# Service difficulty reports: N263CA, cancelled Nov 16, 2006

A list on [N263CA, cancelled Nov 16, 2006](https://openairdocs.org/deregistered/N263CA-2006-11-16.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 · 55 reports

- [SDR COMA0110004](https://openairdocs.org/sdr/COMA0110004.md): Frame · corroded · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Frame
  > UPON COMPLIANCE OF 2C INSPECTION TASK 131-012 AND 132-012 THE FUSELAGE FRAME 20 CHANNEL BETWEEN STRINGERS 20L AND 20R WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURE REPAIR MANUAL STANDARD PRACTICES AND SRM 53-10-04 FIGURE 201 A
- [SDR COMA0010108](https://openairdocs.org/sdr/COMA0010108.md): Floorbeam · cracked · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Floor Beam
  > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.
- [SDR COMA0010123](https://openairdocs.org/sdr/COMA0010123.md): Skin · chafed · May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin
  > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.
- [SDR COMA0010122](https://openairdocs.org/sdr/COMA0010122.md): Skin · chafed · May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin
  > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.
- [SDR COMA0010121](https://openairdocs.org/sdr/COMA0010121.md): Skin · chafed · May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin
  > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.
- [SDR COMA0010120](https://openairdocs.org/sdr/COMA0010120.md): Skin · chafed · May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin
  > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.
- [SDR COMA0010119](https://openairdocs.org/sdr/COMA0010119.md): Shear Tie · cracked · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Structure
  > UPON COMPLIANCE OF 2C INSPECTION TASK 231-012, WHILE GAINING ACCESS THE LT FUSELAGE SKIN SUPPORT BETWEEN FRAMES 12 AND 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES.
- [SDR COMA0010118](https://openairdocs.org/sdr/COMA0010118.md): Shear Tie · cracked · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Structure
  > UPON COMPLIANCE OF 2C INSPECTION TASK 232-012, THE FUSELAGE FRAME 13A SKIN SUPPORT AT STRINGER 14R WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3653-1, REV IR, 5-6-00.
- [SDR COMA0010117](https://openairdocs.org/sdr/COMA0010117.md): Strap · corroded · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Structure
  > UPON COMPLIANCE OF 2C INSPECTION TASK 164-012, THE CARGO COMPARTMENT FLOOR SUPPORT AFT RT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5-15-
- [SDR COMA0010116](https://openairdocs.org/sdr/COMA0010116.md): Strap · corroded · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Structure
  > UPON COMPLIANCE OF 2C INSPECTION TASK 163-012, THE CARGO COMPARTMENT FLOOR SUPPORT AFT LT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5-15-
- [SDR COMA0010115](https://openairdocs.org/sdr/COMA0010115.md): Strap · corroded · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Structure
  > UPON COMPLIANCE OF 2C INSPECTION TASK 162-012, THE CARGO COMPARTMENT FLOOR SUPPORT FORWARD RT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV IR, 5
- [SDR COMA0010113](https://openairdocs.org/sdr/COMA0010113.md): Stringer · dented · May 19, 2000 · N263CA · Emb EMB120RT · Nacelle/Pylon, Longeron/Stringer
  > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE DENTED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 54-10-01 FIGURE 202.
- [SDR COMA0010112](https://openairdocs.org/sdr/COMA0010112.md): Skin · gouged · May 19, 2000 · N263CA · Emb EMB120RT · Cargo/Baggage Doors
  > UPON COMPLIANCE OF 2C INSPECTION TASK 813-02Z, THE CARGO DOOR SKIN WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 52-30-01 FIGURE 201.
- [SDR COMA0010111](https://openairdocs.org/sdr/COMA0010111.md): Support Bracket · cracked · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Structure
  > RIVET HEAD WAS NOTICED CRACKED ON LEFT SIDE OF FUSELAGE AT FRAME 9. INTERNAL INVESTIGATION FOUND THE SKIN SUPPORT TO BE CRACKED. THE SKIN SUPPORT WAS REPLACED IAW EMB-120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, REV IR, 2-16-93.
- [SDR COMA0010110](https://openairdocs.org/sdr/COMA0010110.md): Strap · corroded · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FUSELAGE FORWARD LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-2, REV IR, 12-4-96.
