N108ML1994 Fokker F.28 MK 0100
This N-number isn't registered right now. Below is its last known registration, canceled Nov 1, 2002.
Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply12 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Wells Fargo Bank Northwest NA Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Sep 11, 1995
- Canceled
- Nov 1, 2002
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jan 12, 1995
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Fokker
- Model
- F.28 MK 0100
- Year
- 1994
- Serial number
- 11484
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 111
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- A0238A
Engine
- Make and model
- Rolls-Royc Tay 650-15
- Type
- Turbo-jet
- Power
- 15,100 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1995 – 2002Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (4)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2005-10-07 | Fokker Model F.28 Series Airplanes | Jun 21, 2005 | Airframe (F.28 MK 0100) |
| 2002-07-03 | Fokker Model F.28 Series Airplanes | Apr 19, 2002 | Airframe (F.28 MK 0100) |
| 2001-22-08 | Fokker Model F.28 Series Airplanes | Dec 4, 2001 | Airframe (F.28 MK 0100) |
| 96-13-05 | Fokker Model F28 Series Airplanes (Excluding Model F28 Mark 0100 Series Airplanes) | Jul 26, 1996 | Airframe (F.28 MK 0100)Certain serial numbers: 11003–11241; 11991; 11992. Only with: Excluding Model F28 Mark 0100 series airplanes. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (12)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Engine oil · transmitter · faultyJul 11, 2001
AT 500 FT AFTER T/O AT TPA OIL PRESS LIMIT ENG NR 2 FAULTED. REMOVED AND REPLACED NR 2 ENG OIL PRESSURE TRANSMITTER IAW AMM 77-47-01. LEAK AND OPS CHECK GOOD. GROUND RAN NR 1 & 2 ENGINES TO TOGA (1171 EPR) POWER IAW AMM 71-00-00. NO FAULTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · shaft · shearedOct 18, 2000
NR 1 ENGINE WOULD NOT SPOOL BEYOND 10 PERCENT N2. REPLACED NR 1 STARTER IAW AMM 80-11-01,OPS CK BAD. SHEARED STARTER SHAFT. NR 1 ENGINE GEARBOX JAMMED. REMOVED AND REPLACED NR 1 ENGINE IAW MIDWAY WORK PACKAGE WORK CARD F4604, LEAK AND OPS CK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · brake assy · leakingJun 1, 2000
TAXIING INTO RDU OTHER A/C REPORTED SMOKE COMING FROM LT MAIN WHEEL AREA. REMOVED AND REPLACED NR 2 BRAKE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Windows · windshield · crackedMar 30, 2000
CAPTAINS OUTER WINDSHIELD CRACKED AT FL 290 IN CRUISE. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW F-100 MM 56-11-00. REMOVED AND REPLACED WINDSHIELD HEAT CONTROLLER IAW F-100 AMM 30-45-01. OPERATIONAL TEST GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · o ring · failedNov 2, 1999
HYDRAULIC SYSTEM 1 LOW QUANTITY IN AIR. AIRCRAFT RETURNED TO RDU. FOUND SYSTEM NR 1 ENGINE NR 2 HYDRAULIC PUMP LEAKING AT OUTPUT LINE. QUICK DISCONNECT. REPLACED O-RING AND OPS CHECKED NR 1 SYSTEM HYDRAULIC PUMPS FOR ENGINE NR 1 AND NR 2. NO LEAKS FOUND IAW MM 29-11-01.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · transducer · failedJul 6, 1999
FLT 118 RDU TO SWF, ON TAKEOFF ROLL HAD LIFT DUMPER FAULT. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED NR 2 MAIN LANDING GEAR WHEEL SPEED TRANSDUCER IAW F-100 MM 32-45-22. NO DEFECTS NOTED, OKAY FOR SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · power sys · malfunctionedJun 9, 1999
CREW REPORTED, IN FLIGHT LOST LANDING GEAR DOWN INDICATION. ALSO, LIGHTS INOP ON LEFT HAND EFIS CONTROL PANEL, SELECTOR LIGHT INDICATION ON NR 1 COM CONTROL PANEL AND ADF CONTROL PANEL. EVERYTHING RETURNED TO NORMAL WHEN EXTERNAL POWER WAS CONNECTED. RAN BOTH ENGINES CHECKED ELECTRICAL POWER…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Autoflight · auto throttle · malfunctionedApr 7, 1998
BOTH AUTO THROTTLES FAULTED ON T/O ROLL, ABORTED AT 20 KNTS. INDICATED BOTH AUTO THROTTLES RESET AND NO AUTOLAND MESSAGE APPEARED ON THE MFDU. PERFORMED TEST OF FCC1 AND FCC2 IAW 22-11-00. PERFORMED TEST OF AUTO THROTTLES 1 AND 2 IAW 22-31-00, COULD NOT DUPLICATE ANY FAULT.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · retract mech · malfunctionedDec 9, 1997
RDU - FLT 1 - RIGHT MLG WILL NOT RETRACT AS REPORTED BY PILOT. PERFORMED FUNCTIONAL TEST OF LANDING GEAR. ALL LANDING GEAR INDICATION NORMAL AND GEAR RETRACTED NORMAL IAW F100 MM 32-00-00. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Hydraulic power · o-ring · failedNov 24, 1997
RDU - FLT 2 - LOST SYSTEM 1 HYD EN ROUTE DCA/RDU, CAPTAIN DEACTIVATED SYSTEM 1 HYD DECLARED EMERGENCY. LANDED AIRCRAFT SAFELY. RDU MAINTENANCE FOUND O-RING ON ENGINE NR 2 SYSTEM NR 1 HYD PUMP BAD. REMOVED AND REPLACED PRESSURE LINE O-RING AND BACK UP O-RING ON NR 1 HYD PUMP. GROUND RAN A/C. NO…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 12 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026