# Service difficulty reports: N165YV

A list on [N165YV](https://openairdocs.org/aircraft/N165YV.md).

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

Page 1 of 2 · 60 reports

- [SDR GLBA2017083100683](https://openairdocs.org/sdr/GLBA2017083100683.md): Snubber · inoperative · Aug 29, 2017 · N165YV · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE CABIN DOOR FREE FALLS OPEN. REMOVED & REPLACED CABIN DOOR SNUBBER IAW MM 52-10-01. OPS CHECKED GOOD
- [SDR GLBA2017082800682](https://openairdocs.org/sdr/GLBA2017082800682.md): Rib · cracked · Aug 28, 2017 · N165YV · Beech 1900D · Elevator, Spar/Rib
  > MAJOR REPAIR - MAINTENANCE REPORTED THAT THE LEFT HAND ELEVATOR'S OUTBOARD MOUNT BRACKET IS LOOSE AND BOTH ATTACHING RIBS ARE CRACKED. RIVET HOLES ARE CRACKED ON MAIN SPAR WHERE RIBS ATTACH. ELEVATOR WAS REMOVED FOR INSPECTION ON 08/21/17. MAJOR REPAIR DETERMI
- [SDR GLBA2017053000663](https://openairdocs.org/sdr/GLBA2017053000663.md): Cable · bent · May 28, 2017 · N165YV · Beech 1900D · Passenger/Crew Doors
  > MAINTENANCE REPORTED THAT THE LOWER FORWARD AIRSTAIR DOOR CABLE ROD WAS BENT. REMOVED AND REPLACED THE LOWER FORWARD AIRSTAIR DOOR HANDRAIL CABLE IAW BMM 52-10-02, OPS CHECKED GOOD.
- [SDR GLBA2016082400606](https://openairdocs.org/sdr/GLBA2016082400606.md): Trim Panel · unsecure · Aug 23, 2016 · N165YV · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE AIRSTAIR DOOR AFT TRIM IS LOOSE AND BINGING THE DOOR, PREVENTING THE DOOR FROM OPENING. MAINTENANCE REPLACED THE NUTS AND SECURED THE TRIM PIECE, DOOR OPERATES NORMALLY.
- [SDR GLBA2015092900550](https://openairdocs.org/sdr/GLBA2015092900550.md): Clevis · bent · Sep 27, 2015 · N165YV · Beech 1900D · Passenger/Crew Doors
  > DURING A MX INSPECTION, FOUND THAT THE AIRSTAIR DOOR LOWER FWD HANDRAIL CABLE CLEVIS WAS BENT. R & R THE CABLE ASSEMBLY IAW BMM 52-10-02. PN ON & OFF 1440-43GLA.
- [SDR GLBA2015091600537](https://openairdocs.org/sdr/GLBA2015091600537.md): Tire · blown · Sep 15, 2015 · N165YV · Beech 1900D · Tire
  > THE NR 1 TIRE BLEW ON LANDING. THE TIRE DEVELOPED A FLAT SPOT DURING BRAKING THAT RESULTED IN LOSS OF TIRE PRESS. R & R THE NR 1 WHEEL ASSEMBLY IAW TC 1900-3240.00. PN 5006028-5, SN ON 1325, SN OFF 1681. OK FOR CONTINUED SERVICE.
- [SDR GLBA2015022700500](https://openairdocs.org/sdr/GLBA2015022700500.md): Master Cylinder · worn · Feb 26, 2015 · N165YV · Beech 1900D · Master Cylinder/Brake Valve
  > PILOT REPORTED THAT THE LT BRAKE WAS INOPERATIVE FROM THE CAPTAIN SEAT, EXTREMELY SOFT FROM THE FIRST OFFICER SEAT. REPLACED O RINGS ON THE SWIVEL FITTINGS ON THE NR 1 BRAKE. REPLACED THE CAPTAINS LT MASTER CYLINDER IAW BMM 32-40-06. OPERATIONS CHECK & LEAK
- [SDR GLBA2014120100474](https://openairdocs.org/sdr/GLBA2014120100474.md): Cam Lock · lack of lube · Nov 29, 2014 · N165YV · Beech 1900D · Passenger/Crew Doors
  > PILOT REPORTED THAT THE MAIN CABIN DOOR HANDLE IS VERY DIFFICULT TO MOVE WHEN THE DOOR IS BROUGHT TO THE CLOSED POSITION, HANDLE IN NORMAL FASHION WITH DOOR OPEN. LUBRICATED THE CAM LOCKS OPERATIONS CHECKED GOOD IAW BMM 12-20-00, OPERATIONS CHECKED GOOD.
