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 IXXA060431SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS335.25. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA060424SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE LOWER SKIN CORRODED FROM STATION XFS735 TO XFS885. REPAIRED PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862 · Wing, Plate/SkinSDR IXXA060423SAngle · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING TEE ANGLE CRACKED AT STATION XRS162. REPAIRED PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862 · Wing, Attach FittingsSDR IXXA060197SFitting · crackedDURING ROUTINE C CHECK FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 26 LEFT. REPLACED DAMAGED END FITTING WITH NEW PER APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862 · Fuselage Miscellaneous StructureSDR IXXA060183SFitting · crackedDURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 23 RIGHT. REPLACED DAMAGED END FITTING, AND FASTENERS AT STATION Y1530 LONGERON 23 RIGHT IAW DC8 SRM 53-2-0, AND 51-1-20D.Jun 7, 2004 · N41CX · Doug DC862 · Fuselage Main, Longeron/StringerSDR IXXA060445SFitting · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF340. REPAIRED PER ALL APPLICABLE DATAJun 5, 2004 · N41CX · Doug DC862 · Trailing Edge FlapsSDR IXXA060422SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD AILERON LOWER SKIN DENTED AND SCRATCHED AT STATION XA524. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862 · AileronsSDR IXXA060421SPanel · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE LOWER PANEL CORRODED AROUND SCREWS AT STATION XRS169. REPAIRED PER ALL APPLICABLE DATA.Jun 5, 2004 · N41CX · Doug DC862 · Wing, Plate/SkinSDR ARWA20040507Actuator · malfunctionedUNABLE TO EXTEND FUEL DUMP CHUTES ELECTRICALLY, MOTOR STOPPED APPROXIMATELY 3300 FULL EXTENDED. TRANSFERRED TO DMI NR 18536 CATEGORY (C) IAW MEL 28-9-1. INSTALLED CAT (C) PLACARD; PENDING CLOSING OF DMI. PERFORMED OPERATIONAL CHECK OF FUEL DUMP CHUTE ELECT MMay 21, 2004 · N810BN · Doug DC862 · Fuel Dump SystemSDR ARWA20040506Gyro · faultyCAPTAIN'S COMPASS FAILED IN FLIGHT. REMOVED AND REPLACED CAPTAIN'S PICTORIAL DEVIATION INDICATOR (PDI) AND DIRECTIONAL GYRO (DG) IAW MM 31-10-1 AND MM 34-21-1. SWAPPED INSTRUMENT AMPS IAW 34-00. SYSTEM GROUND TEST NORMAL IAW 34-21-0, 34-52-0 AND 34-28-0.May 21, 2004 · N810BN · Doug DC862 · Directional Gyro and Indicating SystemSDR IXXA0400017OArm · bentIN CRUISE "DOORS NOT LATCHED LIGHT" CAME ON FOR 10 MINUTES. MAINTENANCE FOUND LT LANDING GEAR DOOR LATCH ROLLER ARMS BENT. REMOVED AND REPLACED LATCH ROLLER ARMS. WITH DOORS CLOSED FOUND LT DOOR LATCH ROLLER STOP BOLT SPACER CONTACTING RAIL ASSEMBLY. PERFORMEDMar 