# N10AH: 1990 Gates Learjet 35A, registration cancelled 2019-10-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 17, 2019
- Exported to: Australia
- Status when cancelled: Valid registration
- Airframe: [Gates Learjet 35A](https://openairdocs.org/model/gates-learjet-35a) (registry code 5170602)
- Engine: [Garrett TFE731 series](https://openairdocs.org/engine/garrett-tfe731-series) (registry code 29001)
- Data sheets: [TCDS A10CE](https://openairdocs.org/tcds/A10CE), [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (OpenAirDocs)
- Serial number: 657
- Year built: 1990
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 2, 1990
- Certificate issued: August 26, 2019
- Last registry action: August 26, 2019
- Mode S code: A00263
- Owner when cancelled: [Gateway Air Center Inc](https://openairdocs.org/faa-owner/GATEWAY%20AIR%20CENTER%20INC)
- Location: [Merced, CA](https://openairdocs.org/faa-place/CA/Merced)
- Owner type: Corporation
- Owner's area on the map: 37.3431° N, 120.4100° W: Placed by OpenAirDocs at the center of ZIP code 95340, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N10AH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=10AH
- Page: https://openairdocs.org/deregistered/N10AH-2019-10-17

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

## Service difficulty reports (10)

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

- [SDR G1IA2019031100000](https://openairdocs.org/sdr/G1IA2019031100000), Mar 7, 2019: LIGHT. INOPERATIVE. FAR 135.415 REPORT. PILOT REPORTS "AFTER T/O COPILOT REACHED FOR GEAR HANDLE AND AFTER RETRACTION HE NOTICED THAT PRIOR TO GEAR RETRACTION, THE NOSE GEAR DOWN &
- [SDR G1IA2018012110AH](https://openairdocs.org/sdr/G1IA2018012110AH), Jan 21, 2018: REGISTER. OBSTRUCTED. CABIN CREW REPORTED LIGHT WHITE SMOKE IN THE CABIN, 10 MINUTES BEFORE LANDING. SMOKE APPEARED TO BE MOMENTANEOUS AND NOT APPARENT TO THE FLIGHT CREW. THE SMOKE 
- [SDR G1IA2017022210AH1](https://openairdocs.org/sdr/G1IA2017022210AH1), Feb 22, 2017: CONTROL SWITCH. STICKING. PILOT REPORTED AFTER DEPARTURE, PRIMARY PITCH TRIM CONTINUED TO RUN AFTER COPILOT RELEASED THE SWITCH. EXECUTED PITCH TRIM MALFUNCTION EMERGENCY CHECKLIST AND R
- [SDR G1IA20160225001](https://openairdocs.org/sdr/G1IA20160225001), Feb 23, 2016: WARNING SYSTEM. FALSE ACTIVATION. FLYING WITH A PATIENT, TWO PILOTS & TWO MEDICS. WE WERE AWARE OF ADVISORIES FOR SEVERE TURBULENCE AT HIGHER ALTITUDES SO WE WERE AT FL260, 280 - 290KNOTS, AT AB
- [SDR G1IA20151015001](https://openairdocs.org/sdr/G1IA20151015001), Oct 12, 2015: UNKNOWN. ODOR. FAR 135.415 REPORT, DURING ROUTINE CHECK FLIGHT, WHILE TESTING STAB HEAT, AN ENVIRONMENTAL BURNING SMELL WAS NOTICED AS SOON AS THE STAB HEAT WAS TURNED ON. SME
- [SDR 2010FA0000396](https://openairdocs.org/sdr/2010FA0000396), Apr 21, 2010: LINE. CHAFED. THE SOURCE OF A FUEL LEAK WAS TRACED TO THE RT MAIN FUEL LINE TO THE FILTER AND SHUTOFF VALVE IN THE AFT EQUIPMENT BAY JUST FWD OF THE RT MAIN SHIP BATTERY. THE
- [SDR 2002FA0001181](https://openairdocs.org/sdr/2002FA0001181), Oct 13, 2002: COMPUTER. MALFUNCTIONED. NOSE WHEEL STEERING WILL NOT ARM. FOUND NO OUTPUT VOLTAGE ON P224 PIN A. 1.0 VAC REQUIRED FROM THIS PIN.
- [SDR 2002FA0000264](https://openairdocs.org/sdr/2002FA0000264), Mar 13, 2001: SOLENOID. INTERMITTENT. SPOILER OPERATION INTERMITTENT. MAINIFOLD ASSEMBLY HAS TWO SOLENOIDS, APPEARS THAT ONE MAY BE STICKING OR HAVE AN ELECTRICAL PROBLEM.
- [SDR 2000ZZZX373](https://openairdocs.org/sdr/2000ZZZX373), Jan 20, 2000: ROD END. WORN. DURING A 1,200 HOUR T/R INSPECTION, FOUND WORN ACTUATOR ROD END BUSHING BRACKET. THE BRACKETS ARE ACTUALLY PART OF THE THRUST REVERSER DOOR. THEY ARE CAST INTO 
- [SDR 99ZZZX1727](https://openairdocs.org/sdr/99ZZZX1727), Apr 9, 1999: BRACKET. CRACKED. BRACKET CRACKED AT OPPOSITE END OF WHERE ACTUATOR MOUNTS. LEFT FLAP ACTUATOR BRACKET FOUND CRACKED AT INSPECTION. THE ENTIRE BRACKET IS COMPOSED OF 5 PIECES. TH

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