# Service difficulty reports: N256CA, cancelled Oct 11, 2007

A list on [N256CA, cancelled Oct 11, 2007](https://openairdocs.org/deregistered/N256CA-2007-10-11.md).

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

- [SDR COMA9910166](https://openairdocs.org/sdr/COMA9910166.md): Fdau · malfunctioned · Oct 21, 1999 · N256CA · Emb EMB120RT · Flight Management Computing Hardware System
  > FDAU CIRCUIT BREAKER TRIPPED. REPLACED THE FDAU.
- [SDR COMA9910165](https://openairdocs.org/sdr/COMA9910165.md): Bleed Valve · failed · Oct 15, 1999 · N256CA · Emb EMB120RT · Pneumatic Distribution System
  > DURING CLIMB-OUT OF MCO, THE CROSS BLEED VALVE WOULD NOT CLOSE. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE CROSS BLEED VALVE.
- [SDR COMA9910135](https://openairdocs.org/sdr/COMA9910135.md): Bulb · failed · Aug 17, 1999 · N256CA · Emb EMB120RT · Stall Warning System
  > STALL WARNING LIGHT ILLUMINATED. REPLACED THE NR 2 STALL PANEL LIGHT BULB.
- [SDR COMA9910121](https://openairdocs.org/sdr/COMA9910121.md): Radar · failed · Jul 26, 1999 · N256CA · Emb EMB120RT · Weather Radar System
  > RADAR STUCK IN MAP MODE. COULD NOT DUPLICATE. REPLACED THE WXT-250B FOR TROUBLESHOOTING.
- [SDR COMA9910117](https://openairdocs.org/sdr/COMA9910117.md): Control Module · malfunction · Jul 22, 1999 · N256CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT. REPLACED CONTROL MODULE.
- [SDR COMA9910109](https://openairdocs.org/sdr/COMA9910109.md): Connector · loose · Jul 8, 1999 · N256CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY FLOOR LIGHTS AFT OF ROW 5 ARE INOPERATIVE. SECURED LOOSE WIRING CONNECTOR.
- [SDR COMA9910105](https://openairdocs.org/sdr/COMA9910105.md): Sign · broken · Jul 6, 1999 · N256CA · Emb EMB120RT · Emergency Lighting
  > EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN.
- [SDR COMA9910102](https://openairdocs.org/sdr/COMA9910102.md): Pressure Switch · malfunctioned · Jun 29, 1999 · N256CA · Emb EMB120RT · Fuel Pressure Indicating
  > LEFT ENGINE LOW FUEL PRESSURE WARNING. REPLACED THE LOW PRESSURE SWITCH.
- [SDR COMA9910097](https://openairdocs.org/sdr/COMA9910097.md): Sign · missing · Jun 21, 1999 · N256CA · Emb EMB120RT · Emergency Lighting
  > EXIT SIGN MISSING AT ROW 5. REPLACED EXIT SIGN.
- [SDR COMA9910093](https://openairdocs.org/sdr/COMA9910093.md): Door · not latched · Jun 12, 1999 · N256CA · Emb EMB120RT · Fluid Service Doors
  > DOORS WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT CLOSED PROPERLY. CLOSED AND LATCHED FUEL SERVICE PANEL.
- [SDR COMA9910058](https://openairdocs.org/sdr/COMA9910058.md): Sign · broken · Apr 7, 1999 · N256CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN.
- [SDR COMA9910041](https://openairdocs.org/sdr/COMA9910041.md): Altimeter · loose · Mar 5, 1999 · N256CA · Emb EMB120RT · Altimeter, Barometric/Encoder
  > PILOTS ALTIMETER VIBRATED DURING TAKEOFF. SECURED ALTIMETER.
- [SDR COMA9960062](https://openairdocs.org/sdr/COMA9960062.md): Beam · corroded · Feb 9, 1999 · N256CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > DURING AN E5 PART A INSPECTION, CORROSION DAMAGE WAS FOUND ON THE UPPER SURFACE OF THE CENTER OMEGA BEAM AT FRAME 16. THE DAMAGE CONSISTS OF 1 HOLE AND 4 AREAS OF PITTING. THE HOLE WAS CLEANED UP, DEBURNED AND SHARP EDGES REMOVED. THE 4 AREAS OF PITTING WAS
- [SDR COMA9910022](https://openairdocs.org/sdr/COMA9910022.md): Door · not secured · Jan 23, 1999 · N256CA · Emb EMB120RT · Door Warning System
  > DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL, AIRCRAFT RETURNED TO THE GATE. SECURED FUEL SERVICE DOOR FASTENER.
