# Service difficulty reports: Dornier Luftfahrt DO 328-100

A list on [Dornier Luftfahrt DO 328-100](https://openairdocs.org/model/dornier-luftfahrt-do-328-100.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 41 · 2,017 reports

- [SDR 2026FA0000335](https://openairdocs.org/sdr/2026FA0000335.md): Fuel Sys · leaking · May 7, 2026 · N3016 · Dorner DO328100 · Fuel Storage
  > AFTER COMPLETING SB-328-28-598 FUEL – REPLACEMENT OF BONDING STRAPS INSIDE FUEL TANK ON D328 A/C 3016 DURING HEAVY CHECK, WE EXPERIENCED ADDITIONAL DELAYED FUEL LEAKS. FUEL TANK ACCESS PANELS WERE REMOVED, THE SB WAS ACCOMPLISHED, AND THE FUEL CELLS WERE CLOSE
- [SDR 2024FA0000267](https://openairdocs.org/sdr/2024FA0000267.md): Shear Pin · broken · Mar 28, 2024 · N941EF · Dorner DO328100 · Nose/Tail Landing Gear
  > DURING TAKEOFF ON MARCH 28, 2024, 08:31 UTC FROM EDMO AIRFIELD FOR A MAINTENANCE ACCEPTANCE FLIGHT, THE TOWING LINK OF MSN 3016 (N941EF) DETACHED FROM THE AIRCRAFT (NOSE LANDING GEAR). THE CAUSE CAN ONLY BE A BROKEN SHEAR PIN. THE TOWING LINK AND THE SHEAR PIN
- [SDR CA160203014](https://openairdocs.org/sdr/CA160203014.md): Engine · malfunctioned · Jan 28, 2016 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) ON FOUR SEPARATE OCCASIONS, THE CREW EXPERIENCED A REDUCTION OF TORQUE ON THE RIGHT ENGINE. ON ALL OCCASIONS, THE POWER LEVER WAS FREE TO MOVE BUT MOVEMENT HAD NO EFFECT. THEY ALSO NOTED THAT ON ALL OCCASIONS, THE TORQUE BEGINS TO REDUCE AT LOW OAT AND O
- [SDR J8UR2015FA0000515](https://openairdocs.org/sdr/J8UR2015FA0000515.md): Actuator · activated · Oct 28, 2015 · N307EF · Dorner DO328100 · Stall Warning System
  > AIRCRAFT STICK PUSHER FAILED IN THE RETRACTED POSITION, ELEVATORS BEING HELD IN FULL NOSE DOWN DEFLECTION, AFTER BEING TESTED BY THE AIRCREW ON PREFLIGHT CHECKS. THE FAILURE WAS NOT DISCOVERED UNTIL THE ACFT WAS LINED UP AND CLEARED FOR TAKEOFF FROM RUNWAY 22
- [SDR CA151019003](https://openairdocs.org/sdr/CA151019003.md): Wheel · failed · Oct 15, 2015 · Dorner DO328100 · Wheel/Ski/Float
  > (CAN) WHEEL ASSY INNER HALF WAS FOUND WITH THE BEAD AREA SEPARATED AND TIRE DEFLATED. ALL OTHER TIRES FULLY INFLATED. THE BEAD AREA HAD A DARK CAST TO THE METAL THAT LOOKED LIKE THE POSSIBLE START OF A POSSIBLE CRACK. THIS ASSEMBLY HAD THE LAST NDT COMPLETED J
- [SDR 2014F00085](https://openairdocs.org/sdr/2014F00085.md): Alternator · cracked · Apr 23, 2014 · N577EF · Dorner DO328100 · AC Inverter
  > WHILE CLIMBING THROUGH, FL 140, THE FLIGHT CREW REPORTED LOSS OF OIL PRESSURE ON THE RT ENGINE. THEY IMMEDIATELY FEATHERED THEN SHUTDOWN THE ENGINE AND RETURNED TO THE DEPARTURE AIRPORT. THE MAINTENANCE REPAIR TEAM DISCOVERED THE RT ENGINE'S ALTERNATOR HALVE