21, 2004 · N799AL · Doug DC862 · Landing Gear DoorsSDR IXXA0400008OWindshield · crackedONE HOUR AND A HALF INTO CRUISE FROM KBWI THE CAPTAINS WINDSHIELD CRACKED. CREW RETURNED THE AIRCRAFT TO KBWI AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED WINDSHIELD AND HEAT CONTROLLER PER ALL APPLICABLE MANUALS. OPERATIONAL CHECK WAS GOODJan 31, 2004 · N41CX · Doug DC862 · Flight Compartment WindowsSDR ARWA20040105Attach Fitting · looseDURING PREFLIGHT FOUND ELEVATOR STARBOARD SIDE UP SLIGHTLY AND PORT SIDE SLIGHTLY DOWN, SLIGHT DIFFERENCE IN TRAVEL BETWEEN PORT AND STARBOARD SIDE ELEVATORS. FOUND LOOSE ATTACHMENT AT PORT SIDE ELEVATOR ATTACHMENT TO TORQUE TUBE. PERFORMED ELEVATOR INSPECTIJan 30, 2004 · N8974U · Doug DC862 · Elevator Miscellaneous StructureSDR ARWA20040106Switch · inoperativeSTARTED TAKE-OFF ROLL, AILERON POWER LIGHT CAME ON. REMOVED AND REPLACED MANUAL CONTROL IND SWITCH IAW MM 27-11-14; OPERATIONAL CHECK NORMAL IAW MM 27-11-14 AND 27-11-0.Jan 27, 2004 · N810BN · Doug DC862 · Aileron Control SystemSDR IXXA0400004OEngine · malfunctionedDURING CLIMB, THE NR 1 ENGINE WOULD NOT GO ABOVE 1.60 EPR WHEN SETTING CLIMB POWER. CREW RETURNED AIRCRAFT TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED NR 1 ENGINE FCU MOISTURE TRAP AND INSPECTED PRBC. NO DEFECTS WERE NOTED. PERFORMED ALL OPERATJan 11, 2004 · N31CX · Doug DC862 · Engine (Turbine/Turboprop)SDR IXXA0400003OLink Assy · brokenDURING CLIMB, 1550Z WHILE TRANSITIONING THROUGH FL 330 CREW SUSPECTED NOSE GEAR OPENED IN FLIGHT. SLOWED AIRCRAFT BELOW 230 DESCENDED AND RETURNED AIRPORT. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED NOSE GEAR DOOR ADJUSTMENT/TEST. FOUND LT FWD NOSJan 10, 2004 · N31CX · Doug DC862 · Landing Gear Door Retract SectionSDR IXXA0400002ORelease System · stickingDURING TAKE OFF, WHEN GEAR RETRACTED HAD EVIDENCE OF NOISE AND VIBRATRION COMING FROM NOSE GEAR AREA. GEAR WAS RECYCLED AND ALL INDICATIONS WERE NORMAL. MAINTENANCE FOUND LT FORWARD NOSE GEAR DOOR MANUAL RELEASE MECHANISM STICKING INTERMITTENTLY. MAINTENJan 10, 2004 · N31CX · Doug DC862 · Landing Gear Door Retract SectionSDR IXXA0400001ODoor · unlatchedAFTER TAKE OFF AND GEAR RETRACTION, CREW NOTICED A VIBRATION AND NOISE. CREW RECYCLED LANDING GEAR, DID NOT CORRECT PROBLEM. SUSPECT NOSE GEAR DOOR NOT CLOSE PROPERLY. CREW CONTINUED FLIGHT TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENACE PERFORMED FUNCJan 9, 2004 · N31CX · Doug DC862 · Landing Gear Door Retract SectionSDR IXXA0300086ODownlock Switch · brokenWHEN GEAR WAS EXTENED THE LT GEAR LIGHT DID NOT ILLUMINATE. AFTER CYCLING GEAR ALL THREE GEAR LIGHTS WERE NORMAL. MAINTENANCE REMOVED AND REPLACED LT MAIN LANDING GEAR DOWN