# Service difficulty reports: N255CA, cancelled Aug 23, 2013

A list on [N255CA, cancelled Aug 23, 2013](https://openairdocs.org/deregistered/N255CA-2013-08-23.md).

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

- [SDR COMA9910054](https://openairdocs.org/sdr/COMA9910054.md): Connector · loose · Apr 3, 1999 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > LANDING GEAR SELECTOR LOCK DID NOT RELEASE AFTER TAKEOFF. SECURED LOOSE AIR/GROUND SENSOR WIRING CONNECTION (PO316).
- [SDR COMA9910049](https://openairdocs.org/sdr/COMA9910049.md): Sequence Valve · leaking · Mar 29, 1999 · N255CA · Emb EMB120RT · Landing Gear Door Retract Section
  > HYDRAULIC LEAK, RIGHT HAND WHEEL WELL. REPLACED O RING AT DOOR SEQUENCE VALVE.
- [SDR COMA9910013](https://openairdocs.org/sdr/COMA9910013.md): Door · not latched · Jan 16, 1999 · N255CA · Emb EMB120RT · Fluid Service Doors
  > DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR OPEN, CLOSED AND LATCHED DOOR.
- [SDR COMA9810247](https://openairdocs.org/sdr/COMA9810247.md): Door · not latched · Nov 1, 1998 · N255CA · Emb EMB120RT · Fluid Service Doors
  > DOOR WARNING DURING TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT LATCHED. SECURED DOOR.
- [SDR COMA9810145](https://openairdocs.org/sdr/COMA9810145.md): Beam · corroded · Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER OMEGA BEAM. THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NR 1957-5, REV IR, 6-23-98.
- [SDR COMA9810144](https://openairdocs.org/sdr/COMA9810144.md): Strap · corroded · Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP. THE BUTT STRAP WAS REPLACED PER AERODESIGN REPORT NR 1671-1, REV A, 1-28-97.
- [SDR COMA9810143](https://openairdocs.org/sdr/COMA9810143.md): Tee Section · corroded · Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE RIGHT HAND T-SECTION AT FRAME 16. THE T-SECTION WAS REPLACED PER SRM STANDARD PRACTICES.
- [SDR COMA9810142](https://openairdocs.org/sdr/COMA9810142.md): Tee Section · corroded · Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE LEFT HAND T-SECTION AT FRAME 16. THE T-SECTION WAS REPLACED PER SRM STANDARD PRACTICES.
- [SDR COMA9810141](https://openairdocs.org/sdr/COMA9810141.md): Strap · corroded · Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP. THE BUTT-STRAP WAS REPLACED PER SRM STANDARD PRACTICES.
- [SDR COMA9810124](https://openairdocs.org/sdr/COMA9810124.md): Fcu · malfunction · May 19, 1998 · N255CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP AND ADVANCED SWS INDICATIONS ON MAP. REPLACED THE FLAP CONTROL UNIT.
- [SDR COMA9810122](https://openairdocs.org/sdr/COMA9810122.md): Hose · leaking · May 14, 1998 · N255CA · Emb EMB120RT · Engine Oil Cooler
  > LOW OIL PRESSURE WARNING ON RIGHT HAND ENGINE INFLIGHT SHUTDOWN. REPLACED OIL COOLER HOSE ASSEMBLY THAT WAS LEAKING DUE TO CHAFING DAMAGE.
- [SDR COMA9810083](https://openairdocs.org/sdr/COMA9810083.md): Sensor · dirty · Mar 30, 1998 · N255CA · Emb EMB120 · Landing Gear Position and Warning
  > THE LT MLG INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTION. LANDING GEAR WAS CYCLED AND 2ND RETRACTION WAS NORMAL. COULD NOT DUPLICATE DISCREPANCY. CLEANED INDICATION SENSORS AND CONNECTIONS. AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9810049](https://openairdocs.org/sdr/COMA9810049.md): Spinner Bulkhead · cracked · Mar 2, 1998 · N255CA · Emb EMB120RT · Propeller Spinner Section
  > DURING PREFLIGHT INSPECTION, THE RIGHT PROPELLER SPINNER BULKHEAD WAS FOUND TO BE CRACKED APPROXIMATELY 1.5 INCH ALONG THE BULKHEAD OUTER WALL BEHIND BLADE NR 2. AIRCRAFT WAS FERRIED BACK TO CVG HANGAR AND BULKHEAD REMOVED FOR REPAIR. DAMAGE APPEARS TO BE DU
- [SDR COMA9710498](https://openairdocs.org/sdr/COMA9710498.md): Sensor · defective · Dec 15, 1997 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. EMERGENCY SYSTEM USED TO LOWER LANDING GEAR. REPLACED DEFECTIVE RT MLG DOWNLOCK PROXIMITY SENSOR.