- [SDR CA140326009](https://openairdocs.org/sdr/CA140326009.md): Blade · damaged · Mar 12, 2014 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) CUSTOMER REPORTED NOISE FROM RT ENGINE IN TRANSIENT FROM CLIMB TO CRUISE, APPROXIMATELY 15 MINUTES INTO FLIGHT, AND WITH A LOSS OF POWER. PILOT INDUCED THE IFSD FOLLOWED BY ACFT RETURNING TO AIRPORT AND PERFORMED UNEVENTFUL SINGLE ENGINE LANDING. ON GRO
- [SDR CA140225021](https://openairdocs.org/sdr/CA140225021.md): Relay · failed · Feb 20, 2014 · Dorner DO328100 · DC Power Distribution System
  > (CAN) ON DEPARTURE AFTER ROTATION "MC" RT ALT FAIL ILLUMINATED. "MC" WAS AWKNOWLEDGED AND DEPATURE PROCEDURE WAS FOLLOWED AS NORMAL. WHEN SAFE CREW RAN "MC" R ALT FAIL CHECKLIST. TIEING LT ALT CAUSED LT ALT TO FAIL ALSO. IAW QRH AC TIE WAS UNTIED AND LT ALT
- [SDR CA130808004](https://openairdocs.org/sdr/CA130808004.md): Stator · damaged · Jul 16, 2013 · Dorner DO328100 · Turbine Section
  > (CAN) ON A WALK AROUND INSPECTION OF THE DO 328-100 AS LISTED ABOVE, IT WAS NOTED THAT WHILE ROTATING THE NR 2 PROPELLER BY HAND THAT A SLIGHT RUB AND SLOWING OF THE PROP OCCURRED. A BOROSCOPE INSPECTION WAS COMPLETED AND FOUND SLIGHT RUBBING OF THE PT BLADES
- [SDR CA130212001](https://openairdocs.org/sdr/CA130212001.md): Engine · power loss · Jan 24, 2013 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) "DURING REPOSITIONING FLIGHT AFTER MAINTENANCE (NO MAINTENANCE DONE ON THE ENGINE, ABOUT 1.5 HR INTO THE FLIGHT THE ENGINE NR 2 TORQUE AND FUEL FLOW GRADUALLY DROPPED SLOWLY. THE PILOT TRIED MANUAL ECU BUT NO EFFECT. THE ENGINE WAS SHUTDOWN AND THE ACFT
- [SDR CA121228004](https://openairdocs.org/sdr/CA121228004.md): Fuel Control · malfunctioned · Nov 16, 2012 · Dorner DO328100 · Fuel Control/Turbine Engines
  > (CAN) DURING FLIGHT AT FL240, TORQUE FLUCTUATIONS ON TH RT ENGINE WITH A DROP OF APPROXIMATELY 40 OCCURRED. THE ACFT EXPERIENCED A YAW AND ROLL MOMENT. EMERGENCY PROCEDURES WERE FOLLOWED AND THE ACFT RETURNED TO DESTINATION WHERE AN UNEVENTFUL LANDING WAS MA
- [SDR CA121119021](https://openairdocs.org/sdr/CA121119021.md): Gear · damaged · Nov 12, 2012 · Dorner DO328100 · Turbine Engine Reduction Gear
  > (CAN) DURING CLIMB, CREW REPORTED A CHIP DETECTOR INDICATION MESSAGE FOLLOWED BY LOSS OF OIL PRESSURE. THE ENGINE WAS SHUTDOWN AND SECURED BEFORE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED AT THE DEPARTURE AIRPORT. POST FLIGHT INSPECTION FOUND A CR