- [SDR GLBA2014092200444](https://openairdocs.org/sdr/GLBA2014092200444.md): Skin · dented · Sep 22, 2014 · N165YV · Beech 1900D · Vertical Stabilizer, Plate/Skin
  > MAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND DENT IN THE VERT STAB LE, DENT AREA BEGINS AT CSS 54.026, JUST ABOVE RIB UPWARD TO CSS 66.00, DEPTH APPROX.5 INCHES TO.75 INCHES, ALLOWING FOR ORIGINAL CONTOUR AT LE. REPAIRED THE AFFECTED AREA &
- [SDR GLBA2014092200445](https://openairdocs.org/sdr/GLBA2014092200445.md): Structure · cracked · Sep 22, 2014 · N165YV · Beech 1900D · Vertical Stabilizer Miscellaneous Structure
  > DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT FWD VERT STAB HAT SECTION AT FWD FLANGE BEND RADIUS,.20% CHORD & VSS 90.0, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-009. MATERIA
- [SDR GLBA2014091900442](https://openairdocs.org/sdr/GLBA2014091900442.md): Rib · cracked · Sep 18, 2014 · N165YV · Beech 1900D · Wing, Rib/Bulkhead
  > MAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT WING INBD RIB AT JUNCTION WITH WING SPAR FS 288, RIB ANGLE DOUBLER CRACKED 1.1 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-190
- [SDR GLBA2014091900440](https://openairdocs.org/sdr/GLBA2014091900440.md): Frame · cracked · Sep 17, 2014 · N165YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE FUSELAGE FRAME CHANNEL AT FS 177.35 & STRINGER 13L IN THE FRAME FLANGE BEND RADIUS,.7 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 1
- [SDR GLBA2014091900441](https://openairdocs.org/sdr/GLBA2014091900441.md): Frame · cracked · Sep 17, 2014 · N165YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT FUSELAGE FRAME AT FS 177.35 & STRINGER 9AR RADIATING UPWARD FROM STRINGER 9AR CUT OUT,.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IA
- [SDR V0DR20140908002](https://openairdocs.org/sdr/V0DR20140908002.md): Wheel · cracked · Sep 8, 2014 · N165YV · Beech 1900D · Air Distribution Fan
  > RECEIVED VENT BLOWER IN FOR OVERHAUL. THE TECHNICIAN WAS REASSEMBLING THE VENT BLOWER, AFTER GETTING THE BLOWER ASSEMBLY TOGETHER HE PREPARED THE VENT BLOWER TO RUN IN THE BRUSHES. NOTED THAT WITH POWER APPLIED TO THE VENT BLOWER A NOISE, FAINT, WAS HEARD UP
- [SDR V0DR20140908001](https://openairdocs.org/sdr/V0DR20140908001.md): O-Ring · deteriorated · Sep 8, 2014 · N165YV · Beech 1900D · Propeller Hub Section
  > CUSTOMER REPORTED POSSIBLE OIL COMING FROM PROPELLER HUB & BLADE SOCKETS. RECEIVED PROPELLER ASSEMBLY IN, PRIOR TO DISASSEMBLY TECHNICIANS APPLIED PRESS FOR TROUBLESHOOTING PURPOSES, BUT NO DROP IN AIR PRESS WAS NOTED. THE TECHNICIANS PROCEEDED TO DISASSEMBL
- [SDR GLBA2013082300302](https://openairdocs.org/sdr/GLBA2013082300302.md): Handle · unsecure · Aug 22, 2013 · N165YV · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE OUTSIDE HANDLE ON OVERWING EXIT 4C DOES NOT STAY SECURE IN FLIGHT. MX RESECURED THE OUTSIDE DOOR HANDLE. OPS CHECK GOOD REF BMM 52-20-00-201. LATER THAT DAY MX REEXAMINED DURING SCHEDULED MX, NOTING THAT EMERGENCY EXIT 4C EXTERIOR HAND
- [SDR GLBA2013082300301](https://openairdocs.org/sdr/GLBA2013082300301.md): Handle · unsecure · Aug 22, 2013 · N165YV · Beech 1900D · Emergency Exits
  > PILOT REPORTED THE 4C OUTER HANDLE ON THE OVERWING EXIT IS POPPED. MX SECURED THE EMERGENCY EXIT OUTER HANDLE. OPS CHECKED GOOD REF BMM 52-20-00-201.