- [SDR COMA9710415](https://openairdocs.org/sdr/COMA9710415.md): Stator · cracked · Sep 19, 1997 · N255CA · Emb EMB120RT · Brake
  > DURING TEARDOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.
- [SDR COMA9710372](https://openairdocs.org/sdr/COMA9710372.md): Tee Section · corroded · Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 4C INSEPCTION TASK 5320-151-01I, REVEALED RIGHT T-SECTION AT FRAME 28 TO BE CORRODED. REMOVED CORRODED T-SECTION AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51.
- [SDR COMA9710371](https://openairdocs.org/sdr/COMA9710371.md): Sill · corroded · Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 4C INSPECTION TASK 5330-161-01I, REVEALED RIGHT CARGO COMPARTMENT SILL TO BE CORRODED BEYOND LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES CHAPTER 51.
- [SDR COMA9710370](https://openairdocs.org/sdr/COMA9710370.md): Floorbeam · corroded · Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Main, Floor Beam
  > DURING 4C INSPECTION TASK 5320-151-01I, REVEALED RIGHT FLOORBEAM AT FRAME 33 TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51 FOR LIKE TO LIKE PART REPLACEMENT.
- [SDR COMA9710369](https://openairdocs.org/sdr/COMA9710369.md): Angle · corroded · Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 4C INSPECTION TASK 5320-151-01I, REVEALED AFT EMERGENCY EXIT GUIDE PIN FITTINGS TO HAVE CORROSION BETWEEN FITTINGS AND THE EXIT SILL LOWER ATTACHE ANGLE. FURTHER INVESTIGATION REVEALED THAT THERE IS NO PRIMER OR SEALANT BETWEEN OR ON THESE PIECES. REP
- [SDR COMA9710368](https://openairdocs.org/sdr/COMA9710368.md): Fitting · corroded · Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING 4C INSPECTION TASK 5320-151-01I, REVEALED AFT EMERGENCY EXIT GUIDE PIN FITTINGS TO HAVE CORROSION BETWEEN THE FITTINGS AND THE EXIT SILL LOWER ATTACH ANGLE. FURTHER INVESTIGATION REVEALED THAT THERE IS NO PRIMER OR SEALANT BETWEEN OR ON THESE PIECES.
- [SDR COMA9710332](https://openairdocs.org/sdr/COMA9710332.md): Solenoid · failed · Jul 17, 1997 · N255CA · Emb EMB120RT · Passenger Oxygen System
  > ON C-CHECK TASK 35-09, THE PASSENGER OXYGEN MASKS AT SEAT 1BC FAILED TO DEPLOY. THE OXYGEN MASK DOOR SOLENOID AT THAT LOCATION WAS REPLACED, SYSTEM TESTS NORMAL.
- [SDR COMA9710181](https://openairdocs.org/sdr/COMA9710181.md): Connector · broken · Mar 17, 1997 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT. REPLACED DEFECTIVE WIRING CONNECTOR AT RT MLG UPLOCK.
- [SDR COMA9710099](https://openairdocs.org/sdr/COMA9710099.md): Pitchlock Screw · damaged · Feb 3, 1997 · N255CA · Emb EMB120RT · Propeller Controlling System
  > PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT DUE TO BEING STRUCK BY LAVORATORY CART WHILE STATIC ON AIRCRAFT RAMP. DURING PROPELLER IMPACT INSPECTION ACTUATOR FEATHER STOP TAB WAS FOUND TO BE DISPLACED APPROXIMATELY.125 FEET. ACTUATOR S/N 20383 WAS SUBSEQUENTLY
- [SDR COMA9710088](https://openairdocs.org/sdr/COMA9710088.md): Rollers · dirty · Jan 25, 1997 · N255CA · Emb EMB120RT · Leading Edge Devices
  > OUTBOARD FLAPS FAILED TO RETRACT. REPLACED THE ROLLERS ON THE RT OUTBOARD FLAP.
