# Service difficulty reports: N261CA, cancelled May 5, 2006 A list on [N261CA, cancelled May 5, 2006](https://openairdocs.org/deregistered/N261CA-2006-05-05.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 · 70 reports - [SDR COMA0010316](https://openairdocs.org/sdr/COMA0010316.md): Pump · leaking · Aug 15, 2000 · N261CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), Main > GREEN HYDRAULIC SYSTEM LOST ALL FLUID. REPLACED THE LEFT ENGINE HYDRAULIC PUMP. - [SDR COMA0010302](https://openairdocs.org/sdr/COMA0010302.md): Sensor · malfunctioned · Jul 19, 2000 · N261CA · Emb EMB120RT · Elevator Control System > TAKEOFF TRIM AURAL WARNING. REPLACED ELEVATOR TRIM TAB PROXIMITY SENSOR. - [SDR COMA0010200](https://openairdocs.org/sdr/COMA0010200.md): Skin · chafed · Jun 14, 2000 · N261CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF2C INSPECTION TASK 5410-432-04I, THE LEFT 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 COMA0010199](https://openairdocs.org/sdr/COMA0010199.md): Skin · chafed · Jun 14, 2000 · N261CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE LEFT 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 COMA0010198](https://openairdocs.org/sdr/COMA0010198.md): Skin · gouged · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 192-01Z, THE RIGHT FUSELAGE SKIN AT STRINGER 17R, 3 INCHES FORWARD OF FRAME 24 WAS FOUND TO BE GOUGED BY THE DEICE PRESSURE REGULATOR. THE DAMAGED PART WAS REPAIRED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES - [SDR COMA0010197](https://openairdocs.org/sdr/COMA0010197.md): Floor Support · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE FUSELAGE LEFT SIDE FRAME 13 FLOOR PROP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00. - [SDR COMA0010196](https://openairdocs.org/sdr/COMA0010196.md): Floor Support · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE FUSELAGE RIGHT SIDE FRAME 13 FLOOR PROP WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3647-1, REV IR, 5-3-00. - [SDR COMA0010195](https://openairdocs.org/sdr/COMA0010195.md): Shear Tie · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 261-01Z, THE FUSELAGE FRAME 40 SKIN SUPPORT BETWEEN STRINGERS 3L AND 4L WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010194](https://openairdocs.org/sdr/COMA0010194.md): Shear Tie · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE SKIN SUPPORT BEHIND CAPTAIN''S DV WINDOW FRAME WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010193](https://openairdocs.org/sdr/COMA0010193.md): Skin · gouged · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE LOWER RIGHT FUSELAGE SKIN JUST UNDER THE LAV DUMP VALVE DOUBLER WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 53-00- - [SDR COMA0010192](https://openairdocs.org/sdr/COMA0010192.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-142-03I, THE RIGHT HAND FLOORBEAM BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 2174-1, REV IR, 1-15-97. - [SDR COMA0010191](https://openairdocs.org/sdr/COMA0010191.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-141-03I, THE LEFT HAND FLOORBEAM BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 2174-1, REV IR, 1-15-97. - [SDR COMA0010190](https://openairdocs.org/sdr/COMA0010190.md): Threshold · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-141-03I, THE LEFT HAND FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010189](https://openairdocs.org/sdr/COMA0010189.md): Threshold · gouged · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 164-01Z, THE AFT RIGHT HAND CARGO FLOOR SILL WAS FOUND TO BE DAMAGED BY AN INTERIOR LINING SCREW. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-1, REV I - [SDR COMA0010188](https://openairdocs.org/sdr/COMA0010188.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD FLOOR SUPPORT RIGHT HAND BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL MANUAL STANDARD PRACTICES. - [SDR COMA0010187](https://openairdocs.org/sdr/COMA0010187.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LEFT HAND FLOOR BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010186](https://openairdocs.org/sdr/COMA0010186.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LEFT HAND FLOOR 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 COMA0010185](https://openairdocs.org/sdr/COMA0010185.