# N720AE: 2000 Embraer EMB-135LR, registration cancelled 2019-09-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 9, 2019 - Status when cancelled: Valid registration - Airframe: [Embraer EMB-135LR](https://openairdocs.org/model/embraer-emb-135lr) (registry code 3260305) - Engine: [Allison AE3007C series](https://openairdocs.org/engine/allison-ae3007c-series) (registry code 03028) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 145279 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 8, 2000 - Certificate issued: December 17, 2018 - Last registry action: December 17, 2018 - Mode S code: A9A391 - Owner when cancelled: [Kingman Airline Services Inc](https://openairdocs.org/faa-owner/KINGMAN%20AIRLINE%20SERVICES%20INC) - Location: [Kingman, AZ](https://openairdocs.org/faa-place/AZ/Kingman) - Owner type: Corporation - Owner's area on the map: 35.0799° N, 113.7486° W: Placed by OpenAirDocs at the center of ZIP code 86401, within about 20 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N720AE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=720AE - Page: https://openairdocs.org/deregistered/N720AE-2019-09-09 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-135LR: https://openairdocs.org/model/embraer-emb-135lr.md ## Service difficulty reports (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SIMA20131024007](https://openairdocs.org/sdr/SIMA20131024007), Oct 24, 2013: PANEL. MISINSTALLED. LEFT OVERWING EMERGENCY EXIT BINDING AND WILL NOT OPEN. ACFT REMOVED FOR SERVICE. REMOVED AND REINSTALLED SIDEWALL PANEL THAT SURROUNDS LT OVERWING EXIT CORRECT - [SDR SIMA20131024006](https://openairdocs.org/sdr/SIMA20131024006), Oct 24, 2013: LIGHT. INOPERATIVE. MID CABIN EMERGENCY LIGHT ON CEILING IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-50-13. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE. - [SDR SIMA20131005004](https://openairdocs.org/sdr/SIMA20131005004), Oct 5, 2013: SIGN. INOPERATIVE. OVERHEAD CEILING, AISLE, EMERGENCY LIGHT AT EMERGENCY EXIT ROW INOPERATIVE. R & R SIGN ASSY AT EMERGENCY ROW IAW MM 33-50-15, OPS CHECKED GOOD. - [SDR SIMA20130924004](https://openairdocs.org/sdr/SIMA20130924004), Sep 24, 2013: LIGHT. OBSTRUCTED. EMERGENCY FLOOR LIGHTS COVERED BY CARPET, ROWS 2-5. RELOCATED CENTER FLOOR COVERING IAW AMM 25-24-01. OPS CHECK GOOD. - [SDR SIMA20130826004](https://openairdocs.org/sdr/SIMA20130826004), Aug 26, 2013: ENGINE. POWER LOSS. CREW REPORTED DURING CRUISE FLT, NR 1 ENGINE FUEL IMPELLER BYPASSED ILLUMINATED ON EICAS. NR 1 ENGINE WOULD NOT PRODUCE FULL POWER AND ENGINE WAS SPUTTERING LIK - [SDR SIMA20130625001](https://openairdocs.org/sdr/SIMA20130625001), Jun 25, 2013: HANDLE. DETACHED. DURING MX INSPECTION, FOUND MAIN DOOR INSIDE HANDLE DETACHED. ACFT REMOVED FROM SERVICE. INSTALLED MAIN DOOR HANDLE IAW AMM 52-11-01. OPS CHECKED GOOD. ACFT RET - [SDR SIMA20130513001](https://openairdocs.org/sdr/SIMA20130513001), May 12, 2013: DAU. INOPERATIVE. ON FLIGHT 4471 THE CREW REPORTED THEY HAD ELECTRICAL PROBLEMS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LGA. