# N329MX: 1996 Dornier Luftfahrt 328-100

- Status: Valid registration
- Airframe: [Dornier Luftfahrt 328-100](https://openairdocs.org/model/dornier-luftfahrt-328-100) (registry code 2996100, 36 seats)
- Engine: [Pratt & Whitney Canada PW119B](https://openairdocs.org/engine/pratt-whitney-canada-pw119b) (registry code 52133)
- Data sheets: [TCDS A45NM](https://openairdocs.org/tcds/A45NM) (Deutsche Aircraft GmbH), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 3049
- Year built: 1996
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Experimental, research and development
- Airworthiness date: December 10, 2009
- Certificate issued: August 7, 2021
- Expires: August 31, 2028
- Mode S code: A390E8
- Registered owner: [Bay Aeroservices Inc](https://openairdocs.org/faa-owner/BAY%20AEROSERVICES%20INC)
- Location: [Austin, TX](https://openairdocs.org/faa-place/TX/Austin)
- Owner type: Corporation
- Owner's area on the map: 30.2933° N, 97.7661° W: Placed by OpenAirDocs at the center of ZIP code 78703, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=329MX
- Page: https://openairdocs.org/aircraft/N329MX

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 102 in force

### Matched by airframe (Dornier Luftfahrt 328-100)

- [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

### Matched by engine (Pratt & Whitney Canada PW119B)

- [AD 2013-15-08](https://openairdocs.org/ad/2013-15-08): First-stage PT blades · Pratt & Whitney Canada PW118A, PW118B, PW119B and 15 more. Effective Sep 17, 2013
- [AD 2012-26-08](https://openairdocs.org/ad/2012-26-08): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Feb 15, 2013
- [AD 2003-16-04](https://openairdocs.org/ad/2003-16-04): Fuel heaters · Pratt & Whitney Canada PW118, PW118A, PW118B and 19 more. Effective Sep 10, 2003
- [AD 98-14-02](https://openairdocs.org/ad/98-14-02): Fuel Manifold Transfer Tubes · Pratt & Whitney Canada PW118, PW118A, PW118B and 17 more. Effective Aug 31, 1998
- [AD 97-17-05](https://openairdocs.org/ad/97-17-05): Gas Generator Case Drain Ports · Pratt & Whitney Canada PW118, PW118A, PW118B and 17 more. Effective Sep 9, 1997

### 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
- [AD 2012-11-14](https://openairdocs.org/ad/2012-11-14) (historical): Propeller shafts · Pratt & Whitney Canada PW118, PW118A, PW118B and 20 more. Effective Jul 20, 2012

All 121: https://openairdocs.org/aircraft/N329MX/ads.md

## Information bulletins (advisory) (2 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 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
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## 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 DEN00FA063](https://openairdocs.org/ntsb/DEN00FA063), Mar 20, 2000: Dornier 328-100 (N329MX), Denver, CO, substantial damage. Probable cause: uncommanded retraction of the nose and right main landing gears during landing roll for reasons undetermined.

## FAA accident and incident reports (2)

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.

- [Accident 20000320007389A](https://openairdocs.org/incident/20000320007389A), Mar 20, 2000: Dorner DO328100 (N329MX), Denver, CO, No damage. (-23) Upon landing, the right main landing gear collapsed and as the aircraft slowed to a speed that the pilot could no longer control the aircraft direction,…
- [Incident 19980622024639I](https://openairdocs.org/incident/19980622024639I), Jun 22, 1998: N329MX, Denver, CO, Minor damage. Vectored between and unde 2 wx cells. Encountered hail which cracked copilot window, fuselage, props. Returned den.

