# N104ML: Fokker F.28 MK 0100, registration cancelled 2001-03-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 7, 2001 - Exported to: Netherlands - 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: 11445 - Type of aircraft: Fixed wing multi engine - Certificate issued: November 10, 1993 - Last registry action: November 16, 1999 - Mode S code: A014AE - Owner when cancelled: [First Security Bank Na Trustee](https://openairdocs.org/faa-owner/FIRST%20SECURITY%20BANK%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/N104ML - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=104ML - Page: https://openairdocs.org/deregistered/N104ML-2001-03-07 From the FAA registry file of November 5, 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 (14) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR JBXA000211](https://openairdocs.org/sdr/JBXA000211), Nov 2, 2000: CONNECTOR. DIRTY. FLT 7 RDU/BOS - NR 1 ENG TGT INDICATES LARGE FLUCTUATIONS IN ALL PHASES OF FLIGHT. FUEL FLOW ON NR 1 INDICATES 300 - 400 LBS HIGHER THAN NR 2 ON HIGH POWER SETT - [SDR JBXA0000194](https://openairdocs.org/sdr/JBXA0000194), Aug 6, 2000: ENGINE. OVERTEMP. ABORTED TAKEOFF FLL, NR 2 ENGINE TGT WARNING TEMP WAS APPROX 875 PULLED BACK THRUST LEVERS TO 1.5 EPR TO ALLOW TGT TO DECREASE TO BELOW 735. PERFORMED OVER TEMP - [SDR JBXA0000148](https://openairdocs.org/sdr/JBXA0000148), Feb 20, 2000: THRUST REVERSER. MALFUNCTIONED. ENGINE NR 1 REVERSER MESSAGE ON CLIMB-OUT THROUGH 240. PERFORMED OPERATIONAL CHECK OF NR 1 THRUST REVERSER IAW AMM 78-30-00, OPS CHECK GOOD. - [SDR JBXA9900099](https://openairdocs.org/sdr/JBXA9900099), Aug 19, 1999: COMPUTER. MALFUNCTIONED. FLT 79 RDU/LGA- ON CLIMBOUT HAD STALL COMPUTER WARNING ASSOCIATED WITH MULTIPLE FAULTS ON RT MFDU. AIR RETURN TO RDU. PERFORMED OPERATIONAL CHECK OF STALL WARNI - [SDR JBXA9900093](https://openairdocs.org/sdr/JBXA9900093), Jul 24, 1999: ENGINE. VIBRATION. AFTER LIFTOFF IN RDU CREW GOT A VIBRATION HIGH ENG. NR 2 INDICATION ON INNER TAPE (N2). OCCURRED WITH VIBRATION SWITCH IN BOTH NORMAL AND ALTERNATE POSITIONS. C - [SDR JBXA9900070](https://openairdocs.org/sdr/JBXA9900070), Feb 25, 1999: PITOT HEAD. INOPERATIVE. FLT 112 RDU TO LGA, AFTER TAKEOFF PITOT NR 3 HEAT WARNING LMFDU. PITOT NR 3 HEAT FAULT WOULD NOT RESET. RETURNED TO RDU. REMOVED AND REPLACED NR 3 PITOT HEAD. O - [SDR JBXA9900068](https://openairdocs.org/sdr/JBXA9900068), Feb 18, 1999: DOOR. MISSING. ON WALK AROUND, FOUND APU SERVICE PANEL MISSING. REPLACED APU SERVICE PANEL IAW AMM 52-44-00. - [SDR JBXA9900066](https://openairdocs.org/sdr/JBXA9900066), Jan 25, 1999: BULB. FAILED. AFTER SELECTING LANDING GEAR UP ON TAKEOFF THE NOSE GEAR INDICATOR INDICATED THAT IT WAS STILL DOWN AND LOCKED. THE LANDING GEAR WAS CYCLED DOWN AND THEN UP TWI - [SDR JBXA980052](https://openairdocs.org/sdr/JBXA980052), Oct 1, 1998: UNION. CRACKED. INFLIGHT, HYDRAULIC SYSTEM NR 1 QUANTITY DOWN TO 34 PERCENT. AIRCRAFT DIVERTED TO EWR. TROUBLE SHOOTING, FOUND NR 1 SYSTEM LEAKING AT T-FITTING MLG HYDRAULIC TU - [SDR JBXA980034](https://openairdocs.org/sdr/JBXA980034), Mar 8, 1998: CONTROLLER. MALFUNCTIONED. RDU - FLT 304 - LT WINDOW HEAT FAULTED WHEN POWER APPLIED FOR TAKEOFF. CORRECTIVE ACTION: INSPECTED LT WINDSHIELD AND SIDE WINDOWS. NO DEFECTS NOTED. PERFORMED - [SDR JBXA970019](https://openairdocs.org/sdr/JBXA970019), Jul 20, 1997: HYDRAULIC PUMP. FAILED. NUMBER 1 HYDRAULIC SYSTEM LOW QUANTITY. CREW PREFORMED MANUAL GEAR EXTENTION DUE TO LOSS OF HYDRAULIC SYSTEM NUMBER 1. BOTH MAIN LANDING GEAR DOORS WHERE DAMAGE - [SDR JBXA970005](https://openairdocs.org/sdr/JBXA970005), Feb 24, 1997: FUEL FLOW REG. MALFUNCTIONED. AFTER TAKEOFF PARTIAL THORTTLE ONLY ON RIGHT ENGINE RETURN TO RDU PARTIAL POWER. REMOVED AND REPLACED RIGHT ENGINE FUEL FLOW REGULATOR IAW F-100 MM 73-21-01. PE - [SDR JBXA00033](https://openairdocs.org/sdr/JBXA00033), Dec 6, 1996: AUTO THROTTLE. MALFUNCTIONED. BDL - FLT 222 - NO AUTO THROTTLE ON FMA, ABORTED TAKEOFF AT BDL. PERFORMED AUTO THROTTLE SERVO TEST PER MM 22-31-01 AND AFCAS PANEL PROCEDURES PER MM 22-41-00. - [SDR JBXA00031](https://openairdocs.org/sdr/JBXA00031), Nov 25, 1996: AUTO THROTTLE. MALFUNCTIONED. BOS - FLT 552 - DURING TAKEOFF ROLL, ABORTED TAKEOFF DUE TO AUTO THROTTLE FAULT 1 AND 2 THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE PERFORMED THRUST REV ## Other aircraft with N104ML - [Cancelled 2012-06-14](https://openairdocs.org/deregistered/N104ML-2012-06-14): Chamberlain Mark R VANS RV-10, S/N 40016, built 2006. Exported to Australia. Owner: [Chamberlain Mark R](https://openairdocs.org/faa-owner/CHAMBERLAIN%20MARK%20R), [Temecula, CA](https://openairdocs.org/faa-place/CA/Temecula) --- 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.