# N828AE: 2002 Embraer EMB-135KL, registration cancelled 2024-05-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 16, 2024 - Exported to: Chad - 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: 145604 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 26, 2002 - Certificate issued: January 10, 2024 - Last registry action: January 10, 2024 - Mode S code: AB4E98 - 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/N828AE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=828AE - Page: https://openairdocs.org/deregistered/N828AE-2024-05-16 From the FAA registry file of November 3, 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 (45) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SIMA20140305010](https://openairdocs.org/sdr/SIMA20140305010), Mar 5, 2014: DOOR. SCRATCHED. MAIN PAX DOOR HAS A SCRATCH THAT MEASURES 2 1/4 INCHES L X 1/8 INCH W X .005 INCHES DEEP, 5/8 INCH FROM AFT EDGE & 8 INCHES FROM THE BOTTOM. PERFORMED REPAIR OF - [SDR SIMA20131229005](https://openairdocs.org/sdr/SIMA20131229005), Dec 29, 2013: SMOKE DETECTOR. FAILED. GATE REPORTED LAVATORY SMOKE DETECTION HORN GOING OFF. R & R LAVATORY SMOKE SENSOR IAW 140 AMM 26-44-01, OPERATIONS CHECKED GOOD. - [SDR SIMA20131126010](https://openairdocs.org/sdr/SIMA20131126010), Nov 26, 2013: FLASHLIGHT. DEFECTIVE. CAPTAIN`S FLASHLIGHT NOT CHARGING. R & R THE CAPTAIN'S FLASHLIGHT ASSEMBLY IAW EMB 140 AMM 33-50-16, OPERATIONS CHECKED GOOD. - [SDR SIMA20131112011](https://openairdocs.org/sdr/SIMA20131112011), Nov 12, 2013: WIRE. BROKEN. EMERGENCY LIGHT HAS A BROKEN WIRE. R & R EMERGENCY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. - [SDR SIMA20131012005](https://openairdocs.org/sdr/SIMA20131012005), Oct 12, 2013: BATTERY PACK. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R POWER SUPPLY AND BATTERY PACK IAW WC 33-700-19. OPS CHECKED IAW WC 33-700-17. - [SDR SIMA20130905005](https://openairdocs.org/sdr/SIMA20130905005), Sep 5, 2013: CARBON SEAL. LEAKING. HEAVY OIL ODOR THRU ENVIROMENTAL SYS AFTER ADDING THRUST DURING DESCENTS AND CLIMB. FOUND OIL TO BE LEAKING FROM NR 1 ENGINE CARBON SEAL. REMOVED AND REPLACED T - [SDR SIMA20130818004](https://openairdocs.org/sdr/SIMA20130818004), Aug 18, 2013: LAMP. INOPERATIVE. LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10, OPS CHECKED GOOD. - [SDR SIMA20130818003](https://openairdocs.org/sdr/SIMA20130818003), Aug 18, 2013: LAMP. INOPERATIVE. RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-50-10, OPS CHECKED GOOD. - [SDR SIMA20130621003](https://openairdocs.org/sdr/SIMA20130621003), Jun 21, 2013: INVERTER. FAILED. DURING B-INSPECTION, FOUND THE FLOOR PROXIMITY LIGHTS OUT AT ROWS 4-5. ACFT REMOVED FROM SERVICE. R & R THE EMERGENCY LIGHTING DC/AC INVERTER IAW AMM 33-50-01. - [SDR SIMA20130521005](https://openairdocs.org/sdr/SIMA20130521005), May 21, 2013: FLASHLIGHT. BROKEN. DURING B-INSPECTION, FOUND THE FWD CABIN FLASHLIGHT HAS A BROKEN SWITCH. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FORWARD CABIN FLASHLIGHT IAW AMM 33-51-01. - [SDR SIMA20130505003](https://openairdocs.org/sdr/SIMA20130505003), May 5, 2013: BATTERY. INOPERATIVE. DURING B INSPECTION FOUND THE EMERGENCY LIGHT STRIPS POWERED BY THE NR 3 POWER PACK WAS INOPERABLE. SUSPECT NR 5 INVERTER. THE AIRCRAFT WAS REMOVED FROM SERVICE - [SDR SIMA20130217003](https://openairdocs.org/sdr/SIMA20130217003), Feb 17, 2013: BOLT. MISSING. ON FLIGHT 2717 THE CREW REPORTED THEY COULD NOT OPEN THE CABIN DOOR FROM INSIDE THE AIRCRAFT. THE GATE AGENT OPENED FROM OUTSIDE. THE AIRCRAFT WAS REMOVED FROM - [SDR SIMA20130126002](https://openairdocs.org/sdr/SIMA20130126002), Jan 26, 2013: FLASHLIGHT. ODOR. DURING MAINTENANCE INSPECTION FOUND AN UNUSUAL ODOR IN COCKPIT, SUSPECT POSSIBLE SMELL FROM FORWARD FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY. THE AIRCRAFT WAS REMOV - [SDR SIMA20130124002](https://openairdocs.org/sdr/SIMA20130124002), Jan 24, 2013: CONTROL VALVE. FAILED. FLIGHT 4190. WHILE ENROUTE, PERFORMED ANTI ICE TEST AND NOTICED AN UNFAMILIAR ODOR AS SOON AS THE TEST WAS COMPLETE. WHEN PACKS WERE BOTH ONLINE, ODOR DISAPPEAR - [SDR SIMA20121118003](https://openairdocs.org/sdr/SIMA20121118003), Nov 18, 2012: BATTERY. DISCHARGED. DURING B INSPECTION FOUND THE LEFT FORWARD EMERGENCY LIGHT ABOVE WING INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FORWARD E - [SDR SIMA20120924007](https://openairdocs.org/sdr/SIMA20120924007), Sep 24, 2012: WIRE. BROKEN. DURING B INSPECTION FOUND THE EMREGENCY LIGHTS FLOOR LIGHTING STRIP AT ROWS 7-8 INOPERABLE. THE WIRE WAS BROKEN DURING MAINTENANCE. THE AIRCRAFT WAS REMOVED FRO - [SDR SIMA20120817001](https://openairdocs.org/sdr/SIMA20120817001), Aug 17, 2012: UNKNOWN. ODOR. THE CREW REPORTED THAT UPON STARTING APU AT GATE AND TURNING ON PACK 2 THERE WAS STONG ODOR OF FUEL IN THE COCKPIT AND BACK TO ABOUT ROW 7. THE AIRCRAFT WAS REM - [SDR SIMA20120705005](https://openairdocs.org/sdr/SIMA20120705005), Jul 5, 2012: CRADLE. DAMAGED. DURING MAINTENANCE INSPECTION FOUND THAT THE FORWARD CABIN EF-2C RECHARGEABLE FLASHLIGHT CRADLE SHOWS EVIDENCE OF OVERHEATING. THE AIRCRAFT WAS REMOVED FROM SER - [SDR SIMA20120705004](https://openairdocs.org/sdr/SIMA20120705004), Jul 5, 2012: CRADLE. DAMAGED. DURING MAINTENANCE INSPECTION FOUND THAT THE AFT CABIN EF-2C RECHARGEABLE FLASHLIGHT CRADLE SHOWS EVIDENCE OF OVERHEATING. THE AIRCRAFT WAS REMOVED FROM SERVICE - [SDR SIMA20120625001](https://openairdocs.org/sdr/SIMA20120625001), Jun 25, 2012: MECHANISM. UNSECURE. ON FLIGHT 2897 THE CREW REPORTED THE MAIN ENTRY DOOR WILL NOT OPEN FROM INSIDE OF AIRCRAFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. RE-SECURED DOOR MECHANSIM PER - [SDR SIMA20120430002](https://openairdocs.org/sdr/SIMA20120430002), Apr 30, 2012: FRAME. CRACKED. DURING MAINTENANCE INSPECTION FOUND FRAME 23 CRACKED BELOW STRINGER 15R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAME 23 IAW AEA EO EM-53MR-1808. THE A - [SDR SIMA20120419009](https://openairdocs.org/sdr/SIMA20120419009), Apr 19, 2012: WIRE. BROKEN. DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY LIGHT STRIP WIRE BROKEN AT SIDE FLOOR PANEL 261BF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY L - [SDR SIMA20120401005](https://openairdocs.org/sdr/SIMA20120401005), Apr 1, 2012: LENS. CRACKED. DURING PS-2 INSPECTION FOUND THE LEFT AFT EMERGENCY LIGHT LENS CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY - [SDR SIMA20120401004](https://openairdocs.org/sdr/SIMA20120401004), Apr 1, 2012: CHARGER. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE NR 4 BATTERY CHARGER ASSEMBLY DUE A CHANGE, DUE TO FAULTY LEFT OVERWING EXTERIOR EMERGENCY LIGHT. THE AIRCRAFT WAS REMOV - [SDR SIMA20120322006](https://openairdocs.org/sdr/SIMA20120322006), Mar 22, 2012: HOLDER. BROKEN. DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S EMERGENCY FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FLAS - [SDR SIMA2012054002](https://openairdocs.org/sdr/SIMA2012054002), Feb 22, 2012: CRADLE. CRACKED. DURING B-INSPECTION, FOUND THE LOWER ARM OF EMERGENCY FLASHLIGHT HOLDER BEHIND CAPTAIN'S SEAT IS CRACKED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BR - [SDR SIMA201124904](https://openairdocs.org/sdr/SIMA201124904), Sep 2, 2011: STRUT. FAILED. ON FLIGHT 3240 THE CREW REPORTED THE RIGHT MAIN GEAR STRUT FAILED. THE CREW DECLARED AN EMERGENCY INBOUND TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRC - [SDR SIMA201017304](https://openairdocs.org/sdr/SIMA201017304), Jun 21, 2010: COUPLING. DEFECTIVE. ON FLIGHT 4359 DURING THE CLIMBOUT PASSING THROUGH 7,000 FEET THE CREW RECEIVED A PACK 1/2 VALVE FAIL MESSAGE FOLLOWED BY A STRONG ELECTRICAL BURNING ODOR. THE - [SDR SIMA201014405](https://openairdocs.org/sdr/SIMA201014405), May 20, 2010: FRAME. DAMAGED. DURING MAINTENANCE BASE INSPECTION FOUND TOOL MARKS ON INBOARD WEB OF FRAME 61 BETWEEN STRINGERS 16R AND 17R. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WI - [SDR SIMA201014404](https://openairdocs.org/sdr/SIMA201014404), May 19, 2010: FITTING. GOUGED. DURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT AILERON PCA FITTING LUGS ON AILERON TO BE GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED - [SDR SIMA201014403](https://openairdocs.org/sdr/SIMA201014403), May 19, 2010: ATTACH FITTING. WORN. DURING MAINTENANCE BASE INSPECTION FOUND LEFT AILERON PCA OUTBOARD ATTACH FITTING ON AILERON HAT BUSHING MIGRATING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOV - [SDR SIMA201014402](https://openairdocs.org/sdr/SIMA201014402), May 18, 2010: FITTING. GOUGED. DURING MAINTENANCE BASE INSPECTION FOUND FRAME 68 SHEAR CLIP GOUGED JUST ABOVE CARGO DOOR SILL. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED GOUGED AREA IAW - [SDR SIMA201013305](https://openairdocs.org/sdr/SIMA201013305), May 16, 2010: SILL. CORRODED. SUPPLEMENTAL INFORMATION: CARGO DOOR SILL HAS NUMEROUS AREAS OF CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CARGO DOOR SILL IAW EMBRA - [SDR SIMA201013803](https://openairdocs.org/sdr/SIMA201013803), May 15, 2010: SKIN. CRACKED. DURING MAINTENANCE BASE VISIT FOUND THE FUSELAGE SKIN HAS SMALL CRACKS AT FRAME 75 APPROXIMATELY 2 INCHES RIGHT OF VERTICAL STABILIZER. THE CRACK LENGTH ARE: 3 - [SDR SIMA201013802](https://openairdocs.org/sdr/SIMA201013802), May 15, 2010: SKIN. CRACKED. DURING MAINTENANCE BASE VISIT FOUND THE FUSELAGE SKIN HAS SMALL