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 AMWA15036Spar · corrodedCORROSION LT AND AFT MAIN SPAR FLANGE. REPAIRED IAW ENGINEERING REPORT NR 6772-3 REV A DATED JUN 25, 2007.Jul 9, 2007 · N155ZV · Beech 1900D · Wing SparSDR GUUA07090701Powerpack · defectiveFLIGHT: 9174, AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR POWER PACK MOTOR. LANDING GEAR OPERATIONAL CHECK NORMAL.Jul 9, 2007 · N231YV · Beech 1900D · Landing Gear Retraction/Extension SystemSDR NSVA20070178Switch · out of adjustWHILE IN CRUISE FLIGHT, RED "IN TRANSIT" INDICATOR ILLUMINATED IN LANDING GEAR HANDLE. GEAR EXTENDED SUCCESSFULLY. JACK ACFT, RETRACTED GEAR, LIGHT IN HANDLE ILLUMINATED DURING RETRACTION AND WENT OUT AT END OF UP CYCLE. EXTENDED GEAR LIGHT IN HANDLE OPERATJul 8, 2007 · N155CJ · Beech 1900D · Landing Gear Position and WarningSDR AMWA28032Spar · shearedSHEARED AND STRETCHED RIVETS AT LT AND RT WS 114.25. REPAIRED IAW ER NR 6699-2 REV 1R.Jul 5, 2007 · N126YV · Beech 1900D · Wing SparSDR GLBA20060961Torquemeter · malfunctionedABORTED TAKEOFF, FLIGHT 5063, UPON TAKEOFF PILOTS REPORTED THAT THE LT TORQUE INDICATOR STUCK AND WOULD NOT WORK CORRECTLY. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE LT TORQUE GAUGE IAW MM 33-10. OPERATIONAL CHECK OF THE SYSTEM GOOD.Jul 2, 2007 · N154GL · Beech 1900D · Engine BMEP/Torque IndicatingSDR GLBA20060960Skin · damagedHOLE IN FUSELAGE ON THE RT SIDE FORWARD OF FS 423.25 AND 2 INCHES ABOVE STRINGER 12R. APPROXIMATELY 1 INCH V SHAPE HOLE/CUT. MAINTENANCE REPAIRED AFFECTED AREA WITH A FLUSH REPAIR IAW MFG SRM 51-70. RII COMPLIED WITH IAW TASKCARD 8.2.1. HOLE CUTOUT SIZE 1.3 INJul 1, 2007 · N247GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA06270701Rod · bentFLIGHT: 5407, DURING APPROACH NOSE LANDING GEAR WOULD NOT COME DOWN ON THE FIRST TRY RECYCLED, LANDING GEAR EXTENDED NORMALLY. REPLACED NOSE LANDING GEAR ACTUATOR, OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.Jun 27, 2007 · N87551 · Beech 1900D · Landing Gear ActuatorSDR GUUA06270702Warning Horn · malfunctionedFLIGHT: 9259 DURING APPROACH LANDING GEAR WARNING HORN SOUNDS WHEN POWER IS PULLED BACK, WHILE SILENCING THE HORN SILENCE BUTTON NOT WORKING. PERFORMED LANDING GEAR OPERATIONAL CHECK NO DEFECTS NOTED.Jun 27, 2007 · N38537 · Beech 1900D · Landing Gear Position and WarningSDR CA070803016Compressor · seized(CAN) ON APPROACH, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A LOSS OF OIL PRESSURE AND AN INCREASE IN INTER-TURBINE TEMPERATURE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED COMPRESSOR SEIZURE AND INTERNAL OIL LEAKAGE. MFG WILL INJun 26, 2007 · Beech 1900D · Turbine Engine Compressor SectionSDR GUUA06260701Downlock Switch · damagedFLIGHT: 9244 FLL/GGT DURING APPROACH THE LANDING GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE IN THE DOWN POSITION. NOSE GEAR INDICATED