- [SDR XV6A2012110200009](https://openairdocs.org/sdr/XV6A2012110200009.md): Skin Panel · cracked · Nov 2, 2012 · N330MX · Dorner DO328100 · Wing, Plate/Skin
  > RIGHT LEADING EDGE OUTBOARD (WING RT) LEAKING FUEL. A CRACK IN THE LOWER WING PANEL HAS BEEN FOUND WITH AN APPROX LENGTH OF 30 MM, LOCATED INBOARD RIB 12 AT THE RUN-OUT OF STRINGER 14. REPAIRED CRACK IN RIGHT LEADING EDGE OUTBOARD IAW 328-100-SPR A000104718
- [SDR CA121105006](https://openairdocs.org/sdr/CA121105006.md): Engine · malfunctioned · Oct 26, 2012 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) ON START UP FOR A RE-POSITIONING FLIGHT, THE CAPTAIN WAS ADVISED BY GROUND HANDLERS OF A PROBLEM WITH THE LT ENGINE. THE ENGINE WAS SHUTDOWN AND INSPECTION FOUND THAT A QTY OF OIL FROM ENGINE HAD BEEN LOST. OIL WAS ALSO FOUND IN THE NR 5 BEARING VENT T
- [SDR CA120925004](https://openairdocs.org/sdr/CA120925004.md): Control Unit · malfunctioned · Sep 24, 2012 · Dorner DO328100 · Propeller Controlling System
  > (CAN) DURING GROUND RUN OF THE ENGINES, THE CREWS NOTICED THAT THE LT PROPRELLER WOULD NOT FEATHER WHILE IN GROUND IDLE POSITION EITHER ELECTRICALLY USING FEATHER PUMP, OR MANUALLY USING THE CONDITION LEVERS. BUT THE PROP WOULD FEATHER WHEN POWER LEVERS ARE I
- [SDR XV6A201109010013](https://openairdocs.org/sdr/XV6A201109010013.md): Shutoff Valve · defective · Sep 1, 2011 · N330M · Dorner DO328100 · Pneumatic Distribution System
  > BLEED SOV FAIL MSG. TIME ON UNIT NOT TRACKED.
- [SDR XV6A2011051300008](https://openairdocs.org/sdr/XV6A2011051300008.md): Shuttle Valve · failed · May 11, 2011 · N328MX · Dorner DO328100 · Hydraulic System, Main
  > HYD PROXIMITY VALVE CLOSED CAS MESSAGE RECEIVED IN CRUISE FLIGHT (FL220). CREW PERFORMED THE ASSOCIATED QRH CHECKLIST PROCEDURE INCLUDING THE HYD FAILURE LANDING CHECKLIST. AT INITIAL TOUCHDOWN (FLAPS UP LANDING), ACFT HAD GOOD AERODYNAMIC CONTROL WITH ENGIN
- [SDR CA110330008](https://openairdocs.org/sdr/CA110330008.md): Wheel · damaged · Mar 28, 2011 · Dorner DO328100 · Tire
  > (CAN) LT I/B MAIN WHEEL ASSY WAS REPLACED ON 28-MAR-11 DUE TO A VERY BAD LEAK. THIS MAIN WHEEL ASSYÏ¿½S TIRE PRESSURE WAS ADJUSTED TO THE CORRECT SETTING ON 25-MAR-11 AND WAS THEN FOUND TO HAVE ONLY 40 PSI IN IT 3 DAYS LATER AFTER NO FLYING. THIS WAS VERY CON
- [SDR CA110331013](https://openairdocs.org/sdr/CA110331013.md): Computer · malfunctioned · Mar 24, 2011 · Dorner DO328100 · Flight Management Computing Hardware System
  > (CAN) FLIGHT MANAGEMENT SYSTEM DATA BASE CAUSES THE FMS TO RESET ON APPROACH INTO AIRPORT. MFG ENGINEERS ARE WORKING ON A SOFTWARE FIX. FMS DATA BASE IS FUNCTIONING NORMALLY AT ALL OTHER COMPANY AIRPORTS.
