# Service difficulty reports: N156CA, cancelled Sep 6, 2005 A list on [N156CA, cancelled Sep 6, 2005](https://openairdocs.org/deregistered/N156CA-2005-09-06.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 SWIA200110134](https://openairdocs.org/sdr/SWIA200110134.md): Flap Track · dirty · Aug 27, 2001 · N156CA · Emb EMB120RT · Trailing Edge Flaps > ON APPROACH TO OXR, HAD FLAP DISAGREEMENT (INBOARD FLAPS TWO BARS). RETURNED TO LAX.CLEANED FLAP TRACKS. CYCLED FLAPS, COULD NOT DUPLICATE. - [SDR SWIA200110125](https://openairdocs.org/sdr/SWIA200110125.md): Annunciator · malfunctioned · Aug 23, 2001 · N156CA · Emb EMB120RT · Trailing Flap Position Indicating System > FLAPS SET 45 DEGREES ON FINAL, CONTINUITY FAULT ILLUMINATED FOR OUTBOARD PAIR OF FLAPS.REPLACED ANNUNCIATOR/I WITH VERSION II PER MM 27-50-00. OPS CHECK OK ON GROUND TESTS. - [SDR SWIA200110120](https://openairdocs.org/sdr/SWIA200110120.md): Annunciator · malfunctioned · Aug 11, 2001 · N156CA · Emb EMB120RT · Trailing Edge Flap Control System > RECEIVED FLAP CONTROL FAULT WARNING WHEN SELECTING FLAPS TO 15 DEGREES. RESET WAS SUCCESSFUL AFTER PRESSING RESET TWICE.REPLACED FLAP ANNUNCIATOR IAW MM 27-50-05. OPS CHECK GOOD. - [SDR SWIA200110019](https://openairdocs.org/sdr/SWIA200110019.md): Flap Track · defective · Jul 5, 2001 · N156CA · Emb EMB120RT · Trailing Edge Flaps > FLAP DISAGREEMENT AFTER TAKEOFF WHEN MOVING FLAPS FROM 15 DEGREES TO 0 DEGREES. APPEARS TO BE NACELLE FLAPS REPEATEDLY. PERFORMED FLAP INSPECTION AND FLAP TROUBLESHOOTING. REMOVED LEFT INBOARD FLAP. REPLACED ALL ROLLERS IAW 27-50-12 AND REPLACED OUTBOARD T - [SDR SWIA972619](https://openairdocs.org/sdr/SWIA972619.md): Potentiometer · failed · Jun 5, 2001 · N156CA · Emb EMB120RT · Trailing Edge Flap Control System > FLAP DISAGREEMENT LIGHT MOMENTARILY ILLUMINATED AFTER TAKEOFF. FAULT CODE STORED IN MEMORY BANK INDICATED FLAP SELECTOR POTENTIOMETER FAILED. REPLACED FLAP SELECTOR. OPS CHECK GOOD ON GROUND CHECK. P/N: 120-42642-507 S/N ON: 120028R - [SDR SWIA972544](https://openairdocs.org/sdr/SWIA972544.md): Indicator · failed · Apr 30, 2001 · N156CA · Emb EMB120RT · Airspeed/Mach Indicator > HIGH SPEED AURAL WARNING SOUNDED DURING TAKEOFF, RIGHT AFTER POWER LEVERS WERE SET FOR TAKEOFF TORQUE. REPLACED NR 1 AIRSPEED INDICATOR WITH SERVICEABLE UNIT IAW MM 34-12-01. OPS CHECK GOOD. COMPLIED WITH PITOT/STATIC CHECK IAW MM 34-11-00. NO LEAKS NOTED - [SDR SWIA972448](https://openairdocs.org/sdr/SWIA972448.md): Switch · out of adj · Mar 6, 2001 · N156CA · Emb EMB120RT · Door Warning System > CARGO DOOR OPEN INDICATIONS ON CLIMBOUT, RED LIGHT ON MAP AND TRIPLE CHIME. RETURNED TO SEA. ADJUSTED CARGO DOOR MICROSWITCH. OPS CHECK GOOD. - [SDR SWIA972352](https://openairdocs.org/sdr/SWIA972352.md): Pressure Switch · malfunctioned · Feb 10, 2001 · N156CA · Emb EMB120RT · Engine Oil Pressure > OIL PRESSURE RED LIGHT ILLUMINATES AND ORAL WARNING OIL PRESSURE GAUGE FLUCTUATED BETWEEN 45-55. RETURNED TO LAX. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE SWITCH WITH SERVICEABLE SWITCH. PERFORMED ENGINE RUN OIL PRESSURE INDICATION WAS NORMAL WITH NO F - [SDR SWIA972412](https://openairdocs.org/sdr/SWIA972412.md): Warning Light · illuminated · Feb 5, 2001 · N156CA · Emb EMB120RT · Engine Oil Pressure > LEFT OIL PRESSURE LIGHT ILLUMINATED CLIMBING THROUGH 16,500 FEET. FOLLOWED QRH PROCEDURES RETURNED BACK TO SBA. LIGHT EXTINGUISH THEREAFTER. INSPECTED LEFT ENGINE, SERVICED ENGINE OIL, CLEANED CANNON PLUG ON OIL PRESS SWITCH AND RAN ENGINE AT 100 PERCENT TO - [SDR SWIA972263](https://openairdocs.org/sdr/SWIA972263.md): Door · damaged · Jan 12, 2001 · N156CA · Emb EMB120RT · Air Distribution System > IN DESCENT FROM FL240 CABIN FILLED WITH SMOKE. DIVERTED TO PDX. REPLACED LEFT RAM AIR DOOR IAW MM 21-26-01. OPS CHECK GOOD. - [SDR SWIA972208](https://openairdocs.org/sdr/SWIA972208.md): Smoke · detected · Dec 25, 2000 · N156CA · Emb EMB120RT · Air Distribution System > LIGHT SMOKE IN CABIN ON DESCENT TO RDD. RAN MEMORY/FLOW CHECK LIST (NO OXY OR SMOKE GOGGLES), RECIRC/GASPER OFF, THEN RIGHT, THEN LEFT PAC AND STOPPED SMOKE. DID FULL RAMP CHECK OF PACKS, UNABLE TO DUPLICATE. INSPECTED BOTH PACKS AND RAM AIR VALVES FOR DISCR - [SDR SWIA972081](https://openairdocs.org/sdr/SWIA972081.md): Regulator · out of adj · Nov 6, 2000 · N156CA · Emb EMB120RT · Engine Oil Pressure > PILOT REPORTED LOSS OF OIL PRESSURE (DROPPED IN YELLOW BAND) AND LOSS OF POWER (LEFT). DIVERTED TO EUGENE. ADJUSTED OIL PRESSURE REGULATOR PER MM 72-1-50. OPS AND LEAK CHECKS GOOD. REPLACED LEAKING FUEL OIL HEATER PER MM 72-01-40. OPS AND LEAK CHECKS ON - [SDR SWIA971957](https://openairdocs.org/sdr/SWIA971957.md): Control Unit · failed · Sep 5, 2000 · N156CA · Emb EMB120RT · Landing Gear Selector > LANDING GEAR WOULD NOT RETRACT. RETURNED TO SEA. REMOVED AND REPLACED LANDING GEAR CONTROL MODULE IAW MM 32-31-01. P/N ON: 120-38594-501, S/N: 120027, S/N OFF: 120085. - [SDR SWIA971458](https://openairdocs.org/sdr/SWIA971458.md): Tq Indicator · malfunctioned · Apr 9, 1999 · N156CA · Emb EMB120RT · Engine BMEP/Torque Indicating > LARGE RIGHT ENGINE TORQUE FLUCTUATIONS FROM 60 PERCENT TO 84 PERCENT ON CLIMB THROUGH 5000. RETURNED TO PDX. RAN RIGHT ENGINE BUT COULD NOT DUPLICATE PROBLEM. - [SDR SWIA971418](https://openairdocs.org/sdr/SWIA971418.md): Valve · failed · Feb 28, 1999 · N156CA · Emb EMB120RT · Pneumatic Distribution System > EN ROUTE TO CLD LEFT DUCT LEAK LIGHT ILLUMINATED. FOLLOWED QRH AND LIGHT DID NOT EXTINGUISH. SHUT DOWN LEFT ENGINE AND RETURNED TO LAX. RAN AIRCRAFT AND DUPLICATED DISCREPANCY. ISOLATED REGULATOR/RELIEF VALVE AS FAULTY. INSTALLED SERVICEABLE VALVE AND RAN - [SDR SWIA971348](https://openairdocs.org/sdr/SWIA971348.md): O Ring · failed · Dec 28, 1998 · N156CA · Emb EMB120RT · Pneumatic Distribution System > LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH QRH AND RETURNED TO PSP AND CONTACTED MAINTENANCE. FOUND O-RINGS WORN ON COUPLER SLEEVE CAUSING LEFT ENGINE BLEED AIR DUCT TUBE ASSEMBLY TO LEAK AT LEADING EDGE AND AT WING TO FUSEL - [SDR SWIA971343](https://openairdocs.org/sdr/SWIA971343.md): Warning · activated · Dec 22, 1998 · N156CA · Emb EMB120RT · Trailing Flap Position Indicating System > AFTER TAKEOFF, CONTROL FAULT ILLUMINATED. QRH DID NOT CLEAR FAULT. RETURNED FOR LANDING AT SMF. OPERATED FLAPS UP AND DOWN COUPLE OF TIMES, NO DISCREPANCY NOTED. COULD NOT DUPLICATE PROBLEM. - [SDR SWIA971294](https://openairdocs.org/sdr/SWIA971294.md): Ias Indicator · leaking · Oct 21, 1998 · N156CA · Emb EMB120RT · Airspeed/Mach Indicator > ON TAKEOFF, FO'S AIRSPEED, ALTIMETER AND VSI VERY ERRATIC. ALTIMETER AS MUCH AS 1,500 FEET BEHIND CAPTAINS. AIRSPEED INDICATOR 0 KNOTS MOST OF THE TIME. RETURNED