# Service difficulty reports: N266CA, cancelled Aug 21, 2012

A list on [N266CA, cancelled Aug 21, 2012](https://openairdocs.org/deregistered/N266CA-2012-08-21.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 · 59 reports

- [SDR COMA0110040](https://openairdocs.org/sdr/COMA0110040.md): Battery · discharged · Mar 6, 2001 · N266CA · Emb EMB120RT · Emergency Lighting
  > AFT CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY.
- [SDR COMA0110002](https://openairdocs.org/sdr/COMA0110002.md): Relay · malfunctioned · Dec 28, 2000 · N266CA · Emb EMB120RT · Landing Gear Position and Warning
  > AFTER GEAR RETRACTION, HYDRAULIC LOW LEVEL WARNING. GEAR DOORS DID NOT CLOSE. REPLACED THE LANDING GEAR RELAY BOX.
- [SDR COMA0010304](https://openairdocs.org/sdr/COMA0010304.md): Skin · gouged · Jul 14, 2000 · N266CA · Emb EMB120RT · Fuselage Main, Plate/Skin
  > UPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-C01E, THE FUSELAGE RT LOWER SKIN BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-
- [SDR COMA0010277](https://openairdocs.org/sdr/COMA0010277.md): Skin · gouged · Jul 14, 2000 · N266CA · Emb EMB120RT · Fuselage Main, Plate/Skin
  > UPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-CO1E, THE FUSELAGE RT LOWER SKIN BELOW LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR NR SST-
- [SDR COMA0060457](https://openairdocs.org/sdr/COMA0060457.md): Battery · discharged · May 25, 2000 · N266CA · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHT BATTERY.
- [SDR COMA0010107](https://openairdocs.org/sdr/COMA0010107.md): Adi · malfunctioned · May 20, 2000 · N266CA · Emb EMB120RT · Attitude and Direction Data System
  > NR 1 ADI FLICKERING. REPLACED THE NR 1 ADI.
- [SDR COMA0010039](https://openairdocs.org/sdr/COMA0010039.md): Radar · malfunctioned · Mar 16, 2000 · N266CA · Emb EMB120RT · Weather Radar System
  > RADAR SPOKING DURING SWEEPS. REPLACED THE WX RADAR RT WXT-25013.
- [SDR COMA9910171](https://openairdocs.org/sdr/COMA9910171.md): Mechanism · lack of lube · Nov 4, 1999 · N266CA · Emb EMB120RT · Passenger/Crew Doors
  > DOOR WARNING DURING FLIGHT. CLEANED AND LUBED DOOR MECHANISM.
- [SDR COMA9910156](https://openairdocs.org/sdr/COMA9910156.md): Switches · dirty · Oct 3, 1999 · N266CA · Emb EMB120RT · Door Warning System
  > AFTER DEPARTURE FROM LAN, THE CABIN DOOR WARNING CAUTION ACTIVATED ON MAP. AIRCRAFT RETURNED TO THE FIELD. CLEANED ALL CABIN DOOR MICROSWITCHES, OPERATIONAL CHECK INDICATED CABIN DOOR INDICATING SYSTEM SATISFACTORY.
- [SDR COMA9910118](https://openairdocs.org/sdr/COMA9910118.md): Door · not closed · Jul 25, 1999 · N266CA · Emb EMB120RT · Fluid Service Doors
  > SERVICE DOOR WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT COMPLETELY CLOSED. SECURED FUEL SERVICE DOOR.
- [SDR COA9910095](https://openairdocs.org/sdr/COA9910095.md): Sign · broken · Jun 17, 1999 · N266CA · Emb EMB120RT · Emergency Lighting
  > EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN.
- [SDR COMA9910051](https://openairdocs.org/sdr/COMA9910051.md): Handle · broken · Mar 31, 1999 · N266CA · Emb EMB120RT · Landing Gear Doors
  > LEFT MAIN LANDING GEAR DOOR WILL NOT CLOSE. REPLACED GEAR DOOR HANDLE.
