUDDER PACKAGE. REPLACED YAW COMPUFeb 24, 1996 · N1803 · Doug DC862 · Autopilot ComputerSDR 96ZZZM272Unsafe Light · illuminatedRIA FLT NR 7700 MIA - DOVER AIRCRAFT RETURNED TO MIA AFTER TAKEOFF WHEN MLG DOOR UNSAFE LIGHT ILLUMINATED. IN MIA, AIRCRAFT JACKED AND RIGGED LEFT DOOR ACTUATOR. OPS CHECK OK, AIRCRAFT RETURNED TO SERVICE. (M)Feb 11, 1996 · N8974U · Doug DC862 · Landing Gear Position and WarningSDR ABXA9600185Battery Pack · dischargedDURING PREFLIGHT INSPECTION, FOUND EMERGENCY EXIT LIGHT CONTROL CIRCUIT BREAKER POPPED. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. EMERGENCY LIGHT SYSTEM OPS CHECKED GOOD IAW DC-8 MM.Feb 7, 1996 · N805AX · Doug DC862 · Emergency LightingSDR 96ZZZX905Skin · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT LOWER AREA, STR 34R BETWEEN STA 1220 AND STA 1240, FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 51-1-0. (X)Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/SkinSDR 96ZZZX904Doubler · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT, STR 21R BETWEEN STA 1160 AND STA 1180, FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH E.O. NR RCH D85310-6124. (X)Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX903Doubler · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT STR 21R BETWEEN STA 1160 AND STA 1180, FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER SRM 53-2-5. (X)Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX902Doubler · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT, LT SIDE STR 21L BETWEEN STA 1240 AND STA 1260, FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH E.O. D85310-6124, REV 1.Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX901Doubler · corrodedLEVEL 2 CORROSION/AFT CARGO COMPARTMENT, LT SIDE STR 21L, BETWEEN STA 1240 AND STA 1260, FLOOR SUPPORT CORRODED. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PER RICH DRAWING D85310-6124. (X)Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Miscellaneous StructureSDR 96ZZZX900Skin · corrodedLEVEL 2 CORROSION/LOWER FUSELAGE IS BULGED WITH CORROSION AT FS 540R BETWEEN LONGERONS 35R AND 34R BELOW FORWARD CARGO DOOR SILL PLATE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 52-2-1.Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/SkinSDR 96ZZZX899Skin · corrodedLEVEL 2 CORROSION/2 SMALL SKIN BULGES JUST AFT OF NR 4 PIT DOOR FS 1290, STR 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1.Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/SkinSDR 96ZZZW49Skin · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT LOWER AREA STRINGER 34R BETWEEN STA 1220 AND 1240 FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-1-0.Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/SkinSDR 96ZZZW48Stringer · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT STRINGER 21R BETWEEN STA 1160 AND 1180 FLOOR SUPPORT HAS CORROSION. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER SMR 53-2-5.Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZW47Stringer · corrodedLEVEL 2 CORROSION, AFT CARGO COMPARTMENT LEFT SIDE STRINGER 21L BETWEEN STA 1240 AND 1260 FUSELAGE SKIN HAS CORROSION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER RICH EO D85310-6124 REV 1.Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Longeron/StringerSDR 96ZZZW46Skin · corrodedLEVEL 2 CORROSION, LOWER FUSELAGE IS BULGED WITH CORROSION AT FS 540R BETWEEN LONGERONS 35R AND 34R BELOW FORWARD CARGO DOOR SILL PLATE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER SRM 52-2-1.Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/SkinSDR 96ZZZW45Skin · corrodedLEVEL 2 CORROSION, TWO SMALL SKIN BULGES JUST AFT OF NR 4 PIT DOOR FS 1290 STRINGER 28R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-2-1.Feb 5, 1996 · N8974U · Doug DC862 · Fuselage Main, Plate/SkinSDR C1HA960008Reg · malfunctionedAT 70 KNOTS NR 2 ENGINE COMPRESSOR STALLED. ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 ENG REGULATOR AND RELIEF VALVE. OPS CHECK GOOD ON HIGH SPEED TAXI. (M)Feb 1, 1996 · N802MG · Doug DC862 · Turbine Engine Compressor SectionSDR 96ZZZM372Relief Valve · malfunctionedAT 70 KNOTS NR 2 ENGINE COMPRESSOR STALLED. ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 ENG REGULATOR AND RELIEF VALVE. OPS CHECK GOOD ON HIGH SPEED TAXI. (M)Feb 1, 1996 · N802MG · Doug DC862 · Turbine Engine Compressor SectionSDR IXXA9606Air Distr · odorEN ROUTE BETWEEN LPLA AND KWRT, THE AIR CONDITIONING SYSTEM INTERMITTENTLY PRODUCED THE STRONG SMELL OF OIL IN THE COCKPIT. THE FLIGHT CREW SUSPECTED A TURBOCOMPRESSOR OIL SEAL FAILURE. INSPECTION ON THE GROUND IN KWRT SHOWED THE TC'S TO BE NORMAL, WITH NO LJan 31, 1996 · N21CX · Doug DC862 · Air Distribution SystemSDR C1HA960009Ps4 Line · cloggedAT TAKEOFF ROTATION NR 2 ENGINE COMPRESSOR STALLED 4 OR 5 TIMES. REDUCED NR 2 THRUST LEVER TO CLEAR THE CONDITION. ADVANCED THRUST LEVER BACK TO NORMAL MCT, ALL PARAMETERS NORMAL. NO FURTHER ABNORMALITY. CLEARED PS4 LINE AND RESECURED. ENGINE RUN PER MM 7Jan 31, 1996 · N802MG · Doug DC862 · Turbine Engine Compressor SectionSDR IXXA9604Ballast · failedEN ROUTE BETWEEN PDX, AND OAK, THE FLIGHT CREW NOTED THE SMELL OF SMOKE COMING FROM THE ENGINE INDICATION PANEL. IN OAK, MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT A FLUORESCENT LIGHTING BALLAST HAD FAILED, EMITTING THE SMELL. THE FLUORESCENT LIGJan 27, 1996 · N735PL · Doug DC862 · Passenger Compartment LightingSDR ARWA9601003Skin · crackedDURING POST FLIGHT INSPECTION, AN 8.5 FUSELAGE SKIN PUNCTURE WAS NOTED AT FS 288.00 TO 297.00 AT LONGERON 32R. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER I/A/W SRM 53-2-1 FIG 7. SEALED AREA I/A/W SRM 51-1-11.Jan 27, 1996 · N802BN · Doug DC862 · Fuselage Main, Plate/SkinSDR IXXA95134Grnd Shift Mech · out of rigON DEPARTURE OUT OF EWR, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE 'RETRACT' POSITION. THE AIRCRAFT APPEARED TO BE STUCK IN THE 'GROUND' MODE. THE AIRCRAFT RETURNED TO EWR FOR MAINTENANCE. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE FACILITY WHERE THE NOSJan 3, 1996 · N51CX · Doug DC862 · Landing Gear Retraction/Extension SystemSDR C1HA960005Switch · failedCABIN ALT. WARNING HORN FAILED TO COME ON DURING ENTIRE LOSS OF PRESSURIZATION. FOUND CABIN LOW PRESSURE WARNING HORN SILENCE SWITCH FAILED OPEN AND BAD CONNECTION ON CABIN LOW PRESSURE SWITCH. REMOVED AND REPLACED SILENCE SWITCH AND REPAIRED CONNECTION SYSTJan 3, 1996 · N802MG · Doug DC862 · Cabin Pressure Control SystemSDR C1HA960004Bullet · snow packedPRIOR TO REACHING V1, NR 2 ENGINE COMPRESSOR STALLED. VISUALLY INSPECTED NR 2 ENGINE INTAKE. FOUND SNOW ON NOSE BULLET. REMOVED SNOW, INSPECTED COMPRESSOR, TAIL PIPE, NO DEFECTS NOTED. RAN ENGINES 2 AND 3 ON TAKEOFF POWER. IAW CHAPTER 71, NO DEFECTS NOTEDJan 3, 1996 · N802MG · Doug DC862 · Turbine Engine Air Inlet SectionSDR ARWA9701001Seal · leakingAFTER DEPARTURE, SHUT DOWN NR 1 