Boeing DHC-7-102

Service difficulty reports · 246

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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 = 'DHC7102'
  ORDER BY difficulty_date DESC"

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SDR CA970507009Wheel Half · cracked(CAN) DURING EDDY CURRENT INSPECTION SEVERAL CRACK INDICATIONS WERE FOUND AT SEVERAL LUG BOSSES ALONG THE BOTTOM SIDE, PARALLEL TO THE WHEEL BOLT HOLES. THE CRACKS VARIED IN LENGTH FROM 1/2" TO OVER 1" AND TO A DEPTH OF OVER .060.Apr 23, 1997 · Dhav DHC7102 · Wheel/Ski/FloatSDR 97ZZZM732Line · crackedFLT 704 - PID-FLL, PILOT REPORTED IN FLIGHT LOSS OF FLUID AND PRESSURE NR 1 HYDRAULIC SYSTEM. AIRCRAFT MADE AN EMERGENCY LANDING. AIRCRAFT WAS TOWED TO THE GATE AND PASSENGERS DEPLANED. INSPECTION FOUND HYDRAULIC LINE FROM ENGINE DRIVEN PUMP TO FIREWALL CRAApr 6, 1997 · N4860J · Dhav DHC7102 · Hydraulic System, MainSDR M4VA97003Connector · dirtyFLT 22 - DURING TAKEOFF ROLL NR 2 TORQUE INDICATOR DIGITAL READNUT WENT INOP. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. NR 2 TORQUE DIGITAL READOUT WAS PLACED ON MEL. SYSTEM WAS LATER INSPECTED, TORQUE TRANSMITTER CANNON PLUG WMar 31, 1997 · N47RM · Dhav DHC7102 · Engine BMEP/Torque IndicatingSDR CA970421066Fitting Assembly · cracked(CAN) CRACKED BAGGAGE DOOR FITTING AT LOWER FORWARD PIN. FOUR AIRCRAFT FOUND WITH SAME PROBLEM.Mar 31, 1997 · Dhav DHC7102 · Cargo/Baggage DoorsSDR CA970421064Fitting Assembly · cracked(CAN) CRACKED BAGGAGE DOOR FITTING AT LOWER FORWARD PIN. FOUR AIRCRAFT FOUND WITH SAME PROBLEM.Mar 31, 1997 · Dhav DHC7102 · Cargo/Baggage DoorsSDR CA970408008Fitting Assembly · cracked(CAN) CRACKED BAGGAGE DOOR FITTING AT LOWER FORWARD PIN. FOUR AIRCRAFT FOUND WITH SAME PROBLEM.Mar 31, 1997 · Dhav DHC7102 · Cargo/Baggage DoorsSDR M4VA97001Connector · contaminatedFLT 22 - DURING TAKEOFF ROLL, NR 2 TORQUE INDICATOR DIGITAL READOUT WENT INOP. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. NR 2 TORQUE DIGITAL READOUT WAS PLACED ON MEL. SYSTEM WAS LATER INSPECTED, TORQUE TRANSMITTER CANNON PLUG Mar 10, 1997 · N47RM · Dhav DHC7102 · Engine BMEP/Torque IndicatingSDR M4VA97002Seal · failedFLT 71 - AIRCRAFT PRESSURIZED AFTER TAKEOFF THROUGH 12,000 FEET. CABIN DOOR SEAL DEPRESSURIZED, AIRCRAFT WOULD NOT PRESSURIZE AFTER THAT. RETURNED TO GRAND JUNCTION. FOUND DOOR SEAL RUPTURED. REPLACED DOOR SEAL. (X)Feb 13, 1997 · Dhav DHC7102 · Passenger/Crew DoorsSDR 97ZZZM271Line · crackedAFTER FLIGHT NR 752, MECHANIC DISCOVERED OIL DRIPPING FROM NR 2 NACELLE, OIL COMING OUT OF INTAKE AREA. AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR FERRY FLIGHT TO FLL, WITH NR 2 ENGINE SHUT DOWN. UPON COMPLETION OF FERRY INSPECTION FOUND LEFT OIL COOLERJan 28, 1997 · N4860J · Dhav DHC7102 · Engine Oil Distribution (Airframe Furnished)SDR CA970203012De-Icer Boot · separated(CAN) AFTER LANDING AND DURING WALKAROUND BEFORE TURN AROUND, PILOT NOTICED OUTBOARD OF #4 NACELLE BOOT MISSING. BOOT FOUND ON BUTTON OF RUNWAY.Jan 24, 1997 · Dhav DHC7102 · Air Intake Anti/De-Ice SystemSDR HNAA9790105Door Seal · malfunctionedFLT 3145 - DCA-ORF - ON TAXI OUT, THE RIGHT CARGO DOOR REAR SEAL DID NOT INFLATE. THE AIRCRAFT RETURNED TO THE GATE. SECURED DOOR HANDLE. (M)Jan 16, 1997 · N901HA · Dhav DHC7102 · Cargo/Baggage DoorsSDR 97ZZZM181Seal · tornFLT 9022 - PILOT REPORTS, LOW OIL PRESS NR 4 ENG AND NR 4 ENG OIL PRESSURE CAUTION LIGHT ON. PILOT SHUT DOWN NR 4 ENGINE. THE A/C WAS INSPECTED AND FOUND TO BE SAFE FOR FERRY FLIGHT TO FLL WITH THE NR 4 ENGINE SHUT DOWN. AFTER FERRY FLIGHT, INSPECTION FOUNDJan 2, 1997 · N234SL · Dhav DHC7102 · Turbine Engine Accessory DriveSDR HNAA9690582Unsafe Light · illuminatedFLT 3281 - BWI-DCA - THE NOSE GEAR UNSAFE LIGHT ILLUMINATED IN FLIGHT. SELECTED GEAR DOWN AND GOT THREE GREEN DOWN AND LOCKED INDICATION. THE AIRCRAFT CONTINUED ON TO DCA AND LANDED WITHOUT INCIDENT. EVALUATION FLIGHT WAS SATISFACTORY. AT RON, INSPECTED NOSDec 19, 1996 · N905HA · Dhav DHC7102 · Landing Gear Position and WarningSDR 97ZZZM133Check Valve · leakingFLT NR 783 - FLL-PBI - PILOT REPORTED SMOKE COMING OUT OF NR 1 ENGINE INTAKE AFTER SHUTDOWN. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR 3 ENGINE FERRY FLIGHT TO FLL. EMERGENCY FUEL SHUTOFF T-HANDLE WAS PULLED. UPON ARRIVAL AT FLL, INSPECTION FOUND FUEL DNov 27, 1996 · N4860J · Dhav DHC7102 · Engine Fuel DistributionSDR 97ZZZM156Compressor Blade · splitFLT - 759 - MIA-PID - PILOT REPORTED NR 1 TORQUE 3000 AT 11,000 FEET AND T5 AT 770 DEG, NG 93 PERCENT. OTHER ENGINES RUNNING NORMAL WITH 3700 TORQUE. A/C RETURNED TO MIA. THE A/C WAS INSPECTED AND FOUND TO BE SAFE FOR 3 ENGINE FERRY TO FLL. MAINTENANCE REPNov 21, 1996 · N8041D · Dhav DHC7102 · Turbine Engine Compressor SectionSDR 96ZZZM1543Flex Line · holeFLT 4920 - PID-PBI - PILOT REPORTED NR 1 HYD SYSTEM LOSS OF FLUID AND PRESSURE. PILOT REPORTED EMERGENCY TO PBI. PILOT LANDED AIRCRAFT AND TAXIED TO THE GATE AND PASSENGERS DEPLANED. MAINTENANCE INSPECTION FOUND LEFT INBOARD GROUND SPOILER HYDRAULIC LINE TONov 11, 1996 · N703MG · Dhav DHC7102 · Hydraulic System, MainSDR 97ZZZM134Comp Inlet Case · crackedFLT 4909 - MIA-PID - PILOT REPORTED, NR 4 ENGINE FAILED IN FLIGHT (TORQUE OFF, T5 RISE) AND PROP LOCKED UP. ENGINE SHUTDOWN. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR 3 ENGNIE FERRY TO FLL. THE NR 4 T-HANDLE WAS SECURED. UPON RETURN TO FLL, INSPECTION Nov 4, 1996 · N234SL · Dhav DHC7102 · Turbine Engine Air Inlet SectionSDR 97ZZZM132Cable · separatedFLT 4908 - PID-MIA - AN ATTEMPT TO FEATHER, NR 4 ENG FAILED. FUEL SHUTOFF HANDLE WAS PULLED AND THE T5 TEMP INCREASED TO 1000 DEG. 