# Service difficulty reports: N259CA, cancelled Oct 17, 2007 A list on [N259CA, cancelled Oct 17, 2007](https://openairdocs.org/deregistered/N259CA-2007-10-17.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 3 · 107 reports - [SDR COMA0210019](https://openairdocs.org/sdr/COMA0210019.md): Brake Assy · failed · May 8, 2002 · N259CA · Emb EMB120RT · Landing Gear Brake System > FLIGHT 5042 ANTI-SKID WARNING DURING T/O ROLL.REPLACED THE L/H INBD BRAKE ASSY. - [SDR COMA0210011](https://openairdocs.org/sdr/COMA0210011.md): Engine · Mar 31, 2002 · N259CA · Emb EMB120RT · Engine (Turbine/Turboprop) > FLIGHT 5057 LT AND RT ENGINES T6 EXCEEDS 800 DEGREES C AT TAKE OFF POWER.C/W LT AND RT ENGINE COMPRESSOR WASH. - [SDR COMA0210009](https://openairdocs.org/sdr/COMA0210009.md): Sensor · malfunctioned · Mar 24, 2002 · N259CA · Emb EMB120RT · Engine BMEP/Torque Indicating > FLIGHT 5029 T6 WARING DURING T/O.REPLACED THE L/H ENGINE TORQUE. - [SDR COMA0210008](https://openairdocs.org/sdr/COMA0210008.md): Control Box · malfunctioned · Feb 23, 2002 · N259CA · Emb EMB120RT · Landing Gear Retraction/Extension System > FLIGHT 5018 L/H MLG DISAGREEMENT WARNING WHEN GEAR RETRACTED.REPLACED THE L/G CONTROL BOX. - [SDR COMA0210007](https://openairdocs.org/sdr/COMA0210007.md): Control Box · malfunctioned · Feb 23, 2002 · N259CA · Emb EMB120RT · Landing Gear Retraction/Extension System > FLIGHT 5061 LANDING GEAR DISAGREEMENT WARNING WHEN GEAR RETRACTED.REPLACED THE L/G CONTROL BOX. - [SDR COMA0110163](https://openairdocs.org/sdr/COMA0110163.md): Eec · malfunctioned · Dec 17, 2001 · N259CA · Emb EMB120RT · Fuel Control/Turbine Engines > FLIGHT 5061 - LEFT ENGINE WILL NOT ACHIEVE REQUIRED TORQUE.REPLACED THE L/H ENGINE EEC. - [SDR COMA0110155](https://openairdocs.org/sdr/COMA0110155.md): Wheel · cracked · Nov 11, 2001 · N259CA · Emb EMB120RT · Wheel/Ski/Float > FLIGHT 5825 DURING PREFLIGHT INSPECTION, THE CREW NOTICED THAT THE RIGHT MAIN INBOARD WHEEL INNER HALF WAS CRACKED AND A PORTION OF THE FLANGE WAS SLIGHTLY PROTRUDING. THE WHEEL FLANGE HAD GOUGED THE LOWER TORQUE-LINK OF THE RIGHT MAIN GEAR.THE WHEEL ASSEMBL - [SDR COMA0110154](https://openairdocs.org/sdr/COMA0110154.md): Cap · Oct 22, 2001 · N259CA · Emb EMB120RT · Engine Oil Pressure > FLIGHT #5057. DURING CRUISE FLIGHT THE RIGHT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI, CREW DECLARED AN EMERGENCY AND PERFORMED AN INFLIGHT SHUT DOWN OF THE RIGHT ENGINE.REPLACED THE RIGHT ENGINE OIL SERVICING FILLER CAP AND NECK. - [SDR COMA0110144](https://openairdocs.org/sdr/COMA0110144.md): Gauge · faulty · Sep 24, 2001 · N259CA · Emb EMB120RT · Propeller Feathering/Reversing > FLIGHT #5062. DURING TAKE OFF FROM NAS THE RIGHT ENGINE PROPELLER AUTO FEATHERED AT 80 KNOTS, ABORTED TAKE OFF AND RETURNED TO THE GATE.REPLACED THE RIGHT ENGINE TORQUE GAUGE. - [SDR COMA0110140](https://openairdocs.org/sdr/COMA0110140.md): Skin · dented · Sep 1, 2001 · N259CA · Emb EMB120RT · Fuselage Main, Plate/Skin > CREW REPORTS DENT ON RIGHT SIDE OF FUSELAGE BETWEEN FRAME 18 AND FRAME 19 AFTER DEBRIS STRUCK RIGHT PROPELLER.DAMAGED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED. WORK DONE IN ACCORDANCE WITH EMBRAER STRUCTURES REPAIR MANUAL CHAPTER 53-0 - [SDR COMA0110041](https://openairdocs.org/sdr/COMA0110041.md): Battery · discharged · Mar 7, 2001 · N259CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS, ROWS 7 TO 10 ARE INOPERABLE. REPLACED THE EMERGENCY BATTERY. - [SDR COMA0110025](https://openairdocs.org/sdr/COMA0110025.md): Control Valve · malfunctioned · Jan 22, 2001 · N259CA · Emb EMB120RT · Air Intake Anti/De-Ice System > LEFT ENGINE INTAKE DEICE IS INOP. REPLACED THE INTAKE EJECTOR VALVE. - [SDR COMA0110024](https://openairdocs.org/sdr/COMA0110024.md): Line · worn · Jan 22, 2001 · N259CA · Emb EMB120RT · Air Intake Anti/De-Ice System > LEFT ENGINE INTAKE DEICE IS INOPERABLE. REPLACED WORN AIR HOSE. - [SDR COMA0010404](https://openairdocs.org/sdr/COMA0010404.md): Light · inoperative · Nov 21, 2000 · N259CA · Emb EMB120RT · Emergency Lighting > EMERGENCY LIGHTS FROM ROW 5 AFT ARE INOP. COULD NOT DUPLICATE. EMERGENCY LIGHTS FUNCTION NORMAL. - [SDR COMA0010210](https://openairdocs.org/sdr/COMA0010210.md): Skin · chafed · Jun 29, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STURCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7/25/99. - [SDR COMA0010242](https://openairdocs.org/sdr/COMA0010242.md): Beam · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CABIN FLOOR SUPPORT FWD CENTER OMEGA BEAM WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #2181-9, IR, 6/23/00. - [SDR COMA0010241](https://openairdocs.org/sdr/COMA0010241.md): Threshold · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RIGHT HAND CABIN FLOOR SUPPORT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010240](https://openairdocs.org/sdr/COMA0010240.md): Strap · gouged · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 163-01Z, THE CARGO COMPARTMENT AFT LT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE GOUGED BY INTERIOR LINING SCREWS. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010239](https://openairdocs.org/sdr/COMA0010239.md): Threshold · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE CABIN FLOOR SUPPORT LT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010238](https://openairdocs.org/sdr/COMA0010238.md): Strap · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE CABIN FLOOR SUPPORT LT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010237](https://openairdocs.org/sdr/COMA0010237.md): Frame · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Frame > UPON COMPLIANCE OF 2C INSPECTION TASK 151/152-01Z, THE FUSELAGE FRAME 38 CHANNEL AT 6 O''CLOCK WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPAIRED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3674-4, IR, 6/24/00. - [SDR COMA0010236](https://openairdocs.org/sdr/COMA0010236.md): Floorbeam · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121/122-O1I, THE CABIN FLOOR SUPPORT CENTER CROSSBEAM AT FRAME 12 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010235](https://openairdocs.org/sdr/COMA0010235.md): Floorbeam · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LEFT HAND CABIN FLOOR SUPPORT CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARED PRACTICES. - [SDR COMA0010234](https://openairdocs.org/sdr/COMA0010234.md): Floorbeam · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 142-01Z, THE RIGHT HAND FLOOR SUPPORT CROSSBEAM AT FRAME 20 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010233](https://openairdocs.org/sdr/COMA0010233.md): Floorbeam · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Floor Beam > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE RIGHT HAND CABIN FLOOR SUPPORT CROSSBEAM AT FRAME 16 WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010232](https://openairdocs.org/sdr/COMA0010232.md): Angle · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE CABIN FLOOR SUPPORT ANGLE UNDER PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3711-1, IR, 6/24/00. - [SDR COMA0010231](https://openairdocs.org/sdr/COMA0010231.md): Angle · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TAXK 131-01Z, THE CABIN FLOOR SUPPORT ANGLE UNDER PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3711-1, IR 6/24/00. - [SDR COMA0010230](https://openairdocs.org/sdr/COMA0010230.md): Strap · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 141-01Z, THE LEFT HAND CABIN FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010229](https://openairdocs.org/sdr/COMA0010229.md): Strap · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE LEFT HAND CABIN FLOOR SUPPORT BUTTSTRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010228](https://openairdocs.org/sdr/COMA0010228.md): Bracket · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 262-01Z, THE CARGO DOOR AFT TRACTS TOP MOUNT BRACKET WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1657-3, IR, 6/12/00. - [SDR COMA0010227](https://openairdocs.org/sdr/COMA0010227.md): Shear Tie · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-O5I, THE FUSELAGE SKIN SUPPORT AT FRAME 9 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #660-1, IR, 2/16/93. - [SDR COMA0010226](https://openairdocs.org/sdr/COMA0010226.md): Shear Tie · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-222-05I, THE RIGHT HAND FUSELAGE SKIN SUPPORT AT FRAME 9 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #660-1, IR, 2/16/93. - [SDR COMA0010225](https://openairdocs.org/sdr/COMA0010225.md): Strap · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 132-01Z, THE CABIN FWD RT FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010224](https://openairdocs.org/sdr/COMA0010224.md): Strap · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CABIN FORWARD CENTER FLOOR SUPPORT BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010223](https://openairdocs.org/sdr/COMA0010223.md): Buttstrap · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131/132-01Z, THE CABIN FLOOR SUPPORT FORWARD CENTER BUTT STRAP WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1671-1, REV