Raytheon 1900D

Service difficulty reports · 7,152

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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 = '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 S2YA97005Engine · contaminatedKE/SBN - FLT 1162 - THE FLIGHT CREW SMELLED AN UNUSUAL ODOR WHEN THE BLEED AIR VALVES WERE TURNED ON AFTER TAKEOFF. THE CREW PERFORMED AN AIR TURNBACK TO MKE AND LANDED WITHOUT ANY OTHER PROBLEMS. ONCE ON THE GROUND, MAINTENANCE INSPECTED THE A/C, THEY NOTEDFeb 19, 1997 · N881SK · Beech 1900D · Engine (Turbine/Turboprop)SDR S2YA97004Seal · out of positionMKE/DSM - FLT 1751 - FLIGHT CREW PERFORMED AN AIR TURNBACK DUE TO THE CABIN DOOR SEAL SQUEALING VERY LOUDLY. THE DOOR SEAL HAD BEEN CHANGED BY MAINTENANCE PRIOR TO DEPARTURE. WHEN THE AIRCRAFT LANDED, MAINTENANCE INSPECTED THE DOOR SEAL AND FOUND A SMALL PORFeb 16, 1997 · N91SK · Beech 1900D · Passenger/Crew DoorsSDR GLBA97028Prop Deice Boot · missingRDU - RIGHT PROPELLER DE-ICE BOOT MISSING. MAINTENANCE INSTALLED NEW BOOT. (X)Feb 14, 1997 · N202ZK · Beech 1900D · Propeller Deice Boot SectionSDR GLBA97025Switch · closedCMH - LANDING GEAR WOULD NOT EXTEND. GEAR MANUALLY EXTENDED. MAINTENANCE REPLACED HYDRAULIC SERVICE VALVE MICROSWITCH. (M)Feb 11, 1997 · N204YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 97ZZZX852Bearing · brokenPROPELLER WAS DISASSEMBLED DUE TO LOOSE BLADES (IN EXCESS OF .75 INCH FORE/AFT). ON INSPECTION, FOUND BLADE S/N 930 INNER BEARING RACE DAMAGED. ONE SIDE OF SPLIT RACE CRACKED INTO DOWN CENTER OF BALL RIDE AREA AND OTHER HALF OF SPLIT RACE CRACKED UP ABOUT ONFeb 8, 1997 · N94UX · Beech 1900D · Propeller Blade SectionSDR 97ZZZX851Bearing · splitPROPELLER WAS DISASSEMBLED DUE TO 'LOOSE' BLADES (IN EXCESS OF .75 INCH FORE/AFT). ON INSPECTION, FOUND BLADE S/N 982 INNER BEARING RACE (1 SIDE OF SPLIT BEARING) SPLIT (CRACKED) 1 INCH THROUGH CENTER OF BALL RUN AREA, BALLS WERE PITTED.Feb 8, 1997 · N94UX · Beech 1900D · Propeller Blade SectionSDR S2YA97009Downlock Switch · dirtySBN/MKE - FLT 1161 - DURING THE LANDING APPROACH INTO MKE, CREW HAD TO CYCLE THE LANDING GEAR 3 TIMES IN ORDER TO GET A NOSE GEAR DOWN AND LOCKED INDICATION. THE FLIGHT CREW DECLARED AN EMERGENCY AND LANDED AT MKE WITHOUT INCIDENT. WHEN MAINTENANCE TROUBLESHFeb 6, 1997 · N85SK · Beech 1900D · Landing Gear Position and WarningSDR MASA97009Fcu · malfunctionedFLT 5264 - RIGHT ENGINE COMPRESSOR STALLED BELOW 2700 LBS TORQUE. AN EMERGENCY WAS DECLARED AND THE ENGINE WAS FEATHERED AND SHUTDOWN AS A PRECAUTIONARY MEASURE. T/S SYSTEM, CLEANED THE P3 AND PY LINES. REMOVED AND REPLACED BLEED VALVE AND FCU. PERFORMED GFeb 6, 1997 · N78YV · Beech 1900D · Fuel Control/Turbine EnginesSDR 97ZZZM540Bleed Valve Assy · malfunctionedFLT 5264 - RIGHT ENGINE COMPRESSOR STALLED BELOW 2700 LBS TORQUE. AN EMERGENCY WAS DECLARED AND THE ENGINE WAS FEATHERED AND SHUTDOWN AS A PRECAUTIONARY MEASURE. T/S SYSTEM, CLEANED THE P3 AND PY LINES. REMOVED AND REPLACED BLEED VALVE AND FCU. PERFORMED GFeb 6, 1997 · N78YV · Beech 1900D · Compressor Bleed ValveSDR C2XA97CL012Transducer · failedCLE - FLT 3151 - CREW REPORTED THAT THE STALL WARNING CAME ON AT TAKEOFF AND REMAINED ON. