N109ML

Cancelled 2004

Deregistered aircraft · 1995 Fokker F.28 MK 0100 · Rolls-Royce TAY-650-15

Cancelled
August 16, 2004
Exported to
Netherlands
Status when cancelled
Valid registration
Serial number
11485
Year built
1995
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 10, 1995
Certificate issued
September 6, 1995
Last registry action
October 29, 2002
Mode S code
A02741
Owner type
Corporation

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.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N109ML and the event date: up to this one’s cancellation.

Service difficulty reports · 11

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

SDR JBXA000296Control Box · faultyIN FLIGHT THE ANTI-SKID FAULT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED ANTI-SKID CONTROL BOX IAW F100 AMM 32-45-01. SYSTEM OPS CHECKED GOOD.Jun 21, 2001 · N109ML · Fokker F28MK0100 · Brake Anti-Skid SectionSDR JBXA000272Transmitter · failedRETURNED TO RDU DUE TO NR 2 ENGINE LOW OIL PRESSURE INDICATION. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE TRANSMITTER IAW 77-47-01. PERFORMED GROUND RUN OF ENGINE NR 2 AT DIFFERENT POWER SETTINGS. COULD NOT DUPLICATE LOW OIL PRESSURE. REF MDW NRC 14811Apr 22, 2001 · N109ML · Fokker F28MK0100 · Engine Oil PressureSDR JBXA000271Connector · dirtyAIRCRAFT INDICATED LOW OIL PRESSURE (NR 2 ENGINE) ON MFDU. FOLLOWED PROCEDURE AND MFDU SHOWED HIGH TGT INDICATION. FOLLOWED PROCEDURE AND RETURNED TO RDU. CLEANED CANNON PLUG ON OIL PRESSURER TRANSDUCER IAW AMM 79-32-01, TGT WITHIN LIMITS OF AMM 71-00-00 . Apr 21, 2001 · N109ML · Fokker F28MK0100 · Engine Oil PressureSDR JBXA00240Blade · nickedNICK FOUND IN NR 2 ENGINE FAN BLADE ON POST FLIGHT INSPECTION. REMOVED AND REPLACED NR 2 ENGINE IAW MIDWAY AIRLINES WORKCARDS F4624 AND 4622.Feb 24, 2001 · N109ML · Fokker F28MK0100 · Turbine Engine Compressor SectionSDR JBXA0000181Transducer · failedLIFTDUMP FAULTED ON TAKEOFF AT 90 KTS. ABORTED TAKEOFF. REMOVED AND REPLACED LT INBOARD WHEEL SPEED TRANSDUCER. OPS CHECK GOOD IAW F-100 AMM 32-42-02.Jun 11, 2000 · N109ML · Fokker F28MK0100 · Flight Control SystemSDR JBXA0000144Fire Bottle · leakingON TAXI OUT, HEARD LOUD HISS AND COCKPIT STARTED TO FILL WITH SMOKE. TURNED PACKS OFF AND SMOKE STOPPED. FOUND FLIGHT DECK FIRE EXTINGUISHER LEAKING. REMOVED AND REPLACED FLIGHT DECK FIRE EXTTIGUISHER IAW AMM 26-24-01.Feb 11, 2000 · N109ML · Fokker F28MK0100 · Fire Bottle, PortableSDR JBXA9900128Transducer · failedFLT 9 RDU - BOS, ON TAKEOFF AT APPROX 75 KTS HAD LIFT DUMPER FAULT ON LEFT MFDU. ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED OPS CHECK OF PSEU, NO FAULT NOTED. LIFT DUMPERS CHECKED GOOD IAW AMM 31-41-01. REMOVED AND REPLACED NR 4 WHEEL SPEED TRANSDUCERDec 13, 1999 · N109ML · Fokker F28MK0100 · Drag Control SystemSDR JBXA980045Fire Loop · malfunctionedAPU FIRE INDICATION (L) MFDU ON DESCENT. USED APU FIRE BOTTLE. INSPECTED APU COMPARTMENT, NO EVIDENCE OF ANY FIRE. ASSIGNED TO DMI 05457 PER MEL 49-00-1 - APU INOPERATIVE. (X)Jul 23, 1998 · N109ML · Fokker F28MK0100 · Fire DetectionSDR JBXA970027Door · crackedRDU - FLT 5 - RDU TO BOS AFTER TAEKOFF BIRDSTRIKE, AT BOS PERFORMED BIRDSTRIKE INSPECTION PER MIDWAY MM. FOUND DAMAGE TO RIGHT MLG DOOR. ISSUED FERRY PERMIT BOS/RDU. AIRCRAFT FLOWN GEAR DOWN AT 200 KNOTS. RDU MAINTENANCE REMOVED RIGHT MLG DOOR IAW AMM 52-8Dec 7, 1997 · N109ML · Fokker F28MK0100 · Landing Gear DoorsSDR JBXA00016Outflow Vlv · failedRDU - FLT 901 - LOST CABIN PRESSURIZATION CONTROL. BOTH CABIN PRESSURE CONTROLLERS FAULTED, TRIED TO CONTROL MANUALLY WITH NO RESPONSE. ALL OXYGEN MASKS DEPLOYED. REPLACED PRIMARY OUTFLOW VALVE IAW AMM 21-51-03. OPS CHECK OF AUTO AND MANUAL SYSTEM GOOD. (Aug 6, 1996 · N109ML · Fokker F28MK0100 · Pressure Regulator/Outflow ValveSDR JBXA089502Relay · malfunctionedRDU/PBI - FLT 304 - AIR RETURNED TO RDU DUE TO LANDING GEAR HANDLE WOULD NOT LIFT. MAINTENANCE FOUND ANTI-RETRACTION SOLENOID DID NOT RETRACT. ENTERED A DEFERRED MAINTENANCE ITEM. SYSTEM OPERATED NORMALLY FROM TIME OF FIRST FAILURE. SUSPECT RELAY STICKING.Jul 25, 1995 · N109ML · Fokker F28MK0100 · Landing Gear Retraction/Extension System

Other aircraft with N109ML · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N109ML is registered now to the first aircraft listed.