# Service difficulty reports: N182YV, cancelled Mar 8, 2012

A list on [N182YV, cancelled Mar 8, 2012](https://openairdocs.org/deregistered/N182YV-2012-03-08.md).

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

- [SDR GLBA20111003H](https://openairdocs.org/sdr/GLBA20111003H.md): Uplock Switch · inoperative · Oct 1, 2011 · N182YV · Beech 1900D · Landing Gear Position and Warning
  > PILOT REPORTED THAT THE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER THE GEAR WAS RETRACTED. MX REPLACE THE RT LANDING GEAR UPLOCK SWITCH PN: H11-1541GLA IAW TC 1900-3260-00, SYS OPS CHECKED GOOD.
- [SDR GLBA20110930F](https://openairdocs.org/sdr/GLBA20110930F.md): Line · leaking · Sep 29, 2011 · N182YV · Beech 1900D · Fuel Storage
  > PILOT REPORTED THAT FUEL WAS DRIPPING FROM HYD LINES IN LT WHEEL WELL. MX CLEANED AND INSPECTED THE AREA, NO LEAK FOUND.
- [SDR GLBA20110927F](https://openairdocs.org/sdr/GLBA20110927F.md): Handle · unsecure · Sep 26, 2011 · N182YV · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE DOOR HANDLE ON THE FWD RT EMERGENCY EXIT DOOR APPEARS TO BE RECESSED. MX RESECURED THE EMER EXIT DOOR IAW BMM 52-20-00, OK FOR SERVICE.
- [SDR GLBA20110926K](https://openairdocs.org/sdr/GLBA20110926K.md): Extinguisher · overserviced · Sep 24, 2011 · N182YV · Beech 1900D · Fire Bottle, Portable
  > PILOT REPORTED THAT THE PASSENGER FIRE EXTINGUISHER READ OUT IN THE RED, OVER CHARGED. MX REPLACED THE FIRE EXTINGIUSHER.
- [SDR GLBA20110915F](https://openairdocs.org/sdr/GLBA20110915F.md): Pcb · inoperative · Sep 14, 2011 · N182YV · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT AUTOFEATHER ANNUNCIATOR IS INOPERATIVE. REPLACED THE AUTOFEATHER PCB REF BMM 20-00-01, OPS CHECKED GOOD.
- [SDR GLBA20110914001](https://openairdocs.org/sdr/GLBA20110914001.md): Annunciator · inoperative · Sep 14, 2011 · N182YV · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT AUTOFEATHER ANNUNCIATOR IS INOPERATIVE. OPEN
- [SDR GLBA20110816G](https://openairdocs.org/sdr/GLBA20110816G.md): Landing Gear · malfunctioned · Aug 15, 2011 · N182YV · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED THAT WHILE ON A CHECK FLIGHT THE LANDING GEAR WAS SELECTED DOWN, NOTHING HAPPENED AND HAD TO MANUALLY EXTEND THE GEAR, GOT 3 GREENS AND LANDING. MX INSPECTED THE SYS, RESET CB IN LT WHEEL WELL AND CHECKED RELAY K13, PERFORMED GEAR SWINGS IAW AI
- [SDR GLBA20110722F](https://openairdocs.org/sdr/GLBA20110722F.md): Cable · broken · Jul 21, 2011 · N182YV · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE SNUBBER CABLE BROKE UPON OPENING THE AS DOOR. MX REPLACED THE CABLE IAW BMM 52-10-01-201, PN: 129-514119-1GLA.
- [SDR GLBA20110718G](https://openairdocs.org/sdr/GLBA20110718G.md): Bulb · missing · Jul 15, 2011 · N182YV · Beech 1900D · Emergency Lighting
  > DURING PREFLIGHT THE PILOT FOUND THE INST EMERGENCY LIGHT BULB MISSING. MX REPLACED THE EMERGENCY LIGHT BULB, PN: 1864 IAW BMM 33-10-04.