TO SEA. COPILOTS IAS INDICATOR HAS A STATIC LEAK. REMOVED AND REPLACED COPILOTS IAS INDICATOR - [SDR SWIA971285](https://openairdocs.org/sdr/SWIA971285.md): Actuator · malfunctioned · Oct 9, 1998 · N156CA · Emb EMB120RT · Landing Gear Actuator > ON APPROACH HAD US DO A GO-AROUND. ON GO-AROUND, NOSE GEAR A AND B REMAINED ON, (NO GROUND LIGHTS). NOSE GEAR WOULD NOT COME UP. REPLACED NOSE GEAR ACTUATOR FOR TROUBLESHOOTING. ALSO, REPLACED BAD ROD-END ASSY. SWUNG GEAR SEVERAL TIMES. ALL CHECKS GOOD. - [SDR SWIA971258](https://openairdocs.org/sdr/SWIA971258.md): Actuator · failed · Sep 9, 1998 · N156CA · Emb EMB120RT · Elevator Tab Control System > IN DESCENT FLIGHT MAP TRIM FAIL AP DISCONNECT. AIRCRAFT PITCHED UP. DIFFICULT TO CONTROL PITCH. TO DESCEND, IT TOOK ALL NOSE DOWN TRIM AND FORWARD YOKE PRESSURE, (AP TRIM SEVO NOT ILLUMINATED WHEN LOOK AT IT). INSPECTED AND FOUND LEFT ELEVATOR TRIM ACTUATO - [SDR SWIA971252](https://openairdocs.org/sdr/SWIA971252.md): Trim Tab · out of position · Sep 9, 1998 · N156CA · Emb EMB120RT · Elevator Tab Control System > DURING DESCENT, AUTO PILOT DISCONNECTED. FOUND TRIM WHEEL AT FORWARD LIMIT AND TRIM INDICATOR AT 1-8 UNITS DOWN. AIRCRAFT SPEED REDUCTION REQUIRED TO REDUCE STICK FORCES TO NORMAL. ACCOMPLISHED ELEVATOR TRIM TAB DEFLECTION CHECK PER MM 27-32-00, TRAVEL WITH - [SDR SWIA971251](https://openairdocs.org/sdr/SWIA971251.md): Control Panel · failed · Sep 9, 1998 · N156CA · Emb EMB120RT · Autopilot System > DURING INITIAL CLIMB AT 1000 FT, ELECTRIC TRIM RAN AWAY FORWARD TO STOP. ROLLED TRIM BACK AND IT RAN FORWARD TO STOP AGAIN, EACH TIME SOUNDING AUTO PILOT AURAL WARNING. THE AUTO PILOT WAS NOT ON AT THE TIME. TRIED TO TURN RIGHT, WAS UNABLE BECAUSE AUTO PILO - [SDR COMA9810040](https://openairdocs.org/sdr/COMA9810040.md): Wire · shorted · Feb 5, 1998 · N156CA · Emb EMB120RT · Light System Wiring > NAVIGATION LIGHTS CIRCUIT BREAKER TRIPPED. REPAIRED SHORTED WIRE RIGHT HAND WING. - [SDR COMA9810034](https://openairdocs.org/sdr/COMA9810034.md): Battery · dischaged · Jan 30, 1998 · N156CA · Emb EMB120RT · Emergency Lighting > EMERGENCY FLOOR LIGHTING IS INOP. REPLACED EMERGENCY BATTERIES. - [SDR COMA9710497](https://openairdocs.org/sdr/COMA9710497.md): Frame · cracked · Dec 12, 1997 · N156CA · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > DURING 1C INSPECTION, TASK 419-012 REVEALED A CRACK IN LEFT NACELLE UPPER HALF-FRAME. REPLACED HALF-FRAME USING AERODESIGN REPORT 2524-2. - [SDR COMA9710496](https://openairdocs.org/sdr/COMA9710496.md): Frame · cracked · Dec 12, 1997 · N156CA · Emb EMB120RT · Nacelle/Pylon, Frame/Spar/Rib > DURING 1C INSPECTION, TASK 419-012 REVEALED A CRACK IN LEFT NACELLE UPPER HALF FRAME. THE CRACK WAS.52 LONG AND STARTED AT A NUTPLATE FASTENER. THE NUTPLATE IS ONE OF FOUR INSTALLED TO ATTACH THE EXHAUST DUCT MOUNT BRACKET. REPAIRED HALF-FRAME USING AERODE - [SDR COMA9710487](https://openairdocs.org/sdr/COMA9710487.md): Sequence Valve · out of adjust · Dec 3, 1997 · N156CA · Emb EMB120RT · Landing Gear Retraction/Extension System > THE RIGHT HAND MLG DOES NOT RETRACT. ADJUSTED THE RIGHT HAND MLG DOORS SEQUENCE VALVES. - [SDR COMA9710308](https://openairdocs.org/sdr/COMA9710308.md): Aural Warning · sounded · Jun 6, 1997 · N156CA · Emb EMB120RT · Central Warning > TAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. TRIM WAS CONFIRMED