UNSAFE CONDITION. RECYCLED LANDING GEAR OBTAINED GOOD INDICATIONS. REPLACED NOSE GEAR DOWNLOCK SWITCH Jun 26, 2007 · N87551 · Beech 1900D · Landing Gear Position and WarningSDR GUUA06250701Bracket · bentFLIGHT: 9224, DURING FINAL APPROACH NOSE GEAR DID NOT INDICATE DOWN AND LOCK UNTIL FIVE TO TEN SECONDS AFTER SELECTED DOWN POSITION. REPLACED NOSE LANDING GEAR DOWNLOCK BRACKET. OPERATIONAL CHECK NORMAL.Jun 25, 2007 · N87551 · Beech 1900D · Fuselage Main, Attach FittingsSDR NSVA20070164Connector · unsecureCABIN DOOR ANNUNCIATOR ILLUMINATED WITH DOOR CLOSED DURING TAKEOFF ROLL. ADJUSTED LATCH, REMOVED AND SECURED CONNECTOR ON DOOR HANDLE MICRO SWITCH, MEL NR 25979 CLEARED ON 6/30/2007.Jun 24, 2007 · N243CJ · Beech 1900D · Door System WiringSDR GUUA06240701Handle · failedFLIGHT: 9128, DURING APPROACH NOSE GEAR DID NOT IMMEDIATELY SAFE INDICATION AFTER APPROXIMATELY 5 SECONDS NOSE GEAR SHOWED DOWN AND LOCKED WITH AN ASSOCIATED POPPED CIRCUIT BREAKER. REPLACED LANDING GEAR CONTOL HANDLE. OPERATIONAL CHECK NORMAL.Jun 24, 2007 · N87551 · Beech 1900D · Landing Gear SelectorSDR AMWA85564BCBattery · weakDURING FLT, THE BATTERY CHARGE ANNUN ILLUMINATED. CONTINUED TO DESTINATION WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP UP IS A NUISANCE WRITEUP WITH SEVERE DISTRACTION TO THE AIR CREW.REMOVED AND REPLACED BATTERY AND ADJUSTED VOLTAGE REJun 24, 2007 · N142ZV · Beech 1900D · Battery/Charger SystemSDR NSVA20070161Connector · unsecureUPPER BULB IN MLG HANDLE INOP. RELAMPED WITH NO HELP. CHECKED AND SECURED CONNECTORS ON PCB AND LDG HANDLE WIRES AND PERFORMED OPS CHK IAW AMM 32-60-00 GOOD.Jun 22, 2007 · N155CJ · Beech 1900D · Landing Gear System WiringSDR GLBA20060958Connector · looseAIR RETURN, ENROUTE, PILOTS REPORTED THAT THE NR 1 ENGINE FIRELOOP ANNUCIATOR AND T-HANDLE FLICKERED. AIRCRAFT RETURNED TO DEPARTURE AND A SUBSEQUENT FERRY FLIGHT WAS PERFORMED FOR REPAIRS. MAINTENANCE INSPECTED THE AFFECTED SYSTEM AND DISCOVERED A SHORTED WJun 20, 2007 · N245GL · Beech 1900D · Fire Protection System WiringSDR AMWA531030Door Frame · crackedTHE PASSENGER ENTRY DOOR FRAME AT FS150 HAS 6 SMALL CRACKS TOTALING APPROX 1.5 INCHES IN LENGTH. THE CRACKS WERE LOCATED AT THE TOP DOOR STRUT ATTACH BRACKET MOUNTING HOLE (3 EA) AND THE BOTTOM DOOR STRUT ATTACH BRACKET MOUNTING HOLE. REPAIRED IAW ENGINEERINJun 20, 2007 · N138YV · Beech 1900D · Fuselage Main, StructureSDR AMWA31034CSkin · damagedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE, DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW AIRCRAFT ENGINEERING INC REPORT NR 6732Jun 20, 2007 · N138YV · Beech 1900D · Nacelle/Pylon, Plate/SkinSDR AMWA31034BStructure · damagedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE, DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW AIRCRAFT ENGINEERING REPORT NR 6732-1 Jun 20, 2007 · N138YV · Beech 1900D · Nacelle/Pylon, Main FrameSDR AMWA31034AFrame · chafedFUSELAGE FRAMES DAMAGED BY CHAFFING. REPAIRED IAW ENGINEERING REPORT NR 6732-2 REV 1R.Jun 20, 2007 · N138YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20060957Blade · damagedEXTENDED ROLLOUT, UPON LANDING, PILOTS REPORTED THAT DUE TO LANDING ROLLOUT BEYOND THE END OF THE RUNWAY, THE RT PROP NR 2 ENGINE STRUCK A RECTANGULAR BOX. PRELIMINARY DAMAGE INDICATES PROP BLADE DAMAGE AND HOLE IN FUSELAGE. [08-01-07] MX INSTALLED TEMP REJun 20, 2007 · N253GL · Beech 1900D · Fuselage Main, Plate/SkinSDR NSVA20070156Transducer · malfunctionedRETURN TO GATE, LEFT ENGINE OIL PRESSURE DROPPED TO 60 PSI AND REMAINED AT 60 DURING TAXI OUT. OIL PRESSURE NEEDLE BEGAN BOUNCING BETWEEN 60 PSI AND 110 PSI. REMOVED AND REPLACED OIL PRESSURE TRANSDUCER IAW BMM 1900D 79-50-00-207 RAN LT ENG FOR LEAK AND OPS Jun 18, 2007 · N171CJ · Beech 1900D · Engine Oil PressureSDR GLBA20060955Angle · crackedUPON ROUTINE INSPECTION, MAINTENANCE DISCOVERED CRACK AT LT FS 288 WL.70.0. LENGTH OF CRACK 1.75 NR. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. MAINTENANCE REPAIRED AFFECTED AREA AT FS 288 WS 70.0 IAW SRM 53-90-23-001. IWO NR 94109. RII COMPLIED IJun 18, 2007 · N170GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA20060956Angle · crackedUPON ROUTINE INSPECTION MAINTENANCE DISCOVERED CRACK AT RT FS 288 WL 70.0. LENGTH OF CRACK 1.75 INCHES. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. MAINTENANCE REPAIRED AFFECTED AREA AT FS 288 WS 70.0 IAW SRM 53-90-23-001. IWO NR 94109. RII COMPLIJun 18, 2007 · N170GL · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA0956Angle · crackedUPON ROUTINE INSPECTION MAINTENANCE DISCOVERED CRACK AT RT FS 288 WL 70.0. LENGTH OF CRACK 1.75 INCHES. UPON COMPLETION OF REPAIRE RII INSPECTION IS REQUIRED. [OPEN]Jun 18, 2007 · N170GL · Beech 1900D · Fuselage Miscellaneous StructureSDR AMWA85394BCConnector · corrodedBATT CHARGE ANNUN ILLUMINATES 3-5 MIN, EXTINGUISHES BRIEFLY, RE-ILLUMINATES FOR 2+ MIN, THEN REMAINED EXTINGUISHED FOR REMAINDER OF FLT. CONTINUED TO DESTINATION W/O FURTHER INCIDENT. CLEANED CORROSION OFF OF CONNECTORJun 17, 2007 · N10675 · Beech 1900D · Battery/Charger SystemSDR NSVA20070159Circuit Board · malfunctionedGEAR HANDLE UNSAFE LIGHT REMAINED ILLUMINATED AFTER RETRACTION. REMOVED AND REPLACED PCB LOGIC RELAY BOARD IAW 32-30-00. PN OFF/ON 112-364021-1, SN OFF 11, SN ON 775-8-85. OPS CHECK GOOD. ALSO, REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW 32-10-00 PJun 15, 2007 · N155CJ · Beech 1900D · Landing Gear SelectorSDR GUUA06150701Wire · looseFLIGHT: 9278, DURING FLIGHT, RT DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. CONTINUED TO DESTINATION, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE AT THE RT FIRE BOTTLE.Jun 15, 2007 · N231YV · Beech 1900D · Fire Protection System WiringSDR