- [SDR GLBA20110621F](https://openairdocs.org/sdr/GLBA20110621F.md): Uplock Switch · failed · Jun 20, 2011 · N182YV · Beech 1900D · Landing Gear Position and Warning
  > "SUP" - SIG EVENT - PILOT REPORTED THAT WHEN THE RETRACTED THE GEAR, THE INTRANSIT LIGHT WOULD NOT EXTINGUISH, LANDING GEAR EXTENDED WITH 3 GREENS WITH NO INTRANSIT LIGHT. MX REPLACED THE NLG UPLOCK SWITCH, OPS CHECK GOOD.
- [SDR GLBA20110525G](https://openairdocs.org/sdr/GLBA20110525G.md): Pump · worn · May 24, 2011 · N182YV · Beech 1900D · Fuel Boost Pump
  > PILOT REPORTED THAT THE RT FUEL PSI LOW LIGHT ILLUMINATED DURING FLIGHT, TURNED STANDBY PUMP ON AND LIGHT EXTINGUISHED. MX R & R THE RT LOW PRESS FUEL PUMP IAW BMM 23-10-00, LEAK AND OPS CK GOOD, PN 114-3890425 SN ON: B-952-019 SN OFF: B1448.
- [SDR GLBA20110524F](https://openairdocs.org/sdr/GLBA20110524F.md): Switch · out of rig · May 23, 2011 · N182YV · Beech 1900D · Door Warning System
  > PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED AT FLIGHT LEVEL 240, MAX DIFF WAS 4.7, MAX DIFF DIDN'T CHANGE. PUT ON MEL. MAINTENANCE FOUND THE PRESSURE LOCK SWITCH SLIGHTLY OUT OF RIG, RE-ADJESTED PRESSURE LOCK SWITCH IAW BMM 52-70-02, ALL CHECKS
- [SDR GLBA20110516G](https://openairdocs.org/sdr/GLBA20110516G.md): Placard · misinstalled · May 15, 2011 · N182YV · Beech 1900D · Placards and Markings
  > - SIG EVENT - PILOT REPORTED THAT THE EMERGENCY EXIT PLACARD IS AT THE WRONG SEAT. PLACARD IS IN 7C AND SHOULD BE IN 5C. MX INSTALLED THE PLACARD IN THE PROPER LOCATION.
- [SDR GLBA20110420J](https://openairdocs.org/sdr/GLBA20110420J.md): Frame · cracked · Apr 19, 2011 · N182YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 500 AND STRINGERS 4L & 5L CRACKED AT THE STRUT MOUNT UPPER IB NUTPLATE AREA,.65" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL RE
- [SDR GLBA20110420H](https://openairdocs.org/sdr/GLBA20110420H.md): Frame · cracked · Apr 19, 2011 · N182YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT FS 456 AND STRINGER 3L & 4L AT THE GAS STRUCT MOUNT UPPER IB NUTPLATE AREA,.25" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED
- [SDR GLBA20110420F](https://openairdocs.org/sdr/GLBA20110420F.md): Spar · cracked · Apr 19, 2011 · N182YV · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A CRACK RADIATING FROM THE DEICE TUBING HOLE IN THE HORIZONTAL STAB MAIN SPAR CENTER WEB,.3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I
- [SDR GLBA20110418F](https://openairdocs.org/sdr/GLBA20110418F.md): Frame · cracked · Apr 18, 2011 · N182YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME AT F.S. 456 AND STRINGER 9AR CRACKED.15" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-023. MATER
- [SDR GLBA20110418G](https://openairdocs.org/sdr/GLBA20110418G.md): Frame · cracked · Apr 18, 2011 · N182YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CRACKED.2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-025. MATERI
- [SDR GLBA201007121](https://openairdocs.org/sdr/GLBA201007121.md): Spline · stripped · Jul 12, 2010 · N182YV · Beech 1900D · Engine Fuel Pump
  > PILOT REPORTED THAT DURING TAKEOFF (CLIMB OUT) ENROUTE, NR 1 ENGINE FAILED & AUTOFEATHERED, ENGINE SHUTDOWN BY ITSELF, THE AIRCRAFT LANDED BACK AT FIELD WITHOUT INCIDENT. MX INSPECTED NR 1 ENGINE GAS GENERATOR FOR ROTATION, NO OBSTRUCTIONS IN THE INTAKE, CHECK
- [SDR GLBA20100628F](https://openairdocs.org/sdr/GLBA20100628F.md): Switch · dirty · Jun 27, 2010 · N182YV · Beech 1900D · Indicating/Recording System
  > SMOKE/SMELL - PILOTS REPORTED THAT WITH THE BATTERY ON, ALL OF THE ANNUNCIATORS REMAINED ILLUMINATED WITH A SLIGHT BURNING SMELL BEING NOTICED. MX REMOVED AND CLEANED THE MICRO SWITCHES ON THE PUSH TO TEST SWITCH. THE OPS CHECK WAS GOOD. REF MM 33-10-00.
