# Service difficulty reports: N258CA, cancelled Dec 3, 2012 A list on [N258CA, cancelled Dec 3, 2012](https://openairdocs.org/deregistered/N258CA-2012-12-03.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 · 93 reports - [SDR COMA0110030](https://openairdocs.org/sdr/COMA0110030.md): Channel · cracked · Jan 24, 2001 · N258CA · Emb EMB120RT · Passenger/Crew Doors > DURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE CHANNEL, THIRD FROM BOTTOM, WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES. - [SDR COMA0110029](https://openairdocs.org/sdr/COMA0110029.md): Channel · cracked · Jan 24, 2001 · N258CA · Emb EMB120RT · Passenger/Crew Doors > DURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE LOWER CHANNEL WAS FOUND TO BE CRACKED AT BOTH ENDS. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES. - [SDR COMA0110028](https://openairdocs.org/sdr/COMA0110028.md): Control Cable · worn · Jan 24, 2001 · N258CA · Emb EMB120RT · Rudder Control System > DURING 1C CHECK TASK 27-62, THE RIGHT SIDE OUTBOARD RUDDER CONTROL CABLE WAS FOUND TO BE WORN WHERE IT PASSES THROUGH THE WING BOX FAIRLEADS. THE CABLE WAS REPLACED PER THE AMM. - [SDR COMA0110027](https://openairdocs.org/sdr/COMA0110027.md): Channel · cracked · Jan 24, 2001 · N258CA · Emb EMB120RT · Passenger/Crew Doors > DURING 1C CHECK TASK 52-14, THE PAX DOOR STRUCTURE U-CHANNEL WAS FOUND TO BE CRACKED. THE CHANNEL WAS REPLACED PER SRM STANDARD PRACTICES. - [SDR COMA0110026](https://openairdocs.org/sdr/COMA0110026.md): Angle · cracked · Jan 24, 2001 · N258CA · Emb EMB120RT · Aerodynamic Fairings > DURING 1C CHECK TASK 194-01Z, THE RIGHT OVERWING FAIRING ATTACH ANGLE ON TOP OF THE WING WAS FOUND TO BE CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH AERODESIGN REPORT 1226-21, REV IR, 7/6/99. - [SDR COMA0110006](https://openairdocs.org/sdr/COMA0110006.md): Landing Gear · lack of lube · Jan 7, 2001 · N258CA · Emb EMB120RT · Main Landing Gear > RT MLG INDICATED UNSAFE. CLEANED AND LUBRICATED LANDING GEAR. - [SDR COMA0010373](https://openairdocs.org/sdr/COMA0010373.md): Battery · discharged · Oct 10, 2000 · N258CA · Emb EMB120RT · Emergency Lighting > SEVERAL EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY. - [SDR COMA0010315](https://openairdocs.org/sdr/COMA0010315.md): Pickup · out of adj · Aug 6, 2000 · N258CA · Emb EMB120RT · Propeller Synchronizer Section > RIGHT HAND ENGINE NP OSCILLATING 99 T 102.8 PERCENT. ADJUSTED PROP SYNC. PULSE PICKUP GAPS TO M/M SPECIFICATIONS. - [SDR COMA0010300](https://openairdocs.org/sdr/COMA0010300.md): Tire · discharged · Jul 12, 2000 · N258CA · Emb EMB120RT · Tire Tube > RIGHT HAND MLG TIRE LOW PRESSURE. REPLACED WHEEL TIRE ASSY. - [SDR COMA0010106](https://openairdocs.org/sdr/COMA0010106.md): Lever · malfunctioned · May 16, 2000 · N258CA · Emb EMB120RT · Power Lever > LEFT ENGINE POWER LEVER ADVANCED CAUSING OVER TORQUE AND OVER TEMP. DOWN LOADED DFDR AND FOUND TORQUE AND TEMP EXCEEDENCE TO BE WITHIN M/M LIMITATIONS. - [SDR COMA0010105](https://openairdocs.org/sdr/COMA0010105.md): Door · not closed · May 16, 2000 · N258CA · Emb EMB120RT · Fluid Service Doors > SERVICE DOOR WARNING. FOUND FUEL SERVICE DOOR NOT SECURE. LATCHED DOOR AND AIRCRAFT RETURNED TO SERVICE. - [SDR COMA0010104](https://openairdocs.org/sdr/COMA0010104.md): Warning Light · illuminated · May 14, 2000 · N258CA · Emb EMB120RT · Landing Gear Position and Warning > RIGHT MLG DISAGREE INDICATION DURING EXTENSION. CLEANED AND LUBRICATED LANDING GEAR. A/C RETURNED TO SERVICE. - [SDR COMA0010103](https://openairdocs.org/sdr/COMA0010103.md): Skin · chafed · May 11, 2000 · N258CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5400-432-01I, 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 COMA0010102](https://openairdocs.org/sdr/COMA0010102.md): Skin · chafed · May 11, 2000 · N258CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-01I, THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGE PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99. - [SDR COMA0010101](https://openairdocs.org/sdr/COMA0010101.md): Skin · chafed · May 11, 2000 · N258CA · 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 COMA0010100](https://openairdocs.org/sdr/COMA0010100.md): Fitting · misdrilled · May 11, 2000 · N258CA · Emb EMB120RT · Wing, Landing Gear Attach Fittings > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT WING FRONT OUTBOARD MAIN LANDING GEAR FITTING WAS FOUND TO BE MISDRILLED FROM PREVIOUS REPAIR. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR - [SDR COMA0010099](https://openairdocs.org/sdr/COMA0010099.md): Stringer · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Nacelle/Pylon, Longeron/Stringer > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LT NACELLE OUTBOARD STRINGER NR 1 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3656-1-REV IR, 5-10-00. - [SDR COMA0010098](https://openairdocs.org/sdr/COMA0010098.md): Skin · chafed · May 11, 2000 · N258CA · 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 #3364-1, REV IR, 7-25-99. - [SDR COMA0010097](https://openairdocs.org/sdr/COMA0010097.md): Support Bracket · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5320-141/142-01I, THE FUSELAGE SKIN SUPPORT AT FRAME 21, BETWEEN STRINGERS 21L AND 21R, WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010096](https://openairdocs.org/sdr/COMA0010096.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 163-01Z, THE LT AFT FUSELAGE BUTT STRAP (SILL) WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010095](https://openairdocs.org/sdr/COMA0010095.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 162-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010094](https://openairdocs.org/sdr/COMA0010094.