- [SDR GLBA2013062400264](https://openairdocs.org/sdr/GLBA2013062400264.md): Motor · odor · Jun 24, 2013 · N165YV · Beech 1900D · Trailing Edge Flap Control System
  > PILOT REPORTED THAT THEY SMELLED ELECTRICAL SMOKE IN THE AFT CABIN DURING SHUTDOWN. REPLACED THE FLAP MOTOR, SYS OPS CHECKED GOOD, NO BURNING ODOR NOTED.
- [SDR GLBA2012111400111](https://openairdocs.org/sdr/GLBA2012111400111.md): Bulkhead · gouged · Nov 13, 2012 · N165YV · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A GOUGE IN THE UPPER PRESSURE BULKHEAD AT FS 84.00 AT ANGLE ATTACH AREA ABOVE CENTER AVIONICS SHELF, TORN IN A TRIANGLE SHAPE 1.35",.8",.7". MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-069.
- [SDR GLBA2012111200106](https://openairdocs.org/sdr/GLBA2012111200106.md): Bulkhead · cracked · Nov 12, 2012 · N165YV · Beech 1900D · Fuselage Main, Bulkhead
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND SEVEN CRACKS IN THE RT FWD PRESSURE BULKHEAD AT FASTENERS, THE OTBD ROW TO DOUBLE ROW TO FASTENERS AT THE INBD EDGE OF BULKHEAD, 2.375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW EO 12-1900-53-068.
- [SDR GLBA2012051601](https://openairdocs.org/sdr/GLBA2012051601.md): Actuator · inoperative · May 15, 2012 · N165YV · Beech 1900D · Landing Gear Actuator
  > PILOT REPORTED LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL EXTENSION, DECLARED EMERGENCY, LANDED SAFELY. MX MEGGED WIRING FROM TB150 TO ALL ACTUATORS, HANDLE TO PCB A316 AND TO SERVO VALVE, ALL CHECKED GOOD, R & R RT ACTUATOR, IAW TC 1900-3230-10
- [SDR GLBA2012051401](https://openairdocs.org/sdr/GLBA2012051401.md): Actuator · inoperative · May 12, 2012 · N165YV · Beech 1900D · Landing Gear Actuator
  > PILOT REPORTED THAT THE LANDING GEAR FAILED TO EXTEND NORMALLY, PERFORMED MANUAL EXTENSION, DECLARED AN EMERGENCY, LANDED SAFELY. MX WAS ABLE TO DUPLICATE PROBLEM, REPLACED RT MLG ACTUATOR. REF TC 1900-3230.10, OPS CHECKED GOOD.
- [SDR GLBA2012051101](https://openairdocs.org/sdr/GLBA2012051101.md): Powerpack · malfunctioned · May 10, 2012 · N165YV · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOT REPORTED ON APPROACH, LANDING GEAR WOULD NOT EXTEND, DECLARED AN EMERGENCY, MANUALLY PUMPED GEAR DOWN, 3 GREENS, LANDED SAFELY. MX REPLACED THE HYD POWER PACK IAW BMM 32-30-04.
- [SDR GLBA2012050701](https://openairdocs.org/sdr/GLBA2012050701.md): Wire · damaged · May 4, 2012 · N165YV · Beech 1900D · Instrument System Wiring
  > PILOT REPORTED THAT WHEN THEY TURNED ON THE MASTER PANEL LIGHT SWITCH, NOTICED AN ELECTRICAL BURNING ODOR, NO SMOKE NOTED, TURNED SWITCH OFF, ODOR WENT AWAY. MX REPAIRED A WIRE ON THE PROPELLER AMP INDICATOR, NO ODOR NOTED.
- [SDR GLBA20110912G](https://openairdocs.org/sdr/GLBA20110912G.md): Annunciator · inoperative · Sep 11, 2011 · N165YV · Beech 1900D · Propeller Feathering/Reversing
  > PILOT REPORTED THAT THE AUTOFEATHER OFF ANNUNCIATOR DID NOT ILLUMINATE WITH THE PRESS-TO-TEST. MAINTENANCE REPLACED THE AUTOFEATHER ANNUNCIATOR, OPS CHECKED GOOD.
