# Service difficulty reports: Dornier DO-228-202

A list on [Dornier DO-228-202](https://openairdocs.org/model/dornier-do-228-202.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 51 reports

- [SDR BIGA20200623002](https://openairdocs.org/sdr/BIGA20200623002.md): Control Box · malfunctioned · Jun 17, 2020 · N255BH · Dorner DO228202 · Fire Detection
  > THE RIGHT FIRE CONTROL BOX FLASHED A FIRE WARNING WHILE IN FLIGHT. TROUBLESHOOTING REVEALED THE BOX WAS FAULTY AND IT WAS REPLACED WITH A SERVICEABLE UNIT. NO FURTHER INDICATIONS WERE OBSERVED.
- [SDR BIGA20200609001](https://openairdocs.org/sdr/BIGA20200609001.md): Restrictor Valve · leaking · Jun 3, 2020 · N257MC · Dorner DO228202 · Landing Gear Retraction/Extension System
  > THE RESTRICTOR VALVE ASSEMBLY (ATTACHED TO THE SHUTTLE VALVE ON THE NOSE LANDING GEAR ACTUATOR) BLEW OUT IT'S BODY SEALING O-RING LEADING TO COMPLETE HYDRAULIC FLUID LOSS AFFECTING STEERING, BRAKING AND FLAP ACUATION. THIS HAPPENED ON TAXI FOR FLIGHT. THE LAND
- [SDR XV6A2016122700004](https://openairdocs.org/sdr/XV6A2016122700004.md): Pump · inoperative · Dec 27, 2016 · N501VA · Dorner DO228202 · Hydraulic Pump (Electric/Engine), Main
  > AFTER STARTING ENGINES AND TURNING HYDRAULICS ON, THERE WAS NO PRESSURE. INSTALLED SERVICEABLE HYDRAULIC POWER PACK ASSY IAW DO228 AMM 29-10-19. FUNCTIONAL AND LEAK CHECKED GOOD. (SUSPECT HYDRAULIC PUMP FAILED INTERNALLY. HYDRAULIC PUMP MOTOR OPS CHECK GOO
- [SDR XV6A2016102500003](https://openairdocs.org/sdr/XV6A2016102500003.md): Control Handle · intermittent · Oct 25, 2016 · N501VA · Dorner DO228202 · Landing Gear Selector
  > AFTER LANDING CHECKLIST WAS COMPLETED, PULLED THE LANDING GEAR HANDLE, DID NOT RESPOND (NO RED BLINKING LIGHT, NO NOISE FROM THE LANDING GEAR EXTENSION), NOTHING HAPPENED. CYCLED IT 3 TIMES WITH NO RESPONSE. THEN FLIPPED HYDRAULIC TO MANUAL, CYCLED GEAR HAND
- [SDR XV6A2016052200002](https://openairdocs.org/sdr/XV6A2016052200002.md): Unknown · odor · May 22, 2016 · N501VA · Dorner DO228202 · Air Distribution System
  > ELECTRICAL "HOT" ODOR NOTED WHILE IN PATTERN. PERFORMED POWER/ON OPS CHECKS OF EXTERNAL POWER, AVIONICS POWER, STATIC INVERTERS, INSTRUMENT PANEL AND COCKPIT LIGHTS, AND PASSENGER INFORMATION LIGHTS. APPLIED HYD POWER, CHECKED COCKPIT HEATERS, EXTENDED AND RE
- [SDR XV6A2016050300001](https://openairdocs.org/sdr/XV6A2016050300001.md): Hose · chafed · May 3, 2016 · N409VA · Dorner DO228202 · Hydraulic System, Main
  > AFTER GEAR EXTENSION NWS, NOSE WHEEL STEERING, BYPASS ANNUNCIATOR ILLUMINATED AND HYDRAULIC PRESSURE INDICATED 0 BAR. AFTER INSPECTION FOUND NWS HYD LINE CHAFED, CAUSING LOSS OF HYDRAULIC PRESSURE. R & R SAID LINE IAW DO-228, AMM 32-20-01. TIMES AND CYCLES O
