# Service difficulty reports: Fokker F.28 MK 1000

A list on [Fokker F.28 MK 1000](https://openairdocs.org/model/fokker-f-28-mk-1000.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 15 · 704 reports

- [SDR CA051012009](https://openairdocs.org/sdr/CA051012009.md): Skin · cracked · Oct 2, 2005 · Fokker F28MK1000 · Emergency Exits
  > DURING SERVICE CHECK, 13 INCH CRACK DISCOVERED ON EXTERNAL SKIN OF FWD SERVICE/EMERGENCY DOOR. NO REPLACEMENT DOOR WAS IN STOCK. REPAIRS WERE COMPLETED AS PER STRUCTURAL REPAIR MANUAL. THIS AREA IS COVERED BY STRUCTURAL INSPECT PROGRAM WHICH IS COMPLETED EV
- [SDR CA030106012](https://openairdocs.org/sdr/CA030106012.md): Ecu · malfunctioned · Jan 3, 2003 · Fokker F28MK1000 · Fire Detection
  > (CAN) THE SUBJECT AIRCRAFT HAVE BAGGAGE COMPARTMENT SMOKE DETECTION AND FIRE SUPPRESSION SYSTEM INSTALLED, SUPLEMENTAL TYPE CERTIFICATE SA02-134. THE FIRE SUPPRESSION SYSTEM INCLUDES TWO HALON BOTTLES, DIVERTER VALVES, AND ASSOCIATED PIPING AND HALON NOZZLES.
- [SDR CA020725011](https://openairdocs.org/sdr/CA020725011.md): Squat Switch · failed · Jul 21, 2002 · Fokker F28MK1000 · Landing Gear Position and Warning
  > (CAN) T/O WAS REJECTED AT APPROX 60/70 KNOTS DUE TO T/O WARNING HORN ASSOCIATED WITH A GPW CAUTION LIGHT AND STICK SHAKER. LT AND RT SQUAT SWITCHES REPLACED. AIRCRAFT TEST FLOWN SATISFACTORY.
- [SDR CA020604009](https://openairdocs.org/sdr/CA020604009.md): Door · separated · Jun 2, 2002 · Fokker F28MK1000 · Emergency Exits
  > (CAN) LT EMERGENCY EXIT OPENED UPON LANDING INTO YYC. AIRCRAFT SWAPPED. RECTIFICATION THE OVER WING EXIT WAS INSPECTED WITH NO FAULTS FOUND. OVER CENTER SPRINGS WERE REPLACED AND DOOR WAS RIGGED AS PER THE MAINTENANCE MANUAL. THE FORCE REQUIRED TO OPEN THE D
- [SDR AUS20020804](https://openairdocs.org/sdr/AUS20020804.md): Actuator · leaking · May 16, 2002 · Fokker F28MK1000 · Landing Gear Door Actuator
  > (AUS) RH MAIN LANDING GEAR DOOR AFT ACTUATOR LEAKING INTERNALLY.
- [SDR AUS20020805](https://openairdocs.org/sdr/AUS20020805.md): Indicator · out of adjust · May 15, 2002 · Fokker F28MK1000 · Fuel Quantity Indicator
  > (AUS) FUEL QUANTITY INDICATOR OUT OF CALIBRATION.
- [SDR AUS20020803](https://openairdocs.org/sdr/AUS20020803.md): Sequence Valve · malfunctioned · May 6, 2002 · Fokker F28MK1000 · Landing Gear Retraction/Extension System
  > (AUS) NOSE LANDING GEAR RETRACTION SYSTEM FAULTY. NLG SEQUENCE VALVE ADJUSTED. NLG DOOR SELECTOR VALVE AND NLG DOOR ACTUATOR RESTRICTOR REPLACED.
- [SDR AUS20020802](https://openairdocs.org/sdr/AUS20020802.md): Door · chafed · May 3, 2002 · Fokker F28MK1000 · Landing Gear Doors
  > (AUS) RT NOSE LANDING GEAR DOOR RUBBING ON RT NOSE WHEEL. LT NOSE WHEEL RUBBING ON WHEEL CUTOUT. NOSE WHEEL CENTERING OUT OF ADJUSTMENT.
