# Service difficulty reports: N237YV, cancelled Feb 10, 2012

A list on [N237YV, cancelled Feb 10, 2012](https://openairdocs.org/deregistered/N237YV-2012-02-10.md).

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

- [SDR GLBA20110802F](https://openairdocs.org/sdr/GLBA20110802F.md): Placard · delaminated · Aug 1, 2011 · N237YV · Beech 1900D · Placards and Markings
  > PILOT REPORTED THAT THE AIR STAIR DOOR PLACARD DELAMINATED. MX REPLACED THE PLACARD.
- [SDR GLBA20110801G](https://openairdocs.org/sdr/GLBA20110801G.md): Mount · worn · Jul 29, 2011 · N237YV · Beech 1900D · Passenger/Crew Doors
  > MX FOUND THE AIRSTAIR DOOR LOWER COUNTER BALANCE HAS A WORN MOUNT HOLE. MX REPLACED THE LOWER BALANCE MOUNT IAW BMM 52-10-01, PN: 126-514105-33, OPS CK GOOD.
- [SDR GLBA20110706F](https://openairdocs.org/sdr/GLBA20110706F.md): Tire · failed · Jul 5, 2011 · N237YV · Beech 1900D · Wheel/Ski/Float
  > PILOT REPORTED THAT THE LT INBD MAIN TIRE STRIPPED OF ITS CORD AFTER TOUCHDOWN, SHIMMY ON TOUCHDOWN. MX REPLACED THE NR 2 WHEEL ASSY IAW IAM TC 1900-3240-01.
- [SDR GLBA20100309F](https://openairdocs.org/sdr/GLBA20100309F.md): Frame · cracked · Mar 8, 2010 · N237YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK IN THE FRAME RADIUS AT THE AIRSTAIR DOOR ENTRANCE FWD FRAME AT FS 177.350 AT APPROX STR 12L WAS FOUND, CRACK APPROX.5". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW
- [SDR GLBA20100302G](https://openairdocs.org/sdr/GLBA20100302G.md): Frame · cracked · Mar 2, 2010 · N237YV · Beech 1900D · Fuselage Main, Frame
  > UPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L CRACK IS APPROX 2" LONG. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-007. MATERIALS UTILIZED ARE INCLUDED IN THE
- [SDR GLBA20100302FA](https://openairdocs.org/sdr/GLBA20100302FA.md): Spar · damaged · Mar 1, 2010 · N237YV · Beech 1900D · Wing Spar
  > MAJOR REPAIR - UPON ROUTINE SCHEDULED MX A LOCK FASTENER HOLE IN THE LT WING SPAR AT APPROX WS 93.250 WAS FOUND STEPPED. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-57-002. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA20100302F](https://openairdocs.org/sdr/GLBA20100302F.md): Frame · cracked · Mar 1, 2010 · N237YV · Beech 1900D · Wing Spar
  > MAJOR REPAIR - UPON ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT THE RADIUS OF FRAME AT FS 177.350 AT APPROX STR 12L. CRACK IS APPROX 2" LONG.
