# Fokker F.27MK 100

- Type: Aircraft model (FAA registry)
- Registry code: 4990617
- Manufacturer (registry): FOKKER
- Model: F.27MK 100
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 55
- Weight class: 20,000 lb and over
- Cruise speed: 222 mph
- Certification: Type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/fokker-f-27mk-100

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft

None registered with this model now.

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA84AA014](https://openairdocs.org/ntsb/DCA84AA014), Jan 13, 1984: Fokker F27-100 (N148PM), Jamaica, NY, substantial damage
- [NTSB NYC83LA036](https://openairdocs.org/ntsb/NYC83LA036), Nov 30, 1982: Fokker F-27-100 (N141PM), New Haven, CT, substantial damage

## FAA accident and incident reports (3)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19880410070359I](https://openairdocs.org/incident/19880410070359I), Apr 10, 1988: Fokker F27MK100 (N141PM), Atlantic City, NJ, Minor damage. Aircraft jumped chocks on engine start. Hit power cart. Passengers exited aircraft before stairs were lowered.
- [Accident 19840113000789A](https://openairdocs.org/incident/19840113000789A), Jan 13, 1984: Fokker F27MK100 (N148PM), Jamaica, NY, Substantial damage. Lost both engines on takeoff due to ice ingestion. Crew ignored airframe prior icing. Failed to check engine inlets
- [Accident 19821130060749A](https://openairdocs.org/incident/19821130060749A), Nov 30, 1982: Fokker F27MK100 (N141PM), New Haven, CT, Substantial damage. Right propeller struck the APU cart while moving out of gate area. Taxi began before cart was moved away completely

## Service difficulty reports (7)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA031209001](https://openairdocs.org/sdr/CA031209001), Aug 10, 2003: REGULATOR. MISINSTALLED. (CAN) NR 2 ENGINE FAILED TO ACCELERATE AT ALTITUDE DURING ALPHA FLOOR PROTECTION TEST. (AIRCRAFT SLOWS TO MINIMUM SPEED. AUTO THROTTLE SHOULD KICK IN AND ACCELE
- [SDR CA020304006](https://openairdocs.org/sdr/CA020304006), Feb 22, 2002: SLEEVE. MISREPAIRED. (CAN) TWO FUEL FLOW REGULATORS RECEIVED HAD SLIPPER SLEEVE ASSEMBLIES INSTALLED IN REVERSE MODE. THESE UNITS HAD BEEN PREVIOUSLY REPAIRED BY ROLLS ROYCE BRAZIL 
- [SDR JBXA000199](https://openairdocs.org/sdr/JBXA000199), Aug 21, 2000: TIRE. DAMAGED. WHEN POWER WAS APPLIED AND A/C BEGAN TO ROLL THERE WAS A HEAVY VIBRATION COMING FROM THE NOSE GEAR. ABORTED AT 40 KTS. REMOVED AND REPLACED NOSE TIRES.
- [SDR 99ZZZX2069](https://openairdocs.org/sdr/99ZZZX2069), Apr 14, 1999: SEAL. FAILED. THE LP ROTOR WAS FREE TO ROTATE AND THE HP ROTOR WAS CONFIRMED AS BEING SEIZED. THERE WAS NO APPRECIABLE BACKLASH NOTED WHILE ATTEMPTING TO ROTATE THE HP ROTOR.
- [SDR AU980693](https://openairdocs.org/sdr/AU980693), Jun 27, 1998: SUPERCHARGER. FAILED. (AUS) RIGHT ENGINE DRIVEN CABIN SUPERCHARGER FAILED. GEARBOX CHIP DETECTOR CONTAMINATED WITH METAL. PART TOTAL CYCLES: 1,611.
- [SDR AU980694](https://openairdocs.org/sdr/AU980694), Jun 17, 1998: WINDSHIELD. CRACKED. (AUS) PILOT'S WINDSCREEN OUTER PANEL CRACKED.
- [SDR AU961030](https://openairdocs.org/sdr/AU961030), Jul 1, 1996: HOSE. FRAYED. (AUS) FUEL PUMP COLLECTOR TANK TO FIREWALL FUEL HOSE LOCATED IN RH WHEEL WELL FRAYED AND WORN - CAUSED BY INCORRECT FITMENT OF GREASE NIPPLE ON LANDING GEAR - P

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