# Service difficulty reports: N218YV, cancelled Aug 18, 2015

A list on [N218YV, cancelled Aug 18, 2015](https://openairdocs.org/deregistered/N218YV-2015-08-18.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR A8OA2014F00068](https://openairdocs.org/sdr/A8OA2014F00068.md): Pressure Switch · defective · Feb 9, 2014 · N218YV · Beech 1900D · Propeller Controlling System
  > LEFT ENGINE AFX, AUTOFEATHER, ANNUNCIATOR DOES NOT ILLUMINATE WITH POWER LEVERS ABOVE 89-91 PERCENT N1.
- [SDR A8OA2013040200004](https://openairdocs.org/sdr/A8OA2013040200004.md): Pressure Switch · defective · Mar 31, 2013 · N218YV · Beech 1900D · Engine Oil Indicating System
  > WITH AUTOFEATHER ARMED AND POWERED AND PASSING APPROX 93-94 PERCENT THE AFX ANNUNCIATOR ILLUMINATES. AFTER TROUBLESHOOTING, REMOVED DEFECTIVE RT HIGH OIL PRESSURE SWITCH, INSTALLED NEW SWITCH IAW MM CHAPTER 61-21-01. GROUND RUN UP OPERATED WITHIN SPECIFICATI
- [SDR GLBA20110531F](https://openairdocs.org/sdr/GLBA20110531F.md): Bulkhead · cracked · May 31, 2011 · N218YV · Beech 1900D · Wing Main, Frame Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE BULKHEAD WHERE THE HYD POWERPACK ATTACHES, LT INBD WING, 3.6" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-004. MATERIALS UTILI
- [SDR GLBA20110526G](https://openairdocs.org/sdr/GLBA20110526G.md): Skin · damaged · May 26, 2011 · N218YV · Beech 1900D · Ailerons
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MX FOUND THE AILERON SCRAPED 32" OF OTBD, TOP LWR AND FWD SKIN DAMAGED AND OTBD 4 RIBS AND DOUBLERS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-27-0
- [SDR GLBA20110516H](https://openairdocs.org/sdr/GLBA20110516H.md): Circuit Board · inoperative · May 14, 2011 · N218YV · Beech 1900D · Propeller/Propulsor System Wiring
  > SIG EVENT - PILOT REPORTED THAT THE LT AFX ANNUNCIATOR AND REPEATER FLICKERED AND THEN WENT OUT, CAME BACK ON FOR A WHILE AND WENT OUT AGAIN. MX REPLACED PCB 129.
- [SDR GLBA20110307F](https://openairdocs.org/sdr/GLBA20110307F.md): Structure · cracked · Mar 5, 2011 · N218YV · Beech 1900D · Stabilizer Control System
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RT STABILON OB TIP DAMAGED WHILE PARKING IN HANGER. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-55-005. MATERIALS UTILIZED ARE INCL
- [SDR GLBA20110214G](https://openairdocs.org/sdr/GLBA20110214G.md): Structure · damaged · Feb 12, 2011 · N218YV · Beech 1900D · Vertical Stabilizer Miscellaneous Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX THE RT STABILON WAS DAMAGED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSP IAW EO 11-1900-55-003. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA20110202F](https://openairdocs.org/sdr/GLBA20110202F.md): Structure · cracked · Feb 2, 2011 · N218YV · Beech 1900D · Horizontal Stabilizer Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND 4 CRACKS AROUND THE VENT HOLE IN THE VERT STAB BEHIND THE BULLET CTR WEB, ALL 4 CRACKS ARE.5" IN LENGTH. SUPLEMENTAL INFORMATION WILL BE SUBMITTED UPON COMPLETION OF THE REPAIR AND RETENTION OF THE PAP
