# N360LJ: 1980 Gates Learjet 35A, registration cancelled 2010-03-09

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 9, 2010
- Exported to: Venezuela
- Status when cancelled: Valid registration
- Airframe: [Gates Learjet 35A](https://openairdocs.org/model/gates-learjet-35a) (registry code 5170602)
- Engine: [AiResearch TFE731 series](https://openairdocs.org/engine/airesearch-tfe731-series) (registry code 01518)
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE) (OpenAirDocs)
- Serial number: 360
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-jet
- Airworthiness: Standard, transport
- Airworthiness date: October 25, 1980
- Certificate issued: January 16, 2009
- Last registry action: January 16, 2009
- Mode S code: A40D4F
- Owner when cancelled: [Expectra Aviation Inc](https://openairdocs.org/faa-owner/EXPECTRA%20AVIATION%20INC)
- Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover)
- Owner type: Corporation
- Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N360LJ
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=360LJ
- Page: https://openairdocs.org/deregistered/N360LJ-2010-03-09

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 Gates Learjet 35A: https://openairdocs.org/model/gates-learjet-35a.md

## Service difficulty reports (4)

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

- [SDR DELA20040004](https://openairdocs.org/sdr/DELA20040004), Dec 2, 2004: CONTROL VALVE. FAILED. FLT CREW REPORTED DURING CLIMB TO 12,000 FT, CABIN ALTITUDE WARNING AND EMERGENCY PRESSURIZATION SYSTEM ACTIVATED. FLT CREW FOLLOWED THE "LOSS OF PRESSURIZATION
- [SDR 2004F00143](https://openairdocs.org/sdr/2004F00143), Mar 16, 2004: SWITCH. FAILED. DURING TAXI, WITH ANTI-SKID SYSTEM ON, HYDRAULIC PRESSURE WAS PRESENT BUT NO BRAKING ACTION OCCURRED. FURTHER INVESTIGATION REVEALED THAT THE RIGHT MLG DOWN SAF
- [SDR 2004F00099](https://openairdocs.org/sdr/2004F00099), Feb 6, 2004: TRANSDUCER. MALFUNCTIONED. CREW REPORTED ERRATIC BRAKING WITH ANTI-SKID SYSTEM ENGAGED. FURTHER INVESTIGATION FOUND THAT THE ANTI-SKID 'OFF' LIGHTS WOULD FAIL TO COME ON AND WOULD NOT RES
- [SDR 20010430CW011](https://openairdocs.org/sdr/20010430CW011), Apr 10, 2001: MODULE. DEFECTIVE. DURING A PREFLIGHT, NR 1 ALTIMETER C/B TRIPPED AND WOULD NOT RESET. AFTER TROUBLESHOOTING FOUND SDC MODULE DEFECTIVE WITH MOISTURE. THE TRIP WAS MOVET TO A LR55

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