'T' HANDLE WAS RESET AND TEMP DROPPED AND ENG CONTINUED TO RUN. MX PULLED 'T' HANDLE AND THE T5 WENT TO 600 DEG. START BUTTONOct 25, 1996 · N703MG · Dhav DHC7102 · Propeller Controlling SystemSDR 96ZZZM1493Seq Valve · leakingFLT 4918 - PID-MIA - PILOT REPORTED NOSE WHEEL LANDING GEAR LIGHT WAS RED AND TRANSIT LIGHT ON IN FLIGHT. UPON ARRIVAL AT MIA THE AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR GEAR DOWN FERRY FLIGHT TO FLL. MX FOUND NOSE GEAR DOORS WOULD NOT FULLY RETRACT.Oct 9, 1996 · N8041D · Dhav DHC7102 · Landing Gear Retraction/Extension SystemSDR 96ZZZM1492Oil Cooler · failureFLT NR 4922 - PID-PBI - PILOT REPORTED DURING CLIMB-OUT NR 3 OIL TEMPERATURE ABOVE RED LINE. DID PRECAUTIONARY SHUT DOWN OF NR 3 ENGINE AND RETURNED TO PID. INSPECTION REVEALED SLUDGE IN THE VERNATHERM. THE VERNATHERM WAS REPLACED AND NR 3 ENGINE WAS RUN. Oct 7, 1996 · N234SL · Dhav DHC7102 · Engine Oil CoolerSDR 96ZZZM1491Switch · wornFLT NR 4920 - PID-PBI - PILOT REPORTS TILLER MIC IS STUCK IN THE OPEN POSITION. THE AIRCRAFT WAS INSPECTED AND FOUND TO BE IN SAFE CONDITION FOR FERRY FLIGHT TO FLL MAINTENANCE BASE. MAINTENANCE REMOVED AND REPLACED PUSH TO TALK SWITCH ON TILLER. OPERATIONAOct 7, 1996 · N234SL · Dhav DHC7102 · Audio Integrating SystemSDR 96ZZZM1490Wire · frayedFLT 4903 - FLL-PID - UPON LANDING, PILOT REPORTED SMOKE AND ELECTRICAL BURNING SMELL COMING FROM BEHIND AND LEFT OF CAPTAINS SEAT. INSPECTION FOUND FAULTY WIRES, FRAYED AND LOOSE ATTACHED TO STANDBY ATTITUDE INDICATOR POWER SUPPLY. WIRES SECURED, CIRCUIT BREOct 6, 1996 · N4860J · Dhav DHC7102 · Attitude Gyro and Indicating SystemSDR 96ZZZM1472Skin · gougedPBI - AIRCRAFT WAS STRUCK BY A GROUND AIR CONDITIONING CART BEING TOWED BY A TUG. THE STRIKE OCCURRED ONTHE LEFT SIDE REAR FROM STATION X781. THE DAMAGE IS CLASSIFIED AS A GOUGE. AN DER WAS CONTACTED AND REPAIRS ADE IAW DRAWING NR 96 PARA 052R0-1 AND M0 NR Sep 27, 1996 · N4860J · Dhav DHC7102 · Fuselage Main, Plate/SkinSDR HNAA9690566Proximity Box · failedFLT 3084 - DCA-PHL - AFTER GEAR RETRACTION, THE LEFT MAIN RED GEAR LIGHT CYCLES ON AND OFF CONTINUOUSLY. LOUD BANGING NOISE COMING FROM THE NOSE GEAR AREA. THE AIRCRAFT TURNED BACK AND LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 MAIN GEAR PROXSep 19, 1996 · N905HA · Dhav DHC7102 · Landing Gear Position and WarningSDR 96ZZZM1399O-Ring · nickedFLT 4905 - MIA-PID - PILOT SHUTDOWN NR 3 ENGINE ON APPROACH TO PID DUE TO LOW OIL PRESSUE (BELOW RED LINE, WARNING LIGHT CAME ON). TROUBLESHOOTING INDICATED O-RING IN OIL FILLER NECK TO BE UNSERVICEABLE. REPLACED O-RING AND OPERATIONAL CHECK OK. AIRCRAFT RESep 11, 1996 · N703MG · Dhav DHC7102 · Turbine Engine Oil SystemSDR 96ZZZM1398Bracket · brokenFLT 4911 - FLL-PID - RETURNED TO FLL, PILOT REPORTS NOSE GEAR ONLY RETRACTS HALFWAY SELECTING GEAR UP (MAIN RETRACTED OK). INSPECTION REVEALED NOSE GEAR DOOR ACTUATOR ATTACH BRACKET TORN OFF AND NOSE GEAR