# N299SK: 2001 Embraer EMB-135KL, registration cancelled 2020-04-03 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 3, 2020 - Exported to: Guernsey - 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: 145532 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 30, 2001 - Certificate issued: May 14, 2018 - Last registry action: September 12, 2018 - Mode S code: A31883 - Owner when cancelled: [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE) - Location: Bungay Norfolk, United Kingdom - Owner type: Corporation - The mark today: https://openairdocs.org/aircraft/N299SK - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=299SK - Page: https://openairdocs.org/deregistered/N299SK-2020-04-03 From the FAA registry file of November 7, 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 (26) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA20140403102](https://openairdocs.org/sdr/CHQA20140403102), Apr 3, 2014: FIRE LOOP. FAULTY. CREW REPORTED THAT AFTER TAKEOFF, THEY RECEIVED AN ENG 1 FIRE DETECTION FAIL MSG. THE CREW DIVERTED THE ACFT & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE ENG - [SDR CHQA20130728197](https://openairdocs.org/sdr/CHQA20130728197), Jul 28, 2013: ENGINE. ODOR. DURING FLIGHT THERE WAS AN OIL BURNING ODOR IN THE COCKPIT WHILE USING BLEED SYSTEM 1 AND BOTH PACK SYSTEMS TURNED ON. THE ODOR WAS ONLY PRESENT IN THE COCKPIT - [SDR CHQA20130727193](https://openairdocs.org/sdr/CHQA20130727193), Jul 27, 2013: UNKNOWN. ODOR. DURING ALL PHASES OF FLIGHT, A SLIGHT OIL BURNING ODOR WAS PRESENT. MX RAN BOTH ENGINES WITH THE ENGINE BLEED AND PACK SYS TURNED ON. NO ODORS OR DEFECTS WERE N - [SDR CHQA20130625136](https://openairdocs.org/sdr/CHQA20130625136), Jun 25, 2013: BULB. INOPERATIVE. DURING INSPECTION, THE OVERHEAD COCKPIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE COCKPIT EMERGENCY LIGHT BULB. OPS CHECKS WERE GOOD WITH NO - [SDR CHQA20130504153](https://openairdocs.org/sdr/CHQA20130504153), May 4, 2013: SKIN. DAMAGED. DURING INSPECTION, A TOOLING MARK ON THE INTERIOR BELLY SKIN WAS FOUND ADJACENT TO STRINGER 21L AND BETWEEN FRAMES 10 AND 11. THE SKIN WAS REPAIRED IN ACCORDANC - [SDR CHQA20130502162](https://openairdocs.org/sdr/CHQA20130502162), May 2, 2013: FRAME. DAMAGED. DURING INSPECTION, AN ELONGATED RIVET HOLE WAS FOUND ON FRAME 12 BETWEEN STRINGERS 21R AND 20R. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-008257. - [SDR CHQA20130502161](https://openairdocs.org/sdr/CHQA20130502161), May 2, 2013: SUPPORT. DAMAGED. DURING INSPECTION, A MISDRILLED RIVET HOLE ON THE RIGHT CONTROL CABLE QUADRANT SUPPORT. THE SUPPORT BRACKETS AND QUADRANT SUPPORT WERE REPLACED IN ACCORDANCE WI - [SDR CHQA20130501159](https://openairdocs.org/sdr/CHQA20130501159), May 1, 2013: STRINGER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21L BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130501158](https://openairdocs.org/sdr/CHQA20130501158), May 1, 2013: SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND IN THE LEFT AILERON QUADRANT SUPPORT WEB AT FRAMES 12-13 AND STRINGERS 20L-21L. THE QUADRANT SUPPORT WAS REPLACED IN ACCO - [SDR CHQA20130501157](https://openairdocs.org/sdr/CHQA20130501157), May 1, 2013: SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND IN THE RIGHT AILERON QUADRANT SUPPORT WEB AT FRAME 12 AND 13 AND STRINGERS 20R AND 21R. THE RIGHT QUADRANT SUPPORT WAS RE - [SDR CHQA20130501156](https://openairdocs.org/sdr/CHQA20130501156), May 1, 2013: STRINGER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21R BETWEEN FRAMES 13 AND 9. THE STRINGER WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20130501151](https://openairdocs.org/sdr/CHQA20130501151), May 1, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION AND CRACKS WERE FOUND ON THE FLOORBOARD SUPPORT FLANGE OF THE LEFT OMEGA BEAM BETWEEN FRAME 24 AND FRAME 25. THE OMEGA BEAM WAS REP - [SDR CHQA20130430160](https://openairdocs.org/sdr/CHQA20130430160), Apr 30, 2013: FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 13 BETWEEN STRINGERS 21L AND 20L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130426155](https://openairdocs.org/sdr/CHQA20130426155), Apr 26, 2013: FITTING. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 7L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND - [SDR CHQA20130426154](https://openairdocs.org/sdr/CHQA20130426154), Apr 26, 2013: FITTING. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 73 BETWEEN STRINGER 8R AND 9R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130426152](https://openairdocs.org/sdr/CHQA20130426152), Apr 26, 2013: FITTING. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP ON FRAME 66 BETWEEN STRINGERS 6L AND 7L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130426150](https://openairdocs.org/sdr/CHQA20130426150), Apr 26, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE SCREW HOLE ON THE CENTER OMEGA LEFT SIDE BETWEEN FRAMES 24 AND 25. THE CENTER OMEGA BEAM WAS REPAIRED IN ACCORDANC - [SDR CHQA20130426149](https://openairdocs.org/sdr/CHQA20130426149), Apr 26, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA AT THE CARBON CROSS MEMBER FRAME 27. THE OMEGA BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20130426148](https://openairdocs.org/sdr/CHQA20130426148), Apr 26, 2013: FITTING. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE SHEAR CLIP AT FRAME 73 BETWEEN STRINGER 8L AND 9L. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20130426147](https://openairdocs.org/sdr/CHQA20130426147), Apr 26, 2013: BRACKET. CRACKED. DURING INSPECTION, A CRACK WAS FOUND IN THE BRACKET BETWEEN FRAME 64 AND FRAME 65 AT STRINGER 5L. THE BRACKET WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02, 51-3 - [SDR CHQA20130426146](https://openairdocs.org/sdr/CHQA20130426146), Apr 26, 2013: DOUBLER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER LEFT OMEGA FRAME 20. THE DOUBLER WAS REPLACED IN ACCORDANCE WITH SRM 53-00-10. - [SDR CHQA20120428134](https://openairdocs.org/sdr/CHQA20120428134), Apr 28, 2012: SELECTOR SWITCH. FAULTY. CREW REPORTED, RECEIVED A BLEED 2 VALVE CLOSED MESSAGE IN FLIGHT. THE CREW FOLLOWED THE QUICK-REFERENCE HANDBOOK BUT THE VALVE WOULD NOT INDICATE OPEN. THE AIRC - [SDR CHQA200900164](https://openairdocs.org/sdr/CHQA200900164), Jul 26, 2009: ENGINE. MAKING METAL. FLIGHT 5356, JAX TO STL. ON DESCENT INTO STL, THE CREW HEARD A THUMP FROM THE REAR OF THE AIRCRAFT AS THRUST WAS DECREASED TO FLIGHT IDLE. A SHARP SPIKE IN E2 E - [SDR CHQA200900135](https://openairdocs.org/sdr/CHQA200900135), May 30, 2009: SMOKE DETECTOR. FAULTY. DURING CLIMB OUT, THE CREW RECEIVED A LAV SMOKE WARNING MESSAGE ON THE EICAS DISPLAY. THIS WAS ACCOMPANIED BY A HAZE OR SMOKE WITH CONDENSATION COMING FROM THE - [SDR CHQA200900265](https://openairdocs.org/sdr/CHQA200900265), Jan 3, 2009: LINE. LOOSE. DURING CRUISE, THE FLIGHT CREW NOTICED AN OIL BURN RATE OF (2) QUARTS PER HOUR AND THE OIL QUANTITY OF E2 HAD DROPPED BELOW 6 QTS. THE FLIGHT DIVERTED IN ORDER - [SDR CHQA200500113](https://openairdocs.org/sdr/CHQA200500113), Jun 13, 2005: WARNING LIGHT. ACTIVATED. DURING CLIMB AT FL210, RECEIVED "AILERON SYS 1 FAIL" EICAS MESSAGE. LEVELED OFF AT FL230 AND TOLD ATC TO STAND BY. FOLLOWED QRH AND TURNED OFF AILERON SYSTEM 1 ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB CEN14LA262](https://openairdocs.org/ntsb/CEN14LA262), May 28, 2014: Embraer EMB 135KL (N299SK), Traverse City, MI, substantial damage. Probable cause: An in-flight collision with a bird during the descent to land, which resulted in substantial damage to the airplane. ## FAA accident and incident reports (2) 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. - [Accident 20140528007079A](https://openairdocs.org/incident/20140528007079A), May 28, 2014: Embraer EMB-135KL (N299SK), Traverse City, MI, Substantial damage. On may 28th 2014 at 15:00 eastern daylight time, an Embraer E-135 aircraft, N299SK, registered to wells fargo bank and operated by chautauqua airlines,… - [Incident 20030129006039I](https://openairdocs.org/incident/20030129006039I), Jan 29, 2003: Emb EMB135KL (N299SK), Indianapolis, IN. (-23) Chautauqua airlines inc. (chqa) flight 5758 enroute from pit to stl diverted without incident to ind due to a low hydraulic indication. Chqa maintenance… --- 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.