- [SDR GLBA20100505G](https://openairdocs.org/sdr/GLBA20100505G.md): Stringer · cracked · May 5, 2010 · N218YV · Beech 1900D · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND IN A CUTOUT AT STRINGER 9AR AND F.S. 177.3. CRACK IS APPROX.8" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-019. MATERIALS UTILIZED ARE INC
- [SDR GLBA20100505F](https://openairdocs.org/sdr/GLBA20100505F.md): Stringer · cracked · May 5, 2010 · N218YV · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND IN A CUTOUT AT STRINGER 9AR AND FS 163.9. CRACK IS APPROX.5" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-018. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA2009091409G](https://openairdocs.org/sdr/GLBA2009091409G.md): Skin · cracked · Sep 12, 2009 · N218YV · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - PILOTS REPORTED THAT THE FUSELAGE WAS PUNCTURED IN THE LT FUSELAGE JUST FWD OF FS 273.25 ON THE UPPER SKIN. DAMAGED AREA APPROX 2.1 INCH BY 3.5 INCH. (2) CRACKS PRESENT. (1) CRACK APPROX 2.3 INCHES AND THE OTHER 1.1 INCH IN LENGTH. MX REPA
- [SDR GLBA20090914F](https://openairdocs.org/sdr/GLBA20090914F.md): Skin · gouged · Sep 12, 2009 · N218YV · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - PILOTS REPORTED A SMALL DENT IN THE LT FUSELAGE JUST FWD OF FS 258.25 ON THE UPPER SKIN. DAMAGED AREA APPROX.250 INCH BY.750 INCH. MX REPAIRED THE AFFECTED AREA IAW EO 09-1900-53-019. RII INSP C/W IAW GLA EO 09-1900-53-019.
- [SDR GLBA20090720F](https://openairdocs.org/sdr/GLBA20090720F.md): Skin · cracked · Jul 17, 2009 · N218YV · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING ROUTINE SCHEDULED MX TWO CRACKS ON TOP OF FUSELAGE AT FS 150.6 WERE DISCOVERED. TOP CENTERLINE 1 RIVET HEAD SHEARED INBD OF CRACK 1.250 INCHES LONG AND A.250 INCH CRACK LT OF CENTERLINE. MX REPAIRED AFFECTED AREA IAW EO 09-1900-53-009. REPAIR AREA A
- [SDR GLBA20090508C](https://openairdocs.org/sdr/GLBA20090508C.md): Valve · worn · May 8, 2009 · N218YV · Beech 1900D · Vacuum Distribution System
  > FLIGHT 5145 - THE PILOTS REPORTED THAT DURING CRUISE THE VACUUM PRESSURE WAS READING AS LOW AS 3.5 AT FLIGHT LEVEL 220. MAINTENANCE REMOVED AND REPLACED THE VACUUM REGULATOR VALVE IAW B1900D MM 37-00-01. THE OPERATIONAL CHECK WAS GOOD.
- [SDR GLBA20090408B](https://openairdocs.org/sdr/GLBA20090408B.md): Vor System · inoperative · Apr 8, 2009 · N218YV · Beech 1900D · Visual Omnirange (VOR) System
  > PILOTS REPORTED THAT THE NR 2 NAV RADIO WAS INOPERATIVE AND RETURNED TO DEN. MAINTENANCE REMOVED AND REPLACED THE VOR-ILS RECEIVER IAW MM 34-20-00. OPERATIONAL CHECK WAS GOOD.
- [SDR GLBA200903211](https://openairdocs.org/sdr/GLBA200903211.md): Cable · loose · Mar 21, 2009 · N218YV · Beech 1900D · Propeller Controlling System
  > PILOTS REPORTED THAT TAKEOFF ABORTED DUE TO 2 PROP RPM AT 1500. MAINTENANCE FOUND THE GOVERNOR CONTROL CABLE LOOSE FROM FORWARD MOUNT. RE-ATTACHED & SAFETIED. OPERATIONAL CHECKS GOOD I.A..W 61-20-00.