- [SDR COMA9710047](https://openairdocs.org/sdr/COMA9710047.md): Flap Tracks · dirty · Jan 20, 1997 · N255CA · Emb EMB120RT · Trailing Edge Flaps
  > FLAP DISAGREEMENT AFTER TAKEOFF. CLEANED LEFT OUTBOARD FLAP TRACKS.
- [SDR COMA9710039](https://openairdocs.org/sdr/COMA9710039.md): Flap · bent · Jan 16, 1997 · N255CA · Emb EMB120RT · Trailing Edge Flaps
  > FLAP FAIL WARNING. REPLACED LEFT OUTBOARD FLAP, OPERATIONAL CHECK GOOD.
- [SDR COMA9710030](https://openairdocs.org/sdr/COMA9710030.md): Roller · malfunctioned · Jan 13, 1997 · N255CA · Emb EMB120RT · Trailing Edge Flaps
  > FLAP DISAGREEMENT UPON FLAP RETRACTION AFTER TAKEOFF. REPLACED LT OUTBOARD FLAP ROLLERS 4 EACH. OPERATIONAL CHECK GOOD.
- [SDR COMA9710025](https://openairdocs.org/sdr/COMA9710025.md): Fuel Door · loose · Jan 12, 1997 · N255CA · Emb EMB120RT · Fluid Service Doors
  > DOOR LIGHT ON MAP CAME ON DURING TAKEOFF. RESECURED FUEL DOOR FASTENERS.
- [SDR COMA9610256](https://openairdocs.org/sdr/COMA9610256.md): Stringer · cracked · Aug 19, 1996 · N255CA · Emb EMB120RT · Nacelle/Pylon, Longeron/Stringer
  > INSPECTION REVEALED A CRACK IN THE RIGHT NACELLE LT STRINGER 1. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 2000-1, DATED 8-17-96.
- [SDR COMA9610250](https://openairdocs.org/sdr/COMA9610250.md): Butt Strap · corroded · Aug 19, 1996 · N255CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > INSPECTION REVEALED CORROSION ON THE FORWARD CABIN FLOOR SUPPORT OM26A BEAM BUTT STRAP ON THE LEFT SIDE GALLEY AREA. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB120 5RM STANDARD PRACTICES.
- [SDR COMA9610240](https://openairdocs.org/sdr/COMA9610240.md): Hyd Syst · moisture contam · Aug 3, 1996 · N255CA · Emb EMB120RT · Hydraulic System, Main
  > RT HYDRAULIC RESERVOIR LOW PRESSURE WARNING ILLUMINATED. DRAINED MOISTURE FROM RESERVOIR, SYSTEM CHECK NORMAL.
- [SDR COMA9610171](https://openairdocs.org/sdr/COMA9610171.md): Overheat Switch · defective · Jun 8, 1996 · N255CA · Emb EMB120RT · Pneumatic Indicating System
  > RT BLEED AIR DUCT OVERHEAT WARNING CAME ON DURING FLIGHT. REPLACED DEFECTIVE DUCT OVERHEAT SWITCH.
- [SDR COMA9610144](https://openairdocs.org/sdr/COMA9610144.md): Sig Cond Unit · malfunction · May 15, 1996 · N255CA · Emb EMB120RT · Propeller Controlling System
  > AUTO FEATHER SYSTEM WILL NOT TEST OR ARM. REPLACED THE RT ENGINE SIGNAL CONDITIONER UNIT.
- [SDR COMA9610070](https://openairdocs.org/sdr/COMA9610070.md): Prox Sensor · defective · Feb 7, 1996 · N255CA · Emb EMB120RT · Central Warning
  > TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. TRIM WAS CONFIRMED IN THE GREEN BAND. REPLACED THE LT ELEVATOR TRIM PROXIMITY SENSOR.
- [SDR COMA9610072](https://openairdocs.org/sdr/COMA9610072.md): Hose Assy · leaking · Feb 6, 1996 · N255CA · Emb EMB120RT · Engine Fuel Distribution
  > RT ENGINE IS LEAKING FUEL. REPLACED THE MOTIVE FLOW FUEL RETURN HOSE AND FITTING AT THE ENGINE HMU, DUE TO DAMAGED THREADS.
