Beech 1900D

Service difficulty reports · 7,152

Newest first. General aviation reporting is voluntary.

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 97ZZZX1789Comp Contl Unit · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6Nov 1, 1996 · N87SK · Beech 1900D · Attitude and Direction Data SystemSDR 97ZZZX1788Comp Contl Unit · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6,Nov 1, 1996 · N801SK · Beech 1900D · Attitude and Direction Data SystemSDR 97ZZZX1787Comp Contl Unit · inoperativeDURING THE MONTH OF NOVEMBER, THERE WERE SEVEN CCU-65 COMPENSATION CONTROL UNITS, P/N 622-6135-014, REMOVED DUE TO PART OR ALL OF BACKLIGHTING BEING INOPERATIVE. THE PARTS TIME SINCE OVERHAUL WERE 6,805.5 HRS FROM N NR 118SK; 6,526.6 HRS FROM N NR 831SK; 6,Nov 1, 1996 · N831SK · Beech 1900D · Attitude and Direction Data SystemSDR 96ZZZX6169Line Assy · crackedFILL LINE TUBES ASSY CRACKED AT FLARE. LOSS OF FLUID IN HYDRAULIC SYSTEM SUFFICIENT TO ILLUMINATE LOW FLUID LIGHT. GEAR EXTENDED NORMALLY.Nov 1, 1996 · N225GL · Beech 1900D · Hydraulic System, MainSDR 96ZZZM1567Blade · crackedFOUND POWER TURBINE BLADE HALF MISSING.Oct 25, 1996 · N45AR · Beech 1900D · Turbine SectionSDR GLBA96211Yaw Sensor · malfunctionedRDU - TWO HARD UNCOMMANDED RUDDER TURNS WITH AUTOPILOT ENGAGED. TURNED OFF RUDDER BOOST. MAINTENANCE SECURED CANNON PLUG AT YAW RATE SENSOR. (M)Oct 23, 1996 · N169GL · Beech 1900D · Rudder Control SystemSDR S2YA960028Switch · out of adjustFLT 1265 - AFTER TAKEOFF, THE CREW NOTICED THE GEAR HANDLE UNSAFE LIGHTS REMAINED ILLUMINATED AND THE WARNING HORN SOUNDED CONTINUOUSLY WHEN LANDING GEAR HANDLE WAS RAISED TO THE RETRACT POSITION. MAINTENANCE ADJUSTED FLAP LIMIT SWITCH S4 AND ADJUSTED FLAP SYOct 21, 1996 · N891SK · Beech 1900D · Landing Gear Position and WarningSDR CA961029008O-Ring · broken(CAN) PILOT REPORTED THAT THE RIGHT BLEED AIR FAIL WARNING LIGHT CAME ON. INSPECTION FOUND THE OUTBOARD 'O' RING AT THE JUNCTION OF THE BLEED AIR DUCT AT WS 0.00 APPROXIMATELY WAS DRY AND BROKEN, AND CAUSED A BLEED AIR LEAK.Oct 21, 1996 · Beech 1900D · Pneumatic Distribution SystemSDR CA961112030O-Ring · missing(CAN) PILOT REPORTED THE RIGHT BLEED AIR FAIL ANNUNCIATOR LIGHT WAS ON. INVESTIGATION FOUND A HOLE IN THE EVA TUBE. THE HOLE WAS CAUSED BY A LEAK AT THE BLEED AIR JUNCTION AT STA. 29.06. TWO 'O' RINGS P/N 19357-222 WERE NOTED AS MISSING. IT IS LIKELY THAT THE Oct 18, 1996 · Beech 1900D · Compressor Bleed ControlSDR GLBA96204Eva System · leakingMSP - RIGHT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED. MAINTENANCE REPAIRED LEAK IN EVA SYSTEM. OPS CHECKED GOOD. (X)Oct 17, 1996 · N210UX · Beech 1900D · Compressor Bleed ControlSDR S2YA960027Flap Motor · overheatedDURING RUNUP BEFORE FIRST FLIGHT OF THE DAY, THE CREW NOTICED SMOKE IN THE CABIN, MAINTENANCE FOUND THE FLAP MOTOR WINDINGS HAD OVERHEATED INTERNALLY. IT WAS REPLACED BUT THE FLAP