ENGINE DUE TO HIGH OIL CONSUMPTION. FOUND ENGINE FUEL PUMP AND NASH PUMP GARLOC SEALS LEAKING. REMOVED AND REPLACED GARLOC SEALS, NO LEAK NOTED.Jan 3, 1996 · N810BN · Doug DC862 · Turbine Engine Accessory DriveSDR ABXA9600006Door · damagedTHE GEAR UNSAFE LIGHT ILLUMINATED IN-FLIGHT. RECYCLED GEAR WITH NO EFFECT. DOWN INDICATIONS NORMAL. GEAR DOOR LATCH LIGHTS WERE CHECKED AND LEFT DOOR INDICATED UNLATCHED. FOUND LEFT LANDING GEAR DOOR DAMAGED DUE TO ICE ACCUMULATION. REPAIRED DOOR IAW ABX Jan 3, 1996 · N803AX · Doug DC862 · Landing Gear DoorsSDR C1HA96002Oxygen Line · brokenDEPLOYED MASK IAW RAPID CABIN DEPRESSURIZATION CHECK LIST AND MASK DID NOT DEPLOY. CABIN CLIMBED THROUGH 16,000 FEET AND DID NOT DEPLOY AUTOMATICALLY. FOUND OXYGEN LINE BROKEN. REMOVED AND REPLACED. OPS CHECK GOOD. (X)Jan 2, 1996 · N802MG · Doug DC862 · Passenger Oxygen SystemSDR C1HA960001Outflow Valve · froze upAT TOP OF DESCENT, PRESSURIZATION STARTED TO CLIMB THAT WAS UNCONTROLLABLE IN MAN. AND AUTOMATIC. LEVER FELT CABLES WERE BOUND. FOUND OUTFLOW VALVE COMPARTMENT WET. REPAIRED AFT LAV. PLUMBING DRIED OUT LPS3 OUTFLOW COMPARTMENT. DRIED AND LUBED OUTFLOW VALJan 2, 1996 · N802MG · Doug DC862 · Pressure Regulator/Outflow ValveSDR ABXA9501047Prox Switch · out of adjustUPON GEAR RETRACTION FROM ILN, GEAR NOT LATCHED LIGHT REMAINED ON. DISCRIMINATOR PANEL (F/E STATION) INDICATED RIGHT MAIN DOOR NOT LATCHED. CYCLED LANDING GEAR WITH NO DIFFERENCE. PROCEEDED TO DESTINATION AT FL 330 AND M.65. COMPLIED WITH MAB DC-8-32-6. MDec 28, 1995 · N804AX · Doug DC862 · Landing Gear Position and WarningSDR 96ZZZX316Filter · cloggedMAO - ON FLIGHT TO MAO, AIRCRAFT DIVERTED TO SJU DUE TO EXCESSIVELY HIGH ENGINE FUEL PRESSURE ON NR 1 AND NR 4 ENGINES. REMOVED NR 1 AND NR 4 ENGINE FUEL TEMP REGULATOR FILTERS. FOUND TO BE CLOGGED. INSTALLED NEW FILTERS AND ENGINE RUN-UP CHECKED NORMAL. ADec 23, 1995 · N810BN · Doug DC862 · Engine Fuel DistributionSDR ABXA951045Prox Box · malfunctionedAFTER TAKEOFF FROM TPA, RED GEAR UNSAFE LIGHT REMAINED ON. NO LIGHT WAS ON IN ANY GEAR/DOOR POSITION. RECYCLED GEAR AND PERFORMED ABNORMALS IAW DC-8 OPS MANUAL. NO HELP. REPLACED MAIN LANDING GEAR DOOR PROXIMITY BOX AND CLEANED UPLATCH ASSEMBLIES ON BOTH GDec 22, 1995 · N804AX · Doug DC862 · Landing Gear Position and WarningSDR ABXA9501044Connector · dirtyAFTER TAKEOFF FROM ILN, GEAR NOT LATCHED LIGHT REMAINED ILLUMINATED AND RIGHT MAIN GEAR DOOR NOT LATCHED WAS ILLUMINATED. RECYCLED GEAR AND PERFORMED ABNORMAL PROCEDURE IAW DC-8 OPS MANUAL. NO HELP. CLEANED CONNECTOR AT PROXIMITY SWITCH AFTER VERIFYING MALFDec 22, 1995 · N804AX · Doug DC862 · Landing Gear Position and WarningSDR 96ZZZM15Retract Mech · malfunctionedFLT - NR 651 - KPDX-KDAY - ON GEAR RETRACTION, A LOUD NOISE AND VIBRATION WAS NOTICED IN THE NOSE AREA. THE LANDING GEAR WAS RECYCLED WITH THE SAME RESULTS. RETURNED TO KPDX. MAINTENANCE INSPECTED THE UPLATCH FITTINGS, TRUNNION AND THE NOSE WHEEL WELL. NO Dec 21, 1995 · N995CF · Doug DC862 · Landing Gear Retraction/Extension SystemSDR 96ZZZX315Gen Control Pnl · failedKBOG - FLT 239 - AFTER APPROXIMATELY ONE HOUR INTO FLIGHT WITH ALL GENERATORS IN PARALLEL MODE, ALL LIGHTS IN AIRCRAFT WENT ON AND OFF SEVERAL TIMES. OPERATED GENERATORS IN ISOLATED MODE. AFTER APPROXIMATELY TWO MINUTES, NR 1 GENERATOR TRIPPED OFF-LINE WHEN Dec 20, 1995 · N810BN · Doug DC862 · AC Generation System
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