AMWA14030Skin · wornRIVET IN LT IB FLAP DOVETAIL PULLED THROUGH THE SKIN. REPAIRED IAW BSRM 51-70-00 TYPICAL SKIN REPAIRS RIVET SPACING AND PANEL SIZE WERE AS ORIGINALJun 15, 2007 · N161YV · Beech 1900D · Trailing Edge FlapsSDR GLBA20060954Acm · contaminatedAIR RETURN - FLIGHT 5134 - ENROUTE FROM LBF TO DEN PILOTS REPORTED SMOKE/MIST IN THE CABIN AFTER DEPARTURE. MAINTENANCE TROUBLESHOT THE ISSUE AND FOUND NO SMOKE, HOWEVER, MIST WAS WAS REPORTED AND MAINTENANCE FOUND AN EXCESSIVE AMOUNT OF MOISTURE IN THE AIR CYJun 13, 2007 · N170GL · Beech 1900D · Cabin Cooling SystemSDR NSVA20070158Relay · intermittentGEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. REMOVED AND REPLACED PCB A406 DUE TO RELAY K3 INTERMITTENT IAW WD7 91-34-01. OPS CHECK GOOD IAW AMM 32-60-00, PN OFF 112-364021-1, SN ON 11, SN OFF 582892.Jun 12, 2007 · N155CJ · Beech 1900D · Landing Gear Position and WarningSDR AMWA7026DRib · corrodedBIO CORROSION LT WING RIB AT WS 124.588, NEAR WHERE RIB ATTACHES TO MAIN SPAR. REPAIRED IAW REPORT 6702-6 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Wing, Rib/BulkheadSDR AMWA7026CSkin · chafedFRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE RT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Nacelle/Pylon, Plate/SkinSDR AMWA7026BSkin · chafedFRICTION CHAFING DURING OPERATION HAS CAUSED WORN SEGMENTS ON THE LT NACELLE (TURTLEBACK) SKINS. REPAIRED IAW REPORT 6702-5 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Nacelle/Pylon, Plate/SkinSDR AMWA7026ARib · corrodedBIO CORROSION RT WING RIB AT WS125.00; AREA NEAR THE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW A REPORT 6702-4 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Wing, Rib/BulkheadSDR AMWA7020ESkin · crackedFUSELAGE SKIN CRACKED, LENGTH APPROX 1.5 INCHES. REPAIRED IAW REPORT #6702-3 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, Plate/SkinSDR AMWA7020DSkin · crackedRT WING SKIN CRACKED BETWEEN FS303.25 AND FS310.75 AT WS25. LENGTH OF CRACK APPROX 5.5 INCHES. REPAIRED IAW REPORT 6702-2 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Wing, Plate/SkinSDR AMWA7020BFrame · chafedFUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, FrameSDR AMWA7020AFrame · chafedFUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW REPORT 6702-1 REV 1R.Jun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, FrameSDR AMWA7020CFrame · chafedFUSELAGE FRAMES DAMAGED BY FRICTION CHAFFING. REPAIRED IAW ACFT REPORT NR 6702-1 REV 1RJun 12, 2007 · N126YV · Beech 1900D · Fuselage Main, FrameSDR GUUA06120702Skin · corrodedAT SCHEDULED INSPECTION DISCOVERED SKIN CORROSION AT FS 438.250, STRINGER WL 13R. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW MFG STRUCTURAL REPAIR MANUAL 51-70-06.Jun 12, 2007 · N87550 · Beech 1900D · Fuselage Main, Plate/SkinSDR NSVA20070154Wire · chafedGEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION, INSPECTED LANDING GEAR FOR ANY OBVIOUS DAMAGE FOUND NO DAMAGE. FOUND RT DOWN SWITCH WITH CHAFED WIRES. REMOVED AND REPLACED SWITCH IAW AMM 32-60-02. OPS CHECK GOOD, P/N ON/OFF H11-1541.Jun 10, 2007 · N155CJ · Beech 1900D · Landing Gear System WiringSDR GUUA06090703Bushing · frozenAT SCHEDULED FLEET CAMPAIGN INSPECTION, LT FWD EMERGENCY EXIT WILL NOT OPEN FROM INSIDE. REPLACED BUSHING.Jun 9, 2007 · N45AR · Beech 1900D · Emergency ExitsSDR GUUA06090702Wire · looseFLIGHT: 9170 FLL/TCB, AFTER TAKEOFF THE NR (1) FIRE DISCHARGE ANNUNCIATOR FLICKERED ON AND OFF. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. SECURED LOOSE WIRE ON THE NR (1) FIRE BOTTLE.Jun 9, 2007 · N81536 · Beech 1900D · Fire Protection System WiringSDR BSAASDR0721Wire · chafedWHEN CREW SELECTED GEAR DOWN, THE LANDING GEAR CONTROL CB IMMEDIATELY TRIPPED. CREW EXTENDED GEAR AND LANDED WITH NO FURTHER INCIDENT. A CHAFED WIRE FOR THE GEAR DOWN MICROSWITCH WAS FOUND UNDER THE CABIN FLOOR BENEATH SEAT 4A. THE WIRE WAS GROUNDING ON A DEJun 7, 2007 · N139ZV · Beech 1900D · Landing Gear System WiringSDR BSAASDR0718Actuator · malfunctionedTHE LANDING GEAR CIRCUIT BREAKER TRIPPED WHEN CREW SELECTED GEAR DOWN DURING APPROACH. GEAR WAS EXTENDED MANUALLY AND CREW LANDED WITHOUT INCIDENT. AFTER EXTENSIVE TROUBLESHOOTING, THE RIGHT MAIN LANDING GEAR ACTUATOR WAS CHANGED DUE TO A SUSPECTED FAULT IN Jun 7, 2007 · N139ZV · Beech 1900D · Landing Gear ActuatorSDR AMWA85129BCCharger · looseAFTER TAXI FROM GATE THE BATTERY CHARGE ANNUN ILLUM. AC RETURNED TO GATE WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN ILLUM WRITEUP IS CONSIDERED A NUISANCE AND EXTREME DISTRACTION TO THE PILOT. RESEATED A-130 PCB, OPS CHECKED GOOD.Jun 5, 2007 · N127ZV · Beech 1900D · Battery/Charger SystemSDR 85129BCCharger · looseAFTER TAXI FROM GATE THE BATTERY CHARGE ANNUN ILLUM. AC RETURNED TO GATE WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUN ILLUM WRITEUP IS CONSIDERED A NUISANCE AND EXTREME DISTRACTION TO THE PILOT. RESEATED A-130 PCB, OPS CHECKED GOOD.Jun 5, 2007 · N127ZV · Beech 1900D · Battery/Charger SystemSDR CA070607009Blade · cracked(CAN) DURING ROUTINE MAINTENANCE, THE LT PROPELLER BLADE NR 1 WAS FOUND CRACKED. THE CRACK RAN CHORD WISE APPROXIMATELY 2.3750 INCH FROM THE BLADE ROOT WITH A LENGTH OF APPROXIMATELY 1 INCH. THE PROPELLER HAS BEEN REPLACED AND WILL BE SENT FOR REPAIR AS WELL AJun 4, 2007 · Beech 1900D · Propeller Blade SectionSDR GUUA06020701Uplock Switch · shortedFLIGHT: 9282, DURING APPROACH WHEN LANDING GEAR SELECTED DOWN NO (3) GREEN INDICATION CIRCUIT BREAKER POPPED RESET BREAKER AND ALL INDICATIONS OPERATED NORMALLY. REPLACED RIGHT MAIN LANDING GEAR UPLOCK SWITCH. LANDING GEAR OPERATIONAL CHECK NORMAL. TEST FLIGHJun 2, 2007 · N16540 · Beech 1900D · Landing Gear Position and Warning
Back to Beech 1900D