- [SDR COMA0010109](https://openairdocs.org/sdr/COMA0010109.md): Floorbeam · cracked · May 19, 2000 · N263CA · Emb EMB120RT · Fuselage Main, Floor Beam
  > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE RT FLOOR PROP AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00.
- [SDR COMA0010064](https://openairdocs.org/sdr/COMA0010064.md): Circuit Breaker · tripped · May 10, 2000 · N263CA · Emb EMB120RT · Engine Controls
  > LEFT HAND, FLIGHT IDLE STOP SOLENOID, CIRCUIT BREAKER IS TRIPPED. RESET CIRCUIT BREAKER, TESTED SYSTEM FOUND TO OPERATE NORMAL.
- [SDR COMA0010024](https://openairdocs.org/sdr/COMA0010024.md): Sign · loose · Feb 5, 2000 · N263CA · Emb EMB120RT · Emergency Lighting
  > EXIT SIGN AT ROW 5 FELL OFF. REPLACED EXIT SIGN.
- [SDR COMA9910177](https://openairdocs.org/sdr/COMA9910177.md): Sign · broken · Nov 29, 1999 · N263CA · Emb EMB120RT · Emergency Lighting
  > EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN.
- [SDR COMA9910147](https://openairdocs.org/sdr/COMA9910147.md): Relay · failed · Sep 15, 1999 · N263CA · Emb EMB120RT · DC Power Distribution System
  > THE EMERGENCY BUS LIGHT ILLUMINATED DURING FLIGHT AND WOULD NOT EXTINGUISH. REPLACED RELAY KO440.
- [SDR COMA0010131](https://openairdocs.org/sdr/COMA0010131.md): Sign · broken · Aug 11, 1999 · N263CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN.
- [SDR COMA9910111](https://openairdocs.org/sdr/COMA9910111.md): Sensor · failed · Jul 14, 1999 · N263CA · Emb EMB120RT · Landing Gear Position and Warning
  > LEFT HAND MLG DISAGREEMENT LIGHT REMAINS ON AFTER GEAR RETRACTED. REPLACED THE UPLOCK PROXIMITY SENSORS.
- [SDR COMA9910104](https://openairdocs.org/sdr/COMA9910104.md): Battery · discharged · Jul 1, 1999 · N263CA · Emb EMB120RT · Emergency Lighting
  > FORWARD FLOOR EMERGENCY LIGHTING WAS WEAK. REPLACED EMERGENCY BATTERY.
- [SDR COMA9910094](https://openairdocs.org/sdr/COMA9910094.md): Sensor · malfunction · Jun 13, 1999 · N263CA · Emb EMB120RT · Landing Gear Position and Warning
  > LANDING GEAR DID NOT EXTEND NORMALLY. OVERRIDE SYSTEM WAS USED. REPLACED THE LEFT HAND MLG DOWNLOCK PROX SENSOR SWITCH.
- [SDR COMA9910090](https://openairdocs.org/sdr/COMA9910090.md): Hyd Syst · reqd service · Jun 4, 1999 · N263CA · Emb EMB120RT · Hydraulic System, Main
  > GREEN HYDRAULIC SYSTEM LOW PRESSURE WARNING DURING GEAR RETRACTION. SERVICED HYDRAULIC RESERVOIR TO PROPER LEVEL.
- [SDR COMA9910061](https://openairdocs.org/sdr/COMA9910061.md): Angle · corroded · Apr 15, 1999 · N263CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > WHILE PERFORMING TASK 5320-252-04E ON A 2000 FLIGHT CYCLE INSPECTION, FOUND AFT EXIT PIN RECEPTACLES TO BE CORRODED BETWEEN RECEPTACLES AND FLOOR ANGLE. REMOVED FLOOR ANGLE AND PIN RECEPTACLES AND REPLACED WITH SERV UNITS IAW EMB-120-SRM.
- [SDR COMA9910060](https://openairdocs.org/sdr/COMA9910060.md): Angle · corroded · Apr 15, 1999 · N263CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > WHILE PERFORMING TASK 5320-252-04E ON 2000 FLIGHT CYCLE INSPECTION, FOUND LOWER FLOOR ANGLE OF AFT EXIT TO BE CORRODED BETWEEN ANGLE AND PIN RECEPTACLES. REMOVED ANGLE AND PINS AND REPLACED WITH SERVICEABLE UNITS IAW EMB-120 SRM.
