# Dornier Luftfahrt DO 328-100

- Type: Aircraft model (FAA registry)
- Registry code: 2996000
- Manufacturer (registry): DORNIER LUFTFAHRT GMBH
- Model: DO 328-100
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 36
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A45NM](https://openairdocs.org/tcds/A45NM) (OpenAirDocs)
- Holder: Deutsche Aircraft GmbH
- Registered aircraft: 3
- Page: https://openairdocs.org/model/dornier-luftfahrt-do-328-100

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.

- [AD 2025-15-05](https://openairdocs.org/ad/2025-15-05): Fuel · Deutsche 328-100 and 328-300. Effective Sep 3, 2025
- [AD 2025-06-08](https://openairdocs.org/ad/2025-06-08): Landing gear · Deutsche 328-100 and 328-300. Effective May 8, 2025
- [AD 2024-19-16](https://openairdocs.org/ad/2024-19-16): Equipment/furnishings · Deutsche 328-100 and 328-300. Effective Nov 26, 2024
- [AD 2023-23-07](https://openairdocs.org/ad/2023-23-07): Flight Controls · Deutsche 328-100 and 328-300. Effective Jan 16, 2024
- [AD 2023-22-07](https://openairdocs.org/ad/2023-22-07): Fuselage · Deutsche 328-100. Effective Dec 26, 2023
- [AD 2022-21-07](https://openairdocs.org/ad/2022-21-07): Placards and markings, Equipment/furnishings · Deutsche 328-100 and 328-300. Effective Dec 15, 2022
- [AD 2020-07-20](https://openairdocs.org/ad/2020-07-20): Time Limits/Maintenance Checks · 328 Support Services 328-100. Effective May 26, 2020
- [AD 2019-24-14](https://openairdocs.org/ad/2019-24-14): Wings · 328 Support Services 328-100. Effective Feb 3, 2020
- [AD 2019-15-03](https://openairdocs.org/ad/2019-15-03): Wings · 328 Support Services 328-100. Effective Sep 19, 2019
- [AD 2018-19-13](https://openairdocs.org/ad/2018-19-13): Stabilizers · 328 Support Services 328-100 and 328-300. Effective Oct 31, 2018
- [AD 2017-21-06](https://openairdocs.org/ad/2017-21-06): Fuel · 328 Support Services 328-100 and 328-300. Effective Dec 20, 2017
- [AD 2014-03-15](https://openairdocs.org/ad/2014-03-15): Placards and Markings; and Doors. · 328 Support Services 328-100 and 328-300. Effective Apr 9, 2014
- [AD 2012-07-03](https://openairdocs.org/ad/2012-07-03): Equipment/Furnishings · 328 Support Services 328-100 and 328-300. Effective May 10, 2012
- [AD 2012-04-06](https://openairdocs.org/ad/2012-04-06): Engine Controls · 328 Support Services 328-100. Effective Apr 4, 2012
- [AD 2012-01-08](https://openairdocs.org/ad/2012-01-08): Flight Controls · 328 Support Services 328-100 and 328-300. Effective Feb 29, 2012
- [AD 2011-18-13](https://openairdocs.org/ad/2011-18-13): Wings · 328 Support Services 328-100 and 328-300. Effective Oct 25, 2011
- [AD 2011-15-07](https://openairdocs.org/ad/2011-15-07): Stabilizers · 328 Support Services 328-100 and 328-300. Effective Aug 22, 2011
- [AD 2010-07-02](https://openairdocs.org/ad/2010-07-02): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 26 more. Effective May 3, 2010
- [AD 2008-17-01 R1](https://openairdocs.org/ad/2008-17-01-R1): Fuel system · 328 Support Services 328-100. Effective Dec 21, 2009
- [AD 2009-18-14](https://openairdocs.org/ad/2009-18-14): Flight controls · 328 Support Services 328-100 and 328-300. Effective Oct 14, 2009
- [AD 2009-10-03](https://openairdocs.org/ad/2009-10-03): Flight controls · 328 Support Services 328-100 and 328-300. Effective May 26, 2009
- [AD 2008-13-23](https://openairdocs.org/ad/2008-13-23): Elevator assembly · 328 Support Services 328-100. Effective Aug 6, 2008
- [AD 2005-13-04](https://openairdocs.org/ad/2005-13-04): Fuselage drain line · 328 Support Services 328-100 and 328-300. Effective Jul 26, 2005
- [AD 2005-13-03](https://openairdocs.org/ad/2005-13-03): Flight control systems · 328 Support Services 328-100 and 328-300. Effective Jul 26, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2004-22-06](https://openairdocs.org/ad/2004-22-06): Metal oxide varistor (MOV) modules · 328 Support Services 328-100 and 328-300. Effective Dec 2, 2004