- [SDR GLBA20090315A](https://openairdocs.org/sdr/GLBA20090315A.md): Governor · low torque · Mar 3, 2009 · N218YV · Beech 1900D · Propeller Governor
  > ABORTED TAKEOFF BECAUSE THE RT PROPELLER RPM ONLY CAME UP TO 1600 AND THEY THEN ABORTED THE TAKEOFF. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE RIGHT PROPELLER GOVERNOR OUT RIG. MAINTENANCE RIGGED THE ENGINEBY TURNING THE PROP RPM SCREW OUT AND TESTED TH
- [SDR GLBA200910092](https://openairdocs.org/sdr/GLBA200910092.md): Switch · out of adjust · Jan 5, 2009 · N218YV · Beech 1900D · Propeller Feathering/Reversing
  > ON FINAL APPROACH THE PILOTS REPORTED THAT THE NR 2 ENGINE BEGAN TO AUTO-FEATHER AT 500 LBS OF TORQUE. MX ADJUSTED THE LT AND RT AUTOFEATHER ARMING SWITCHES IAW B1900D MM 61-21. OPS CHECK WAS GOOD.
- [SDR GUUA12040702](https://openairdocs.org/sdr/GUUA12040702.md): Hinge Bracket · corroded · Dec 4, 2007 · N218YV · Beech 1900D · Elevator Miscellaneous Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET.
- [SDR GUUA12040701](https://openairdocs.org/sdr/GUUA12040701.md): Hinge Bracket · corroded · Dec 4, 2007 · N218YV · Beech 1900D · Elevator Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET.
- [SDR GUUA11240701](https://openairdocs.org/sdr/GUUA11240701.md): Annunciator · warning light · Nov 24, 2007 · N218YV · Beech 1900D · Extinguishing System
  > FLIGHT: 9269, DURING FLIGHT, RT FIRE DISCHARGE ANUNCIATOR ILLUMINATED. REPLACED TERMINAL ON RT FIRE EXTINGUISHER.
- [SDR GUUA11130701](https://openairdocs.org/sdr/GUUA11130701.md): Downlock Switch · loose · Nov 13, 2007 · N218YV · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9200, DURING APPROACH LANDING GEAR UNSAFE LIGHTS DID NOT ILLUMINATE (3) GREEN INDICATION DID NOT ILLUMINATE WHEN GEAR HANDLE PLACED IN THE DOWN POSITION. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. REPLACED CIRCUIT BREAKER 16 AND RESECURED LT MAIN
- [SDR GUUA05200702](https://openairdocs.org/sdr/GUUA05200702.md): Switch · out of adjust · May 20, 2007 · N218YV · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9267 EYW/MIA DURING APPROACH LANDING GEAR HORN AND LIGHT ANNUNCIATED AT ABOUT 75 PERCENT N1 OR ABOUT 500LBS OF TORQUE. SYSTEM WORKS BUT AT A LOWER VALUE THAN NORMAL. ADJUSTED PEDESTAL SWITCHES OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.
- [SDR GUUA05040703](https://openairdocs.org/sdr/GUUA05040703.md): Circuit Breaker · unknown · May 4, 2007 · N218YV · Beech 1900D · Landing Gear System Wiring
  > FLIGHT: 9247 FLL/FLL - AFTER TAKEOFF LANDING, GEAR DID NOT RETRACT. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED THE LANDING GEAR CONTROL CIRCUIT BREAKER. OPERATIONAL CHECK NORMAL.
- [SDR GUUA10100601](https://openairdocs.org/sdr/GUUA10100601.md): Unknown · odor · Oct 10, 2006 · N218YV · Beech 1900D · Air Distribution System
  > DURING FLIGHT, STRONG LUBRICATION SMELL PRESENT IN THE COCKPIT AND CABIN. INSPECTED UNDER FLOORBOARDS IN CABIN AND COCKPIT CLEANED HYDRAULIC FLUID DUE TO OVERSERVICE NO LUBRICATION SMELL NOTED AT THIS TIME.
- [SDR GUUA06110601](https://openairdocs.org/sdr/GUUA06110601.md): Actuator · malfunctioned · Jun 11, 2006 · N218YV · Beech 1900D · Landing Gear Actuator
  > FLIGHT:9280 EYW/TPA AFTER TAKEOFF WHEN LANDING GEAR SELECTED UP THREE GREEN ANNUNCIATOR ILLUMINATED, MOTOR RUNS INTERMITTENT, BREAKER POPS. CONTINUED TO TPA LANDED WITHOUT INCIDENT. MAINTENANCE FERRY TO FLL. REPLACED LEFT MAIN LANDING GEAR ACTUATOR. TEST F
- [SDR GUUA05180601](https://openairdocs.org/sdr/GUUA05180601.md): Valve · faulty · May 18, 2006 · N218YV · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT: 9235 JAX/TPA DURING APPROACH LANDING GEAR RELAY CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AND LOWERED LANDING GEAR NORMALLY. REPLACED LANDING GEAR SERVICE VALVE.
