# Service difficulty reports: N178YV

A list on [N178YV](https://openairdocs.org/aircraft/N178YV.md).

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

- [SDR GLBA2013100800337](https://openairdocs.org/sdr/GLBA2013100800337.md): Skin · dented · Oct 5, 2013 · N178YV · Beech 1900D · Wing, Plate/Skin
  > DURING A SCHEDULED INSPECTION FOUND A DENT AFTER A BIRD STRIKE TO THE RIGHT WING AT WS 264.74 AND 283.74, 19" LONG X 1.75" DEEP. REPAIRED AREA IAW EO 13-1900-57-018. MAJOR REPAIR.
- [SDR GLBA2013021400176](https://openairdocs.org/sdr/GLBA2013021400176.md): Unknown · odor · Feb 13, 2013 · N178YV · Beech 1900D · Air Distribution System
  > PILOT REPORTED THAT THERE WAS A STRONG ELECTRICAL ODOR IN THE COCKPIT. MX INSPECTED ACFT DUCT SYS, RAN ACFT AND OPS CHECKED SYS WITH FLIGHT CREW, NO DEFECTS NOTED.
- [SDR GLBA2012112700118](https://openairdocs.org/sdr/GLBA2012112700118.md): Switch · failed · Nov 26, 2012 · N178YV · Beech 1900D · Emergency Lighting
  > PILOT REPORTED GLARE SHIELD EMERGENCY LIGHTS FAIL TO ILLUMINATE ON CAPTAIN`S SIDE. MAINTENANCE REPLACED THE SWITCH, OPS CHECKED GOOD.
- [SDR GLBA2012110100101](https://openairdocs.org/sdr/GLBA2012110100101.md): Skin · dented · Nov 1, 2012 · N178YV · Beech 1900D · Fuselage Main, Plate/Skin
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A DENT IN THE RT FUSELAGE LOCATED BETWEEN STRINGERS 10R AND 11R AT FS 228.25 AND 243.25 IN A AREA OF 6" BY 4.6", WITH A DEPTH OF.15". REPAIRED IAW EO 12-1900-53-063. MAJOR REPAIR
- [SDR GLBA2012103000095](https://openairdocs.org/sdr/GLBA2012103000095.md): Spar Cap · cracked · Oct 30, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT UPPER 2ND FASTENER HOLE, CRACK RADIATES UPWARD AND DOWNWARD AT THE OB EDGE OF FASTENER HOLE,.2 ICHES IN LENGTH. REPAIRED IAW EO 12-1900-55-052. MAJOR REPAIR
- [SDR GLBA2012103000094](https://openairdocs.org/sdr/GLBA2012103000094.md): Spar · misrepaired · Oct 30, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > - DURING A SCHEDULED ROUTINE INSP FOUND THAT THE HORIZONTAL STAB FWD SPAR WEB MISREPAIRED. REPAIRED IAW EO 12-1900-55-053. MAJOR REPAIR
- [SDR GLBA2012103000097](https://openairdocs.org/sdr/GLBA2012103000097.md): Spar Cap · cracked · Oct 30, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT THE UPPER FASTENER HOLE AT VSS 84.10, 20 PERCENT, CRACK RADIATES DOWNWARD & OTBD FROM FASTENER HOLE,.15 INCHES IN LENGTH. REPAIRED IAW EO 12-1900-55-054. MAJO
- [SDR GLBA2012102900092](https://openairdocs.org/sdr/GLBA2012102900092.md): Structure · cracked · Oct 29, 2012 · N178YV · Beech 1900D · Fuselage Main, Structure
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK AT FS 451 AND STRINGER 10R IN THE BEND RADIUS PROTRUDING UPWARD,.5" IN LENGTH. REPAIRED IAW EO 12-190 0-53-059.
- [SDR GLBA2012102900091](https://openairdocs.org/sdr/GLBA2012102900091.md): Structure · cracked · Oct 29, 2012 · N178YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP FOUND CRACK AT A PREVIOUS REPAIR AT FS 163.97 AND STRINGER 9AR FRAME PROTRUDING OUT OF A STOP DRILL,.25" IN LENGTH. REPAIRED IAW EO 12-1900-53-060.
- [SDR GLBA2012072500019](https://openairdocs.org/sdr/GLBA2012072500019.md): Fuse · inoperative · Jul 24, 2012 · N178YV · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED THE SYS FUSE, OPS CHECKED GOOD.