- [SDR COMA9810255](https://openairdocs.org/sdr/COMA9810255.md): Battery · discharged · Nov 4, 1998 · N266CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHTING IS WEAK. REPLACED EMERGENCY BATTERY.
- [SDR COMA9810227](https://openairdocs.org/sdr/COMA9810227.md): Engine · malfunctioned · Oct 5, 1998 · N266CA · Emb EMB120RT · Engine (Turbine/Turboprop)
  > RIGHT HAND ENGINE NP WAS 104 PERCENT AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. GROUND RUNS AND FLIGHT CHECK WERE SATISFACTORY.
- [SDR COMA9810178](https://openairdocs.org/sdr/COMA9810178.md): Ahrs · malfunction · Aug 14, 1998 · N266CA · Emb EMB120RT · Integrated Flight System
  > ATTITUDE DISPLAY WARNING DURING TAKEOFF. REPLACED THE NR 1 AHRS.
- [SDR COMA9810161](https://openairdocs.org/sdr/COMA9810161.md): Battery · discharged · Jul 19, 1998 · N266CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY LIGHTS ROW 1 AND 2 ARE INOPERABLE. REPLACED EMERGENCY BATTERY.
- [SDR COMA9810149](https://openairdocs.org/sdr/COMA9810149.md): Sign · broken · Jun 28, 1998 · N266CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY EXIT SIGN AT ROW 5 BROKEN. REPLACED SIGN.
- [SDR COMA9810065](https://openairdocs.org/sdr/COMA9810065.md): Fan · overheated · Mar 14, 1998 · N266CA · Emb EMB120RT · Air Distribution Fan
  > STRONG ELECTRICAL SMELL IN COCKPIT. RIGHT HAND RECIRCULATION FAN CIRCUIT BREAKER TRIPPED. REPLACED THE RIGHT HAND RECIRCULATION FAN.
- [SDR COMA9710509](https://openairdocs.org/sdr/COMA9710509.md): Brush Block · worn · Dec 24, 1997 · N266CA · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System
  > RIGHT HAND PROPELLER DE-ICE FAILED. REPLACED THE BRUSH BLOCK ASSY.
- [SDR COMA9710490](https://openairdocs.org/sdr/COMA9710490.md): Rccb · malfunction · Dec 6, 1997 · N266CA · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice System
  > LEFT HAND PROPELLER DE-ICE FAILED DURING FLIGHT. REPLACED THE LEFT HAND PROPELLER DE-ICE SYSTEM RCCB.
- [SDR COMA9710488](https://openairdocs.org/sdr/COMA9710488.md): Light · loose · Dec 2, 1997 · N266CA · Emb EMB120RT · Emergency Lighting
  > EMERGENCY FLOOR LIGHT AT GALLEY AREA IS LOOSE. SECURED FLOOR LIGHT ASSY.
- [SDR COMA9710435](https://openairdocs.org/sdr/COMA9710435.md): Bracket · cracked · Oct 21, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > UPON REPLACEMENT OF A BROKEN CARGO DOOR LIFTING MECHANISM TORSION BAR, THE TORSION BAR SUPPORT BRACKET BETWEEN FUSELAGE FRAMES 38 AND 39, WAS FOUND TO BE CRACKED. THE BRACKET WAS REPLACED PER AERODESIGN REPORT NR 1397-1, REV IR 2-15-95, AND EMBRAER FAX NR TPE
- [SDR COMA9710417](https://openairdocs.org/sdr/COMA9710417.md): Stator · cracked · Sep 22, 1997 · N266CA · Emb EMB120RT · Brake
  > DURING TEARDOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.