- [AD 2004-20-15](https://openairdocs.org/ad/2004-20-15): Engine Air Inlet De-icing System · 328 Support Services 328-100. Effective Nov 17, 2004
- [AD 2004-12-14](https://openairdocs.org/ad/2004-12-14): AC power cables · 328 Support Services 328-100. Effective Jul 22, 2004
- [AD 2004-09-17](https://openairdocs.org/ad/2004-09-17): Rudder spirng tab · 328 Support Services 328-100 and 328-300. Effective Jun 9, 2004
- [AD 2004-09-12](https://openairdocs.org/ad/2004-09-12): Passenger seats · 328 Support Services 328-100 and 328-300. Effective Jun 9, 2004
- [AD 2004-06-16](https://openairdocs.org/ad/2004-06-16): Ground spoiler assembly · 328 Support Services 328-100. Effective May 4, 2004
- [AD 2004-03-36](https://openairdocs.org/ad/2004-03-36): Engine control cables · 328 Support Services 328-100. Effective Mar 24, 2004
- [AD 2003-19-03](https://openairdocs.org/ad/2003-19-03): Nose landing gear (NLG) · 328 Support Services 328-100 and 328-300. Effective Oct 27, 2003
- [AD 2003-11-24](https://openairdocs.org/ad/2003-11-24): Upper and lower torsion bars of the rudder tab · 328 Support Services 328-100. Effective Jun 23, 2003
- [AD 2003-05-08](https://openairdocs.org/ad/2003-05-08): Flight Data Recorder (FDR) and Cockpit Voice Recorder (CVR) Impact Switches · 328 Support Services 328-100 and 328-300. Effective Apr 18, 2003
- [AD 2003-03-17](https://openairdocs.org/ad/2003-03-17): Aileron, Elevator, Rudder Trim Tabs, and Rudder Spring Tab Screws · 328 Support Services 328-100 and 328-300. Effective Mar 12, 2003
- [AD 2002-26-21](https://openairdocs.org/ad/2002-26-21): Electrical wire harness · 328 Support Services 328-100 and 328-300. Effective Feb 12, 2003
- [AD 2002-16-16](https://openairdocs.org/ad/2002-16-16): Actuating cartridge on the auxiliary power unit (APU) · 328 Support Services 328-100 and 328-300. Effective Sep 23, 2002
- [AD 2002-16-13](https://openairdocs.org/ad/2002-16-13): Rudder spring tab · 328 Support Services 328-100 and 328-300. Effective Sep 20, 2002
- [AD 2002-03-15](https://openairdocs.org/ad/2002-03-15): Left- and Right-Hand Potentiometer Levers of the Aileron Flight Control System · 328 Support Services 328-100 and 328-300. Effective Mar 27, 2002
- [AD 2002-01-17](https://openairdocs.org/ad/2002-01-17): AC Pump of Main Hydraulic System · 328 Support Services 328-100. Effective Feb 14, 2002
- [AD 2001-26-14](https://openairdocs.org/ad/2001-26-14): Honeywell GP-300 Guidance and Display Controller · 328 Support Services 328-100. Effective Feb 8, 2002
- [AD 2001-15-04](https://openairdocs.org/ad/2001-15-04): Roll Spoiler Actuators · 328 Support Services 328-100. Effective Aug 29, 2001
- [AD 2000-26-09 R1](https://openairdocs.org/ad/2000-26-09-R1): Structural Integrity · 328 Support Services 328-100. Effective Feb 7, 2001
- [AD 2000-24-03 R1](https://openairdocs.org/ad/2000-24-03-R1): Airplane flight manual (AFM) · 328 Support Services 328-100. Effective Jan 8, 2001
- [AD 2000-07-04](https://openairdocs.org/ad/2000-07-04): Flight Idle Backup System · 328 Support Services 328-100. Effective May 16, 2000
- [AD 2000-04-23](https://openairdocs.org/ad/2000-04-23): Rudder Spring Tab · 328 Support Services 328-100 and 328-300. Effective Mar 22, 2000
- [AD 2000-02-08](https://openairdocs.org/ad/2000-02-08): Ground Spoiler Actuator · 328 Support Services 328-100. Effective Mar 2, 2000
- [AD 99-19-16](https://openairdocs.org/ad/99-19-16): AFM - Limitations Section - Ice Protection System · 328 Support Services 328-100. Effective Dec 27, 1999
- [AD 99-23-15](https://openairdocs.org/ad/99-23-15): Flight Attendant Panel 19VE · 328 Support Services 328-100. Effective Dec 17, 1999