- [SDR GLBA201206112](https://openairdocs.org/sdr/GLBA201206112.md): Actuator · failed · Jun 8, 2012 · N178YV · Beech 1900D · Landing Gear Actuator
  > CREW TRIED TO EXTENDED THE GEAR NORMALLY BUT THE GEAR FAILED TO EXTEND. CREW RAN CHECKLIST AND EXTENDED THE GEAR MANUALLY. AFTER MANUAL EXTENSION THERE WERE NO ABNORMAL INDICATIONS NOTED. MX R & R RT MAIN LANDING GEAR ACTUATOR IAW TC 1900-3230.10, REV 1. OP
- [SDR GLBA2012040501](https://openairdocs.org/sdr/GLBA2012040501.md): Spar · cracked · Apr 5, 2012 · N178YV · Beech 1900D · Horizontal Stabilizer, Spar/Rib
  > MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, FOUND A SMALL CRACK ON THE HORIZONTAL STAB AFT SPAR CENTER WEB AT 2-OCLOCK POSITION AS VIEWED FROM REAR,.125" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW FR EO 02
- [SDR GLBA20120103F](https://openairdocs.org/sdr/GLBA20120103F.md): Seat Track · worn · Jan 2, 2012 · N178YV · Beech 1900D · Fuselage, Seat/Cargo Attach Fittings
  > MAJOR REPAIR - SEAT TRACK AT FS 423 AND WL 95, CORNER WORN.05",.12" ON LT SIDEWALL. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 12-1900-53-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
- [SDR GLBA201109072](https://openairdocs.org/sdr/GLBA201109072.md): Lamp · burned out · Sep 6, 2011 · N178YV · Beech 1900D · Emergency Lighting
  > INSTRUMENT EMERGENCY LIGHT ON CAPTAIN'S SIDE BURNED OUT. MX REPLACED THE BULB IAW BMM 33-10-04, OPS CHECKED GOOD.
- [SDR GLBA20110907F](https://openairdocs.org/sdr/GLBA20110907F.md): Bulb · inoperative · Sep 6, 2011 · N178YV · Beech 1900D · Emergency Lighting
  > PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT ON THE CA'S SIDE BURNED OUT. MX REPLACED THE BULB PN: 1864, IAW BMM 33-10-04, OPS CK GOOD.
- [SDR GLBA20110831G](https://openairdocs.org/sdr/GLBA20110831G.md): Unknown · smoke · Aug 29, 2011 · N178YV · Beech 1900D · Instrument Panel
  > PILOT REPORTED THAT SMOKE WAS COMING FROM UNDER THE GLARESHIELD. MX RAN ENGINES, WS HEAT, AND BLEEDS, NO SMOKE NOTED AT THIS TIME.
- [SDR GLBA201104141](https://openairdocs.org/sdr/GLBA201104141.md): Unknown · odor · Apr 14, 2011 · N178YV · Beech 1900D · Air Distribution System
  > PASSENGERS REPORTED A STRONG FUELD SMELL IN THE BACK OF THE AIRCRAFT. MAINTENANCE RAN BOTH ENGINES AND INSPECTED FOR FUEL LEAKS AND ODORS INSIDE IN THE AIRCRAFT, COULD NOT DUPLICATE ANY ODORS OR LEAKS, OK FOR SERVICE.
- [SDR GLBA20110215F](https://openairdocs.org/sdr/GLBA20110215F.md): Structure · cracked · Feb 15, 2011 · N178YV · Beech 1900D · Vertical Stabilizer Miscellaneous Structure
  > DURING A SCHEDULED ROUNTINE INSP MX, FOUND THE RT STABILON HAS A.5" HOLE 9" FROM T/E CORNER, CRACK RADIATED FROM INBD EDGE OF HOLE 1" IN LENGTH. MAINTENANCE COULD NOT REPAIR RT STABILON, REPLACED RT STABILON IAW BMM 55-10-01-201, NO RII REQUIRED FOR INSTALLA
- [SDR GLBA20101215F](https://openairdocs.org/sdr/GLBA20101215F.md): Skin · cracked · Dec 15, 2010 · N178YV · Beech 1900D · Emergency Exits
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A CRACK IN THE INNER SKIN OF THE 6A EMERGENCY EXIT DOOR LOWER FWD CORNER,.7" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-52-007. MATERIALS UTIL
- [SDR GLBA20101213F](https://openairdocs.org/sdr/GLBA20101213F.md): Skin · cracked · Dec 13, 2010 · N178YV · Beech 1900D · Fuselage Main, Plate/Skin
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE DOME SKIN AT FS 150 AND RT OF STRINGER NR 1,.75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-063. MATERIALS UTILIZ
- [SDR GLBA20101213G](https://openairdocs.org/sdr/GLBA20101213G.md): Frame · cracked · Dec 13, 2010 · N178YV · Beech 1900D · Fuselage Main, Frame
  > MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A CRACK IN THE RT FUSELAGE FRAME AT FS 456 & STR 10R AT THE STRINGER CUTOUT,.3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 10-1900-53-062.
