# Service difficulty reports: N168CA, cancelled Mar 1, 2001 A list on [N168CA, cancelled Mar 1, 2001](https://openairdocs.org/deregistered/N168CA-2001-03-01.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 · 71 reports - [SDR COMA9910079](https://openairdocs.org/sdr/COMA9910079.md): Sign · broken · May 12, 1999 · N168CA · Emb EMB120RT · Emergency Lighting > EXIT SIGN DETACHED AT SEAT 5A. REPLACED EXIT SIGN. - [SDR COMA9910076](https://openairdocs.org/sdr/COMA9910076.md): Sensor · failed · May 8, 1999 · N168CA · Emb EMB120RT · Landing Gear Retraction/Extension System > GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED NOSE LANDING GEAR A SYSTEM PROX SENSOR. - [SDR COMA9910014](https://openairdocs.org/sdr/COMA9910014.md): Lamp · failed · Jan 17, 1999 · N168CA · Emb EMB120RT · Emergency Lighting > EMERGENCY FLOOR LIGHT AT CABIN DOOR IS INOPERABLE. REPALCED LIGHT BULB. - [SDR COMA9810291](https://openairdocs.org/sdr/COMA9810291.md): Fitting · failed · Dec 28, 1998 · N168CA · Emb EMB120RT · Turbine Engine Oil System > LEFT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI, IN FLIGHT SHUT DOWN. REPLACED ELBOW FITTING THAT HAD BUCKED OUT ON THE OIL PUMP COVER. - [SDR COMA9810284](https://openairdocs.org/sdr/COMA9810284.md): Support · cracked · Dec 14, 1998 · N168CA · Emb EMB120RT · Wing Miscellaneous Structure > RIGHT WING SKIN SUPPORT NR 37 AT RIB NR 9 CRACKED. REPLACED SKIN SUPPORT. - [SDR COMA9810283](https://openairdocs.org/sdr/COMA9810283.md): Support · cracked · Dec 14, 1998 · N168CA · Emb EMB120RT · Wing Miscellaneous Structure > RIGHT WING SKIN SUPPORT NR 30 AT RIB 6 CRACKED. REPLACED SKIN SUPPORT. - [SDR COMA9810280](https://openairdocs.org/sdr/COMA9810280.md): Stringer · cracked · Dec 14, 1998 · N168CA · Emb EMB120RT · Wing, Longeron/Stringer > RIGHT WING STRINGER NR 10 CRACKED BETWEEN RIBS NR 7 AND NR 8. REPAIRED WITH TWO PIECE DOUBLER. - [SDR COMA9810279](https://openairdocs.org/sdr/COMA9810279.md): Support · cracked · Dec 14, 1998 · N168CA · Emb EMB120RT · Wing Miscellaneous Structure > WING SKIN SUPPORT CRACKED. REPLACED SKIN SUPPORT. - [SDR COMA9810281](https://openairdocs.org/sdr/COMA9810281.md): Support · broken · Dec 12, 1998 · N168CA · Emb EMB120RT · Wing Miscellaneous Structure > DURING FUEL LEAK REPAIR, FOUND SKIN SUPPORT BROKEN IN THE RIGHT WING, RIB 16, BOTTOM CENTER. REPLACED SKIN SUPPORT. - [SDR COMA9810273](https://openairdocs.org/sdr/COMA9810273.md): Window Post · cracked · Nov 27, 1998 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > FOUND CRACK ON POST BETWEEN PILOTS WINDSHIELD AND DV WINDOW. INSTALLED DOUBLER ON WINDOW POST IAW EMB EST-474/95 DATE 01NOV95. - [SDR COMA9810226](https://openairdocs.org/sdr/COMA9810226.md): Sign · broken · Oct 5, 1998 · N168CA · Emb EMB120RT · Emergency Lighting > EXIT SIGN ROW 5 IS BROKEN. REPLACED EXIT SIGN. - [SDR COMA9810189](https://openairdocs.org/sdr/COMA9810189.md): Connector · loose · Sep 9, 1998 · N168CA · Emb EMB120RT · Attitude Gyro and Indicating System > EAD1 AND EHS1 TUBES FAILED DURING TAKEOFF. REPAIRED LOOSE WIRE CONNECTION AT CIRCUIT BREAKER CB0256. - [SDR COMA9810190](https://openairdocs.org/sdr/COMA9810190.md): Deice Indication · malfunctioned · Sep 6, 1998 · N168CA · Emb EMB120RT · Ice Detection > ABNORMAL DEICE, F/O FCP AND FO EFIS TUBE INDICATIONS DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. - [SDR COMA9810184](https://openairdocs.org/sdr/COMA9810184.md): Relay Box · malfunction · Aug 30, 1998 · N168CA · Emb EMB120RT · Landing Gear Retraction/Extension System > LANDING GEAR DID NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX. - [SDR COMA9810114](https://openairdocs.org/sdr/COMA9810114.md): Battery · discharged · May 8, 1998 · N168CA · Emb EMB120RT · Emergency Lighting > EMERGENCY FLOOR PATH LIGHTING VERY DIM. REPLACED EMERGENCY BATTERY. - [SDR COMA9810053](https://openairdocs.org/sdr/COMA9810053.md): Battery · discharged · Mar 3, 1998 · N168CA · Emb EMB120RT · Emergency Lighting > CABIN DOOR EMERGENCY EXIT SIGN IS INOPERABLE, EMERGENCY FLOOR PATH LIGHTING TO ROW 3 IS INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY. - [SDR COMA9710398](https://openairdocs.org/sdr/COMA9710398.md): Tee Section · corroded · Aug 27, 1997 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK REVEALED CORROSION ON FLOOR T-SECTION THAT WAS OUT OF LIMITS. REMOVED CORRODED FLOOR T-SECTION AND INSTALLED SERVICEABLE T-SECTION USING EMB SRM STANDARD PRACTICES. - [SDR COMA9710400](https://openairdocs.org/sdr/COMA9710400.md): Support · corroded · Aug 26, 1997 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-132-01I