# Service difficulty reports: N205CA, cancelled Feb 11, 2009 A list on [N205CA, cancelled Feb 11, 2009](https://openairdocs.org/deregistered/N205CA-2009-02-11.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR COMA9810180](https://openairdocs.org/sdr/COMA9810180.md): Battery · discharged · Aug 18, 1998 · N205CA · Emb EMB120RT · Emergency Lighting > AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY. - [SDR COMA9810171](https://openairdocs.org/sdr/COMA9810171.md): Door · not latched · Aug 6, 1998 · N205CA · Emb EMB120RT · Fluid Service Doors > SERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED DOOR CLOSED AND AIRCRAFT RETURNED TO SERVICE. - [SDR COMA9810150](https://openairdocs.org/sdr/COMA9810150.md): Switch · dirty · Jul 1, 1998 · N205CA · Emb EMB120RT · Propeller Feathering/Reversing > AUTOFEATHER SYSTEM INOPERABLE DURING TAKEOFF. CLEANED THE AUTOFEATHER ARMING SWITCHES IN POWER LEVER QUADRANT. - [SDR COMA9810120](https://openairdocs.org/sdr/COMA9810120.md): Sign · loose · May 13, 1998 · N205CA · Emb EMB120RT · Emergency Lighting > EXIT SIGN LOOSE AT ROW 5A. REPLACED EXIT SIGN. - [SDR COMA9810108](https://openairdocs.org/sdr/COMA9810108.md): T/O Warning · malfunction · Apr 22, 1998 · N205CA · Emb EMB120RT · Central Warning > 'TRIM' AURAL WARNING DURING TAKEOFF. REPLACED THE AUDIO WARNING UNIT. - [SDR COMA9810078](https://openairdocs.org/sdr/COMA9810078.md): Actuator · malfunctuating · Mar 25, 1998 · N205CA · Emb EMB120RT · Trailing Edge Flap Actuator > OUTBOARD FLAP INDICATION IS FLUCTUATING BETWEEN 2 AND 7 UNITS. COULD NOT DUPLICATE DISCREPANCY. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR FOR TROUBLESHOOTING. - [SDR COMA9810015](https://openairdocs.org/sdr/COMA9810015.md): Crossbeam · corroded · Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > 2C TASK 532D-147-03I REVEALED RIGHT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEABLE PART USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810014](https://openairdocs.org/sdr/COMA9810014.md): Crossbeam · corroded · Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > 2C TASK 151-01Z REVEALED LEFT CROSSBEAM TO BE CORRODED AT FRAME 33. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810009](https://openairdocs.org/sdr/COMA9810009.md): Crossbeam · corroded · Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > 2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 23 TO BE CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810008](https://openairdocs.org/sdr/COMA9810008.md): Crossbeam · corroded · Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810007](https://openairdocs.org/sdr/COMA9810007.md): Crossbeam · corroded · Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810006](https://openairdocs.org/sdr/COMA9810006.md): Sill · corroded · Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CABIN SILL RIGHT TO BE HEAVILY CORRODED. REMOVED CORRODED SILL AND INSTALLED SERVICABLE SILL USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810005](https://openairdocs.org/sdr/COMA9810005.md): Buttstrap · corroded · Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810004](https://openairdocs.org/sdr/COMA9810004.md): Buttstrap · corroded · Jan 7, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CENTER BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810013](https://openairdocs.org/sdr/COMA9810013.md): Crossbeam · corroded · Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > 2C TASK 532D-147-03I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICEBLE PART USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810012](https://openairdocs.org/sdr/COMA9810012.md): Crossbeam · corroded · Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > 2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVICABLE PART USING EMB 120 STANDARD PRACTICES. - [SDR COMA9810011](https://openairdocs.org/sdr/COMA9810011.md): Crossbeam · corroded · Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > 2C TASK 5320-147-03I REVEALED CROSSBEAM (RIGHT) AT FRAME 23 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES. - [SDR COMA9810010](https://openairdocs.org/sdr/COMA9810010.md): Crossbeam · corroded · Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > 2C INSPECTION TASK 5310-131-01I REVEALED THAT THE RIGHT CROSSBEAM AT FRAME 16 WAS CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES. - [SDR COMA9810003](https://openairdocs.org/sdr/COMA9810003.md): Buttstrap · corroded · Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB 120 SRM STANDARD PRACTICES. - [SDR COMA9810002](https://openairdocs.org/sdr/COMA9810002.md): Frame T-Section · corroded · Jan 6, 1998 · N205CA · Emb EMB120RT · Fuselage Main, Frame > DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT MIDDLE T-SECTION AT FRAME 16 TO BE HEAVILY CORRODED. REMOVED CORRODED T-SECTION AND INSTALLED SERVICABLE T-SECTION USING EMB120 SRM STANDARD PRACTICES. - [SDR COMA9710483](https://openairdocs.org/sdr/COMA9710483.md): Solenoid · shorted · Nov 26, 1997 · N205CA · Emb EMB120RT · Passenger Oxygen System > ON 1C TASK 35-09, THE OXYGEN MASKS AT ROW 9 FAILED TO DEPLOY. INVESTIGATION FOUND THE OXYGEN MASK DOOR SOLENOID TO BE SHORTED. THE SOLENOID WAS REPLACED WITH A NEW PART, OK FOR SERVICE. - [SDR COMA9710467](https://openairdocs.org/sdr/COMA9710467.md): Relay Box · malfunctioned · Oct 31, 1997 · N205CA · Emb EMB120RT · Air Distribution System > SMOKE IN COCKPIT AND CABIN AFTER PUSH BACK. FOUND GROUND COOLING FANS NOT OPERATING. REPLACED THE LANDING GEAR RELAY BOX. - [SDR COMA9710333](https://openairdocs.org/sdr/COMA9710333.md): Pcu · damaged · Jul 17, 1997 · N205CA · Emb EMB120RT · Propeller Controlling System > PCU ASSEMBLY REMOVED FROM AIRCRAFT FOR AD 95-22-12 COMPLIANCE. UPON INITIAL RECEIVING INSPECTION SEVERAL OF THE FORWARD PORTION OF THE SPLINES WERE FOUND TO BE GROUND DOWN. PCU WAS REMOVED FROM SERVICE AND RETURNED TO MANUFACTURER FOR FURTHER DISPOSITON. - [SDR COMA9710315](https://openairdocs.org/sdr/COMA9710315.md): Radar Antenna · failed · Jun 17, 1997 · N205CA · Emb EMB120RT · Weather Radar System > WEATHER RADAR DOES NOT WORK. REPLACED THE ANTENNA. - [SDR COMA9710298](https://openairdocs.org/sdr/COMA9710298.md): Actuator · malfunction · May 24, 1997 · N205CA · Emb EMB120RT · Trailing Edge Flap Actuator > FLAP CONTROL FAULT WARNING WITH FLAPS RETRACTED. REPLACED THE LT OUTBOARD FLAP ACTUATOR. - [SDR COMA9710276](https://openairdocs.org/sdr/COMA9710276.md): Skin · bird strike · May 19, 1997 · N205CA · Emb EMB120RT · Fuselage Main, Plate/Skin > BIRD STRIKE ON LOWER FUSELAGE. INSPECTED EXTERIOR OF AIRCRAFT AND FOUND NO EVIDENCE OF BIRD STRIKE. - [SDR COMA9710262](https://openairdocs.org/sdr/COMA9710262.md): Flap Contl Unit · malfunctioned · May 8, 1997 · N205CA · Emb EMB120RT · Trailing Edge Flap Control System > FLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP CONTROL UNIT. - [SDR COMA9610338](https://openairdocs.org/sdr/COMA9610338.md): Deice Boots · worn · Dec 3, 1996 · N205CA · Emb EMB120RT · Airfoil Anti/De-ice System > LT AND RT WING DEICE BOOTS AND LT AND RT ENGINE INLET DEICE BOOTS FAILED DURING FLIGHT. REPLACED WING AND ENGINE INLET DEICE BOOTS. - [SDR COMA9610298](https://openairdocs.org/sdr/COMA9610298.md): Sign · missing · Oct 8, 1996 · N205CA · Emb EMB120RT · Emergency Lighting > EMERGENCY EXIT SIGN AT ROW 5 IS MISSING. REPLACED EMERGENCY EXIT