Raytheon 1900D

Service difficulty reports · 7,152

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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 = '1900D'
  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 MASA99143Torque Gauge · failedFLT 5977 - PIT-ART - AFTER DEPARTURE FROM PIT, THE CAPTAIN REPORTED THAT THE NR 2 ENGINE TORQUE AND FUEL FLOW WERE FLUCTUATING IN FLIGHT. THE AIRCRAFT DIVERTED TO DUJ WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE TORQUE GAUGE AND THEAug 19, 1999 · N65YV · Beech 1900D · Engine BMEP/Torque IndicatingSDR C2XA99CL088Heat · malfunctionedCLE-MBS - FLT 3251 - THE CREW REPORTED THAT THE RIGHT PITOT HEAT WOULD NOT TURN ON. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE RIGHT PITOT HEAT IAW B1900D MM 30-30-00, NO DEFECTS WERE NOTED. TAug 19, 1999 · N69548 · Beech 1900D · Pitot/Static Anti-Ice SystemSDR C2XA99CL086Retract Mech · req'd serviceCLE-PIT - FLT 3030 - THE CREW REPORTED THE LEFT MAIN GEAR LIGHT DID NOT ILLUMINATED WHEN THE GEAR WAS SELECTED DOWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE HYDRAULIC RESEVOIR AND PERFORMED OPS CHECK OF THE GEAR IAW B1900D MM 3Aug 19, 1999 · N49543 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 99ZZZM780Fuel Flow Gauge · failedFLT 5977 - PIT-ART - AFTER DEPARTURE FROM PIT, THE CAPTAIN REPORTED THAT THE NR 2 ENGINE TORQUE AND FUEL FLOW WERE FLUCTUATING IN FLIGHT. THE AIRCRAFT DIVERTED TO DUJ WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE TORQUE GAUGE AND THEAug 19, 1999 · N65YV · Beech 1900D · Fuel Flow IndicatingSDR C2XA99CL085Switch · failedCLE - FLT 3439 - THE CREW REPORTED THAT ON TAKEOFF THE 'AFX DISABLE' LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. THE CREW ABORTED TAKEOFF AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE A/F HIGAug 18, 1999 · N49543 · Beech 1900D · Propeller Controlling SystemSDR 99ZZZM624Pc Board · failedCLE - FLT 3439 - THE CREW REPORTED THAT ON TAKEOFF THE 'AFX DISABLE' LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. THE CREW ABORTED TAKEOFF AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE A/F HIGAug 18, 1999 · N49543 · Beech 1900D · Central WarningSDR MASA99141Governor · failedFLT 6461 - FMN-PHX - AFTER DEPARTURE FROM FMN, THE CREW REPORTED THAT BOTH PROPELLERS WOULD NOT EXCEED TO 1550 RPM. THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE REMOVED AND REPLACED THE RIGHT OVERSPEED GOVERNOR. ALSO, INSPECTED THE LEFT PROPELLER, NO DISAug 17, 1999 · N132YV · Beech 1900D · Propeller GovernorSDR C2XA99CL081Switch · dirtyABE-CLE - FLT 3005 - THE CREW REPORTED THAT AFTER SELECTING THE GEAR DOWN THAT THE LEFT GEAR DOWN INDICATION CAME ON AND THEN WENT OUT. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE LEFT LANDING GEAR DOWNLOCK SWITCH AND PAug 16, 1999 · N87550 · Beech 1900D · Landing Gear Position and WarningSDR C2XA99CL079Switch · dirtyAZO-CLE - FLT 3032 - THE CREW REPORTED THE LANDING GEAR LIGHTS ON THE RIGHT SIDE DID NOT ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GEAR SWINGS AND FOUND THE RT DOWNLOCK INDICATOR TO BE VERAug 15, 1999 · N81536 · Beech 1900D · Landing Gear Position and WarningSDR C2XA99CL077Actuator · failedLAN - THE CREW REPORTED THAT THE RIGHT MAIN GEAR LIGHT DID NOT ILLUMINATE WITH THE GEAR SELECTED DOWN. THE AIRCRAFT LANDED IN LAN WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR ACTUATOR AND PERFORMED OPERATIONAL CHECK IAW B190Aug 12, 1999 · N81533 · Beech 1900D · Landing Gear ActuatorSDR MASA99130Windshield · crackedFLT 6494 - PHX-GYM - THE CAPTAIN REPORTED THAT THE F/O'S WINDSHIELD CRACKED IN FLIGHT. THE AIRCRAFT LANDED IN GYM WITHOUT INCIDENT. THE AIRCRAFT WAS FOUND TO BE AIRWORTH FOR FERRY TO FMN. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD. OPS CHECK GOOD. THAug 8, 1999 · N132YV · Beech 1900D · Flight Compartment WindowsSDR C2XZ99CL072Pc Board · failedCLE - FLT 3056 - THE CREW REPORTED THE 'AFX DISABLE' LIGHT REMAINED ILLUMINATED UP TO 15,000 FEET. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PC BOARD, AND PERFORMED OPERATIONAL CHECKS OF THE AUTOFEATHERAug 8, 1999 · N49543 · Beech 1900D · Propeller Feathering/ReversingSDR CA990818008Bearing · stiff(CAN) PILOTS REPORTED AFTER TAKEOFF, THE ELEVATOR CONTROLS BECAME JAMMED IN NOSE UP POSITION. CONTROL COLUMN WAS STIFF DUE TO TIGHT BEARINGS IN SUPPORT ASSY. (1295241001 - LOWER ROLLER, 1295241005 - UPPER ROLLER). MARKS ON THE ROLLERS INDICATE POSSIBLE FOD CAug 7, 1999 · Beech 1900D · Elevator Control SystemSDR C2XA99CL069Pc Board · failedIAD - FLT 3015 - THE CREW REPORTED THAT ON TAKEOFF ROLL, THE 'AFX DISABLE' ANNUNCIATOR ILLUMINATED AT 90 KIAS, THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTEANCE REMOVED AND REPLACED PCBA123 AND PERFORMED OPS CHECKS AND Aug 7, 1999 · N49543 · Beech 1900D · Propeller Feathering/ReversingSDR C2XA99CL068Switch · dirtyCAK - FLT 3008 - THE CREW REPORTED THAT ON TAKEOFF ROLL, THE 'AFX DISABLE' ANNUNCIATOR ILLUMINATED AND THE LEFT AUTOFEATHER SYSTEM UNARMED. THE AIRCRAFT REJECTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED PRESSURE SWITCHESAug 3, 1999 · N49543 · Beech 1900D · Propeller Feathering/ReversingSDR C2XA99CL065Retract Mech · malfunctionedRIC - FLT 3055 - THE CREW REPORTED THE GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT RETURNED TO RIC WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND PERFORMED OPERATIONAL CHECK OF THE GEAR IAW BEECHCRAFT MM 32-30-00. NO DEFECTS WERAug 3, 1999 · N81538 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 99ZZZX3375Torque Knee · crackedSOCKET WAS CRACKED BELOW ATTACH POINT OF LOWER TORQUE KNEE. SUBMITTER STATED THEY HAVE FOUND THE SAME CRACK IN THE LAST EIGHT LANDING GEAR OVERHAULED.Aug 2, 1999 · Beech 1900D · Main Landing Gear Strut/Axle/TruckSDR C2XA99CL060Pcu · out of adjustCLE - FLT 3023 - THE CREW REPORTED THE PROPS ONLY REACHED 1,650 RPM AT FULL POWER. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE NR 1 AND NR 2 ENGINE HIGH PROP RPM IAW BEECH 1900D MM 61-20-00 AND PERFORMED OPERATIONAL CJul 31, 1999 · N87551 · Beech 1900D · Propeller Controlling SystemSDR C2XA99CL062Bleed Air System · malfunctionedFWA - FLT 120G - THE CREW REPORTED THAT SMOKE ENTERED THE CABIN IN-FLIGHT DURING SINGLE ENGINE SIMULATION, THE AIRCRAFT RETURNED TO FWA WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE RIGHT ENVIRONMENTAL BLEED AIR SYSTEM ON MEL NR 21-14 CONTROL NR 183678 CATJul 29, 1999 · N69549 · Beech 1900D · Pneumatic Distribution SystemSDR 99ZZZX3715Altimeter · reads highALTIMETER FOUND TO BE INDICATING 50 FEET HIGH FROM 1,000 FEET TO 2,500 FEET. ALL OTHER TEST POINTS WERE WITHIN LIMITS.Jul 29, 1999 · N255GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 99ZZZX3077Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FIVE CRACKS.Jul 29, 1999 · Beech 1900D · Propeller Blade SectionSDR 99ZZZX3704Directional Gyro · failedFLIGHT CREW REPORTED THE COMPASS CARD DID NOT MOVE IN THE FREE OR SLAVED MODES WHEN THE AIRCRAFT WAS TURNED. REMOVED AND REPLACED DIRECTIONAL GYRO. SUBMITTER STATED THIS IS THE FOURTH TIME THIS GYRO HAS HAD THIS PROBLEM REPORTED (DIFFERENT AIRCRAFT). ALL SHJul 26, 1999 · N154GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 99ZZZX3419Altimeter · malfunctionedALERT LIGHT IN ALTIMETER COMES ON WHEN POWER IS APPLIED. THIS UNIT WAS REMOVED FROM STOCK AND HAD BEEN OVERHAULED AND WAS BACK FOR SUBSEQUENT REPAIRS UNDER WARRANTY ON TWO OCCASIONS SINCE MARCH 2, 1999. INITIAL TESTS BY INSTALLER FOUND THAT PINS B AND E WERE Jul 26, 1999 · N255GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 99ZZZX3010Centering Arm · misalignedIT WAS DISCOVERED UPON OPS CHECK OF NEWLY INSTALLED NOSE GEAR JUST OUT OF OVERHAUL, THAT THE NOSE WHEEL WAS NOT CENTERING PROPERLY. AFTER FURTHER EXAMINATION, IT WAS DETERMINED THE CYLINDER ASSY (P/N 114-820022-17) CENTERING ARM ATTACHMENT HOLES (6) WERE ROTAJul 26, 1999 · Beech 1900D · Landing Gear Steering SystemSDR C2XA99CL061Prop Control · malfunctionedCLE - FLT 3154 - THE CREW REPORTED ON TAKEOFF ROLL, THE NR 1 PROPELLER ONLY WENT TO 1,650 RPM AND THE NR 2 PROPELLER ONLY WENT TO 1,670 RPM. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED GROUND OPERATIONAL CHECKS IAW BEECHJul 24, 1999 · N87551 · Beech 1900D · Propeller Controlling SystemSDR MASA99125Hook Mechanism · wornPHX/FMN - FLT 6462 - THE CAPTAIN REPORTED A FORWARD UPPER COWL LOOSE. THE AIRCRAFT RETURNED TO PHX. MAINTENANCE PERFORMED AN INSPECTION OF THE COWL AND FOUND ONE LOCK PARTIALLY LOOSE. THEY RESECURED THE COWL AND DEEMED THE ASSEMBLY AND THE AIRCRAFT AIRWORTHJul 23, 1999 · N76ZV · Beech 1900D · Engine Cowling SystemSDR MASA99123Warning · activatedPHL/LEB - FLT 5274 - THE AIRCRAFT HAD A RIGHT BLEED AIR FAIL ANNUNCIATOR LIGHT ILLUMINATE AND THE CREW DECLARED AN EMERGENCY. MAINTENANCE ACTON WAS DEFERRED PER 21-3-2. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)Jul 22, 1999 · N120YV · Beech 1900D · Pneumatic Indicating SystemSDR 99ZZZX3498Altimeter · bindingKOLLSMAN KNOB FOUND BINDING WHEN REMOVED FROM STOCK. RETURNED.Jul 22, 1999 · N184UX · Beech 1900D · Altimeter, Barometric/EncoderSDR CA990728063Bearing · failed(CAN) CREW REPORTED PREVIOUS PROBLEMS WITH GENERATOR STAYING ON-LINE. DURING TAXI TO HANGAR, AREA SMOKE WAS OBSERVED FROM ENGINE COMPARTMENT. STARTER WAS REMOVED AND REPLACED DUE TO REAR BEARING FAILURE.Jul 20, 1999 · Beech 1900D · Starter-GeneratorSDR MASA99120Warning · activatedIFP/PHX - FLT 6377 - THE CREW DECLARED AN EMERGENCY DUE TO A CABIN DOOR ANNUNCIATOR ILLUMINATED. THE AIRCRAFT LANDED IN PHX SAFELY. MAINTENANCE ACTION WAS DEFERRED PER MEL 52-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)Jul 17, 1999 · N93ZV · Beech 1900D · Door Warning SystemSDR C2XA99CL056Vertical Gyro · malfunctionedCLE - FLT 3056 - THE CREW REPORTED THE NR 2 EADI DISPLAY WENT BLANK IN-FLIGHT MOMENTARILY. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 VERTICAL GYRO IAW COLLINS CMM AND PERFORMED OPERATIONAL CHECKS WIJul 16, 1999 · N87557 · Beech 1900D · Attitude Gyro and Indicating SystemSDR 99ZZZX3517Servo · mismanufacturedAIRCRAFT YAWS LEFT AND RIGHT UNCOMMANDED (SAME CONDITION WITH YAW DAMP 'OFF'). SELECTED RUDDER BOOST TO 'OFF' AND CONTINUED FLIGHT WITH NO ADDITIONAL PROBLEMS. TROUBLESHOOTING BY MAINTENANCE PERSONNEL FOUND PRIMARY RUDDER SERVO TO BE DRIVING RUDDER IN WRONG Jul 15, 1999 · N192GL · Beech 1900D · Autopilot Main ServoSDR 99ZZZX2787Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FIVE CRACKS.Jul 13, 1999 · Beech 1900D · Propeller Blade SectionSDR 99ZZZX2786Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.Jul 13, 1999 · Beech 1900D · Propeller Blade SectionSDR MASA99118Warning · activatedPHX/YUM - FLT 6389- THE AIRCRAFT IN CRUISE WHEN THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND LANDED IN YUM WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION WAS DEFERRED PER MEL 52-1. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)Jul 12, 1999 · N93ZV · Beech 1900D · Door Warning SystemSDR 99ZZZX3261Wire · failedNR 2 COMM CONTROL HEAD STARTED SMOKING ON CLIMB-OUT. REMOVED AND REPLACED NR 2 COMM CONTROL (PN 622-6520-008) AND REPAIRED CHAFED AND BURNED WIRES ON PIN 28 AND PIN 37 OF CONNECTOR J176. WIRING HAD CHAFED AND SHORTED OUT. COMM CONTROL CIRCUIT BOARD WAS BURNJul 12, 1999 · N122UX · Beech 1900D · Communications System WiringSDR MASA99117Engine · failedIAD/SYR - FLT 5299 - RIGHT ENGINE OIL PSI DROPPED IN-FLIGHT. THE CREW DECLARED AN EMERGENCY AND DIVERTED ITH. THE AIRCRAFT LANDED WTHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE. OPS CHECK GOOD. THE AIRCRAFT RETURNED TO SERVICE. (XJul 10, 1999 · N124YV · Beech 1900D · Engine (Turbine/Turboprop)SDR CA990728059Line Cover · cracked(CAN) AFTER TAKEOFF, A METALLIC BANGING OR RATTLING NOISE WAS HEARD IN COCKPIT AND CABIN. UPON INSPECTION, IT WAS DISCOVERED THAT THE HYDRAULIC LINE COVER IN THE NOSE WHEELWELL WAS SEVERELY CRACKED. THE CRACKS ALLOWED THE PART TO VIBRATE AND CAUSE THE NOISE.Jul 8, 1999 · Beech 1900D · Hydraulic System, MainSDR CA990719003Switch · failed(CAN) PILOT REPORTED ON APPROACH TO CYBL, GEAR WAS SELECTED DOWN, ALL GEAR WENT DOWN, ALL LIGHTS ILLUMINATED, BUT PILOT NOTCED LT MAIN DOWN AND LOCKED LIGHT WAS A DIM GREEN. ON APPROACH TO YVR, GEAR WAS SELECTED DOWN, LT INDICATION WAS NOTED TO BE EVEN DIMMERJul 8, 1999 · Beech 1900D · Landing Gear Position and WarningSDR CA990728062Switch · defective(CAN) DURING CRUISE FLIGHT, THE FLIGHT CREW NOTED THE INTRANSIT RED LIGHT ILLUMINATE. MAINTENANCE FOUND THE LT UPLOCK SWITCH DEFECTIVE.Jul 6, 1999 · Beech 1900D · Landing Gear Position and WarningSDR MASA99111Fuel Pump · failedFLT 5906 - PIT-FKL - AFTER TAKEOFF, THE AIRCRAFT EXPERIENCED A FUEL PUMP FAILURE ON THE NR 1 ENGINE. THE CREW DECLARED AN EMERGENCY, AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION WAS DEFERRED PER MEL 28-5. THE AIRCRAFT WAS RETURNED Jul 1, 1999 · N173YV · Beech 1900D · Engine Fuel PumpSDR 99ZZZM619Altimeter · failedPILOT REPORTED THAT THE ALTIMETER INDICATED 100 FEET LOW ON THE GROUND. REMOVED AND REPLACED PILOTS ALTIMETER. BENCH CHECK VERIFIED THAT THE ALTIMETER INDICATED PLUS/MINUS 100 FT AT ALL TEST POINTS. THIS IS THE 5TH REPORTED SUCH FAILURE OF THIS ALTIMETER. Jun 30, 1999 · N211UX · Beech 1900D · Altimeter, Barometric/EncoderSDR MASA99108Engine · failedROW/DFW - FLT 1030 - AIRCRAFT WAS ON CLIMB-OUT WHEN THE RIGHT ENGINE TORQUE AND OIL PRESSURE DECREASED AND THE OIL TEMPERATURE INCREASED. THE CAPTAIN REDUCED POWER ON THE RIGHT ENGINE, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS RETURNED TO THE FIELD. MAIJun 28, 1999 · N112ZV · Beech 1900D · Engine (Turbine/Turboprop)SDR GLBA99024Computer · inoperableRUDDER HAD FULL DEFLECTION WHEN YAW DAMPER ENGAGED. REPLACED YAW DAMPER COMPUTER. (X)Jun 25, 1999 · N192GL · Beech 1900D · Autopilot SystemSDR CA990728057Weather Radar · malfunctioned(CAN) AIRCRAFT ENTERED A CLOUD, DURING CRUISE FLIGHT, THAT WAS NOT SHOWING ON THE RADAR INDICATORS. THIS CLOUD CONTAINED HAIL WHICH STRUCK THE AIRCRAFT LEADING EDGES CAUSING COSMETIC DAMAGE. THE CREW REPORTED THAT THIS CLOUD WAS NOT SHOWING ON THE SCREENS ASJun 25, 1999 · Beech 1900D · Weather Radar SystemSDR CA990728056Weather Radar · malfunctioned(CAN) AIRCRAFT ENTERED A CLOUD DURING CRUISE FLIGHT AT APPROXIMATELY 16,000 FEET. THE RADAR WAS TURNED ON AND BEING MONITORED. THE CLOUD WAS NOT SHOWN ON THE INDICATORS FOR EITHER CREW MEMBER. THE CLOUD CONTAINED HAILTHE SIZE OF LARGE PEAS TO THE SIZE OF MAJun 24, 1999 · Beech 1900D · Weather Radar SystemSDR GLBA99023Transmitter · failedRIGHT ENGINE WOULD NOT MAKE TORQUE WORN O-RING ON BLEED VALVE. REPLACED O-RING AND REPLACED TORQUE TRANSMITTER, WOULD NOT CALIBRATE. (M)Jun 23, 1999 · N96UX · Beech 1900D · Engine BMEP/Torque IndicatingSDR C2XA99CL048Connector · contaminatedCLE - FLT 3169 - THE CREW REPORTED THE RADAR WAS PAINTING RED AT FULL TILT UP, THE AIRCRAFT DID A AIR RETURN TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED MOISTURE FROM THE R/T CONNECTOR AND PERFORMED RADAR GROUND CHECKS IAW BEECHCRAFT MM 34-40-0Jun 23, 1999 · N87550 · Beech 1900D · Weather Radar SystemSDR 99ZZZX3705Altimeter · failedPILOT REPORTED THE ADJUSTMENT KNOB WOULD SET THE ALTITUDE, BUT WOULD NOT ADJUST THE BAROMETRIC WINDOW SETTING. REMOVED AND REPLACED PILOT'S ALTIMETER. DEFECT WAS VERIFIED DURING BENCH CHECK.Jun 23, 1999 · N260GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 99ZZZX3703Altimeter · malfunctionedPILOT REPORTED THE PILOT'S ALTIMETER TO BE READING 150 FEET HIGH. REMOVED AND REPLACED PILOT'S ALTIMETER. SUBSEQUENT BENCH CHECK VERIFIED ALTIMETER TO BE INDICATING 150 FEET HIGH. THE BAROMETRIC WINDOWS DISPLAYED 1,017 MILLIBARS AT 29.92 IHG.Jun 23, 1999 · N153GL · Beech 1900D · Altimeter, Barometric/Encoder
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