DOORS JAMMED UP. FREED THE DOORS AND INSPECTED AREA FSep 6, 1996 · N25AG · Dhav DHC7102 · Landing Gear Door ActuatorSDR 96ZZZM1388Engine · failedFLT 4924 - PID-MIA - DIVERTED TO NAS, LOST NR 1 ENGINE ERRATIC TORQUE INDICATION, THEN HIGH T5 AND LOW OIL PRESSURE. SHUT DOWN BEFORE TOTAL FAILURE. NR 1 CHIP DETECTOR ILLUMINATED. NR 1 ENGINE WAS INSPECTED AND FOUND TO HAVE METAL IN OIL AND ON OIL FILTER. Aug 25, 1996 · N703MG · Dhav DHC7102 · Engine (Turbine/Turboprop)SDR 96ZZZM1433Engine · failedFLT 4927 - MIA-PID - PILOT REPORTED NR 3 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED. ON FINAL IN TO PID, OIL PRESSURE CONTINUED TO DROP. PILOT SHUT DOWN NR 3 ENGINE. THE AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR 3 ENGINE FERRY TO FAug 20, 1996 · N4860J · Dhav DHC7102 · Engine (Turbine/Turboprop)SDR HNAA9690555Fuel Contl Unit · failedFLT NR 3258 - DCA-BWI - THE NR 4 ENGINE TORQUE ROLLED BACK INFLIGHT AND NG DROPPED TO APPROXIMATELY 40 PERCENT. THE ENGINE WAS SHUTDOWN INFLIGHT IAW STANDARD PROCEDURES. THE AIRCRAFT TURNED BACK AND LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE NAug 6, 1996 · N905HA · Dhav DHC7102 · Fuel Control/Turbine EnginesSDR HNAA9690542Lock Actuator · failedFLT 3254 - DCA-ORF - ON APPROACH INTO DCA, THE LEFT MAIN GEAR WOULD NOT EXTEND UNTIL THE NOSE AND RIGHT MAIN WERE FULLY EXTENDED. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE LOCK ACTUATOR AND LOWER DRAG STRUT. (M)Jun 21, 1996 · N905HA · Dhav DHC7102 · Landing Gear Retraction/Extension SystemSDR 96ZZZM1179Lwr Drag Strut · failedFLT 3254 - DCA-ORF - ON APPROACH INTO DCA, THE LEFT MAIN GEAR WOULD NOT EXTEND UNTIL THE NOSE AND RIGHT MAIN WERE FULLY EXTENDED. THE AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. REMOVED AND REPLACED THE LOCK ACTUATOR AND LOWER DRAG STRUT. REFERENCE HNAA9690542Jun 21, 1996 · N905HA · Dhav DHC7102 · Landing Gear Retraction/Extension SystemSDR HNAA9690538Smoke Detector · failedFLT 3170 - HPN-DCA - THE LAVATORY SMOKE DETECTOR SOUNDED IN FLIGHT. THE DETECTOR WAS MEL'D PER MEL 26-15 AND THE AIRCRAFT CONTINUED OPERATION WITHOUT INCIDENT. AT RON, THE SMOKE DETECTOR WAS REMOVED AND REPLACED. (M)Jun 10, 1996 · N905HA · Dhav DHC7102 · Smoke DetectionSDR HNAA9690531Uplock Cyl · failedFLT NR 3332 - PHL-DCA - ON APPROACH INTO DCA, THE NOSE WHEEL ATTEMPTS TO CYCLE DOWN WITH GEAR HANDLE IN THE UP POSITION. INDICATIONS ARE A RED NOSE UNSAFE LIGHT FOLLOWED BY A HANDLE LIGHT AT WHICH TIME THE HYDRAULIC SYSTEM TAKES OVER AND FORCES THE GEAR BACK May 18, 1996 · N905HA · Dhav DHC7102 · Landing Gear Retraction/Extension SystemSDR 96ZZZX3644Connector · corrodedTPA/MIA - FLT 4937 - PILOT REPORTED INDICATOR FOR NR 4 FUEL FLOW WAS FLUCTUATING AND HANGING UP. AIRCRAFT WAS FERRIED FROM MIA TO FLL AFTER INSPECTION AND MAG STICK CHECKED FOR FUEL QUANTITY. MAINTENANCE REPLACED NR 4 AND NR 5 