SYSTEM WAS DEFERRED DUE TO RIGGING REQUIRED. (M)Oct 16, 1996 · N891SK · Beech 1900D · Trailing Edge Flap ActuatorSDR C2XA96CL034Actuator · brokenCLE - FLT 9363 - THE CREW REPORTED THAT DURING A TRAINING FLIGHT, THE LEFT MAIN LANDING GEAR WOULD NOT INDICATE A DOWN AND LOCKED CONDITION. THE AIRCRAFT LANDED AT CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE LEFT MAIN LANDIG GEOct 16, 1996 · N16540 · Beech 1900D · Landing Gear ActuatorSDR 96ZZZX5987Air Distr · odorON FINAL APPROACH, PILOT REPORTED SMELLING A BURNING ODOR. MECHANIC INSPECTED, FOUND AIRCRAFT SAFE FOR FERRY FLIGHT TO DENVER. MECHANIC IN DENVER INSPECTED, REMOVED FLOOR PANELS AND PERFORMED GROUND RUNS WITH BLEED OFF AND ON. RAN FLAPS. COULD NOT DUPLICATOct 16, 1996 · N240YV · Beech 1900D · Air Distribution SystemSDR MESA201666Wire · shortedFLT 5960 EN ROUTE TO PITTSBURGH - NOTICED SPARKS COMING FROM POST AND AREA AROUND PRESSURIZATION DUMP SWITCH ON CENTER CONSOLE IN COCKPIT. MAINTENANCE INSPECTED AREA AND REPAIRED WIRE ON POST LIGHT ASSY, P/N A8970C1327. AIRCRAFT RETURNED TO SERVICE. (X)Oct 15, 1996 · N14YV · Beech 1900D · Light System WiringSDR GLBA96201Packing · failedISN - RIGHT BLEED AIR FAIL ILLUMINATED IN-FLIGHT. MAINTENANCE REPLACED PACKINGS IN RIGHT DUCT ASSY AND REPAIRED EVA TUBING. SYSTEM OPERATED NORMALLY. (X)Oct 13, 1996 · N211UX · Beech 1900D · Pneumatic Distribution SystemSDR GLBA96200Packing · missingHON - RIGHT BLEED AIR FAIL ILLUMINATED AND LEFT BLEED WILL NOT HOLD PRESSURE. MAINTENANCE FOUND PACKINGS MISSING IN BLEED DUCT ASSY ON LEFT SIDE. INSTALLED PACKINGS, REPAIRED EVA TUBING AND OPERATED NORMALLY. (X)Oct 11, 1996 · N208GL · Beech 1900D · Pneumatic Distribution SystemSDR CA961025011Fire Detector · broken(CAN) #1 ENGINE FIRE WARNING LIGHT FLICKERED IN FLIGHT, BUT NO OTHER INDICATIONS. PRECAUTIONARY ENGINE SHUTDOWN WAS CARRIED OTU. POST FLIGHT INSPECTION OF THE ENGINE FOUND THE FIRE LOOP BROKEN UNDER THE REAR OF THE ENGINE. A NEW FIRE LOOP WAS INSTALLED.Oct 11, 1996 · Beech 1900D · Fire DetectionSDR 96ZZZX5923O-Ring · crackedFLT 5636 - LT BLEED AIR FAIL LIGHT CAME ON IN-FLIGHT. MAINTENANCE FOUND FOUR SEALS BRITTLE AND CRACKED BETWEEN FUSELAGE AND ACM WHICH MELTED HOLE IN EVA TUBING. AIRCRAFT TOTAL TIME 254 HOURS.Oct 5, 1996 · N233YV · Beech 1900D · Pneumatic Distribution SystemSDR 96ZZZM1551Pin · backed outNOSE GEAR COLLAPSED ON TAXI. CLEAR VFR DAY. NOSE DRAG LEG UPPER PIN BACKED OUT. ISSUED FLEET CAMPAIGN DIRECTIVE TO INSPECT ENTIRE FLEET FOR UPPER DRAG LEG PIN INSTALLATION. (M)Oct 5, 1996 · N4ZV · Beech 1900D · Nose/Tail Landing GearSDR 96ZZZM1520Beta Cable · bindingJUST AFTER TAKEOFF FROM GALLUP, LEFT ENGINE LOST POWER. RETURNED TO GATE. MAINTENANCE FOUND LEFT BETA CABLE BOUND UP AND CAUSED BETA VALVE TO COME OUT OF RIG. REPLACED BETA CABLE AND RIGGED. (M)Oct 5, 1996 · N35YV · Beech 1900D · Propeller Controlling SystemSDR S2YA960030Pressure Switch · failedDURING THE MONTH OF OCTOBER THERE WERE TWO FUEL PRESSURE SWITCH (P/N 101-389018-21) FAILURES. AIRCRAFT N NR 901SK PRESSURE SWITCH S/N NR 2895 FAILED AT 1316.4 HOURS. AIRCRAFT N NR 148SK PRESSURE SWITCH S/N NR 2050 FAILED AT 3320.0 HOURS. THE PRESSURE SWITCHOct 1, 1996 · Beech 1900D · Fuel Indicating SystemSDR EY2R9601172Clamp · corrodedPROP ASSY COUNTERWEIGHT CLAMP FOUND CORRODED.Oct 1, 1996 · Beech 1900D · Propeller AssemblySDR EY2R9600156Blade · crackedBLADE CRACKED LEADING EDGEOct 1, 1996 · Beech 1900D · Propeller Blade SectionSDR C2XA96CL023Switch · dirtyCLE - FLT 3107 - CREW REPORTED GREEN LIGHT FOR THE NOSE LANDING GEAR CAME ON ABOUT ONE MINUTE AFTER GEAR EXTENSION, NO OTHER WARNING INDICATIONS. MAINTENANCE INSPECTED AIRCRAFT AND CLEANED NOSE GEAR MICROSWITCHES. OPERATIONAL CHECKS WERE GOOD IAW B100D MM 32Sep 30, 1996 · N49543 · Beech 1900D · Landing Gear Position and WarningSDR 96ZZZM1547Windshield · crackedCO-PILOT WINDSHIELD CRACKED IN SEVERAL PLACES. DURING FLIGHT, WEATHER PLUS 12 DEGREES CELSIUS AT 4,000 FEET.Sep 12, 1996 · N125YV · Beech 1900D · Flight Compartment WindowsSDR C2XA96CL031Blower · failedFLT 3013 - CREW REPORTED A STRONG SMELL OF SMOKE IN THE COCKPIT AND CABIN, GREY SMOKE WAS ALSO VISIBLY OBSERVED. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FORWARD VENT BLOWER IAW B1900D MM 21-10-01. OPERATIONAL CHECKS WERE GOOD, AIRCRAFT RESep 9, 1996 · N87551 · Beech 1900D · Air Distribution FanSDR C2XA96CL030Computer · faultedRIC - FLT 3053 - CREW REPORTED THE STALL WARNING SOUNDED AFTER ROTATION WITH THE LANDING GEAR DOWN AND FLAPS AT 17 DEGREES, WARNING CONTINUED TO SOUND AFTER LANDING GEAR AND FLAPS WERE RETRACTED. AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT ANDSep 8, 1996 · N81535 · Beech 1900D · Stall Warning SystemSDR 96ZZZM1397Truss · crackedDURING SCHEDULED DETAIL INSPECTION, FOUND SEVERAL OF THE EIGHT ISOLATOR PADS FAILED ON RIGHT ENGINE. SUBSEQUENT INVESTIGATION REVEALED TRUSS CRACKED AT LINSEED RIVET JUST AFT OF TOP INBOARD AREA A AND WELD JOINT CRACK AT TOP INBOARD AREA A (TYPICAL). REMOVEDSep 8, 1996 · N65YV · Beech 1900D · Engine Mount SectionSDR C2XA96CL027Actuator · failedCLE - FLT 3097 - CREW REPORTED THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. THE GREEN LIGHT DID ILLUMINATE AFTER THE LANDING GEAR WAS CYCLED SEVERAL TIMES. MAINTNANCE INSPECTED ACFT AND REMOVED AND REPLACED NOSE GEAR ACTUATOR IASep 4, 1996 · N49543 · Beech 1900D · Landing Gear ActuatorSDR 96ZZZX5198Limit Switch · out of adjustAZO - FLT 3018 - CREW REPORTED AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. ACFT RETURNED TO AZO, FLAPS RETRACTED TO ZERO AFTER LANDING. MAINTENANCE INSPECTED ACFT AND RELEASED IT IAW MEL 27-2 CONTROL NR 895224. AFTER ACFT RETURNED TO A MAINTENANCE BASE (CLE) THSep 3, 1996 · N87550 · Beech 1900D · Trailing Edge Flap Control SystemSDR 96ZZZX5046Nozzle · pluggedAT DISASSEMBLY, THE NR 3 