# N802AE: 2001 Embraer EMB-135KL, registration cancelled 2021-02-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 24, 2021 - 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: 145471 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 17, 2001 - Certificate issued: February 24, 2020 - Last registry action: February 24, 2020 - Mode S code: AAE950 - Owner when cancelled: [Envoy Air Inc](https://openairdocs.org/faa-owner/ENVOY%20AIR%20INC) - Location: [Irving, TX](https://openairdocs.org/faa-place/TX/Irving) - Owner type: Corporation - Owner's area on the map: 32.9106° N, 97.0005° W: Placed by OpenAirDocs at the center of ZIP code 75063, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N802AE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=802AE - Page: https://openairdocs.org/deregistered/N802AE-2021-02-24 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 (63, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SIMA20150105002](https://openairdocs.org/sdr/SIMA20150105002), Jan 5, 2015: TARGET. OUT OF ADJUST. LEADING EDGE AIR & GND FAIL MSG ON EICAS. REF ITEM 2 THIS LOG PAGE FOR ACTION TAKEN. ADJUSTED NLG PROXIMITY SWITCH TARGET IAW AMM 32-63-05. OPERATIONS CHECKED G - [SDR SIMA20141018004](https://openairdocs.org/sdr/SIMA20141018004), Oct 18, 2014: VALVE. DEFECTIVE. AUTO & MANUAL PRESSURIZATION INOPERATIVE. MAX DELTA P ACHIEVED DURING FLIGHT .4 PSI ALL AOM 1 PROCEDURES ACCOMPLISHED. R & R GND CONNECTION VLV IAW AMM 21-22-04 - [SDR SIMA20140902002](https://openairdocs.org/sdr/SIMA20140902002), Sep 2, 2014: LIGHT. INOPERATIVE. BRAKE ON LIGHT WILL NOT ILLUMINATE. REPLACED PARK BRAKE LIGHT IAW AMM 20-13-04 & RESET EMER BRAKE CB. OPERATIONS CHECKED GOOD IAW AMM 32-44-11. BULBS USED FROM - [SDR SIMA20140530001](https://openairdocs.org/sdr/SIMA20140530001), May 30, 2014: LIGHT. INOPERATIVE. RIGHT WING TO FUSELAGE FAIRING FWD EMER LIGHT INOPERATIVE. R & R RT WING TO FUSELAGE FAIRING FWD EMER LIGHT IAW AMM 33-50-10. OPERATIONS CHECKED GOOD. - [SDR SIMA20140326012](https://openairdocs.org/sdr/SIMA20140326012), Mar 26, 2014: LAMP. OUT OF POSITION. LEFT SIDE EMERGENCY LIGHTS AFT LIGHT IS OUT. REPOSITIONED LAMP IAW AMM 33-50-10, LIGHT ILLUMINATES, OPS CHECKED GOOD. - [SDR SIMA20140317003](https://openairdocs.org/sdr/SIMA20140317003), Mar 17, 2014: AUDIO PANEL. FAILED. DURING DESCENT INTO ABI FIRST OFFICER`S ACP APPEARED TO SHORT OUT WITH STATIC NOISE IN FIRST OFFICER`S SPEAKER & HEADSET. ALSO STRONG SMELL OF BURNING ELEC CIRC - [SDR SIMA20140205002](https://openairdocs.org/sdr/SIMA20140205002), Feb 5, 2014: FLASHLIGHT. INOPERATIVE. FLASHLIGHT ABOVE FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. R & R FLASHLIGHT ASSEMBLY IAW AMM 25-60-11, OPERATIONS CHECKED GOOD. - [SDR SIMA20131227006](https://openairdocs.org/sdr/SIMA20131227006), Dec 27, 2013: SEALANT. LOOSE. CA SIDE OVERWING EMERGENCY LIGHT SEALANT COMING OFF. RE-SEALED EMERGENCY LIGHT SLEEVE IAW 140 MM 51-00-00 SRM. - [SDR SIMA20130924005](https://openairdocs.org/sdr/SIMA20130924005), Sep 24, 2013: CRADLE. BROKEN. F/A REAR FLASHLIGHT HOLDER BROKEN. REPLACED AND OPS CHECK AFT F/A FLASH LIGHT BRACKET IAW AMM 33-50-16. OPS CHECK GOOD. - [SDR SIMA20130703004](https://openairdocs.org/sdr/SIMA20130703004), Jul 3, 2013: WHEEL. ABNORMAL. THE CREW ABORTED TAKEOFF DUE TO EXCESSIVE NOSE WHEEL SHIMMY ON TAKEOFF ROLL OVER 80 KTS. ACFT