# Service difficulty reports: N163YV, cancelled Jun 9, 2010

A list on [N163YV, cancelled Jun 9, 2010](https://openairdocs.org/deregistered/N163YV-2010-06-09.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 · 51 reports

- [SDR AMWA88898](https://openairdocs.org/sdr/AMWA88898.md): Master Cylinder · weak · Dec 3, 2007 · N163YV · Beech 1900D · Master Cylinder/Brake Valve
  > DURING TAXI INTO GATE, THE PILOT'S LT BRAKE PEDAL LOST PRESSURE. PRESSURE WAS REGAINED AFTER PUMPING PEDAL. MAINTENANCE BLED BRAKES AND CLEARED DISCREPANCY.
- [SDR AMWA88571](https://openairdocs.org/sdr/AMWA88571.md): Brake · weak · Nov 13, 2007 · N163YV · Beech 1900D · Brake
  > AFTER LANDING THE CAPTAIN REPORTED THAT THE LT BRAKE WAS SPONGY AND MUSHY. REPLACED NR 1 AND NR 2 BRAKE ASSEMBLIES AND CLEARED DISCREPANCY.
- [SDR AMWA88211](https://openairdocs.org/sdr/AMWA88211.md): Annunciator · false indication · Oct 26, 2007 · N163YV · Beech 1900D · Door Warning System
  > CABIN DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. AIRCRAFT LANDED AND MAINTENANCE VERIFIED DOOR WAS SECURED AND PROBLEM WAS A FAULTY ANNUNCIATOR. ANNUNCIATOR PLACED IN DEFERRED STATUS. REMAINS DEFERRED AS OF 10/29/07.
- [SDR AMWA86756BC](https://openairdocs.org/sdr/AMWA86756BC.md): Battery · false activation · Aug 17, 2007 · N163YV · Beech 1900D · Battery/Charger System
  > BATTERY CHARGE ANNUNCIATOR ILLUMINATED WHEN GEAR WAS EXTENDED AND THEN EXTINGUISHED. AC LANDED WITH NO FURTHER INCIDENT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS A NUISANCE WRITEUP AND DISTRACTION TO THE CREW. COULD NOT DUPLICATE ON GROUND, OPS CHECKS NOR
- [SDR AMWA86499](https://openairdocs.org/sdr/AMWA86499.md): Rod · broken · Aug 7, 2007 · N163YV · Beech 1900D · Rudder Control System
  > ON APPROACH TO GRI, CAPT PEDALS LOST RUDDER CONTROL. CAPT TRANSFERRED CONTROL OF THE ACFT TO THE FO. FO PEDALS HAD RUDDER CONTROL. FO LANDED WITH NO FURTHER INCIDENT. OCCURENCE REPORT FILED. REMOVED AND REPLACED RUDDER INTERCONNECT ROD (ROD END), RIGGED R
- [SDR AMWA06032E](https://openairdocs.org/sdr/AMWA06032E.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032D](https://openairdocs.org/sdr/AMWA06032D.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032C](https://openairdocs.org/sdr/AMWA06032C.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032U](https://openairdocs.org/sdr/AMWA06032U.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032H](https://openairdocs.org/sdr/AMWA06032H.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032G](https://openairdocs.org/sdr/AMWA06032G.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING INC. REPORT 6799-1 REV 1R.
- [SDR AMWA06032B](https://openairdocs.org/sdr/AMWA06032B.md): Structure · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Nacelle/Pylon, Main Frame
  > FRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 6799-2 REV 1R.
- [SDR AMWA06032A](https://openairdocs.org/sdr/AMWA06032A.md): Structure · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Nacelle/Pylon, Main Frame
  > FRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 6799-2 REV 1R.