AT TAKEOFF SETTING. COULD NOT DUPLICATE DISCREPANCY. RESET AURAL WARNING UNIT, SYSTEM TEST NORMAL. - [SDR COMA9710235](https://openairdocs.org/sdr/COMA9710235.md): Blade · delaminated · May 5, 1997 · N156CA · Emb EMB120RT · Propeller Blade Section > PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON FURTHER INSPECTION, THE NR 3 BLADE WAS FOUND TO HAVE A DELAMINATION OF 40 SQ INCHES LOCATED ON THE CAMBER SIDE OF THE BLADE AND BEGINNING AT BLADE STATION 38. BLADE WAS REMOVED FROM SERV - [SDR COMA9710234](https://openairdocs.org/sdr/COMA9710234.md): Blade · delaminated · May 5, 1997 · N156CA · Emb EMB120 · Propeller Blade Section > PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON FURTHER INSPECTION, THE NR 2 BLADE WAS FOUND TO HAVE A DELAMINATION OF 74 SQ INCHES LOCATED ON THE CAMBER SIDE OF THE BLADE AND BEGINNING AT BLADE STATION 32. BLADE WAS REMOVED FROM SERV - [SDR COMA9710227](https://openairdocs.org/sdr/COMA9710227.md): Antenna · failed · Apr 30, 1997 · N156CA · Emb EMB120RT · Weather Radar System > WEATHER RADAR DISPLAY INOPERATIVE DURING CLIMB OUT. REPLACED THE WEATHER RADAR ANTENNA. - [SDR COMA9710177](https://openairdocs.org/sdr/COMA9710177.md): Stop Tab · bent · Mar 14, 1997 · N156CA · Emb EMB120RT · Propeller Assembly > PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N 248 WAS FOUND TO BE BENT APPROXIMATELY 0.125. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND HELD FOR PROPOSED FUTURE REPAIR. - [SDR COMA9710176](https://openairdocs.org/sdr/COMA9710176.md): Bearing Insert · worn · Mar 14, 1997 · N156CA · Emb EMB120RT · Propeller Assembly > PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BLADE PIN BEARING INSERT WAS FOUND TO BE WORN IN AN OVAL FASHION. FURTHER INSPECTION SHOWED THAT THE INSERT HAD WORN TO.083 AT THE THINNEST POINT AND.0 - [SDR COMA9710175](https://openairdocs.org/sdr/COMA9710175.md): Bearing Insert · worn · Mar 14, 1997 · N156CA · Emb EMB120RT · Propeller Assembly > PROPELLER ASSEMBLY REMOVED FROM AIRCRAFT FOR HUB MAJOR INSPECTION. UPON INITIAL RECEIVING INSPECTION THE BLADE PIN BEARING INSERT WAS FOUND TO BE IN AN OVAL FASHION. FURTHER INSPECTION SHOWED THAT THE INSERT HAD WORN TO.082 AT THE THINNEST POINT AND.099 AT - [SDR COMA9710171](https://openairdocs.org/sdr/COMA9710171.md): Antenna · failed · Mar 14, 1997 · N156CA · Emb EMB120RT · Weather Radar System > WEATHER RADAR IS INOP. REPLACED THE RADAR ANTENNA. - [SDR COMA9710168](https://openairdocs.org/sdr/COMA9710168.md): Hydraulic Syst · reqd service · Mar 7, 1997 · N156CA · Emb EMB120RT · Hydraulic System, Main > THE LT (GREEN) HYDRAULIC SYSTEM LOW QUANTITY WARNING WAS ON DURING GEAR RETRACTION. THE RESERVOIR QUANTITY WAS AT THE BOTTOM OF THE GREEN RANGE. SERVICED HYDRAULIC SYSTEM TO FULL LEVEL, SYSTEM OPERATION NORMAL. - [SDR COMA9710077](https://openairdocs.org/sdr/COMA9710077.md): Coupler · inoperative · Jan 21, 1997 · N156CA · Emb EMB120RT · Localizer/VOR System > ILS COURSE MOVES PLUS OR MINUS 1 DOT ON FINAL. REPLACED INBOARD COUPLER, OPERATIONAL CHECK GOOD. - [SDR COMA9710016](https://openairdocs.org/sdr/COMA9710016.md): Filter · clogged · Jan 5, 1997 · N156CA · Emb EMB120RT · Engine Fuel Distribution > FUEL FILTER IMPENDING BYPASS WARNING DURING FLIGHT. REPLACED RT ENGINE FUEL FILTERS. - [SDR COMA9610403](https://openairdocs.org/sdr/COMA9610403.md): Separator · cracked · Dec 16, 