# N106ML: Fokker F.28 MK 0100, registration cancelled 2001-07-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 12, 2001
- Exported to: France
- Status when cancelled: Triennial form not returned
- Airframe: [Fokker F.28 MK 0100](https://openairdocs.org/model/fokker-f-28-mk-0100) (registry code 4990807)
- Serial number: 11477
- Type of aircraft: Fixed wing multi engine
- Certificate issued: January 12, 1994
- Last registry action: July 9, 2001
- Mode S code: A01C1C
- 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/N106ML
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=106ML
- Page: https://openairdocs.org/deregistered/N106ML-2001-07-12

From the FAA registry file of October 28, 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 (9)

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

- [SDR JBXA000276](https://openairdocs.org/sdr/JBXA000276), Apr 30, 2001: WARNING LIGHT. ILLUMINATED. WHEN LEVELING AT 31,000 FT JAMMED STAB AMBER WARNING ON MFDU. PERFORMED AFCAS TEST IAW AMM 22-11-00, NO FAULTS FOUND. OPERATIONAL CHECK OF FLIGHT CONTROL SERVO 
- [SDR JBXA000207](https://openairdocs.org/sdr/JBXA000207), Oct 17, 2000: STRUCTURE. VIBRATION. LOUD VIBRATING NOISE ON TAKEOFF ROLL. PERFORMED HIGH SPEED TAXI AND ENGINE HIGH POWER RUN IAW F-100 AMM 71-00-00, NO FAULTS NOTED. VIBRATION SURVEY PERFORMED IA
- [SDR JBXA0000163](https://openairdocs.org/sdr/JBXA0000163), Apr 8, 2000: WARNING LIGHT. ILLUMINATED. FLT 650 RDU/BOS, NR 1 ENG THRUST REVERSER WARNING LIGHT FOR EXTENSION COMES ON AND OFF REPETIVELY DURING CLIMBOUT. ASSIGNED TO DMI NR 07968 PER MEL NR 78-30-1.
- [SDR JBXA0000162](https://openairdocs.org/sdr/JBXA0000162), Mar 31, 2000: FILTER. CLOGGED. AT FL 350 HYD SYS 1 OVERHEAT FAULT LIGHT ILLUMINATED. RETURNED TO RDU. REMOVED AND REPLACED NR 1 HYDRAULIC SYSTEM RETURN FILTER IAW AMM 29-13-05 AND NR 1 ENGINE
- [SDR JBXA0000141](https://openairdocs.org/sdr/JBXA0000141), Jan 24, 2000: CONNECTOR. CONTAMINATED. JAMMED STAB . CLEANED SWITCH AND HARNESS CANNON PLUG OPERATIONAL CHECK GOOD AT THIS TIME I-A-W AMM 27-43-04.
- [SDR JBXA9900076](https://openairdocs.org/sdr/JBXA9900076), Mar 17, 1999: O RING. WORN. NR 1 HYDRAULIC SYSTEM QUANTITY LOW (FOLLOWED OPS PROCEDURE, ALT LG EXTENSION). FOUND NR 2 ENGINE HYDRAULIC PUMP QUICK DISCONNECT FITTING O-RING WORN (LEAKING). 
- [SDR JBXA980035](https://openairdocs.org/sdr/JBXA980035), Mar 28, 1998: MANIFOLD. FAILED. RDU - FLT 375 - SYSTEM NR 2 RUDDER FAULTED. REMOVED AND REPLACED RUDDER MANIFOLD IAW F-100 MM 27-22-01, OPS CHECK GOOD. (M)
- [SDR JBXA980033](https://openairdocs.org/sdr/JBXA980033), Feb 11, 1998: PLA TRANSMITTER. OUT OF ADJUST. RDU - FLT 931 - ON TAKEOFF ROLL, AUTOTHROTTLES ARMED AND ENGAGED. INSUFFICIENT POWER AND NO AUTOTHROTTLE MOVEMENT. TAKEOFF ABORTED AT APPROX 70 KTS. RDU MX ADJU
- [SDR JBXA9500002](https://openairdocs.org/sdr/JBXA9500002), Nov 3, 1995: HYDRAULIC PUMP. LEAKING. ABE/RDU - FLT 670 - LOW HYDRAULIC QUANTITY SYSTEM 1 DURING FLIGHT. UPON INSPECTION IN RDU FOUND O-RING ON NR 1 SYSTEM RT ENGINE HYDRAULIC PUMP CUT. REPLACED O-R

## Other aircraft with N106ML

- [Registered now](https://openairdocs.org/aircraft/N106ML): Raytheon C90GT, S/N LJ1757

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