- [SDR GLBA20100324F](https://openairdocs.org/sdr/GLBA20100324F.md): Skin · dented · Mar 23, 2010 · N182YV · Beech 1900D · Wing, Plate/Skin
  > MAJOR REPAIR - PILOTS REPORTED THAT A BIRD STRIKE OCCURRED ON SHORT FINAL ON THE LT WING, LT OTBD SECTION OF THE WING. BETWEEN WING SIDE 249.5 & WING SIDE 261.5. DENT IS APPROX 12" IN LENGTH AND APPROX.5" IN DEPTH.
- [SDR GLBA20100129F](https://openairdocs.org/sdr/GLBA20100129F.md): Skin · damaged · Jan 25, 2010 · N182YV · Beech 1900D · Elevator, Plate/Skin
  > COMPONENT REPAIR - DURING A LIGHTINING STRIKE INSP OF THE ACFT AN EXIT HOLE WAS FOUND ON THE LT ELEVATOR. THE ELEVATOR WAS REMOVED AND REPLACED. IAW MM 27-30-00. EXIT HOLE IS ON OTBD. T/E HOLE.75" WIDE X.5" DEEP. DETERMINATION THAT THE ELEVATOR REQUIRED A
- [SDR GLBA20091104H](https://openairdocs.org/sdr/GLBA20091104H.md): Skin · cracked · Nov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE SKIN AT F.S. 498.25 ABOVE STRINGER 10R. THE CRACK RADIATES THROUGH A RIVET HOLE. MAINTENANCE REPAIRED THE AFT FUSELAGE SKIN AT F.S. 498.25 AND COMPLIED WITH REQUIRED RII INSPECTI
- [SDR GLBA20091104J](https://openairdocs.org/sdr/GLBA20091104J.md): Frame · bent · Nov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, Frame
  > DURING ROUTINE SCHEDULED MAINTENANCE A FRAME WAS FOUND BENT AT F.S. 451 BETWEEN STRINGER 6R & 7R. DAMAGE FOUND UNDER PREVIOUS REPAIR TO FUSELAGE SKIN. MAINTENANCE REPLACED THE DAMAGED FRAME AND PERFORMED THE REQUIRED II INSPECTIONS AT F.S. 451 BETWEEN STRINGER
- [SDR GLBA20091104G](https://openairdocs.org/sdr/GLBA20091104G.md): Skin · cracked · Nov 4, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING ROUTINE SCHEDULED MAINTENANCE THE FUSELAGE SKIN WAS FOUND CRACKED AT F.S. 447 BETWEEN STRINGERS 6R AND 7R. CRACK LOCATED AT UPPER FORWARD CORNER OF A PREVIOUS REPAIR. CRACK IS APPROXIMATELY.5" IN LENGTH. MAINTENANCE REPAIRED THE SKIN AND PERFORMED THE
- [SDR GLBA20091030G](https://openairdocs.org/sdr/GLBA20091030G.md): Frame · bent · Oct 29, 2009 · N182YV · Beech 1900D · Fuselage Main, Frame
  > SCHEDULED MAINTENANCE A FUSELAGE FRAME WAS FOUND BENT AT FS 198.25 ON THE LEFT HAND SIDE OF THE FUSELAGE AT STRINGER 6L. MAINTENANCE REPAIRED THE FRAME AND PERFORMED THE REQUIRED RII INSPECTIONS AT FS 198.25 AT STRINGER 6L IAW EO 09-1900-53-025 REV.1. MATERIAL
- [SDR GLBA20091030J](https://openairdocs.org/sdr/GLBA20091030J.md): Frame · bent · Oct 29, 2009 · N182YV · Beech 1900D · Fuselage Main, Frame
  > DURING ROUTINE SCHEDULED MAINTENANCE STRINGER 6L WAS FOUND BENT JUST AFT OF FUSELAGE FRAME AT F.S. 198.25. MAINTENANCE REPAIRED STRINGER 6L AND PERFORMED THE REQUIRED RII INSPECTIONS AT F.S. 198.25 IAW EO 09-1900-53-026 R1. MATERIALS UTILIZED ARE INCLUDED IN T
