Raytheon 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR MASA98080Skin · crackedDURING ROUTINE MAINTENANCE, DISCOVERED SKIN CRACK APPROXIMATELY 2 INCHES LONG ON LOWER RIGHT FUSELAGE IN SPAR AREA. REPAIR WAS COMPLETED BY STOP DRILLING CRACK AND INSTALLING REINFORCEMENT DOUBLER TO AFFECTED AREA IAW BEECH STRUCTURAL REPAIR MANUAL CHAPTER 53SDR MASA98079Skin · crackedDURING ROUTINE MAINTENANCE, DISCOVERED A SKIN CRACK APPROXIMTELY 1.5 INCHES LONG AT FORWARD OUTBOARD LEFT SIDE OF NR 2 VHF ANTENNA. COMPLETED REPAIR BY STOP DRILLING CRACK AND INSTALLING A REINFORCEMENT DOUBLER TO SKIN CRACK IAW BEECHCRAFT STRUCTUAL REPAIR MASDR CA980513012Bracket · broken(CAN) THE TAXI LIGHT HOUSING IS RETAINED TO A BRACKET P/N 114-364137-3 BY A RIVET. THE RIVET HAD SHEARED AND THE LIGHT ASSEMBLY WAS HANGING BY THE ELECTRICAL WIRES. SUBMITTER STATED THIS SITUATION COULD AFFECT THE OPERATION OF THE NOSE GEAR.SDR CA980513011Tube · chafed(CAN) NOSE LANDING STEERING TUBE CHAFED NEXT TO RIVETS. THE DAMAGE WAS AT THE FRONT AND REAR OF RIVETS THAT HOLD THE ROD END. CHAFED AREA WAS TO A DEPTH OF 0.015 THOUSANDS OF AN INCH.SDR CA980506008Wire · misrouted(CAN) IN REFERENCE TO ELECTRICAL LOAD DISTRIBUTION, DC POWER LEFT WIRING DIAGRAM MANUAL ATA 24-61-02, WIRE NR A2-4-P170-J WAS CONNECTED TO TERMINAL NR 5 INSTEAD OF TERMINAL NR 1. IN THIS SITUATION THE LEFT GENERATOR WAS HARD TO COME ON LINE AFTER ENGINE STARTSDR CA980506007Wire · misinstalled(CAN) IN REFERENCE TO ELECTRICAL LOAD DISTRIBUTION, DC POWER LEFT WIRING DIAGRAM MANUAL ATA 24-61-02, WIRE NR A2-4-P170-J WAS CONNECTED TO TERMINAL NR 5 INSTEAD OF TERMINAL NR 1. IN THIS SITUATION, THE LEFT GENERATOR WAS HARD TO COME ON LINE AFTER THE ENGINE SDR CA980506006Wire · misrouted(CAN) IN REFERENCE TO ELECTRICAL LOAD DISTRIBUTION, DC POWER RIGHT WIRING DIAGRAM MANUAL ATA 24-61-02, WIRE NR A2-4P170-J WAS CONNECTED TO TERMINAL NR 5 INSTEAD OF TERMINAL NR 4. IN THIS SITUATION, THE RIGHT GENERATOR WAS HARD TO COME ON LINE AFTER AN ENGINE SDR CA980506005Wire · misrouted(CAN) IN REFERENCE TO ELECTRICAL LOAD DISTRIBUTION, DC POWER RIGHT WIRING DIAGRAM MANUAL ATA 24-61-02, WIRE NR A2-4-P170-J WAS CONNECTED TO TERMINAL NR 5 INSTEAD OF TERMINAL NR 4. IN THIS SITUATION, THE RIGHT GENERATOR WAS HARD TO COME ON LINE AFTER ENGINE STSDR 98ZZZM897Skin · crackedICT OVERNIGHT MAINTENANCE FOUND A .5 INCH CRACK IN LEFT INBOARD FLAP BOTTOM SKIN 36 INCHES FROM INBOARD END AND 2 INCH AFT OF LE. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)SDR MASA98074Hyd Power Pack · cavitatedFLT 5069 - FMN-GUP - AFTER DEPARTURE GEAR WOULD NOT FULLY RETRACT. PILOT SELECTED GEAR DOWN AND THE NOSE GEAR WOULD NOT FULLY EXTEND. PILOT ATTEMPTED TO PUMP GEAR DOWN AND DID RECEIVE DOWN AND LOCKED INDICATION. CREW DECLARED AN EMERGENCY AND PERFORMED A FLSDR CA980416018Switch · failed(CAN) AFTER TAKEOFF, WHEN FLAPS SELECTED FROM 17 DEGREES TO ZERO DEGREES, THE FLAPS DID NOT RETRACT. AIRCRAFT RETURNED TO BASE AND LANDED SAFELY. MAINTENANCE CHECK FOUND FLAP