- [SDR BIGA20160219001](https://openairdocs.org/sdr/BIGA20160219001.md): Fire Warning · false activation · Feb 19, 2016 · N263MC · Dorner DO228202 · Fire Detection
  > AFTER CONFIRMING A BLEED AIR SEAL COUPLING LEAK ON SDR BIGA20160114-001, THE ACFT FIRE DETECTION SYS WAS GND TESTED NORMAL. A TEST FLIGHT WAS REQUESTED, DURING THE FLIGHT THE LT FIRE DETECTION FLICKERED. AGAIN THE SYS WAS TESTED ON THE GND & COULD NOT BE DUP
- [SDR BIGA20160114001](https://openairdocs.org/sdr/BIGA20160114001.md): Seal · worn · Jan 11, 2016 · N263MC · Dorner DO228202 · Pneumatic Distribution System
  > PILOT WAS PERFORMING A NIGHT CURRENCY FLIGHT, AS HE BEGAN HIS FINAL APPROACH THE LT ENG FIRE WARNING CAME ON. THE PILOT PULLED BACK POWER & THE FIRE LIGHT WENT OUT BELOW 40% TORQUE. PUSHING THE POWER UP CAUSED THE LIGHT TO COME BACK ON. THE PILOT LANDED WIT
- [SDR CA151110009](https://openairdocs.org/sdr/CA151110009.md): Wire · burned · Nov 6, 2015 · Dorner DO228202 · Electrical Power System Wiring
  > (CAN) ON START THE RT ENGINE WOULD NOT LITE OFF. ROTATION UNKNOWN. FLIGHT CREW NOTIFIED MAINTENANCE. FLIGHT WAS EVENTUALLY CANCELLED. UPON INVESTIGATION, MAINTENANCE NOTICED THE RCR AND WIRES WELDED AND BURNED.
- [SDR BIGA20150406001](https://openairdocs.org/sdr/BIGA20150406001.md): Control Rod · worn · Apr 6, 2015 · N257MC · Dorner DO228202 · Aileron Control System
  > DURING INSPECTION, THE AILERON CONTROL ROD WAS FOUND TO BE WORN APPROX 15% OF THE THICKNESS. THE ROD WAS WORN FROM THE AILERON GUST LOCK SYS & SEEMS ONLY WEAR ON THE PILOTS OTBD SIDE DUE TO A SLIGHT MISALIGNMENT OF THE GUST LOCK.
- [SDR XV6A2015021600001](https://openairdocs.org/sdr/XV6A2015021600001.md): Bearing · binding · Feb 16, 2015 · N501VA · Dorner DO228202 · Trailing Edge Flaps
  > AFTER LANDING, DURING FLAP RETRACTION, CONTROL WHEEL MOVES RIGHT. DURING INSPECTION, FOUND BOTH INBD AILERON BEARINGS TIGHT. R & R LT AND RT AILERON BEARING ARMS IAW EO-DO228-57-20-2015-01.
- [SDR XV6A2014080500005](https://openairdocs.org/sdr/XV6A2014080500005.md): Motor · failed · Aug 5, 2014 · N501VA · Dorner DO228202 · Hydraulic Pump (Electric/Engine), Main
  > GEAR HANDLE DOWN & NO INDICATION OF ANY HYD PRESS OR GEAR MOVEMENT. RAN QRH & PERFORMED EMER GEAR EXTENSION CHECKLIST. R & R HYD POWER PACK, OPERATIONS CHECKED GOOD. DISCOVERED HYD ELEC MOTOR FAILED ON HYD POWER PACK, ELEC MOTOR SENT FOR OVERHAUL FOR FINDIN
- [SDR XV6A2014072600003](https://openairdocs.org/sdr/XV6A2014072600003.md): Actuator · failed · Jul 26, 2014 · N501VA · Dorner DO228202 · Landing Gear Actuator
  > NO INDICATION OF RT LG DOWN & LOCKED. R & R MLG ACTUATOR, OPS CHECKED GOOD.