- [SDR COMA9910016](https://openairdocs.org/sdr/COMA9910016.md): Battery · discharged · Jan 20, 1999 · N256CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY.
- [SDR COMA9810285](https://openairdocs.org/sdr/COMA9810285.md): Door · not latched · Dec 15, 1998 · N256CA · Emb EMB120RT · Fluid Service Doors
  > SERVICE DOOR WARNING DURING TAKEOFF. CLOSED AND LATCHED SINGLE POINT FUEL SERVICE DOOR.
- [SDR COMA9810253](https://openairdocs.org/sdr/COMA9810253.md): Sign · loose · Nov 4, 1998 · N256CA · Emb EMB120RT · Emergency Lighting
  > ROW 5 EXIT SIGN FELL OFF. REPLACED THE EXIT SIGN.
- [SDR COMA9810248](https://openairdocs.org/sdr/COMA9810248.md): Latch · not secured · Nov 3, 1998 · N256CA · Emb EMB120RT · Service Doors
  > DOOR WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT CLOSED. SECURED SERVICE DOOR.
- [SDR COMA9810241](https://openairdocs.org/sdr/COMA9810241.md): Sign · broken · Oct 22, 1998 · N256CA · Emb EMB120RT · Emergency Lighting
  > CREW REPORTED EMERGENCY EXIT SIGN BROKEN. REPLACED EXIT SIGN AT SEAT 5A.
- [SDR COMA9810228](https://openairdocs.org/sdr/COMA9810228.md): Door · not latched · Oct 6, 1998 · N256CA · Emb EMB120RT · Fluid Service Doors
  > SERVICE DOOR WARNING DURING TAKEOFF. SECURED LATCHES ON SINGLE POINT FUEL SERVICE DOOR.
- [SDR COMA9810217](https://openairdocs.org/sdr/COMA9810217.md): Door · not latched · Sep 17, 1998 · N256CA · Emb EMB120RT · Fluid Service Doors
  > SERVICE DOOR WARNING ON DURING FLIGHT. CLOSE AND LATCHED SINGLE POINT FUEL SERVICE DOOR.
- [SDR COMA9810185](https://openairdocs.org/sdr/COMA9810185.md): Door · unlatched · Aug 30, 1998 · N256CA · Emb EMB120RT · Fluid Service Doors
  > DOORS WARNING AFTER TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT SECURED. CLOSED AND LATCHED DOOR.
- [SDR COMA9810179](https://openairdocs.org/sdr/COMA9810179.md): Sequence Valve · failed · Aug 18, 1998 · N256CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > NLG WOULD NOT RETRACT. REPLACED THE LEFT HAND NLG DOOR SEQUENCE VALVE.
- [SDR COMA9810175](https://openairdocs.org/sdr/COMA9810175.md): Sign · broken · Aug 11, 1998 · N256CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN ASSY.
- [SDR COMA9810127](https://openairdocs.org/sdr/COMA9810127.md): Pump · inoperative · May 21, 1998 · N256CA · Emb EMB120RT · Propeller Controlling System
  > LEFT ENGINE ELECTRIC FEATHER PUMP IS INOP. REPLACED AUXILIARY FEATHER PUMP.
- [SDR COMA9710416](https://openairdocs.org/sdr/COMA9710416.md): Stator · cracked · Sep 22, 1997 · N256CA · Emb EMB120RT · Brake
  > DURING TEARDOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.
- [SDR COMA9710348](https://openairdocs.org/sdr/COMA9710348.md): Frame · chafed · Aug 10, 1997 · N256CA · Emb EMB120RT · Fuselage Main, Frame
  > RIGHT AFT EMERGENCY EXIT FRAME NIB HAS GOUGES AT FORWARD SECTION OF NIB. REMOVED DAMAGED FRAME. INSTALLED NEW SERVICEABLE FRAME P/N 120-26331-002 IN ACCORDANCE WITH EMBRAER EMB 120 SRM 51-10-02 PART 3 AND 51-40-02.
- [SDR COMA9710347](https://openairdocs.org/sdr/COMA9710347.md): Frame · chafed · Aug 9, 1997 · N256CA · Emb EMB120RT · Fuselage Main, Frame
  > RIGHT AFT EMERGECY EXIT AFT FUSELAGE FRAME HAS CHAFE DAMAGE FROM SCREW HEAD. REMOVED DAMAGED FRAME. INSTALLED NEW SERVICEABLE FRAME P/N 120-26331-001 IAW EMBRAER EMB 120 SRM 51-10-02 PART 3 AND 51-40-02.