- [SDR COMA9710209](https://openairdocs.org/sdr/COMA9710209.md): Frame · burned · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Main, Frame
  > ON 2C TAS K 313-01Z, FUSELAGE FRAME 52 CANTED FRAME, UPPER HALF, WAS FOUND DAMAGED BY ARCING OF THE APU GENERATOR WIRE TERMINALS BOLTED TO THE FRAME. THE FRAME UPPER HALF WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES AND THE APU FIREWALL WAS REPAIRED PER SR
- [SDR COMA9710208](https://openairdocs.org/sdr/COMA9710208.md): Beam · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-131/132-O1I, THE CABIN DOOR FLOOR SUPPORT FORWARD CENTER OMEGA BEAM WAS FOUND DAMAGED IN THREE PLACES, 1) CORROSION, 2) SMALL CRACK, 3) HOLE CAUSED BY CARPET TRIM SCREW IMPROPERLY INSTALLED. THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NR
- [SDR COMA9710207](https://openairdocs.org/sdr/COMA9710207.md): Frame · couged · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Main, Frame
  > ON 4C TASK 5330-262-01I, FUSELAGE FRAME 44 WAS FOUND DAMAGED BY CARGO COMPARTMENT LINING SCREWS IMPROPERLY INSTALLED ON RT SIDE. FRAME 44 WAS REPAIRED PER AERODESIGN REPORT NR 2243-1,REV.IR, 3-26-97.
- [SDR COMA9710206](https://openairdocs.org/sdr/COMA9710206.md): Angle · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 4C TASK 5320-152-01I, THE FUSELAGE DOOR FRAME, FOR THE RT AFT EMERGENCY EXIT LOWER ANGLE WAS FOUND CORRODED, WHERE THE EXIT DOOR LOWER GUIDE PIN RECEPTACLES (P/N 120-27743-001) ARE ATTACHED TO IT. THE RECEPTACLES AND THE ANGLE WERE REPLACED PER SRM CHAP 51
- [SDR COMA9710205](https://openairdocs.org/sdr/COMA9710205.md): Butt Strap · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5320-141-03I, THE CABIN FLOORBEAM LT BUTT-STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710204](https://openairdocs.org/sdr/COMA9710204.md): Tee Section · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT T-SECTION OF FRAME 20 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710203](https://openairdocs.org/sdr/COMA9710203.md): Crossbeam · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT CROSSBEAM AT FRAME 20 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710202](https://openairdocs.org/sdr/COMA9710202.md): Sill · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT FORWARD LT SILL WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710200](https://openairdocs.org/sdr/COMA9710200.md): Tee Section · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-131-01I, THE CABIN FLOOR SUPPORT LT T-SECTION AT FRAME 16 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710199](https://openairdocs.org/sdr/COMA9710199.md): Crossbeam · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-132-01I, THE CABIN FLOOR SUPPORT RT CROSSBEAM AT FRAME 16 WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710198](https://openairdocs.org/sdr/COMA9710198.md): Butt Strap · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-132-01I, THE FORWARD RT FLOOR BEAM BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710197](https://openairdocs.org/sdr/COMA9710197.md): Butt Strap · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-131-01I, THE FORWARD LEFT FLOORBEAM BUTT-STRAP, WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710196](https://openairdocs.org/sdr/COMA9710196.md): Butt Strap · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-131/132-01I, THE CABIN FLOORBEAM CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710195](https://openairdocs.org/sdr/COMA9710195.md): Butt Strap · corroded · Mar 27, 1997 · N266CA · Emb EMB120RT · Fuselage Miscellaneous Structure
  > ON 2C TASK 5310-131/132O1I, THE FORWARD CABIN FLOOR SUPPORT CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED PER AERODESIGN REPORT NR 1671-1, REV. A, 1-28-97.
- [SDR COMA9710194](https://openairdocs.org/sdr/COMA9710194.md): Angle · cracked · Mar 27, 1997 · N266CA · Emb EMB120RT · Wing Miscellaneous Structure
  > ON 2C TASK 5720-651-01I, THE RIGHT WING LOWER SKIN SUPPORT ANGLE, AT RIB 16, BETWEEN STRINGERS 8 AND 10, WAS FOUND CRACKED. THE ANGLE WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710193](https://openairdocs.org/sdr/COMA9710193.md): Angle · cracked · Mar 27, 1997 · N266CA · Emb EMB120RT · Wing Miscellaneous Structure
  > ON 2C TASK 5720-622-01I, THE RIGHT WING LOWER SKIN SUPPORT ANGLE WAS FOUND CRACKED AT RIB 8, BETWEEN STRINGERS 10 AND 11. THE ANGLE WAS REPLACED PER SRM CHAP 51 STANDARD PRACTICES.