- [SDR GLBA20110805H](https://openairdocs.org/sdr/GLBA20110805H.md): Seal · out of position · Aug 4, 2011 · N165YV · Beech 1900D · Emergency Exits
  > PILOT REPORTED THAT THE EMERGENCY EXIT DOOR AT 4C MAKES A LOUD SOUND DURING FLIGHT. MX REMOVED 4C EMER EXIT DOOR AND FOUND TRIM SEAL MISPLACED, REPOSITIONED SEAL AND INSTALLED EXIT DOOR IAW BMM 52-20-00, PRESURIZED ACFT IAW BMM 21-30-00, NO DEFECTS NOTED.
- [SDR GLBA20110805G](https://openairdocs.org/sdr/GLBA20110805G.md): Bulb · inoperative · Aug 4, 2011 · N165YV · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE LIGHT IN THE AS DOOR WINDOW DOES NOT COME ON WHEN PUSHED. MX REPLACED THE BULB IAW BMM 33-20-01, OPS CHECKED GOOD.
- [SDR GLBA20110715F](https://openairdocs.org/sdr/GLBA20110715F.md): Oxygen Mask · stuck · Jul 13, 2011 · N165YV · Beech 1900D · Crew Oxygen System
  > PILOT REPORTED THAT WHEN SELECTING EMERGENCY POSITION ON THE CAPT'S O2 MASK, IT WILL NOT MOVE FROM NORMAL POSITION TO 100 PERCENT. MX REPLACED THE MASK PN: 359-62612 SN OFF 9444, SN ON 12065 IAW MM 35-10-00, OPS CK GOOD.
- [SDR GLBA20110706M](https://openairdocs.org/sdr/GLBA20110706M.md): Cable · worn · Jul 4, 2011 · N165YV · Beech 1900D · Passenger/Crew Doors
  > "SUP" - DURING A WALK-AROUND, THE PILOT FOUND THE FWD BOTTOM A/S DOOR CABLE ROD END BENT. MX R & R THE FWD BOTTOM A/S DOOR CABLE IAW BMM 52-10-02, PN: 1440-43GLA.
- [SDR GLBA20110706L](https://openairdocs.org/sdr/GLBA20110706L.md): Panel · loose · Jul 4, 2011 · N165YV · Beech 1900D · Emergency Exits
  > DURING AN INSPECTION, THE PILOT FOUND THE EMERGENCY EXIT INTERIOR PANEL LOOSE. MX RESECURED SPRINGS ON EMERGENCY EXIT INTERIOR PANEL BUTTON IAW BMM 52-20-00.
- [SDR GLBA20110630O](https://openairdocs.org/sdr/GLBA20110630O.md): Switch · false activation · Jun 30, 2011 · N165YV · Beech 1900D · Door Warning System
  > PILOT REPORTED THAT WHILE CLIMBING THROUGH 8,000 FT HAD A CABIN DOOR ANNUNCIATOR ILLUMINATE, NO EMERGENCY DECLARED, RETURN TO BASE. MX CHECKED CABIN DOOR SWITCHES FOR LOOSE CONNECTIONS, LUBRICATED. SWITCHES OPS CHECKED GOOD REF AIM 12-10-0, CHAP 12. REMOVED
- [SDR GLBA20110601F](https://openairdocs.org/sdr/GLBA20110601F.md): Skin · debonded · Jun 1, 2011 · N165YV · Beech 1900D · Passenger/Crew Doors
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE AS DOOR SKIN DEBONDED FROM FWD TO AFT EDGE FROM THE LWR EDGE, AREA OF 24" BY 6". MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-005
- [SDR GLBA20110601J](https://openairdocs.org/sdr/GLBA20110601J.md): Frame · cracked · Jun 1, 2011 · N165YV · Beech 1900D · Fuselage Main, Frame
  > DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND FRAME CRACK AT FS 164 & STRINGER 9AR AT THE STRINGER CUTOUT,.3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-038. MATERIALS UTILIZED ARE
- [SDR GLBA20110601G](https://openairdocs.org/sdr/GLBA20110601G.md): Frame · cracked · Jun 1, 2011 · N165YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE SKIN AT FS 150 & STRINGER 9AL AT THE LOWER SNUBBER MOUNT AND AS DOOR FUSELAGE FRAME CRACKED AT SNUBBER UP MOUNT NUTPLATE AREA, BOTH 1.3" IN LENGTH. MAINTENANCE REPAIRED THE A
