# N340LS: 1995 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 PW119C](https://openairdocs.org/engine/pratt-whitney-canada-pw119c) (registry code 52163)
- 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: 3040
- Year built: 1995
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Experimental, research and development
- Airworthiness date: April 28, 2015
- Certificate issued: June 3, 2013
- Expires: June 30, 2029
- Mode S code: A3BE59
- Registered owner: [US Air Force Special Operations Command](https://openairdocs.org/faa-owner/US%20AIR%20FORCE%20SPECIAL%20OPERATIONS%20COMMAND)
- Location: [Hurlburt Field, FL](https://openairdocs.org/faa-place/FL/Hurlburt%20Field)
- Owner type: Government
- Owner's area on the map: 30.4264° N, 86.7193° W: Placed by OpenAirDocs at the center of ZIP code 32544, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=340LS
- Page: https://openairdocs.org/aircraft/N340LS

From the FAA registry file of October 22, 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): 103 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 PW119C)

- [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 2006-19-06](https://openairdocs.org/ad/2006-19-06): Propeller shaft · Pratt & Whitney Canada PW118, PW118A, PW118B and 14 more. Effective Sep 29, 2006
- [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 122: https://openairdocs.org/aircraft/N340LS/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

None matched to N340LS.

## FAA accident and incident reports (1)

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 20000911029249I](https://openairdocs.org/incident/20000911029249I), Sep 11, 2000: Dorner DO328100 (N340LS), Chicago, IL. (-23)While holding and waiting for take-off clearance at the 27L run up pad, a fire warning (later confirmed false) was indicated in the #2 engine. The warning…