- [SDR AMWA06032V](https://openairdocs.org/sdr/AMWA06032V.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032T](https://openairdocs.org/sdr/AMWA06032T.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032S](https://openairdocs.org/sdr/AMWA06032S.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032R](https://openairdocs.org/sdr/AMWA06032R.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032M](https://openairdocs.org/sdr/AMWA06032M.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032Q](https://openairdocs.org/sdr/AMWA06032Q.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032P](https://openairdocs.org/sdr/AMWA06032P.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032O](https://openairdocs.org/sdr/AMWA06032O.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032N](https://openairdocs.org/sdr/AMWA06032N.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032L](https://openairdocs.org/sdr/AMWA06032L.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032K](https://openairdocs.org/sdr/AMWA06032K.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032J](https://openairdocs.org/sdr/AMWA06032J.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032F](https://openairdocs.org/sdr/AMWA06032F.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06032I](https://openairdocs.org/sdr/AMWA06032I.md): Frame · chafed · Jul 25, 2007 · N163YV · Beech 1900D · Fuselage Main, Frame
  > FUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.
- [SDR AMWA06002](https://openairdocs.org/sdr/AMWA06002.md): Spar Cap · corroded · Jul 24, 2007 · N163YV · Beech 1900D · Wing Spar
  > BIO CORROSION LT SPAR, ALT SPAR FLANGE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW ENGINEERING REPORT 6799-3 REV 1R.
- [SDR AMWA84592](https://openairdocs.org/sdr/AMWA84592.md): Brake · binding · May 11, 2007 · N163YV · Beech 1900D · Landing Gear Brake System
  > DURING ROLLING TAKEOFF, CAPT HAD EXCESSIVE BRAKE DRAG AND ABORTED TAKEOFF. RETURNED TO GATE W/O FURTHER INCIDENT. ADJUSTED PARKING BRAKE HANDLE AND VALVES.
- [SDR AMW1070010901](https://openairdocs.org/sdr/AMW1070010901.md): Skin Panel · cracked · Jan 8, 2007 · N163YV · Beech 1900D · Fuselage Main, Plate/Skin
  > DISCOVERED DURING MAINTENANCE INSPECTION FOR PRESSURIZATION PROBLEM. MAINTENANCE FOUND THE FUSELAGE SKIN TO BE CRACKED ALONG THE RT SIDE OF THE NR 1 COMM ANTENNA. THE CRACK WAS 7 IN LONG, EXTENDING FROM APPROX FS 213.00 TO FS 220.750 RUNNING PARALLEL TO THE A
- [SDR AMWA078434](https://openairdocs.org/sdr/AMWA078434.md): Actuator · worn · Jul 14, 2006 · N163YV · Beech 1900D · Landing Gear Actuator
  > UPON GEAR EXTENSION CREW OBSERVED THE GEAR TRANSIT LIGHT WOULD NOT GO OUT. CREW ACCOMPLISHED REQUIRED PROCEDURES AND LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE WAS CALLED AND REMOVED AND REPLACED LT. MAIN GEAR ACTUATOR, THE (CR110) DIODE, LOWER LEGEN
- [SDR 71813](https://openairdocs.org/sdr/71813.md): Brake Assy · malfunctioned · Jul 17, 2005 · N163YV · Beech 1900D · Landing Gear Brake System
  > UPON TAXI INTO DUJ, CREW EXPERIENCED RIGHT BRAKE SPONGY. PARKED AND CHOCKED AIRCRAFT WITH NO FURTHER INCIDENT. MAINTENANCE BLED BRAKES. THEREFORE THERE WERE NO PARTS USED.
- [SDR 70891](https://openairdocs.org/sdr/70891.md): Connector · dirty · May 18, 2005 · N163YV · Beech 1900D · Propeller Governor
  > RT PROP WILL ONLY MAKE 1550 UNDER POWER. MAINTENANCE CLEANED OVERSPEED GOVERNOR CONNECTOR PLUG. THEREFORE NO PARTS WERE USED.