- [SDR XV6A2014071500002](https://openairdocs.org/sdr/XV6A2014071500002.md): Engine · warning light · Jul 15, 2014 · N405VA · Dorner DO228202 · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT AT 9500 FT, MASTER WARNING HORN & LIGHT SOUNDED. LT OIL PRESSURE ANNUNCIATOR ILLUMINATED & TORQUE DROPPED. RAN QRH ENG FAILURE CHECKLIST, DECLARED AN EMERGENCY & DIVERTED. REMOVED LT PROPELLER & ENGINE AS AN ASSEMBLY. INSTALLED SERVICE
- [SDR BIGA20140711001](https://openairdocs.org/sdr/BIGA20140711001.md): Wire · broken · Jul 9, 2014 · N263MC · Dorner DO228202 · Electrical Power System Wiring
  > THE LEFT GENERATOR SYSTEM KICKED OFF LINE. AFTER TROUBLESHOOTING THE SYSTEM THE 20 GAUGE "D" WIRE WAS FOUND TO BE BROKEN INSIDE THE SHEATH IN THE ENGINE COMPARTMENT AND WAS ONLY DETECTABLE BY OHM CHECKING THE HARNESS. DURING THE OHM READING CHECKS OF THE GEN
- [SDR XV6A2013112500009](https://openairdocs.org/sdr/XV6A2013112500009.md): Shutoff Valve · stuck · Nov 25, 2013 · N402VA · Dorner DO228202 · Fuel Controlling System
  > LEFT ENGINE FIRE BOTTLE FIRED DUE TO FIRE INDICATION DURING VENT. 1C EMERGENCY EXIT REMOVED FOR POSSIBLE GROUND EVAC. ENGINE VENT WAS DUE TO ABORTED START, LEFT ENGINE HUNG AT 32-33 PERCENT, NO TEMP LIMIT REACHED - 60 SECONDS. DURING TROUBLESHOOTING OF NR 3
- [SDR XV6A2013040600003](https://openairdocs.org/sdr/XV6A2013040600003.md): Uplock · malfunctioned · Apr 6, 2013 · N409VA · Dorner DO228202 · Landing Gear Retraction/Extension System
  > AFTER SELECTING GEAR UP, GEAR INTRANSIT LIGHT ILLUMINATED AND PUMP PRESSURE ZERO. REMOVED AND REPLACED RIGHT MLG UPLOCK IAW DO228 AMM 32-30-10. OPS CHECK GOOD.
- [SDR XV6A2013033000002](https://openairdocs.org/sdr/XV6A2013033000002.md): Fabric · missing · Mar 30, 2013 · N409VA · Dorner DO228202 · Elevator, Plate/Skin
  > UPPER LEFT FABRIC OF ELEVATOR MISSING WAS DETECTED ON POST FLIGHT WALK AROUND. REMOVED AND REPLACED LEFT ELEVATOR IAW DO228 AMM 55-20-00 OPS CHECK GOOD. NOTE: APPROXIMATE TIME SINCE RECOVERING FOR LEFT ELEVATOR 952.3 FLIGHT HOURS.
- [SDR CA120716018](https://openairdocs.org/sdr/CA120716018.md): Skin · separated · Jul 12, 2012 · Dorner DO228202 · Elevator, Plate/Skin
  > (CAN) DEPARTED WHILE LEVELING OFF INTO CRUISE, A BANG WAS HEARD AND FOLLOWED BY A VIBRATION FELT IN THE CONTROLS AND CONTROLLABILITY PROBLEMS. THE CREW DECLARED AN EMERGENCY AND LANDED SAFELY BACK. AFTER LANDING IT WAS DISCOVERED THAT APPROXIMATELY 95 PERCENT
- [SDR XV6A2012052500005](https://openairdocs.org/sdr/XV6A2012052500005.md): Uplock Switch · inoperative · May 25, 2012 · N405VA · Dorner DO228202 · Landing Gear Position and Warning
  > UPON LEAVING BAR 10, PLACED GEAR HANDLE IN UP POSITION, GEAR UNSAFE LIGHT CONTINUED TO FLASH. RAN QRH AND PLACED GEAR IN THE DOWN POSITION, THEN RECYCLED TO THE UP POSITION, GEAR UNSAFE CONTINUED TO FLASH. RETURNED GEAR TO THE DOWN POSITION. AIRCRAFT DIVERT