A, 1/28/97. - [SDR COMA0010221](https://openairdocs.org/sdr/COMA0010221.md): Threshold · corroded · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 131-01Z, THE CABIN FLOOR SUPPORT FWD LT SILL WAS FOUND TO BE CORRODED. THE DAMAGED PART WAS REPLACED IAW EMB120 STUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010220](https://openairdocs.org/sdr/COMA0010220.md): Angle · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Wing Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5320-244-01I, THE RIGHT WING 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 #1226-21, IR, 7/6/99. - [SDR COMA0010219](https://openairdocs.org/sdr/COMA0010219.md): Skin · gouged · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Plate/Skin > UPON COMPLIANCE OF 2 YEAR CORROSION INSPECTION TASK 5310-132-COIE, THE FUSELAGE SKIN BELOW THE 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 #SST-1569/00 - [SDR COMA0010218](https://openairdocs.org/sdr/COMA0010218.md): Support Bracket · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 232-01Z, 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 #3653-I, IR, 5/6/00. - [SDR COMA0010217](https://openairdocs.org/sdr/COMA0010217.md): Support Bracket · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE FUSELAGE SKIN SUPPORT, COCKPIT OVERHEAD LEFT SIDE WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010216](https://openairdocs.org/sdr/COMA0010216.md): Support Bracket · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Main, Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-221-05I, THE FUSELAGE SKIN SUPPORT BEHIND THE CAPTAIN''S DV WINDOW AS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES. - [SDR COMA0010215](https://openairdocs.org/sdr/COMA0010215.md): Floor Support · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-122-01I, THE RIGHT FLOOR PROP AT FUSELAGE FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3647-1, IR, 5/3/00. - [SDR COMA0010214](https://openairdocs.org/sdr/COMA0010214.md): Floor Support · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Fuselage Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5310-121-01I, THE LEFT FLOOR PROP AT FUSELAGE FRAME 13 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3647-1, IR, 5/3/00. - [SDR COMA0010213](https://openairdocs.org/sdr/COMA0010213.md): Skin · chafed · Jun 28, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RIGHT 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, IR, 7/25/99. - [SDR COMA0010212](https://openairdocs.org/sdr/COMA0010212.md): Skin · chafed · Jun 28, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RIGHT 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 #3364-IR, 7/25/99. - [SDR COMA0010211](https://openairdocs.org/sdr/COMA0010211.md): Skin · chafed · Jun 28, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Plate/Skin > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, 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 #3364-1, IR, 7/25/99. - [SDR COMA0010209](https://openairdocs.org/sdr/COMA0010209.md): Bulkhead · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Nacelle/Pylon, Main Frame > UPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LEFT NACELLE BULKHEAD SUPPORT AT FRAME 14 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3712-1, IR, 6/24/00. - [SDR COMA0010208](https://openairdocs.org/sdr/COMA0010208.md): Angle · cracked · Jun 28, 2000 · N259CA · Emb EMB120RT · Wing Miscellaneous Structure > UPON COMPLIANCE OF 2C INSPECTION TASK 5320-243-01I, THE LEFT WING ATTACH ANGLE FOR FAIRING 193 WAS FOUND TO BE CRACKED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #1226-21, REV IR, 7/6/99. - [SDR COMA0010207](https://openairdocs.org/sdr/COMA0010207.md): Spar Cap · chafed · Jun 28, 2000 · N259CA · Emb EMB120RT · Wing Spar > UPON COMPLIANCE OF 2C INSPECTION TASK 191-01Z, THE LEFT WING AUX SPAR UPPER CAP WAS FOUND TO BE CHAFED BY FAIRING 191. THE DAMAGED PART WAS REPAIRED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND EMBRAER REPAIR #SST-1567-/00. - [SDR COMA0010060](https://openairdocs.org/sdr/COMA0010060.md): Duct · leaking · Apr 27, 2000 · N259CA · Emb EMB120RT · Pneumatic Distribution System > LEFT HAND BLEED AIR DUCT LEAK WARNING. TIGHTENED LOOSE HOSE CLAMPS AT LEFT HAND ACM. Next page: https://openairdocs.org/deregistered/N259CA-2007-10-17/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 = 'N259CA' AND deregistration_id = 'N259CA-2007-10-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N259CA-2007-10-17/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.