- [SDR CA100726017](https://openairdocs.org/sdr/CA100726017.md): Starter Gen · failed · Jul 23, 2010 · Dorner DO328100 · Starter-Generator
  > (CAN) LT STATER-GENERATOR FAILED PRIOR TO DESCENT. PILOTS FOLLOWED QRH CHECKLIST AND ATTEMPTED TO RESET IT. STARTER-GEN WOULD NOT RESET. REMAINDER OF THE FLIGHT WAS COMPLETED WITH DC-TIE ON. MX TROUBLESHOT THE ISSUE TO A FAILURE OF THE STARTER-GEN. THE START
- [SDR XV6A2010042400006](https://openairdocs.org/sdr/XV6A2010042400006.md): Light · inoperative · Apr 24, 2010 · N330MX · Dorner DO328100 · Emergency Lighting
  > LT REAR EMERGENCY EXTERNAL EXIT LIGHT INOP.
- [SDR XV6A2009102800010](https://openairdocs.org/sdr/XV6A2009102800010.md): Light · inoperative · Oct 28, 2009 · N330MX · Dorner DO328100 · Emergency Lighting
  > LEFT SIDE EXTERNAL EMERGENCY LIGHTS DO NOT WORK (BOTH EXTERNAL LIGHTS ON THE LEFT SIDE).
- [SDR XV6A2009101400009](https://openairdocs.org/sdr/XV6A2009101400009.md): Light · inoperative · Oct 14, 2009 · N329MX · Dorner DO328100 · Emergency Lighting
  > EMERGENCY STRIP FLOOR LIGHTING OUT ROWS 4-7.
- [SDR CA090806012](https://openairdocs.org/sdr/CA090806012.md): Control Unit · malfunctioned · Aug 5, 2009 · Dorner DO328100 · Cabin Cooling System
  > FLIGHT CREW WAS TAXING OUT FOR ITS FIRST FLIGHT OF THE DAY WHEN THEY STARTED TO SMELL SMOKE IN THE COCKPIT. FA INFORMED THE CREW THAT THERE WAS ALSO SMOKE IT THE CABIN. ENGINES WERE SHUTDOWN AND QRH WAS CONSULTED. CREW NOTED THAT SMOKE WAS ELIMINATED ONCE THE
- [SDR XV6A2009071800009](https://openairdocs.org/sdr/XV6A2009071800009.md): Battery Pack · discharged · Jul 18, 2009 · N331VA · Dorner DO328100 · Emergency Lighting
  > EMERGENCY EXIT SIGN 8A NOT LIGHTING.
- [SDR CA090701002](https://openairdocs.org/sdr/CA090701002.md): Pseu · malfunctioned · Jun 28, 2009 · Dorner DO328100 · Hydraulic System, Main
  > ON CLIMB AFTER TAKEOFF, PILOT RECEIVED A CAS MESSAGE "PRIORITY VALVE CLOSED" GEAR AND FLAPS IN-TRANIST STOPPED, HYD PRESSURE CAS MESSAGE HIGH. THEN ALL HYD PRESSURE WAS LOST. PILOT RETURNED TO AIRPORT OF DEPARTURE TO LAND. HAD EMERGENCY CREWS STANDBY FOR P
- [SDR XV6A2009031600005](https://openairdocs.org/sdr/XV6A2009031600005.md): Battery Pack · discharged · Mar 16, 2009 · N331MX · Dorner DO328100 · Emergency Lighting
  > ON LINE SERVICE CHECK, FOUND 6LK EPSU BATTERY PACK INOP.
- [SDR XV6A2009031000002](https://openairdocs.org/sdr/XV6A2009031000002.md): Battery Pack · discharged · Mar 10, 2009 · N329MX · Dorner DO328100 · Emergency Lighting
  > EMERGENCY FLOW LIGHTING INOP BY ROWS 4 THROUGH 6, FOUND ON LINE SERVICE CHECK. EMERGENCY PATH LIGHTING BATTERY PACK FOUND DISCHARGED.