- [SDR GLBA200909011](https://openairdocs.org/sdr/GLBA200909011.md): Landing Gear · malfunctioned · Sep 1, 2009 · N178YV · Beech 1900D · Landing Gear Retraction/Extension System
  > PILOTS REPORTED THEY HEARD LOUD MOTOR NOISE ON AND OFF. CONSISTENTLY WITH THE MOTOR NOISE THEY NOTICED THE DC LOAD WOULD GAIN 10-20 PERCENT. AFTER SEVERAL MIN OF THE THIS THEY NOTICED THE GEAR HANDLE IN TRANSIT LIGHT ILLUMINATED. IT EXTINGUISHED SHORTLY AFT
- [SDR GLBA20090821A](https://openairdocs.org/sdr/GLBA20090821A.md): Power Cable · out of rig · Aug 21, 2009 · N178YV · Beech 1900D · Power Lever
  > AIR RETURN, DUE TO UNAVAILABILITY OF PWR ON THE NR 2 ENG. PILOTS REPORTED THAT AN AIR RETURN OCCURRED DUE TO THE UNAVAILABILITY OF PWR ON NR 2 ENG. MX RIGGED RT ENG PWR CABLE ROD END IAW. OPS CHECK WAS GOOD. RII INSP COMPLIED IAW TASKCARD 4.3.13 AND WAS FOU
- [SDR GLBA20090605G](https://openairdocs.org/sdr/GLBA20090605G.md): Skin · cracked · Jun 4, 2009 · N178YV · Beech 1900D · Rudder, Plate/Skin
  > MAJOR REPAIR, DURING ROUTINE MX A CRACK WAS FOUND ON THE RUDDER TRIM ROD CUT OUT. APPROX RUDDER STA CSS 31.20. CRACK APPROX.375 INCH LONG. MX REMOVED DAMAGED AND REPAIRED THE AFFECTED AREA IAW EO-09-1900-27-001. RII INSPECTIONS COMPLIED WITH AND RUDDER BALAN
- [SDR GUU2008F00035](https://openairdocs.org/sdr/GUU2008F00035.md): Brake · weak · Aug 4, 2008 · N178YV · Beech 1900D · Landing Gear Brake System
  > FLIGHT 9148 MHH/FLL. PILOT REPORTED FIRST OFFICER LT RUDDER PEDAL GOES TO THE FLOOR WHEN DEPRESSED AND NO BRAKES. BACK BLED BRAKE SYSTEM. OPERATIONAL CHECK NORMAL. (S)
- [SDR GUUA05110804](https://openairdocs.org/sdr/GUUA05110804.md): Hinge Bracket · corroded · May 11, 2008 · N178YV · Beech 1900D · Elevator Miscellaneous Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED RT CTR ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED RT CTR ELEVATOR HINGE BRACKET.
- [SDR GUUA05110803](https://openairdocs.org/sdr/GUUA05110803.md): Hinge Bracket · corroded · May 11, 2008 · N178YV · Beech 1900D · Elevator Miscellaneous Structure
  > DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT OB ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED LT OB ELEVATOR HINGE BRACKET.
- [SDR GUUA11090703](https://openairdocs.org/sdr/GUUA11090703.md): Brake · weak · Nov 9, 2007 · N178YV · Beech 1900D · Landing Gear Brake System
  > FLIGHT: 9171 MHH/MIA, DURING TAXI LT BRAKE WILL NOT STOP AIRCRAFT WHEN FULLY DEPRESSED. INSPECTED UNDER FLOOR FOR LEAKS. BLED LT BRAKE ASSEMBLIES. OPEARATIONAL CHECK GOOD.