Historical (superseded or no longer in force):

- [AD 2024-03-07](https://openairdocs.org/ad/2024-03-07) (historical): Fuel · Deutsche 328-100 and 328-300. Effective Apr 16, 2024
- [AD 2011-01-07](https://openairdocs.org/ad/2011-01-07) (historical): Flight controls · 328 Support Services 328-100 and 328-300. Effective Feb 9, 2011
- [AD 2009-21-06](https://openairdocs.org/ad/2009-21-06) (historical): Equipment/furnishings. · 328 Support Services 328-100 and 328-300. Effective Nov 20, 2009
- [AD 2009-06-09](https://openairdocs.org/ad/2009-06-09) (historical): MLG (main landing gear) · 328 Support Services 328-100. Effective Apr 28, 2009
- [AD 2008-17-01](https://openairdocs.org/ad/2008-17-01) (historical): Fuel pumps · 328 Support Services 328-100. Effective Sep 17, 2008
- [AD 2008-14-16](https://openairdocs.org/ad/2008-14-16) (historical): Passenger door · 328 Support Services 328-100 and 328-300. Effective Aug 21, 2008
- [AD 2008-10-51](https://openairdocs.org/ad/2008-10-51) (historical): Rear trailing edge · 328 Support Services 328-100 and 328-300. Effective Jun 3, 2008
- [AD 2006-22-05](https://openairdocs.org/ad/2006-22-05) (historical): Integrated navigation units (INUs) · 328 Support Services 328-100, 328-300, Jetstream Model 4101 and 27 more. Effective Dec 1, 2006
- [AD 2005-13-24](https://openairdocs.org/ad/2005-13-24) (historical): Environmental control system · 328-100. Effective Jul 29, 2005
- [AD 2004-09-16](https://openairdocs.org/ad/2004-09-16) (historical): Rudder spring tab lever · 328-100 and 328-300. Effective Jun 9, 2004
- [AD 2004-06-01](https://openairdocs.org/ad/2004-06-01) (historical): Main landing gear (MLG) · 328 Support Services 328-100. Effective Apr 28, 2004
- [AD 2000-26-09](https://openairdocs.org/ad/2000-26-09) (historical): Structural Integrity · 328-100. Effective Feb 7, 2001
- [AD 2000-24-03](https://openairdocs.org/ad/2000-24-03) (historical): Hydraulic Lines Pressurization · 328-100. Effective Jan 8, 2001
- [AD 99-22-15](https://openairdocs.org/ad/99-22-15) (historical): Roll Spoiler Actuators · 328-100. Effective Dec 7, 1999
- [AD 98-22-07](https://openairdocs.org/ad/98-22-07) (historical): AFM - Retraction Of Flaps · 328-100. Effective Nov 12, 1998
- [AD 98-04-06](https://openairdocs.org/ad/98-04-06) (historical): Outer Wings For Fuel Leakage Inspection · 328 Support Services 328-100. Effective Feb 25, 1998
- [AD 96-12-13](https://openairdocs.org/ad/96-12-13) (historical): Honeywell GP-300 Guidance And Display Controller · 328-100 and 328-300. Effective Jun 26, 1996
- [AD 95-04-51](https://openairdocs.org/ad/95-04-51) (historical): Engine Air Inlet De-Icing System · 328-100. Effective Apr 6, 1995

All 115: https://openairdocs.org/model/dornier-luftfahrt-do-328-100/ads.md

## Information bulletins (advisory) (3)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021
- [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008

## Registered aircraft (3)

- [N28AY](https://openairdocs.org/aircraft/N28AY): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1994, S/N 3024
- [N645HM](https://openairdocs.org/aircraft/N645HM): [645th Aeronautical Engineering Group (Aesg)](https://openairdocs.org/faa-owner/645TH%20AERONAUTICAL%20ENGINEERING%20GROUP%20(AESG)), [Wright Pat, OH](https://openairdocs.org/faa-place/OH/Wright%20Pat), built 1994, S/N 3013
- [N90YP](https://openairdocs.org/aircraft/N90YP): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), S/N 3044

## NTSB investigations (1)

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 SEA96IA074](https://openairdocs.org/ntsb/SEA96IA074), Mar 31, 1996: Dornier DO 328-100 (N334PH), Eugene, OR, incident, minor damage. Probable cause: delamination of the wing de-icing boot, due to the boot reaching its life limit.