- [SDR GLBA20100118A](https://openairdocs.org/sdr/GLBA20100118A.md): Boot · sparks · Jan 18, 2010 · N237YV · Beech 1900D · Propeller/Rotor Anti-Ice/De-Ice System
  > SPARKS WERE COMING FROM NR 1 PROP WHEN DE-ICE WAS ENGAGED HAD LARGE BURN MARK ON BOOT. MX R & R THE LT PROPELLER IAW TASKCARD 1900-6110.00. THE OPS CHECK AND LEAK CHECK WERE GOOD PN HC-E4A-3J SN ON HJ2050, SN OFF HJ1695. RII INSPECTIONS WAS SATISFACTORY IAW
- [SDR GLBA20091120F](https://openairdocs.org/sdr/GLBA20091120F.md): Bleed Air Sys · contaminated · Nov 17, 2009 · N237YV · Beech 1900D · Air Distribution System
  > SMOKE/SMELL - PILOTS REPORTED THAT BURNING ODOR WAS PRESENT FROM THE CAPTAINS SIDE THAT SMELLED LIKE PLASTIC. NO SMOKE WAS OBSERVED. MX CLEANED GLYCOL FROM WINDOW DRIP TRAY AND INSPECTED THE FUEL PANEL FOR ANY EVIDENCE OF GLYCOL. NONE NOTED. MX RAN THE AC
- [SDR GLBA200910211](https://openairdocs.org/sdr/GLBA200910211.md): Bearing · deteriorated · Oct 20, 2009 · N237YV · Beech 1900D · Wheel/Ski/Float
  > UPON LANDING, IT FELT LIKE THE LT BRAKE WAS SLUGGISH AND THE SWA THE LT MAIN TIRE OUTSIDE WHEEL FALL OFF OF THE HUB ASSY. MX REMOVED AND REPLACED THE LT MLG IAW MM 32-10-00, RII INSP COMPLIED IAW TASKCARD 4.3.6 AND RII OF UP/DOWN/SAFETY SWITCH INSTALLATION WA
- [SDR GLBA200907061](https://openairdocs.org/sdr/GLBA200907061.md): Engine · power loss · Jul 6, 2009 · N237YV · Beech 1900D · Engine (Turbine/Turboprop)
  > ON CLIMB THROUGH 9000 FT, NR 2 PROP RPM DROPPED TO 500 RPM & TORQUES INCREASED TO 4700 FT LBS. SUSPECTED GOVERNOR FAILURE, SET MAX PWR, PROP LEVERS FULL FWD, & VERIFIED MLG & FLAPS UP. NR 2 ENG TORQUE STAYED AT 4700 FT LBS FOR APPROX 30 SEC & RE-SET TO 2000 F
- [SDR GLBA20090531F](https://openairdocs.org/sdr/GLBA20090531F.md): Circuit Board · inoperative · May 29, 2009 · N237YV · Beech 1900D · Propeller/Propulsor System Wiring
  > THE PILOTS REPORTED THAT THE AFX SYS FEATHERED THE NR 1 PROPELLER WHILE ON FINAL WITH PROPS FULL FWD AND TORQUE AT 1000 LBS. MX REMOVED AND REPLACED THE A123 PRINTED CIRCUIT BOARD IAW MM 20-00-01. OPS CHECKS WERE NORMAL.
- [SDR GLBA20090522G](https://openairdocs.org/sdr/GLBA20090522G.md): Pressure Switch · worn · May 18, 2009 · N237YV · Beech 1900D · Propeller Feathering/Reversing
  > AFX ANNUNCIATORS AND REPEATER LIGHTS WOULD NOT ILLUMINATE WHEN POWER ADVANCED ABOVE 1000 FT LBS ON TAKEOFF ROLL. MAINT REMOVED AND REPLACED THE HIGH PRESSURE SWITCH CONNECTOR PLUG IAW GMM 9.3.0. MAINT ALSO REMOVED AND REPLACED THE NR1 AUTOFEATHER HIGH PRESSU
- [SDR GLBA20090520F](https://openairdocs.org/sdr/GLBA20090520F.md): Circuit Board · failed · May 18, 2009 · N237YV · Beech 1900D · Propeller Indication System
  > PILOTS REPORTED THAT THE AFX ANNUNCIATORS AND REPEATER LIGHTS EXTINGUISHED AFTER V. THE AFX FAULT ANNUNCIATOR DID NOT ILLUMINATE. MAINT REMOVED AND REPLACED THE PRINTED CIRCUIT BOARD A123 IAW 1900D MM 61-20-00. MAINT ADDTIONALLY COMPLIED WITH FLEET CAMPAIGN DI
- [SDR GLBA20090329A](https://openairdocs.org/sdr/GLBA20090329A.md): Windshield · cracked · Mar 29, 2009 · N237YV · Beech 1900D · Flight Compartment Windows
  > PILOTS REPORTED THAT THE CAPTAINS WINDSHIELD CRACKED ON/IN CRUISE FLIGHT. AIRCRAFT RETURNED TO "DEN". MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDOW IAW SRM 56-10-00.