- [SDR COMA9710157](https://openairdocs.org/sdr/COMA9710157.md): Roller · dirty · Feb 23, 1997 · N266CA · Emb EMB120RT · Trailing Edge Flaps
  > FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKE OFF. REPLACED OUTBOARD FLAP ROLLERS.
- [SDR COMA9710152](https://openairdocs.org/sdr/COMA9710152.md): Switch · malfunction · Feb 14, 1997 · N266CA · Emb EMB120RT · Trailing Edge Flap Control System
  > FLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP SELECTOR HANDLE.
- [SDR COMA9710100](https://openairdocs.org/sdr/COMA9710100.md): Test Panel · malfunction · Feb 2, 1997 · N266CA · Emb EMB120RT · Stall Warning System
  > STALL WARNING ACTIVATED DURING FLIGHT. REPLACED THE STALL TEST PANEL.
- [SDR COMA9610335](https://openairdocs.org/sdr/COMA9610335.md): Sig Cond Unit · malfunction · Nov 21, 1996 · N266CA · Emb EMB120RT · Propeller Controlling System
  > AUTOFEATHER WARNING SOUNDED AFTER TAKEOFF. REPLACED THE RT SIGNAL CONDITIONER UNIT.
- [SDR COMA9610329](https://openairdocs.org/sdr/COMA9610329.md): Sig Cond Unit · malfunction · Nov 8, 1996 · N266CA · Emb EMB120RT · Propeller Controlling System
  > AUTO COARSEN SYSTEM DID NOT ARM DURING TAKEOFF. REPLACED THE SIGNAL CONDITIONER UNIT.
- [SDR COMA9610328](https://openairdocs.org/sdr/COMA9610328.md): Fastener · worn · Nov 8, 1996 · N266CA · Emb EMB120RT · Fluid Service Doors
  > SERVICE DOOR WARNING ON AFTER TAKEOFF. REPLACED LATCHES ON FUEL SINGLE POINT SERVICE DOOR AND SECURED DOOR CLOSED.
- [SDR COMA9610294](https://openairdocs.org/sdr/COMA9610294.md): Relay Box · malfunction · Oct 4, 1996 · N266CA · Emb EMB120RT · Landing Gear Position and Warning
  > LANDING GEAR RETRACTED NORMALLY AND INDICATED UP, BUT THE LANDING GEAR AURAL WARNING SOUNDED CONTINUOUSLY. REPLACED THE LANDING GEAR RELAY BOX.
- [SDR COMA9610287](https://openairdocs.org/sdr/COMA9610287.md): Sequence Valve · malfunction · Sep 25, 1996 · N266CA · Emb EMB120RT · Landing Gear Door Retract Section
  > LANDING GEAR WILL NOT RETRACT. REPLACED LT MLG DOOR SEQUENCE VALVES.
- [SDR COMA9610253](https://openairdocs.org/sdr/COMA9610253.md): Bulb · failed · Aug 21, 1996 · N266CA · Emb EMB120RT · Emergency Lighting
  > LT AFT EMERGENCY LIGHT IS INOP. REPLACED BULB.
- [SDR COMA9610245](https://openairdocs.org/sdr/COMA9610245.md): Pcu · leaking · Aug 8, 1996 · N266CA · Emb EMB120RT · Propeller Controlling System
  > LEFT ENGINE LOW OIL PRESSURE WARNING DURING TAKEOFF. OIL LEAKING FROM LEFT NACELLE.
- [SDR COMA9610229](https://openairdocs.org/sdr/COMA9610229.md): Solenoid · failed · Jul 21, 1996 · N266CA · Emb EMB120RT · Power Lever
  > LEFT POWER LEVER, FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER, TRIPPED. REPLACED THE FLIGHT IDLE STOP SOLENOID.

Next page: https://openairdocs.org/deregistered/N266CA-2012-08-21/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 = 'N266CA' AND deregistration_id = 'N266CA-2012-08-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N266CA-2012-08-21/reports

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