# Service difficulty reports: N244YV, cancelled Jul 10, 2012

A list on [N244YV, cancelled Jul 10, 2012](https://openairdocs.org/deregistered/N244YV-2012-07-10.md).

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

- [SDR AMWA071001017](https://openairdocs.org/sdr/AMWA071001017.md): Skin · chafed · Dec 6, 2007 · N244YV · Beech 1900D · Wing, Plate/Skin
  > FRICTION CHAFING DURING ENGINE OPERATION CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. CHAFING WAS ALONG THE ENTIRE LENGTH AND SHAPE OF THE NACELLE. OBTAINED APPROVED DATA AND REPAIRED WING SKIN.
- [SDR AMWA1001010A](https://openairdocs.org/sdr/AMWA1001010A.md): Spar · damaged · Nov 9, 2007 · N244YV · Beech 1900D · Wing Spar
  > AT RT WING WS 54.75 FOUND 0.50 INCH HOLE THROUGH SUB SPAR. HOLE HAD EVIDENCE OF POSSIBLE ELECTRICAL ARCING AT WIRING GROUNDING ATTACHMENT. REPAIRED IAW APPROVED DATA AND CLEARED DISCREPANCY.
- [SDR AMWA87546](https://openairdocs.org/sdr/AMWA87546.md): Battery · corroded · Sep 19, 2007 · N244YV · Beech 1900D · Battery/Charger System
  > AFTER ARRIVING, THE CREW CALLED MAINT CONTROL TO WRITEUP THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS A NUISANCE ALARM AND IS DISTRACTING TO THE FLIGHTCREW. MAINTENANCE CLEANED THE BATTERY SHUNT, OPS NORMAL.
- [SDR AMWA86034](https://openairdocs.org/sdr/AMWA86034.md): Switch · malfunctioned · Jul 13, 2007 · N244YV · Beech 1900D · Propeller Controlling System
  > DURING FLT LT PROPS WENT INTO AUTOFEATHER. LANDED WITH NO FURTHER INCIDENT. PERFORMED CHECK FLT AND WAS UNSATISFACTORY. REMOVED AND REPLACED LOW AND HIGH TQ SWITCH, A123PCB. TEST FLT SATISFACTORY
- [SDR AMWA84318BC](https://openairdocs.org/sdr/AMWA84318BC.md): Battery Cable · corroded · Apr 30, 2007 · N244YV · Beech 1900D · Electrical Power System Wiring
  > BATT CHARGE ANNUNCIATOR ILLUMINATED ON DEPARTURE JUST AFTER GEAR RETRACTION. THIS BATTERY CHARGE ANNUNCIATOR LIGHT ILLUM IS CONSIDERED A NUISANCE WARNING, CAUSING SERIOUS DISTRACTIONS TO THE PILOTS. CLEANED AND RESECURED BATTERY CONNECTIONS.
- [SDR AMWA078811](https://openairdocs.org/sdr/AMWA078811.md): Eadi · odor · Aug 7, 2006 · N244YV · Beech 1900D · Attitude and Direction Data System
  > AFTER TAKEOFF, CREW NOTICES SMELL (ELECTRICAL ODOR) IN FLIGHT DECK. DECLARED AN EMERGENCY W/EQUIP LANDED AND TAXIED OFF RUNWAY. SHUT ENGINES DOWN ON TAXI WAY. NO FURTHER INCIDENTS. MAINTENANCE FERRIED A/C. MAINTENANCE REMOVED AND REPLACED CAPTIANS EADI, IAW B
- [SDR AMWA078595](https://openairdocs.org/sdr/AMWA078595.md): Brake · weak · Jul 25, 2006 · N244YV · Beech 1900D · Landing Gear Brake System
  > CREW REPORTED AFTER LANDING, THAT THE LT BRAKE WAS WEAK. MAINTENANCE WAS CALLED AND FOUND LT BRAKE WEAR TO BE WITHIN LIMITS. BLED BRAKES AND OPS CHECKED NORMAL. WORK DONE IAW BMM 32-40-05
- [SDR AMWA078586](https://openairdocs.org/sdr/AMWA078586.md): Engine · malfunctioned · Jul 24, 2006 · N244YV · Beech 1900D · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF RT ENGINE TORQUE DROPPED TO 2000 FTLBS A/C RTF WITHOUT FURTHER INCIDENT. MAINTENANCE WAS CALLED AND ADJUSTED THE RT ENGINE LOW TORQUE SETTINGS. OPERATIONAL CHECK NORMAL. IAW BMM-76-10-00.
- [SDR 1060504022A](https://openairdocs.org/sdr/1060504022A.md): Spar Cap · corroded · May 23, 2006 · N244YV · Beech 1900D · Wing Spar
  > BIO-CORROSION RT MAIN SPAR CAP AT WS 124.588. REPAIRED IAW MFG FR-CO-01350 REV.1
- [SDR 1060504022](https://openairdocs.org/sdr/1060504022.md): Spar Cap · corroded · May 23, 2006 · N244YV · Beech 1900D · Wing Spar
  > BIO-CORROSION LT MAIN SPAR CAP AT WS124.588. REPAIRED IAW MFG FR-CO-01350 REV.1
- [SDR AMWA77016](https://openairdocs.org/sdr/AMWA77016.md): Windscreen · cracked · Apr 17, 2006 · N244YV · Beech 1900D · Flight Compartment Windows