- [SDR GLBA200811131](https://openairdocs.org/sdr/GLBA200811131.md): Stringer · cracked · Nov 11, 2008 · N237YV · Beech 1900D · Fuselage Main, Longeron/Stringer
  > DURING CONFORMITY CHECKS A CRACK WAS FOUND AT STRINGER CUTOUT AT FS 177 AND 9R. CRACK RADIATES.2 INCH. REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW B1900D SRM 51-70 AT FS 177. REPAIR AREA APPROX 4.6 INCHES BY 2.6 INCHES. 2024 T3,.071 INCHES, MS20470 RI
- [SDR BSAASDR0715](https://openairdocs.org/sdr/BSAASDR0715.md): Warning System · malfunctioned · May 20, 2007 · N237YV · Beech 1900D · Pneumatic Indicating System
  > ON DESCENT THE RT BLEED FAIL ANNUNCIATOR ILLUMINATED. THE CREW LANDED WITH NO FURTHER INCIDENT. EXTENSIVE TROUBLESHOOTING WAS COMPLETED WITH NO DEFECTS FOUND & MULTIPLE GROUND RUNS WERE COMPLETED, BUT COULD NOT DUPLICATE THE PROBLEM.
- [SDR BSAASDR0621](https://openairdocs.org/sdr/BSAASDR0621.md): Spar Cap · corroded · Oct 20, 2006 · N237YV · Beech 1900D · Wing Spar
  > LEVEL 3 PITTING CORROSION WAS FOUND INITIALLY AROUND THE QUICK DRAIN IN THE 3RD INTERIOR SKIN DOUBLER. THIS CORROSION STARTED FROM THE UNTREATED EDGE OF THE QUICK DRAIN FITTING HOLE IN THE WING SKIN, AND PROGRESSED IN ALONG THE BOND LINE BETWEEN THE SKINS. W
- [SDR 58290](https://openairdocs.org/sdr/58290.md): Indicator · stuck · Jan 26, 2004 · N237YV · Beech 1900D · Propeller Indication System
  > ON TAKEOFF ROLL THE LT PROP INDICATOR BEGAN TO READ HIGH, IT THEN WENT TO 2000 AND STUCK. CREW ABORTED TAKEOFF AND RETURNED TO GATE, ON SHUT DOWN INDICATOR STUCK AT 600. THERE WAS NO FURTHER INCIDENT OCCUR. COULD NOT DUPLICATE THE PROBLEM.
- [SDR 52776AMWA1](https://openairdocs.org/sdr/52776AMWA1.md): Generator · failed · Jul 20, 2003 · N237YV · Beech 1900D · DC Generating System
  > ON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RT GENERATOR WOULD NOT STAY ONLINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RIGHT GENERATOR WILL NOT ENERGIZE. MAINTENANCE REMOVED AND REPLACED GENERATOR, GCU AND REPAIRED A WIRE
- [SDR 52776](https://openairdocs.org/sdr/52776.md): Starter Gen · failed · Jul 20, 2003 · N237YV · Beech 1900D · Starter-Generator
  > ON FLIGHT 5521 TAXING OUT, THE CREW NOTICED THE RIGHT GENERATOR WOULD NOT STAY ON LINE. THE AIRCRAFT RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE FOUND THAT THE RIGHT GENERATOR WILL NOT ENERGIZE. THE CORRECTIVE ACTION WAS THAT MAINTENANCE REMOVED AND REPLACED
- [SDR AMWA17](https://openairdocs.org/sdr/AMWA17.md): Finger Doubler · cracked · Mar 5, 2003 · N237YV · Beech 1900D · Fuselage, Powerplant Attach Fittings
  > WHILE PERFORMING AN "A" CHECK ON THE RT ENGINE TRUSS, MAINTENANCE FOUND THAT THE FINGER DOUBLER WAS CRACKED. MAINTENANCE REMOVED AND REPAIRED THE FINGER DOUBLER. NO TEARDOWN REPORT WILL BE REQUIRED.
- [SDR AMWA18](https://openairdocs.org/sdr/AMWA18.md): Plate · damaged · Mar 5, 2003 · N237YV · Beech 1900D · Fuselage, Powerplant Attach Fittings
  > WHILE PERFORMING AN "A" CHECK ON THE LT ENGINE TRUSS, MAINTENANCE FOUND THAT THE LEFT PRESSURE PLATES HAVE RIVET HEAD CONTACT. MAINTENANCE REPAIRED THE PRESSURE PLATE PER THE STANDARD REPAIR MANUAL 57-95-02. NO TEARDOWN REPORT WILL BE REQUIRED.