- [SDR GLBA20091030L](https://openairdocs.org/sdr/GLBA20091030L.md): Angle · cracked · Oct 26, 2009 · N182YV · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING ROUTINE SCHEDULED MAINTENANCE A PREVIOUS REPAIR WAS FOUND CRACKED ON THE RIGHT HAND HEAVY ANGLE AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 1". MAINTENANCE REPAIRED THE RIGHT HAND HEAVY ANGLE AND PERFORMED THE REQUIRED RII INSPECTIONS IAW E.O. 09-1900-53
- [SDR GLBA20091030H](https://openairdocs.org/sdr/GLBA20091030H.md): Angle · cracked · Oct 26, 2009 · N182YV · Beech 1900D · Fuselage Miscellaneous Structure
  > DURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN BEND RADIUS AT F.S. 303.25 AFT OF FUSELAGE FRAME. CRACK LENGTH APPROXIMATELY 1". PREVIOUS REPAIR INSTALLED BETWEEN F.S. 288 & 303.25. MAINTENANCE REPAIRED THE HEAVY ANGLE AT F.S
- [SDR GLBA20090928G](https://openairdocs.org/sdr/GLBA20090928G.md): Skin · damaged · Sep 25, 2009 · N182YV · Beech 1900D · Elevator, Plate/Skin
  > UPON INSPECTION OF THE ACFT A LIGHTNING STRIKE WAS FOUND ON THE RT ELEVATOR TOP SKIN. MAINTENANCE REMOVED AND REPLACED THE ELEVATOR I.A.W. 27-30-00. MX REMOVED AND REPLACED THE ELEVATOR HOWEVER THE ELEVATOR WAS REPAIRED AND THE RII INSPECTIONS COMPLIED WITH IA
- [SDR GLBA2009](https://openairdocs.org/sdr/GLBA2009.md): Skin · cracked · Sep 9, 2009 · N182YV · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - WHILE PERFORMING OTHER MAINTENANCE RELATED TO AN ANTENNA REPLACEDMENT A RIVET HEAD WAS FOUND MISSING AND TWO SMALL CRACKS WERE FOUND THAT WERE APPROXIMATELY.2" IN LENGTH EMMANATING FROM RIVET HOLE ON THE TOP AT F.S. 150.6 TO RIGHT OF THE CENTER
- [SDR GLBA20090424F](https://openairdocs.org/sdr/GLBA20090424F.md): Skin · leaking · Apr 21, 2009 · N182YV · Beech 1900D · Wing, Plate/Skin
  > DURING SCHEDULED MX A FUEL LEAK WAS FOUND ON THE LT WING LE ON A PREVIOUS REPAIR FROM APPROX WS 239 TO WS 249.75. MX REPAIRED THE LT WING LE PREVIOUS REPAIR IAW EO-09-1900-57-004. ALL RII INSP REQUIREMENTS COMPLIED WITH IAW EO-09-1900-57-004.
- [SDR GLBA200903212](https://openairdocs.org/sdr/GLBA200903212.md): Actuator · worn · Mar 21, 2009 · N182YV · Beech 1900D · Landing Gear Actuator
  > PILOTS REPORTED THAT DURING GEAR EXTENSION THE LEFT MAIN GEAR WAS FLICKERING ON AND OFF AND REC IN TRANSIT LIGHTS WERE ILLUMINATED. THEY RECYCYLED THE LANDING GEAR AND STILL HAD NO GREEN LIGHTS ON THE LEFT MAIN GEAR. THEY PERFORMED A MANUAL GEAR EXTENSION AND
- [SDR BSAASDR0725](https://openairdocs.org/sdr/BSAASDR0725.md): Skin · torn · Oct 5, 2007 · N182YV · Beech 1900D · Trailing Edge Flaps
  > RIGHT FLAP HUMP MISSING LARGE SECTION OF SHEET METAL. FLAP WAS REMOVED AND REPLACED.