- [SDR XV6A2012051600004](https://openairdocs.org/sdr/XV6A2012051600004.md): Relay · intermittent · May 16, 2012 · N405VA · Dorner DO228202 · Landing Gear Retraction/Extension System
  > ON FINAL APPROACH AT 1Z1, GEAR DOWN SELECTED AND NO HYDRAULIC PRESSURE INDICATED AND GEAR DID NOT EXTEND. TRIED SEVERAL TIMES TO SWITCH MANUAL "ON" AND IT DID NOT WORK. RETURNED TO VGT AND TRIED SEVERAL TIMES AGAIN TO GET HYDRAULICS TO WORK TO NO AVAIL. FIN
- [SDR XV6A2012051500003](https://openairdocs.org/sdr/XV6A2012051500003.md): Gauge · faulty · May 15, 2012 · N405VA · Dorner DO228202 · Engine Oil Temperature
  > DURING CRUISE, NR 1 OIL TEMP WENT INTO RED LINE. CONTACTED MOC AND PERFORMED PRECAUTIONARY ENGINE SHUT-DOWN (LEFT ENGINE). TROUBLESHOT SYSTEM, VERIFIED OIL TEMP INDICATION INACCURATE. REPLACED OIL TEMP BULB, NO HELP, ORIGINAL TEMP BULB REINSTALLED. ALL WIR
- [SDR CA120516004](https://openairdocs.org/sdr/CA120516004.md): Adapter · failed · May 12, 2012 · Dorner DO228202 · Turbine Engine Oil System
  > (CAN) ON THE 12 OF MAY 0424ZULU, ACFT WAS INBD FOR LANDING WHEN THE CREW REPORTED THEY HAD AN OIL FLUCTUATION FOLLOWED SHORTLY BY A TORQUE FLUCTUATION ON THE RT ENGINE. THE RT ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE AND REQUESTED ARFF VEHICLES ON STAND
- [SDR BIGA201205151202](https://openairdocs.org/sdr/BIGA201205151202.md): Linkage · out of adjust · May 12, 2012 · N266MC · Dorner DO228202 · Propeller Feathering/Reversing
  > THE AIRCRAFT WAS TEST FLOWN FOR NTS SHUTDOWN WHICH REQUIRES THE SHUTDOWN OF THE NR 2 ENGINE IN FLIGHT. THE SPEED LEVER WAS PULLED OVER THE GATE AND INTO THE STOP AND FEATHER POSITION, THE MANUAL FUEL SHUTOFF CUT THE FUEL TO THE ENGINE, BUT THE FEATHER VALVE D
- [SDR XV6A2011102500015](https://openairdocs.org/sdr/XV6A2011102500015.md): Thermocouple · faulty · Oct 25, 2011 · N405VA · Dorner DO228202 · Engine Oil Temperature
  > DURING FLIGHT, NR 1 ENGINE INDICATED HIGH OIL TEMP, IN YELLOW. CREW ACCOMPLISHED QRH AND MADE AN UNSCHEDULED LANDING INTO 1G4. REPLACED LT OIL TEMP INDICATOR WITH REPAIRED INDICATOR, PROBLEM STILL EXISTS. REPLACED LT OIL TEMP BULB WITH NEW BULB. OPS CHECK
- [SDR CA110707005](https://openairdocs.org/sdr/CA110707005.md): Skin · delaminated · Jul 6, 2011 · Dorner DO228202 · Elevator, Plate/Skin
  > ELEVATOR FABRIC DELAMINATED AND SEPARATED FROM STRUCTURE OF CONTROL SURFACE CAUSING AIRFRAME BUFFET AND UNCOMMANDED ELEVATOR OSCILLATIONS.
- [SDR XV6A2010101300012](https://openairdocs.org/sdr/XV6A2010101300012.md): Tire · failed · Oct 12, 2010 · N409VA · Dorner DO228202 · Wheel/Ski/Float
  > FOUND LT AND RT NOSE WHEEL AND TIRE ASSY DAMAGED.