1996 · N156CA · Emb EMB120RT · Airfoil Anti/De-ice System > WING AND STABILIZER INBD DE-ICE BOOTS ARE INOP. REPLACED A CRACKED BLEED AIR WATER SEPARATOR. - [SDR COMA9610355](https://openairdocs.org/sdr/COMA9610355.md): Skin · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Main, Plate/Skin > DURING 2C INSPECTION, FOUND FUSELAGE INNER SKIN FOUND CORRODED AT PAX DOOR CUTOUT, BENEATH BOTTOM FWD DOOR CUTOUT REINFORCEMENT DOUBLER. THE DAMGE WAS REPAIRED PER AERODESIGN REPORT NR 2118-1, REV IR, DATED 12-3-96. - [SDR COMA9610354](https://openairdocs.org/sdr/COMA9610354.md): Sill · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR STRUCTURE RT SILL CORRODED. REPLACED SILL WITH NEW PART PER EMB120 SRM STANDARD PRACTICES CHAPTER 51. - [SDR COMA9610353](https://openairdocs.org/sdr/COMA9610353.md): Butt Strap · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR STRUCTURE RT BUTT STRAP CORRODED. REPLACED BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610352](https://openairdocs.org/sdr/COMA9610352.md): Butt Strap · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FUSELAGE FWD CENTER FLOOR SUPPORT STRUCTURE BUTT STRAP CORRODED. REPLACED CENTER BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610351](https://openairdocs.org/sdr/COMA9610351.md): Butt Strap · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FWD FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT STRAP CORRODED. REPLACED LT BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610350](https://openairdocs.org/sdr/COMA9610350.md): Crossbeam · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT LT CROSSBEAM CORRODED. REPLACED CROSSBEAM WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610349](https://openairdocs.org/sdr/COMA9610349.md): Sill · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT SILL CORRODED. REPLACED LT SILL PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610348](https://openairdocs.org/sdr/COMA9610348.md): Butt Strap · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE LT BUTT STRAP CORRODED. REPLACED LT BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51 AND AERODESIGN REPORT 31671-2, REV IR, DATED 12-4-96. - [SDR COMA9610347](https://openairdocs.org/sdr/COMA9610347.md): Stringer · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Main, Longeron/Stringer > DURING 2C INSPECTION, FOUND FUSELAGE STRINGER 18L CORRODED AT FWD END, FS 4088.0. REPAIRED STRINGER PER AERODESIGN REPORT NR 1990-2, REV IR DATED 9-15-96. - [SDR COMA9610346](https://openairdocs.org/sdr/COMA9610346.md): Crossbeam · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FUSELAGE FLOOR SUPPORT RT CROSSBEAM AT FRAME 16 HAD CORROSION. REPLACED RT CROSSBEAM WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610345](https://openairdocs.org/sdr/COMA9610345.md): Butt Strap · corroded · Dec 9, 1996 · N156CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, FOUND FUSELAGE FWD FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP CORRODED. REPLACED CENTER BUTT STRAP WITH NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. Next page: https://openairdocs.org/deregistered/N156CA-2005-09-06/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 = 'N156CA' AND deregistration_id = 'N156CA-2005-09-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N156CA-2005-09-06/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.