- [SDR GUUA04280601](https://openairdocs.org/sdr/GUUA04280601.md): Circuit Breaker · tripped · Apr 28, 2006 · N218YV · Beech 1900D · Landing Gear Retraction/Extension System
  > FLIGHT:9266 MHH/PBI AFTER TAKEOFF LANDING GEAR CIRCUIT BREAKER TRIPPED LANDING GEAR WOULD NOT RETRACT. DIVERTED TO FLL LANDED WITHOUT INCIDENT. TROUBLESHOT LANDING GEAR SYSTEM. CHECKED POWER PACK FLUID. LANDING GEAR OPERATIONAL CHECKS NORMAL NO DEFECTS NOTED
- [SDR GUUA04240601](https://openairdocs.org/sdr/GUUA04240601.md): Printed Ckt Board · faulty · Apr 24, 2006 · N218YV · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9246, AFTER TAKEOFF LANDING GEAR CIRCUIT BREAKER POPPED COULD NOT RETRACT THE LANDING GEAR. DIVERTED, LANDED WITHOUT INCIDENT. REPLACED TIME DELAY PC BOARD.
- [SDR GUUA04160601](https://openairdocs.org/sdr/GUUA04160601.md): Elec Connector · dirty · Apr 16, 2006 · N218YV · Beech 1900D · Landing Gear Position and Warning
  > FLIGHT: 9287, DURING APPROACH, LANDING GEAR RELAY CIRCUIT BREAKER POPPED.CLEANED LT AND RT NOSE LANDING GEAR ACTUATOR CONNECTOR PLUGS FOR DOWN LOCK SWITCHES. OPERATIONAL CHECK NORMAL, NO DEFECTS NOTED.
- [SDR GUUA02010601](https://openairdocs.org/sdr/GUUA02010601.md): Annunciator · loose · Feb 1, 2006 · N218YV · Beech 1900D · Landing Gear Position and Warning
  > EYW/FLL DURING APPROACH LANDING GEAR WARNING SOUNDED. TIGHTENED LANDING GEAR ANNUNCIATOR HOUSING.
- [SDR 65837](https://openairdocs.org/sdr/65837.md): Gas Generator · malfunctioned · Oct 14, 2004 · N218YV · Beech 1900D · Engine (Turbine/Turboprop)
  > DURING CRUISE, OIL PRESSURE LOW ANNUNCIATOR ILLUMINATED, OIL PRESSURE GAUGE INDICATED 50 AND SLOWLY DROPPING, CREW SECURED LT ENGINE AND DECLARED AND EMERGENCY AND LANDED. REMOVED AND REPLACED LT GAS GENERATOR, POWER SECTION AND PROPELLER, RIGGED ENGINE, PER
- [SDR 58817](https://openairdocs.org/sdr/58817.md): Knob · unsecure · Feb 13, 2004 · N218YV · Beech 1900D · Brake
  > RT BRAKE WILL NOT RELEASE. RESECURED BRAKE PARKING KNOB, LUBED ACT.
- [SDR 57171](https://openairdocs.org/sdr/57171.md): Gyro · inoperative · Dec 18, 2003 · N218YV · Beech 1900D · Directional Gyro and Indicating System
  > SHORTLY AFTER DEPARTURE FROM PIT CREW NOTICED CAPT'S GYROSCOPIC DIRECTIONAL COMPASS SYSTEM WASN'T WORKING CORRECTLY. SO DECEIDED TO RETURN TO PIT. AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. T/S REPAIRED PINS 5 AND 7 OF CONNECTOR J203 AT NR 1 FLUX DETECTO
- [SDR AMWA65](https://openairdocs.org/sdr/AMWA65.md): Rib · cracked · Oct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 39.289 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT AND ONE PLACE ON THE LEFT SIDE NEAR THE CENTER STRINGER INTERSECTION. REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE TO BMM P
- [SDR AMWA64](https://openairdocs.org/sdr/AMWA64.md): Rib · cracked · Oct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE RIGHT SIDE NEAR AFT STRINGERS INTERSECTION REPAIRED CRACK TO RIB FLANGE IN ACCORDANCE TO BMM P/N 114-590021-9, 51-70-03.