- [SDR GUUA11090702](https://openairdocs.org/sdr/GUUA11090702.md): Brake · weak · Nov 9, 2007 · N178YV · Beech 1900D · Landing Gear Brake System
  > FLIGHT: 9180 FPO/MIA, DURING TAXI LT BRAKE WILL NOT STOP AIRCRAFT WHEN DEPRESSED FULLY. PERFORMED LT BRAKE BLEEDING. OPERATIONAL CHECK GOOD.
- [SDR GUUA12150601](https://openairdocs.org/sdr/GUUA12150601.md): Unknown · smoke · Dec 15, 2006 · N178YV · Beech 1900D · Air Distribution System
  > FLIGHT:9279 PBI/NAS AFTER TAKEOFF ODOR OF SMOKE IN THE COCKPIT AND CABIN. RETURNED TO PBI LANDED WITHOUT INCIDENT. RAN AIRCRAFT WITH ALL EQUIPMENT ON NO SIGN OF SMOKE ODOR NOTED. TEST FLIGHT SATISFACTORY.
- [SDR GUUA05020601](https://openairdocs.org/sdr/GUUA05020601.md): Transfer Tube · leaking · May 2, 2006 · N178YV · Beech 1900D · Engine Fuel Distribution
  > FLIGHT: 9259 FLL/MHH DURING FLIGHT SMELL OF FUEL IN THE COCKPIT. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED RT ENGINE FUEL NOZZLE TRANSFER TUBES AT THE THREE O CLOCK POSITION.
- [SDR GUU2005F00007](https://openairdocs.org/sdr/GUU2005F00007.md): Gasket · leaking · Mar 9, 2005 · N178YV · Beech 1900D · Turbine Engine Oil System
  > DURING FLIGHT, RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. SECURED THE RT ENGINE. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT ENGINE OVERSPEED GOVERNOR GASKET. OPS LEAK CHECK NORMAL. (K)
- [SDR 60419](https://openairdocs.org/sdr/60419.md): Downlock Switch · dirty · Apr 8, 2004 · N178YV · Beech 1900D · Landing Gear Position and Warning
  > ON LANDING APPROACH IN EYW. AIRCRAFT LOST ALL INDICATION ON POSITION OF RT LANDING GEAR. CREW ABORTED LANDING. CYCLED GEAR AND GOT THREE DOWN AND LOCKED INDICATION. LANDED SAFELY WITH NO FURTHER INCIDENT. CLEANED DOWNLOCK SWITCHES. JACKED AIRCRAFT AND PERFORM
- [SDR 58728](https://openairdocs.org/sdr/58728.md): Switch · stuck · Feb 10, 2004 · N178YV · Beech 1900D · Trailing Edge Flap Control System
  > AFTER TAKEOFF FLAPS STUCK AT A PLACE IN BETWEEN 17 DEGREES & 34 DEGREES. CREW THEN DECIDED TO RETURN TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENTS. CLEANED LT / RT SPLIT FLAP SWITCHES OPS CK NORMAL.
- [SDR AMWA24](https://openairdocs.org/sdr/AMWA24.md): Rib · cracked · Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.
- [SDR AMWA23](https://openairdocs.org/sdr/AMWA23.md): Rib · cracked · Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.
- [SDR AMWA22](https://openairdocs.org/sdr/AMWA22.md): Rib · cracked · Aug 18, 2003 · N178YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL MANUAL P/N 114-590021-9, 51-70-03.