- [SDR CA100908004](https://openairdocs.org/sdr/CA100908004.md): Bearing · broken · Jul 30, 2010 · Dorner DO228202 · Accessory Gearboxes
  > WHILE PULLING THE PROP THROUGH BY HAND AN UNUSUAL NOISE WAS HEARD. FURTHER INVESTIGATION REVEALED AN OIL FILTER BYPASS INDICATION AND METAL PARTICLES IN THE OIL FILTER. ENGINE WAS REMOVED AND FORWARDED FOR INSP AND REPAIR. TEARDOWN SHOWED THAT THE PN 3103585
- [SDR CA100119014](https://openairdocs.org/sdr/CA100119014.md): Roller · damaged · Jan 16, 2010 · Dorner DO228202 · Nose/Tail Landing Gear
  > (CAN) THE NLG FAILED TO RETRACT CORRECTLY, LODGING GEAR LEG LOCKING ROLLER INTO ABOVE SPACE BETWEEN UPLOCK IMPACT LATCH, AND THE UPLOCK HSG (INDICATED BY SCORE MARKS ON THE ROLLER THAT MEASURE PERFECTLY WITH THE UPLOCK LATCH AND UPLOCK HSG). OLEO PRESSURE KEP
- [SDR CA090819003](https://openairdocs.org/sdr/CA090819003.md): Link Assy · broken · Aug 18, 2009 · Dorner DO228202 · Passenger Compartment Equipment
  > CREW CLEANING CABIN BEFORE FLIGHT, IT WAS NOTICED THAT ONE OF THE PASSENGER SEAT BELTS HAD COME LOOSE AT THE ATTACHMENT BRACKET. UPON FURTHER EXAMINATION, IT WAS NOTED THAT PN 31768 LINK ASSY HAD FAILED CAUSING THE SEAT BELT TO DETACH FROM THE SEAT.
- [SDR CA090330004](https://openairdocs.org/sdr/CA090330004.md): Tire · deflated · Mar 29, 2009 · Dorner DO228202 · Tire
  > (CAN) UPON LANDING, THE CREW NOTICED THE ACFT "PULLING" SLIGHTLY TO THE LEFT. THE ACFT TAXIIED IN AND UPON INVESTIGATION BY THE FLIGHT CREW NOTICED THAT THE LT NOSEWHEEL HAD DEFLATED.
- [SDR CA081022006](https://openairdocs.org/sdr/CA081022006.md): Carbon Seal · leaking · Oct 19, 2008 · Dorner DO228202 · Turbine Engine Oil System
  > (CAN) NR 1 ENGINE CREW SHUT DOWN DUE TO STEADY DROP OF OIL PRESSURE AND TORQUE FLUCTUATION, BELIEVED LATER THAT THE REAR CARBON SEAL BEGAN TO LEAK THUS INGESTION OIL IN ENGINE AND BURNT. ENGINE REMOVED FROM ACFT TO BE SENT FOR FURTHER TESTING AT ENGINE SHOP.
- [SDR CA080815001](https://openairdocs.org/sdr/CA080815001.md): Fuel Control · malfunctioned · Aug 11, 2008 · Dorner DO228202 · Fuel Control/Turbine Engines
  > (CAN) ACFT WAS RELEASED TO A SATISFACTORY TEST FLIGHT FOLLOWING NR 1 ENGINE CHANGE. A NTS IN FLIGHT SHUT DOWN WAS TO BE PERFORMED BEFORE ACFT COULD BE RELEASED BACK TO SERVICE. ACFT DEPARTED AND HAD A NORMAL TAKE OFF AND PROCEED WITH NTS SHUT DOWN. PILOT PROC
- [SDR CA080718004](https://openairdocs.org/sdr/CA080718004.md): Potentiometer · malfunctioned · Jul 17, 2008 · Dorner DO228202 · Steering Unit
  > (CAN) ON TAKE OFF ACFT ROTATED PILOT FELT SOMETHING ABNORMAL IN RUDDER PEDALS, SELECTED GEAR UP, GEAR HANDLE WOULD NOT MOVE, PILOT OBSERVED GEAR HANDLE LOCK STILL IN PLACE. ACFT FLOWN BACK TO BASE, PILOT DID A LOW FLYBY WHERE IT WAS CONFIRMED THAT THE NOSE G
- [SDR XV6A200700003](https://openairdocs.org/sdr/XV6A200700003.md): Fire Loop · worn · Nov 16, 2007 · N404VA · Dorner DO228202 · Fire Detection
  > LEFT FIRE HANDLE LIGHT AND MASTER WARNING WENT OFF IN FLIGHT FOR ONE SECOND (TWICE). REMOVED AND REPLACED FIRE WARNING LOOP DETECTOR IAW 26-10-05. LEFT ENGINE FIRE LOOP TEST OPS CHECK GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE.