- [SDR AMWA63](https://openairdocs.org/sdr/AMWA63.md): Rib · cracked · Oct 10, 2003 · N218YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, THE RIB FLANGE AT CANTED STAB STA 54.026 WAS FOUND CRACKED IN THREE PLACES ON THE RIGHT SIDE NEAR THE FORWARD, CENTER AND AFT STRINGERS AND TWO PLACES ON THE LEFT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANC
- [SDR 048076](https://openairdocs.org/sdr/048076.md): Keel · gouged · Feb 21, 2003 · N218YV · Beech 1900D · Fuselage Main, Keel
  > WHILE DOING AN INSPECTION, MAINTENANCE DISCOVERED THE LT INBOARD MAIN LANDING GEAR KEEL WAS GOUGED. MAINTENANCE REPAIRED THE KEEL. NO TEARDOWN REPORT WILL BE REQUIRED.
- [SDR AMWA13](https://openairdocs.org/sdr/AMWA13.md): Spar Cap · chafed · Feb 16, 2003 · N218YV · Beech 1900D · Wing Spar
  > UPON A MAINTENANCE CHECK IT WAS DISCOVERED THAT BOTH THE RIGHT AND LEFT SPAR CAP WAS CHAFING THE WHEEL WELL. BLENDED THE CHAFED AREA IN ACCORDANCE TO RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT WILL BE REQUIRED.
- [SDR 047632](https://openairdocs.org/sdr/047632.md): Tube · cracked · Feb 6, 2003 · N218YV · Beech 1900D · Engine Bleed Air System
  > UPON APPROACH FOR LANDING ON FLIGHT 5441 IN CHARLOTTE NORTH CAROLINA, THE LEFT ENGINE TORQUE FELL TO BETWEEN 0-500LBS. ALL THE OTHER ENGINE INDICATIONS WERE NORMAL. THE CREW THEN SHUT DOWN THE ENGINE. THE CREW ALSO DID THE EMERGENCY CHECKLIST AND DECLARED AN E
- [SDR MASA98144](https://openairdocs.org/sdr/MASA98144.md): Cowling · loose · Jul 18, 1998 · N218YV · Beech 1900D · Engine Cowling System
  > FLT 5499 - JAX-MCO - ON APPROACH, THE CREW NOTICED THE RT PROP PITCH CHANGING UNCOMMANDED. THEY THEN NOTICED THE RT TOP COWLING WAS COMING LOOSE, AND WAS RESTING ON THE PROP GOVERNOR AND BETA VALVE. THE CREW DECLARED AN EMERGENCY, SHUT DOWN THE RT ENGINE, AN
- [SDR MASA98131](https://openairdocs.org/sdr/MASA98131.md): Computer · malfunctioned · Jun 25, 1998 · N218YV · Beech 1900D · Ground Proximity System
  > FLT 5451 - PFN-MCO - ON SHORT FINAL APPROACH TO MCO, CREW RECEIVED A 'TOO LOW GEAR' AURAL WARNING. INITIATED A GO AROUND AND REQUESTED THE RESCUE TRUCKS STANDBY. ALL OTHER GEAR INDICATIONS WERE NORMAL AND THE GPWS DID NOT ACTIVATE ON THE SECOND APPROACH. TH
- [SDR MASA98002](https://openairdocs.org/sdr/MASA98002.md): Pressure Switch · failed · Jan 1, 1998 · N218YV · Beech 1900D · Propeller Controlling System
  > PIT/MBS - FLT 5999 - LEFT AUTOFEATHER FAILED ON CLIMB-OUT. MAINTENANCE REMOVED AND REPLACED PRESSURE SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

## 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 = 'N218YV' AND deregistration_id = 'N218YV-2015-08-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N218YV-2015-08-18/reports

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