- [SDR AUS20020801](https://openairdocs.org/sdr/AUS20020801.md): Downlock · contaminated · May 2, 2002 · Fokker F28MK1000 · Landing Gear Retraction/Extension System
  > (AUS) LANDING GEAR DOWNLOCK SWITCH AND DOOR UPLOCK SWITCH CONTAMINATEDWITH DIRT AND GREASE.
- [SDR AUS20020585](https://openairdocs.org/sdr/AUS20020585.md): Blade · damaged · Mar 6, 2002 · Fokker F28MK1000 · Turbine Engine Compressor Section
  > (AUS) NR 1 ENGINE HPC BLADE TRAILING EDGE DAMAGED.
- [SDR AUS20020576](https://openairdocs.org/sdr/AUS20020576.md): A/C Pack · failed · Feb 25, 2002 · Fokker F28MK1000 · Cabin Cooling System
  > (AUS) NR 2 AIR CONDITIONING PACK FAILED. INVESTIGATION COULD FIND NO FAULT.
- [SDR AUS20020575](https://openairdocs.org/sdr/AUS20020575.md): Actuator · faulty · Feb 16, 2002 · Fokker F28MK1000 · Landing Gear Actuator
  > (AUS) RH MAIN LANDING GEAR FAULTY. INVESTIGATION FOUND RH MAIN LANDINGGEAR ACTUATOR SLOW TO RETRACT.
- [SDR AUS20020541](https://openairdocs.org/sdr/AUS20020541.md): Actuator · faulty · Feb 6, 2002 · Fokker F28MK1000 · Landing Gear Retraction/Extension System
  > (AUS) RH MAIN LANDING GEAR DOWNLOCK ACTUATOR FAULTY.
- [SDR AUS20020539](https://openairdocs.org/sdr/AUS20020539.md): Fitting · leaking · Feb 5, 2002 · Fokker F28MK1000 · Alternator-Generator Drive
  > (AUS) NO1 ENGINE CONSTANT SPEED DRIVE (CSD) OIL PRESSURE FITTINGLEAKING.
- [SDR AUS20020538](https://openairdocs.org/sdr/AUS20020538.md): Diode · faulty · Feb 3, 2002 · Fokker F28MK1000 · Landing Gear Retraction/Extension System
  > (AUS) LANDING GEAR RETRACTION SYSTEM DIODE FAULTY.
- [SDR CA020607017](https://openairdocs.org/sdr/CA020607017.md): Starter · failed · Feb 2, 2002 · Fokker F28MK1000 · APU Start/Ignition System
  > (CAN) THIS APU HAS HAD TWO OCCURRENCES OF THE STARTER DRIVE SHAFT SHEARING. THE AIRCRAFT WAS INSPECTED DURING C CHECK IN REGARDS TO THESE SNAGS WITH NO FAULTS. THE APU STARTER DRIVE TRAIN HAS HAD NO FAULTS SINCE.
- [SDR AUS20020176](https://openairdocs.org/sdr/AUS20020176.md): Accessory Unit · faulty · Jan 26, 2002 · Fokker F28MK1000 · Audio Integrating System
  > (AUS) AUDIO ACCESSORY UNIT FAULTY.
- [SDR AUS20020185](https://openairdocs.org/sdr/AUS20020185.md): Tube · leaking · Jan 15, 2002 · Fokker F28MK1000 · Pneumatic Distribution System
  > (AUS) PNEUMATIC TUBE LEAKING FROM DOWNSTREAM PRESSURE TAPPING.
- [SDR AUS20020179](https://openairdocs.org/sdr/AUS20020179.md): Switch · out of adjust · Jan 7, 2002 · Fokker F28MK1000 · Landing Gear Position and Warning
  > (AUS) RT MAIN LANDING GEAR DOOR FORWARD UPLOCK SWITCH OUT OF ADJUSTMENT.
- [SDR AUS20020186](https://openairdocs.org/sdr/AUS20020186.md): Battery · overheated · Jan 1, 2002 · Fokker F28MK1000 · Battery/Charger System
  > (AUS) FORWARD BATTERY OVERHEATED.