## FAA accident and incident reports (10)

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 20070523012819I](https://openairdocs.org/incident/20070523012819I), May 23, 2007: Dorner DO328100 (N473PS), Santa Ana, CA, Minor damage. (-23) Ground power unit operator failed to completely remove plug from external power receptacle. Upon driving away with ground power unit cord still attached,…
- [Incident 20021022030119I](https://openairdocs.org/incident/20021022030119I), Oct 22, 2002: Dorner DO328100 (N470PS), Pittsburgh, PA, Minor damage. (-23) On 10/22/02 at 1732 EDT during an in-flight medical emergency, jetstream airlines flight 4032 struck a rescue vehicle while taxiing to the gate. Minor…
- [Incident 20020416019069I](https://openairdocs.org/incident/20020416019069I), Apr 16, 2002: Dorner DO328100 (N471PS), Allentown, PA. (-23) Flt 4151 was enroute from elmria "elm" to philadelphia "phl", and was 4 min out of elm, when hyd priority valve closed "cas", at this point crew ref: to…
- [Incident 20020309002979I](https://openairdocs.org/incident/20020309002979I), Mar 9, 2002: Dorner DO328100 (N471PS), Pittsburgh, PA. (-23) On March 9, 2002, psa flight #4173 returned to pit due to an ice protection discrepancy (elevator horn heat, weather conditions dictated not to…
- [Incident 20011212038429I](https://openairdocs.org/incident/20011212038429I), Dec 12, 2001: Dorner DO328100 (N339PH), Omaha, NE, Minor damage. (-23) Air Wisconsin flight 1755 diverted into Omaha, NE because of an egress hatch warning. Contract maintenance found that the left hand emergency exit…
- [Incident 20010105000059I](https://openairdocs.org/incident/20010105000059I), Jan 5, 2001: Dorner DO328100 (N432JS), Pittsburgh, PA. (-23) Psa flight 4018 departed pit on 1-5-01, at 6000 feet the captain noticed the crack in the co-pilots window, reduced cabin pressure and returned to pit.…
- [Incident 19991205035569I](https://openairdocs.org/incident/19991205035569I), Dec 5, 1999: Dorner DO328100 (N432JS), Pittsburgh, PA, Minor damage. (-23) On December 5, 1999, at 2248E, a DO-328, s/n 3045, registered as N432JS operating as vnaa flight 4064, returned to land at pit runway 28L after reporting…
- [Incident 19990707016749I](https://openairdocs.org/incident/19990707016749I), Jul 7, 1999: Dorner DO328100 (N339PH), Denver, CO. As full power was being applied for take-off, the cabin filled with smoke and haze. Captain schulz took the aappropriate action and shutdown both engines and…
- [Incident 19960331044229I](https://openairdocs.org/incident/19960331044229I), Mar 31, 1996: Dorner DO328100 (N334PH), Eugene, OR, Minor damage. (-5)The flight crew reported that as the airplane was climbing between 14,000 feet and 16,000 feet in light icing conditions, they felt a moderate shudder. The…
- [Incident 19951214045299I](https://openairdocs.org/incident/19951214045299I), Dec 14, 1995: Dorner DO328100 (N334PH), Seattle, WA, Minor damage. Lightning strike during approach. Damaged left wing tip. Nav light assembly missing. Burn marks on rivets.