## Service difficulty reports (13)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR XV6A2009101400009](https://openairdocs.org/sdr/XV6A2009101400009), Oct 14, 2009: LIGHT. INOPERATIVE. EMERGENCY STRIP FLOOR LIGHTING OUT ROWS 4-7.
- [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 A6WA200330009](https://openairdocs.org/sdr/A6WA200330009), Apr 24, 2003: BATTERY. INOPERATIVE. EMERGENCY LIGHT GO DIM AND THEN OUT. REMOVED AND REPLACED BATTERY AS REQUIRED IAW JOB INSTRUCTION CARD. NO FURTHER OCCURRANCES, NO REPEATS, NO TRENDS. SUSPECT L
- [SDR M8XA9800013](https://openairdocs.org/sdr/M8XA9800013), Jun 22, 1998: WINDSHIELD. DEFECTIVE. AIRCRAFT RETURNED TO DEN BECAUSE OF A CRACKED RIGHT FRONT WINDSHIELD AS A RESULT OF ENCOUNTERING A HAIL STORM SHORTLY AFTER TAKEOFF. AIRCRAFT LANDED IN DEN WITH
- [SDR M8XA9800002](https://openairdocs.org/sdr/M8XA9800002), Feb 7, 1998: INDICATION. MALFUNCTIONED. CREW REPORTED THAT THEY RECEIVED NO VISUAL EICAS INDICATION THAT THE GROUND SPOILERS WERE ARMED AFTER THE CONDITION LEVERS WERE ADVANCED TO THE TAKEOFF POSITION
- [SDR M8XA9700019](https://openairdocs.org/sdr/M8XA9700019), Dec 17, 1997: VALVE. DEFECTIVE. EN ROUTE, THE FLIGHT CREW REPORTED A PROBLEM WITH THE EMERGENCY/ PARKING BRAKE ACCUMULATOR PRESSURE INDICATION. THIS IS A REPEAT OF SAME PROBLEM EXPERIENCED EAR
- [SDR M8XA9700018](https://openairdocs.org/sdr/M8XA9700018), Dec 17, 1997: PRESS SWITCH. DEFECTIVE. EN ROUTE, RECEIVED A CAS MESSAGE EMERGENCY/PARKING BRAKE ACCUMULATOR PRESSURE ALERT. DIVERTED TO COS WHERE MX WAS AVAILABLE. ACFT LANDED WITH NO FURTHER INCIDEN
- [SDR M8XA329MXC2](https://openairdocs.org/sdr/M8XA329MXC2), Dec 12, 1997: BUSHING. DEFECTIVE. COS - WHILE ACCOMPLISHING THE LANDING GEAR INSPECTION PORTION OF THE C-CHECK, MAINTENANCE NOTICED THE LEFT MAIN LANDING GEAR AFT TRUNNION BUSHING WAS MIGRATING.
- [SDR M8XA329MXC1](https://openairdocs.org/sdr/M8XA329MXC1), Dec 12, 1997: ACTUATOR. DEFECTIVE. COS - WHILE ACCOMPLISHING THE LANDING GEAR INSPECTION PORTION OF THE C-CHECK, MAINTENANCE NOTICED A SLIGHT AMOUNT OF 'PITTING' ON THE ACTUATOR ROD OF THE LEFT M
- [SDR M8XA9700017](https://openairdocs.org/sdr/M8XA9700017), Oct 30, 1997: WARNING. ACTIVATED. DURING THE TAKEOFF ROLL, THE FLIGHT CREW WAS ALERTED BY A GROUND SPOILERS NOT STOWED CAS MESSAGE. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MX CONDUCTE
- [SDR M8XA970010](https://openairdocs.org/sdr/M8XA970010), Jul 8, 1997: PROBE. DEFECTIVE. EN ROUTE, THE FLIGHT CREW NOTICED THIER WAS NO LOW PRESSURE COMPRESSOR SPEED (NL) INDICATION FOR THE LEFT ENGINE. MAINTENANCE CONTROL ADVISED THE CREW TO DIVERT
- [SDR M8XA970005](https://openairdocs.org/sdr/M8XA970005), Mar 14, 1997: WINDOW. DEFECTIVE. COS - FLT 1125 - FLT 1114 - EN ROUTE FROM DRO TO COS, CREW REPORTED A FAILURE OF THE FIRST OFFICERS DIRECT VISION WINDOW, CREW DESCENDED TO A LOWER ALTITUDE AND
- [SDR M8XA970001](https://openairdocs.org/sdr/M8XA970001), Jan 6, 1997: UPLOCK. MALFUNCTION. FLT 3517 - AIRCRAFT RETURNED TO FIELD AFTER CREW WAS ALERTED TO MLG NOT UP AND LOCKED INDICATION. AIRCRAFT LANDED COS WITHOUT FURTHER INCIDENT. COS MAINTENANCE 

## STCs that may be installed (OpenAirDocs) (40)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Dornier Luftfahrt 328-100)

- [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

### Approved for the engine (Pratt & Whitney Canada PW119B)

- [STC SE2805SO](https://openairdocs.org/stc/SE2805SO): Installation of an oil tank safety cap adapter which is intended to prevent loss of oil in the event of loss or damage to the oil filler cap. Jet Avion Corporation
- [STC SE00344LA](https://openairdocs.org/stc/SE00344LA): Installation of Western Filter Corp. oil filter element, P/N WF334638, as a replacement for the P&W Canada filter element, P/N 3112895-01, in the lubrication system. Western Filter Corporation
- [STC SE00097LA](https://openairdocs.org/stc/SE00097LA): Installation of strainer element, P/N 90220, as a replacement for strainer element, P/N 3106403-01, in the oil pressure transfer tube assembly. Ejay Filtration, Inc
- [STC SE00074LA](https://openairdocs.org/stc/SE00074LA): Installation of Puroflow filter element, P/N 11-11064, as a replacement for P&W Canada filter element, P/N3029315 (and optional numbers) in the reduction gearbox scavenge oil filtering system. Puroflow Corporation
- [STC SE00075LA](https://openairdocs.org/stc/SE00075LA): Installation of Puroflow filter element, P/N 11-11065, as a replacement for P&W Canada filter element, P/N3112895-01, in the reduction gearbox scavenge oil filtering system. Puroflow Corporation
- [STC SE00076LA](https://openairdocs.org/stc/SE00076LA): Installation of Puroflow filter element, P/N 11-11084, as a replacement for P&W Canada filter element, P/N3035681 (and optional part numbers) in the engine fuel filtering system. Puroflow Corporation
- [STC SE00079LA](https://openairdocs.org/stc/SE00079LA): Installation of Puroflow filter element, P/N 11-11085, as a replacement for P&W Canada filter element, P/N3035728 (and optional part numbers) in the engine fuel filtering system. Puroflow Corporation
- [STC SE00082LA](https://openairdocs.org/stc/SE00082LA): Installation of Puroflow filter element, P/N 11-11102, as a replacement for P&W Canada filter element, P/N3038454, in the engine fuel filtering system. Puroflow Corporation
- [STC SE00083LA](https://openairdocs.org/stc/SE00083LA): Installation of Puroflow filter element, P/N 70-106, as a replacement for P&W Canada filter element, P/N3034190, in the reduction gearbox scavenge oil filtering system. Puroflow Corporation

## Related

- Other Dornier Luftfahrt 328-100 aircraft: https://openairdocs.org/model/dornier-luftfahrt-328-100/aircraft.md
- The Pratt & Whitney Canada PW119B engine: https://openairdocs.org/engine/pratt-whitney-canada-pw119b.md

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