- [SDR CA011218011](https://openairdocs.org/sdr/CA011218011.md): Windshield · cracked · Dec 15, 2001 · Fokker F28MK1000 · Flight Compartment Windows
  > (CAN) ENROUTE CREW NOTED SPARKING AND ARCING IN CAPTAIN'S WINDSHIELD, FOLLOWED BY DELAMINATION AND CRACKING OF GLASS PANE(S). CREW CONTACTED ATC AND REQUESTED DIVERSION TO OTTAWA (YOW) AS CLOSEST ALTERNATE, AND LANDED WITH NO FURTHER INCIDENT. CREW REPORTED
- [SDR CA011217024](https://openairdocs.org/sdr/CA011217024.md): Windshield · cracked · Dec 7, 2001 · Fokker F28MK1000 · Flight Compartment Windows
  > (CAN) SHORTLY AFTER TAKEOFF FROM SASKATOON (YXE), CREW NOTED A "BRIGHT FLASH" IN CAPTAIN'S WINDSHIELD. CREW DE-SELECTED WINDSHIELD HEAT IMMEDIATELY, SHORTLY THEREAFTER CENTRE GLASS PLY CRACKED. NO PRESSURIZATION LOSS WAS REPORTED, & CREW ELECTED TO RETURN YXE
- [SDR AUS20011434](https://openairdocs.org/sdr/AUS20011434.md): Oil Tank · leaking · Nov 29, 2001 · Fokker F28MK1000 · APU Oil System
  > (AUS) APU OIL TANK LEAKING.
- [SDR AUS20011352](https://openairdocs.org/sdr/AUS20011352.md): Landing Gear · out of adjust · Nov 28, 2001 · Fokker F28MK1000 · Landing Gear Retraction/Extension System
  > (AUS) MAIN LANDING GEAR SUSPECT OUT OF ADJUSTMENT.
- [SDR AUS20011353](https://openairdocs.org/sdr/AUS20011353.md): Actuator · faulty · Nov 26, 2001 · Fokker F28MK1000 · Landing Gear Door Actuator
  > (AUS) RT MAIN LANDING GEAR DOOR NOT FULLY RETRACTING DUE TO A FAULTY REAR DOOR ACTUATOR.
- [SDR AUS20011354](https://openairdocs.org/sdr/AUS20011354.md): Uplock · out of adjust · Nov 19, 2001 · Fokker F28MK1000 · Landing Gear Position and Warning
  > (AUS) LT MAIN LANDING GEAR DOOR UPLOCK SUSPECT OUT OF ADJUSTMENT.
- [SDR AUS20011398](https://openairdocs.org/sdr/AUS20011398.md): Warning System · faulty · Nov 13, 2001 · Fokker F28MK1000 · Landing Gear Position and Warning
  > (AUS) RT MAIN LANDING GEAR LIGHT REMAINED ON AFTER GEAR RETRACTION. INVESTIGATION COULD FIND NO POSITIVE CAUSE OF DEFECT.
- [SDR AUS20011397](https://openairdocs.org/sdr/AUS20011397.md): Fire Detector · malfunctioned · Nov 6, 2001 · Fokker F28MK1000 · Fire Detection
  > (AUS) NR 1 ENGINE FIRE WARNING ON STARTUP. FIRE BOTTLES ACTIVATED. INSPECTION COULD FIND NO EVIDENCE OF FIRE. INVESTIGATION FOUND THE ENGINE INNER COWLING FIRE WARNING SENSING ELEMENT FAILED THE INSULATION TEST.
- [SDR AUS20011422](https://openairdocs.org/sdr/AUS20011422.md): Connector · shorted · Oct 28, 2001 · Fokker F28MK1000 · Fire Detection
  > (AUS) NR 1 ENGINE FIRE WARNING PANEL TEST SWITCH CONNECTION SHORT CIRCUITING. FALSE FIRE WARNING RESULTED IN OPERATION OF THE FIRE EXTINGUISHER.