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIR - [SDR SIMA20130509005](https://openairdocs.org/sdr/SIMA20130509005), May 9, 2013: CRADLE. BROKEN. DURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S EMERGENCY FLASHLIGHT CRADLE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FIRS - [SDR SIMA20130301003](https://openairdocs.org/sdr/SIMA20130301003), Mar 1, 2013: CRADLE. DEFECTIVE. ON FLIGHT 3337 THE CREW REPORTED THE EMERGENCY FLASHLIGHT CRADLE AFT-ON LAV WALL DOES NOT HOLD FLASHLIGHT IN PLACE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOV - [SDR SIMA20121121012](https://openairdocs.org/sdr/SIMA20121121012), Nov 21, 2012: LIGHT. INOPERATIVE. DURING B INSPECTION FOUND THE RIGHT AFT OVERWING EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AFT OVERWING - [SDR SIMA20120928007](https://openairdocs.org/sdr/SIMA20120928007), Sep 28, 2012: CRADLE. BROKEN. DURING MAINTENANCE INSPECTION FOUND THE CAPTAIN’S EMERGENCY FLASHLIGHT BASE, (CRADLE) BROKEN. WILL NOT HOLD FLASHLIGHT FIRM IN BASE. THE AIRCRAFT WAS REMOVED FR - [SDR SIMA20120914001](https://openairdocs.org/sdr/SIMA20120914001), Sep 11, 2012: ROLL PIN. UNSECURE. ON FLIGHT 2820 THE CREW REPORTED WHILE CLIMBING THROUGH 13,00 FEET THE CAPTAIN’S JUMP SEAT MALFUNCTIONED. THE SEAT WAS STUCK IN A 3/4 REAR POSITION, IT WOULD NO - [SDR SIMA20120821005](https://openairdocs.org/sdr/SIMA20120821005), Aug 21, 2012: BATTERY PACK. INOPERATIVE. DURING MAINTENANCE INSPECTION, FOUND THE EMERGENCY LIGHT BATTERY PACK NR 3 INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 EMER - [SDR SIMA20120510020](https://openairdocs.org/sdr/SIMA20120510020), May 10, 2012: FLASHLIGHT. INTERMITTENT. ON FLIGHT 2772 THE FLIGHT ATTENDANT REPORTED THE ENTRY DOOR FLASHLIGHT INTERMITTENTLY WORKED--NOT INDICATING CHARGING. THE AIRCRAFT WAS REMOVED FROM SERVICE. PE - [SDR SIMA20120425013](https://openairdocs.org/sdr/SIMA20120425013), Apr 25, 2012: FLASHLIGHT ASSY. BROKEN. FLIGHT 3228, CREW REPORTED THE FLIGHT ATTENDANT’S REAR CABIN FLASHLIGHT WILL NOT STAY IN THE HOLDER. FOUND AFT FLASHLIGHT HOLDER EAR BROKEN OFF. REMOVED AND REP - [SDR SIMA20120401007](https://openairdocs.org/sdr/SIMA20120401007), Apr 1, 2012: SMOKE DETECTOR. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE FORWARD CARGO SMOKE DETECTOR INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT SMOKE DET - [SDR SIMA2012051016](https://openairdocs.org/sdr/SIMA2012051016), Feb 18, 2012: INVERTER. INOPERATIVE. DURING B-INSPECTION, FOUND THE EMERGENCY EXIT SIGN OVER THE SERVICE DOOR INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 2 EMERGENCY LIG - [SDR SIMA2012032001](https://openairdocs.org/sdr/SIMA2012032001), Jan 31, 2012: LIGHT. INOPERATIVE. DURING MAINTENANCE INSPECTION FOUND THE AILSE EMERGENCY LIGHT AT SEAT 9A INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AILSE EMERG - [SDR SIMA2011301003](https://openairdocs.org/sdr/SIMA2011301003), Oct 26, 2011: MEDICAL KIT. UNSERVICEABLE. DURING MAINTENANCE BASE VISIT FOUND THE MEDICAL KIT SEAL BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE MEDICAL KIT IAW EMB-135 MM 25-6 - [SDR SIMA201118903](https://openairdocs.org/sdr/SIMA201118903), Jul 6, 2011: DOOR. BINDING. ON FLIGHT 3333 THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO CLOSE. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED MAIN CABIN DOOR FOR DEFECTS. MAINTENANC - [SDR SIMA201004610](https://openairdocs.org/sdr/SIMA201004610), Feb 14, 2010: BATTERY. DISCHARGED. DURING MAINTENANCE CHECK FOUND THAT ALL OF THE FORWARD CABIN EMERGENCY LIGHTS FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED - [SDR SIMA200726802](https://openairdocs.org/sdr/SIMA200726802), Sep 24, 2007: ACTUATOR. LEAKING. HYDRAULIC NR 1 LOW QUANTITY LEVEL WENT FROM TOP OF YELLOW TO BOTTOM OF YELLOW IN LESS THAN 40 MINUTES. DID NOT GET A HYDRAULIC FAIL MESSAGE. REMOVED AND REPLACE - [SDR SIAM200726003](https://openairdocs.org/sdr/SIAM200726003), Sep 16, 2007: INVERTER. MALFUNCTIONED. AS CREW SET THRUST 115V BUSS OFF LINE WITH ASSOCIATED MESSAGES. DID LOW SPEED ABORT AND RETURNED TO GATE. REMOVED AND REPLACED STATIC INVERTER IAW EMB135 AMM 24 - [SDR SIMA200722204](https://openairdocs.org/sdr/SIMA200722204), Aug 9, 2007: BALLAST. BURNED. ELECTRICAL ODOR IN CABIN AT SEAT 1A. FOUND BALLAST RT8425 AND RT8400 BURNED. REMOVED AND REPLACED BALLAST IAW EMB AMM 33-21-03. OPERATIONAL CHECK GOOD. RETURNED - [SDR SIMA200721402](https://openairdocs.org/sdr/SIMA200721402), Jul 31, 2007: CONTROL MODULE. BURNED. BURNING ODOR FROM GALLEY AREA. REMOVED AND REPLACED LIGHT BALLAST IAW EMB AMM 33-21-05 AND REMOVED AND REPLACED CONTROL MODULE ASSEMBLY IAW EMB AMM 33-21-01, BO - [SDR SIMA200720428](https://openairdocs.org/sdr/SIMA200720428), Jun 22, 2007: FLOOR SUPPORT. CORRODED. RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 203. RETURNED AIRCR - [SDR SIMA200720423](https://openairdocs.org/sdr/SIMA200720423), Jun 20, 2007: FLOOR SUPPORT. CORRODED. LEFT OMEGA BEAM CORRODED BETWEEN 24 AND 25. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW EMB SRM 53-00-10, FIGURE 202. RETURNED AIRCRAFT TO SERV - [SDR SIMA200720424](https://openairdocs.org/sdr/SIMA200720424), Jun 20, 2007: SILL. CORRODED. SERVICE DOOR SILL FOUND CORRODED. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02 AND 51-40-04. RETURNED AIRCRAFT TO SERVICE. - [SDR SIMA200530105](https://openairdocs.org/sdr/SIMA200530105), Oct 25, 2005: SKIN. PEELING. DURING MBV INSPECTION, FOUND RIGHT THRUST REVERSER OUTBOARD MIDDLE SKIN PEELING BACK ON LEADING EDGE. INSTALLED NEW RIGHT THRUST REVERSER OUTBOARD MIDDLE SKIN I - [SDR SIMA200530104](https://openairdocs.org/sdr/SIMA200530104), Oct 25, 2005: DOUBLER. CORRODED. DURING MBV INSPECTION, FOUND LEFT OMEGA RIGHT SIDE DOUBLER AT FRAME 20 IS CORRODED. INSTALLED NEW DOUBLER IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE. (M - [SDR SIMA200530103](https://openairdocs.org/sdr/SIMA200530103), Oct 25, 2005: PROFILE. CORRODED. SAW - DURING MBV INSPECTION, FOUND PROFILE Z AT FRAME 22 IS CORRODED. INSTALLED NEW PROFILE Z IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR SIMA200530102](https://openairdocs.org/sdr/SIMA200530102), Oct 25, 2005: FLOOR SUPPORT. CORRODED. SAW - DURING MBV INSPECTION, FOUND LEFT FLOOR SUPPORT RAMP BETWEEN FRAMES 19 AND 20 IS CORRODED. INSTALLED NEW FLOOR SUPPORT RAMP IAW EMB SRM 5-40-02. AIRCRAFT - [SDR SIMA200530101](https://openairdocs.org/sdr/SIMA200530101), Oct 25, 2005: FLOOR SUPPORT. CORRODED. SAW - DURING MBV INSPECTION, FOUND RIGHT FLOOR SUPPORT RAMP BETWEEN FRAMES 19 AND 20 IS CORRODED. INSTALLED NEW FLOOR SUPPORT RAMP IAW EMB SRM 51-40-02. AIRCRAF - [SDR SIMA200412704](https://openairdocs.org/sdr/SIMA200412704), May 1, 2004: ODOR. DETECTED. JFK - FLT 4754 - DURING CLIMB, CREW REPORTED A STRONG BURNING ODOR IN COCKPIT. AIRCRAFT WAS RETURNED TO JFK AND LANDED WITH NO FURTHER INCIDENTS REPORTED. MAINT - [SDR SIMA200408802](https://openairdocs.org/sdr/SIMA200408802), Mar 26, 2004: CONTROL UNIT. FAULTY. BNA- FLT 4856 - CREW REPORTED A DUAL PITCH TRIM FAIL ON DESCENT. AUTOPILOT WAS ON AND DID NOT TOUCH ANYTHING. RECEIVED FAILURE OF MAIN AND BACK UP PITCH TRIM AN - [SDR SIMA200326506](https://openairdocs.org/sdr/SIMA200326506), Sep 16, 2003: STRINGER. CHAFED. ABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFED BY BLENDING AREA. PERFOR - [SDR SIMA200326505](https://openairdocs.org/sdr/SIMA200326505), Sep 12, 2003: FLOORBEAM. CORRODED. ABI - DURING AN IMBV INSPECTION, THE TOP OF THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 20 REMOVED CORROSION BY CREATING A CUT OUT - [SDR SIMA200226106](https://openairdocs.org/sdr/SIMA200226106), Sep 16, 2002: WINDSHIELD. MALFUNCTIONED. JFK - FLT 4548 - CREW REPORTED A NOTICEABLE BURNING SMELL IN THE COCKPIT STARTING DURING CLIMB-OUT. AT APPROXIMATELY 14,000 FEET THE SMELL VARIED FROM VERY STRO - [SDR SIMA200208304](https://openairdocs.org/sdr/SIMA200208304), Feb 25, 2002: BEAM. CORRODED. ABI - THIS IS LEVEL 2 FINDING. CORROSION FOUND ON GALLEY RIGHT BEAM. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EMB GST-0636/02. (M) - [SDR SIMA200208301](https://openairdocs.org/sdr/SIMA200208301), Feb 25, 2002: FLOORBEAM. CORRODED. THIS IS A LEVEL 2 FINDING. CORROSION GALLEY FORWARD DIGITAL. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EMB GST-0634/02. (M) - [SDR SIMA200208302](https://openairdocs.org/sdr/SIMA200208302), Feb 25, 2002: GUSSET. CORRODED. ABI - THIS IS A LEVEL 2 FINDING. CORROSION GALLEY CENTER BEAM GUSSET. RESTORED PROTECTIVE COATING, DAMAGE ACCEPTED AS IS IAW EMB GST-0636/02. (M) - [SDR SIMA20011041](https://openairdocs.org/sdr/SIMA20011041), Apr 14, 2001: ENGINE. OVERTEMP. CHA - FLT 4418 - CREW REPORTED TO FIELD DUE TO NR 1 ENGINE TRYING TO OVERTEMP. AT CLIMB, NR 1 ENGINE WAS AT 800 DEGREES AND THE NR 2 AT 697 DEGREES. (M) - [SDR SIMA2332](https://openairdocs.org/sdr/SIMA2332), Aug 20, 2000: SMOKE DETECTOR. INOPERATIVE. BOS - FLT 5056 - LAVATORY FIRE INDICATION ON F/A PANEL 5 MINUTES AFTER TAKEOFF. PUT ON MEL. MAINTENANCE REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW EMB MM. --- 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.