BEARING WAS FOUND COMPLETELY DESTROYED. IT APPEARS TO BE OIL STARVATION DUE TO THE NR 3 AND NR 4 BEARING OIL NOZZLE BEING PLUGGED. WHEN THE NOZZLE WAS FLOW CHECKED, IT REVEALED 3 OF THE 4 OIL PORTS WERE PLUGGED. THE BLOCKAGE APPEARS Sep 2, 1996 · N35YV · Beech 1900D · Turbine SectionSDR S2YA960029Tach Indicator · inoperativeDURING THE MONTH OF SEPTEMBER THERE WERE THREE TURBINE TACH INDICATORS, P/N 114-380036-5, THAT HAD PART OF THEIR LIGHTED DIGITAL READOUT BURN OUT, THE ANALOG PORTION OF THE INDICATOR REMAINED OPERATIVE. THE PARTS' TOTAL TIMES WERE 6105 HOURS FROM A/C N NR 801Sep 1, 1996 · Beech 1900D · Engine RPM Indicating SystemSDR EY2R9601007Hub · corrodedHUB CORRODED.Sep 1, 1996 · Beech 1900D · Propeller Hub SectionSDR EY2R9600109Blade · crackedPROP BLADE LEADING EDGE CRACKEDSep 1, 1996 · Beech 1900D · Propeller Blade SectionSDR 96ZZZM1332Turbine · failedDURING APPROACH TO DIA, LEFT ENGINE SURGED AND LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. CREW NOTICED SMOKE COMING FROM LEFT EXHAUST STACKS. SECURED LEFT ENGINE AND LANDED WITHOUT INCIDENT. (M)Aug 29, 1996 · N35YV · Beech 1900D · Turbine SectionSDR 96ZZZM1331Gas Generator · failedDURING APPROACH TO DIA, LEFT ENGINE SURGED AND LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. CREW NOTICED SMOKE COMING FROM LEFT EXHAUST STACKS. SECURED LEFT ENGINE AND LANDED WITHOUT INCIDENT. (M)Aug 29, 1996 · N35YV · Beech 1900D · Turbine SectionSDR C2XA96IA223Deice Boot · debondedTYL - FLT 9447 - PILOT REPORTED DURING A POST-FLIGHT WALKAROUND INSPECTION, FOUND LT PROPELLER HAD ONE DEICE BOOT DEBONDED FROM BLADE. THE DEICE BOOT REMOVED AND ACFT FERRIED TO IAH WHERE MAINTENANCE INSTALLED A DEICE BOOT ON PROPELLER. ACFT WAS THEN APPROVEAug 28, 1996 · N82539 · Beech 1900D · Propeller Deice Boot SectionSDR C2XA96CL021Switch · dirtyCLE - FLT 3242 - CREW REPORTED AFTER LANDING GEAR EXTENSION, NOSE GEAR LIGHT DID NOT ILLUMINATE. THE CREW RECEIVED NO WARNING HORN WITH THE POWER REDUCED OR WITH FLAPS SET AT 35 DEGREES, THE LIGHT TESTED PROPERLY WITH THE PRESS-TO-TEST SWITCH. THE LIGHT DID Aug 27, 1996 · N49543 · Beech 1900D · Landing Gear Position and WarningSDR C2XA96CL020Pc Board · faultedCLE - FLT 3102 - CREW REPORTED LANDING GEAR HANDLE WOULD NOT GO INTO RETRACT POSITION WITHOUT USING DOWNLOCK RELEASE BUTTON. MAINTENANCE INSPECTED AND RELEASED ACFT IAW B1900D MEL NR 32-8, CONTROL NR 89516. ON 8-28-96, MAINTENANCE REMOVED AND REPLACED THE PRAug 26, 1996 · N49543 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR S2YA960024Tire · flat spottedAFTER THE FLIGHT CREW DEPARTED MKE ON FLT NR 1053, THE CREW NOTED SEVERE VIBRATION FROM THE NOSE, RETURNED TO MKE. MAINTENANCE CHANGED THE NOSE WHEEL ASSY, AND IT WAS DETERMINED THAT A TIRE FLAT SPOT OUT OF BALANCE CONDITION CAUSED THE VIBRATION. (M)Aug 23, 1996 · N831SK · Beech 1900D · TireSDR C2XA96CL019Indicator · faultedCLE - FLT 3278 - CREW