REMOVED FROM SERVICE. COMPLIED WITH HIGH SPEED TAXI. NO EXCESSIVE - [SDR SIMA20130621006](https://openairdocs.org/sdr/SIMA20130621006), Jun 21, 2013: DOOR. BINDING. DURING MX INSPECTION, FOUND MAIN PASSENGER DOOR HARD TO OPEN. ACFT REMOVED FROM SERVICE. ADJUSTED AFT UPPER STOP AND LUBED DOOR IAW 52-18-00. OPS CHECKED AND OP - [SDR SIMA20130525006](https://openairdocs.org/sdr/SIMA20130525006), May 25, 2013: BATTERY. DISCHARGED. DURING B INSPECTION FOUND THE NR 4 AND NR 5 FLOOR EMERGENGY LIGHT STRIPS INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR 3 EMERGENCY BATTERY AND CHA - [SDR SIMA20130415002](https://openairdocs.org/sdr/SIMA20130415002), Apr 15, 2013: ROLLER. DIRTY. ON FLIGHT 4263 THE CREW REPORTED THE CABIN MAIN DOOR WAS HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. CLEANED AND LUBRICATED DOOR ROLLER IAW E - [SDR SIMA20130313003](https://openairdocs.org/sdr/SIMA20130313003), Mar 14, 2013: ROLLER. LACK OF LUBE. ON FLIGHT 3987 FOUND MAIN CABIN DOOR HARD TO OPEN AND CLOSE. THE AIRCRAFT WAS REMOVE FROM SERVICE. LUBRICATED MAIN CABIN DOOR GUIDE ROLLERS AND PERFORMED MAIN D - [SDR SIMA20130117013](https://openairdocs.org/sdr/SIMA20130117013), Jan 17, 2013: SKIN. CRACKED. DURING MAINTENANCE INSPECTION FOUND LEFT REAR FUSELAGE I SKIN ABOVE FRAME 75 CRACKED BEYOND THE LIMITS OF THE SRM. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIR - [SDR SIMA20130117012](https://openairdocs.org/sdr/SIMA20130117012), Jan 17, 2013: DRAG ANGLE. CRACKED. DURING MAINTENANCE INSPECTION FOUND THE RIGHT FORWARD FUSELAGE TO VERTICAL DRAG ANGLE HAS 2 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW AEA EO - [SDR SIMA20121231019](https://openairdocs.org/sdr/SIMA20121231019), Dec 31, 2012: FRAME. CRACKED. FRAME 23, CRACKED BETWEEN STR 15R AND 16R. REPAIRED FRAME 23 BETWEEN STR 15R AND 16R IAW AEA EO EM-53MR-1808. - [SDR SIMA20121231018](https://openairdocs.org/sdr/SIMA20121231018), Dec 31, 2012: SHEAR TIE. CORRODED. CARGO DOOR SHEAR TIE AT FRAME 65 CORRODED. REPAIRED SHEAR TIE IAW AEA EO-EM53-MR-1129. - [SDR SIMA20121231012](https://openairdocs.org/sdr/SIMA20121231012), Dec 31, 2012: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWIN - [SDR SIMA20121231011](https://openairdocs.org/sdr/SIMA20121231011), Dec 31, 2012: INVERTER. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE LAST 3 CENTER AISLE EMERGENCY LIGHT STRIPS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE N - [SDR SIMA20121231010](https://openairdocs.org/sdr/SIMA20121231010), Dec 31, 2012: SEAL. CUT. DURING B INSPECTION FOUND THE PASSENGER DOOR FRAME SEAL CUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MAIN PASSENGER DOOR FRAME SEAL IAW - [SDR SIMA20121231009](https://openairdocs.org/sdr/SIMA20121231009), Dec 31, 2012: CONNECTOR. BROKEN. DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIP 3 CONNECTOR BETWEEN FRAME 34 AND FRAME 35 BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE EMERGE - [SDR SIMA20120728002](https://openairdocs.org/sdr/SIMA20120728002), Jul 28, 2012: BULB. INOPERATIVE. DURING MAINTENANCE INSPECTION, FOUND THE EXTERIOR RIGHT AFT EMERGENCY LIGHT INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE EXTERIOR RIGHT - [SDR SIMA20120702004](https://openairdocs.org/sdr/SIMA20120702004), Jul 2, 2012: GASPER FAN. MALFUNCTIONED. ON FLIGHT 2897 THE FLIGHT ATTENDANT REPORTED A LIGHT