LOCK INDICATION SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE.Dec 24, 2003 · N728PL · Doug DC862 · Landing Gear Position and WarningSDR GKZR200479903Longeron · crackedLEFT L24 HAS ABOUT 1.25 INCH CRACK AFT OF THE FWD MAIN ATTACH BOLT. REMOVED AND REPLACED LT L24 AT STA 903 TO 960 IAW DC8 SRM 51-1-21 & 51-3-0. TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8. TORQUED FWD MAIN ATTACH BOLT IAW DRW 5750553.Dec 11, 2003 · N799AL · Doug DC862 · Fuselage Main, Longeron/StringerSDR ARWA20031204Spar · crackedDURING ACCOMPLISHMENT OF RB 17284 SB 57-090 INSPECTION. LEFT WING FRONT SPAR XFS 517 & XFS 518, LOWER CAP HOLES (2 EACH) WITH CRACKS.Dec 6, 2003 · N810BN · Doug DC862 · Wing SparSDR ARWA20031202Pitot Head · failedON CLIMBOUT OF KMIA, CAPTAIN LOST ALTIMETER, AIRSPEED, AND VSI INDICATIONS.Dec 6, 2003 · N8969U · Doug DC862 · Pitot/Static SystemSDR GKZR200479909Skin · corrodedRIGHT AFT FUS BETWEEN STA 1540 & 1551 HAS CORROSION UNDER PAINT. STARTED REMOVING CORROSION FOUND SMALL POCKET OF INTERGRANULAR, CUT DAMAGED AREA OUT, FABRICATED FILLER & DOUBLER IAW DC8 SRM 53-02-01, TREATED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FILLER & Nov 15, 2003 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR GKZR200479908Finger Doubler · corrodedRIGHT AFT FUSELAGE BETWEEN STA 1540 & 1551 FROM L22R TO L25R PREVIOUS REPAIR HAS 2 RIVETS BLOWN OUT & CORROSION. REMOVED & FABRICATED DOUBLER & FINGER DOUBLER IAW DC8 SRM 53-02-01. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER & FINGER DOUBLER IANov 15, 2003 · N799AL · Doug DC862 · Fuselage Main, Plate/SkinSDR GKZR200479907Floor Panel · corrodedAFT PASS AREA AT STA 1480 FLOOR PANEL SUPPORT CORRODED UNDER FLOOR PLANK. FABRICATED DOUBLER FROM .063 7075T6 IAW DC8 SRM 53-2-3, TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 53-2-3.Nov 8, 2003 · N799AL · Doug DC862 · Fuselage Floor PanelSDR GKZR200479906Support Fitting · crackedLEFT O/B AILERON NR 7 SUPPORT FITTING CRACKED. REMOVED LEFT AILERON IAW DC8 MM 27-11-2, REMOVED AND REPLACED LEFT O/B AILERON O/B ATTACHMENT BRACKET IAW DC8 DRAWING 5619462. REINSTALLED AILERON IAW DC8 MM 27-11-2.Nov 5, 2003 · N799AL · Doug DC862 · Wing, Control Surface Attach FittingsSDR GKZR200479905Support Fitting · crackedRIGHT O/B AILERON NR 7 SUPPORT HINGE FITTING HAS A CRACK AT LWR O/B BOLT HOLE. REMOVED RIGHT O/B AILERON IAW DC8 MM 27-11-2. REMOVED AND REPLACED RIGHT O/B AILERON HINGE SUPPORT FITTING IAW DC8 DRAWING 5619462. REINSTALLED RIGHT O/B AILERON IAW DC8 MM 27-11Nov 4, 2003 · N799AL · Doug DC862 · Wing, Control Surface Attach FittingsSDR GKZR200479902Support Fitting · crackedRIGHT MLG SUPPORT FITTING CRACKED AT TOP ATTACH POINT. REMOVED AND REPLACED