FUEL TANK PROBES DUE TO HIGH REMay 16, 1996 · N8041D · Dhav DHC7102 · Fuel Flow IndicatingSDR 96ZZZX2896Wire · chafedON TEST FLIGHT, AC NR 2 GENERATOR LIGHT CAME ON. DURING TROUBLESHOOTING OF SYSTEM, FOUND WIRE 2420-20001E12A-1 GROUNDED OUT. CONDUIT PASSES BETWEEN REAR SPAR AND FLAP PRIMARY CONTROL TUBE. AREA WHERE WIRES PASS THROUGH IS PRESSED AND WIRE RUBS CONDUIT. SUBApr 30, 1996 · N89068 · Dhav DHC7102 · AC Generation SystemSDR 96ZZZX3264Gearbox · wornMIA/PID - FLT 4925 - DURING TAXI, PILOT REPORTED FORE FLAP CAUTION LIGHT ILLUMINATED. THE AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR FERRY FLIGHT TO FLL MAINTENANCE BASE. FLAPS WERE SET AT 15 DEGREES AND AIRCRAFT FERRIED. MAINTENANCE FOUND BOTH 90 DEGREE BOXApr 18, 1996 · N25AG · Dhav DHC7102 · Trailing Edge Flap Control SystemSDR 96ZZZM1020Spoiler Assy · damagedON PRE-FLIGHT, FLIGHT CREW REPORTED 'RIGHT INBOARD ROLL SPOILER IN NEED OF REPAIR.' INVESTIGATION BY MX FOUND RIGHT INBOARD ROLL SPOILER WAS MISSING 95 PERCENT OF THE SPOILER. ATTACH ARMS AND APPROXIMATELY ONE FOOT OF THE ROLL SPOILER REMAINED. MX REPLACED Apr 9, 1996 · N234SL · Dhav DHC7102 · SpoilersSDR 96ZZZM889Vis · failedFLT 4915 - MIA-PID - PILOT REPORTED THAT DURING TAXI, SMOKE CAME OUT OF THE CAPTAINS INSTRUMENT PANEL. AIRCRAFT WAS FERRIED TO FLL MAINTENANCE BASE. MAINTENANCE REPLACED TCAS/VSI. LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Mar 28, 1996 · N234SL · Dhav DHC7102 · Rate of Climb IndicatorSDR 96ZZZX3418Control Box · inoperativeMIA/TPA - FLT 4938 - PILOT REPORTED SECONDARY INVERTER LIGHT ILLUMINATED. AIRCRAFT WAS FERRIED TO FLL MAINTENANCE BASE. MAINTENANCE REPLACED PARALELLING CONTROL BOX. TEST FLIGHT SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE.Mar 18, 1996 · N4860J · Dhav DHC7102 · AC Generation SystemSDR HNAA9690514Air Cycle Mach · failedFLT NR 3055 - ORF-DCA - DURING PREFLIGHT CHECKS, THE CABIN FILLED WITH SMOKE. THE LEFT PACK WENT RED LINE AND AUTO SHUTOFF DID NOT WORK. FOUND AIR CYCLE MACHINE SEIZED. REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE AND THE LEFT DUCT TEMP SWITCH. (M)Mar 1, 1996 · N905HA · Dhav DHC7102 · Cabin Cooling SystemSDR 96ZZZM669Duct Temp Switch · failedFLT NR 3055 - ORF-DCA - DURING PREFLIGHT CHECKS, THE CABIN FILLED WITH SMOKE. THE LEFT PACK WENT RED LINE AND AUTO SHUTOFF DID NOT WORK. FOUND AIR CYCLE MACHINE SEIZED. REMOVED AND REPLACED THE LEFT AIR CYCLE MACHINE AND THE LEFT DUCT TEMP SWITCH. REFERENCMar 1, 1996 · N905HA · Dhav DHC7102 · Cabin Temperature Control SystemSDR HNAA9690513Actuator · failedFLT NR 3186 - DCA-ORF - ON APPROACH INTO ORF, THE LEFT MAIN GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. ONCE NOSE AND RIGHT MAIN LOCKED, LEFT MAIN STARTED DOWN AND LOCKED INTO PLACE. THE AIRCRAFT LANDED IN ORF WITHOUT INCIDENT. RETORQUED LOCK STRUT FITTING ANFeb 20, 1996 · N905HA · Dhav