REPORTED WHEN LANDING GEAR WAS EXTENDED, NOSE GEAR LIGHT DID NOT ILLUMINATE. THE CREW CYCLED THE LANDING GEAR TWICE AND THE NOSE GEAR LIGHT ILLUMINATED, ALL OTHER INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AAug 23, 1996 · N49543 · Beech 1900D · Landing Gear Position and WarningSDR CA960916017Wire · missing(CAN) THE PITCH TRIM CAUTION LIGHT WAS REPORTED NOT WORKING. INSPECTION FOUND A WIRE MISSING.Aug 14, 1996 · Beech 1900D · Flight Control System WiringSDR CA960909039Tank · leaking(CAN) FUEL LEAK FOUND ON THE TOP RIGHT FUEL TANK (WING) STA. 117.0 TO 159.0. THE FUEL WAS LEAKING FROM A LOOSE RIVET. REPAIR WAS CARRIED OUT AS PER RAYTHEON REPAIR DRAWING KIT 129-4017-1.Aug 12, 1996 · Beech 1900D · Fuel StorageSDR 96ZZZM1299Bearings · wornDURING ROUTINE MAINTENANCE, BOTH AILERONS WERE DISCOVERED AS HAVING EXCESSIVE FREE PLAY. UPON INSPECTION OF COMPONENTS, ALL THREE ATTACHMENT BEARINGS AND MOUNTING HARDWARE WAS FOUND WORN AND LOOSE. BEARINGS AND HARDWARE REPLACED WITH NEW. (M)Aug 7, 1996 · N845CA · Beech 1900D · AileronsSDR 96ZZZM1311Truss · failedDURING COMPLIANCE INSPECTION OF AD 95-02-18 AREA A, RIGHT ENGINE INBOARD UPPER TRUSS WAS FOUND SHEARED AT THE RIVET USED TO SEAL LINSEED OIL. TRUSS WAS REPLACED ENGINE INSPECTED. AIRCRAFT RELEASED FOR SERVICE. (M)Aug 4, 1996 · N31YV · Beech 1900D · Engine Mount SectionSDR S2YA960021Terminal · looseAFTER THE FLIGHT CREW DEPARTED MKE ON FLT NR 1157 FOR MSN, FOUND THAT THE CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT AND DECIDED TO RETURN TO MKE, MEL'D THE CARGO DOOR ANNUNCIATOR SYSTEM 52-2 CAT C. MAINTENANCE LATER FOUND A LOOSE TERMINAL SCREW ON A MICROSJul 30, 1996 · N145SK · Beech 1900D · Door Warning SystemSDR AU961064Flap · damaged(AUS) WING FLAP DAMAGED BY CONTACT WITH UNKNOWN OBJECT - IMPACT DAMAGE ON UNDERSIDE CAUSED BENDING FROM CENTRE WITH BUCKLING TO THE SPAR AND SKINS MAKING IT UNREPAIRABLE - NO DAMAGE TO MOUNTING POIUNTS OR WINGJul 30, 1996 · Beech 1900D · Trailing Edge FlapsSDR S2YA960020Fire Loop · shortedTHE CREW OF FLT NR 1077.3 GRB-MKE - LANDED IN MKE AND DURING TAXI TO THE GATE THEY NOTICED THE LEFT FIRE WARNING T-HANDLE ANNUNCIATOR LIGHTS FLICKERED AND THEN STAYED 'ON'. THE CREW STOPPED THE AIRCRAFT, PROCEEDED TO BLOW THE FIRE BOTTLE AND DEBOARDED THE AIRJul 29, 1996 · N85SK · Beech 1900D · Fire DetectionSDR 96ZZZX4777Vent Blower · failedCREW REPORTED A LIGHT HAZE IN CABIN AND FLT DK. RETURNED TO FIELD WITH NO FURTHER DIFFICULTIES. THE LIGHT HAZE DISSAPATED WHEN CREW DUMPED CABIN. UPON INITIAL INSPECTION, NO INDICATION OF SMOKE OR FLAMES OF ANY KIND WERE FOUND. ALL CIRCUIT BREAKERS WERE SEJul 26, 1996 · N165YV · Beech 1900D · Air Distribution FanSDR 96ZZZM1382Engine · failedON SHORT FINAL, THE RIGHT ENGINE LOST OIL PRESSURE AND THE ENGINE QUIT RUNNING. AIRCRAFT LANDED WITHOUT INCIDENT. (M)Jul 25, 1996 · N51YV · Beech 1900D · Engine (Turbine/Turboprop)
Back to Beech 1900D