RIGHT MLG SUPPORT FITTING (TRAP) IAW DC-8 SRM 51-1-20 & 51-1-21. BORED RIGHT MLG SUPPORT FITTING PER DOUGLAS BLUE PRINT 5611440.Nov 4, 2003 · N799AL · Doug DC862 · Fuselage, Landing Gear Attach FittingsSDR GKZR200479901Panel · crackedNR 4 INBOARD PYLON PLANK CRACKED ABOUT 30 SCREWS AFT FROM L/E BOTTOM ROW. REMOVED NR 4 ENGINE PYLON I/B PLANK PANEL FOR REPAIRS, FABRICATED REPAIR IAW DC-8 SRM 54-2-2, INSTALLED REPAIR IAW DC-8 SRM 54-2-2. REINSTALLED NR 4 ENGINE PYLON PLANK IAW DC-8 SRM 54-Nov 2, 2003 · N799AL · Doug DC862 · Nacelle/Pylon, Plate/SkinSDR GKZR200479904Skin · corrodedRIGHT WING UPPER SURFACE FROM WING ROOT TO STA 624 HAS NUMEROUS LOCATIONS OF EXFOLIATION RUNS FROM FRONT SPAR TO AFT SPAR. REMOVED CORROSION IAW DC8 SRM 51-1-8, NDT VERIFIED ALL WITHIN LIMITS. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FASTENERS IAW DNov 1, 2003 · N799AL · Doug DC862 · Wing, Plate/SkinSDR IXXA0300070OBearing · lack of lubeDURING CLIMB FROM FJDG CREW LOST CABIN PRESSURIZATION. CREW RETURNED TO FJDG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED OUTFLOW VALVE. THEY LUBED MECHANICAL ARMS AND BEARINGS. OPERATIONAL CHECK GOOD BOTH IN AUTO AND MANUAL PER ALL APPLICABLE MANUALS. TOct 29, 2003 · N728PL · Doug DC862 · Pressure Regulator/Outflow ValveSDR ARWA20031004Connector · dirtyON TAKE OFF FROM MGGT, RECEIVED A STICK SHAKE AT 40 KTS. ON ROLL. ABORTED TAKEOFF AND RETURNED TO RAMP. NOTE: ALSO HAD MAIN GEAR SPOILERS INOPERATIVE; LIGHT ILLUMINATED. CLEANED ELECTRICAL CONNECTORS ON STALL WARNING COMPUTER IAW MM 34-16-2 AND OPERATIONAL Oct 24, 2003 · N8968U · Doug DC862 · Stall Warning SystemSDR ARWA20031002Strut · dischargedAFTER SETTING RED POWER ON TAKEOFF ROLL STICK SHAKER CAME ON, ABORTED TAKEOFF (PRIOR 40K). CHECKED PALLET WEIGHTS, LOADING, WEIGHT AND BALANCE; SERVICE NOSE STRUT IAW MM 32-21-2. PERFORMED OPERATIONAL CHECK OF STALL WARNING SYSTEM IAW DC8 MM 41-10-02, NO FUOct 16, 2003 · N8968U · Doug DC862 · Nose/Tail Landing Gear Strut/AxleSDR IXXA0300061OUplock Sensor · contaminatedON APPROACH, WITH ALL 3 MLG'S DOWN AND LOCKED, BOTH (DOOR NOT LATCHED, GEAR NOT LATCHED) LIGHTS WERE ILLUMIN, ALSO AUDIBLE WARNING HORN. GEAR WAS RECYCLED TWICE, THIS CORRECTED PROBLEM. MAINT INSPECTED LANDING GEAR, GEAR DOOR WARNING SYS. NO DEFECTS WERE NOTEDOct 12, 2003 · N728PL · Doug DC862 · Landing Gear Position and WarningSDR IXXA0300059OValve · malfunctionedDURING CLIMB NR 4 ENG QTY DROPPED & OIL PRESS ROSE TO 60 PSI, TEMP INCREASED. POWER WAS REDUCED PARAMETERS REDUCED OIL PRESS, OIL TEMP REDUCED 20 DEGREES & OIL QTY INCREASED. OIL PRESS LIGHT NEVER ILLUM & OIL PRESS NEVER DROPPED BELOW 40 PSI. MX REMOVED & ISep 17, 2003 · N728PL · Doug DC862 · Turbine