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE FORWARD CABIN CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT 1671-1, REV A, 1-28-97. - [SDR COMA0010184](https://openairdocs.org/sdr/COMA0010184.md): Threshold · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD RIGHT HAND CABIN FLOOR SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010183](https://openairdocs.org/sdr/COMA0010183.md): Floorbeam · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD LT FLOOR CROSSBEAM AT FRAME 15 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010182](https://openairdocs.org/sdr/COMA0010182.md): Floorbeam · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE FORWARD RT FLOOR CROSSBEAM AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010181](https://openairdocs.org/sdr/COMA0010181.md): Floorbeam · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LEFT HAND FLOOR CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010180](https://openairdocs.org/sdr/COMA0010180.md): Floorbeam · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RIGHT HAND FLOOR CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STURCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010179](https://openairdocs.org/sdr/COMA0010179.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE FORWARD CABIN FLOOR CENTER BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010178](https://openairdocs.org/sdr/COMA0010178.md): Floorbeam · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FORWARD CABIN FLOOR LEFT HAND CROSSBEAM AT FRAME 14 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010177](https://openairdocs.org/sdr/COMA0010177.md): Frame · gouged · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Frame > UPON COMPLIANCE OF 2C INSPECTION TASK 263/264-01Z, THE FUSELAGE FRAME 46A WAS FOUND TO BE GOUGED BY INTERIOR LINING SCREWS IN TWO PLACES. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010176](https://openairdocs.org/sdr/COMA0010176.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z, THE CARGO COMPARTMENT ENTRYWAY FLOOR BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3661-3, REV IR, 6-12-00. - [SDR COMA0010175](https://openairdocs.org/sdr/COMA0010175.md): Frame · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Frame > UPON COMPLIANCE OF 2C INSPECTION TASK 161/162-01Z, THE FUSELAGE FRAME 42 CHANNEL AT 6 O''CLOCK WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3674-3, REV IR, 6-12-00. - [SDR COMA0010174](https://openairdocs.org/sdr/COMA0010174.md): Crossbeam · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-01I, THE FRAME 12 CROSSBEAM AT COCKPIT ENTRANCE FLOOR WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010173](https://openairdocs.org/sdr/COMA0010173.md): Strap · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 163-012Z, THE AFT LEFT HAND CARGO FLOOR SILL 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, 5-15-00. - [SDR COMA0010172](https://openairdocs.org/sdr/COMA0010172.md): Intercostal · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE 2C INSPECTION TASK 5310-221-05I, THE LEFT HAND COCKPIT OVERHEAD INTERCOSTAL WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010171](https://openairdocs.org/sdr/COMA0010171.md): Floorbeam · corroded · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE FUSELAGE FLOOR T-SECTION OF FRAME 16 LT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010170](https://openairdocs.org/sdr/COMA0010170.md): Angle · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Wing Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-01I, THE LEFT WING UPPER SURFACE ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, REV IR, 7-6- - [SDR COMA0010169](https://openairdocs.org/sdr/COMA0010169.md): Angle · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Wing Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-01I, THE RIGHT WING UPPER SURFACE ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-21, REV - [SDR COMA0010168](https://openairdocs.org/sdr/COMA0010168.md): Skin · gouged · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE RIGHT HAND FORWARD LOWER FUSELAGE SKIN AT STRINGER 17R