ODOR OF SMOKE IN MID CABIN FOR A SHORT TIME. THE ODOR WAS ALSO PRESENT IN THE COCKPIT. THE ODOR WAS NOT ELE - [SDR SIMA20120531003](https://openairdocs.org/sdr/SIMA20120531003), May 31, 2012: PANEL. DAMAGED. DURING B INSPECTION, FOUND THE MAIN DOOR EMERGENCY LIGHT COVER PANEL HAS DIME SIZE HOLE NEXT TO LIGHT ASSEMBLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED A - [SDR SIMA20120411001](https://openairdocs.org/sdr/SIMA20120411001), Apr 7, 2012: UPLOCK. INOPERATIVE. ON FLIGHT 3366 THE CREW REPORTED THAT AFTER TAKEOFF WHEN GEAR WAS SELECT DUP, GOT A LANDING/DISAGREE MESSAGE RIGHT GEAR SHOWED UNSAFE. COMPLIED WITH AOM PROCEDU - [SDR SIMA20120331003](https://openairdocs.org/sdr/SIMA20120331003), Mar 31, 2012: DOOR SEAL. TORN. FOR FLIGHT 3421 THE GATE AGENT REPORTED THE CABIN DOOR SEAL (FRAME SIDE) HAS A TEAR ON UPPER SIDE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR ON MA - [SDR SIMA201132910](https://openairdocs.org/sdr/SIMA201132910), Nov 24, 2011: UNKNOWN. MALFUNCTIONED. TRIED TO START THE APU WITH THE GPU. THE APU DID NOT START & THEN A BURNING SMELL WAS PRESENT IN THE COCKPIT. RESET GPU. STARTED APU IAW EMB GHC. NO DEFECTS NOT - [SDR SIMA2011312007](https://openairdocs.org/sdr/SIMA2011312007), Nov 7, 2011: LIGHT. NOT SEATED. DURING MAINTENANCE BASE VISIT FOUND THE LEFT AND RIGHT EMERGENCY LIGHT ABOVE WING INOPERABLE. FOUND THE LIGHT IN FRONT OF THE LEFT WING EMERGENCY LIGHT INOPERAB - [SDR SIMA201124403](https://openairdocs.org/sdr/SIMA201124403), Sep 1, 2011: LIGHT. INOPERATIVE. FOR FLIGHT 4167 DURING INSPECTION FOUND THE FRONT EMERGENCY FLOOR PROXIMITY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FR - [SDR SIMA201109604](https://openairdocs.org/sdr/SIMA201109604), Apr 2, 2011: LIGHT. INOPERATIVE. FOR FLIGHT 2712 DURING PREFLIGHT INSPECTION FOUND THE LEFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE - [SDR SIMA201105602](https://openairdocs.org/sdr/SIMA201105602), Feb 24, 2011: STRUCTURE. DENTED. WHILE ON THE RAMP THE AIRCRAFT WAS STRUCK BY A DEICE TRUCK NEAR THE SERVICE DOOR. SKIN HAS SEVERAL DENTS ON FRAME 22 BETWEEN STRINGERS 20 AND 18. THE SHEAR CLIP - [SDR SIMA201103406](https://openairdocs.org/sdr/SIMA201103406), Jan 29, 2011: SILL. CORRODED. DURING MAINTENANCE BASE VISIT INSPECTION FOUND CENTER SERVICE DOOR SILL TO HAVE CORROSION AROUND THE NUT PLATES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED - [SDR SIMA201103407](https://openairdocs.org/sdr/SIMA201103407), Jan 28, 2011: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM CORRODED (FORWARD AND AFTWARD OF FRAME 20 ON A PREVIOUS REPAIR). THE AIRCRAFT WAS REMOVED FROM SE - [SDR SIMA201103405](https://openairdocs.org/sdr/SIMA201103405), Jan 28, 2011: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM BETWEEN FRAMES 59-60 TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR T - [SDR SIMA201103404](https://openairdocs.org/sdr/SIMA201103404), Jan 26, 2011: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM AT FRAME 27 TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT OMEGA BEAM AT - [SDR SIMA201103403](https://openairdocs.org/sdr/SIMA201103403), Jan 26, 2011: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE BASE VISIT INSPECTION FOUND LEFT OMEGA BEAM FORWARD OF FRAME 25 AT THE CARBON CROSSMEMBER TO HAVE CORROSION. THE AIRCRAFT WAS REMOVED FROM SE - [SDR