## Service difficulty reports (2,017, newest 50)

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

- [SDR 2026FA0000335](https://openairdocs.org/sdr/2026FA0000335), May 7, 2026: FUEL SYS. LEAKING. 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
- [SDR 2024FA0000267](https://openairdocs.org/sdr/2024FA0000267), Mar 28, 2024: SHEAR PIN. BROKEN. 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 AIRCR
- [SDR CA160203014](https://openairdocs.org/sdr/CA160203014), Jan 28, 2016: ENGINE. MALFUNCTIONED. (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 MOVEMEN
- [SDR J8UR2015FA0000515](https://openairdocs.org/sdr/J8UR2015FA0000515), Oct 28, 2015: ACTUATOR. ACTIVATED. 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
- [SDR CA151019003](https://openairdocs.org/sdr/CA151019003), Oct 15, 2015: WHEEL. FAILED. (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
- [SDR 2014F00085](https://openairdocs.org/sdr/2014F00085), Apr 23, 2014: ALTERNATOR. CRACKED. 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
- [SDR CA140326009](https://openairdocs.org/sdr/CA140326009), Mar 12, 2014: BLADE. DAMAGED. (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 TH
- [SDR CA140225021](https://openairdocs.org/sdr/CA140225021), Feb 20, 2014: RELAY. FAILED. (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 A
- [SDR CA130808004](https://openairdocs.org/sdr/CA130808004), Jul 16, 2013: STATOR. DAMAGED. (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 O
- [SDR CA130212001](https://openairdocs.org/sdr/CA130212001), Jan 24, 2013: ENGINE. POWER LOSS. (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 GRADU
- [SDR CA121228004](https://openairdocs.org/sdr/CA121228004), Nov 16, 2012: FUEL CONTROL. MALFUNCTIONED. (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. EMERGENC
- [SDR CA121119021](https://openairdocs.org/sdr/CA121119021), Nov 12, 2012: GEAR. DAMAGED. (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 
- [SDR XV6A2012110200009](https://openairdocs.org/sdr/XV6A2012110200009), Nov 2, 2012: SKIN PANEL. CRACKED. 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
- [SDR CA121105006](https://openairdocs.org/sdr/CA121105006), Oct 26, 2012: ENGINE. MALFUNCTIONED. (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 INSPECTIO
- [SDR CA120925004](https://openairdocs.org/sdr/CA120925004), Sep 24, 2012: CONTROL UNIT. MALFUNCTIONED. (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 FEATH
- [SDR XV6A201109010013](https://openairdocs.org/sdr/XV6A201109010013), Sep 1, 2011: SHUTOFF VALVE. DEFECTIVE. BLEED SOV FAIL MSG. TIME ON UNIT NOT TRACKED.
- [SDR XV6A2011051300008](https://openairdocs.org/sdr/XV6A2011051300008), May 11, 2011: SHUTTLE VALVE. FAILED. HYD PROXIMITY VALVE CLOSED CAS MESSAGE RECEIVED IN CRUISE FLIGHT (FL220). CREW PERFORMED THE ASSOCIATED QRH CHECKLIST PROCEDURE INCLUDING THE HYD FAILURE LANDIN
- [SDR CA110330008](https://openairdocs.org/sdr/CA110330008), Mar 28, 2011: WHEEL. DAMAGED. (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-
- [SDR CA110331013](https://openairdocs.org/sdr/CA110331013), Mar 24, 2011: COMPUTER. MALFUNCTIONED. (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 FUNCTIO
- [SDR CA100726017](https://openairdocs.org/sdr/CA100726017), Jul 23, 2010: STARTER GEN. FAILED. (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
- [SDR XV6A2010042400006](https://openairdocs.org/sdr/XV6A2010042400006), Apr 24, 2010: LIGHT. INOPERATIVE. LT REAR EMERGENCY EXTERNAL EXIT LIGHT INOP.
- [SDR XV6A2009102800010](https://openairdocs.org/sdr/XV6A2009102800010), Oct 28, 2009: LIGHT. INOPERATIVE. LEFT SIDE EXTERNAL EMERGENCY LIGHTS DO NOT WORK (BOTH EXTERNAL LIGHTS ON THE LEFT SIDE).
- [SDR XV6A2009101400009](https://openairdocs.org/sdr/XV6A2009101400009), Oct 14, 2009: LIGHT. INOPERATIVE. EMERGENCY STRIP FLOOR LIGHTING OUT ROWS 4-7.
- [SDR CA090806012](https://openairdocs.org/sdr/CA090806012), Aug 5, 2009: CONTROL UNIT. MALFUNCTIONED. 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 TH
- [SDR XV6A2009071800009](https://openairdocs.org/sdr/XV6A2009071800009), Jul 18, 2009: BATTERY PACK. DISCHARGED. EMERGENCY EXIT SIGN 8A NOT LIGHTING.