REVEALED LAV SUPPORT ASSY TO BE HEAVILY CORRODED. REMOVED CORRODED LAV SUPPORT AND INSTALLED SERVICEABLE SUPPORT AS PER EMB 120 MAINTENANCE MANUAL. - [SDR COMA9710399](https://openairdocs.org/sdr/COMA9710399.md): Sill · corroded · Aug 26, 1997 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK REVEALED RIGHT CARGO FLOOR SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES. - [SDR COMA9710397](https://openairdocs.org/sdr/COMA9710397.md): Tee Section · corroded · Aug 26, 1997 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK REVEALED FLOOR T-SECTION AT FRAME 28 TO BE CORRODED. REMOVED T-SECTION AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES. - [SDR COMA9710396](https://openairdocs.org/sdr/COMA9710396.md): Crossbeam · corroded · Aug 26, 1997 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK REVEALED LEFT FLOOR CROSSBEAM TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE PART USING EMB-SRM STANDARD PRACTICES. - [SDR COMA9710395](https://openairdocs.org/sdr/COMA9710395.md): Crossbeam · corroded · Aug 26, 1997 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK REVEALED RIGHT MIDDLE FLOOR CROSSBEAM AT FRAME 23 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB SRM STANDARD PRACTICES. - [SDR COMA9710394](https://openairdocs.org/sdr/COMA9710394.md): Sill · corroded · Aug 26, 1997 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CORROSION ON FLOOR SILL THAT IS BEHIND GALLEY. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES. - [SDR COMA9710225](https://openairdocs.org/sdr/COMA9710225.md): Wire · chafed · Apr 24, 1997 · N168CA · Emb EMB120RT · Overheat Detection > LEFTHAND BLEED AIR DUCT WARNING CAME ON DURING BOARDING. REPAIRED DAMAGED WIRE AT CENTER WING BLEED LEAK DETECTOR. - [SDR COMA9710094](https://openairdocs.org/sdr/COMA9710094.md): Windshield · cracked · Jan 27, 1997 · N168CA · Emb EMB120RT · Flight Compartment Windows > CAPTAIN'S WINDSHIELD CRACKED IN LOWER LEFT CORNER. REPLACED CAPTAIN'S WINDSHIELD. - [SDR COMA9710090](https://openairdocs.org/sdr/COMA9710090.md): Tire · failed · Jan 23, 1997 · N168CA · Emb EMB120RT · Tire Tube > RT INBOARD MAIN TIRE BLEW ON LANDING ROLL ANTI-SKID WARNING SOUNDED. REPLACED RT BRAKE CONTROL VALVE AND RT INBOARD WHEEL AND TIRE ASSY. - [SDR COMA9610388](https://openairdocs.org/sdr/COMA9610388.md): Skin · cracked · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Plate/Skin > DURING 20K LANDING INSPECTION, FOUND ONE FASTENER HOLE CRACK INDICATION ON LEFT WING UPPER SKIN AT RIB NR 11. HOLE WAS REPAIRED PER EMBRAER DOCUMENT EST431/96. - [SDR COMA9610387](https://openairdocs.org/sdr/COMA9610387.md): Sill · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED SEVERE CORROSION ON THE FUSELAGE RIGHT AFT EMERGENCY EXIT CUTOUT LOWER SILL. THE SILL WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES CHAPTER 51. - [SDR COMA9610386](https://openairdocs.org/sdr/COMA9610386.md): Skin · misdrilled · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Plate/Skin > DURING COMPLIANCE OF S/B 120-57-0031, ONE FASTENER HOLE IN THE LEFT WING UPPER SKIN WAS MISDRILLED AT RIB 18. THE HOLE WAS REPAIRED PER EMBRAER DOCUMENT EST 430/96. - [SDR COMA9610385](https://openairdocs.org/sdr/COMA9610385.md): Bracket · cracked · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE LEFT FWD FUSELAGE SKIN SUPPORT BRACKET, AT FRAME 9 TO BE CRACKED. THE BRACKET WAS REPLACED PER AERODESIGN REPORT 660-1. - [SDR COMA9610384](https://openairdocs.org/sdr/COMA9610384.md): Butt Strap · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT LT BUTT STRAP TO BE CORRODED. THE BUTT STRAP WAS REPLACED PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610383](https://openairdocs.org/sdr/COMA9610383.md): Butt Strap · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT CENTER BUTT STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610382](https://openairdocs.org/sdr/COMA9610382.md): Butt Strap · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT RT BUTT STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610381](https://openairdocs.org/sdr/COMA9610381.md): Sill · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT RT SILL CORRODED. THE RT SILL WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610380](https://openairdocs.org/sdr/COMA9610380.md): Support · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT T-SECTION, AT FRAME 16 CORRODED. THE T-SECTION WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610379](https://openairdocs.org/sdr/COMA9610379.md): Stringer · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Main, Longeron/Stringer > INSPECTION REVEALED THE FUSELAGE FWD SECTION OF STRINGER 18L CORRODED. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 1990-A, REV IR, DATED 11-6-96. - [SDR COMA9610378](https://openairdocs.org/sdr/COMA9610378.md): Skin · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Main, Plate/Skin > INSPECTION REVEALED THE LOWER FUSELAGE SKIN CORRODED BENEATH THE NR 2 COM ANTENNA. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 2089-1 REV IR, DATED 11-7-96. - [SDR COMA9610377](https://openairdocs.org/sdr/COMA9610377.md): Support · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE FWD LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB 120 SRM PRACTICES, CHAPTER 51. - [SDR COMA9610376](https://openairdocs.org/sdr/COMA9610376.md): Support · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE CENTER SECTION LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED WITH A NEW PART PER EMB 120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610374](https://openairdocs.org/sdr/COMA9610374.md): Support · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE CENTER SECTION AFT LT SIDEWALL SEAT TRACK SUPPORT CORRODED. THE SUPPORT WAS REPLACED PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610373](https://openairdocs.org/sdr/COMA9610373.md): Crossbeam · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE FLOOR SUPPORT CROSSBEAM AT FRAME 16 CORRODED. THE CROSSBEAM WAS REPLACED WITH A NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610372](https://openairdocs.org/sdr/COMA9610372.md): Butt Strap · corroded · Dec 9, 1996 · N168CA · Emb EMB120RT · Fuselage Miscellaneous Structure > INSPECTION REVEALED THE FUSELAGE FWD FLOOR SUPPORT CENTER BUTT-STRAP CORRODED. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51. - [SDR COMA9610371](https://openairdocs.org/sdr/COMA9610371.md): Support · loose · Dec 9, 1996 · N168CA · Emb EMB120RT · Emergency Exits > INSPECTION REVEALED THE AFT RIGHT EMERGENCY EXIT MECHANISM BELLCRANK SUPPORT MOUNTING RIVETS, THROUGH DOOR SKIN TO BE LOOSE CAUSING EXCESSIVE PLAY IN THE DOOR OPENING MECHANISM. THE RIVETS WERE REPLACED PER EMB120 SRM STANDARD PRACTICES, CHAPTER 51, NO OTHER - [SDR COMA9610370](https://openairdocs.org/sdr/COMA9610370.md): Skin · damaged · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Plate/Skin > DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING LOWER SKIN NR 2 LEFT AND RIGHT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623. - [SDR COMA9610369](https://openairdocs.org/sdr/COMA9610369.md): Skin · damaged · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Plate/Skin > DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING LOWER SKIN NR 1 LEFT AND RIGHT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623. - [SDR COMA9610368](https://openairdocs.org/sdr/COMA9610368.md): Rib · damaged · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing, Rib/Bulkhead > DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING RIB NR 1, CL RIB DAMAGED. REMOVED AND REPLACED IAW EMBRAER ENGINEERING DRAWING 120-44623. - [SDR COMA9610367](https://openairdocs.org/sdr/COMA9610367.md): Spar Cap · damaged · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing Spar > DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR CAPS, LOWER LT AND RT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623. - [SDR COMA9610366](https://openairdocs.org/sdr/COMA9610366.md): Spar Web · damaged · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing Spar > DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING FRONT SPAR WEB LT AND RT DAMAGED. PERFORMED REPAIRS IAW EMBRAER ENGINEERING DRAWING 120-44623. - [SDR COMA9610365](https://openairdocs.org/sdr/COMA9610365.md): Aux Spar Cap · damaged · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing Miscellaneous Structure > DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING AUXILIARY SPAR CAPS, LOWER LT AND RT DAMAGED. PERFORMED REPAIR IAW EMBRAER ENGINEERING DRAWING 120-44623. - [SDR COMA9610364](https://openairdocs.org/sdr/COMA9610364.md): Aux Spar Web · damaged · Dec 9, 1996 · N168CA · Emb EMB120RT · Wing Miscellaneous Structure > DETAILED INSPECTION FOLLOWING GEAR UP LANDING REVEALED THE FOLLOWING DAMAGE: WING AUXILIARY SPAR WEB LT AND RT DAMAGED. PERFORMED REPAIR IAW EMBRAER ENGINEERING DRAWING 120-44623. Next page: https://openairdocs.org/deregistered/N168CA-2001-03-01/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 = 'N168CA' AND deregistration_id = 'N168CA-2001-03-01' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N168CA-2001-03-01/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.