ASYMMETRY SWITCH WAS DEFECTIVE.SDR CA980415017Igniter · failed(CAN) DURING START, THE RIGHT HAND CIRCUIT BREAKER FOR THE IGNITION EXCITER TRIPPED REPEATEDLY. THE EXCITER WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR CA980415016Igniter · failed(CAN) DURING NORMAL START, THE NR 1 ENGINE FAILED TO IGNITE. MAINTENANCE REPLACED THE LEFT HAND IGNITION EXCITER AND THE AIRCRAFT WAS REPLEASED FOR SERVICE.SDR CA980415015Igniter · failed(CAN) DURING START ATTEMPT, THE NR 2 ENGINE FAILED TO IGNITE. MAINTENANCE FOUND THE RIGHT HAND IGNITION EXCITER PLUG WAS FAULTY. THE EXCITER WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR 98ZZZM898Skin · crackedOVERNIGHT MAINTENANCE IN ICT, FOUND A SMALL CRACK ON THE RT OUTBOARD FLAP LOWER SKIN TE 10 INCH FROM INBOARD END. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)SDR C2XA98CL035Bracket · brokenCLE - FLT 3041 - CREW REPORTED THAT DURING TAXI THE LEFT ENGINE FIRE DETECTOR ACTIVATED, CREW PERFORMED QRH ITEMS. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ENGINE AND FOUND THE FORWARD FIRE LOOP ATTACHMENT BRACKET BROKEN ALLOSDR MASA98069Cable Drum · out of adjustFLT 5983 - PIT-MBS - CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE DOOR WAS INSPECTED AND THE AIRCRAFT WAS FERRIED TO DUJ. DUJ MAINTENANCE RIGGED THE DOOR CABLE DRUM, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR CA980416019Actuator · inoperative(CAN) PILOT REPORTED LOSING NOSE WHEEL STEERING. MAINTENANCE CHECK REVEALED THE PLUG ON THE ACTUATOR WAS NOT SECURE PREVENTING THE ACTUATOR FROM EITHER ENGAGING OR DISENGAGING. IN THIS STATE THE ACTUATOR WAS NOT CONNECTED TO THE NOSE WHEEL STEERING UNIT. NESDR C2XA98CL034Torque Gauge · intermittentCLE - FLT 3263 - CREW REPORTED THE RIGHT HAND ENGINE TORQUE GAUGE FLUCTUATES FROM 5,000 TO ZERO IN FLIGHT. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE TORQUE GAUGE IAW B1900D MM 77-10-00, OPERATSDR 98ZZZM899Skin · crackedOVERNIGHT MAINTENANCE IN ICT, FOUND TWO .5 INCH CRACKS IN BOTTOM SKIN EXTENDING FROM TWO ADJACENT RIVETS ON THE CENTER SPAR ON THE LEFT OUTBOARD FLAP. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)SDR 98ZZZM892Skin · crackedOVERNIGHT MAINTENANCE ICT, FOUND .5 INCH CRACK IN THE RT OUTBOARD FLAP TE 7 INCH FROM INBOARD END. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)SDR CA980416015Brake · seized(CAN) DURING AN INSPECTION, IT WAS FOUND THAT NR 3 WHEEL WAS DIFFICULT TO ROTATE. FURTHER CHECKING INDICATED THE BRAKE ASSY WAS THE CAUSE AND WAS REPLACED. PART TC: 2,595.SDR 98ZZZM894Skin · crackedOVERNIGHT MAINTENANCE IN ICT, FOUND A .5 INCH CRACK EXTENDING FROM A RIVET ON THE RT INBOARD FLAP DOVETAIL. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)SDR MASA98077Truss Bolts · looseFLT 5330 - JAX-PBI - IN FLIGHT, CREW NOTICED THE RIGHT COWLING WAS LOOSE. CREW REDUCED POWER TO THE RT ENGINE AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE FOUND THE UPPER INBOARD TRUSS BOLT WAS LOOSE. REMOVED AND REPLACED THE ENGINE TRUSS AND BOLTSDR 98ZZZX1906Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.SDR 98ZZZX1901Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS.SDR S2YA98010Engine · malfunctionedAFTER TAKEOFF OF FLT 1235 - MKE TO MQT, THE FLT CREW NOTICED THAT THERE WERE SPARKS COMING OUT OF THE RT ENGINE EXHAUST STACK. THE FLIGHT CREW DECIDED TO RETURN TO MKE SO MAINTENANCE COULD INSPECT THE ENGINE. AFTER AN UNEVENTFUL LANDING MAINTENANCE INSPECTEDSDR CA980406048Control Cable · twisted(CAN) DURING ROUTINE MAINTENANCE, THE ELEVATOR CONTROL TRIM CABLES WERE FOUND TWISTED AROUND EACH OTHER. THE CABLES WERE DISCONNECTED AT MID-FUSELAGE AND UNTWISTED. CABLES RE-TENSIONED AND CHECKED SERVICEABLE.SDR 98ZZZM893Skin · crackedDURING ACCEPTANCE INSPECTION ICT MAINTENANCE, FOUND THE OUTBOARD ATTACH POINT INBOARD ACCESS HOLE ON THE RT INBOARD FLAP HAD SMALL CRACK FROM IT. REPAIRED CRACK IAW AMWA TO 1900-27-00-0001. (M)SDR 98ZZZM900Skin · crackedOVERNIGHT MAINTENANCE, FOUND .5 INCH CRACK IN LHOB FLAP 29.5 INCH FROM OUTBOARD EDGE AND 15 INCH FROM TRAILING EDGE ON BOTTOM SKIN. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)SDR 98ZZZM896Skin · crackedOVERNIGHT MAINTENANCE IN ICT FOUND A 1 INCH CRACK IN TOP SKIN .5 INCH FROM INBOARD AND 9.5 INCH FROM TE ON RHOB FLAP. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M)SDR 98ZZZM455Rib · crackedDURING REMOVAL OF LEFT HORIZONTAL STABILIZER DE-ICE BOOT, RIVET HEADS FROM LEADING EDGE RIBS WERE STUCK TO OLD DE-ICE BOOT. UPON FURTHER INVESTIGATION AND INSPECTION OF COMPLETE HORIZONTAL STABILIZER, A TOTAL OF 6 LEADING EDGE RIBS AND 4 CENTER RIBS WERE FOUNSDR CA980325040Governor · faulty(CAN) AFTER CLIMB, WHILE CRUISE SETTINGS WERE BEING ESTABLISHED THE RIGHT HAND PROPELLER SPEED DROPPED TO 1550 RPM AND HELD THERE. FURTHER CORRECTION INITIATED WERE UNABLE TO MOVE THIS SETTING. AFTER AN UNEVENTFUL LANDING, MAINTENANCE DISPATCHED TO THE AIRCRASDR CA980416017Valve · stuck(CAN) IN REPLACING A FIREWALL FUEL SHUT-OFF VALVE, IT WAS FOUND THAT THE VALVE LEVER COULD CONTACT THE FUEL FILTER SUPPORT BRACKET WHEN IN THE CLOSED POSITION. IN THIS STATE, THE VALVE LEVER COULD NOT RETURN TO THE OPEN POSITION. PART TC: 4,140.SDR CA980416014Bracket · broken(CAN) TAXI LIGHT HOUSING BRACKET FOUND BROKEN. THIS CONDITION COULD INTERFERE WITH THE NOSE LANDING GEAR EXTENSION OR RETRACTION.SDR S2YA98009Brush Block · wornMKE/MQT - FLT 1233 - WHILE IN CRUISE FLIGHT, CREW NOTICED THE RT PROP HEAT INDICATING ONLY 8 AMPS IN AUTO OR MANUAL MODES. THE WEATHER IN THE MQT AREA INDICATED ICING CONDITIONS, SO THE CREW ELECTED TO RETURN TO MKE AFTER CONSULATION WITH MAINTENANCE. AFTER SDR CA980416013Compressor · damaged(CAN) THE AIR CONDITIONER COMPRESSOR, ON THE NR 2 ENGINE, WAS DAMAGED ON THE FRONT OF ITS LEFT SIDE BY RUBBING OF THE PROPELLER CONTROL AND THE CONDITION CONTROL CABLES. THESE TWO CABLES ARE COVERED BY A METAL SHEATH.SDR CA980330002Switch · failed(CAN) DURING APPROACH, NO DOWNLOCK INDICATION FOR NOSE LANDING GEAR. AFTER OVER FLYING THE TOWER, LIGHT INDICATION CAME ON. MAINTENANCE INSPECTED THE NOSE GEAR SWITCHES AND LANDING GEAR RETRACTION TESTS CARRIED OUT. UNABLE TO DUPLICATE FAULT. SUSPECT INTERNSDR C2XA98CL028Turbine · damagedCLE - DURING A SCHEDULED INSPECTION, THE RIGHT ENGINE WAS FOUND TO HAVE A BLADE TIP MISSING ON THE 2ND STAGE POWER TURBINE. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 4272003. OPERATIONAL AND LEAK CHECKS WERE SATISSDR CA980416016Brake · seized(CAN) IN REPLACING NR 4 TIRE, FOUND THE BRAKE ASSEMBLY OF THAT WHEEL WAS SEIZED. PART TC: 2,044.SDR S2YA98008Warning Light · illuminatedFLT 1163 - DAY-SBN - IMMEDIATELY AFTER TAKEOFF, THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE FLT CREW DECIDED TO RETURN TO DAY TO PLACE THE ANNUNCIATOR ON MEL. AFTER AN UNEVENTFUL LANDING, THE CABIN DOOR ANNUNCIATOR WAS PLACED ON MEL. MAINTENANCE INSPECTED TSDR CA980318031Bearing · loose(CAN) DURING ROUTINE MAINTENANCE, THE AIR COMPRESSOR QUILL SHAFT BEARING INNER GREASE SEAL WAS FOUND TO BE LOOSE. THE BEARING ROTATES AT HIGH SPEEDS AND IS CRITICAL TO THE OPERATION. THE DEFECTIVE BEARING WAS REPLACED.SDR S2YA98007Pressure Switch · failedFLT 1162 - MKE-SBN - DURING CLIMB-OUT, THE LT AUTO-FEATHER ANNUNCIATOR EXTINGUISHED. THE CREW DECIDED TO DECLARE AN EMERGENCY AND RETURN TO MKE. AFTER MAKING AN UNEVENTFUL LANDING MAINTENANCE INSPECTED THE A/C AND DETERMINED THAT THE RT HIGH PRESSURE AUTO-FESDR CA980416012Brake · seized(CAN) IN REPLACING NR 3 TIRE DUE TO TIRE BURST, THE BRAKE ASSEMBLY WAS FOUND SEIZED. NEW BRAKE ASSY AND TIRE INSTALLED. PART TC: 3,446.SDR CA980330009Door · not locked(CAN) ON TAKEOFF, CREW FELT AND HEARD BUFFETING IN THE AIRFRAME. NO LIGHT INDICATIONS SUGGESTING A PROBLEM. ON RETURN TO DEPARTURE BASE AND LEAVING AIRCRAFT, IT WAS NOITICED THE AFT CARGO DOOR WAS OPEN. MAINTENANCE ALSO NOTICED THE CARGO DOOR ANNUNCIATOR LISDR MASA98046Switch · out of adjustFLT 5989 - MBS-PIT - EN ROUTE FROM SAGINAW TO PIT, PILOT REPORTED THE PAX DOOR ANNUNC ILLUMINATED. CREW DECLARED AN EMERGENCY AND DIVERTED TO DTW. THE DOOR WAS INSPECTED TO INSURE THAT IT WAS PROPERLY CLOSED AND LOCKED. MAINTENANCE ACTION WAS DEFERRED ON THSDR 98ZZZM385Air Distribution · odorCLE - FLT 3165 - CREW REPORTED A VERY STRONG BURNING SMELL/SULPHUR SMELL IMMEDIATELY AFTER GEAR UP, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, ALSO OPERATIONAL CHECKS WERE PERFORMED WITH ENGINES RUNNING AT DIFFERENT PSDR 98ZZZM435Accumulator · req'd serviceFLT 5657 - AIRCRAFT LOST BRAKING FORCE ON LEFT SIDE AFTER LANDING IN ICT. ICT MAINTENANCE BLED BRAKE SYSTEM AND RETURNED THE AIRCRAFT TO SERVICE WITH NO FURTHER INCIDENT. (M)SDR CA980309004Horn · loose(CAN) FLIGHT CREW REPORTED A VIBRATION IN CERTAIN FLIGHT CONDITIONS. ATTACH RIVETS ON LT AND RT ELEVATOR CONTROL HORNS WERE LOOSE AND WOULD CAUSE VIBRATION IN FLIGHT. HORNS REPLACED.SDR 98ZZZX1100Fork · crackedPROPELLER INSPECTION FOUND FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. THREE CRACKS.
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