- [SDR CA090701002](https://openairdocs.org/sdr/CA090701002), Jun 28, 2009: PSEU. MALFUNCTIONED. 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 PRES
- [SDR XV6A2009031600005](https://openairdocs.org/sdr/XV6A2009031600005), Mar 16, 2009: BATTERY PACK. DISCHARGED. ON LINE SERVICE CHECK, FOUND 6LK EPSU BATTERY PACK INOP.
- [SDR XV6A2009031000002](https://openairdocs.org/sdr/XV6A2009031000002), Mar 10, 2009: BATTERY PACK. DISCHARGED. 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), Mar 6, 2009: STRUCTURE. CRACKED. REPETITIVE EDDY CURRENT INSPECTION IAW RAS-328-57-3051 AND AD 2008-10-15.
- [SDR XV6A2009020500001](https://openairdocs.org/sdr/XV6A2009020500001), Feb 5, 2009: BATTERY PACK. DISCHARGED. 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), Jan 14, 2009: BATTERY PACK. DISCHARGED. ON PREFLIGHT EMERGENCY ESCAPE PATH LIGHTING INOP FROM SEAT ROW 1 THROUGH 3.
- [SDR CA080924013](https://openairdocs.org/sdr/CA080924013), Sep 22, 2008: ENGINE. FLUCTUATES. (CAN) AT ABOUT 50 METERS FROM THE ARRIVAL GATE, THE ENG PARAMETERS STARTED FLUCTUATING. PILOT SHUTDOWN THE ENG. NO REPORTED DAMAGE. TROUBLESHOOTING IN PROGRESS.
- [SDR XV62008F00000](https://openairdocs.org/sdr/XV62008F00000), Jun 3, 2008: CONTROL CABLE. OBSTRUCTED. 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. REMO
- [SDR CA080207007](https://openairdocs.org/sdr/CA080207007), Jan 30, 2008: ELT. FAILED. (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 J
- [SDR CA080220007](https://openairdocs.org/sdr/CA080220007), Jan 15, 2008: OIL SYSTEM. LOW 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 INVESTIGAT
- [SDR CA071121004](https://openairdocs.org/sdr/CA071121004), Nov 20, 2007: TURBINE. SEIZED. (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. AIRCRAF
- [SDR CA070912009](https://openairdocs.org/sdr/CA070912009), Sep 10, 2007: RMU. FAILED. (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 INITI
- [SDR CA070823011](https://openairdocs.org/sdr/CA070823011), Aug 22, 2007: WINDOW. CRACKED. (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 ZE
- [SDR CA070529004](https://openairdocs.org/sdr/CA070529004), May 7, 2007: BOOT. LOOSE. (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 A
- [SDR CA070725004](https://openairdocs.org/sdr/CA070725004), May 4, 2007: BOOT. LOOSE. (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
- [SDR CA070209016](https://openairdocs.org/sdr/CA070209016), Jan 23, 2007: ENGINE. FAILED. (CAN) DURING CRUISE THE ENGINE CHIP DETECTOR AND LOW OIL PRESSURE WARNINGS ACTIVATED AND THE ENGINE FLAMED OUT IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL D
- [SDR CA061107008](https://openairdocs.org/sdr/CA061107008), Nov 1, 2006: TRIM PANEL. SHORTED. (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
- [SDR S2YA06007](https://openairdocs.org/sdr/S2YA06007), Sep 17, 2006: BRACKET. BROKEN. IMMEDIATELY AFTER TAKEOFF OF FLIGHT 2343, THE RT GROUND SPOILER DEPLOYED. THE CREW DECLARED AN EMERGENCY AND IMMEDIATELY RETURNED TO DEPARTURE. OUTSTATION MX FO
- [SDR CA060906022](https://openairdocs.org/sdr/CA060906022), Sep 7, 2006: SEAL. LEAKING. (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 DEP
- [SDR CA060822004](https://openairdocs.org/sdr/CA060822004), Jul 27, 2006: INTAKE. DAMAGED. (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
- [SDR CA060831006](https://openairdocs.org/sdr/CA060831006), Jul 7, 2006: HYDRAULIC SYSTEM. FAILED. (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 FEA
- [SDR R019617](https://openairdocs.org/sdr/R019617), Apr 15, 2006: BEARING. CORRODED. 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 - PRO
- [SDR 2006F00009](https://openairdocs.org/sdr/2006F00009), Jan 26, 2006: LUG. CRACKED. WILL PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.
- [SDR 2006F00008](https://openairdocs.org/sdr/2006F00008), Jan 26, 2006: LUG. CRACKED. WHILE PERFORMING ASB-328-27-036, FOUND SPRING TAB LEVER LUG CRACKED/BROKEN.
- [SDR CA051223016](https://openairdocs.org/sdr/CA051223016), Nov 8, 2005: BOOT. SPLIT. 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 FLIGH

