# N829AE: 2002 Embraer EMB-135KL, registration cancelled 2025-05-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 23, 2025
- 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: 145609
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 30, 2002
- Certificate issued: November 26, 2023
- Last registry action: November 26, 2023
- Mode S code: AB524F
- 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/N829AE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=829AE
- Page: https://openairdocs.org/deregistered/N829AE-2025-05-23

From the FAA registry file of November 4, 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 (44)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR SIMA20140124003](https://openairdocs.org/sdr/SIMA20140124003), Jan 24, 2014: LIGHT. INOPERATIVE. SERVICE DOOR EMERGENCY LAMP INOPERATIVE. R & R LAMP IN EXTERNAL SERVICE DOOR EMERGENCY LIGHT IAW AMM 33-50-10-000-801-A & 33-50-10-400-801-A, OPERATIONS CHECKED
- [SDR SIMA20131029008](https://openairdocs.org/sdr/SIMA20131029008), Oct 29, 2013: FLASHLIGHT ASSY. UNSERVICEABLE. CABIN FLASHLIGHT BEHIND 16B IS LOOSE IN CRADLE AND IS NOT SECURE ENOUGH TO CHARGE. R & R CABIN FLASHLIGHT BEHIND SEAT 16B IAW AMM 33-50-16-4. OPS GOOD.
- [SDR SIMA20131025003](https://openairdocs.org/sdr/SIMA20131025003), Oct 25, 2013: LAMP. INOPERATIVE. RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R BULB IAW AMM 33-50-10, OPS CHECKED GOOD.
- [SDR SIMA20130902002](https://openairdocs.org/sdr/SIMA20130902002), Sep 2, 2013: ROLLER. BINDING. F/A REPORTS MAIN CABIN DOOR HARD TO OPEN. SERVICED MAIN DOOR ROLLERS IAW AMM 53-21-02, OPS CHECK GOOD.
- [SDR SIMA20130727009](https://openairdocs.org/sdr/SIMA20130727009), Jul 27, 2013: LIGHT. INOPERATIVE. SOME EMERGENCY LIGHTS FOUND ON BY GROUND PERSONNEL. PERFORMED CHARGING OF EMERGENCY LIGHT BATTERIES IAW CMM 25-60-03. PERFORMED EMERGENCY OPS CHECKED IAW AMM 33
- [SDR SIMA20130617001](https://openairdocs.org/sdr/SIMA20130617001), Jun 17, 2013: FLASHLIGHT. DEFECTIVE. THE CAPTAIN’S FLASHLIGHT WAS NOT ACCEPTING A CHARGE. THE ACFT WAS REMOVED FROM SERVICE. R & R FLASHLIGHT IAW AMM 25-60-00. THE OPS CHECK WAS GOOD. THE ACFT WAS 
- [SDR SIMA20130520004](https://openairdocs.org/sdr/SIMA20130520004), May 20, 2013: BATTERY. UNSERVICEABLE. DURING MX INSPECTION, FOUND A FEW AFT FLOOR EMERGENCY LIGHTS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE NR4 BATTERY POWER SUPPLY IAW-AMM-33-50-04
- [SDR SIMA20130406002](https://openairdocs.org/sdr/SIMA20130406002), Apr 6, 2013: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE EMERGENCY LIGHT ABOVE SEAT 11C INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP AT
- [SDR SIMA20130406001](https://openairdocs.org/sdr/SIMA20130406001), Apr 6, 2013: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE AFT AISLE EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT AISLE EMERGENCY LIGHT LA
- [SDR SIMA20130330006](https://openairdocs.org/sdr/SIMA20130330006), Mar 30, 2013: FLASHLIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S FLASHLIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S COCKPIT FLASH
- [SDR SIMA20130307003](https://openairdocs.org/sdr/SIMA20130307003), Mar 7, 2013: VALVE. INOPERATIVE. ON FLIGHT 4371 THE CREW REPORTED THAT DURING TEST OF RECIRC FAN PER MEL 21-29, THEY HEARD A LOUD GRINDING NOISE AND EXPERIENCED SMELL OF HEAVY SMOKE/ FUMES. THI
