# Service difficulty reports: N5YV, cancelled Mar 27, 2013 A list on [N5YV, cancelled Mar 27, 2013](https://openairdocs.org/deregistered/N5YV-2013-03-27.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 56207](https://openairdocs.org/sdr/56207.md): Line · broken · Nov 16, 2003 · N5YV · Beech 1900D · Engine Starting System > DURING CRUISE FLIGHT RT ENGINE QUIT. CREW RETURNED TO ABQ AND LANDED WITHOUT ANY INCIDENTS. PASSENGERS DEPLANED AT PRECAUTION WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED P-3 BROKEN LINE. CHANGE IT TO P-3 FILTER. P/N 3123019-01. - [SDR AMWA55](https://openairdocs.org/sdr/AMWA55.md): Rib · cracked · Sep 19, 2003 · N5YV · Beech 1900D · Vertical Stabilizer, Spar/Rib > FOUND TWO CRACKS ON RIB P/N 101-640000-59 AT THE RIVETS BESIDE THE STRINGERS INTERSECTIONS. THE STRINGER THAT INTERSECT THE RIB ARE P/N 101-640000-39 AND 101-640000-46. BOTH CRACKS WERE REAIRED IAW THE MFG STRUCTURAL REPAIR MANUAL. - [SDR 53300](https://openairdocs.org/sdr/53300.md): Rudder · malfunctioned · Aug 6, 2003 · N5YV · Beech 1900D · Rudder Control System > AFTER DEPARTURE, ON FLIGHT 5530, THE CREW HAD A HARD RT THEN LAT UNCOMMANDED RUDDER BOOST. WHILE EXECUTING THE UNCOMMANDED RUDDER BOOST ACTIVATION EMERGENCY PROCEDURE CHECKLIST A THIRD SEVERE RUDDER BOOST ACTIVATION OCCURRED, FOLLOWED BY SEVERE OSCILLATIONS O - [SDR 045745](https://openairdocs.org/sdr/045745.md): Switch · inoperative · Dec 9, 2002 · N5YV · Beech 1900D · Auto Throttle System > DURING TAKE OFF ROLL ON FLIGHT ABOUT 80 KILOMETERS OUT, THE AUTOFEATHER ON AND REPEATER LIGHTS WENT OUT. THIS INDICATED THAT THE AUTOFEATHER WAS NOT ARMED. THE FLIGHT CREW ABORTED THE TAKE OFF AND RETURNED TO THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJ - [SDR 2002F00978](https://openairdocs.org/sdr/2002F00978.md): Gas Generator · malfunctioned · Aug 25, 2002 · N5YV · Beech 1900D · Turbine Engine Compressor Section > LEFT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. OIL PRESSURE WAS BELOW 60 PSI, LEFT ENGINE SHUTDOWN. LEFT GAS GENERATOR AND POWER SECTION WERE REPLACED. (M) - [SDR AMWA042655](https://openairdocs.org/sdr/AMWA042655.md): Engine · lack of lube · Aug 25, 2002 · N5YV · Beech 1900D · Engine (Turbine/Turboprop) > WHILE INFLIGHT FROM PANAMA CITY, FLORIDA THE LEFT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. THE OIL PRESSURE WAS BELOW 60 PSI. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO FIELD WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THE THE - [SDR 042655](https://openairdocs.org/sdr/042655.md): Gas Generator · failed · Aug 25, 2002 · N5YV · Beech 1900D · Engine (Turbine/Turboprop) > WHILE INFLIGHT FROM PANAMA CITY, FLORIDA THE LEFT ENGINE LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED. THE OIL PRESSURE WAS BELOW 60 PSI. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO FIELD WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THE THE LE - [SDR 2002F00977](https://openairdocs.org/sdr/2002F00977.md): Control Cable · improper · Aug 20, 2002 · N5YV · Beech 1900D · Aileron Tab Control System > FLT 5466 - AFTER LANDING IN PFN, CREW REPORTED AILERON TRIM WAS IMPROPERLY RIGGED. MAINTENANCE INSPECTED AND FOUND AILERON TRIM CABLE IMPROPERLY INSTALLED. CABLE WAS CORRECTLY INSTALLED AND RIGGED. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE - [SDR 042514](https://openairdocs.org/sdr/042514.md): Aileron · misrigged · Aug 20, 2002 · N5YV · Beech 1900D · Aileron Control System > AFTER LANDING IN PANAMA CITY, FLORIDA ON FLIGHT 5466, THE CREW REPORTED THAT THE AILERON WAS RIGGED IMPROPERLY.MAINTENANCE IN PANAMA CITY FLORIDA, REINSTALLED THE CABLE DRUM AND THE CABLE TENSION. THE AIRCRAFT WAS THEN TEST FLOWN WITH SATISFACTORY RESULTS. NO - [SDR MASA99149](https://openairdocs.org/sdr/MASA99149.md): Lock · dirty · Aug 24, 1999 · N5YV · Beech 1900D · Passenger/Crew Doors > FLT 5972 - PIT-DUJ - PRIOR TO DEPARTURE, THE CREW REPORTED THE CABIN DOOR ANNUNCIATOR LIGHT EXTINGUISHED PRIOR TO LOCKING THE DOOR. MAINTENANCE CLEANED AND LUBED THE SHAFT DOOR LOCK, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR MASA98084](https://openairdocs.org/sdr/MASA98084.md): Hose · leaking · Apr 16, 1998 · N5YV · Beech 1900D · Engine Oil Cooler > FLT 4441 - AFTER TAKEOFF OF TRAINING FLIGHT, CREW NOTICED THE MASTER WARNING FLASHING THEN NOTICED THE OIL PRESSURE LOW ANNUNCIATOR ILLUMINATED. THE ENGINE WAS SECURED AND THE CREW DECLARED AN EMERGENCY. AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAIN - [SDR MASA98028](https://openairdocs.org/sdr/MASA98028.md): Seal · failed · Feb 16, 1998 · N5YV · Beech 1900D · Passenger/Crew Doors > FLT 5288 - PBI-TLH - AT APPROXIMATELY 20,000 FEET, THE CREW HEAR A SHORT BURST FOLLOWED BY IMMEDIATE DECOMPRESSION. THE CREW DECLARED AN EMERGENCY AND EXECUTED A DESCENT TO 10,000 FEET. DURING THE DESCENT THE CREW COULD NOT GET OXYGEN TO FLOW TO THE MASKS UN - [SDR MASA97198](https://openairdocs.org/sdr/MASA97198.md): Wire · chafed · Oct 24, 1997 · N5YV · Beech 1900D · Communications System Wiring > LIT/MSY - FLT 5445 - ON APPROACH TO MSY, PILOT SELECTED GEAR DOWN AND THE LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. THE CREW DECLARED AN EMERGENCY. THE GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED UNEVENTFULLY. THE AIRCRAFT WAS - [SDR MASA97086](https://openairdocs.org/sdr/MASA97086.md): Hinge · corroded · Jul 7, 1997 · N5YV · Beech 1900D · Elevator Structure > DURING A LIGHTNING STRIKE INSPECTION, THE LEFT AND RIGHT OUTBOARD ELEVATOR HINGE ASSEMBLIES WERE FOUND TO HAVE HEAVY CORROSION (EXFOLIATION). REMOVED AND REPLACED THE LEFT AND RIGHT HINGE ASSEMBLIES. (X) - [SDR MASA97054](https://openairdocs.org/sdr/MASA97054.md): Brake Cylinder · worn · May 23, 1997 · N5YV · Beech 1900D · Master Cylinder/Brake Valve > HGR/RDG - FLT 5356 - PILOT'S LEFT BRAKE LOSES PRESSURE WHEN RIGHT RUDDER PEDAL IS DEPRESSED. MAINTENANCE REMOVED AND REPLACED THE LEFT BRAKE CYLINDER, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) - [SDR 96ZZZX890](https://openairdocs.org/sdr/96ZZZX890.md): Sun Gear · defective · Jan 15, 1996 · N5YV · Beech 1900D · Turbine Engine Reduction Gear > ALTHOUGH ALL INDICATIONS POINT TO AN ELECTRICAL DISCHARGE, THE POSSIBILITY OF A SUN GEAR FAILURE IS NOT BEING RULED OUT. THE NR 6 BEARING AND THE SUN GEAR WILL BE SHIPPED FOR FURTEHR INVESTIGATION. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 n_number = 'N5YV' AND deregistration_id = 'N5YV-2013-03-27' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N5YV-2013-03-27/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.