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLAFED THE STALL WARNING COMPUTER AND LIFT TRANSDUCER. THE OPERTIONAL CHECKS WERE UNSUFeb 4, 1997 · N38537 · Beech 1900D · Stall Warning SystemSDR GLBA97016Brakes · reqd serviceSPI - LEFT BRAKE PEDAL GOES ALL THE WAY TO THE FLOOR. MAINTENANCE BLED BRAKE SYSTEM. (X)Feb 3, 1997 · N225GL · Beech 1900D · Landing Gear Brake SystemSDR GLBA97018Connector · dirtyORD - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE CLEANED CANNON PLUGS ON CONTROL HANDLE. (X)Feb 2, 1997 · N10746 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR CA970916004Line · cracked(CAN) ON INSPECTION, HYDRAULIC LEAK FOUND UNDER LT CENTER SECTION. INVESTIGATION REVEALED LEAK LOCATION WAS FROM LINE BETWEEN POWER PACK AND FILLER. CRACKED LINE REPLACED.Jan 31, 1997 · Beech 1900D · Hydraulic System, MainSDR S2YA970003Press/Temp Ind · failedOMA/MCI - FLT 1059 - FLIGHT CREW NOTICED THE LT ENGINE OIL PRESSURE WAS AT 60 PSI DURING CLIMB OUT FROM OMA. THEY DECIDED TO RETURN TO OMA. MAINTENANCE CHECKED THE ENGINE OIL, INSPECTED THE OIL FILTER, AND THE CHIP DETECTOR WITH NO PROBLEMS FOUND. THEY REPLJan 30, 1997 · N145SK · Beech 1900D · Engine Oil TemperatureSDR S2YA970002Transducer · malfunctionedCGV/MKE - FLT 1027 - AFTER FLIGHT CREW REACHED CRUISING ALTITUDE, ENGINES WERE SET TO CRUISE POWER. THE CREW NOTICED THE LT ENGINE OIL PRESSURE AT 65 PSI. THEY DECLARED AN EMERGENCY AND DIVERTED TO IND. MAINTENANCE INSPECTED THE LT ENGINE OIL FILTER, CHECKEJan 29, 1997 · N145SK · Beech 1900D · Engine Oil PressureSDR C2XA97CL009Vertical Gyro · failedCLE - FLT 3239 - CREW REPORTED THAT THE FIRST OFFICERS ELECTRONIC ATTITUDE DIRECTOR INDICATOR FAILED IN FLIGHT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE NR 2 VERTICAL GYRO, ALL OPERATIONAL CHECKS WERE GOOD Jan 29, 1997 · N49543 · Beech 1900D · Attitude Gyro and Indicating SystemSDR CA970326001Strut · flat(CAN) NLG STRUT LOST AIR PRESSURE ON TAKEOFF. GEAR RETRACTED NORMALLY. WHEN GEAR SELECTED DOWN THE MAIN EXTENDED, BUT THE NOSE GEAR DID NOT. A/C LANDED WITH THE MAIN DOWN AND NOSE RETRACTED ON RUNWAY. NOSE WHEEL FORK WAS CAUGHT ON THE RT GEAR FAIRING WHICHJan 28, 1997 · Beech 1900D · Nose/Tail Landing GearSDR GLBA97015Switch · openRDU - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED SERVICE VALVE MICROSWITCH. (M)Jan 26, 1997 · N204YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR MASA97008Blower · failedFLT 5428 - JAN - CREW NOTICED BURNING SMELL HALFWAY THROUGH FLIGHT. FOLLOWED EMERGENCY PROCEDURES, SMOKE CLEARED AND CONTINUED FLIGHT. MAINTENANCE FOUND AFT VENT BLOWER INOP. REPLACED AFT VENT BLOWER. (M)Jan 22, 1997 · N46YV · Beech 1900D · Air Distribution FanSDR MASA97007Flap · damagedSEA - FLT 7833 - RIGHT OUTBOARD FLAP BOUND AND DAMAGED. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP AND ATTACHED HARDWARE. ACFT TTL HRS: 7,027. ACFT TTL CYC: 10,642. (X)Jan 21, 1997 · N75ZV · Beech 1900D · Trailing Edge FlapsSDR 98ZZZX627Actuator · failedPHL - FLT 4474 - GEAR WOULD NOT EXTEND. LT MLG ACTUATOR LEAKING. REMOVED AND REPLACED LT MLG ACTUATOR. GROUND OPS CHECK IAW CHAPTER 32.Jan 21, 1997 · N854CA · Beech 1900D · Landing Gear ActuatorSDR MASA97006Power Lever Sw · out of adjustFLT 7587 - MTJ - LEFT ENGINE AUTOFEATHERED BRIEFLY ON DESCENT, LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED POWER LEVER SWITCHES. (M)Jan 20, 1997 · N42YV · Beech 1900D · Power LeverSDR MALA97005Connector · dirtyPIT - FLT 5869 - STALL HEAT ANNUNCIATOR ILLUMINATED IN FLIGHT ONLY WHEN GEAR IS UP AND STALL HEAT ACTIVATED. TROUBLESHOT SYTEM. CLEANED CANNON PLUG AND TERMINALS ON A150 PC BOARD. FOUND CORROSION ON CANNON PLUG PINS TO GEAR WELL SWITCHES. CLEANED AS NEEDEDJan 16, 1997 · N39ZV · Beech 1900D · Stall Warning SystemSDR 97ZZZM246Ice Vane · missing rivetDURING AN ROUTINE INSPECTION, A RIVET IN THE ICE VANE WAS FOUND MISSING. INSPECTION OF THE COMPRESSOR REVEALED THE BLIND RIVET WENT THOUGH THE ENGINE. THE GAS GEN WAS REPLACED DUE TO FOD. (M)Jan 16, 1997 · N178YV · Beech 1900D · Air Intake Anti/De-Ice SystemSDR C2XA97CL007Safety Switch · failedCLE - FLT 3080 - CREW REPORTED AFTER TAKEOFF AND DURING CLIMB, THE FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE LEFT HAND FLAP SAFETY SWITCH IAW B1900D MM 27-50-00, ALL OPERATIONAL CHECKS WEJan 13, 1997 · N81533 · Beech 1900D · Trailing Edge Flap Control SystemSDR NSVA97005Fuel Filter · trippedRIGHT LOW PRESSURE FUEL FILTER ASSEMBLY BYPASS PIN EXTENDED. REMOVED FILTER ELEMENT, CLEANED. NO FUEL CONTAMINATION OR FAULTY ELEMENT NOTED. SUSPECT FALSE INDICATION. (X)Jan 12, 1997 · N215CJ · Beech 1900D · Aircraft Fuel Distribution SystemSDR C2XA97CL006Relay Board · failedCLE - FLT 3019 - CREW REPORTED THE LEFT SIDE AUTOFEATHER DISARMED ONCE AIRBORNE. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED AUTOFEATHER RELAY BOARD, P/N 129-364079-7, IAW B1900D MM 61-21-00. MAINTENANCE ALSO REMOVED Jan 12, 1997 · N81533 · Beech 1900D · Propeller Controlling SystemSDR S2YA970001Wire Harness · chafedMKG/MKE - FLT 1042 - FLIGHT CREW SELECTED LANDING GEAR HANDLE DOWN FOR LANDING, THE GEAR FAILED TO EXTEND. THE CREW EXTENDED THE LANDING GEAR USING EMERGENCY EXTENSION SYSTEM. AN UNEVENTFUL LANDING WAS MADE. MAINTENENANCE TROUBLESHOT THE SYSTEM. FOUND LANDJan 11, 1997 · N81SK · Beech 1900D · Landing Gear System WiringSDR MASA97003Windshield · failedRKS - FLT 7701 - PILOT WINDSHIELD SMOKED IN-FLIGHT. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED WINDSHIELD. (X)Jan 10, 1997 · N37YV · Beech 1900D · Flight Compartment WindowsSDR MASA97002Gear · collapsedFLT 5326 - FLT CREW ABORTED TAKEOFF, ON LANDING, THE NOSE GEAR COLLAPSED CAUSING DAMAGE TO THE PROPELLERS AND FUSELAGE. AIRCRAFT DAMAGE WAS REPAIRED. GROUND OPS CHECK WAS PERFORMED NO DISCREPANCIES WERE NOTED. TEST FLIGHT WAS PERFORMED SATISFACTORILY AND AIJan 10, 1997 · N139ZV · Beech 1900D · Nose/Tail Landing GearSDR MASA97001Selector Valve · malfunctionedFLG - FLT 5260 - PILOT REPORTED THAT GEAR EXTENDED IN FLIGHT WITH GEAR HANDLE IN UP POSITION. A/C WAS FERRIED TO FMN. DURING TEST FLIGHT, GEAR WAS CYCLED 3 TIMES. ON THE THIRD RETRACTION ATTEMPT, THE GEAR DID NOT RETRACT WITH THE HANDLE IN THE UP POSITION. Jan 9, 1997 · N154ZV · Beech 1900D · Landing Gear SelectorSDR GLBA97004Squat Switch · dirtyBNA - GEAR HAD TO BE EXTENDED MANUALLY. MAINTENANCE CLEANED RT SQUAT SWITCH AND COULD NOT DUPLICATE. TEST FLIGHT SATISFACTORY. (M)Jan 9, 1997 · N204YV · Beech 1900D · Landing Gear Position and WarningSDR 97ZZZX999Hyd Power Pack · malfunctionedFLG - FLT 5260 - PILOT REPORTED THAT GEAR EXTENDED IN FLIGHT WITH GEAR HANDLE IN UP POSITION. A/C WAS FERRIED TO FMN. DURING TEST FLIGHT, GEAR WAS CYCLED 3 TIMES. ON THE THIRD RETRACTION ATTEMPT, THE GEAR DID NOT RETRACT WITH THE HANDLE IN THE UP POSITION. Jan 9, 1997 · N154ZV · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR 97ZZZX1000Gear Handle · malfunctionedFLG - FLT 5260 - PILOT REPORTED THAT GEAR EXTENDED IN FLIGHT WITH GEAR HANDLE IN UP POSITION. A/C WAS FERRIED TO FMN. DURING TEST FLIGHT, GEAR WAS CYCLED 3 TIMES. ON THE THIRD RETRACTION ATTEMPT, THE GEAR DID NOT RETRACT WITH THE HANDLE IN THE UP POSITION. Jan 9, 1997 · N154ZV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR C2XA97CL005Limit Switch · out of adjustCLE - FLT 3267 - CREW REPORTED THAT AFTER TAKEOFF, THE FLAPS WOULD NOT RETRACT AND REMAINED AT 17 DEGREES. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE LEFT HAND FLAP SPLIT LIMIT SWITCH IAW B1900D MM 27-50-05. OPERATIONAL CHECJan 8, 1997 · N17534 · Beech 1900D · Trailing Edge Flap Control SystemSDR NSVA97004Fuel Filter · trippedRIGHT WING LOW PRESSURE FUEL FILTER ASSEMBLY BYPASS PIN EXTENDED. INSTALLED NEW FILTER ASSEMBLY, P/N 114-389032-8, S/N 00950. INSPECTION OF FILTER DID NOT REVEAL FUEL CONTAMINATION OR FAULTY ELEMENT. SUSPECT FALSE INDICATION. (X)Jan 7, 1997 · N215CJ · Beech 1900D · Aircraft Fuel Distribution SystemSDR GLBA97002O-Ring · failedSPW - RIGHT 'BLEED AIR FAIL' ANNUNCIATOR ILLUMINATED AFTER TAKEOFF. MAINTENANCE REPLACED O-RINGS IN BLEED AIR LINE. (M)Jan 5, 1997 · N211UX · Beech 1900D · Pneumatic Distribution SystemSDR NSVA97002Fuel Filter · trippedRIGHT ENGINE LOW PRESSURE FUEL FILTER ASSEMBLY BYPASS PIN EXTENDED. REMOVED AND CLEANED FILTER ELEMENTS. NO FUEL CONTAMINATION NOTED. FILTER ELEMENT