- [SDR SIMA20130307002](https://openairdocs.org/sdr/SIMA20130307002), Mar 7, 2013: ACM. DAMAGED. ON FLIGHT 4007 THE CREW REPORTED THEY NOTICED AN ELECTRICAL SMOKE SMELL WHEN NR 1 PACK WAS SELECTED. PACK 1 DEFFERED PER MEL 21-29 AUTH # 030322D-C. FOUND AIR C
- [SDR SIMA20130226003](https://openairdocs.org/sdr/SIMA20130226003), Feb 26, 2013: UNKNOWN. ODOR. FLIGHT 3512. CREW REPORTED RIGHT AFTER APPLYING TAKEOFF POWER RECEIVED NR 1 PACK OVERLOAD FOR ONE SECOND, THEN WENT AWAY. AFTER CLIMBIMG THROUGH APPROX 500FT, D
- [SDR SIMA20121231005](https://openairdocs.org/sdr/SIMA20121231005), Dec 31, 2012: WIRE. BROKEN. DURING MAINTENANCE INSPECTION FOUND THE PANEL 251BF EMERGENCY LIGHT STRIP WIRES BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE PANEL 25
- [SDR SIMA20121003007](https://openairdocs.org/sdr/SIMA20121003007), Oct 3, 2012: FLASHLIGHT. INOPERATIVE. ON FLIGHT 3058 THE CREW REPORTED THE CAPTAIN FLASHLIGHT WAS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN FLASHLIGHT ASSEM
- [SDR SIMA20120705006](https://openairdocs.org/sdr/SIMA20120705006), Jul 5, 2012: BRACKET. BROKEN. DURING MAINTENANCE INSPECTION FOUND THE COPILOT CONSOLE EMERGENCY FLASHLIGHT BRACKET BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE COP
- [SDR SIMA20120430003](https://openairdocs.org/sdr/SIMA20120430003), Apr 30, 2012: BATTERY. DISCHARGED. DURING MAINTENANCE INSPECTION FOUND THE EMERGENCY BATTERY NR 2 WILL NOT HOLD A CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY
- [SDR SIMA20120413013](https://openairdocs.org/sdr/SIMA20120413013), Apr 13, 2012: CONNECTOR. BROKEN. DURING B-INSPECTION FOUND THE CABIN EMERGENCY LIGHT STRIP CONNECTOR BROKEN OFF AT CABIN FLOOR PANEL 251GF. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE C
- [SDR SIMA20120413012](https://openairdocs.org/sdr/SIMA20120413012), Apr 13, 2012: LIGHT. WRONG PART. DURING B-INSPECTION FOUND THE GALLEY AREA FLOOR PROXIMITY EMERGENCY LIGHT STRIP WAS THE WRONG PART NUMBER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND RE
- [SDR SIMA20120413010](https://openairdocs.org/sdr/SIMA20120413010), Apr 13, 2012: STRINGER. GOUGED. DURING MAINTENANCE INSPECTION FOUND THE STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 GOUGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED STRINGER 19 LEFT BETWE
- [SDR SIMA20120413011](https://openairdocs.org/sdr/SIMA20120413011), Apr 11, 2012: HOLDER. BROKEN. DURING B-INSPECTION FOUND THE NR 6 AND NR 2 PROXIMITY LIGHT HOLDER BROKEN. THE NR 6 PROX LIGHT HAS A BROKEN WIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED
- [SDR SIMA20120308005](https://openairdocs.org/sdr/SIMA20120308005), Mar 8, 2012: LIGHT. INOPERATIVE. DURING B-INSPECTION FOUND THE OVERWING EMERGENCY-LIGHT AT 11A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY OVERHEAD LIG
- [SDR SIMA2012017014](https://openairdocs.org/sdr/SIMA2012017014), Jan 16, 2012: TRIM PANEL. DAMAGED. ON FLIGHT 4258 THE CREW REPORTED THE MAIN CABIN DOOR DOES NOT OPEN FULLY. THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MAIN DOOR HINGE COVER TRIM DAMAGED. REMOV
- [SDR SIMA201126206](https://openairdocs.org/sdr/SIMA201126206), Sep 15, 2011: INVERTER. INOPERATIVE. EMERGENCY EXIT SIGN INOP AT COCKPIT STEP. REMOVED AND REPLACED NR 1 DC/AC INVERTER IAW EMB 140 AMM 33-50-11. OPC GOOD.
