# N110ML: 1995 Fokker F.28 MK 0100, registration cancelled 2003-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 2003
- Exported to: Netherlands
- Status when cancelled: Valid registration
- Airframe: [Fokker F.28 MK 0100](https://openairdocs.org/model/fokker-f-28-mk-0100) (registry code 4990807)
- Engine: [Rolls-Royce TAY-650-15](https://openairdocs.org/engine/rolls-royce-tay-650-15) (registry code 54557)
- Data sheets: [TCDS E25NE](https://openairdocs.org/tcds/E25NE) (OpenAirDocs)
- Serial number: 11486
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 24, 1995
- Certificate issued: August 8, 1995
- Last registry action: October 29, 2002
- Mode S code: A02D51
- Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%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/N110ML
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=110ML
- Page: https://openairdocs.org/deregistered/N110ML-2003-02-03

From the FAA registry file of November 12, 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 Fokker F.28 MK 0100: https://openairdocs.org/model/fokker-f-28-mk-0100.md

## Service difficulty reports (11)

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

- [SDR JBXA000315](https://openairdocs.org/sdr/JBXA000315), Aug 8, 2001: POWERPLANT. OVERTEMP. #1 ENGINE OVERTEMPERATURE/860 DEGREE'S FARENHEIT. CORRECTIVE ACTION: PERFORMED TAY SB 77-1454 IAW TAY 77-1454. CHANGE RESISTOR AFROM CM TO CK. PERFORMED ACCEL A
- [SDR JBXA000297](https://openairdocs.org/sdr/JBXA000297), Jun 22, 2001: ENGINE. MALFUNCTIONED. HIGH EGT APPROACHING REDLINE DURING TOGA TAKEOFF RDU. PEAK TGT 850 FOR 1 SECOND. PERFORMED OPS CHECK OF NR 1 ENGINE TOGA EGT IAW AMM 71-00-00, NO FAULTS NOTED E
- [SDR JBXA000291](https://openairdocs.org/sdr/JBXA000291), Jun 10, 2001: AUTOTHRUST SYS. MALFUNCTIONED. FLT 555 RDU/LGA AUTOTHROTTLE NR 1 AND 2 FAULTED ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. RESET FCC AND FAC NR 1 AND 2 AUTOTHROTTLE, OPS CHECK GOOD IAW 
- [SDR JBXA000279](https://openairdocs.org/sdr/JBXA000279), May 10, 2001: OUTFLOW VALVE. FAILED. CABIN PRESSURE CONTROL FAULT CAME ON AFTER TAKEOFF, CABIN WOULD NOT PRESSURIZE. PLACED CONTROL SWITCH TO MANUAL CABIN STILL WOULD NOT PRESSURIZE. RETURNED TO RD
- [SDR JBXA00267](https://openairdocs.org/sdr/JBXA00267), Apr 18, 2001: CONTROLLER. MALFUNCTIONED. CABIN WILL NOT PRESSURIZE AFTER TAKEOFF. COULD NOT CONTROL MANUALLY. PULLED AND RESET C/B FOR CABIN PRESSURE CONTROLLER. PERFORMED OPERATIONAL CHECK OF CABIN PR
- [SDR JBXA000249](https://openairdocs.org/sdr/JBXA000249), Feb 25, 2001: TRANSDUCER. FAILED. LIFT DUMPER FAULTED ON TAKEOFF ROLL 80-90 KNOTS. FOUND RIGHT OUTBOARD WHEEL SPEED TRANSDUCER FAULTING. REMOVED AND REPLACED NR 4 WHEEL SPEED TRANSDUCER IAW AMM 
- [SDR JBXA000248](https://openairdocs.org/sdr/JBXA000248), Feb 18, 2001: BRAKE ASSY. FAILED. GATE RETURN. BRAKES RELEASED WITH BRAKE APPLICATION SEVERAL TIMES. SET PARKING BRAKE, PUSHED ANTI-SKID TEST, BRAKES RELEASED WITH AIRCRAFT MOVEMENT. TOWED AIRCR
- [SDR JBXA000235](https://openairdocs.org/sdr/JBXA000235), Jan 11, 2001: WARNING LIGHT. ILLUMINATED. LIFT DUMPER FAULT MESSAGE DISPLAYED INTERMITTENTLY. ABORTED TAKEOFF. CLEARED FAULT, AIRCRAFT DEPARTED NORMALLY, NO FURTHER FAULTS.
- [SDR JBXA970014](https://openairdocs.org/sdr/JBXA970014), Apr 21, 1997: PRESS SWITCHES. FAILED. RDU - FLT 443 - AT 10,000 FEET AS A/C ACCELERATED RUD1 AND RUD2 FAULTED WITH YAW DAMP 1 AND 2 AND ALSO STAB TRIM FAULTS 1 AND 2. BOTH RUDDER FAULTS RESET AT 3,0
- [SDR JBXA970013](https://openairdocs.org/sdr/JBXA970013), Apr 18, 1997: FCC. FAILED. RDU - FLT 771 - AIR RETURN DUE TO RUDDER FAULT 1 AND 2, STABILIZER TRIM 1 AND 2 AND YAW DAMPER 1 AND 2 FAULTS ALSO, HAD AFCAS MX REQUIRED MESSAGE. REMOVED AND R
- [SDR JBXA00029](https://openairdocs.org/sdr/JBXA00029), Nov 18, 1996: AUTOTHROTTLE. MALFUNCTIONED. RDU - FLT 771 - BOTH AUTOTHROTTLES FAULTED PRIOR TO 80 KNOTS, ABORTED TAKEOFF. CORRECTIVE ACTION: PERFORMED AFCAS MAINTENANCE, SHOWED TOGA SWITCH, FCC1, FCC2. R

## Other aircraft with N110ML

- [Cancelled 2021-05-08](https://openairdocs.org/deregistered/N110ML-2021-05-08): Boeing 747-406, S/N 24201. Registration expired, pending cancellation. Owner: [Iag Trading LLC](https://openairdocs.org/faa-owner/IAG%20TRADING%20LLC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami)

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