- [SDR XV6A2009030600001](https://openairdocs.org/sdr/XV6A2009030600001.md): Structure · cracked · Mar 6, 2009 · N331MX · Dorner DO328100 · Wing Miscellaneous Structure
  > REPETITIVE EDDY CURRENT INSPECTION IAW RAS-328-57-3051 AND AD 2008-10-15.
- [SDR XV6A2009020500001](https://openairdocs.org/sdr/XV6A2009020500001.md): Battery Pack · discharged · Feb 5, 2009 · N742VA · Dorner DO328100 · Emergency Lighting
  > EMERGENCY EXIT SIGN AT 9-A INOP. REMOVED AND REPLACED EPSU BATTERY AY 6-LK. OPS CHECK GOOD.
- [SDR XV6A](https://openairdocs.org/sdr/XV6A.md): Battery Pack · discharged · Jan 14, 2009 · N328 · Dorner DO328100 · Emergency Lighting
  > ON PREFLIGHT EMERGENCY ESCAPE PATH LIGHTING INOP FROM SEAT ROW 1 THROUGH 3.
- [SDR CA080924013](https://openairdocs.org/sdr/CA080924013.md): Engine · fluctuates · Sep 22, 2008 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) AT ABOUT 50 METERS FROM THE ARRIVAL GATE, THE ENG PARAMETERS STARTED FLUCTUATING. PILOT SHUTDOWN THE ENG. NO REPORTED DAMAGE. TROUBLESHOOTING IN PROGRESS. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.
- [SDR XV62008F00000](https://openairdocs.org/sdr/XV62008F00000.md): Control Cable · obstructed · Jun 3, 2008 · N331MX · Dorner DO328100 · Power Lever
  > R/S POWER LEVER WOULD NOT GO INTO GROUND IDLE AFTER LANDING. FOUND HINGE FROM COCKPIT DOOR INTERFERING WITH CABLES/ PULLEYS TRAVEL AT RT AVIONICS AFT SIDE. REMOVED FOD AS REQUIRED. CABLES/ PULLEYS GROUND RUN SATISFACTORY. A/C APPROVED FOR RTS. (K)
- [SDR CA080207007](https://openairdocs.org/sdr/CA080207007.md): Elt · failed · Jan 30, 2008 · Dorner DO328100 · Emergency Locator Beacon
  > (CAN) NUMEROUS UNCOMMANDED ELT ACTIVATIONS WITH ELT97. HAVE HAD ACTIVATIONS WITH THE AC INFLIGHT AND PARKED ON THE APRON. THE LASTEST WAS WITH ELT S/N-4584 ON JANUARY 30, 2008. THE AC HAD BEEN PARKED ON THE APRON FOR ROUGHLY 2 HOURS WHEN THE ELT SIGNAL WAS D
- [SDR CA080220007](https://openairdocs.org/sdr/CA080220007.md): Oil System · low pressure · Jan 15, 2008 · Dorner DO328100 · Engine Oil Pressure
  > (CAN) DURING CRUISE, THE OIL PRESSURE WAS NOTED TO DROP. THE CREW SHUTDOWN THE ENGINE AND PERFORMED A SINGLE ENGINE LANDING. ENGINE IS BEING SENT FOR INVESTIGATION. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED (TC NR 200
- [SDR CA071121004](https://openairdocs.org/sdr/CA071121004.md): Turbine · seized · Nov 20, 2007 · Dorner DO328100 · Cabin Cooling System
  > (CAN) AIRCRAFT DEVELOPED WHITE SMOKE IN CABIN WHILE TAXING FOR TAKEOFF. PILOTS NOTICED A CAS LT PACK FAIL LIGHT AND AN AFT LAV SMOKE DETECT CAS MESSAGE. AIRCRAFT RETURNED TO BLOCKS AND PASSENGERS DEBOARDED. CAUSE OF SMOKE WAS TURBINE SEIZED CAUSING A LT PACK O