- [SDR COMA9710274](https://openairdocs.org/sdr/COMA9710274.md): Ahrs · failed · May 14, 1997 · N256CA · Emb EMB120RT · Integrated Flight System
  > NR 1 AHRS IS INOP. REPLACED THE NR 1 AHRS.
- [SDR COMA9710264](https://openairdocs.org/sdr/COMA9710264.md): Striker Plate · broken · May 11, 1997 · N256CA · Emb EMB120RT · Door Warning System
  > CARGO DOOR UNSAFE WARNING CAME ON DURING FLIGHT. REPLACED BROKEN DOOR WARNING SWITCH STRIKER PLATE.
- [SDR COMA9610317](https://openairdocs.org/sdr/COMA9610317.md): Stringer · corroded · Oct 28, 1996 · N256CA · Emb EMB120RT · Fuselage Main, Longeron/Stringer
  > C2 INSPECTION FOUND A SMALL AREA OF CORROSION ON FWD FUSELAGE STRINGER 21L BETWEEN FS 3293 AND 3596.5. THE DAMAGED AREA OF THE STRINGER WAS REMOVED AND REPAIRED PER AERODESIGN REPORT NR 1990-3, REV IR, DATED 10-26-96.
- [SDR COMA9610316](https://openairdocs.org/sdr/COMA9610316.md): Skin · gouged · Oct 28, 1996 · N256CA · Emb EMB120RT · Fuselage Main, Plate/Skin
  > C2 INSPECTION FOUND THE LOWER FUSELAGE CENTER SECTION SKIN TO BE GOUGED BY THE RIGHT WING DE-ICE PRESSURE REGULATOR. THE DAMAGED SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 201, SHEET 3, PAGE 204. THE DE-ICE PRESSURE REGULATOR WAS REPOSITIONED FOR PROPER CLEA
- [SDR COMA9610239](https://openairdocs.org/sdr/COMA9610239.md): Prop Governor · malfunctioned · Aug 5, 1996 · N256CA · Emb EMB120RT · Propeller Controlling System
  > LT PROPELLER WILL NOT AUTO-FEATHER OR MANUAL FEATHER. COULD NOT DUPLICAE DISCREPANCY, SYSTEM TEST NORMAL AND ACFT RETURNED TO SERVICE.
- [SDR COMA9610119](https://openairdocs.org/sdr/COMA9610119.md): Steering · pulled left · Apr 1, 1996 · N256CA · Emb EMB120RT · Landing Gear Steering System
  > NOSE WHEEL STEERING PULLED TO LEFT TWICE DURING LANDING ROLL. COULD NOT DUPLICATE. INSPECTED N.W.S. SYSTEM AND TAXI CHECK NORMAL.
- [SDR COMA9610110](https://openairdocs.org/sdr/COMA9610110.md): Uplock Sensor · out of adjust · Mar 22, 1996 · N256CA · Emb EMB120RT · Landing Gear Position and Warning
  > LT MLG INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTED. ADJUSTED THE UPLOCK PROXIMITY SENSOR TO M/M SPECIFICATIONS.
- [SDR COMA9610100](https://openairdocs.org/sdr/COMA9610100.md): Intransit Light · malfunctioned · Mar 9, 1996 · N256CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > LEFT MLG INTRANSIT LIGHTS REMAIN ON AFTER LANDING GEAR RETRACTED. COULD NOT DUPLICATE DISCREPANCY. FOUND ALL ADJUSTMENTS AND CLEARANCES WITHIN LIMITS. ACFT RETURNED TO SERVICE.
- [SDR COMA9610094](https://openairdocs.org/sdr/COMA9610094.md): Filter · dirty · Mar 6, 1996 · N256CA · Emb EMB120RT · Hydraulic System, Main
  > LEFT HYDRAULIC SYSTEM FILTER BYPASS WARNING ILLUMINATED. REPLACED HYDRAULIC SYSTEM FILTER.
- [SDR COMA9610083](https://openairdocs.org/sdr/COMA9610083.md): Hyd Pump · leaking · Feb 13, 1996 · N256CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC FLUID LEAKING FROM RT ENGINE NACELLE. REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP. PART TOTAL CYCLES, 7,269.