SIMA201103401](https://openairdocs.org/sdr/SIMA201103401), Jan 26, 2011: FRAME. CRACKED. DURING MAINTENANCE BASE VISIT INSPECTION FOUND RIGHT FRAME 23 CRACKED AT THE FLOOR LEVEL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED CRACKED FRAME IAW EO E - [SDR SIMA201034101](https://openairdocs.org/sdr/SIMA201034101), Dec 6, 2010: UNKNOWN. MALFUNCTIONED. FOR FLIGHT 2855 SOC REPORTED THE CREW LOST COMMUNICATION RADIOS 1 & 2, WOULD NOT TRANSMIT. THE CREW ELECTED TO RETURN TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDE - [SDR SIMA201013807](https://openairdocs.org/sdr/SIMA201013807), May 18, 2010: LIGHT. INOPERATIVE. DURING MAINTENANCE BASE VISIT FOUND THE LEFT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT OVE - [SDR SIMA201002603](https://openairdocs.org/sdr/SIMA201002603), Jan 24, 2010: PROXIMITY SWITCH. INOPERATIVE. ON FLIGHT 4602 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. COULD NOT SELECT GEAR UP. THE CREW ELECTED TO RETURN T - [SDR SIMA201002604](https://openairdocs.org/sdr/SIMA201002604), Jan 22, 2010: PROXIMITY SWITCH. INOPERATIVE. ON FLIGHT 4455 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AND A WEIGHT ON WHEEL INOPERABLE MESSAGE ON EICAS. THE CREW ELEC - [SDR SIMA201002605](https://openairdocs.org/sdr/SIMA201002605), Jan 22, 2010: PROXIMITY SWITCH. INOPERATIVE. ON FLIGHT 4694 AFTER TAKEOFF THE CREW REPORTED, RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS. THE LANDING GEAR WAS NOT RETRACTED. THE CREW ELECTED T - [SDR SIMA200925204SUP](https://openairdocs.org/sdr/SIMA200925204SUP), Oct 22, 2009: WINDSHIELD. FAILED. ON FLIGHT 4913, DURING CLIMB OUT THE OUTER PANE OF THE FIRST OFFICERS COCKPIT WINDSHIELD SHATTERED. THE CREW ELECTED TO RETURN TO LGA. THE AIRCRAFT WAS REMOVED - [SDR SIMA200925204](https://openairdocs.org/sdr/SIMA200925204), Sep 9, 2009: WINDSHIELD. CRACKED. ON FLIGHT 4913 DURING CLIMBOUT THE OUTER PANE OF THE FIRST OFFICERS COCKPIT WINDSHIELD SHATTERED. THE CREW ELECTED TO RETURN TO LGA. AIRCRAFT REMOVED FROM SERVI - [SDR SIMA200909102](https://openairdocs.org/sdr/SIMA200909102), Mar 30, 2009: FLOOR SUPPORT. CORRODED. DURING HMBV THE LEFT OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. CUT OUT THE DAMAGED AREA. PREPARED A 1.6" X 12.25" FILLER FROM P/N EPNEM53EP54703 AND A 15.5" X - [SDR SIMA200909101](https://openairdocs.org/sdr/SIMA200909101), Mar 30, 2009: SILL. CORRODED. DURING HMBV THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED SERVICE DOOR SILL IN TWO AREAS. ALODINE AND PRIMED BLENDED AREA. FILLED BLENDED AREA USING - [SDR SIMA200720107](https://openairdocs.org/sdr/SIMA200720107), May 25, 2007: SKIN. CRACKED. CRACK DEVELOPED DURING DAMAGE CONTOUR. CUT OUT DAMAGE AREA. FABRICATED DOUBLER AND FILLER. INSTALLED IAW EMB IC 2007-145/03554A, PARAGRAPH 1. - [SDR SIMA200720106](https://openairdocs.org/sdr/SIMA200720106), May 24, 2007: SILL. CORRODED. CARGO DOOR LOWER SILL FOUND CORRODED. REMOVED AND REPLACED LOWER SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. - [SDR SIMA200720104](https://openairdocs.org/sdr/SIMA200720104), May 21, 2007: FLOOR SUPPORT. CORRODED. GALLEY CENTER HAT BEAM CORRODED. REMOVED AND REPLACED HAT BEAM IAW EMB SRM 51-40-02 AND 51-40-04. AIRCRAFT RETURNED TO SERVICE. All 63: https://openairdocs.org/deregistered/N802AE-2021-02-24/reports.md --- 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.