- [SDR COMA9610045](https://openairdocs.org/sdr/COMA9610045.md): Aural Warn Unit · malfunctioned · Jan 28, 1996 · N255CA · Emb EMB120RT · Central Warning
  > TAKEOFF AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE AURAL WARNING UNIT.
- [SDR COMA9610040](https://openairdocs.org/sdr/COMA9610040.md): Pump Hyd · failed · Jan 25, 1996 · N255CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), Main
  > RT ELECTRIC HYDRAULIC PUMP IS INOP. REPLACED THE RT ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP.
- [SDR COMA9610006](https://openairdocs.org/sdr/COMA9610006.md): Vsi · defective · Jan 9, 1996 · N255CA · Emb EMB120RT · Rate of Climb Indicator
  > PILOTS VSI TUBE BLANK. REPLACED THE 1VA-81A TA/VS1.
- [SDR COMA9512040](https://openairdocs.org/sdr/COMA9512040.md): Rollers · defective · Dec 23, 1995 · N255CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP DISAGREEMENT WARNING DURING TAKEOFF CLIMB. REPLACED THE OUTBD FLAP SECTION ROLLERS.
- [SDR COM11952](https://openairdocs.org/sdr/COM11952.md): Power Wire · failed · Aug 13, 1995 · N255CA · Emb EMB120RT · Electrical Power System
  > STRONG SMELL OF ELECTRICAL BURNING IN COCKPIT AREA. FOUND BURNED GALLEY POWER WIRE. SECURED POWER TO GALLEY BY PULLING BREAKERS AND PLACED ON DEFERRED MAINT LIST.
- [SDR COM11905](https://openairdocs.org/sdr/COM11905.md): Computer · defective · May 26, 1995 · N255CA · Emb EMB120RT · Stall Warning System
  > DURING TAKEOFF ROLL, THE STALL WARNING CAME ON. REPLACED STALL WARNING COMPUTER.
- [SDR COM11878](https://openairdocs.org/sdr/COM11878.md): Power Lever · worn · Apr 24, 1995 · N255CA · Emb EMB120RT · Power Lever
  > CREW REPORTED, THAT POWER LEVERS WERE NOT EVEN AT FLIGHT IDLE STOP. THE RT POWER LEVER FLIGHT IDLE STOP PIN AND ROLLER WERE FOUND TO BE WORN OVER 50 PERCENT. THE RT POWER LEVER ASSY WAS REPLACED.
- [SDR COM11845](https://openairdocs.org/sdr/COM11845.md): Trim Actuator · binding · Mar 31, 1995 · N255CA · Emb EMB120RT · Elevator Tab Control System
  > ELEVATOR TRIM IS BINDING. REPLACED THE RT ELEVATOR TRIM ACTUATOR.
- [SDR COM11798](https://openairdocs.org/sdr/COM11798.md): Angle · cracked · Feb 23, 1995 · N255CA · Emb EMB120RT · Vertical Stabilizer
  > DURING INSPECTION TASK 5530-324-03I AND 5530-324-02I, VERTICAL STABILIZER TO FUSELAGE ANGLE WAS FOUND TO BE CRACKED. REPLACED ANGLE IAW AERODESIGN REPORT 1446-1 AND EMB SRM.
- [SDR COM11783](https://openairdocs.org/sdr/COM11783.md): Swivel · leaking · Feb 12, 1995 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > HYDRAULIC LEAK, LEFT MLG. TIGHTENED FITTINGS ON HYDRAULIC SWIVEL.
- [SDR COM11777](https://openairdocs.org/sdr/COM11777.md): Swivel · leaking · Feb 12, 1995 · N255CA · Emb EMB120RT · Landing Gear Brake System
  > HYDRAULIC LEAK, LEFT MLG. REPLACED LEAKING BRAKE LINE SWIVEL.
- [SDR COM11738](https://openairdocs.org/sdr/COM11738.md): Prox Sensor · defective · Jan 23, 1995 · N255CA · Emb EMB120RT · Landing Gear Position and Warning
  > LT MLG GREEN SAFE LIGHT IS INOP, AND RED INTRANSIT LIGHT IS ILLUMINATED. REPLACED THE DOWN LOCK PROXIMITY SENSOR.

## 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 = 'N255CA' AND deregistration_id = 'N255CA-2013-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N255CA-2013-08-23/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.