- [SDR CA070912009](https://openairdocs.org/sdr/CA070912009.md): Rmu · failed · Sep 10, 2007 · Dorner DO328100 · Flight Management Computing Hardware System
  > (CAN) ENROUTE RMU NR1 FAIL CAS MESSAGE, QRH PROCEDURES COMPLETED, THE ODOR OF ELECTRICAL FIRE/SMOKE WAS DETECTED IN THE COCKPIT. DECLARED AN EMERGENCY AND INITIATED ODOR OF SMOKE IN COCKPIT DRILL. PROCEEDED WITHOUT FURTHER INCIDENT.PAX DEPLANED AT GATE,NORM
- [SDR CA070823011](https://openairdocs.org/sdr/CA070823011.md): Window · cracked · Aug 22, 2007 · Dorner DO328100 · Flight Compartment Windows
  > (CAN) ENROUTE AT FLIGHT LEVEL 27,000 THE PILOTS LT SIDE WINDOW CRACKED WITH A LOUD POP. INITIATED DESCENT TO 8,000 FEET AND MANUALLY RAISED CABIN PRESSURE TO ZERO DIFFERENTIAL PRESSURE AND CONTINUED. ADVISED COMPANY OF THE FAILURE PRIOR TO ARRIVAL. AN ENGIN
- [SDR CA070529004](https://openairdocs.org/sdr/CA070529004.md): Boot · loose · May 7, 2007 · Dorner DO328100 · Airfoil Anti/De-ice System
  > (CAN) PILOTS REPORTED LT HORIZONTAL STAB DE-ICE BOOT APPEARS LOOSE. MAINTENANCE INSPECTED THE BOOT AND FOUND THE DE-ICER BOOT HAD COME LOOSE FROM THE AIRCRAFT AT THE AFT EDGES. THE ADHESIVE (3M 1300L) DID NOT SECURE THE DEICER BOOT TO STAB. THE DEICER BOOT WA
- [SDR CA070725004](https://openairdocs.org/sdr/CA070725004.md): Boot · loose · May 4, 2007 · Dorner DO328100 · Airfoil Anti/De-ice System
  > (CAN) PILOTS REPORTED LT HORIZONTAL STAB. DE-ICER BOOT APPEARS LOOSE. MAINTENANCE INSPECTED THE DE-ICER BOOT AND FOUND THE BOOT HAD COME LOOSE FROM THE AIRCRAFT AT THE AFT EDGES. THE ADHESIVE (3M 1300L) DID NOT SECURE THE DE-ICER BOOT TO THE STAB. THE BOOT WA
- [SDR CA070209016](https://openairdocs.org/sdr/CA070209016.md): Engine · failed · Jan 23, 2007 · Dorner DO328100 · Engine (Turbine/Turboprop)
  > (CAN) DURING CRUISE THE ENGINE CHIP DETECTOR AND LOW OIL PRESSURE WARNINGS ACTIVATED AND THE ENGINE FLAMED OUT IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.
- [SDR CA061107008](https://openairdocs.org/sdr/CA061107008.md): Trim Panel · shorted · Nov 1, 2006 · Dorner DO328100 · Flight Compartment Lighting
  > (CAN) ENROUTE THE PILOT REPORTED A STRONG SMELL AND A FLASH OF LIGHT FROM CENTER CONSOLE AREA. THEY TURNED THE INTERIOR DOME LIGHT ON A CONFIRMED THAT A PLASTIC LIGHTING PANEL WAS MELTING ON THE RUDDER LIMITER AND STANDBY ELEVATOR BUTTONS. HE POKED THE SPOT WI
- [SDR S2YA06007](https://openairdocs.org/sdr/S2YA06007.md): Bracket · broken · Sep 17, 2006 · N352SK · Dorner DO328100 · Wing, Attach Fittings
  > IMMEDIATELY AFTER TAKEOFF OF FLIGHT 2343, THE RT GROUND SPOILER DEPLOYED. THE CREW DECLARED AN EMERGENCY AND IMMEDIATELY RETURNED TO DEPARTURE. OUTSTATION MX FOUND THE RT GROUND SPOILER’S ACTUATING BRACKET BROKEN.