- [SDR XV6A200700002](https://openairdocs.org/sdr/XV6A200700002.md): Fabric · torn · Sep 24, 2007 · N403VA · Dorner DO228202 · Elevator, Plate/Skin
  > DURING CRUISE FLIGHT, PILOT FELT A BUMP IN THE CONTROL COLUMN. CONTROL COLUMN MOVED UNCOMMANDED FORWARD AND AFT. POWER REDUCTION RESULTED IN NORMAL FLIGHT CHARACTERISTICS. AFTER NORMAL LANDING FOUND LEFT ELEVATOR UPPER SURFACE FABRIC TORN OFF. DURING INVES
- [SDR 2007F00052](https://openairdocs.org/sdr/2007F00052.md): Tach Generator · false indication · Sep 4, 2007 · N403VA · Dorner DO228202 · Engine RPM Indicating System
  > LEFT RPM INDICATION ABNORMAL PERFORMED PRECAUTIONARY SHUTDOWN. INSPECTION FOUND TACH GENERATOR SHAFT BROKEN. REMOVED AND REPLACED TACH GENERATOR IAW AMM 77-11-03. ENGINE GROUND PERFORMANCE RUN C/W AND PASSED. ALL PARAMETERS NORMAL. AIRCRAFT APPROVED FOR R
- [SDR CA080729005](https://openairdocs.org/sdr/CA080729005.md): Motor · intermittent · Jun 20, 2007 · Dorner DO228202 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) UPON SELECTED GEAR DOWN NOTHING HAPPENED. PILOT THEN CYCLED THE GEAR DOWN AGAIN ALL FUNCTION NORMALLY, 3 GREEN DOWN AND LOCKED. ACFT WAS THEN INSPECTED, NO FAULTS FOUND, MAINT CREWS AND EQUIPMENT WERE FLOWN IN AND PUT A/C ON JACKS GEAR SWUNG NO FAULTS AC
- [SDR CA060306020](https://openairdocs.org/sdr/CA060306020.md): Relay · inoperative · Mar 4, 2006 · Dorner DO228202 · Trailing Edge Flap Control System
  > (CAN) ON APROACH FLAPS WERE SELECTED TO THE NR 2 POSITION AND DID NOT RESPOND. SYSTEM TROUBLESHOOTING FOUND THE RELAY TO BE NOT FUNCTIONING. RELAY WAS REPLACED WITH A SERVICABLE UNIT AND FLAPS TESTED NORMAL (TC NR 20060306020)
- [SDR CA051115007](https://openairdocs.org/sdr/CA051115007.md): Engine · unknown · Nov 13, 2005 · Dorner DO228202 · Engine (Turbine/Turboprop)
  > (CAN) RT ENG DID AN UNCOMMANDED INFLIGHT SHUTDOWN. TROUBLESHOOTING IN PROGRESS. WILL UPDATE FURTHER.
- [SDR CA051013008](https://openairdocs.org/sdr/CA051013008.md): Engine · power loss · Oct 12, 2005 · Dorner DO228202 · Engine (Turbine/Turboprop)
  > RT ENGINE WAS REMOVED FOR LOW TORQUE INDICATION AND SENT OUT FOR REPAIR AFTER TESTING PROVED AN INTERNAL PROBLEM. THE ENGINE WAS RE-INSTALLED FROM REPAIR WITH A NEW TORSION SHAFT SN 05P15649 AND TORQUE SENSOR P/N 3101726 AND NTS TEST FLIGHT WAS CARRIED OUT AN
- [SDR CA050622002](https://openairdocs.org/sdr/CA050622002.md): Stringer · corroded · May 20, 2005 · Dorner DO228202 · Fuselage Main, Longeron/Stringer
  > DURING PRE-BUY INSPECTION, THE PURCHASER VISUALLY NOTED THE PRESENCE OF CORROSION ON THE TOP SURFACE OF THIS STRINGER. UPON FURTHER AND LATER INSPECTION, IT WAS DETERMINED TO REQUIRE REPLACEMENT OF THIS STRINGER.