- [SDR GLBA20110601H](https://openairdocs.org/sdr/GLBA20110601H.md): Frame · cracked · Jun 1, 2011 · N165YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE FRAME AT FS 456 AT STRINGER 10R CUTOUT, LWR INBD EDGE,.25" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-037. MATERIALS UTILIZED A
- [SDR GLBA20110405H](https://openairdocs.org/sdr/GLBA20110405H.md): Stringer · bent · Apr 5, 2011 · N165YV · Beech 1900D · Fuselage Main, Longeron/Stringer
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND STRINGER 12L BENT AT FS 47.5, STRINGER 12L BENT 5" FROM FS 47.5 GOING AFT ALONG STRINGER. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-19
- [SDR GLBA201006151](https://openairdocs.org/sdr/GLBA201006151.md): Unknown · odor · Jun 15, 2010 · N165YV · Beech 1900D · Air Distribution System
  > SIG EVENT - CREW AND PASSENGERS SMELT SMOKE FOR APPROX. 15 SECONDS DURING DESCENT INTO OLF, SMELL CLEARED AND NO FURTHER EVIDENCE OF FIRE, SWEPT CABIN, CARGO, AND COCKPIT WITH NO EVIDENCE OF FIRE. MAINTENANCE INSPECTED ENVIRONMENTAL SYSTEM, FOUND NO EVIDENCE O
- [SDR GLBA20090808A](https://openairdocs.org/sdr/GLBA20090808A.md): Autofeather Sys · malfunctioned · Aug 8, 2009 · N165YV · Beech 1900D · Propeller Feathering/Reversing
  > RT AUTOFEATHER ARM ANNUNCIATOR DID NOT ARM WHEN POWER APPLIED FOR TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE.
- [SDR GLBA20090410B](https://openairdocs.org/sdr/GLBA20090410B.md): Indicator · fluctuates · Apr 10, 2009 · N165YV · Beech 1900D · Engine BMEP/Torque Indicating
  > DURING FLIGHT NOTICED 2 PERCENT FLUCTUATION ON NR 1 N 1 GAUGE AND FLUCTUATIONS ON NR 1 TORQUE GAUGE CONTINUED UNTIL SHUTDOWN. MAINTENANCE R & R LT BETA BLOCK AND RIGGED BETA VALVE LOW PITCH STOP PER MM 76-10-00. MAINTENANCE ADDITIONALLY R & R TACH GENERATOR I
- [SDR GLBA20090304I](https://openairdocs.org/sdr/GLBA20090304I.md): Skin · dented · Mar 3, 2009 · N165YV · Beech 1900D · Wing, Plate/Skin
  > DURING ROUTINE SHEDULED MAINTENANCE THE LT WING, OUTBOARD LEADING EDGE WAS FOUND DENTED AND REQUIRES REPLACEMENT. REPAIRED LT LEADING EDGE SECTION FROM WS 223-271. WORK PERFORMED PER FR-CO-01895 REV.2. STEPS 1 -15, 16 LEAK CHECK OF AFFECTED AREAS PERFORME
- [SDR GLBA20090227F](https://openairdocs.org/sdr/GLBA20090227F.md): Fuel Tank · damaged · Feb 26, 2009 · N165YV · Beech 1900D · Fuel Storage
  > MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE DAMAGE ON THE LEFT AFT AUXILIARY FUEL TANK WALL WAS DISCOVERED. MAINTENANCE REMOVED AFT WALL OF THE LEFT HAND AUX FUEL TANK. FABRICATED NEW, ALODINED AND PRIMED. REINSTALLED AFT WALL PER EO 09-UE165-02.
- [SDR GLBA20090220A](https://openairdocs.org/sdr/GLBA20090220A.md): Skin · distorted · Feb 12, 2009 · N165YV · Beech 1900D · Wing, Plate/Skin
  > MAJOR REPAIR - LEFT HAND INBOARD WING UPPER AFT WING SKIN OUT OF CONTOUR AT STATIONS F.S. 301 W.S. 70.022" F.S. 311 W.S. 70.032", F.S. 319 W.S. 70.035" F.S. 329 W.S. 70.035". MAINTENANCE REPLACED LT UPPER INBOARD SKIN IAW E.O.-09-165-01.