All 2,017: https://openairdocs.org/model/dornier-luftfahrt-do-328-100/reports.md

## STCs that may be installed (OpenAirDocs) (31)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST12070MC](https://openairdocs.org/stc/ST12070MC): Installation of non-essential, not required communications equipment. Sierra Nevada Company LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST00069MC](https://openairdocs.org/stc/ST00069MC): Installation of barriers for various cabin configurations and non-required communications equipment. 3S Certification LLC
- [STC ST00120MC](https://openairdocs.org/stc/ST00120MC): Installation of multiple mission configuration options, including power and mission equipment racks, non-required communications equipment, mission power distribution system, antennas, optional operator console, and provisions for sponsons with the carriage of external stores. Sierra Nevada Corporation
- [STC ST02389AK](https://openairdocs.org/stc/ST02389AK): Installation of a Max-Viz EVS-1500 System and associated hardware. Sierra Nevada Corporation
- [STC ST03911AT](https://openairdocs.org/stc/ST03911AT): Installation of a Honeywell MK V Enhanced Ground Proximity Warning System (EGPWS). Woven Electronics LLC
- [STC ST04508NY](https://openairdocs.org/stc/ST04508NY): Installation of ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST03654NY](https://openairdocs.org/stc/ST03654NY): Installation of Control Horn Anti-Icers. SMR Technologies Inc
- [STC ST00361BO](https://openairdocs.org/stc/ST00361BO): Installation of a Honeywell Primus II (XS-852) ADS-B Out System. Pro Star Aviation, LLC
- [STC ST00204BO](https://openairdocs.org/stc/ST00204BO): Installation of Honeywell Mark V Enhanced Ground Proximity Warning System (EGPWS) (Master Document List 1 configuration) with optional Runway Awareness Advisory System (RAAS) (Master Document List 2 configuration). Pro Star Aviation, LLC
- [STC ST00134MC](https://openairdocs.org/stc/ST00134MC): Installation of a Trimble TA-24S Global Positioning System Receiver. Sierra Nevada Corporation
- [STC ST11138SC](https://openairdocs.org/stc/ST11138SC): This aircraft employs night vision imaging system (NVIS) lighting that has been certified to ensure the aircraft is compatible with NVG. REB Technologies Inc
- [STC ST01181SE](https://openairdocs.org/stc/ST01181SE): Installation of increased security cockpit door. Cascade Aviation Services Inc
- [STC ST00138MC](https://openairdocs.org/stc/ST00138MC): Installation of a cargo door latch capability from inside the aircraft. Sierra Nevada Corporation
- [STC ST00128MC](https://openairdocs.org/stc/ST00128MC): Establishment of procedures and performance data for operations on unpaved runways. Sierra Nevada Corporation
- [STC ST11118SC](https://openairdocs.org/stc/ST11118SC): Installation of a cargo conversion. STC 338 LLC
- [STC ST00121MC](https://openairdocs.org/stc/ST00121MC): Installation of a Ku Band Satellite Communications System and Radome. Sierra Nevada Corporation
- [STC ST00732DE](https://openairdocs.org/stc/ST00732DE): Replacement of the original equipment nickel cadmium batteries with Concorde Model RG-380E/44LS Lead Acid Batteries in accordance with Concorde Battery Corporation Master Drawing List 5-0353, Revision B, dated September 15, 2011 or later FAA approved revision. Concorde Battery Corporation
- [STC ST02636NY](https://openairdocs.org/stc/ST02636NY): Installation of Self Illuminating Floor Path Marking System. Lufthansa Technik AG
- [STC ST00669CH-D](https://openairdocs.org/stc/ST00669CH-D): Installation of a 19 Passenger Corporate Interior. Duncan Aviation Inc
- [STC ST00125SE](https://openairdocs.org/stc/ST00125SE): Installation of a closet. Composite Solutions Corporation
- [STC ST00249SE](https://openairdocs.org/stc/ST00249SE): Modify aft galley by adding a stowage door NTP to close out an existing compartment. Composite Solutions Corporation
- [STC ST09465AC](https://openairdocs.org/stc/ST09465AC): Modification of the cabin floor to be the same level through out the cabin in accordance with Fairchild Aircraft Report R1530, Revision D, dated April 20, 1999, or later FAA approved revision. AvCraft Aviation LLC
- [STC ST09468AC](https://openairdocs.org/stc/ST09468AC): Installation of a corporate/executive interior in accordance with Fairchild Aircraft Incorporated Engineering Change Package (ECP) 3000, Revision AN, dated 8/26/1999, or later FAA approved revision. AvCraft Aviation LLC
- [STC ST09562AC](https://openairdocs.org/stc/ST09562AC): Installation of an engine inlet mounting enhancement to increase the mounting flange service life in accordance with Fairchild Aircraft Inc. Drawing No. SATA716G0001, Rev. IR dated 05/19/2000, including Engineering Order A-2 dated 07/30/2001, or later FAA approved revision. AvCraft Aviation LLC