## Service difficulty reports (16)

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 A6WA200230004](https://openairdocs.org/sdr/A6WA200230004), Feb 17, 2002: COOLING FAN. INOPERATIVE. LEFT PACK HEAT OVERHEATED AFTER LANDING AND SMOKE IN CABIN. MAINTENANCE RESET HX GROUND COOLING FAN C/B, OPS CHECK GOOD AT THIS TIME.
- [SDR A6WA200100065](https://openairdocs.org/sdr/A6WA200100065), Nov 27, 2001: SERVICE DOOR. OPEN. OIL SERVICE DOOR ON COWL 422BL OPENED INFLIGHT. MAINTENANCE SECURED DOOR CLOSED. INSPECTED COWL, NO DAMAGE NOTED.
- [SDR 98ZZZM876](https://openairdocs.org/sdr/98ZZZM876), Oct 10, 1998: ALTERNATOR. FAILED. DEN - FLT 427 - APPROX HALFWAY EN ROUTE TO ASE FROM DEN, CREW RECEIVED A LT ALTERNATOR FAIL MESSAGE. CREW CONTACTED MX CONTROL AND ADVISED OF THE SITUATION. CRE
- [SDR 20000428AP006](https://openairdocs.org/sdr/20000428AP006), Jul 15, 1998: INDICATOR. MALFUNCTIONED. FLT 358 - DURING TAKEOFF ROLL, THE FIRST OFFICER NOTICED THAT THERE WAS NO INDICATION FOR THE AUTO FEATHER SYSTEM ON THE ICAS PAGE HE THEN LOOKED ON THE OVER TO
- [SDR 98ZZZX2421](https://openairdocs.org/sdr/98ZZZX2421), Jun 19, 1998: CONNECTOR. DIRTY. DFW/CUU - FLT 445 - AFTER TAKING POSITION ON THE ACTIVE RUNWAY AND PRIOR TO TAKEOFF ROLL, CREW RECEIVED A 'PROXI LOCK FAIL' AND 'PROXI HYD FAIL' EICAS MESSAGE A
- [SDR ASE97009](https://openairdocs.org/sdr/ASE97009), Dec 29, 1997: POWER PACK. INOPERATIVE. DFW-CUU - FLT 455 - UPON ARRIVAL IN CREW, FOUDN THAT LAST ROW OF EMERGENCY LIGHTING HAD BECOME INOPERATIVE. DISCREPANCY WAS DOCUMENTED IN FLT TIME AND MX LOG. C
- [SDR 97ZZZX1116](https://openairdocs.org/sdr/97ZZZX1116), Jan 28, 1997: O-RING. DAMAGED. AFTER TAKEOFF FROM TSY, THE LT ENGINE OIL PRESSURE STARTED FLUCTUATING AND BEGAN DROPPING OFF. THE CAPTAIN DID A PRECAUTIONARY SHUT DOWN AND RETURNED TO TSY AND
- [SDR 96ZZZM1009](https://openairdocs.org/sdr/96ZZZM1009), May 12, 1996: WINDSHIELD. SHATTERED. WHILE EN ROUTE FROM CUU TO DFW, THE FLIGHT CREW HEARD A POPPING SOUND AND THE FIRST OFFICERS FRONT WINDSHIELD, OUTER LAYER SHATTERED. THE AIRCRAFT CONTINUED TO 
- [SDR 96ZZZM882](https://openairdocs.org/sdr/96ZZZM882), May 6, 1996: WINDSHIELD. SHATTERED. WHILE EN ROUTE AT CRUISE ALTITUDE, THE FLIGHT CREW HEARD A POPPING SOUND AND THE LEFT WINDSHIELD OUTER PANE SHATTERED. THE AIRCRAFT CONTINUED INTO DFW WITHOUT F
- [SDR 96ZZZM691](https://openairdocs.org/sdr/96ZZZM691), Feb 18, 1996: WINDSHIELD. DELAMINATED. PILOTS LEFT SIDE WINDSHIELD DELAMINATED SEVERELY IN FLIGHT FROM ASE TO DFW. THE AIRCRAFT LANDED AT DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS THEN FERRIED T
- [SDR 96ZZZM672](https://openairdocs.org/sdr/96ZZZM672), Feb 18, 1996: WINDSHIELD. DELAMINATED. PILOTS LEFT SIDE WINDSHIELD DELAMINATED SEVERELY IN FLIGHT FROM ASE TO DFW. THE AIRCRAFT LANDED AT DFW WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS THEN FERRIED T
- [SDR 96ZZZM279](https://openairdocs.org/sdr/96ZZZM279), Feb 7, 1996: PSEU BOX. FAILED. AFTER DEPARTING DFW EN ROUTE TO ASE, PROXIMITY SYSTEM FAIL LIGHT CAME ON ALONG WITH HYDRAULIC SYSTEM FAIL. PILOT RETURNED TO DFW AND LANDED WITHOUT FURTHER INCI
- [SDR 96ZZZM275](https://openairdocs.org/sdr/96ZZZM275), Feb 3, 1996: UPLOCK. ICED UP. AFTER DEPARTING DFW, THE FLIGHT CREW SELECTED GEAR UP, NEITHER MAIN GEAR WOULD SHOW UP AND LOCKED. THE CREW THEN SELECTED GEAR DOWN WITH NO PROBLEM. THEY THEN R
- [SDR 96ZZZM274](https://openairdocs.org/sdr/96ZZZM274), Feb 3, 1996: UPLOCK. ICED UP. AFTER DEPARTING DFW, THE FLIGHT CREW SELECTED GEAR UP, NEITHER MAIN GEAR WOULD SHOW UP AND LOCKED. THE CREW THEN SELECTED GEAR DOWN WITH NO PROBLEM. THEY THEN R
- [SDR 96ZZZM264](https://openairdocs.org/sdr/96ZZZM264), Jan 18, 1996: TRANSDUCER. FAILED. AIRCRAFT DEPARTED RIL, FLIGHT NR 100, EN ROUTE TO DFW WHEN THE LEFT ENGINE OIL PRESSURE STARTED FLUCTUATING EXCESSIVELY. THE PILOT SHUTDOWN THE LEFT ENGINE AND 
- [SDR 96ZZZX126](https://openairdocs.org/sdr/96ZZZX126), Nov 15, 1995: SENSOR. FAILED. DTW - AIRCRAFT WAS ON DESCENT TO LAND AT DTW WHEN ECU FAIL MESSAGE APPEARED. THE PILOT RESET THE ECU AND IT STAYED ON LINE FOR APPROXIMATELY 4 MINUTES, THEN FAI

## STCs that may be installed (OpenAirDocs) (32)

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 PW119C)

- [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

## Related

- Other Dornier Luftfahrt 328-100 aircraft: https://openairdocs.org/model/dornier-luftfahrt-328-100/aircraft.md
- The Pratt & Whitney Canada PW119C engine: https://openairdocs.org/engine/pratt-whitney-canada-pw119c.md

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