- [SDR 69476](https://openairdocs.org/sdr/69476.md): Brake · malfunctioned · Mar 2, 2005 · N163YV · Beech 1900D · Landing Gear Brake System
  > AFTER TAXI OUT LEFT BRAKE WILL NOT RELEASE. PASSENGERS DEPLANED ON TAXIWAY. MTC DETERMINED PARKING BRAKE WAS NOT RELEASING COMPLETELY. A/C RETURNED TO GATE AND PARKING BRAKE DEFERRED PER MEL 32-7. A/C RETURNED TO SERVICE. INSTALLED PARKING BRAKE KNOB.
- [SDR 67556](https://openairdocs.org/sdr/67556.md): Brake Assy · weak · Dec 12, 2004 · N163YV · Beech 1900D · Brake
  > CREW EXPERIENCED WEAK BRAKING ACTION ON RIGHT SIDE ON TAXI IN WITH NO FURTHER INCIDENT. BLED BRAKES.
- [SDR 60212](https://openairdocs.org/sdr/60212.md): Door · stuck · Apr 1, 2004 · N163YV · Beech 1900D · Passenger/Crew Doors
  > UPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THRU THE EMERGENCY EXIT AT 6A. REMOVED & REINSTALLED EMERGENCY EX/DOOR
- [SDR 60211](https://openairdocs.org/sdr/60211.md): Cable · damaged · Apr 1, 2004 · N163YV · Beech 1900D · Passenger/Crew Doors
  > UPON DEPLANING IN DDC CREW COULD NOT GET PAX DOOR TO OPEN AFTER SEVERAL ATTEMPS. PASSENGERS WERE UNLOADED THUR EMERGENCY EXIT AT SEAT 6A ALL WERE DEPLANED WITH NO FURTHER INCIDENT. REINSTALLED PASS/DOOR FWD CABLE ON UPPER END.
- [SDR 60146](https://openairdocs.org/sdr/60146.md): Airstair · damaged · Mar 30, 2004 · N163YV · Beech 1900D · Entrance Stairs
  > AIRCRAFT DOOR WOULD NOT LOCK PROPERLY FROM THE INSIDE. MAINTENANCE CALL AND AIRCRAFT WAS MOVED TO THE HANGAR FOR REPAIRS. PERFORMED AIRSTAIR DOOR HONYECOMB INSERT. REPAIR AND SERVICE BULLENTIN 52-3099. RIGGED DOOR. P/N MS2469AS71
- [SDR AMWA35](https://openairdocs.org/sdr/AMWA35.md): Rib · cracked · Sep 7, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > RIB AT CSS 39.289 AT STRG P/N 101-640000-47 STRG P/N 101-640000-42 ON RH SIDE AND STRG P/N 101-640000-39 STRG P/N 101-640000-37 (4EA CRACKS ON THIS RIB)
- [SDR AMWA34](https://openairdocs.org/sdr/AMWA34.md): Rib · cracked · Sep 7, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > RIB AT CSS 54.026 CRACKED AT STRG. 101-640000-47 STRG. P/N 101-640000-42 RT SIDE AND STRG 101-640000-43 STRG P/N 101-640000-39 STRG P/N 10164000041 5 EA CRACKS ON THIS RIB)
- [SDR AMWA30](https://openairdocs.org/sdr/AMWA30.md): Rib · cracked · Aug 18, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE ACCORDANCE TO BEECH SRM MANUAL P/N 114-590021-9, 51-70-03.
- [SDR AMWA29](https://openairdocs.org/sdr/AMWA29.md): Rib · cracked · Aug 18, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE FLANGES AT CANTED STAB STA 24.973, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE TO BEECH SRM P/N 114-590021-9, 51-70-03.
- [SDR AMWA28](https://openairdocs.org/sdr/AMWA28.md): Rib · cracked · Aug 18, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB STA 39.289 AND STAB STA 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH SRM P/N 114-590021-9, 51-70-03.