WAS FOUND TO BE GOUGED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT N - [SDR COMA0010167](https://openairdocs.org/sdr/COMA0010167.md): Shear Tie · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE FUSELAGE FRAME 9 SKIN SUPPORT JUST BELOW CAPTAIN''S DV WINDOW WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1 - [SDR COMA0010166](https://openairdocs.org/sdr/COMA0010166.md): Shear Tie · cracked · Jun 14, 2000 · N261CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-022-05I, THE FUSELAGE FRAME 9 SKIN SUPPORT JUST BELOW F/O''S DV WINDOW WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, RE - [SDR COMA0010165](https://openairdocs.org/sdr/COMA0010165.md): Skin · gouged · Jun 14, 2000 · N261CA · Emb EMB120RT · Cargo/Baggage Doors > UPON COMPLIANCE OF 2C INSPECTION TASK 813-02Z, THE CARGO DOOR SKIN AND PREVIOUS REPAIR DOUBLER 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 COMA0010164](https://openairdocs.org/sdr/COMA0010164.md): Skin · delaminated · Jun 14, 2000 · N261CA · Emb EMB120RT · Trailing Edge Flaps > UPON COMPLIANCE OF 2C INSPECTION TASK 612-01Z, THE RIGHT WING OUTBOARD LEADING EDGE WAS FOUND TO BE DELAMINATED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND SRM 57-40-01, FIGURE 201. - [SDR COMA0010163](https://openairdocs.org/sdr/COMA0010163.md): Stringer · cracked · Jun 12, 2000 · N261CA · Emb EMB120RT · Wing, Longeron/Stringer > THE RIGHT WING STRINGER 10 WAS FOUND TO BE CRACKED JUST INBOARD OF RIB 8. THE STRINGER WAS REPAIRED PER EMB120 SRM 57-20-01, FIGURE 201 AND AERODESIGN REPORT NR 3694-1, REV IR, DATED 6-12-00. - [SDR COMA0010025](https://openairdocs.org/sdr/COMA0010025.md): Battery · discharged · Feb 4, 2000 · N261CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES. - [SDR COMA9910197](https://openairdocs.org/sdr/COMA9910197.md): Battery · discharged · Dec 23, 1999 · N261CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS ARE INOPERABLE. REPLACED THE EMERGENCY BATTERIES. - [SDR COMA9910182](https://openairdocs.org/sdr/COMA9910182.md): Air Conditioning · failed · Dec 6, 1999 · N261CA · Emb EMB120RT · Cabin Cooling System > RIGHT AIR CONDITIONING FAILED. COULD NOT DUPLICATE. SYSTEM FUNCTION CHECK NORMAL. - [SDR COMA9910148](https://openairdocs.org/sdr/COMA9910148.md): Switch · out of adjust · Sep 16, 1999 · N261CA · Emb EMB120RT · Door Warning System > SERVICE DOOR WARNING DURING TAKEOFF. ADJUSTED FUEL SERVICE DOOR SWITCH. - [SDR COMA9910115](https://openairdocs.org/sdr/COMA9910115.md): Sign · broken · Jul 19, 1999 · N261CA · Emb EMB120RT · Emergency Lighting > EXIT SIGN AT ROW 8 IS BROKEN. REPLACED SIGN. - [SDR COMA910113](https://openairdocs.org/sdr/COMA910113.md): Warning · activated · Jul 17, 1999 · N261CA · Emb EMB120RT · Central Warning > TRIM INOPERABLE WARNING DURING TAKEOFF. COULD NOT DUPLICATE. RESET SYSTEM AND AIRCRAFT RETURNED TO SERVICE. - [SDR COMA9910103](https://openairdocs.org/sdr/COMA9910103.md): Circuit Breaker · tripped · Jun 28, 1999 · N261CA · Emb EMB120RT · Power Lever > THE FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKERS ARE TRIPPED. RESET BREAKERS AND FUNCTION CHECK OF SYSTEM NORMAL. - [SDR COMA9910092](https://openairdocs.org/sdr/COMA9910092.md): Sign · inoperative · Jun 6, 1999 · N261CA · Emb EMB120RT · Emergency Lighting > EXIT SIGN AT ROW 5 IS INOP. REPLACED EXIT SIGN. - [SDR COMA9910019](https://openairdocs.org/sdr/COMA9910019.md): Warning · activated · Jan 22, 1999 · N261CA · Emb EMB120RT · Propeller Indication System > DURING TAKEOFF ROLL, AUTOFEAHTER AURAL WARNING ACTIVATED. INSPECTED LT AND RT ENGINE SCU FOR CONDITION AND SECURITY. PERFORMED OPERATIONAL CHECK OF THE AUTOFEATHER SYSTEM, NO DEFECTS NOTED. - [SDR COMA9910017](https://openairdocs.org/sdr/COMA9910017.md): Actuator · leaking · Jan 21, 1999 · N261CA · Emb EMB120RT · Landing Gear Actuator > LT MLG DISAGREEMENT INDICATION WHEN LANDING GEAR RETRACTED. REPLACED THE LT MLG RETRACT ACTUATOR. Next page: https://openairdocs.org/deregistered/N261CA-2006-05-05/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 = 'N261CA' AND deregistration_id = 'N261CA-2006-05-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N261CA-2006-05-05/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.