- [SDR CA050419009](https://openairdocs.org/sdr/CA050419009.md): Pulley · binding · Apr 18, 2005 · Dorner DO228202 · Power Lever
  > (CAN) ACFT DEPARTED & RETURNED WITH PRECAUTIONARY ENGINE SHUTDOWN DUE TO JAMMED POWER LEVER. MX ABLE TO DUPLICATE SYMPTOMS. POWER LEVER CIRCUIT INSPECTED & IN RT SIDEWALL AT PULLEY ASSY, A SMALL SCREW NR 4 DIAMETER.375 INCH LONG FOUND IN IMMEDIATE VICINITY.
- [SDR XV62005F00002](https://openairdocs.org/sdr/XV62005F00002.md): Adapter · cracked · Feb 14, 2005 · N405VA · Dorner DO228202 · Turbine Engine Oil System
  > OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200505213) (K)
- [SDR XV62005F00000](https://openairdocs.org/sdr/XV62005F00000.md): Adapter · cracked · Dec 5, 2004 · N403VA · Dorner DO228202 · Turbine Engine Oil System
  > OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200407922)
- [SDR XV62005F00001](https://openairdocs.org/sdr/XV62005F00001.md): Adapter · cracked · Sep 5, 2004 · N405VA · Dorner DO228202 · Turbine Engine Oil System
  > OIL FILTER ADAPTER CRACKED AT MOUNTING PLATE. (WP19200501116)
- [SDR CA040506006](https://openairdocs.org/sdr/CA040506006.md): Squat Switch · intermittent · May 1, 2004 · Dorner DO228202 · Landing Gear Position and Warning
  > AIRCRAFT DEPARTED AND LANDING GEAR WOULD NOT RETRACT. NOSE WEIGHT SWITCH TESTED AND FOUND TO BE INTERMITTENT. PART CHANGED OUR WITH SERVICABLE UNIT
- [SDR 2002F00759](https://openairdocs.org/sdr/2002F00759.md): Rib · cracked · Jul 11, 2002 · N263MC · Dorner DO228202 · Horizontal Stabilizer, Spar/Rib
  > CRACKS FOUND ON RIB NR 12 ON RIGHT SIDE AND RIB NR 13 ON LEFT SIDE. LT RIB CRACKED THROUGH 4 RIVETS HOLES ON TOP SKIN, LENGTH OF CRACK WAS 5 INCHES. RT RIB CRACKED THROUGH 1 RIVET HOLE, LENGTH OF CRACK WAS 2 INCHES. CRACKS WERE FOUND DURING COMPLIANCE WITH
- [SDR CA980421005](https://openairdocs.org/sdr/CA980421005.md): Skin · damaged · Mar 28, 1998 · Dorner DO228202 · Elevator, Plate/Skin
  > (CAN) DURING CRUISE IN STILL AIR, AIRCRAFT STRUCK BY LIGHTNING. IT APPEARS TO HAVE ENTERED VHF COMM ANTENNA ON FORWARD FUSELAGE BELLY. EXIT POINT WAS AT RIGHT ELEVATOR TRAILING EDGE. A SMALL AREA AT EXIT POINT WAS MELTED INTO A BLOB. THE AFT HALF OF THE EL
- [SDR CA960429006](https://openairdocs.org/sdr/CA960429006.md): Brake · not releasing · Apr 4, 1996 · Dorner DO228202 · Trailing Edge Flap Control System
  > (CAN)PART HAD RECENTLY BEEN INSTALLED. INTERMITTENT PROBLEMS OF FLAP CURRENT LIMITER BLOWING FOUND THAT THE ELECTRIC BRAKE ON THE WING TIP BRAKE (SYMNETRY UNIT) WOULD SOMETIMES TAKE UP TO 4 SECONDS TO RELE ASE AFTER THE INITIAL CLICK OF SOLENOID. TEMPERATURE S

Next page: https://openairdocs.org/model/dornier-do-228-202/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 = 'DO228202'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/dornier-do-228-202/reports

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