Beech 1900C

Service difficulty reports · 1,841

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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 = '1900C'
  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 95ZZZX6637Windshield · brokenSPW - DURING APPROACH, A MALLARD CONTACTED THE LT WINDSHIELD. THE WINDSHIELD COBWEBBED AND HAD A SMALL AMOUNT OF SHATTER. THE UPPER WINDSHIELD BEAM AND LT WINDSHIELD WERE REPLACED. REFERENCE OPERATOR CONTROL NR 95ZZZX6636.Nov 2, 1995 · N60UE · Beech 1900C · Flight Compartment WindowsSDR 95ZZZX6636Beam · bentSPW - DURING APPROACH, A MALLARD CONTACTED THE LT WINDSHIELD. THE WINDSHIELD COBWEBBED AND HAD A SMALL AMOUNT OF SHATTER. THE UPPER WINDSHIELD BEAM AND LT WINDSHIELD WERE REPLACED. REFERENCE OPERATOR CONTROL NR 95ZZZX6637.Nov 2, 1995 · N60UE · Beech 1900C · Fuselage Miscellaneous StructureSDR 95ZZZX6635Power Pack Motor · inoperativeYKN - CREW REPORTED THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. THEY ELECTED TO DIVERT TO GRI, MANUALLY LOWERED THE GEAR, AND ACCOMPLISHED A SUCCESSFUL LANDING. MAINTENANCE CHANGED THE POWER PACK MOTOR, THE RT SQUAT SWITCH, AND THE POSITION INDICATOR DINov 2, 1995 · N123UE · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZX6647Fire Loop Clamp · brokenMCI - FLT 2111 - DURING TAKEOFF AND CLIMB APPROXIMATELY 6:00 A.M., RT T-HANDLE ILLUMINATED FOR ABOUT 10 SECONDS AND EXTINGUISHED. PLANE RETURNED TO GRI FOR MAINTENANCE. AIRCRAFT WAS HEADING TO MCI, FLT 2111. REMOVED AND REPLACED BROKEN FIRE LOOP CLAMP, PN 7Nov 1, 1995 · N125GP · Beech 1900C · Fire DetectionSDR 95ZZZX6644Squat Switch · out of adjustGSP/DAY - FLT 2300 - DURING CLIMB, GEAR WOULD NOT RETRACT. AIR RETURNED TO CMH GATE AND RETURNED TO MAINTENANCE. UPON INSPECTION, MAINTENANCE ADJUSTED SQUAT SWITCH. PERFORMED SEVERAL GEAR SWINGS ON GROUND. AIRCRAFT RELEASED FOR FLIGHT.Nov 1, 1995 · N120GP · Beech 1900C · Landing Gear Position and WarningSDR PLG103195G3Warning Light · illuminatedSYR - FLT 4372 - AFTER TAKEOFF, THE FORWARD CABIN DOOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO SYR LANDING WITHOUT INCIDENT. THE DOOR WARNING SYSTEM WAS MEL'D AND THE AIRCRAFT RETURNED TO SERVICE. THIS WAS THE LAST DAY OF SERVICE FOR THE AIRCRAFOct 31, 1995 · N76YV · Beech 1900C · Door Warning SystemSDR 96ZZZX130Gear Switch · out of adjustMIA/MCO - FLT 427 - PILOT REPORT: NOSE GEAR UNSAFE INDICATION WHILE AIRBORNE, SAFE INDICATION ON GROUND. MAINTENANCE: HAD AIRCRAFT FERRIED TO MIA, GEAR DOWN AND LOCKED, TROUBLESHOT AND ADJUSTED NOSE GEAR DOWNLOCK SWITCH. AIRCRAFT RELEASED.Oct 31, 1995 · N195GA · Beech 1900C · Landing Gear Position and WarningSDR PLG103095G7Trim Actuator · failedFLT NR 4724 - BOS - ON CLIMB-OUT, ELEVATOR TRIM WAS SELECTED, WHICH CONTINUED TO TRAVEL BEYOND THE SELECTED COMMAND. THE CREW SELECTED THE TRIM TO OFF. MANUAL TRIM WAS SELECTED, WHEREUPON THE TRIM SYSTEM WAS FOUND FROZEN. THE AIRCRAFT RETURNED TO BOS LANDINOct 30, 1995 · N3069K · Beech 1900C · Elevator Control SystemSDR 95ZZZX6596Bus Tie · openedDURING CRUISE FLIGHT, LT BUS TIE OPEN WARNING FOLLOWED BY LT DC GENERATOR FAIL WARNING. CAPTAIN LOST HEADSET AUDIO WHICH IS POWERED FROM LT GENERATOR BUS. THIS OCCURRENCE CAUSED LOSS OF COMMUNICATION BETWEEN COCKPIT CREW AT A TIME CREW COORDINATION IS CRITICOct 30, 1995 · N160AM · Beech 1900C · DC Power Distribution SystemSDR 95ZZZM699Retract Mech · failedFLT NR 479 - TPA-MIA - LANDING GEAR FAILED TO EXTEND, BREAKER POPPED. INSPECTED HYDRAULIC SYSTEM, ACCUMULATION SYSTEM AND ELECTRICAL SYSTEM NO DEFECTS NOTED. SWUNG GEAR ON JACKS NO DEFECTS NOTED.Oct 30, 1995 · N199GA · Beech 1900C · Landing Gear Retraction/Extension SystemSDR PLG103095G2Control Pnl · wetFLT NR 3101 - ON CLIMB-OUT FROM LEB, A LOUD SQUEAL WAS HEARD OVER THE HEADSETS WHICH COULD NOT BE CLEARED. THE AIRCRAFT RETURNED TO LEB, LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT WHERE THE AUDIO CONTROL PANEL AND CO-PILOT MIC JACK Oct 28, 1995 · N818BE · Beech 1900C · Audio Integrating SystemSDR 95ZZZX6634Le Skin · crackedMSP - CREW REPORTED A BIRDSTRIKE ON THE RT WING LEADING EDGE 4 FEET OUTBOARD OF NACELLE. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A SEALED FLUSH PATCH REPAIR IAW BEECH SRM 57-90-00, PAGES 14-16.Oct 27, 1995 · N55522 · Beech 1900C · Wing, Plate/SkinSDR 95ZZZX6642Truss · crackedSPW - DURING VISUAL INSPECTION OF AREA 'A' REQUIRED BY AD 95-02-18, THE TRUSS WAS FOUND CRACKED AT THE LT OUTBOARD SIDE AT THE WELD FOR THE COWL MOUNT. THE LT TRUSS WAS REPAIRED IAW BEECH KIT NR 129-9006.Oct 24, 1995 · N60UE · Beech 1900C · Engine Mount SectionSDR 95ZZZX6641Truss · crackedSPW - DURING THE SCHEDULED VISUAL INSPECTION OF AREA 'A' OF THE LT ENGINE TRUSS AS REQUIRED BY AD 95-02-18, A SMALL CRACK WAS FOUND ON THE UPPER RT BRACKET THAT HOLDS THE COWL. THE CRACK WAS REPAIRED IAW BEECH KIT NR 129-9006.Oct 24, 1995 · N98GL · Beech 1900C · Engine Mount SectionSDR PLG102395J1Red Gear Box · failedDURING SHUTDOWN, THE LEFT PROPELLER STOPPED ROTATION IMMEDIATELY AFTER THE CONDITION LEVER WAS PLACED IN THE FUEL CUT OFF POSITION. TECHNICIANS ATTEMPTED TO ROTATE PROPELLER WITHOUT SUCCESS. FURTHER TROUBLESHOOTING REVEALED METAL PARTICLE CONTAMINATION IN THOct 23, 1995 · N15486 · Beech 1900C · Turbine Engine Reduction GearSDR PLG102195G2Py Line · crackedLGA - FLT 4727 - EN ROUTE, THE LEFT ENGINE SPOOLED TO 40 PERCENT N1. THE FLIGHT CREW SECURED THE ENGINE AND DIVERTED TO SWF LANDING WITHOUT INCIDENT. MAINTENANCE WAS NOTIFIED AND DISPATCHED TO THE AIRCRAFT. MAINTENANCE FOUND THE PY LINE BETWEEN THE FCU AND Oct 21, 1995 · N806BE · Beech 1900C · Fuel Controlling SystemSDR PLGA101995EPedal · brokenDURING TAXI IN FROM FLT NR 4453 - THE CAPTAINS RIGHT RUDDER PEDDLE ARM BROKE OFF. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT, AND FOUND ARM HAD FAILED AT PEDAL PIVOT POINT. THE ARM WAS REPLACED AND THE AIRCRAFT WAS RELEASED TO SERVICE. (M)Oct 19, 1995 · N810BE · Beech 1900C · Rudder Control SystemSDR HERA9524Fuel Line · leakingFLT NR 1451 - ANC - ON TAKEOFF, THE NR 1 ENGINE INDICATED 1000 LBS OF TORQUE AT 84 PERCENT NI. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE AND FOUND FUEL LINE, P/N 3040637, LEAKING DUE TO THE GENERATOR BLASOct 16, 1995 · N80598 · Beech 1900C · Engine Fuel DistributionSDR 95ZZZX6645Brake · wornIAD/EWR - AIRCRAFT ON TAKEOFF ROLL PULLED HARD TO LEFT. RETURNED TO GATE. UPON INSPECTION, FOUND NR 1 TIRE WORN. REPLACED TIRE, ALSO BRAKE WAS STICKING. AIRCRAFT BEING FERRIED TO GSO FOR INSTALLATION OF NR 1 BRAKE ASSY. REMOVED AND REPLACED NR 1 BRAKE ANDOct 15, 1995 · N34010 · Beech 1900C · Landing Gear Brake SystemSDR 96ZZZX1Sun Gear · fracturedAN IN-FLIGHT SHUT DOWN OF THE LT ENGINE DUE TO THE FAILURE OF THE POWER SECTION. AT THE TEAR DOWN, THE INVESTIGATION REVEALED THE NR 1 SUN GEAR AS BEING THE MODE OF FAILURE.Oct 13, 1995 · N118YV · Beech 1900C · Turbine Engine Reduction GearSDR 95ZZZX6643Truss · crackedESC - DURING SCHEDULED VISUAL INSPECTION OF AREA 'A' AS REQUIRED BY AD 95-02-18, THE ENGINE TRUSS WAS FOUND CRACKED AT THE INBOARD TOP STRUT AT THE OIL PLUG. THE CRACK WAS REPAIRED IAW BEECH REPAIR KIT 129-9006.Oct 12, 1995 · N55782 · Beech 1900C · Engine Mount SectionSDR PLGA10995E1Ei · trippedBOS/BDR - FLT 4343, BDR FROM BOS DID NOT GET 3 GREEN DOWN AND LOCKED LIGHTS WHEN GEAR WAS EXTENDED. CREW PERFORMED EMERGENCY PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. THE LANDING GEAR E.I. WAS RESET AND ALL 3 GREEN Oct 9, 1995 · N808BE · Beech 1900C · Landing Gear Position and WarningSDR PLGA108951Asymmetry Cam · wornBOS/LEB - FLT 4616 - EN ROUTE WHEN IT WAS NOTED THE FLAPS WOULD NOT RETRACT, AIRCRAFT DIVERTED INTO PSM. MAINTENANCE REMOVED AND REPLACED THE FLAP ASYMMETRY CAM AND FLAP SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED TO SERVICE. (X)Oct 8, 1995 · N818BE · Beech 1900C · Trailing Edge Flap Control SystemSDR 95ZZZX6646Service Valve · stickingGREENSBORO - FLT 2304 - UPON ARRIVAL INTO GREENSBORO 18:00 EASTERN TIME, GEAR WOULD NOT EXTEND, PILOTS MANUALLY EXTENDED