- [SDR SIMA201126205](https://openairdocs.org/sdr/SIMA201126205), Sep 15, 2011: INVERTER. INOPERATIVE. EMERGENCY EXIT SIGN INOP AT COCKPIT STEP. REMOVED AND REPLACED NR 1 DC/AC INVERTER IAW EMB 140 AMM 33-50-11. OPC GOOD.
- [SDR SIMA201031905](https://openairdocs.org/sdr/SIMA201031905), Nov 15, 2010: LIGHT. INOPERATIVE. DURING MAINTANCE BASE VISIT FOUND THE RIGHT OVERWING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVE
- [SDR SIMA201030804](https://openairdocs.org/sdr/SIMA201030804), Nov 3, 2010: ILS SYSTEM. ERRATIC. ON FLIGHT 2930 THE CREW REPORTED VIA TELEPHONE UPON APPROACH TO SHV BOTH INSTRUMENT LANDING SYSTEMS AND LOCALIZER INDICATIONS WERE ERRATIC AND UNRELIABLE. THE C
- [SDR SIMA201026304](https://openairdocs.org/sdr/SIMA201026304), Sep 20, 2010: LIGHT. INOPERATIVE. DURING MAINTENANCE BASE PS-2 INSPECTION FOUND THE RIGHT WING TO FUESLAGE FARING AFT EMERGENCY LIGHT BULB OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND
- [SDR SIMA201014003](https://openairdocs.org/sdr/SIMA201014003), May 20, 2010: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE BASE VISIT FOUND THE FORWARD DIGITAL "WEB" TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DAMAGE, FABRICATED AND INSTALLED SP
- [SDR SIMA201014005](https://openairdocs.org/sdr/SIMA201014005), May 20, 2010: FRAME. DAMAGED. DURING MAINTENANCE BASE VISIT FOUND DAMAGE TO FRAME 27 AND STRINGER 15L. THE AIRCRAFT WAS REMOVED FROM SERVICE. CUT OUT DAMAGE AND FABRICATED AND INSTALLED REPA
- [SDR SIMA201014004](https://openairdocs.org/sdr/SIMA201014004), May 19, 2010: CONNECTOR. DAMAGED. DURING MAINTENANCE BASE VISIT FOUND THE AFT EMERGENCY LIGHT STRIP CONNECTOR TO BE DAMAGED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED CONNECTOR
- [SDR SIMA201013907](https://openairdocs.org/sdr/SIMA201013907), May 19, 2010: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EMB SR
- [SDR SIMA201013906](https://openairdocs.org/sdr/SIMA201013906), May 19, 2010: GUSSET. CORRODED. DURING MAINTENANCE BASE VISIT FOUND THE RIGHT BEAM GUSSET AT FRAME 22 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED CORRODED GUSSET AND INSTALL
- [SDR SIMA201013901](https://openairdocs.org/sdr/SIMA201013901), May 19, 2010: FLOOR SUPPORT. CORRODED. DURING MAINTENANCE BASE VISIT FOUND THE LEFT OMEGA BEAM (PREVIOUS REPAIR) AT FRAME 20 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EMB SR
- [SDR SIMA201010206](https://openairdocs.org/sdr/SIMA201010206), Apr 9, 2010: PRIORITY VALVE. FAILED. ON FLIGHT 3469 ON TAKEOFF THE CREW REPORTED THAT AFTER GEAR RETRACTION IT SOUNDED LIKE NOSE GEAR DOORS WERE OPENED FOLLOWED BY LANDING GEAR AIR/GROUND FAIL MESS