  > DURING DECENT INTO PIT AT APPROX 14,000 FT. CREW HEARD CAPTIANS WINDSHIELD CRACK. LANDED IN PIT WITH NO FURTHER INCIDENT. MAINTENANCE THEN REMOVED AND REPLACED THE WINDSHIELD.
- [SDR 76399](https://openairdocs.org/sdr/76399.md): Fire Loop · warning light · Mar 15, 2006 · N244YV · Beech 1900D · Fire Detection
  > RT FIRE LOOP WARNING ILLUMINATED IN FLIGHT WITH RT FIRE HANDLE ILLUMINATION MORE INFO TO BE ADDED LATER. CONTROL NR 76398.
- [SDR 76398](https://openairdocs.org/sdr/76398.md): Fire Loop · out of position · Mar 15, 2006 · N244YV · Beech 1900D · Fire Detection
  > RIGHT FIRE LOOP WARNING ILLUMED IN FLIGHT WITH RIGHT FIRE HANDLE ILLUMINATION. MAINTENANCE WAS CALLED AND REPOSITIONED FIRELOOP OPS CHECKS NORMAL. NO PARTS WERE USED.
- [SDR AMWA76380](https://openairdocs.org/sdr/AMWA76380.md): Connector · loose · Feb 14, 2006 · N244YV · Beech 1900D · Fire Protection System Wiring
  > RIGHT FIRE LOOP CAUSES MASTER WARNING TO ILLUMINATE IN FLIGHT. MAINTENANCE CAME AND RESECURED A LOOSE CONNECTION AT THE FORWARD CONNECTOR. OPS CHECK NORMAL.
- [SDR 68755](https://openairdocs.org/sdr/68755.md): Brake Assy · weak · Jan 28, 2005 · N244YV · Beech 1900D · Brake
  > ON CREWS FIRST FLIGHT CHECKS LEFT BRAKE WAS WEAK. A/C RETURNED TO THE HANGAR. MTC BLED BRAKES AND A/C RETURNED TO SERVICE. BLED BRAKES.
- [SDR 57827](https://openairdocs.org/sdr/57827.md): Autofeather Sys · malfunctioned · Jan 11, 2004 · N244YV · Beech 1900D · Propeller Feathering/Reversing
  > ON TAXI OUT CREW BEGAN STARTING LT ENGINE, AFTER GETTING IT STARTED PROPS WOULDN'T COME OUT. ALSO THE AUTOFEATHER WOULDN'T TEST. CREW RETURNED TO THE GATE WITH NO FURTHER INCIDENT. RAN BOTH ENGINES, ALL SYS OPS CK NORMAL.
- [SDR AMW2002F00003](https://openairdocs.org/sdr/AMW2002F00003.md): Pump · failed · Sep 16, 2002 · N244YV · Beech 1900D · Engine Fuel Distribution
  > WHILE FLIGHT WAS ENROUTE, THE LT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEREFORE RETURNED THE AIRCRAFT TO THE FIELD WITHOUT ANY FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THAT REPLACED THE LT LOW PRESSURE ENGINE DRIVEN FUEL PUMP.
- [SDR 98ZZZM257](https://openairdocs.org/sdr/98ZZZM257.md): Bulkhead · cracked · Jan 22, 1998 · N244YV · Beech 1900D · Trailing Edge Flaps
  > ICT MAINTENANCE FOUND SMALL CRACK IN DOVETAIL BULKHEAD. REPAIRED IAW AMWA TO 1900-27-00-0001. ICT MAINTENANCE FOUND 2 CRACKS IN TOP SKIN. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 98ZZZM258](https://openairdocs.org/sdr/98ZZZM258.md): Skin · cracked · Jan 15, 1998 · N244YV · Beech 1900D · Trailing Edge Flaps
  > ICT MAINTENANCE FOUND SMALL CRACK IN TOP SKIN OF LEFT OUTBOARD FLAP AT INBOARD ATTACH BRACKET. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 97ZZZM1202](https://openairdocs.org/sdr/97ZZZM1202.md): Skin · cracked · Oct 11, 1997 · N244YV · Beech 1900D · Trailing Edge Flaps
  > AT ICT OVERNIGHT MAINTENANCE, THE RT OUTBOARD FLAP WAS FOUND TO HAVE A.5 INCH LONG CRACK 8 INCHES FROM OUTBOARD EDGE AND 4 INCHES FROM LE BOTTOM SKIN. FLAP WAS REPAIRED IAW AMWA TO 1900-27-00-0001 AND SRM 51-70. (M)
- [SDR 97ZZZX4168](https://openairdocs.org/sdr/97ZZZX4168.md): Bracket · chafed · Jun 19, 1997 · N244YV · Beech 1900D · Trailing Edge Flaps
  > REMOVED AND REPLACED RIGHT TRAILING EDGE FLAP ATTACH BRACKET IAW SRM 51-40 DUE TO CHAFING, P/N 3516505031.
- [SDR 97ZZZX4169](https://openairdocs.org/sdr/97ZZZX4169.md): Flap · cracked · Jun 10, 1997 · N244YV · Beech 1900D · Trailing Edge Flaps
  > RIGHT INBOARD FLAP WAS FOUND TO HAVE A CRACK INBOARD OF DOVETAIL. STOP DRILLED AND INSTALLED DOUBLER.

## 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 = 'N244YV' AND deregistration_id = 'N244YV-2012-07-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N244YV-2012-07-10/reports

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