GEAR. REMOVED AND REPLACED HYDRAULIC SERVICE VALVE.Oct 6, 1995 · N19016 · Beech 1900C · Hydraulic System, MainSDR 95ZZZX6123Le Skin · crackedSPW - DURING ROUTINE INSPECTION, A 4 INCH CRACK WAS FOUND ON THE LT WING 4 FEET INBOARD OF THE TIP AND 3 INCHES AFT OF THE TOP AFT EDGE OF THE WING BOOT. A FLUSH PATCH WAS INSTALLED IAW BEECH SRM 51-70-00, PAGES 26-27 AND LEAK CHECKED OK.Oct 4, 1995 · N87GL · Beech 1900C · Wing, Plate/SkinSDR 95ZZZM654Eva Tube · leakingLEFT BLEED AIR FAIL ILLUMINATED IN FLIGHT, RETURNED TO IAD. REPAIRED HOLE IN EVA TUBE DUE TO CHAFING.Oct 2, 1995 · N39019 · Beech 1900C · Compressor Bleed ControlSDR 95ZZZM652Relay · failedEN ROUTE, LANDING GEAR WOULD NOT EXTEND, AFTER SEVERAL TRIES GEAR CAME DOWN ON ITS OWN WITH HANDLE IN DOWN POSITION. AIRCRAFT FERRIED TO GSO. REMOVED AND REPLACED LANDING GEAR RELAY. (M)Oct 2, 1995 · N19016 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZM592Skin · crackedRIGHT OUTBOARD FLAP CRACKED .75 INCH ON TRAILING EDGE, 35 INCHES FROM OUTBOARD END OF FLAP. STOPPED DRILLED AND INSTALLED DOUBLER. (M)Oct 2, 1995 · N137YV · Beech 1900C · Trailing Edge FlapsSDR PLGA92895G1Skin · crackedDURING PILOT PREFLIGHT, A 3.5 INCH SPANWISE UPPER WING SKIN CRACK WAS NOTED ON THE LEFT WING. THE CRACK WAS CENTERED AT APPROXIMATELY LWS 151.0, 22.5 INCH AFT OF WING SPAR CENTER LINE. CRACK WAS REPAIRED IAW BEECH DWG FR-60-00001 AND BEECH SRM. AIRCRAFT RETSep 28, 1995 · N815BE · Beech 1900C · Wing, Plate/SkinSDR 95ZZZM653Gear Handle · malfunctionedLANDING GEAR WON'T EXTEND. AFTER A FEW MINUTES GEAR WENT DOWN. LANDING WAS ACOMPLISHED WITH NO FURTHER PROBLEMS. MAINTENANCE REPLACED HANDLE ASSEMBLY. (M)Sep 28, 1995 · N19016 · Beech 1900C · Landing Gear SelectorSDR 95ZZZX6286Downlock Switch · malfunctionedMCO/MIA - FLT 428 - PILOT REPORT: GEAR UNSAFE LIGHT ON IN-FLIGHT. MAINTENANCE REMOVED AND REPLACED NOSE GEAR DOWNLOCK AND RIGHT MAIN UPLOCK SWITCHES.Sep 27, 1995 · N196GA · Beech 1900C · Landing Gear Position and WarningSDR HERA9522Circuit Card · dirtyFLT NR 1426 - LANDING GEAR WOULD NOT COME DOWN WHEN SELECTED. THE GEAR WAS RECYCLED BUT HAD NO EFFECT. AFTER GOING AROUND AND RIGHT BEFORE STARTING THE MANUAL GEAR EXTENSION CHECKLIST THE LANDING GEAR CAME DOWN. THE GEAR WAS CHECKED VISUALLY AND THE LANDINGSep 25, 1995 · N55635 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR 95ZZZX6122Windshield · crackedMBL - AFTER DEPARTURE AND DURING CLIMB-OUT, THE NR 1 WINDSHIELD CRACKED. THE CREW ELECTED AN AIR TURN-BACK AND COMPLETED AN UNEVENTFUL LANDING. MAINTENANCE REPLACED THE WINDSHIELD.Sep 22, 1995 · N55782 · Beech 1900C · Flight Compartment WindowsSDR PLGA92095E1Selector · malfunctionedBOS-YSJ - FLT NR 4945 - DURING APPROACH, THE GEAR WOULD NOT EXTEND WHEN GEAR HANDLE WAS ACTIVATED. CREW PERFORMED EMERGENCY PROCEDURE FOR A GEAR EXTENSION. GEAR EXTENDED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED GEAR WAS DOWN AND LOCKED, ANSep 20, 1995 · N3069K · Beech 1900C · Landing Gear SelectorSDR 95ZZZX6119Precooler · leakingHON - DURING CLIMB-OUT AFTER DEPARTURE, THE CREW ELECTED AN AIR TURN-BACK DUE TO SMOKE IN THE CABIN. AFTER AN UNEVENTFUL LANDING, MAINTENANCE FOUND OIL IN THE RT PRECOOLER. THE INSTALLATION TESTED SATISFACTORILY.Sep 20, 1995 · N126UE · Beech 1900C · Cabin Cooling SystemSDR 95ZZZM591Skin · crackedDURING ROUTINE MAINTENANCE, A CRACK APPROXIMATELY 1 INCH WAS FOUND 34 INCHES FROM OUTBOARD END. REPAIRED WITH A DOUBLER. (M)Sep 20, 1995 · N134YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZM590Rib · crackedDURING ROUTINE MAINTENANCE, RIGHT INBOARD FLAP WAS FOUND TO HAVE CRACKED AT TRAILING EDGE APPROXIMATELY 1 INCH LONG, AND ONE WAS .5 INCH LONG ON SECOND RIB FROM OUTBOARD END. REPAIRED WITH DOUBLER. (M)Sep 20, 1995 · N134YV · Beech 1900C · Trailing Edge FlapsSDR 95ZZZX6121Truss · crackedSPW - DURING ROUTINE INSPECTION REQUIRED BY AD 95-02-18, MAINTENANCE FOUND THE LT TRUSS CRACKED ALONG THE TOP COWLING ATTACH BRACKETS BOTH INBOARD AND OUTBOARD. THE TRUSS WAS REPLACED.Sep 18, 1995 · N125GL · Beech 1900C · Engine Mount SectionSDR HERA9521Downlock Switch · out of adjustFLT NR 1125 - ON LANDING GEAR EXTENSION COULD NOT GET A SAFE NOSE GEAR INDICATION, (GREEN LIGHT). AIRCRAFT LANDED ANC WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE GEAR DOWNLOCK SWITCH AND AFTER NUMEROUS TESTS RETURNED THE AIRCRAFT TO SERVICE. (M)Sep 17, 1995 · N80346 · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZM665Skin · crackedDURING ROUTINE MAINTENANCE, A CRACK AT THE OUTBOARD BUMPER STOP AND ON BOTTOM OF FLAP, AFT OF SPAR APPROXIMATELY 12 INCHES FROM OUTBOARD END. REPAIRED WITH DOUBLERS.Sep 15, 1995 · N121ZR · Beech 1900C · Trailing Edge FlapsSDR 95ZZZX6118Truss · chafedSPW - DURING A ROUTINE INSPECTION, MAINTENANCE FOUND RT TRUSS INBOARD UPPER TUBE CHAFED. THE CHAFE WAS REPAIRED BY WELDING IAW REPAIR NR 2 OF BEECH KIT 129-9006-1.Sep 14, 1995 · N105GL · Beech 1900C · Engine Mount SectionSDR HERA9520Bracket · bentFLT NR 1122 - ON LANDING AT ANC, WHEN THE LANDING GEAR WAS EXTENDED, THE NOSE GEAR FAILED TO GET A SAFE INDICATION (GREEN LIGHT). THE LANDING GEAR HANDLE LIGHT REMAINED ILLUMINATED AND THE WARNING HORN REMAINED SOUNDING UNTIL THE NOSEWHEEL TOUCHED DOWN. THE Sep 13, 1995 · N80598 · Beech 1900C · Landing Gear Position and WarningSDR HERA9519Relay · errodedFLT NR 1481 - ON APPROACH TO LANDING