- [SDR COMA9610030](https://openairdocs.org/sdr/COMA9610030.md): Pump · defective · Jan 14, 1996 · N256CA · Emb EMB120RT · Propeller Controlling System
  > LEFT ENGINE PROPELLER WILL NOT UNFEATHER. REPLACED THE PROPELLER OVERSPEED GOVERNOR OIL PUMP.
- [SDR COMA9610008](https://openairdocs.org/sdr/COMA9610008.md): Roller · worn · Jan 8, 1996 · N256CA · Emb EMB120RT · Trailing Edge Flaps
  > FLAP DISAGREEMENT INDICATION AFTER TAKEOFF. REPLACED WORN ROLLERS ON LT OUTBOARD FLAP.
- [SDR COMA9610007](https://openairdocs.org/sdr/COMA9610007.md): Indication · malfunctioned · Jan 8, 1996 · N256CA · Emb EMB120RT · Trailing Flap Position Indicating System
  > FLAP DISAGREEMENT INDICATION AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY - ACFT RETURNED TO SERVICE.
- [SDR COMA9512031](https://openairdocs.org/sdr/COMA9512031.md): Roller · worn · Dec 18, 1995 · N256CA · Emb EMB120RT · Trailing Edge Flap Control System
  > RECEIVED FLAP DISAGREE WARNING, WHEN FLAPS SELECTED TO ZERO DEGREES. REPLACED THE ROLLERS ON THE RT OUTBD FLAP.
- [SDR COMA9511496](https://openairdocs.org/sdr/COMA9511496.md): Sensor · defective · Sep 17, 1995 · N256CA · Emb EMB120RT · Cabin Temperature Sensor
  > RT DUCT OVERHEAT WARNING, WARNING REMAINED ON WHEN THE TEMPERATURE WAS SELECTED TO FULL COLD. REPLACED THE DUCT OVER TEMPERATURE SENSOR.
- [SDR COM11949](https://openairdocs.org/sdr/COM11949.md): Cooling Fan · failed · Aug 10, 1995 · N256CA · Emb EMB120RT · Air Distribution Fan
  > DURING TAXI, RT A/C PACK PRODUCED SMOKE IN CABIN. PACK FAILED AND DUCT LEAK INDICATOR ON. REPLACED THE RT GROUND COOLING FAN.
- [SDR COM11865](https://openairdocs.org/sdr/COM11865.md): Latch · broken · Apr 18, 1995 · N256CA · Emb EMB120RT · Landing Gear Door Retract Section
  > RT MLG INBD DOOR LATCH IS BROKEN. REPLACED LATCH ASSY.
- [SDR COM11847](https://openairdocs.org/sdr/COM11847.md): Latch · broken · Apr 5, 1995 · N256CA · Emb EMB120RT · Hydraulic Compartment Doors
  > RIGHT HYDRAULIC PACK SERVICE DOOR HAS A BROKEN LATCH. REPLACED LATCH.
- [SDR COM11811](https://openairdocs.org/sdr/COM11811.md): Gcu · defective · Mar 5, 1995 · N256CA · Emb EMB120RT · DC Generating System
  > RIGHT ENGINE STARTER DOES NOT TERMINATE START SEQUENCE AT 50 PERCENT. REPLACED THE GCU.
- [SDR COM11734](https://openairdocs.org/sdr/COM11734.md): Servo · defective · Jan 18, 1995 · N256CA · Emb EMB120RT · Elevator Control System
  > ELECRIC TRIM IS INOP, AND MANUAL TRIM FEELS ROUGH. REPLACED THE PITCH TRIM SERVO.
- [SDR COM11719](https://openairdocs.org/sdr/COM11719.md): Hyd Syst · frozen · Jan 4, 1995 · N256CA · Emb EMB120RT · Hydraulic System, Main
  > GREEN SYSTEM HYDRAULIC RESEVOIR LOW PRESSURE INDICATOR ON. RESERVOIR PRESSURIZATION SYSTEM CONTAINED MOISTURE WHICH FROZE. PURGED MOISTURE FROM SYSTEM.
- [SDR COM11713](https://openairdocs.org/sdr/COM11713.md): Control Box · defective · Jan 1, 1995 · N256CA · Emb EMB120RT · Brake Anti-Skid Section
  > DURING LANDING ANTI-SKID FAILED. REPLACED THE ANTI-SKID CONTROL BOX.

## 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 = 'N256CA' AND deregistration_id = 'N256CA-2007-10-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N256CA-2007-10-11/reports

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