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Aircraft record

N850US1989 Fokker F.28 MK 0100

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 28, 2003.

Safety record in brief:1 NTSB incident (Nov 1990)4 ADs may apply18 service difficulty reports

Registration
Deregistered
Last based in
Wilmington, DE
owner city / state
Owners
1
since 2003
NTSB events
1
1990
ADs may apply
4
confirm with A&P
Service reports
18
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Wilmington Trust Co Trustee
Owner type
Corporation
City, state
Wilmington, DE
Certificate issued
Apr 14, 2003
Canceled
May 28, 2003
Airworthiness
Standard · Transport
Airworthiness date
Aug 31, 1989

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 data

Airframe

Manufacturer
Fokker
Model
F.28 MK 0100
Year
1989
Serial number
11276
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
ABA92B

Engine

Type
Turbo-jet

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2003Wilmington Trust Co TrusteeWilmington, DE

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Incident

Nov 11, 1990 · Atlanta, GA

FROZEN MOISTURE IN THE STABILIZER ACTUATOR HYDRAULIC SERVO VALVE WHICH RESULTED IN REDUCED MOVEMENT OF THE SERVO VALVE AND LIMITED ITS ABILITY TO RESPOND TO FLIGHT CONTROL INPUTS. THE LACK OF RESPONSE FROM THE SERVO VALVE RESULTED IN THE JAMMED STABILIZER MESSAGE. A FACTOR WAS THE INADEQUATE DESIGN OF THE SERVO VALVE WHICH PRECLUDED MOISTURE DRAINAGE.

Injuries
None
Report
ATL91IA017

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ATL91IA017)

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.

ADSubjectEffectiveApplies to
2005-10-07Fokker Model F.28 Series AirplanesJun 21, 2005Airframe (F.28 MK 0100)
2002-07-03Fokker Model F.28 Series AirplanesApr 19, 2002Airframe (F.28 MK 0100)
2001-22-08Fokker Model F.28 Series AirplanesDec 4, 2001Airframe (F.28 MK 0100)
96-13-05Fokker Model F28 Series Airplanes (Excluding Model F28 Mark 0100 Series Airplanes)Jul 26, 1996Airframe (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 (18)

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.

  • Lights · relay · faultyAug 22, 2001

    PHL - FLT 2249 - EN-ROUTE MHT-PHL, THE EMERGENCY EXIT LIGHTS WOULDN'T ILLUMINATE WHEN THE LANDING GEAR WAS EXTENDED. MAINTENANCE REPLACED EXIT LIGHTING RELAY K2618A. OPERATIONALLY CHECKED OK. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedJul 17, 2000

    PIT - FOUND TWO HOLES IN SKIN .75 INCH BY .5 INCH AND .5 INCH BY .25 INCH, RT SIDE STATION 29959 AFT OF APU EXHAUST. REPAIRED PER SRM 53-00-02, INSTALLED REPAIR DOUBLER. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedJul 17, 2000

    PIT - FOUND A HOLE IN SKIN .5 INCH BY .375 INCH, STATION 28868 RT SIDE AFT OF APU EXHAUST. REMOVED DOUBLER, FABRICATED NEW DOUBLER PER SRM 53-00-02. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Lights · battery pack · dischargedSep 8, 1998

    IND - LOW LEVEL EMERGENCY FLOOR LIGHTS INOPERATIVE AFT OF ROW 16. MAINTENANCE REPLACED THE 6 VOLT INVERTER AND TWO BATTERY PACKS. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · inverter · inoperativeSep 8, 1998

    IND - LOW LEVEL EMERGENCY FLOOR LIGHTS INOPERATIVE AFT OF ROW 16. MAINTENANCE REPLACED THE 6 VOLT INVERTER AND TWO BATTERY PACKS. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery pack · dischargedMar 22, 1998

    IND - MAINTENANCE FOUND TWO INOPERATIVE CEILING EMERGENCY LIGHTS IN MID CABIN. MAINTENANCE REPLACED THE BATTERY PACK. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · switch · failedJan 13, 1998

    PIT - FLT 670 - ON TAKEOFF, THE LANDING GEAR WOULD NOT COME UP. OVERRIDE WAS USED AND GEAR CAME UP. TAKEOFF CONFIGURATION RED WARNING MESSAGE. THEN FLT/GRD CONFIGURE AMBER MESSAGE, RED WARNING WENT OUT; ALSO, GOT ANTI-SKID AMBER MESSAGE AND STAB TRIM INDICATOR RAN TO FULL DOWN, SOME DOWN PRESSURE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · power supply · failedMay 25, 1997

    IND - FOUND AISLE EMERGENCY LIGHTS AT ROWS 4 AND 5 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK POWER SUPPLY. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · synchronizer · failedJan 25, 1997

    FLT 271 - RIC-LGA - AFTER TAKEOFF, FLAPS WOULD NOT RETRACT PAS 8 DEGREES. NO EMERGENCY WAS DECLARED. FLIGHT RETURNED TO RIC WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT OUTBOARD FLAP SYNCHRO. (M)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · outflow valve · failedOct 4, 1996

    AVL-CLT - FLT 1062 - AFTER TAKEOFF, NR 1 AUTOPRESSURE FAILED. NR 2 AUTOPRESSURE WAS ON MEL. CAPTAIN WENT TO MANUAL AND WAS UNABLE TO CONTROL PRESSURE. FLIGHT CLIMBED TO FL060 AND CABIN PRESSURE ALTITUDE CLIMBED 2000 FPM. CREW DESCENDED AND SHUT DOWN PACKS. FLIGHT RETURNED TO AVL WITHOUT FURTHER…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 18 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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