- [SDR 2002F00272](https://openairdocs.org/sdr/2002F00272.md): Door · out of rig · Feb 25, 2002 · N237YV · Beech 1900D · Emergency Exits
  > DURING CREW CHANGE, THE ON COMING CREW FOR AIRCRAFT FOUND THE RIGHT FORWARD EMERGENCY EXIT DOOR NOT FLUSH WITH THE EXTERIOR OF THE AIRCRAFT. AIRCRAFT MAINTENANCE FOUND THE DOOR TO BE OUT OF RIG, AND ADJUSTED THE DOOR PER MAINTENANCE INSTRUCTION. RETURNED TO
- [SDR 98ZZZM895](https://openairdocs.org/sdr/98ZZZM895.md): Skin · cracked · May 23, 1998 · N237YV · Beech 1900D · Trailing Edge Flaps
  > ICT OVERNIGHT MAINTENANCE, FOUND LEFT INBOARD FLAP TOP SKIN CRACKED AT INBOARD ATTACH BRACKET. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 97ZZZX4233](https://openairdocs.org/sdr/97ZZZX4233.md): Skin · cracked · Sep 17, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > ICT - OVERNIGHT, MAINTENANCE FOUND A CRACK 2 INCHES LONG AT TRAILING EDGE 16 INCHES OUT. STOP DRILLED AND PATCHED IAW SRM 51.00 AND TO 1900-27-00-0001. (X)
- [SDR 97ZZZM976](https://openairdocs.org/sdr/97ZZZM976.md): Skin · cracked · Aug 26, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > DURING A NIGHT INSPECTION, AT ICT, REPAIRED 2 INCHES LONG Y SHAPED CRACK ON RHIB FLAP TOP SKIN IAW WITH TO 1900-27-0001. (M)
- [SDR 97ZZZM975](https://openairdocs.org/sdr/97ZZZM975.md): Skin · cracked · Aug 22, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > AT ICT, AN OVERNIGHT MAINTENANCE INSPECTION, FOUND A CRACK ON THE LHOB. REPAIRED CRACK ON LHOB FLAP TOP SKIN IAW TO 1900-27-00-0001.
- [SDR 97ZZZM907](https://openairdocs.org/sdr/97ZZZM907.md): Flap · cracked · Aug 6, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > RIGHT INBOARD FLAP HAS A.5 INCH CRACK IN TOP SKIN 10 INCHES IN FROM OUTBOARD END ADN 3 INCHES UP FROM TRAILING EDGE. STOP DRILLED CRACK AND PATCH IAW TO 1900-27-00-0001. (M)
- [SDR 97ZZZM940](https://openairdocs.org/sdr/97ZZZM940.md): Dovetail Blkhead · cracked · Jun 19, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > REPLACED LOOSE RIVETS IN DOVETAIL. INSTALLED DOUBLER OVER CRACK IN DOVETAIL BULKHEAD IAW SRM 51-40. REPLACED ACTUATOR ATTACH BRACKET. WORK ACCOMPLISHED IAW TO 1900-27-00-0001. (M)
- [SDR 97ZZZM972](https://openairdocs.org/sdr/97ZZZM972.md): Bulkhead · cracked · Jun 17, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > DURING BEECH TEMP REV 5-6, AN INSPECTION, FOUND THREE CRACKS ON RHIB FLAP DOVETAIL BULKHEAD. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 97ZZZM971](https://openairdocs.org/sdr/97ZZZM971.md): Dovetail · cracked · Jun 17, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > DURING BEECH TEMP REV 5-6 AN INSPECTION, FOUND A CRACK ON THE INBOARD SIDE OF RIGHT DOVETAIL 7 INCH FROM LEADING EDGE. REPAIRED IAW AMWA TO 1900-27-00-0001.
- [SDR 97ZZZM946](https://openairdocs.org/sdr/97ZZZM946.md): Flap · cracked · May 28, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > DURING ROUTINE A.375 INCH CRACK WAS FOUND ON THE 'DOVETAIL'. REPAIRED IAW SRM AND AMWA T.O 1900 27 00 0001. (M)
- [SDR 97ZZZX2778](https://openairdocs.org/sdr/97ZZZX2778.md): Flap · cracked · Apr 23, 1997 · N237YV · Beech 1900D · Trailing Edge Flaps
  > DURING ROUTINE MAINTENANCE, A CRACK WAS FOUND ON RT INBOARD FLAP. REPAIRED IAW SRM AND AMW TO.

## 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 = 'N237YV' AND deregistration_id = 'N237YV-2012-02-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N237YV-2012-02-10/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.