- [SDR AUS20011423](https://openairdocs.org/sdr/AUS20011423.md): Lever · obstructed · Oct 23, 2001 · Fokker F28MK1000 · Landing Gear Selector
  > (AUS) LANDING GEAR LEVER OBSTRUCTED.
- [SDR AUS20011420](https://openairdocs.org/sdr/AUS20011420.md): Pin · missing · Oct 21, 2001 · Fokker F28MK1000 · Engine Controls
  > (AUS) RT ENGINE HP FUEL VALVE RELAY LEVER TO CONTROL ROD CONNECTION BOLT / NUT SPLIT PIN MISSING. NUT WAS LOOSE AND ALMOST SEPARATED FROM BOLT.
- [SDR AUS20011431](https://openairdocs.org/sdr/AUS20011431.md): Line · cracked · Oct 12, 2001 · Fokker F28MK1000 · Pneumatic Indicating System
  > (AUS) PNEUMATIC SYSTEM BACKUP VALVE TO STUB WING SENSE LINE CRACKED AT FLARE.
- [SDR AUS20011429](https://openairdocs.org/sdr/AUS20011429.md): Indicator · faulty · Oct 3, 2001 · Fokker F28MK1000 · DME/TACAN System
  > (AUS) DME SYSTEM FAULTY.
- [SDR CA010921008](https://openairdocs.org/sdr/CA010921008.md): Indicator · false indication · Sep 19, 2001 · Fokker F28MK1000 · Engine Oil Temperature
  > (CAN) AIRCRAFT WAS INVOLVED IN AN INFLIGHT PRECAUTIONARY SHUTDOWN OF ONE ENGINE DUE TO AN INDICATION OF OIL TEMP INDICATION TO RED LINE ENROUTE TO SANDSPIT. THE TROUBLESHOOTING PROVED THAT IT WAS AN INDICATION PROBLEMM ONLY.THE AIRCRAFT WAS RETURNED TO SERVICE
- [SDR AUS20011302](https://openairdocs.org/sdr/AUS20011302.md): Duct · failed · Sep 17, 2001 · Fokker F28MK1000 · Engine Bleed Air System
  > (AUS) APU AIR DUCT RUPTURED IN AREA DOWNSTREAM OF THE APU LOAD CONTROL AIR VALVE.
- [SDR CA011003005](https://openairdocs.org/sdr/CA011003005.md): Control Unit · sticking · Sep 14, 2001 · Fokker F28MK1000 · Stabilizer Control System
  > (CAN) AIRCRAFT REPORTED TO HAVING THE FLIGHT MASTER CAUTION LIGHT ILLUMINATED ALONG WITH BOTH STAB CONTROL CAUTION LIGHTS ON TAKEOFF OUT OF TORONTO (YYZ). THE AIRCRAFT RETURNED TO TORONTO FOR AN UNEVENTFUL LANDING. THE HORIZONTAL STABILIZER CONTROL UNIT WAS RE
- [SDR AUS20011300](https://openairdocs.org/sdr/AUS20011300.md): Pipe · cracked · Sep 10, 2001 · Fokker F28MK1000 · Aileron Control System
  > (AUS) RT AILERON ACTUATOR RETURN PIPE CRACKED AND LEAKING. LOSS OFHYDRAULIC FLUID.
- [SDR AUS20011428](https://openairdocs.org/sdr/AUS20011428.md): Wire · broken · Sep 1, 2001 · Fokker F28MK1000 · Landing Gear Position and Warning
  > (AUS) LANDING GEAR ANTI-RETRACTION SUPPRESSION DIODE WIRE BROKEN OFF AND INSULATION WASHERS BADLY WORN.
- [SDR AUS20011426](https://openairdocs.org/sdr/AUS20011426.md): Bulb · unapproved part · Aug 30, 2001 · Fokker F28MK1000 · Landing Gear Position and Warning
  > (AUS) LT MAIN LANDING GEAR DOWNLIGHT FITTED WITH INCORRECT PART NUMBER BULB. UNAPPROVED PART.
