# N295SK: 2001 Embraer EMB-135KL, registration cancelled 2017-01-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 18, 2017 - Exported to: Australia - Status when cancelled: Valid registration - Airframe: [Embraer EMB-135KL](https://openairdocs.org/model/embraer-emb-135kl) (registry code 3260302) - Engine: [Rolls-Royce AE3007 series](https://openairdocs.org/engine/rolls-royce-ae3007-series) (registry code 54582) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145513 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 1, 2001 - Certificate issued: December 12, 2016 - Last registry action: December 12, 2016 - Mode S code: A309A7 - Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N295SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=295SK - Page: https://openairdocs.org/deregistered/N295SK-2017-01-18 From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Embraer EMB-135KL: https://openairdocs.org/model/embraer-emb-135kl.md ## Service difficulty reports (41) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA20140908267](https://openairdocs.org/sdr/CHQA20140908267), Sep 8, 2014: TRUNNION. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT MLG FWD UPPER TRUNNION. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-075943A. - [SDR CHQA20140908266](https://openairdocs.org/sdr/CHQA20140908266), Sep 8, 2014: TRUNNION. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE RT MLG UPPER FWD TRUNNION. THE TRUNNION WAS REPAIRED IAW ETD 2014-145-075943A. - [SDR CHQA20140827269](https://openairdocs.org/sdr/CHQA20140827269), Aug 27, 2014: BRACKET. CHAFED. DURING INSPECTION THE LT EMER EXIT DOOR WAS FOUND TO BE CHAFED & BENT ON THE BRACKET ON THE AFT SIDE. THE DOOR WAS REPAIRED IAW ETD 2014-145-073270. - [SDR CHQA20140827260](https://openairdocs.org/sdr/CHQA20140827260), Aug 27, 2014: FITTING. DAMAGED. DURING INSPECTION THE LT AILERON PCA OTBD FITTING WAS FOUND TO HAVE AN ENLARGED HOLE. THE LT AILERON PCA OTBD FITTING WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140826265](https://openairdocs.org/sdr/CHQA20140826265), Aug 26, 2014: BEARING. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE LT MLG UPPER AFT TRUNNION BEARING. THE TRUNNION BEARING WAS REPAIRED IAW ETD 2014-145-075943A. - [SDR CHQA20140824271](https://openairdocs.org/sdr/CHQA20140824271), Aug 24, 2014: SKIN. DENTED. DURING INSPECTION A DENT FROM STRIKE DAMAGE BETWEEN FRAME 70 - 72 & STRINGERS 13 - 14R WAS REPAIRED IAW ETD 2014-145-071479. - [SDR CHQA20140826264](https://openairdocs.org/sdr/CHQA20140826264), Aug 24, 2014: BEARING. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE RT MLG UPPER AFT TRUNNION BEARING. THE TRUNNION BEARING WAS REPAIRED IAW ETD 2014-145-075943. - [SDR CHQA20140822263](https://openairdocs.org/sdr/CHQA20140822263), Aug 22, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140822261](https://openairdocs.org/sdr/CHQA20140822261), Aug 22, 2014: REPAIR. CORRODED. DURING INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM FLOOR FLANGE AT FRAME 20 WAS FOUND TO BE CORRODED. THE FLANGE WAS REPAIRED IAW SRM 53-00-10. - [SDR CHQA20140820270](https://openairdocs.org/sdr/CHQA20140820270), Aug 20, 2014: SKIN. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE SKIN AT FRAME 25 & STRINGERS 20 - 21L. THE SKIN WAS REPAIRED IAW SRM 53-22-01. - [SDR CHQA20140820268](https://openairdocs.org/sdr/CHQA20140820268), Aug 20, 2014: SKIN. DAMAGED. DURING INSPECTION A LIGHTNING STRIKE REPAIR WAS COMPLETED ON NR 1 FRAME 27 - 28 AT STRINGER 21L & FRAME 28 AT STRINGER 18L - 19L. THE REPAIR WAS MADE IAW SRM 53 - [SDR CHQA20140820262](https://openairdocs.org/sdr/CHQA20140820262), Aug 20, 2014: REPAIR. CHAFED. DURING INSPECTION A PREVIOUS REPAIR WAS FOUND TO BE CHAFED BELOW ACCESS DOOR 113EL. THE PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM53-11-01. - [SDR CHQA20130123042](https://openairdocs.org/sdr/CHQA20130123042), Jan 23, 2013: SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON SUPPORT WEB FOR AILERON TORQUE TUBE BETWEEN FRAME 13 AND 14 AND STRINGERS 21R AND 20R. THE AILERON TORQUES TUBE SUPPOR - [SDR CHQA20130123041](https://openairdocs.org/sdr/CHQA20130123041), Jan 23, 2013: FITTING. CRACKED. DURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR CLIP AT FRAME 66 BETWEEN STRINGERS 8L AND 9L. THE DAMAGED SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 53-31 - [SDR CHQA20120309082](https://openairdocs.org/sdr/CHQA20120309082), Mar 9, 2012: SKIN. CRACKED. DURING INSPECTION, THE RIGHT ELEVATOR LEADING EDGE SKIN WAS FOUND TO BE CRACKED AT THE SERVO TAB CONTROL ROD AT STA YH 1310. A HIGH FREQUENCY EDDY CURRENT INSPE - [SDR CHQA20120308081](https://openairdocs.org/sdr/CHQA20120308081), Mar 8, 2012: FRAME. CRACKED. DURING INSPECTION, THE RIGHT FRAME 10 WAS FOUND TO BE CRACKED. THE RIGHT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH - [SDR CHQA20120308080](https://openairdocs.org/sdr/CHQA20120308080), Mar 8, 2012: FRAME. CRACKED. DURING INSPECTION, THE LEFT FRAME 10 WAS FOUND TO BE CRACKED. THE LEFT FRAME 10 WAS REPLACED. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH S - [SDR CHQA20120308079](https://openairdocs.org/sdr/CHQA20120308079), Mar 8, 2012: FRAME. CRACKED. DURING INSPECTION, THE RIGHT FRAME 23, JUST BEHIND THE RIGHT SILL NUMBER 1 WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE RIGHT FRAME 23 JUST BEHIND THE RIGH - [SDR CHQA20120308078](https://openairdocs.org/sdr/CHQA20120308078), Mar 8, 2012: SKIN. GOUGED. DURING INSPECTION, FOUR GOUGES WERE FOUND ON THE LEFT SKIN PANEL BETWEEN FRAME 20 AND FRAME 22 BETWEEN STRINGERS 19L AND 17L. THE LEFT SKIN BETWEEN FRAME 20 AND - [SDR CHQA20120308077](https://openairdocs.org/sdr/CHQA20120308077), Mar 8, 2012: SKIN. DENTED. DURING INSPECTION, MULTIPLE DENTS WERE FOUND ON THE RIGHT SKIN BETWEEN FRAME 3 AND FRAME 4, SIX INCHES ABOVE THE NOSE LANDING GEAR DOOR CUTOUT. A HIGH FREQUENCY - [SDR CHQA201100492](https://openairdocs.org/sdr/CHQA201100492), Dec 18, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT, CEILING AISLE EMERGENCY LIGHT 1 AND COCKPIT FLOOD LIGHT WERE FOUND TO BE INOPERATIVE. MAINTENANCE - [SDR CHQA201100201](https://openairdocs.org/sdr/CHQA201100201), May 30, 2011: SHEAR PLATE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FRAMES BAGGAGE DOOR SHEAR CLIP. THE DAMAGED AREA OF THE SHEAR CLIP WAS REMOVED AND A NEW SECTION WAS INSTALL - [SDR CHQA201100200](https://openairdocs.org/sdr/CHQA201100200), May 30, 2011: FLOOR SUPPORT. DAMAGED. DURING INSPECTION THE CENTER FUSELAGE III OMEGA BEAM WAS FOUND TO BE DAMAGED. THE OMEGA BEAM WAS REPAIRED IAW SRM 53-23-02-RE AND EMBRAER ETD 2011-145-100373. - [SDR CHQA201100215](https://openairdocs.org/sdr/CHQA201100215), May 28, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE RIGHT OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA201100214](https://openairdocs.org/sdr/CHQA201100214), May 28, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE MID OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA201100213](https://openairdocs.org/sdr/CHQA201100213), May 28, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION A CRACK WAS FOUND ON THE CABIN FLOOR STRUCTURE LEFT OMEGA BEAM FLANGE AT FRAME 47. THE CRACK WAS REPAIRED IN ACCORDANCE WITH SRM 53-23-02. - [SDR CHQA201100051](https://openairdocs.org/sdr/CHQA201100051), Mar 8, 2011: CONTROLLER. INOPERATIVE. CREW REPORTED, AFTER TAKEOFF WERE UNABLE TO CONTROL THE CABIN ALTITUDE IN MANUAL MODE WHILE THE AUTO MODE WAS ON DEFERRAL. IT WAS REPORTED THAT THE CABIN ALTITU - [SDR CHQA201100034](https://openairdocs.org/sdr/CHQA201100034), Feb 8, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE LEFT AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT BULB IN THE LEFT AFT EMERGENCY EXIT LIGHT WITH - [SDR CHQA200900212](https://openairdocs.org/sdr/CHQA200900212), Sep 30, 2009: LIGHT. BROKEN. WHILE REMOVING FLOOR STRIP FOR REMOVAL OF GASPER FAN, THE FLOOR PROX LIGHT STRIP BROKE. THE LIGHT STRIP AT ROW 14A WAS REPLACED AND CHECKED NORMAL PER EMB AMM 3 - [SDR CHQA200900095](https://openairdocs.org/sdr/CHQA200900095), Mar 31, 2009: HEATER. SHORTED. FLIGHT 5323, MKE TO STL - DURING DESCENT INTO STL, AT AROUND 11,000 FT SMOKE WAS SMELLED AND SEEN IN THE COCKPIT. THE CREW FOUND THE SOURCE TO BE AT THE BASE OF - [SDR CHQA200900264](https://openairdocs.org/sdr/CHQA200900264), Jan 2, 2009: PROXIMITY SWITCH. DIRTY. IMMEDIATELY AFTER TAKEOFF THE CREW RECEIVED A LG AIR/GND FAIL EICAS MESSAGE. THE LANDING GEAR INDICATED 3 GREEN DOWN AND LOCKED WITH THE LEVER DOWN. THE QRH WAS - [SDR CHQA200800173](https://openairdocs.org/sdr/CHQA200800173), Sep 1, 2008: SOLENOID. FAULTY. FLIGHT 5325 ICT TO STL. THE FLIGHT CREW REPORTED A LOUD AIR SOUND FROM THE NLG AREA DURING FLIGHT. THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND F - [SDR CHQA200600134](https://openairdocs.org/sdr/CHQA200600134), Oct 16, 2006: BULB. INOPERATIVE. EMERGENCY LIGHT OVER WING EXIT INOPERATIVE. TESTED EMERGENCY LIGHT SYSTEM IAW EMB 140 MM 33-50-00. NO DEFECTS NOTED. - [SDR CHQA200600096](https://openairdocs.org/sdr/CHQA200600096), Jul 31, 2006: BATTERY. MISINSTALLED. PROXIMITY EMERGENCY LIGHT STRIP ON CENTER AISLE FLOOR FRONT HALF NOT WORKING. FOUND BATTERY INSTALLED INCORRECTLY. INSTALLED BATTERY IAW EMB 140 MM 30-50-04. LI - [SDR CHQA200600095](https://openairdocs.org/sdr/CHQA200600095), Jul 30, 2006: CONNECTOR. DISCONNECTED. LEFT OVERWING EMERGENCY LIGHT DOES NOT COME ON WHEN SWITCHED TO THE ON POSITION. FOUND LIGHT NOT PLUGGED IN. PLUGGED IN LIGHT AND OPS CHECK GOOD IAW EMB 140 MM - [SDR CHQA200600094](https://openairdocs.org/sdr/CHQA200600094), Jul 27, 2006: BATTERY. INOPERATIVE. AFT HALF OF EMERGENCY LIGHT ON CEILING PANEL BETWEEN PASSENGER CABIN EMERGENCY EXIT INOPERATIVE. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY IAW EMB 140 M - [SDR CHQA200500136](https://openairdocs.org/sdr/CHQA200500136), Aug 4, 2005: BULB. BURNED OUT. LEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IAW EMB 140 MM 33-50-10. OPS CHECK GOOD. - [SDR CHQA200500076](https://openairdocs.org/sdr/CHQA200500076), Apr 7, 2005: WARNING SYSTEM. FALSE INDICATION. WHILE CRUISING AT FL350 BOTH AMBER GUST LOCK WARNING LIGHTS ILLUMINATED. THE QRH PROCEDURES WERE RUN, WHICH AT THE END STATED TO LAND AT THE NEAREST SUITABLE AI - [SDR CHQA200500064](https://openairdocs.org/sdr/CHQA200500064), Mar 27, 2005: BULB. BURNED OUT. LEFT HAND AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED LEFT HAND AFT OVERWING EMERGENCY EXIT LIGHT. OPS CHECK GOOD IAW EMB 140 AMM 33-50-09. - [SDR CHQA000565](https://openairdocs.org/sdr/CHQA000565), Oct 7, 2004: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY BATTERY IAW EMB 140 AMM 33-50-09. OPS CHECK GOOD. - [SDR CHQA200500010](https://openairdocs.org/sdr/CHQA200500010), Jan 21, 2004: BATTERY PACK. DISCHARGED. LEFT HAND OVERWING FORWARD EMERGENCY LIGHT IS INOP. AISLE EGRESS LIGHT AND CABIN FLOOD LIGHTS ARE INOP. REMOVED AND REPLACED EMERGENCY EGRESS BATTERY PACK PER E ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20040519008909I](https://openairdocs.org/incident/20040519008909I), May 19, 2004: Emb EMB135KL (N295SK), St Louis, MO. (-23) Crew aborted takeoff due to erroneous engine indication. Aircraft taxied back to the gate without incident. Maintenance found water in the landing gear… --- 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.