CRACK AT FRAME 75 APPROXIMATELY 2 INCHES LEFT OF VERTICAL STAB. THE CRACK LENGTH IS .25 INCH. TH - [SDR SIMA201013306](https://openairdocs.org/sdr/SIMA201013306), May 9, 2010: SILL. CORRODED. DURING MAINTENANCE BASE VISIT FOUND THE CARGO DOOR SILL HAS NUMEROUS AREAS OF CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE CORRECTIVE ACTION INFORMATIO - [SDR SIMA200922902](https://openairdocs.org/sdr/SIMA200922902), Aug 16, 2009: WARNING SYSTEM. MALFUNCTIONED. ON FLIGHT 4601 - CREW RECEIVED AN EICAS MESSAGE INDICATING A SPOILER FAIL MESSAGE THAT CYCLED BETWEEN OPEN AND CLOSED. CREW DECLARED AN EMERGENCY AND LANDED WIT - [SDR SIMA200815104](https://openairdocs.org/sdr/SIMA200815104), May 25, 2008: SILL. CORRODED. DURING A MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL. CLEANED AND ALODINED NEW SLLL AND INSTALLED IAW EMB 145 SRM (SRM - [SDR SIMA200733803](https://openairdocs.org/sdr/SIMA200733803), Dec 1, 2007: DOWNLOCK SWITCH. DEFECTIVE. CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. ALSO HAD A LANDING GEAR AIR/GND FAIL ON EICAS. CAPT DIVERTED TO LGA. AIRCRAFT LANDED SAFELY WITH NO OTHER - [SDR SIMA200534801](https://openairdocs.org/sdr/SIMA200534801), Dec 11, 2004: BATTERY PACK. DISCHARGED. CREW NOTED WHEN ACTIVATING EMERGENCY LIGHTS FOR TEST, LIGHTS WOULD ILLUMINATE THEN FADE OUT FAST. CA REPLACED ALL 4 EMERGENCY LIGHT BATTERIES. OPERATONAL CHECK - [SDR SIMA200424703](https://openairdocs.org/sdr/SIMA200424703), Aug 26, 2004: CHANNEL. CORRODED. SAW - DURING CPCP INSPECTION, MAINTENANCE FOUND CORROSION ON SERVICE DOOR SILL PLATE. REMOVED AND REPLACED THE SERVICE DOOR SILL PLATE CHANNEL IAW EMB 140 SRM 5 - [SDR SIMA200424702](https://openairdocs.org/sdr/SIMA200424702), Aug 26, 2004: CHANNEL. CORRODED. SAW - DURNG CPCP INSPECTION, MAINTENANCE FOUND HAT BEAM CORRODED BETWEEN FRAMES 19 AND 20. HAT BEAM REPLACED IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. - [SDR SIMA200424704](https://openairdocs.org/sdr/SIMA200424704), Aug 26, 2004: FLOOR SUPPORT. CORRODED. DURING CPCP INSPECTION, MAINTENANCE FOUND CORROSION ON LEFT OMEGA BEAM. REPAIRED LEFT OMEGA BEAM IAW EMB 140 SRM 53-21-10 FIG 201. AIRCRAFT WAS RETURNED TO SERV - [SDR SIMA200331001](https://openairdocs.org/sdr/SIMA200331001), Nov 5, 2003: BATTERY PACK. INOPERATIVE. DURING TAXI IN CRWE NOTED FORWARD PORTION OF CABIN EMERGENCY LIGHTS INOPERATIVE. RAI NR 1 EMERGENCY BATTERY PACK P/N 20131A, S/N 67884, NR 2 BATTERY PACK P/N 20 - [SDR SIMA200226109](https://openairdocs.org/sdr/SIMA200226109), Sep 16, 2002: ENGINE. BIRD INGESTION. AFTER TAKE OFF FROM SJC THE AIRCRAFT ENCOUNTERED ABOUT A DOZEN BIRDS WHICH WERE INGESTED INTO BOTH ENGINES. AN EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO S ## 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 20110902021199I](https://openairdocs.org/incident/20110902021199I), Sep 2, 2011: Embraer EMB-135KL (N828AE), Dfw Airport, TX, No damage. On 09/02/2011 American eagle airlines (aea) aircraft N828AE operating as flight #3240 declared and reported an emergency while landing at Dallas/ft. worth… --- 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.