Engine Oil SystemSDR ARWA20030803O-Ring · wornLOG PAGE 110832. DISCREPANCY: AT TOP OF DESCEND LOSS OF HYDRAULIC FLUID AND PRESSURE; COMPLETED ABNORMAL HYDRAULIC LANDING CHECKLIST. REMOVED AND REPLACED RT AILERON POWER ACTUATOR HYDRAULIC O-RINGS TO SWIVEL VALVE IAW DC8 MM 27-14-01. PERFORMED LEAK CHECKAug 13, 2003 · N8969U · Doug DC862 · Aileron Control SystemSDR IXXA0300051OValve · damagedON CLIMBOUT FROM PHIK THE LEFT PACK DUCT TEMPERATURE WENT TO 80 DEGREES. CREW TURNED OFF PACK AND THE TEMPERATURE WENT UP. CREW RETURNED TO PHIK AND LANDED WITH OUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT AIR MIX VALVE IN ACCORDANCE WITH ALL APPLICAJul 29, 2003 · N31CX · Doug DC862 · Air Distribution SystemSDR IXXA0300050OEngine · leakingDURING FLIGHT FROM GOOY TO EDDS NR 4 ENGINE HAD A LOW OIL PRESSURE, LOW OIL QUANTITY AND HIGH TEMPERTURE WARNING. THE ENGINE WAS SHUT DOWN AND THE CREW RETURNED AIRCRAFT TO GOOY. MAINTENANCE INSPECTION IS ON GOING. AS MORE INFORMATION BECOMES AVAILABLE IT WJul 25, 2003 · N799AL · Doug DC862 · Engine (Turbine/Turboprop)SDR ARWA20030708Floorbeam · corrodedDURING A-CHECK INSPECTION, THE FOLLOWING WAS FOUND; AFT ACCESSORY COMPARTMENT STATION 1520, RBL 32 FLOORBEAM UPPER FLANGE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM UPPER AFT FLANGE AT STATION 1520 RBL 32 IAW AVITAS ENGINEERING ORDER AROW-034RO-1, PAGES 1 TOJul 22, 2003 · N802BN · Doug DC862 · Fuselage Main, Floor BeamSDR IXXA0300048OGyro · failedAFTER TAKEOFF FROM WSAP NR 1 COMPASS PRECESSING 8-10 DEGREES IN APPROX. 1 1/2 MINUTES. CREW RETURNED TO WSAP AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WILL PROVIDE MORE INFORMATION AS IS BECOMES AVAILABLE. MAINTENANCE REMOVED AND REPLACED NR 1 DIJul 14, 2003 · N31CX · Doug DC862 · Directional Gyro and Indicating SystemSDR ARWA20030702Skin · crackedNR 34M. DURING "A" CHECK NON-ROUTINE INSPECTION, THE FOLLOWING WAS FOUND- NLG WW LT SIDE, STA. 208 L-33L CORNER WITH .2500 INCH CRACK. TRIMMED OUT CRACK ON EDGE OF NOSE SKIN AT NOSE LANDING GEAR DOOR LEFT AFT CORNER AND FABRICATED FILLER FROM 707STG.O50 AND Jul 7, 2003 · N8974U · Doug DC862 · Fuselage Main, Plate/SkinSDR ARWA20030701Computer · malfunctionedLOG PAGE 504844. RUDDER KICKING AFTER TAKEOFF AND OSCILATING. FOUND YAW CHANNEL COMPUTER; REMOVED AND REPLACED YAW CHANNEL COMPUTER AND PERFORMED OPERATIONAL CHECK SYSTEM IAW MM 22-10-37 CHECKED GOOD. CHECKED AND PERFORMED RUDDER OPERATIONAL CHECK IAW MM 27Jul 2, 2003 · N8968U · Doug DC862 · Autopilot ComputerSDR ARWA20030603Engine · failedPRECAUTIONARY SHUTDOWN NR 2 ENGINE; TIME 0030. OIL PRESSURE -0 OIL TEMP 145. ENGINE WINDMILLED 3 1/2 HOURS, ZERO OIL PRESSURE. ALL ABNORMAL PROCEDURES FOLLOWED. REMOVED