CONDITION, SUSPECT FALSE INDICATION. (X)Jan 3, 1997 · N215CJ · Beech 1900D · Aircraft Fuel Distribution SystemSDR GLBA97001Retract Mech · malfunctionedRDU - GEAR EXTENDED 15 SECONDS AFTER HANDLE WAS EXTENDED. MAINTENANCE CYCLED GEAR NUMEROUS TIMES AND COULD NOT DUPLICATE. (M)Jan 3, 1997 · N204YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR C2XA97CL001Compressor · blades damagedCLE - DURING A SCHEDULED INSPECTION, THE LEFT ENGINE COMPRESSOR BLADES WERE FOUND TO DAMAGED BEYOND LIMITS BY FOREIGN OBJECTS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW B1900D MM 71-00-00, ALL RIGGING AND OPERATIONAL CHECKS WERE GOOD IAW B1900D MM Jan 3, 1997 · N16540 · Beech 1900D · Turbine Engine Compressor SectionSDR S2YA97008Oxygen Lines · failedDURING THE TIME CHANGE OF OXYGEN BOTTLES, MANY A/C HAD FILL AND CROSS-OVER OXYGEN LINE FITTINGS CRACKED. THE LINE FITTINGS, MADE OF BRASS HAD ALL CRACKED UP THE SIDE OF THE B-NUT. WHEN TESTING THE LINES BEFORE REMOVAL, MOST SHOWED SIGNS OF LEAKING. ONE LINEJan 1, 1997 · Beech 1900D · Oxygen SystemSDR S2YA97006Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N145SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR 97ZZZX1812Oxygen Lines · failedDURING THE TIME CHANGE OF OXYGEN BOTTLES, MANY A/C HAD FILL AND CROSS-OVER OXYGEN LINE FITTINGS CRACKED. THE LINE FITTINGS, MADE OF BRASS HAD ALL CRACKED UP THE SIDE OF THE B-NUT. WHEN TESTING THE LINES BEFORE REMOVAL, MOST SHOWED SIGNS OF LEAKING. ONE LINEJan 1, 1997 · Beech 1900D · Oxygen SystemSDR 97ZZZX1811Oxygen Lines · failedDURING THE TIME CHANGE OF OXYGEN BOTTLES, MANY A/C HAD FILL AND CROSS-OVER OXYGEN LINE FITTINGS CRACKED. THE LINE FITTINGS, MADE OF BRASS HAD ALL CRACKED UP THE SIDE OF THE B-NUT. WHEN TESTING THE LINES BEFORE REMOVAL, MOST SHOWED SIGNS OF LEAKING. ONE LINEJan 1, 1997 · Beech 1900D · Oxygen SystemSDR 97ZZZX1796Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N901SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR 97ZZZX1795Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N891SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR 97ZZZX1794Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N881SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR 97ZZZX1793Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N831SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR 97ZZZX1792Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N801SK · Beech 1900D · Attitude Gyro and Indicating SystemSDR 97ZZZX1791Vertical Gyro · failedDURING THE MONTH OF JANUARY, SEVEN 332D-11T VERTICAL GYROS (P/N 622-4565-001) FAILED. THE TIMES FOR THE VG'S WERE: 1,639.3 HRS ON N NR 145SK; 5,375.1 HRS ON N NR 79SK; 6,125.4 ON N NR 801SK; 2,328.9 HRS ON N NR 831SK; 3,063.1 HRS ON N NR 881SK; 6,820.9 HRSJan 1, 1997 · N79SK · Beech 1900D · Attitude Gyro and Indicating System
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