- [SDR SIMA201009102](https://openairdocs.org/sdr/SIMA201009102), Mar 31, 2010: WARNING SYSTEM. MALFUNCTIONED. ON FLIGHT 3500 DURING THE APPROACH THE CREW REPORTED THAT WITH THE LANDING GEAR DOWN INDICATIONS SHOWED 3 GREEN. RECEIVED A CONTINUOUS TRIPLE CHIME. THE CREW EL
- [SDR SIMA200934908](https://openairdocs.org/sdr/SIMA200934908), Dec 11, 2009: SELECTOR. MALFUNCTIONED. ON FLIGHT 4400 DURING THE CLIMBOUT THE CREW REPORTED, LOST FUEL QUANTITY INDICATIONS FOR TANK 2 AND RECEIVED A FUEL IMBALANCE MESSAGE ON EICAS. THE CREW ALSO RE
- [SDR SIMA200923603](https://openairdocs.org/sdr/SIMA200923603), Aug 23, 2009: WIRE HARNESS. FAULTY. ON FLIGHT 4620 THE CREW DECLARED AN EMERGENCY INTO BOS DUE TO A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT LANDED SAFELY WITH NO INCIDENT. AIRCRAFT REMO
- [SDR SIMA200815105](https://openairdocs.org/sdr/SIMA200815105), May 27, 2008: SILL. CORRODED. DURING A MBV INSPECTION, FOUND CARGO DOOR SLLL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL, DRILLED AND ALODINED NEW PART. INSTALLED NEW SLLL IAW EMB SRM 
- [SDR SMIA200803702](https://openairdocs.org/sdr/SMIA200803702), Feb 4, 2008: DAU. MALFUNCTIONED. ON FLIGHT 4548 CREW REPORTED AT GEAR EXTENSION. EICAS BREAK OUTBOARD INOP. CREW DECLARED AN EMERGENCY MESSAGE REMOVED AFTER LANDING. AIRCRAFT REMOVED FROM SERVI
- [SDR SIMA200730902](https://openairdocs.org/sdr/SIMA200730902), Nov 2, 2007: PRESSURE SWITCH. MALFUNCTIONED. CREW ELECTED TO RETURN INTO CLT DUE TO RUDDER SYS 1/2 INOPERATIVE MESSAGE ON EICAS FOLLOWED BY AUTO PILOT AND YAW DAMPER FAIL ON EICAS AIRCRAFT RETURNED TO CLT 
- [SDR SIMA200730903](https://openairdocs.org/sdr/SIMA200730903), Oct 31, 2007: PROBE. MALFUNCTIONED. CREW REPORTED ON TAKE OFF ROLL AT APPROX 10 KIAS, "SPS ADVANCE" MESSAGE ILLUMINATED ON EICAS. CREW ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. AIRCRAFT RET
- [SDR SIMA200636002](https://openairdocs.org/sdr/SIMA200636002), Dec 24, 2006: RELAY. BURNED. STRONG ELECTRICAL FUMES, FUMES DISSAPATED AFTER FAN TURNED OFF. C/A - FOUND RELAY K0054 SOCKET BLOWN, K0454 AND K0035 DAMAGED. REMOVED AND REPLACED RELAYS. OPER
- [SDR SIMA200633106](https://openairdocs.org/sdr/SIMA200633106), Nov 22, 2006: WARNING SYSTEM. MALFUNCTIONED. AT 80 KNOTS RECEIVED RUDDER SYSTEM 1 INOP MESSAGE, ABORTED TAKEOFF. RUDDER SYSTEM 2 INOP MESSAGE. AOM CHECKLIST FOLLOWED AND BOTH SYSTEMS RESET. ACCOMPLISHED EM

## 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 20091211052359I](https://openairdocs.org/incident/20091211052359I), Dec 11, 2009: Embraer EMB-135KL (N829AE), Raleigh, NC, No damage. Aircraft returned to rdu after takeoff with fuel indicator problems. System was mel'ed.

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