- [SDR BSAASDR0710](https://openairdocs.org/sdr/BSAASDR0710.md): Bypass Valve · malfunctioned · Apr 30, 2007 · N165YV · Beech 1900D · Cabin Pressure Control System
  > INITIAL REPORT - DURING CLIMB, THE RIGHT ENVIR FAIL LIGHT CAME ON, CREW RETURNED TO STATION WITH NO FURTHER INCIDENT. INITIALLY DEFERRED PER MEL 21-4. THE PRECOOLER BYPASS VALVE AND THE PRESSURE REGULATOR VALVE WERE REMOVED AND REPLACED. SYSTEM OPERATIONAL
- [SDR BSAASDR0614](https://openairdocs.org/sdr/BSAASDR0614.md): Skin · corroded · Jun 6, 2006 · N165YV · Beech 1900D · Wing, Plate/Skin
  > LEVEL 1 SURFACE CORROSION WAS FOUND IN THE LEFT AND RIGHT WINGS IN THE AREA OF THE QUICK DRAINS OUTBOARD OF THE NACELLES AND FORWARD OF THE SPAR AT WS 125 TO 128. CORROSION WAS EVALUATED, DETERMINED TO BE LEVEL 1 SURFACE CORROSION, IT WAS CLEANED OFF, AND THE
- [SDR 69959](https://openairdocs.org/sdr/69959.md): Wire · damaged · Mar 25, 2005 · N165YV · Beech 1900D · Electrical Power System Wiring
  > CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT. FIRST OFFICER OBSERVED SMOKE FROM AVIONICS BAY AREA. ALL AIRCRAFT SYSTEMS WERE OPERATING NORMALLY. REMOVED AND REPLACED INVERTER. NR 1 INVERTER WIRING AT A226 PANEL BROKEN AND LOOSE CAUSING ARCING. REPAIRED
- [SDR 63379](https://openairdocs.org/sdr/63379.md): Hydraulic System · low · Jul 26, 2004 · N165YV · Beech 1900D · Hydraulic System, Main
  > RECEIVED CALL FROM CAPTAIN HIS LT BRAKE WAS BLEEDING OFF. THEN CALLED MAINTENANCE IN PIT. BLEED LT BRAKE AND SERVICED HYDRAULIC BRAKE GROUND CK GOOD. LEAK CK GOOD
- [SDR 63383](https://openairdocs.org/sdr/63383.md): Brake · low · Jul 26, 2004 · N165YV · Beech 1900D · Brake
  > RECEIVED CALL FROM CREW ABOUT BRAKES FEELING SPONGY. CALLED PIT MAINTENANCE. BLEED LT AND RT BRAKES. SERVICED BRAKE HYDRAULIC RESERVIOR LEAK CK GOOD.
- [SDR 60371](https://openairdocs.org/sdr/60371.md): Brake · malfunctioned · Apr 7, 2004 · N165YV · Beech 1900D · Landing Gear Brake System
  > CREW CALLED REPORTING BRAKES FELT SOFT. MAINTENANCE CALLED PIT.
- [SDR 58644](https://openairdocs.org/sdr/58644.md): Solenoid · worn · Feb 6, 2004 · N165YV · Beech 1900D · Auto Throttle System
  > AFTER ARRIVAL TO PIT ON FLIGHT 5528. RIGHT PROP WENT INTO GROUND FINE. CORRECTIVE ACTION TAKEN R/R LOW PITCH SOLENOID CLEVIS HARDWARE RIGGED.
- [SDR 58596](https://openairdocs.org/sdr/58596.md): Propeller · out of adjust · Feb 5, 2004 · N165YV · Beech 1900D · Propeller Controlling System
  > WHILE TAXIING IN ON FLIGHT 5433, THE RIGHT PROP STUCK IN LOW PITCH. THE AIRCRAFT ARRIVED AT THE GATE WITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE LOW PITCH. NO PARTS WERE USED.

Next page: https://openairdocs.org/aircraft/N165YV/reports.md?page=2

## 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 = 'N165YV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N165YV/reports

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