- [SDR 2002F00231](https://openairdocs.org/sdr/2002F00231.md): Warning Horn · false activation · Dec 22, 2001 · N178YV · Beech 1900D · Stall Warning System
  > ON DECEMBER 22, 2001, THE STALL WARNING HORN SOUNDED IMMEDIATELY AFTER TAKEOFF. THE PILOT REPORTED THAT THE HORN WOULD NOT SILENCE, AND THEN RETURNED THE AIRCRAFT TO ICT WITHOUT ANY FURTHER INCIDENT. MAINTNANCE CORRECTED THE PROBLEM, AND RETURNED TO THE AIRC
- [SDR 97ZZZM1087](https://openairdocs.org/sdr/97ZZZM1087.md): Fuel Control · worn · Sep 28, 1997 · N178YV · Beech 1900D · Fuel Control/Turbine Engines
  > FLT CREW IN ICT REPORTED LEFT ENGINE RESPONDING SLOW TO POWER LEVER INPUT. MAINTENANCE IN ICT INSPECTED AND FOUND THE FUEL CONTROL UNIT CONTROL ARM ASSEMBLY WORN. MAINTENANCE REPLACED FUEL CONTROL UNIT IAW EMM 72-00 AND MM 76-00 AND RETURNED TO THE AIRCRAFT
- [SDR 97ZZZX4244](https://openairdocs.org/sdr/97ZZZX4244.md): Skin · cracked · Sep 2, 1997 · N178YV · Beech 1900D · Trailing Edge Flaps
  > DURING DETAIL NR 1 WING INSPECTION, FOUND RIGHT OUTBOARD FLAP SKIN HAS A.25 INCH CRACK. STOP-DRILLED CRACK. PATCHED OVER CRACK USING FLAP STOCK, THREE ORIGINAL RIVETS, AND FOUR ADDITIONAL RIVETS IAW T.O. 1900-27-00-0001. (X)
- [SDR 97ZZZX4236](https://openairdocs.org/sdr/97ZZZX4236.md): Dovetail Blkhd · cracked · Jul 17, 1997 · N178YV · Beech 1900D · Trailing Edge Flaps
  > DURING BEECH TEMP. REV. 5-6 INSPECTION, FOUND 1 INCH CRACK AT LEFT INBOARD FLAP. DOVE TAIL BULKHEAD UPPER ROW. REPAIRED IAW T.O. 1900-27-00-0001. (X)
- [SDR 97ZZZM961](https://openairdocs.org/sdr/97ZZZM961.md): Skin · cracked · Jul 13, 1997 · N178YV · Beech 1900D · Trailing Edge Flaps
  > AT ICT, OVERNIGHT MAINTENANCE INSPECTION FOUND A 1 INCH CRACK IN LEFT OUTBOARD FLAP APPROX 31 INCHES FROM OUTBOARD EDGE OF FLAP STOP. DRILLED CRACK USING A SIZE.09375 DRILL BIT. FABRICATED AND INSTALLED A 2.5 INCH BY 2.5 PATCH USING FLAP SKIN STOCK IAW BEEC
- [SDR 97ZZZX4239](https://openairdocs.org/sdr/97ZZZX4239.md): Brackets · worn · Jul 2, 1997 · N178YV · Beech 1900D · Trailing Edge Flaps
  > DURING BEECH TEMP. REV. 5-6 INSPECTION, FOUND INBOARD AND OUTBOARD ATTACHING BRACKETS AT INBOARD ATTACHING POINT WORN. REMOVED AND REPLACED BRACKETS AND RE-ASSEMBLED IAW SRM 57-00. (X)
- [SDR 97ZZZM965](https://openairdocs.org/sdr/97ZZZM965.md): Skin · cracked · Jun 30, 1997 · N178YV · Beech 1900D · Trailing Edge Flaps
  > DURING BEECH TEMP REV INSPECTION, FOUND CRACK APPROX 1 INCH LONG ON FLAP LEADING EDGE. REPAIRED CRACKED IAW AMWA TO 1900-27-00-0001.
- [SDR 97ZZZM246](https://openairdocs.org/sdr/97ZZZM246.md): Ice Vane · missing rivet · Jan 16, 1997 · N178YV · Beech 1900D · Air Intake Anti/De-Ice System
  > DURING AN ROUTINE INSPECTION, A RIVET IN THE ICE VANE WAS FOUND MISSING. INSPECTION OF THE COMPRESSOR REVEALED THE BLIND RIVET WENT THOUGH THE ENGINE. THE GAS GEN WAS REPLACED DUE TO FOD. (M)
- [SDR 96ZZZM381](https://openairdocs.org/sdr/96ZZZM381.md): Ice Vane · cracked · Dec 19, 1995 · N178YV · Beech 1900D · Air Intake Anti/De-Ice System
  > DURING ROUTINE MAINTENANCE, THE RIGHT FIXED ICE VALVE WAS FOUND TO TO HAVE SEVERAL CRACKS.
- [SDR 96ZZZX128](https://openairdocs.org/sdr/96ZZZX128.md): Windshield · cracked · Nov 14, 1995 · N178YV · Beech 1900D · Flight Compartment Windows
  > CAPTAIN'S WINDSHIELD CRACKED ALONG THE OUTBOARD EDGE OF WINDSHIELD APPROXIMATELY 14 INCHES LONG. REMOVED AND REPLACED WINDSHIELD. AIRCRAFT HAD 74 FLIGHT HOURS AND 119 CYCLES SINCE NEW FROM BEECHCRAFT.

## 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 = 'N178YV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N178YV/reports

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