AT ANC, THE LANDING GEAR HANDLE WAS SELECTED TO THE DOWN POSITION BUT DID NOT GET ANY LIGHTS INDICATING THE GEAR WAS DOWN AND LOCKED. THE EMERGENCY EXTENSION HAND PUMP WAS PUMPED BUT THERE WAS NO INDICATION OF PRESSURE, BUSep 12, 1995 · N55635 · Beech 1900C · Landing Gear Retraction/Extension SystemSDR PLGA91095JBearing · spalledBOS/BTV - FLT 4330 - DURING CRUISE FLIGHT, CREW EXPERIENCED SEVERAL LOUD BANGS FROM LT ENGINE AS ENG LOST POWER. ITT INCREASED TO 975 DEGREES CELSIUS PLUS & RISING AS OTHER PARAMETERS DECREASED. ENG SHUT DOWN & ACFT DIVERTED TO MHT WHERE UNEVENTFUL SINGLE ENSep 11, 1995 · N6929M · Beech 1900C · Turbine Engine Compressor SectionSDR 95ZZZM695Beta Linkage · out of adjustIMMEDIATELY AFTER LIFT OFF FROM ANC, NR 2 ENGINE AUTO FEATHERED. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BETA LINKAGE OUT OF ADJUSTMENT RIGGED BETA, TORQUE AND PROPELLER LINKAGES. ENGINE RUN AND AUTO FEATHER SYSTEM CHECK NORMSep 10, 1995 · N80532 · Beech 1900C · Propeller Controlling SystemSDR 95ZZZM514Truss · chafedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND THE RT ENGINE TRUSS CHAFED IN AREA 'B' AS DESCRIBED IN BEECH SB 2255R7 AND AD 95-02-18, THE DAMAGE WAS REPAIRED IAW REPAIR NR 2 OF BEECH KIT 129-9006-1. (M)Aug 31, 1995 · N123UE · Beech 1900C · Engine Mount SectionSDR 95ZZZM515Truss · crackedSPW - DURING THE ROUTINE VISUAL INSPECTION REQUIRED BY AD 95-02-18, THE RIGHT TRUSS WAS FOUND CRACKED IN AREA 'A'. THE TRUSS WAS CHANGED AND ENGINE FUNCTIONAL TEST WAS SATISFACTORY.Aug 30, 1995 · N174GL · Beech 1900C · Engine Mount SectionSDR 95ZZZM513Engine · failedORD-BRL - FLT NR 5927 - THE LEFT ENGINE FAILED AND WAS SECURED. THE CREW DIVERTED TO GBC ON SINGLE ENGINE AND COMPLETED AND UNEVENTFUL LANDING. MAINTENANCE CHANGED ENGINES. SUSPECT BEARING FAILURE. (M)Aug 30, 1995 · N122GL · Beech 1900C · Engine (Turbine/Turboprop)SDR PLGA827951GSwitch · intermittentLGA- FLT NR 4732 ON APPROACH THE RT MLG DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE WHEN THE GEAR WAS SELECTED DOWN. DURING ABNORMAL CHECKLIST PROCEDURES THE DOWN AND LOCKED LIGHT ILLUMINATED. THE AIRCRAFT LANDED IN LGA WITHOUT INCIDENT. THE AIRCRAFT WAS THENAug 27, 1995 · N817BE · Beech 1900C · Landing Gear Position and WarningSDR 95ZZZM512N1 Indicator · out of adjustDEN - THE CREW ELECTED AN AIR TURN BACK AFTER OBSERVING THE RT ENGINE AT 104 PERCENT AND 2700 LBS TORQUE WOULD NOT MAKE REQUIRED TORQUE. THE CREW ACCOMPLISHED AN UNEVENTFUL LANDING. MAINTENANCE CALIBRATED THE TORQUE SYSTEM, THE ITT SYSTEM, COMPRESSOR WASHED Aug 24, 1995 · N87GL · Beech 1900C · Engine RPM Indicating System
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