- [SDR BSAASDR0607](https://openairdocs.org/sdr/BSAASDR0607.md): Spar Cap · damaged · Feb 27, 2006 · N182YV · Beech 1900D · Wing Spar
  > PITTING CORROSION WAS FOUND ON THE RIGHT WING ON THE LOWER WING SPAR CAP IN THE THIRD ELEMENT SPAR STRAP JUST AFT OF THE WING DRAIN LOCATED JUST OUTBOARD OF THE NACELLE IN THE WING LEADING EDGE. THE DAMAGE AREA IS APPROXIMATELY.5 INCH WIDE AND WENT INTO THE
- [SDR 67971](https://openairdocs.org/sdr/67971.md): Annunciator · failed · Dec 26, 2004 · N182YV · Beech 1900D · Landing Gear Position and Warning
  > TAIL DE-ICE ANNUNCIATOR FAILED IN FLIGHT DURING ICING CONDITIONS, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED TAIL DE-ICE SENSOR AND SERVICED TUBES, OPS CHECK GOOD.
- [SDR 63594](https://openairdocs.org/sdr/63594.md): Fire Detector · malfunctioned · Aug 2, 2004 · N182YV · Beech 1900D · Fire Detection
  > ON TAKEOFF ROLL OUT, FLIGHT CREW OBSERVED LT ENGINE FIRE BOTTLE DISCHARGED ANNUN. ILLUMINATED. CREW ABORTED TAKE OFF AND RETURNED TO THE GATE WITH NO FURTHER INCIDENT. THE BOTTLE WAS SAID THAT IT WAS NOT DISCHARGED. REMOVED AND REPLACED 173 PC BOARD FIRE DET
- [SDR 58784](https://openairdocs.org/sdr/58784.md): Pressure Switch · inoperative · Feb 12, 2004 · N182YV · Beech 1900D · Ice Detection
  > AFTER DEPARTING FROM MSS. CREW CLIMBED THROUGH INCING CONDITIONS AND FOUND TAIL DE-ICE TO BE INOP. IN BOTH MODES. THEY DIVERTED TO DUJ. UNDER A DISPATCH DECLARED EMERGENCY AND LANDED SAFELY WITH NOT FURTHER INCIDENTS.CORRECTIVE ACTION THAT WAS TAKEN IS R&R'D T
- [SDR 58604](https://openairdocs.org/sdr/58604.md): Annunciator · false indication · Feb 5, 2004 · N182YV · Beech 1900D · Door Warning System
  > WHILE ON FLIGHT, PASSENGER DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CAPTAIN FOLLOWED PROCEDURES TO LAND AT AN ALTERNATE FIELD TRI. CREW INSPECTED DOOR AND FOUND ANNUNCIATOR GAVE FALSE ILLUMINATION. THIS ITEM WAS DEFERRED. THEN PROCEEDED TO FINAL DESTINA
- [SDR 54574](https://openairdocs.org/sdr/54574.md): Switch · out of adjust · Sep 20, 2003 · N182YV · Beech 1900D · Door Warning System
  > MASTER WARNING ILLUM WITH A CABIN DOOR ANNUNCIATOR. TAKEOFF WAS ABORTER AFT RETURNED TO GATE. ADJUSTED CABIN DOOR ANNUNCIATOR LIGHT SWITCH.
- [SDR AMWA33](https://openairdocs.org/sdr/AMWA33.md): Rib · cracked · Sep 7, 2003 · N182YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > RIB CRACKED AT CSS 69.184 AT STRG P/N 101-640000-46 RT AND STRG P/N 101-640000-45 LT SIDE (2EA CRACK AT THIS RIB).
- [SDR AMWA32](https://openairdocs.org/sdr/AMWA32.md): Rib · cracked · Sep 7, 2003 · N182YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > RIB AT CS 54.026 CRACKED AT STRG. P/N 101-640000-46 STRG P/N 101-640000-47 ON RT SIDE AND STRG P/N 101-640000-39 LT SIDE (3EA CRACKS ON THIS RIB).