- [SDR CA060906022](https://openairdocs.org/sdr/CA060906022.md): Seal · leaking · Sep 7, 2006 · Dorner DO328100 · Turbine Engine Oil System
  > (CAN) FOLLOWING TAKEOFF ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND DECAY TO ZERO. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED A LEAKING ALTERNATOR DRIVE SEAL. (TC NR 20060906022)
- [SDR CA060822004](https://openairdocs.org/sdr/CA060822004.md): Intake · damaged · Jul 27, 2006 · Dorner DO328100 · Engine Air Intake System
  > (CAN) OUR AC WAS ABOUT TO DEPART WHEN DEFECT WAS SPOTTED. DURING A NORMAL PRE-FLIGHT PILOT WALK AROUND OUR PILOT NOTICED A GAP/ ABNORMAL SPACE BETWEEN THE LOWER ENGINE INLET AND THE UPPER MATING COWL. WE GROUNDED THE A/C TO AOG STATUS AND SENT AME`S TO RESCU
- [SDR CA060831006](https://openairdocs.org/sdr/CA060831006.md): Hydraulic System · failed · Jul 7, 2006 · Dorner DO328100 · Propeller Feathering/Reversing
  > (CAN) AIRCRAFT READIED AND RT ENGINE START PARAMETERS NORMAL. RT CONDITION LEVER ADVANCED TO MIN. RT PROP DOES NOT UNFEATHER. RT CONDITION LEVER RETARDED TO FEATHER. RT CONDITION LEVER ADVANCED TO MIN. RT PROP DOES NOT UNFEATHER. MAINTENANCE CALLED TO SI
- [SDR R019617](https://openairdocs.org/sdr/R019617.md): Bearing · corroded · Apr 15, 2006 · Dorner DO328100 · Propeller Blade Section
  > INSTALLED NEW BEARINGS AND FORK AND COMPLIED WITH ALL APPLICABLE SERVICE BULLETINS. PROP WAS DISASSEMBLED FOR SHIPMENT. TSN 14711:35, TSO 2101:09. 1/26/03 - PROP WAS ASSEMBLED AND INSTALLED ON AC302. 4/11/06 - PROP HAS ACCUMULATED 546 HOURS. ALL SIX C-743
- [SDR 2006F00009](https://openairdocs.org/sdr/2006F00009.md): Lug · cracked · Jan 26, 2006 · N462PS · Dorner DO328100 · Empennage Structure
  > WILL PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.
- [SDR 2006F00008](https://openairdocs.org/sdr/2006F00008.md): Lug · cracked · Jan 26, 2006 · N462PS · Dorner DO328100 · Empennage Structure
  > WHILE PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.
- [SDR CA051223016](https://openairdocs.org/sdr/CA051223016.md): Boot · split · Nov 8, 2005 · Dorner DO328100 · Airfoil Anti/De-ice System
  > CREW REPORTED A FAIL INDICATION FOR THE RT HORIZONTAL STAB DEICE BOOT. UPON INSPECTION BY MAINTENANCE THE BOOT HAD A 12 INCH SPLIT AND WAS REPLACED. NO IN FLIGHT HANDLING PROBLEMS WHERE REPORTED.)

Next page: https://openairdocs.org/model/dornier-luftfahrt-do-328-100/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 = 'DO328100'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/dornier-luftfahrt-do-328-100/reports

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