SIGN. - [SDR COMA9610263](https://openairdocs.org/sdr/COMA9610263.md): Flap Contl Unit · malfunction · Aug 27, 1996 · N205CA · Emb EMB120RT · Trailing Edge Flap Control System > FLAP DISAGREE WARNING AFTER TAKEOFF. REPLACED THE FLAP CONTROL UNIT. PART TOTAL CYCLES, 2,052. - [SDR COMA9610158](https://openairdocs.org/sdr/COMA9610158.md): Propeller · leaking · Jun 1, 1996 · N205CA · Emb EMB120RT · Propeller Assembly > LEFT ENGINE LEAKED A LARGE AMOUNT OF OIL DURING TAXI FROM HANGAR TO GATE. REPLACED THE LT PROPELLER ASSY. - [SDR COMA9610137](https://openairdocs.org/sdr/COMA9610137.md): Control Valve · failed · Apr 26, 1996 · N205CA · Emb EMB120RT · Air Intake Anti/De-Ice System > LEFT INLET BOOT FAILED IN-FLIGHT. REPLACED LEFT INLET DEICE EJECTOR VALVE. - [SDR COMA9610116](https://openairdocs.org/sdr/COMA9610116.md): Wire · chafed · Mar 28, 1996 · N205CA · Emb EMB120RT · Hydraulic Power System Wiring > RT HYDRAULIC RESERVOIR LOW PRESSURE INDICATOR ILLUMINATED. REPAIRED CHAFED WIRE AT PRESSURE SWITCH. - [SDR COMA9610095](https://openairdocs.org/sdr/COMA9610095.md): Control Box · malfunction · Mar 7, 1996 · N205CA · Emb EMB120RT · Landing Gear Position and Warning > LANDING GEAR INTRANSIT LIGHTS REMAINED ON WITH GEAR RETRACTED. REPLACED THE LANDING GEAR CONTROL BOX. - [SDR COMA9610084](https://openairdocs.org/sdr/COMA9610084.md): Flap Tracks · dirty · Feb 17, 1996 · N205CA · Emb EMB120RT · Trailing Edge Flap Control System > FLAP DISAGREEMENT WARNING WHEN FLAPS RETRACTED AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. CLEANED AND INSPECTED FLAP TRACKS AND OPERATIONAL CHECK NORMAL. - [SDR COMA9610046](https://openairdocs.org/sdr/COMA9610046.md): Annunciator · defective · Jan 28, 1996 · N205CA · Emb EMB120RT · Trailing Edge Flap Control System > TAKEOFF FLAPS AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE FLAP ANNUNCIATOR UNIT. - [SDR COMA9512035](https://openairdocs.org/sdr/COMA9512035.md): Iva-81a Av · defective · Dec 20, 1995 · N205CA · Emb EMB120RT · Rate of Climb Indicator > THE PILOTS VSI IS COMPLETELY UNUSABLE IN ALL PHASES OF FLIGHT. REPLACED THE PILOTS TCASIVSI. - [SDR COM11936](https://openairdocs.org/sdr/COM11936.md): Tq Sig Cond · defective · Jul 27, 1995 · N205CA · Emb EMB120RT · Propeller Controlling System > LEFT TORQUE INDICATION ERRATIC. LEFT PROPELLER AUTOFEATHERED. REPLACED THE TORQUE SIGNAL CONDITIONER. - [SDR COM11924](https://openairdocs.org/sdr/COM11924.md): Ahrs · defective · Jun 28, 1995 · N205CA · Emb EMB120RT · Integrated Flight System > PILOTS ESHI SHOWS RED FLAG. REPLACED THE NR NR 1 AHRS. - [SDR COM11859](https://openairdocs.org/sdr/COM11859.md): Engine · failed · Apr 13, 1995 · N205CA · Emb EMB120RT · Engine (Turbine/Turboprop) > LEFT ENGINE FAILED ABRUPTLY IN FLIGHT. REMOVED AND REPLACED LEFT ENGINE. - [SDR COM11843](https://openairdocs.org/sdr/COM11843.md): Skin Support · cracked · Mar 30, 1995 · N205CA · Emb EMB120RT · Wing Miscellaneous Structure > THE FOLLOWING P/N WING SKIN SUPPORTS WERE FOUND CRACKED DURING INSPECTION TASK 5720-551/651-01I AND 5720-552/652-01I. THE SKIN SUPPORTS WERE REPLACED IAW AERODESIGN REPORT NR 1327-2. P/N: 120-17056-007, 4 EA; 120-17056-019, 1 EA; 120-17056-013, 1 EA; 120-170 - [SDR COM11838](https://openairdocs.org/sdr/COM11838.md): Sensor · defective · Mar 27, 1995 · N205CA · Emb EMB120RT · Landing Gear Position and Warning > NLG A SYSTEM INTRANSIT LIGHT IS ILLUMINATING INTERMITTENTLY. REPLACED THE NLG DOWNLOCK 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 = 'N205CA' AND deregistration_id = 'N205CA-2009-02-11' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N205CA-2009-02-11/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.