- [SDR AMWA31](https://openairdocs.org/sdr/AMWA31.md): Rib · cracked · Sep 7, 2003 · N182YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-39, 1EA CRACK AT THIS RIB.
- [SDR AMWA8](https://openairdocs.org/sdr/AMWA8.md): Spar Cap · chafed · Feb 12, 2003 · N182YV · Beech 1900D · Wing Spar
  > UPON A DETAILED INSPECTION MAINTENANCE FOUND THE ELECTRIC LINE CHAFING ON RIGHT FORWARD WING SPAR IN THE WHEEL WELL. BLENDED LOWER WING SPAR CAP IN ACCORDANCE WITH RAYTHEON FIELD REPAIR. NO TEARDOWN REPORT IS REQUIRED.
- [SDR 97ZZZM968](https://openairdocs.org/sdr/97ZZZM968.md): Turbine · failed · Aug 9, 1997 · N182YV · Beech 1900D · Turbine Section
  > IN MCI, THE RIGHT ENGINE HAD A CONTAINED ENGINE FAILURE DURING START. REMOVED AND REPLACED RIGHT ENGINE GAS GENERATOR AND POWER SECTION. TEAR DOWN INSP REVEALED THE COMPRESSOR TURBINE CENTER BOLT AND KEY WASHER WAS NOT SUFFICIENTLY LUBRICATED AT INSTALLATION
- [SDR 97ZZZX4237](https://openairdocs.org/sdr/97ZZZX4237.md): Dovetail Blkhd · cracked · Jun 28, 1997 · N182YV · Beech 1900D · Trailing Edge Flaps
  > DURING BEECH TEMP. REV 5-6 FLAP INSPECTION, THE LEFT INBOARD FLAP DOVETAIL BULKHEAD WAS FOUND WITH A CRACK. STOP DRILLED AND INSTALLED DOUBLER IAW AMWA T.O. 1900-27-00-0001. (X)
- [SDR 97ZZZM977](https://openairdocs.org/sdr/97ZZZM977.md): Bracket · worn · Jun 28, 1997 · N182YV · Beech 1900D · Trailing Edge Flaps
  > AT ICT OVERNIGHT MAINTENANCE INSPECTION PER BEECH TEMP REV 5-6, FOUND LHOB FLAP. INBOARD ATTACH BRACKET WORN. REMOVED AND REPLACED ATTACH BRACKET IAW SRM 57-00 AND 51-40.
- [SDR 96ZZZM1243](https://openairdocs.org/sdr/96ZZZM1243.md): P3 Line · loose · Jul 17, 1996 · N182YV · Beech 1900D · Fuel Controlling System
  > FLT 5627 - AFTER TAKEOFF RIGHT ENGINE ROLLED BACK TORQUE AND THEN STABILIZED AT ABOUT 1000 FT/LBS OF TORQUE, AIRCRAFT. RETURNED TO FIELD AT MCI. MAINTENANCE TIGHTENED P3 LINE C/W FLIGHT TEST RETURNED AIRCRAFT TO SERVICE. (M)
- [SDR 96ZZZX1754](https://openairdocs.org/sdr/96ZZZX1754.md): Blade · split · Feb 18, 1996 · N182YV · Beech 1900D · Propeller Blade Section
  > DURING ROUTINE MAINTENANCE, THE TRAILING EDGE WAS FOUND SPLIT APROXIMATELY 1.5 INCHES. REPAIRED IAW HARTZELL MM AND FORM 8110-3.
- [SDR 96ZZZX1753](https://openairdocs.org/sdr/96ZZZX1753.md): Blade · split · Feb 10, 1996 · N182YV · Beech 1900D · Propeller Blade Section
  > DURING ROUTINE MAINTENANCE, PROPELLER BLADE, SN 1655, WAS FOUND TO HAVE A 4 INCH SPLIT ON TRAILING EDGE. REPAIRED IAW HARTZELL MM AND FORM 8110-3 FROM HARTZELL.

## 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 = 'N182YV' AND deregistration_id = 'N182YV-2012-03-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N182YV-2012-03-08/reports

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