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 161-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010093](https://openairdocs.org/sdr/COMA0010093.md): Support Bracket · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 242-01Z, THE RT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010092](https://openairdocs.org/sdr/COMA0010092.md): Support Bracket · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 232-01Z, THE RT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010091](https://openairdocs.org/sdr/COMA0010091.md): Threshold · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FUSELAGE FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010090](https://openairdocs.org/sdr/COMA0010090.md): Threshold · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE FUSLAGE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010089](https://openairdocs.org/sdr/COMA0010089.md): Threshold · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE RT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010088](https://openairdocs.org/sdr/COMA0010088.md): Threshold · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010087](https://openairdocs.org/sdr/COMA0010087.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010086](https://openairdocs.org/sdr/COMA0010086.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 152-01Z, THE RT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010085](https://openairdocs.org/sdr/COMA0010085.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 142-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010083](https://openairdocs.org/sdr/COMA0010083.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 142-01Z, THE RT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010082](https://openairdocs.org/sdr/COMA0010082.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RT FWD FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010081](https://openairdocs.org/sdr/COMA0010081.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 151-01Z, THE LT FUSELAGE FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010080](https://openairdocs.org/sdr/COMA0010080.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL MANUAL STANDARD PRACTICES. - [SDR COMA0010079](https://openairdocs.org/sdr/COMA0010079.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010078](https://openairdocs.org/sdr/COMA0010078.md): Strap · corroded · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LT FWD FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010077](https://openairdocs.org/sdr/COMA0010077.md): Support Bracket · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 232-01Z, THE FUSELAGE RT SKIN SUPPORT AT FRAME 13A AND 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, - [SDR COMA0010076](https://openairdocs.org/sdr/COMA0010076.md): Support Bracket · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 222-01Z, THE RT FUSELAGE SKIN SUPPORT AT FRAME 9 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR STANDARD PRACTICES AND AERODESIGN REPORT NR 660-1, REV IR, 2-16-93. - [SDR COMA0010075](https://openairdocs.org/sdr/COMA0010075.md): Floorbeam · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LT COCKPIT FLOOR SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR EST-145-/96. - [SDR COMA0010074](https://openairdocs.org/sdr/COMA0010074.md): Support Bracket · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 231-01Z, WHILE GAINING ACCESS THE LT COCKPIT SKIN SUPPORT BRACKET BEHIND TO DV WINDOW FRAME WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010073](https://openairdocs.org/sdr/COMA0010073.md): Floorbeam · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE RT COCKPIT FLOOR SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR EST-145/96. - [SDR COMA0010072](https://openairdocs.org/sdr/COMA0010072.md): Angle · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Wing Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-02I, THE RT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 194 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-13, REV IR, 2- - [SDR COMA0010071](https://openairdocs.org/sdr/COMA0010071.md): Angle · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Wing Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-02I, THE LT WING UPPER SKIN ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1226-13 REV IR, 2-7 - [SDR COMA0010070](https://openairdocs.org/sdr/COMA0010070.md): Bracket · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 25-12, WHILE ACQUIRING ACCESS THE CARGO DOOR TORSION BAR FWD SUPPORT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 1397-1, - [SDR COMA0010069](https://openairdocs.org/sdr/COMA0010069.md): Support Bracket · cracked · May 11, 2000 · N258CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 261-01Z, THE FUSELAGE SKIN SUPPORT BRACKET AT FRAME 40, BETWEEN STRINGERS 3L AND 4L, WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010068](https://openairdocs.org/sdr/COMA0010068.md): Skin · gouged · May 11, 2000 · N258CA · Emb EMB120RT · Cargo/Baggage Doors > UPON COMPLIANCE OF 2C INSPECTION TASK 813-022, 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 PG 201-204. - [SDR COMA0010045](https://openairdocs.org/sdr/COMA0010045.md): Selector Knob · contaminated · Mar 24, 2000 · N258CA · Emb EMB120RT · Trailing Edge Flap Control System > FLAPS FAILED AT 25 DEGREES WHEN SELECTED TO 45 DEGREES FOR LANDING. REMOVED DEBRIS FROM FLAP SELECTOR FLAP, OPERATION NORMAL. - [SDR COMA0010036](https://openairdocs.org/sdr/COMA0010036.md): Sensor · malfunctioned · Mar 9, 2000 · N258CA · Emb EMB120RT · Landing Gear Retraction/Extension System > NLG WOULD NOT RETRACT. REPLACED THE NLG DOWN LOCK SWITCH. - [SDR COMA9910188](https://openairdocs.org/sdr/COMA9910188.md): Sign · inoperative · Dec 16, 1999 · N258CA · Emb EMB120RT · Emergency Lighting > EXIT SIGN AT ROW 5 WAS INOPERATIVE. REPLACED EXIT SIGN. Next page: https://openairdocs.org/deregistered/N258CA-2012-12-03/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 = 'N258CA' AND deregistration_id = 'N258CA-2012-12-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N258CA-2012-12-03/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.