- [SDR AMWA20](https://openairdocs.org/sdr/AMWA20.md): Rib · cracked · Aug 18, 2003 · N163YV · Beech 1900D · Vertical Stabilizer, Spar/Rib
  > WHILE PERFORMING AN INSPECTION IN THE VERT STAB, THE RIB FLANGES AT CANTED STAB STA 24.937, STAB, STA 39.289 AND STAB 54.026 WERE FOUND CRACKED. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BEECH STRUCTURAL REPAIR MANUAL P/N 114-590021-9, 51-70-03.
- [SDR AMW2002F00001](https://openairdocs.org/sdr/AMW2002F00001.md): Hose · leaking · Feb 27, 2002 · N163YV · Beech 1900D · Engine Oil Distribution (Airframe Furnished)
  > ENROUTE, THE CREW NOTICED THAT THE OIL PRESSURE LOW LIGHT FLICKERED AND THE OIL PRESSURE INDICATED LOW. THE CREW REDUCED POWER ON THE LEFT ENGINE AND LANDED WITHOUT INCIDENT.
- [SDR 98ZZZM898](https://openairdocs.org/sdr/98ZZZM898.md): Skin · cracked · Apr 6, 1998 · N163YV · Beech 1900D · Trailing Edge Flaps
  > OVERNIGHT MAINTENANCE IN ICT, FOUND A SMALL CRACK ON THE RT OUTBOARD FLAP LOWER SKIN TE 10 INCH FROM INBOARD END. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 97ZZZM966](https://openairdocs.org/sdr/97ZZZM966.md): Valve · normal · Aug 13, 1997 · N163YV · Beech 1900D · Turbine Engine Oil System
  > LEFT ENGINE WAS SHUT DOWN IN FLIGHT DUE TO HIGH OIL TEMP. EN ROUTE FROM FYV TO MCI. REPLACED OIL FILTER HOUSING O-RINGS. SUSPECT OIL TANK PRESSURIZING VALVE MAY HAVE BEEN STUCK CLOSED. UNABLE TO CONFIRM RELIEF VALVE PROBLEM. VALVE MAY HAVE FREED ITSELF DU
- [SDR 97ZZZX4245](https://openairdocs.org/sdr/97ZZZX4245.md): Flap · cracked · Aug 3, 1997 · N163YV · Beech 1900D · Trailing Edge Flaps
  > ICT - OVERNIGHT MAINTENANCE FOUND 1 INCH CRACK ON TE TOP SKIN OF RIGHT INBOARD FLAP 31 INCHES INBOARD EDGE. STOP-DRILLED CRACK WITH A NR 45 DRILL BIT. FABRICATED A 2 INCH BY 3 INCH PATCH FROM FLAP SKIN STOCK. INSTALLED PATCH USING REFERENCES SRM'S 51-00, 5
- [SDR 97ZZZM947](https://openairdocs.org/sdr/97ZZZM947.md): Flap · cracked · May 29, 1997 · N163YV · Beech 1900D · Trailing Edge Flaps
  > DURING ROUTINE MAINTENANCE A 2 INCH CRACK WAS FOUND ON THE LEFT O/D FLAP, 30 INCHES FROM OUTBOARD EDGE AND 16 INCHES FORWARD OF T/E. REPAIRED WITH DOUBLER IAW AMWA T.O. AND SRM. (M)
- [SDR 96ZZZX115](https://openairdocs.org/sdr/96ZZZX115.md): Gas Shock · bent · Oct 2, 1995 · N163YV · Beech 1900D · Cargo/Baggage Doors
  > WHEN CLOSING CARGO DOOR, THE GAS SHOCK BENT. REMOVED AND REPLACED SHOCK.

Next page: https://openairdocs.org/deregistered/N163YV-2010-06-09/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 = 'N163YV' AND deregistration_id = 'N163YV-2010-06-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N163YV-2010-06-09/reports

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