- [SDR COMA9910043](https://openairdocs.org/sdr/COMA9910043.md): Rheostat · inoperative · Mar 18, 1999 · N263CA · Emb EMB120RT · Flight Compartment Lighting
  > OVERHEAD PANEL LIGHT IS INOPERABLE. REPLACED RHEOSTAT.
- [SDR COMA9810261](https://openairdocs.org/sdr/COMA9810261.md): Sign · broken · Nov 11, 1998 · N263CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY EXIT SIGN AT ROW 8 BROKEN. REMOVED AND REPLACED EXIT SIGN ASSY.
- [SDR COMA9810187](https://openairdocs.org/sdr/COMA9810187.md): Pin · installed · Aug 30, 1998 · N263CA · Emb EMB120RT · Landing Gear Retraction/Extension System
  > NLG DID NOT RETRACT. REMOVED NLG DOWN LOCK SAFETY PIN. AIRCRAFT RETURNED TO SERVICE.
- [SDR COMA9810151](https://openairdocs.org/sdr/COMA9810151.md): Pcu · malfunction · Jun 30, 1998 · N263CA · Emb EMB120RT · Propeller Controlling System
  > RIGHT HAND RPM DROPPED 30 PERCENT DURING TAKEOFF ROLL. REPLACED THE RIGHT HAND PCU.
- [SDR COMA9810102](https://openairdocs.org/sdr/COMA9810102.md): Leak Warning · activated · Apr 15, 1998 · N263CA · Emb EMB120RT · Pneumatic Indicating System
  > RIGHT HAND DUCT LEAK WARNING DURING TAKEOFF. COULD NOT DUPLICATE PROBLEM.
- [SDR COMA9810030](https://openairdocs.org/sdr/COMA9810030.md): Aural Warn Unit · loose · Jan 26, 1998 · N263CA · Emb EMB120RT · Central Warning
  > TAKEOFF TRIM AURAL WARNING DURING TAKEOFF. SECURED LOOSE AURAL WARNING UNIT IN RACK.
- [SDR COMA9810024](https://openairdocs.org/sdr/COMA9810024.md): Sensor · defective · Jan 15, 1998 · N263CA · Emb EMB120RT · Elevator Tab Control System
  > TRIM WARNING DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR.
- [SDR COMA9810023](https://openairdocs.org/sdr/COMA9810023.md): Bearing · worn · Jan 13, 1998 · N263CA · Emb EMB120RT · Propeller Blade Section
  > DURING PROPELLER DYNAMIC BALANCING PROCEDURES, IT WAS DETERMINED THAT THE PROPELLER COULD NOT BE BALANCED. FURTHER INSPECTION OF PROPELLER FOUND NR 2 BLADE TO BE EXCESSIVELY LOOSE. FURTHER INSPECTION FOUND BLADE PIN BEARING TO BE WORN TO 0.080 WALL THICKNESS
- [SDR COMA9710507](https://openairdocs.org/sdr/COMA9710507.md): Circuit Breaker · tripped · Dec 26, 1997 · N263CA · Emb EMB120RT · Central Warning
  > TRIM WARNING DURING TAKEOFF. AURAL WARNING CIRCUIT BREAKER WAS TRIPPED. RESET BREAKER AND SYSTEM TEST NORMAL.
- [SDR COMA9710504](https://openairdocs.org/sdr/COMA9710504.md): Lamp · failed · Dec 19, 1997 · N263CA · Emb EMB120RT · Emergency Lighting
  > LEFT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LAMP.
- [SDR COMA9710482](https://openairdocs.org/sdr/COMA9710482.md): Seal · leaking · Nov 19, 1997 · N263CA · Emb EMB120RT · Turbine Engine Accessory Drive
  > LEFT ENGINE OIL PRESSURE DECREASED TO 40 PSI DURING FLIGHT (IFSD). REPLACED THE START/GENERATOR DRIVE OIL SEAL.
- [SDR COMA9710214](https://openairdocs.org/sdr/COMA9710214.md): Latch · broken · Apr 3, 1997 · N263CA · Emb EMB120RT · Landing Gear Door Retract Section
  > THE RIGHT MLG OPENED DURING FLIGHT. REPLACED BROKEN RIGHT MLG OUTBD DOOR LATCH ASSEMBLY.