## PMA parts (OpenAirDocs) (672, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [858885-3WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162744085620260107202052.0001): Diaphragm-Air. Wencor, LLC · PMA PQ1370NM · Replaces 858885-3 · Oct 30, 2025
- [P-1119](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192534723120250602133044.0001): Seal Assy. Donaldson Company Inc · PMA PQ2432CE · Replaces 3830159-1 · May 23, 2025
- [804-1201, 804-1205, 804-1205-03, 804-1212, 804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167281928920250612143623.0001): miniQAR MKIII. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [650-0100-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165595102420250603134032.0001): Cellular Module, avCM LTE. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1250-32](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146986044420250612143636.0001): avRDC MAX QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [802-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139661189420250603134036.0001): Kit, avCM 4G Adapter. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [21149GK-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134856381320250612143628.0001): Installation Kit, miniQAR / avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [400-21149G-3-305, 400-21149G-3-315, 400-21149G-3-405, 400-21149G-3-415, 400-21149G-3-505, 400-21149G-3-515, 400-21149G-3-605, 400-21149G-3-615, 400-21149G-3-915](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130374777020250603134043.0001): Assy, LRU Adapter (avRDC or MAX). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [650-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113463217920250603134029.0001): Cellular Module (avCM 4G), GSM / GRPS 4G, Quad Band, SMA. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [400-21149G-3-101, 400-21149G-3-103, 400-21149G-3-105, 400-21149G-3-111, 400-21149G-3-113, 400-21149G-3-115, 400-21149G-3-205, 400-21149G-3-215, 400-21149G-3-715, 400-21149G-3-815](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111191309720250603134040.0001): Assy, LRU Adapter (miniQAR MKIII). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1250-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102366187120250612143632.0001): avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [447883LA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160613339920241107175410.0001): Valve, Safety Assy. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 447883 · Nov 5, 2024
- [HEM90002092](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149421933020250310185343.0001): Decal. Hemico Inc. · PMA PQ2145NE · Replaces 90002092 · Oct 18, 2024
- [858888-3WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145665230820250506130831.0001): Plate, Diaphragm Retaining. Wencor, LLC · PMA PQ1370NM · Replaces 858888-3 · Sep 29, 2024
- [858887-4WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128699324620250506130827.0001): Plate, Diaphragm-Backing. Wencor, LLC · PMA PQ1370NM · Replaces 858887-4 · Sep 29, 2024
- [LA01000X200A20B6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171527610320241016174903.0001): O-Ring. LanAir Research and Development Inc · PMA PQ1031NE · Replaces R01000X200A20B6 · Aug 28, 2024
- [LA449039](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160984151920241016174956.0001): Mask Lock. LanAir Research and Development Inc · PMA PQ1031NE · Replaces 449039 · Aug 28, 2024
- [SJ8665 FP-202](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147614833520240919140819.0001): Spinner Dome Boot. 3M Aerospace · PMA PQ04414CE · Modification part · Aug 22, 2024
- [PM-91](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121206677720250709145718.0001): Spinner Mask. PM Research, Inc. · PMA PQ10049NE · Replaces NA · Jul 5, 2024
- [PM-92](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105442012620260625165244.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Replaces NA · May 13, 2024
- [2609161-3AB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143410276820240322151411.0001): Bumper, Heat Shield. Aero Brake & Spares Inc · PMA PQ0694SW · Replaces 2609161-3 · Feb 1, 2024
- [3163811-7WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130649611620240919140158.0001): Valve - Poppet. Wencor, LLC · PMA PQ1370NM · Replaces 3163811-7 · Jan 30, 2024
- [MDL-0215-00-9302](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194538776520240308150032.0001): Sensor Test Bed. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL-20 15 00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159487561420240308150027.0001): Max-Viz EVS-1500 System. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL-0282-0201-0006](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131787753520240308150030.0001): Installation of a Global Positioning System Receiver. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL-0215-00-9370](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117505500520240308150033.0001): Ku Antenna. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL 0259-0200-0017](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111591784420240308150032.0001): Portals and Provisions. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL 0703-0201-1005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105965560820240308150032.0001): Secure HF Provision. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL-0703-00-9304](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105165812620240308150030.0001): Handles and Placards for Cargo Door Close Modification. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL 0703-00-9334](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103633755820240308150030.0001): ADS-B Disable. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Jan 22, 2024
- [MDL-0215-00-9370](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192086859120240123183206.0001): Ku Antenna. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023
- [MDL 0259-0200-0017](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171498982020240123183206.0001): Portals and Provisions. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023
- [MDL-0215-00-9302](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165985168020240123183206.0001): Sensor Test Bed. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023
- [MDL-0703-00-9304](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156600778120240123183203.0001): Handles and Placards for Cargo Door Close Modification. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023
- [MDL-20 15 00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144835269620240123183201.0001): Max-Viz EVS-1500 System. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023
- [MDL-0282-0201-0006](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140404825920240123183203.0001): Installation of a Global Positioning System Receiver. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023
- [MDL 0703-00-9334](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130213734720240123183204.0001): ADS-B Disable. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023
- [MDL 0703-0201-1005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102282504220240123183205.0001): Secure HF Provision. Sierra Nevada Company LLC · PMA PQ5217NM · Modification part · Dec 20, 2023
- [804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154905343020240924135407.0001): miniQAR MKIII. Avionica LLC. · PMA pq1734ce · Modification part · Dec 8, 2023
- [AAP- 117088](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125776964920230831200746.0001): Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Honeywell P/N 117088 · Aug 28, 2023
- [8-674-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199559081020221122120939.0001): Proximity Sensor Assy. Eldec Corporation · PMA PQ0079NM · Replaces 8-674-01 · Nov 16, 2022
- [8-697-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190635136020221122120940.0001): Proximity Sensor. Eldec Corporation · PMA PQ0079NM · Replaces 8-697-01 · Nov 16, 2022
- [8-700-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186401803720221122120942.0001): PSEU Assy. Eldec Corporation · PMA PQ0079NM · Replaces 8-700-05 · Nov 16, 2022
- [8-700-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172986885920221122120941.0001): PSEU Assy. Eldec Corporation · PMA PQ0079NM · Replaces 8-700-04 · Nov 16, 2022
- [04-1504-1429](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187988917920230315214606.0001): Power Supply. Goodrich Corporation · PMA PQ1352NM · Replaces 04-1504-1429 · Sep 28, 2022
- [02-3601-8021](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178093430020230315214548.0001): Cable Nav Lt LH. Goodrich Corporation · PMA PQ1352NM · Replaces 02-3601-8021 · Sep 28, 2022
- [03-2100-2004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161345687220230315214602.0001): Nav Light. Goodrich Corporation · PMA PQ1352NM · Replaces 03-2100-2004 · Sep 28, 2022
- [03-2103-2003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149261351520230315214603.0001): Nav Light RH. Goodrich Corporation · PMA PQ1352NM · Replaces 03-2103-2003 · Sep 28, 2022
- [04-1604-1429](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140837259020230315214608.0001): Power Supply. Goodrich Corporation · PMA PQ1352NM · Replaces 04-1604-1429 · Sep 28, 2022
- [03-1805-2001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132788514720230315214556.0001): Anti Coll- Light. Goodrich Corporation · PMA PQ1352NM · Replaces 03-1805-2001 · Sep 28, 2022

All of them: https://openairdocs.org/model/dornier-luftfahrt-do-328-100/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Dornier Luftfahrt 328-100](https://openairdocs.org/model/dornier-luftfahrt-328-100): 19 registered aircraft, registry code 2996100
- [Fairchild Dornier 328-100](https://openairdocs.org/model/fairchild-dornier-328-100): 4 registered aircraft, registry code 3370603
- [Fairchild Dornier DORNIER 328-100](https://openairdocs.org/model/fairchild-dornier-dornier-328-100): 1 registered aircraft, registry code 3370605

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