DHC7102 · Landing Gear ActuatorSDR HNAA9690512Actuator · failedDCA/PHL - FLT 3169 - UPON APPROACH TO PHL, THE LT MLG WOULD NOT EXTEND. CREW PERFORMED ALTERNATE GEAR EXTENSION AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LT MLG LOCK ACTUATOR. (X)Feb 19, 1996 · N905HA · Dhav DHC7102 · Landing Gear Retraction/Extension SystemSDR CA960202014P3 Line · cracked(CAN)#1 ENGINE ROLLED BACK TO MIN FLOW ON INBOUND. POST FLIGHT INVESTIGATION FOUND THE LINE FROM THE COMPRESSOR TO THE P3 FILTER CRACKED AT THE FLANGE FITTING. THE LINE WAS REPLACED AND THE AIRCRAFT RETURN ED TO SERVICE.Jan 29, 1996 · Dhav DHC7102 · Fuel Control/Reciprocating EnginesSDR 96ZZZX1283Clamp · deterioratedWHILE PERFORMING MAINTENANCE IN THE FUEL BAY, FOREIGN MATERIAL WAS SEEN IN THE RESIDUAL FUEL. INSPECTION OF THE MATERIAL REVEALED IT TO BE RUBBBER IN COMPOSITION. INVESTIGATION REVEALED THE CLAMPS INSTALLED WERE TA12C60W AND THE CUSHION WAS DISTORTED AND DETJan 19, 1996 · N59AG · Dhav DHC7102 · Fuel StorageSDR CA960126031Bearing · seized(CAN)WHEN FLAPS SELECTED DOWN DURING MAINTENANCE, A LOUD SQUEAL WAS HEARD. INSPECTION FOUND THAT THE LEFT HAND, INBOARD BEARING HANGER ASSEMBLY HAD SEIZED. THE SHAFT THAT RUNS ON THE BEARING WAS SPINNING I N THE SLEEVE. THIRTY PERCENT OF THE SHAFT HAD BEEN WORJan 18, 1996 · Dhav DHC7102 · Trailing Edge Flap Control SystemSDR HNAA9690304Lock Actuator · failedDCA/PHL - FLT 3098 - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP, THE LEFT MAIN GEAR WOULD NOT FULLY RETRACT. THE AIRCRAFT TURNED BACK TO DCA AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LEFT MLG LOCK ACTUATOR. (X)Jan 13, 1996 · N903HA · Dhav DHC7102 · Landing Gear Retraction/Extension SystemSDR NNAA9690103Proximity · failedFLT EN29 - ORF-DCA - AFTER TAKEOFF, GOT RIGHT MAIN GEAR INDICATION 'RED UNSAFE LIGHT', AND THE GEAR HANDLE LIGHT STAYED ON AFTER THE GEAR WAS SELECTED UP. THE AIRCRAFT RETURNED TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE RIGHT HAND PROXIMITYJan 12, 1996 · N901HA · Dhav DHC7102 · Landing Gear Position and WarningSDR HNAA9590125Shuttle Valve · failedFLT NR 3030 - DCA-ORF - AFTER TAKEOFF, WITH GEAR HANDLE UP, HANDLE GEAR TRANSIT LIGHT AND RED LIGHT STAY ON FOR NOSE GEAR. THE AIRCRAFT CONTINUED ON TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NLG GROUND LOCK CABLE. LATER IN THE DAY, FLIGHTDec 22, 1995 · N901HA · Dhav DHC7102 · Landing Gear Retraction/Extension SystemSDR 96ZZZM171Linear Actuator · failedFLT NR 3030 - DCA-ORF - AFTER TAKEOFF, WITH GEAR HANDLE UP, HANDLE GEAR TRANSIT LIGHT AND RED LIGHT STAYED ON FOR NOSE GEAR. THE AIRCRAFT CONTINUED ON TO ORF AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE NLG GROUND LOCK CABLE. LATER IN THE DAY, FLIGDec 22, 1995 · N901HA · Dhav DHC7102 · Landing Gear Retraction/Extension System
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