AND REPLACED NR 2 ENGINE IAW JOB CARDS 72-000-30-02-01, 77-000-00-03-1 & 77-000-02-1; AJun 11, 2003 · N8969U · Doug DC862 · Engine (Turbine/Turboprop)SDR ARWA20030605Door Frame · crackedDURING MAINTENANCE INSPECTION THE FOLLOWING WAS FOUND, FORWARD ENTRY DOOR FRAME, BOTTOM AFT CORNER HFEC INSPECTION REVEALED .1250 INCH CRACK. ACCOMPLISHED REPAIRS AT FORWARD ENTRY DOOR AFT LOWER CORNER IAW SB 53-075 AND DRAWING NR SR08530021.Jun 5, 2003 · N802BN · Doug DC862 · Fuselage Main, StructureSDR IXXA0300040OPressure Switch · shortedON CLIMB FROM KTOL TO KNGU, NR 1 OIL PRESSURE LIGHT CAME ON WITH NORMAL PRESSURE INDICATION. CREW PERFORMED ABNORMAL CHECKLIST. AIRCRAFT LANDED AT KNGU WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED OIL PRESSURE SWITCH IN ACCORDANCE WITH THE DOUGLAS AIRJun 4, 2003 · N799AL · Doug DC862 · Engine Oil PressureSDR IXXA0300037OOutflow Valve · contaminatedDURING CRUISE AT FLIGHT LEVEL 28K CABIN ALTITUDE BEGAN TO CLIMB. CREW ELECTED TO DEPLOY PASSENGER O2 MASKS. FLIGHT CONTINUED TO WSAP AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION MAINTENANCE CLEANED OUTFLOW VALVE, INSPECTED DUCTING AND OPERATIONALLY CHECKED May 25, 2003 · N728PL · Doug DC862 · Pressure Regulator/Outflow ValveSDR IXXA0300033OWarning Horn · false activationON TAKE OF, FROM TOL TO WRI, WITH FLAPS RETRACTING, TAKE OFF WARNING HORN SOUNDS UNTIL PTC IS PLACED IN NORMAL. CREW DID AN AIR TURN AROUND TO TOL. MAINTENANCE PERFORMED A TEST OF FLAP TAKEOFF WARNING SWITCH AND ALL OPERATIONAL CHECKS ARE GOOD AT THIS TIME IN May 6, 2003 · N799AL · Doug DC862 · Trailing Edge Flap ActuatorSDR ARWA20030402Rotary Actuator · jammedRIGHT SUIT CASE HANDLE JAMMED IN FORWARD POSITION AND COULD NOT BE MOVED EVEN WITH C/B PULLED. REMOVED AND REPLACED RIGHT LONGITUDINAL TRIM SERVO ACTUATOR IAW MM 27-41-10. OPERATIONAL CHECK NORMAL IAW MM 27-40-0.Apr 11, 2003 · N802BN · Doug DC862 · Stabilizer ActuatorSDR ARWA20030401Engine · lack of lubeAFTER T/O FROM UTP, DURING CLIMB, FE OBSERVER NR 2 OIL QUANITY INDICATOR READING 2 GALLONS & DECREASING. SWAPPED INDICATORS, NO CHANGE. FOLLOWED ABNORMAL PROCEDURES FOR FUEL DUMPING, LANDED (UTP) LESS THAN MLWG. SERVICED NR 2 ENGINE OIL WITH 9 QTS. OF OIL.Apr 3, 2003 · N8969U · Doug DC862 · Turbine Engine Oil SystemSDR IXXA0300029OLanding Gear · false indicationDURING FLIGHT FROM KWAK TO RJTY LANDING GEAR WAS PUT IN DOWN POSITION. THERE WAS NO LEFT GEAR INDICATION. THE GEAR WAS RECYCLED AND IT INDICATED GEAR DOWN. MAINTENANCE JACKED AIRCRAFT AND SWUNG GEAR A TOTAL OF FIVE TIMES. OPERATIONAL CHECK GOOD IN ACCORDANMar 21, 2003 · N728PL · Doug DC862 · Landing Gear Position and Warning
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