- [SDR COMA9710073](https://openairdocs.org/sdr/COMA9710073.md): Pitchlock Screw · damaged · Jan 23, 1997 · N263CA · Emb EMB120RT · Propeller Controlling System
  > ACTUATOR ASSEMBLY REMOVED ORIGINALLY FOR MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION, THE FEATHER STOP TAB (S/N S0328) WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER.
- [SDR COMA9710042](https://openairdocs.org/sdr/COMA9710042.md): Pcu · inoperative · Jan 16, 1997 · N263CA · Emb EMB120RT · Propeller Controlling System
  > RIGHT PROPELLER WENT TO 103.7 PERCENT RPM ON TAKEOFF. REPLACED RIGHT PROPELLER PCU.
- [SDR COMA9610408](https://openairdocs.org/sdr/COMA9610408.md): Hydraulic Hose · loose · Dec 19, 1996 · N263CA · Emb EMB120RT · Hydraulic System, Main
  > LT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO DURING FLIGHT. EMERGENCY FREE FALL SYSTEM WAS USED TO EXTEND LANDING GEAR. TIGHTENED LOOSE HYDRAULIC PUMP HOSE FITTING AT LT NACELLE FIRE DECK.
- [SDR COMA9610390](https://openairdocs.org/sdr/COMA9610390.md): Engine · failed · Dec 11, 1996 · N263CA · Emb EMB120RT · Engine (Turbine/Turboprop)
  > LEFT ENGINE FAILED AT 23,000 FT, SMOKE IN COCKPIT. CAGED ENGINE AND RETURNED TO FIELD. REPLACED LEFT ENGINE.
- [SDR COMA9610330](https://openairdocs.org/sdr/COMA9610330.md): Deice Lead · broken · Nov 13, 1996 · N263CA · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System
  > RIGHT PROPELLER DEICE FAILED. REPLACED ELECTRICAL DEICE LEAD ON RT PROPELLER.
- [SDR COMA9610311](https://openairdocs.org/sdr/COMA9610311.md): Battery · discharged · Oct 23, 1996 · N263CA · Emb EMB120RT · Emergency Lighting
  > AFT EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY BATTERY.
- [SDR COMA9710433](https://openairdocs.org/sdr/COMA9710433.md): Lamp · failed · Oct 20, 1996 · N263CA · Emb EMB120RT · Emergency Lighting
  > THE AFT LAMP OF THE CABIN FLOOR PATH EMERGENCY LIGHTING IS INOP. REPLACED LAMP.
- [SDR COMA9610296](https://openairdocs.org/sdr/COMA9610296.md): Switch · failed · Oct 7, 1996 · N263CA · Emb EMB120RT · Landing Gear Steering System
  > PILOTS PEDAL STEER DISCONNECT SWITCH IS INOP. REPLACED SWITCH.
- [SDR COMA9610232](https://openairdocs.org/sdr/COMA9610232.md): Hinge · broken · Jul 25, 1996 · N263CA · Emb EMB120RT · Landing Gear Doors
  > RIGHT M.L.G. DID NOT RETRACT WHEN LANDING GEAR WAS SELECTED UP. REPLACED BROKEN LANDING GEAR DOOR AFT HINGE, WHICH DID NOT ALLOW ACTUATION OF THE SEQUENCE VALVE.
- [SDR COMA9610092](https://openairdocs.org/sdr/COMA9610092.md): Autofeather Sw · failed · Mar 2, 1996 · N263CA · Emb EMB120RT · Propeller Controlling System
  > AUTOFEATHER SYSTEM DID NOT ARM DURING TAKEOFF. REPLACED THE AUTOFEATHER ARM MICRO SWITCH IN THE POWER LEVER QUADRANT.
- [SDR COMA9610093](https://openairdocs.org/sdr/COMA9610093.md): Actuator · defective · Feb 29, 1996 · N263CA · Emb EMB120RT · Landing Gear Actuator
  > LT MLG INDICATED UNSAFE. LANDING GEAR CYCLED TWICE WITH SAME RESULTS. USED EMERGENCY SYSTEM TO EXTEND LANDING GEAR AND ALL GEAR INDICATED SAFE. REPLACED THE LT MLG HYDRAULIC ACTUATOR.

Next page: https://openairdocs.org/deregistered/N263CA-2006-11-16/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 = 'N263CA' AND deregistration_id = 'N263CA-2006-11-16'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N263CA-2006-11-16/reports

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