- [SDR AUS20011425](https://openairdocs.org/sdr/AUS20011425.md): Skin · cracked · Aug 29, 2001 · Fokker F28MK1000 · Fuselage Main, Plate/Skin
  > (AUS) FUSELAGE SKIN CRACKED AT THE 12 O'CLOCK POSITION BETWEEN STA 3845 AND STA 4875. CRACK LENGTH APPROXIMATELY 76.2MM (3IN).
- [SDR AUS20011325](https://openairdocs.org/sdr/AUS20011325.md): Fire Loop · faulty · Aug 17, 2001 · Fokker F28MK1000 · Fire Detection
  > (AUS) APU FIRE WARNING SYSTEM LT SENSING ELEMENT FAULTY. FALSE FIRE WARNING RESULTED IN FIRE BOTTLE BEING FIRED.
- [SDR AUS20011415](https://openairdocs.org/sdr/AUS20011415.md): Indicator · stuck · Aug 11, 2001 · Fokker F28MK1000 · Pneumatic Indicating System
  > (AUS) NR 1 HIGH PRESSURE VALVE SWITCH INDICATOR STICKING.
- [SDR AUS20011324](https://openairdocs.org/sdr/AUS20011324.md): Warning System · false activation · Aug 11, 2001 · Fokker F28MK1000 · AC Generator-Alternator
  > (AUS) NR 2 GENERATOR HIGH INLET TEMPERATURE. INVESTIGATION COULD FIND NO CAUSE FOR THE PROBLEM. PLUGS AND CONNECTORS CLEANED.
- [SDR AUS20011416](https://openairdocs.org/sdr/AUS20011416.md): Downlock Switch · intermittent · Aug 8, 2001 · Fokker F28MK1000 · Landing Gear Position and Warning
  > (AUS) NOSE LANDING GEAR DOOR DOWNLOCK MICROSWITCH INTERMITTENT IN OPERATION.
- [SDR AUS20011413](https://openairdocs.org/sdr/AUS20011413.md): Controller · faulty · Aug 4, 2001 · Fokker F28MK1000 · Drag Control System
  > (AUS) LIFT DUMPER BARBER POLE REMAINED ON' AFTER LOCK SWITCH MOVED TO LOCKED POSITION. SUSPECT CAUSED BY FAULTY LIFT DUMPER CONTROL BOX.
- [SDR AUS20011409](https://openairdocs.org/sdr/AUS20011409.md): Pump · malfunctioned · Aug 2, 2001 · Fokker F28MK1000 · Hydraulic Pump (Electric/Engine), Main
  > (AUS) NR 1 ENGINE NR 2 HYDRAULIC SYSTEM PUMP LOW PRESSURE.
- [SDR AUS20010787](https://openairdocs.org/sdr/AUS20010787.md): Boss · out of adj · Jul 24, 2001 · Fokker F28MK1000 · Door Warning System
  > (AUS) SERVICE / EMERGENCY DOOR STRIKER BOSS LOOSE AND MISALIGNED.
- [SDR AUS20010786](https://openairdocs.org/sdr/AUS20010786.md): Reducer · cracked · Jul 22, 2001 · Fokker F28MK1000 · Hydraulic System, Main
  > (AUS) LANDING GEAR HYDRAULIC SYSTEM PRESSURE REDUCER CRACKED. LOSS OF HYDRAULIC FLUID.
- [SDR AUS20010782](https://openairdocs.org/sdr/AUS20010782.md): Drain Valve · stuck · Jul 1, 2001 · Fokker F28MK1000 · Pitot/Static System
  > (AUS) PITOT STATIC SYSTEM DRAIN LINE VALVE STUCK IN OPEN POSITION.
- [SDR AUS20010898](https://openairdocs.org/sdr/AUS20010898.md): Lever · stuck · Jun 21, 2001 · Fokker F28MK1000 · Landing Gear Retraction/Extension System
  > (AUS) LANDING GEAR RETRACTION LEVER STUCK IN DOWN POSITION. CIRCUIT BREAKER L8 POPPED.

Next page: https://openairdocs.org/model/fokker-f-28-mk-1000/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'F28MK1000'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/fokker-f-28-mk-1000/reports

---
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.